Download - Ansys mechanical apdl context sensitive help

Mechanical APDL Context Sensitive Help

Release 15.0ANSYS, Inc.

November 2013Southpointe

275 Technology Drive

Canonsburg, PA 15317 ANSYS, Inc. is

certified to ISO

9001:[email protected]

http://www.ansys.com

(T) 724-746-3304

(F) 724-514-9494

Copyright and Trademark Information

© 2013 SAS IP, Inc. All rights reserved. Unauthorized use, distribution or duplication is prohibited.

ANSYS, ANSYS Workbench, Ansoft, AUTODYN, EKM, Engineering Knowledge Manager, CFX, FLUENT, HFSS and any

and all ANSYS, Inc. brand, product, service and feature names, logos and slogans are registered trademarks or

trademarks of ANSYS, Inc. or its subsidiaries in the United States or other countries. ICEM CFD is a trademark used

by ANSYS, Inc. under license. CFX is a trademark of Sony Corporation in Japan. All other brand, product, service

and feature names or trademarks are the property of their respective owners.

Disclaimer Notice

THIS ANSYS SOFTWARE PRODUCT AND PROGRAM DOCUMENTATION INCLUDE TRADE SECRETS AND ARE CONFID-

ENTIAL AND PROPRIETARY PRODUCTS OF ANSYS, INC., ITS SUBSIDIARIES, OR LICENSORS. The software products

and documentation are furnished by ANSYS, Inc., its subsidiaries, or affiliates under a software license agreement

that contains provisions concerning non-disclosure, copying, length and nature of use, compliance with exporting

laws, warranties, disclaimers, limitations of liability, and remedies, and other provisions. The software products

and documentation may be used, disclosed, transferred, or copied only in accordance with the terms and conditions

of that software license agreement.

ANSYS, Inc. is certified to ISO 9001:2008.

U.S. Government Rights

For U.S. Government users, except as specifically granted by the ANSYS, Inc. software license agreement, the use,

duplication, or disclosure by the United States Government is subject to restrictions stated in the ANSYS, Inc.

software license agreement and FAR 12.212 (for non-DOD licenses).

Third-Party Software

See the legal information in the product help files for the complete Legal Notice for ANSYS proprietary software

and third-party software. If you are unable to access the Legal Notice, please contact ANSYS, Inc.

Published in the U.S.A.

Table of Contents

ANSYS Topic Help .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1

1. No Topics Available .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1

2. ANSYS Home Page .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1

3. Advanced Smart Size Settings .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1

4. Static or Steady-State Analysis ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2

5. Modal Analysis ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2

6. Harmonic Analysis ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2

7. Mode Sup Harmonic Analysis ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2

8. Transient Analysis ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2

9. Full Transient Analysis ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3

10. Substructuring Analysis ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3

11. Spectrum Analysis ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3

12. Arc-Length Options .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3

13. Automatic Fit Mode .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3

14. Boolean Operation Settings .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3

15. CFD Flow Properties ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4

16. ANSYS Help .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4

17. Contour Style .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4

18. Apply Coriolis Effects ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4

19. Table of Cospectral Values vs. Frequencies .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4

20. Damping Specifications .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4

21. Options for DDAM Spectrum ..... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5

22. Device Options .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5

23. Scale DOF Constraints ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5

24. List Binary Files ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5

25. Edge Options .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5

26. Semi Direct Solver Options for Pressure .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5

27. Read Element File ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6

28. ANSYS Help .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6

29. Define Additional Element Table Items .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6

30. Library of Element Types .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6

31. Switch Elem Type .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6

32. Export IGES File ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6

33. Expand Single Solution by Load Step .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7

34. Element Extrusion Options .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7

35. ANSYS File Options .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7

36. Scale Forces .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7

37. ANSYS Help .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7

38. Hidden-Line Options .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7

39. Import IGES File ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8

40. Create Load Case .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8

41. Execute Macro Data Block .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8

42. Element Attributes .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8

43. Meshing Attributes .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8

44. Axes Modification for Graph Plots ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8

45. Mode Combination Methods .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9

46. Curve Modification for Graphs Plots ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9

47. Grid Modifications for Graph Plots ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9

48. Define Material Model ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9

49. Delete Material Properties ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9

iiiRelease 15.0 - © SAS IP, Inc. All rights reserved. - Contains proprietary and confidential information

of ANSYS, Inc. and its subsidiaries and affiliates.

50. Define Nonlinear Material Model ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10

51. List Imported Material ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10

52. ANSYS Help .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10

53. Define Material Model ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10

54. Message Controls ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10

55. Mesher Options .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10

56. Multi-Plotting .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10

57. Multiple Species .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11

58. Read Node File ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11

59. Plot Numbering Controls ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11

60. Expand a Range of Solutions .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11

61. NOTE .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11

62. Viewing Direction .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11

63. Options for Output .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 12

64. Show Status of Output Controls ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 12

65. Data Settings .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 12

66. File Settings .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 12

67. Graph Settings .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 12

68. List Settings .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 12

69. ANSYS Help .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13

70. Contour Element Solution Data .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13

71. Vector Plot of Predefined Vectors ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13

72. List Element Solution .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13

73. FLOTRAN Print Controls ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13

74. List Nodal Solution .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13

75. Fluid Properties ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14

76. Redirects Plots to PSCR .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14

77. Table for PSD vs Frequency .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14

78. Table of Quadspectral Values vs Frequencies .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14

79. Real Constant Set Number 1 for - Resistor ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14

80. Data and File Options .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14

81. References Conditions .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14

82. Rotating Coordinates .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 15

83. Read Results ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 15

84. Radiation Matrix Settings .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 15

85. ANSYS Help .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 15

86. ANSYS Help .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 15

87. ANSYS Help .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 15

88. Size and Shape .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 16

89. Exit from ANSYS .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 16

90. Redirect Plots to GRPH File ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 16

91. Species Conductivity ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 16

92. General Species Data .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 16

93. Steady State Control Settings .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 16

94. ANSYS Help .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 17

95. ANSYS Help .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 17

96. Read Array Parameter Data from File ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 17

97. Setting for Array Parameters Operations .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 17

98. Write Parameters to File ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 17

99. Settings for Single-Point Response Spectrum ..... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 17

100. Symbols ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 18

101. Temperature-dependent Allowable Stresses .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 18

Release 15.0 - © SAS IP, Inc. All rights reserved. - Contains proprietary and confidential informationof ANSYS, Inc. and its subsidiaries and affiliates.iv

Context Sensitive Help

102. Time and Substep Options .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 18

103. Time and Time Step Options .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 18

104. Time Integration Controls ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 18

105. Transient Controls ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 18

106. ANSYS Help .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 19

107. User Defined Mesh .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 19

108. Create Taper Section .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 19

109. ANSYS Help .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 19

110. Write Radiation Matrix To File ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 19

111. Scale Icons Function .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 19

112. Topic Not Found .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20

113. Contour Nodal Solution Data .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20

114. Window Options .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20

115. Radiation Solution Options .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20

116. View Factor Options .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20

117. Line: Copy Divisions .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20

118. Line Flip Bias .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21

119. Animate Over Results ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21

120. Define Global ALE Settings for LS-DYNA Explicit ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21

121. MFS Define .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21

122. MFS Setup .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21

123. MFS Time Control ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21

124. MFS Solution Frequency .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21

125. MFX Solution Control ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 22

126. MFX Time Control ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 22

127. MFX Mapping Operations .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 22

Online Help for ANSYS Dialog Boxes .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 23

1. Pan, Zoom, Rotate .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 23

2. Edit Toolbar/Abbreviations .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 26

3. Hard Copy .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 27

4. PC Hard Copy .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 29

5. Capture Image Feature .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 30

6. Capture Image: Print ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 31

7. Capture Image: Save as .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 32

8. Restore Image .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 33

9. Results Query Picker ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 34

10. Query Solution Data .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 36

11. Array Parameters ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 36

12. Array Parameter Editing: ARRAY Type Arrays .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 37

13. Array Parameter Editing: Table Array .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 39

14. Scalar Parameters ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 40

15. Define Real Constants .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 41

16. Element Types .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 41

17. Offset Working Plane .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 42

18. Working Plane Settings .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 44

19. Define Element Table Data .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 45

20. Define Time-History Variables .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 46

21. Display and Update Nonlinear Convergence Specifications .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 46

22. Solution Controls ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 47

23. MeshTool ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 57

24. Model Query Picker ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 61

25. Contact Wizard .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 63

vRelease 15.0 - © SAS IP, Inc. All rights reserved. - Contains proprietary and confidential information



26. Contact Properties ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 67

27. Define Material Model Behavior ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 78

28. Define Material ID ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 80

29. BeamTool ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 81

30. 2-D and 3-D Annotation .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 86

31. Select Entities: Lines - By Length or by Radius .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 123

32. Select Entities: Elements .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 124

33. Select Entities: By Attributes .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 126

34. Select Entities: Attached to Other Entities ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 128

35. Select Entities: By Location .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 130

36. Select Entities ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 132

37. CrankSlot_Rigid.inp .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 133

38. CrankSlot_flexible.inp .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 141

39. CrankSlot_FlexibleCMS.inp .... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 158

40. Modal Analysis Using WorkBench - Output File ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 176

41. Modal Analysis Using WorkBench - Input File ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 185

Release 15.0 - © SAS IP, Inc. All rights reserved. - Contains proprietary and confidential informationof ANSYS, Inc. and its subsidiaries and affiliates.vi


ANSYS Topic Help

No Topics Available

There are no topics available under this heading at this time.

ANSYS Home Page

The ANSYS Home Page www.ansys.com provides instant access to the latest news and technical inform-

ation available regarding ANSYS, Inc. and the complete line of ANSYS products and services.

When you visit ANSYS Home Page, you will discover a wide range of exciting topics that should prove

to be interesting and informative, no matter what level of experience you have with ANSYS products.

Areas of interest include:

• Descriptions of all ANSYS products.

• Demos that let you try our latest products.

• ANSYS benchmarks consisting of a variety of models created on many different hardware platforms.

• Training information containing course descriptions, dates being held, location and who to contact

for additional information.

• A selection of online documentation.

• ANSYS Support Distributor (ASD) information for your area and how to contact your ASD for additional

information.

• Press releases outlining the newest and most innovative ANSYS product developments and services.

• A customer zone where you can find information about released products, service packs, and new

products.

This list includes only a few of the many items you will find on our home page. Be sure to bookmark

our home page and check back frequently for the latest news and information!

Advanced Smart Size Settings

For information on this topic, select one of the following:

SMRTSIZE

ESIZE

1Release 15.0 - © SAS IP, Inc. All rights reserved. - Contains proprietary and confidential information


http://www.ansys.com

Static or Steady-State Analysis


NLGEOM

NROPT

LUMPM

EQSLV

MSAVE

PIVCHECK

PSTRES

TOFFST

RMRESUME

RMUSE

Modal Analysis


MODOPT

MXPAND

LUMPM

PSTRES

Harmonic Analysis


HROPT

HROUT

LUMPM

Mode Sup Harmonic Analysis


HROPT

HROUT

Transient Analysis


TRNOPT

LUMPM

Release 15.0 - © SAS IP, Inc. All rights reserved. - Contains proprietary and confidential informationof ANSYS, Inc. and its subsidiaries and affiliates.2

ANSYS Topic Help

Full Transient Analysis


NLGEOM

NROPT

EQSLV

TOFFST

Substructuring Analysis


SEOPT

LUMPM

EQSLV

SEGEN

Spectrum Analysis


SPOPT

ANTYPE

Arc-Length Options


ARCLEN

ARCTRM

Automatic Fit Mode


/AUTO

/USER

Boolean Operation Settings


BOPTN

BTOL



Boolean Operation Settings

CFD Flow Properties


FLDATA7

FLDATA8

FLDATA9

FLDATA10

FLDATA11

FLDATA12

ANSYS Help


R command

CIRCU124 in the Element Reference

Coupled-Field Analyses in the Coupled-Field Analysis Guide

Electric Circuit Analysis in the Low-Frequency Electromagnetic Analysis Guide

Contour Style


/CTYPE

/SSCALE

Apply Coriolis Effects


CGLOC

CGOMGA

DCGOMG

Table of Cospectral Values vs. Frequencies


COVAL

PSDFRQ

Damping Specifications


ALPHAD

BETAD

DMPRAT

MDAMP


ANSYS Topic Help

Options for DDAM Spectrum


ADDAM

VDDAM

SED

Device Options


/DEVICE

/SHOW

/DV3D

/UIS

Scale DOF Constraints


DSCALE

DOFSEL

List Binary Files


DUMP

FORM

FILEAUX2

Edge Options


/EDGE

/GLINE

Semi Direct Solver Options for Pressure


FLDATA20

FLDATA20A

FLDATA20B

FLDATA21

FLDATA22

FLDATA23



Semi Direct Solver Options for Pressure

Read Element File


ERRANG

EREAD

ANSYS Help


ESOL

FORCE

SHELL

LAYERP26

Define Additional Element Table Items


AVPRIN

ETABLE

Element Library of the Element Reference

Library of Element Types


ET

Pictorial Summary of the Element Reference

Planning Your Approach of the Modeling and Meshing Guide

Switch Elem Type


ETCHG

Material Models in the ANSYS LS-DYNA User's Guide.

Export IGES File


IGESOUT

/PREP7


ANSYS Topic Help

Expand Single Solution by Load Step


EXPSOL

HREXP

Element Extrusion Options


EXTOPT

TYPE

MAT

REAL

ESYS

ANSYS File Options


/ASSIGN

/FDELE

Scale Forces


FSCALE

DOFSEL

ANSYS Help


HARFRQ

NSUBST

KBC

Hidden-Line Options


/TYPE

/CPLANE

/SHADE

/GRAPHICS



Hidden-Line Options

Import IGES File


IOPTN

IGESIN

/AUX15

Create Load Case


LCDEF

LCFILE

Execute Macro Data Block


*ULIB

*USE

Element Attributes


TYPE

MAT

REAL

ESYS

SECNUM

TSHAP

Meshing Attributes


TYPE

MAT

REAL

ESYS

SECNUM

Axes Modification for Graph Plots


/GRTYP

/XRANGE

/YRANGE


ANSYS Topic Help

/GTHK

/AXLAB

/GROPT

Mode Combination Methods


SRSS

CQC

DSUM

GRP

NRLSUM

Curve Modification for Graphs Plots


/GTHK

/GROPT

/GCOLUMN

/GMARKER

Grid Modifications for Graph Plots


/GTHK

/GROPT

/GRID

Define Material Model


MP

TB

TBDATA

Material Models in the ANSYS LS-DYNA User's Guide

Delete Material Properties


MP

EDMP

Explicit Dynamic Materials



Delete Material Properties

Define Nonlinear Material Model


MP

EDMP


List Imported Material


MPLIST

TBLIST

ANSYS Help


MPREAD

MAT

Define Material Model


MP


Message Controls


/UIS

/NERR

Mesher Options


MOPT

MSHKEY

MSHMID

MSHPATTERN

Multi-Plotting


/GTYPE


ANSYS Topic Help

GPLOT

Multiple Species


MSDATA

KEYOPT

Read Node File


NRRANG

NREAD

Plot Numbering Controls


/PNUM

/NUMBER

Expand a Range of Solutions


NUMEXP

HREXP

NOTE


RESUME

PARRES

*SET

/INPUT

Viewing Direction


/VIEW

/VUP



Viewing Direction

Options for Output


RSYS

ERNORM

AVPRIN

AVRES

/EFACET

SHELL

LAYER

FORCE

Show Status of Output Controls


OUTPR

OUTRES

Data Settings


TIMERANGE

NSTORE

TVAR

File Settings


FILE

NUMVAR

Graph Settings


PLTIME

XVAR

VARNAM

SPREAD

PLCPLX

List Settings


PRTIME


ANSYS Topic Help

NPRINT

VARNAM

LINES

PRCPLX

ANSYS Help


NSOL

ESOL

SOLU

RFORCE

GAPF

Contour Element Solution Data


PLESOL

AVPRIN

Vector Plot of Predefined Vectors


PLVECT

/VSCALE

List Element Solution


PRESOL

FLOTRAN Print Controls


FLDATA5

FLDATA21

List Nodal Solution


PRNSOL

AVPRIN



List Nodal Solution

Fluid Properties


FLDATA12

FLDATA13

Redirects Plots to PSCR


PSCR

/GFILE

/DEVICE

Table for PSD vs Frequency


PSDVAL

PSDFRQ

Table of Quadspectral Values vs Frequencies


QDVAL

PSDFRQ

Real Constant Set Number 1 for - Resistor


R

RMORE

Data and File Options


INRES

FILE

References Conditions


FLDATA14

FLDATA15

FLDATA16


ANSYS Topic Help

FLDATA17

TOFFST

Rotating Coordinates


CGOMGA

CGLOC

Read Results


SET

SUBSET

APPEND

Radiation Matrix Settings


STEF

GEOM

SPACE

ANSYS Help


SFA

STEF

ANSYS Help


SFE

STEF

ANSYS Help


SFL

STEF



ANSYS Help

Size and Shape


/SHRINK

/ESHAPE

/RATIO

/EFACET

/CFORMAT

Exit from ANSYS


/EXIT

FINISH

Redirect Plots to GRPH File


/SHOW

/GFILE

/DEVICE

Species Conductivity


MSPROP

MSVARY

General Species Data


MSSPEC

MSQUAD

MSNOMF

Steady State Control Settings


FLDATA2

FLDATA3

FLDATA5


ANSYS Topic Help

ANSYS Help


TIME

EDINT

EDRST

EDHTIME

EDENERGY

ANSYS Help


*GET

Read Array Parameter Data from File


*VREAD

*TREAD

Setting for Array Parameters Operations


*VCUM

*VABS

*VFACT

*VLEN

*VCOL

*VMASK

Write Parameters to File


*CFOPEN

*VWRITE

Settings for Single-Point Response Spectrum


SVTYP

SED

ROCK



Settings for Single-Point Response Spectrum

Symbols


/PBC

EDFPLOT

/PSF

/PBF

/PSYMB

Temperature-dependent Allowable Stresses


TALLOW

SALLOW

Time and Substep Options


TIME

NSUBST

KBC

AUTOTS

TSRES

Time and Time Step Options


TIME

DELTIM

KBC

AUTOTS

TSRES

Time Integration Controls


TIMINT

TINTP

Transient Controls


FLDATA4

FLDATA4A


ANSYS Topic Help

ANSYS Help


MP

UIMP

User Defined Mesh


SECTYPE

SECOFFSET

SECREAD

Create Taper Section


SECTYPE

SECDATA

ANSYS Help


FLDATA20

FLDATA21

FLDATA22

FLDATA23

Write Radiation Matrix To File


VTYPE

MPRINT

WRITE

Scale Icons Function


/ICSCALE

/ICLWID



Scale Icons Function

Topic Not Found

The help file you have requested cannot be found. Please use the Table of Contents, Index, or a full

text search to locate information on the topic. If you think that you have reached this page as a result

of an error in the online help system, please contact your technical support representative.

Contour Nodal Solution Data


PLNSOL

AVPRIN

/EFACET

Window Options


/PLOPTS

/TRIAD

/REPLOT

Radiation Solution Options


STEF

TOFFST

RADOPT

SPCTEMP

SPCNOD

View Factor Options


HEMIOPT

V2DOPT

VFOPT

Line: Copy Divisions

This function copies line divisions (including spacing ratios) from one line onto other unmeshed lines.

• Pick the line from which divisions will be copied, then pick OK in the picking menu.

• Pick the lines which the divisions should be copied to, then pick OK in the picking menu.

If previous line divisions exist, the copied divisions will overwrite them.


ANSYS Topic Help

Line Flip Bias

This function flips the spacing ratio of line divisions (from one end to the other) on unmeshed line. Pick

the lines, then pick OK in the picking menu.

Animate Over Results


ANDATA

ANMRES

Define Global ALE Settings for LS-DYNA Explicit


EDGCALE

EDALE

MFS Define


MFELEM

MFFNAME

MFS Setup


MFINTER

MFBUCKET

MFTOL

MFS Time Control


MFTIME

MFDTIME

MFRSTART

MFS Solution Frequency


MFCALC

MFOUTPUT



MFS Solution Frequency

MFX Solution Control


MFPSIMUL

MFSORDER

MFRELAX

MFX Time Control


MFTIME

MFDTIME

MFRSTART

MFX Mapping Operations


MFBUCKET

MFCI

MFTOL


ANSYS Topic Help

Online Help for ANSYS Dialog Boxes

Pan, Zoom, Rotate

ANSYS Function Manipulates the view by panning, zooming, and rotating the model.

Active Window(s) Identifies the window or windows that are active with this dialog box.

Any of five windows (if defined) can be the active window, or all windows

may be active at once. All Pan-Zoom-Rotate operations that are initiated

with this dialog box will be done in the active window(s).

Viewing Direction Establishes the direction from which the model is viewed. You will be

looking at the model from one of the chosen directions back to the focus

point, which is normally the centroid of the model.

• Top: The view of the top of the model; the +Y direction.

• Bot: The view of the bottom of the model.

• Left: The view of the left of the model.



• Front: The view of the front of the model; the +Z direction.

• Back: The view of the back of the model.

• Right: The view of the right of the mode; the +X direction.

• Iso: The view of the top right of the model (x = 1,y = 1,z = 1).

• Obliq: Another view of the top right of the model, but from a slightly

different angle (x = 1, y = 2, z = 3).

• WP: The view of the model from the working plane

Zooming Options Chooses the method of zooming.

• Zoom: Prompts you to pick the center and then the edge of your

square window. The portion of the model that fits within this zoom

window will then be redisplayed.

• Box Zoom: Prompts you to pick two outside corners of your zoom

window, rather than the center and outside edge as you would with

Zoom.

• Win Zoom: Prompts you to pick the first corner of your new window,

and then the edge. With this option, the new window automatically

scales to reflect the aspect ratio of the widow that you are working in.

For instance, if your window 1 is rectangular, Win Zoom produces a

rectangular zoom window of the same aspect ratio.

Pan/Zoom Buttons Picking the arrow buttons pans the model up or down, left or right.

Picking the dot buttons zooms straight in or out on the model.

• Arrow Buttons: Use them to pan (change the focus point); indicate

which way you want to move the model in the window, not which

way you want to move the window itself. Think of the window as being

stationary, and the model as being movable in the directions indicated

by the arrow buttons. The rate slider located below the rotate buttons

controls how far the model moves each time you pick an arrow key.

• Dot Buttons: Use them to zoom straight in or out on the model. The

small dot signifies that the image of the model will become smaller,

or that you will be zooming out. Likewise, the large dot indicates that

the image of the model will become larger, or that you will be zooming

in. The rate slider located below the rotate buttons controls the amount

of change in model size from zooming in or out.

Rotate Buttons The rate slider rotates the model about the X-Y-Z screen coordinates.

Your screen coordinate axis origin is centered in each defined window.

The positive X-axis starts at the center of your window and extends to

the right. The positive Y-axis also starts at the center but extends straight

up. The positive Z-axis starts at the center and extends out of the screen

straight at you. Your model will rotate about these axes in the directions



shown on the buttons. The rate slider that is below the rotate buttons

controls the amount of rotation.

Rate Control Determines the amount of pan, zoom, or rotate that is initiated with the

arrow, dot and rotate buttons above. The rate can vary from 1 to 100. A

rate of 1 means that each time you pick one of the buttons, the model

will pan, zoom or rotate a relatively small amount. For instance, a rate

of 1 corresponds to a 1 degree rotation about a screen axis each time

you pick one of the rotation buttons.

Dynamic Mode Pressing this button activates dynamic model/lighting manipulation

modes. If you are running on a 2-D graphics device (such as /SHOW,X11),

you can use your mouse pointer to pan, zoom, or rotate the model. On

a 2-D device, you will automatically be put into model manipulation

mode after pressing this button (see I. Model, below). On a 3-D device

(such as /SHOW,3D), you can choose between manipulating the model

or the lighting by using the buttons below the Dynamic button.

Dynamic Mode: Model If you want to pan, zoom or rotate your model dynamically, press this

button (This is the default dynamic mode if you are using a 2-D device).

Then, when you press and hold down any of your mouse buttons while

the pointer is in the active window, a rubberbanding box will show up

around your model. If you press the left mouse button, you can use the

rubberbanding box to pan, or move your model to where you would like

it to be in your active window. The right button lets you rotate the

model about the screen X and Y axes by moving the mouse pointer. The

center mouse button (shift-right button on a two-button mouse) has two

functions: with it, you can rotate your model about the screen Z axis by

moving the pointer right and left, and you can zoom in and out on your

model by moving the pointer up and down.

Dynamic Mode: Lighting This option is available to you only if you are using a 3-D graphics device.

If you are using a 3-D device, you can use this option to control the light

source location, intensity, and the reflectance of your model. The mouse

buttons function as follows:

• Left: Move in X-direction to increase or decrease the reflectance (or

shininess) of your model. Move in the Y-direction to change the intens-

ity of the directional lights (there are two directional lights, one in

front and one behind your model).

• Middle: Move in the X-direction to rotate the directional lights about

the screen Z-axis. Move in the Y-direction to change the intensity of

the ambient light.

Note

Using a two-button mouse, shift-right to execute the

middle button features.



Pan, Zoom, Rotate

• Right: Move in the X-direction to rotate the directional lights about

the screen Y-axis. Move in the Y-direction to rotate the lights about

the screen X-axis.

Action Buttons Fit: Automatically adjusts that amount of zoom in the active window

so that your entire model can be seen within the window. This is a

•

useful key to use after you have zoomed in a number of times to ex-

amine a portion of your model and now want to view the entire

model.

• Reset: Removes any pan, zoom, or rotate specifications in the active

window. Your model will be displayed in its default orientation and

sized to fit within the active widow.

Edit Toolbar/Abbreviations

List Lists currently defined abbreviations. Pick an abbreviation in this area to

select it (it will appear in the Selection edit box). You can edit or delete

the selected abbreviation.

Selection This area serves two purposes:

• To specify an abbreviation using the *ABBR command format, type

the abbreviation in the box and choose Accept to define it.

• To edit or delete a selected abbreviation (picked from the list area),

modify the abbreviation and choose Accept to change it.

The format to define an abbreviation is *ABBR, Abbr, String,

where Abbr is the abbreviation (up to 8 characters) representing

the string String. The string can be a command, a macro name

(an "unknown command" macro), or a GUI function name (which

calls a dialog box).



Hard Copy

ANSYS Function The PS in the title of this dialog box indicates that you will be using the

PostScript format for graphics that are written to a file or that are sent

directly to a printer. Both of these options are called "hard copies."

Extents With these radio buttons, you can choose to print the entire screen, or

only the portion within the ANSYS Graphics Window. Printing the full

screen sends all visible screen items to the printer, even if the graphics

are not related to ANSYS. When you print the graphics window, all items

within the window are sent to the printer. This feature allows the dis-

played ANSYS graphics to be printed in conjunction with other displays,

including the ANSYS command output window or material propery data

listings. Even non-ANSYS windows, such as a Windows notepad annota-

tion can be included. If only the ANSYS graphics display is desired, be

sure to move other windows or utility boxes (such as the Pan, Zoom,

Rotate, or Meshtool dialogues) out of the way.

Plot Type Specifies the graphics type for your printer. Most laser printers are de-

signed to print black and white (monochrome) or gray scale graphics.

You can print color graphics on many thermal-wax type plotters.

File Type Postscript: Creates PostScript file•



Hard Copy

• TIFF: Creates TIFF file (should not be spooled to a printer)

• EPS with TIFF Preview: Encapsulated PostScript with TIFF preview

(should not be spooled to printer. Use only for inserting graphics inside

a publishing package.)

• JPEG: Creates a .jpg file

• PNG: Creates a .png file

TIFF Compression Toggle Compresses TIFF files and EPS files with TIFF preview (Default=ON). Turn

off when using Word Perfect.

Black/White Toggle Switches black to white, and white to black on hard copies. By default,

the Reverse Video option is on, which means that what you see in white

on your screen is printed in black on your hard copy.

Orientation Specifies how your graphics are oriented on hard copies. The default

orientation is Landscape, which means that the width dimension of the

graphics on your screen corresponds to the height dimension of your

printed page. For instance, if your printed page measures 8 1/2"x11", the

width dimension of the graphics on your screen corresponds to the 11"

height dimension of your page.

Print Command Press this button to send the graphics directly to a printer. Then, in the

corresponding text entry box, fill out the rest of the system level print

command (for example, lpr on UNIX) that you use to send PostScript

graphics files to PostScript printers.

File Command Press this button if you want to write your graphics to a PostScript file.

By default, your graphics are written to a file with the name shown in

the text entry box. You can change the file name to something that more

closely describes your project, but you should keep the default extension

in order to retain the automatic indexing of the extension name. For in-

stance, if you name your first file Shuttle.p01 , and then pick OK or

Apply, the name in the text entry box for the next file to be produced

will automatically be indexed to read Shuttle.p02 .

Note

Open GL (3D) devices require that the Graphics Window contents be brought to the top to

generate plots of partially obstructed window contents. See the /UIS command for more

information on this behavior and how it affects other graphics operations.



PC Hard Copy

ANSYS Function Indicates that graphics will be written to a file or sent directly to a

printer.

Plot Type Specifies the graphics type for your printer. See your printer documenta-

tion for the specific black and white, grayscale and color capabilities.

File Type Bitmap: Creates bitmap file (should not be spooled to a printer)•

• Postscript: Creates PostScript file

• TIFF: Creates TIFF file



TIFF Compression Toggle Compresses TIFF files (Default=ON).

Black/White Toggle Switches black to white, and white to black on to compensate for the

default black background on the ANSYS Graphics Window. By default,

Reverse Video is on, allowing this option to generate white print outs

with black (or shaded/colored) legend, plot and data items.

Orientation Specifies how your graphics are oriented on hard copies. The default

orientation is Landscape.

File Command Writes your graphics to a file. By default, your graphics are written to a

file with the name shown in the text entry box. You can change the file



PC Hard Copy

name to something that more closely describes your project, but you

should keep the default extension.

Note

Open GL (3D) devices require that the Graphics Window contents be brought to the top to

generate plots of partially obstructed window contents. See the /UIS command for more

information on this behavior and how it affects other graphics operations.

Capture Image Feature

The Capture Image feature lets you view multiple displays of your ANSYS model or results quickly and

simultaneously. The feature works by capturing and restoring copies of the Graphics Window.

To capture a copy of the Graphics Window, choose PlotCtrls> Capture Image on the Utility Menu.

The copy is actually a window that you can iconify and that will be the same size as the Graphics Window.

(You may want to shrink the Graphics Window before capturing if you will later be comparing several

images at one time on the screen.) Copies will automatically be named Image1 , Image2 , Image3 ,

etc., numbered sequentially within an ANSYS session. The number of captured images displayed at one

time cannot exceed 20 and is also limited by the amount of memory.

After the image is captured, you can save it to a file (on the copied window, choose File> Save as). On

X11 systems, the file is a coded image file. Use the extension .img when naming the file. On Windows

systems, the file is a Windows bitmap file. Use the extension .BMP for the file name.

Saved image files can be restored during any ANSYS session (choose PlotCtrls> Restore Image on the

Utility Menu).

To print the captured image directly from within ANSYS, choose File> Print on the copied window.

This method of printing produces a hard copy similar in resolution quality to a typical screen dump.



Capture Image: Print

ANSYS Function Prints a hard copy of a captured image. You can write the image to a

graphics file or send it directly to the printer. (Both of these options are

called "hard copies.") This method of printing produces a hard copy

similar in resolution quality to a typical screen dump.

Plot Type Specifies the graphics type for your printer. Most laser printers are de-

signed to print black and white (monochrome) or gray scale graphics.

Color graphics can be printed on many thermal-wax type plotters.

File Type Postscript: Creates PostScript file•

• TIFF: Creates TIFF file (should not be spooled to a printer)

• EPS with TIFF Preview: Encapsulated PostScript with TIFF preview

(should not be spooled to printer). Use only for inserting graphics inside

a publishing package.



TIFF Compression Toggle Compresses TIFF files and EPS files with TIFF preview (Default = ON). Turn

off when using WordPerfect.



Capture Image: Print

Black/White Toggle Switches the color black to the color white on hard copies. By default,

Reverse Video is on, which means that what you see in white on your

screen will be printed in black on your hard copy.

Orientation Specifies how graphics are oriented on hard copies. The default orienta-

tion is Landscape, which means that the width dimension of the captured

image will correspond to the height dimension of your printed page.

Print Command Press this button if you want your graphics to go directly to a printer.

Then, in the corresponding text entry box, fill out the system level print

command (for instance, lpr in Unix) that you use to send PostScript format

files to PostScript printers.

File Command Writes the captured image to a PostScript file. By default, the image will

be written to a file with the name shown in the corresponding text entry

box. You can change the file name into something meaningful for your

project but you should keep the default extension in order to retain the

automatic indexing of the extension name. For instance, if you name the

first file shuttle.p01 and then pick OK, the name in the text entry

box for the next file to be produced will automatically be indexed to

read shuttle.p02 .

Capture Image: Save as

ANSYS Function The File Selection dialog box lets you write a captured image to a file.

On X11 systems, the file is a coded image file. Use the extension .imgwhen naming the file.

Filter The search path (directory and file name) that will be used if you click

on the Filter button. Matching files found upon filtering will be shown

in the Directory and File List areas. By default, the search path for filter-

ing is the working directory with files ending in a .img extension.



Directory List List of directories for specifying where a file is to be written. When you

click on any directory from the list, the corresponding File List area will

change to reflect the files in that directory.

File List List of files from which to choose for writing. This is useful if you want

to overwrite an existing file.

File Name A text entry box where you can directly enter the name of the file to be

written. On X11 systems, use the extension .img .

Action Buttons Filter: Does a search for files that reside in the directory as specified

in the Filter area. Matching files found upon filtering will be shown in

the Directory and File List areas.

•

Restore Image

ANSYS Function The File Selection dialog box lets you read in a previously saved captured

image file.

Filter The search path (directory and file name) that will be used if you click

on the Filter button. Matching files found upon filtering will be shown

in the Directory and File List areas. By default, the search path for filter-

ing is the working directory with files ending in a .img extension.

Directory List List of directories for specifying where a file is to be read from. When

you click on any directory from the list, the corresponding File List area

changes to reflect the files in that directory.

File List List of files from which to choose for reading in.

File Name A text entry box where you can directly enter the name of the file to be

read in.



Restore Image

Action Buttons Filter: Does a search for files that reside in the directory as specified

in the Filter area. Matching files found upon filtering will be shown in

the Directory and File List areas.

•

Results Query Picker

ANSYS Function Identifies the information being queried; either nodal, element, or subgrid

solution data (in this example, element solution data).

Pick Mode Allows you to pick or unpick a location on the model to be queried. You

can use either these toggle buttons or the right mouse button to switch

between pick and unpick modes. The mouse pointer is shown as an up

arrow for picking and a down arrow for unpicking.

Picked Location Shows the number and location (in global Cartesian coordinates) of the

node, element (coordinates are of the element centroid), or subgrid point

being picked for query. You can preview this information by pressing

and dragging the mouse in the graphics area. The picked location is

highlighted on the model as a square on the displaced shape. The nodal

location or element centroid locations are shown in undeformed or de-

formed locations based on the type of display that has been performed.

For undeformed displays (i.e., NPLOT, EPLOT, etc.), the coordinate loca-

tions will be in undeformed global Cartesian coordinates. For deformed

displays (i.e., PLDISP, PLNSOL, PLESOL, etc.), the coordinate locations

will be in deformed global Cartesian coordinates, subject to command

/DSCALE settings.

Queried Data Shows the queried solution data for the node, element, or subgrid point

at the picked location. Use the Max or Min buttons to automatically

obtain the maximum or minimum value of the query data for the viewable

portion of the model.

Generate 3D Annotation Applies the queried information to the model as 3D annotation.



Action Buttons OK: Clears all query data (restores the graphics display without

replotting) and closes the query picking menu.

•

• Apply: Clears all query data (restores the graphics display without

replotting) and redisplays the Query Solution Data (either Nodal, Ele-

ment, or Subgrid) dialog box. You can either use this button on the

picking menu, or, stay in the graphics area and click the middle mouse

button to achieve the same effect.

• Reset: Clears all query data (restores the graphics display without

replotting).

• Cancel: Clears all query data (restores the graphics display without

replotting) and closes the Query Picking menu.

• Min: Shows the minimum value of the query data for the viewable


• Max: Shows the maximum value of the query data for the viewable


Hints on Using the Query Picking Menu

• Query picking is most effective when used in vector mode (for example, with wireframe displays) because

you can read the queried data easily right on top of the model in the Graphics Window. Vector mode is

accessed under PlotCtrls> Device Options (or /DEVICE command).

• Press and drag the left mouse button around on the model for an easy way to see the queried data for

many different points without creating excessive clutter on the screen.

• Use the Reset button often to clear the screen of queried data and get a "clean" model on which to

continue querying.

• The Min and Max buttons are useful for quickly identifying the location and value of the minimum and

maximum query data.

• The results query picker retrieves data from the database. The operations and functions performed are

not written to the log file.

• In Powergraphics the Results Query Picker will provide information for shell elements that corresponds

to the side of the object you see, not what you specified in the SHELL command.



Results Query Picker

Query Solution Data

This is a two-column selection list dialog box. First choose a category of the solution data from the left

column, and then pick the desired component from the right column.

ANSYS Function Identifies the item of the solution data to be queried.

For any picked subgrid point on the model, ANSYS retrieves the data

value from the database and displays it. The /EFACET command

controls the number and location of subgrid points available for

querying and the AVRES command controls the method of averaging

results for querying.

Solution Data Item Categories of solution data. Use the scroll bar to see all valid items.

Solution Data Component Component of the solution data item. The list of valid components varies

depending on the chosen category. Use the scroll bar to see all valid

components.

Selection A visual verification of the chosen item and component of the solution

data. (This is not a text entry box.)

Array Parameters

ANSYS Function This dialog box lists array parameters and gives access to the functions

used to define and edit array parameters.

List Lists currently defined array parameters, including array type and dimen-

sions. Pick a parameter in this area to select it (to Edit [*VEDIT] or Delete

[*DEL] it) or select the Add to define a new array parameter [*DIM].



Array Parameter Editing: ARRAY Type Arrays

This dialog lets you graphically edit an array parameter of type ARRAY [*VEDIT]. (Character array para-

meters cannot be edited graphically.)

ANSYS Function Array Parameter Editor. Identifies the name of the array parameter

which is being edited (in this example, the array parameter is named

"A").

Menu bar A pull-down menu which contains

the following options:

File Menu

• Apply: Applies (saves) all changes

you make to the array parameter.

• Apply/Quit: Applies (saves) all

changes you make to the array

parameter and closes the dialog

box.

• Reset: Resets all values in the array

parameter editor to what they

were at the last Apply.

• Quit: Closes the dialog box. If

changes have not been saved

(Apply ), you will be warned.

Edit Menu A pull-down menu which contains

the following options related to edit-

ing rows and columns:

• Initialize: Initializes all cells in the

selected row or column to the

value shown in the Initialization

Constant input box.

• Copy: Copies the cell values in the

currently selected row or column

to another specified row or



Array Parameter Editing: ARRAY Type Arrays

column. For example, select the

row to be copied, choose Copy

from the Edit menu, and then se-

lect the row to copy to. You can

copy only a row to another row a

column to another column.

• Insert: Inserts zero values in the

row or column before the currently

selected row or column. The values

in the existing rows or columns

shift (down or to the right) to make

room. The values in the last row or

column "fall off" the array.

• Delete: Deletes the values in the

selected row or column. The values

in the remaining rows or columns

shift (up or to the left). The last row

or column is filled with zero values.

• Unselect: Unselects the currently

selected row or column.

Help Displays this help information.

Page Increment To control what increment of the page will be used when moving around

the array via the navigation buttons. Pick full page, half page, or 1 cell.

View Plane To indicate which Z plane of the array parameter is to be displayed for

editing. Pick the number of the desired Z plane.

Array Navigation Buttons To navigate across the currently displayed array plane. The currently se-

lected page increment is used. Use these buttons only when the array

dimensions are greater than the current cell viewing area. (You can view

a maximum of 10 X 10 cells at one time.)

Initialization Constant Enter the number to initialize a row or column, then choose Initialize

from the Edit menu.

Selection Status Displays the row or column currently selected.

Column Borders Used to identify the columns. The column number appears in the border.

Pick a column border to select the entire column.

Row Borders Used to identify the rows. The row number appears in the border. Pick

a row border to select the entire row.

Array Cells Input boxes that correspond to array locations. The location is identified

by the row number (X), column number (Y), and view plane number (Z).

Pick a cell to select it, then enter the desired number.



Array Parameter Editing: Table Array

This dialog lets you graphically edit a TABLE type array parameter [*VEDIT].

ANSYS Function Array Parameter Editor. Identifies the name of the table array parameter

that is being edited. In this example, the array parameter is named

"MYTABLE" and represents a 3-dimension table with the variables TIME,

X, and Y.

Menu Bar A pull-down menu which contains

the following options:

File Menu

• Apply: Applies (saves) all changes

you make to the array parameter.

• Apply/Quit: Applies (saves) all

changes you make to the array

parameter and closes the dialog

box.

• Reset: Resets all values in the array

parameter editor to what they

were at the last Apply.

• Quit: Closes the dialog box. If

changes have not been saved

(Apply), you will be warned.

Help Displays this help information.

Page Increment Controls how much of the page is shifted when moving around the array

via the navigation buttons. Pick full page, half page, or 1 cell.



Array Parameter Editing:Table Array

View Plane Indicates which Z plane of the array parameter is to be displayed for

editing. Click on the desired Z plane to view or edit the array cells corres-

ponding to that Z plane.

Array Navigation Buttons This set of buttons lets you navigate across the currently displayed array

plane. The currently selected page increment is used. Use these buttons

only when the array dimensions are greater than the current cell viewing

area. (You can view a maximum of 10 X 10 cells at one time.)

Variable 1: Variable name corresponding to the first dimension (row)

(see *DIM). Defaults to Row.

Variable 2: Variable name corresponding to the second dimension

(column) (see *DIM). Defaults to Column.

Variable 3: Variable name corresponding to the third dimension

(plane) (see *DIM). Defaults to Plane.

Array Cells Input boxes that correspond to array locations. The location is identified

by the row number (X), column number (Y), and plane number (Z). Pick

a cell to select it, then enter the desired number.

Column Indices Used to identify the columns. The column number appears in the border.

Pick a column border to select the entire column.

Row Indices Used to identify the rows. The row number appears in the border. Pick

a row border to select the entire row.

Scalar Parameters

List Lists currently defined scalar parameters. Pick a parameter in this area

to select it (it will appear in the "Selection" input box). You can use the

currently selected parameter as input elsewhere in the GUI. To do so,

use the middle mouse button to paste it into the desired input field.

Selection This area serves two purposes:



• To specify a parameter using the Name= format (*SET command),

type the parameter in the box and choose Accept to define it.

• To edit or delete a selected parameter (picked from the list area),

modify the parameter and choose Accept to change it.

Define Real Constants

List Lists real constants that you have defined in this listing area. You can

select any of the defined real constants by clicking on that line within

the box. The selected real constant will be highlighted, and you can then

pick either Edit or Delete to modify the real constant set.

Element Types

This dialog box lists all the currently defined element types. You can add additional element types,

change the element options for the currently defined element types, and delete currently defined

element types.

List Lists currently defined element types. Pick an element type in this area

to select it for Options or Delete actions. The selected element type will

be highlighted.



Element Types

Offset Working Plane

ANSYS Function Enables translation and rotation of the working plane. [WPOFFS,

WPROTA, and WPSTYL]

Offset Options Picking these buttons causes an im-

mediate offset of your working plane

Offset Buttons

in the direction shown on the button.

The positive X, Y, and Z working

plane axes correspond to the working

plane triad (see the WP Settings dia-

log box to control the display of the

triad symbol). The amount of offset

is controlled by the Offset Slider

shown below, and the Snap Incr

value on the WP Settings dialog box.

Offset Slider Controls the amount of offset that

occurs with each pick of the Offset

Buttons. If the slider is set to 1, the

offset will be one times the Snap Incr

value on the WP Settings dialog box.



Offset Dialog Input Allows you to input the exact X, Y, Z

offsets for the working plane. For in-

stance, typing in 1,1,1 into this dialog

box and hitting Apply or OK moves

the working plane one unit in each

of the positive X, Y, and Z directions.

Rotate Options Rotates the working plane about the

axis show in the button, in the direc-

Rotate Buttons

tion indicated. For instance, the up-

per right button rotates the working

plane about the X-axis of the current

working plane in a negative direction.

The angle of rotation is controlled by

the Rotate Slider.

Rotate Slider Controls the amount of rotation that

will occur with each pick of the Ro-

tate Buttons.

Rotate Dialog Input Allows you to specify the exact rota-

tion angles for the working plane.

These angles are measured in de-

grees, and the positive direction of

rotation about each axis follows the

right hand rule.

Location Status Displays the current location of the working plane in global Cartesian

coordinates. This status is updated each time the working plane is

translated.

Dynamic Mode Toggle Pressing this button activates dynamic mode, in which you use the mouse

buttons to move the working plane. The left mouse button translates

the working plane in the screen X and Y directions. The middle mouse

button rotates the working plane about its Z axis (moving the mouse

left and right) and in and out of the screen Z (viewing) direction (moving

the mouse up and down). The right mouse button rotates the working

plane about its Y axis (moving the mouse left and right) and about its X

axis (moving the mouse up and down). In all cases, the amount of

movement is controlled by the Snap Incr setting on the WP Settings

dialog box.



Offset Working Plane

Working Plane Settings

System Choose the active working plane system. With the Cartesian (default)

system, you locate points in terms of X and Y coordinates. Points are

located with R and Θ coordinates in a Polar system. [WPSTYL]

Graphics Options Choose what is to be shown to indicate the working plane. The triad

appears in the center (0,0 location) of the working plane, and moves with

the plane as you change the working plane location or orientation. You

can see the orientation of the working plane by displaying the Grid. You

can pick locations anywhere on the working plane, rather than just at

the intersections of the grid lines. The Snap Option controls picking

locations.

Snap Options Controls the locational picking points. If Enable Snap is activated, loca-

tional picks you make will be directed to the nearest Snap point location.

The Snap Incr dialog controls snap point locations. Snap increments are

located every .05 units in the X and Y direction of the working plane

(Cartesian) by default. You can change the spacing of snap locations by

changing the Snap Incr value. If you are using a Polar working plane,

you can control the f increment between snap point locations (Snap

Ang) as well as the radial distance between points (Snap Incr).

Grid Control Spacing: Controls the distance between grid lines. This does not affect

the Snap point locations, which the Snap Options control.

•

• Minimum: This is the minimum X location that you want the grid to

be displayed to (Cartesian system only).



• Maximum: This is the maximum X location that you want the grid to

be displayed to (Cartesian system only).

• Radius: This is the outside radius that you would like the grid to be

displayed to (Polar system only).

• Tolerance: Used only for locational picking for polygon and prism

vertices. The tolerance that an entity's location can deviate from the

specified working plane, while still being considered on the plane.

(defaults to 0.003).

Define Element Table Data

ANSYS Function Defines element table data [ETABLE]. This dialog box defines the element

table values per element for use in further postprocessing [CALC]. You

can reference this data through another dialog box (Add) that displays

available data items for the selected element type.

List Lists results data that have been entered into the element table. The

column headings are as defined below:

• Label: User defined label for element table data.

• Item: Item as defined by the ETABLE command.

• Comp: Component as defined by the ETABLE command.

• Time Stamp: Time when the load step was generated.

Action Buttons Results data will be listed in the “Currently Defined Data and Status”

section as defined with the Add, Update, or Delete buttons.

• Update: Updates the element table. The element table is not automat-

ically refilled (updated) when you read in a different set of results (such

as for a different load step) or when you alter the results in the data-

base (such as by a load case combination).

To refill (update) the column with values from another load step,

select Update [ETABLE,REFL] again.



Define Element Table Data

Define Time-History Variables

ANSYS Function Defines variables for POST26. This dialog box lets you define variables

for further postprocessing in POST26, the Time History postprocessor.

Variables are tables of result items versus time (or frequency). The first

step in POST26 is to define these variables [FORCE, SHELL, LAYER, NSOL,

ESOL, RFORCE, GAPF, and SOLU]. As you define a variable, it is given a

reference number which you will use to denote that variable in future

postprocessing.

List Lists results variables you have defined. The column headings are as fol-

lows:

• Variable: Variable reference number (greater than 1) assigned by AN-

SYS. Reference number 1 is reserved for Time.

• Type: Type of results data defined (NSOL, ESOL, etc.).

• Elem: Element number of variable data.

• Node: Node number of variable data.

• Item: Item label for the type of data being defined (EPEL for elastic

strain, TF for thermal flux, etc.).

• Comp: Component (if required) for the Item listed above.

• Name: User-defined name for each variable. If you don't define a name,

ANSYS gives the variable a name based on the Item and Comp labels.

Action Buttons Defined variables will be listed in the “Currently Defined Specifications”

section as defined with the Add, Update, or Delete buttons.

Display and Update Nonlinear Convergence Specifications



ANSYS Function Defines nonlinear convergence criteria [CNVTOL], and lets you add a

tolerance for nonlinear convergence specifications, edit existing specific-

ations, and delete currently defined specifications.

List Lists convergence specifications that you have defined. As new specific-

ations are added, this listing area updates automatically. You can select

any of the defined convergence specifications by clicking on that line

within the box. The selected specification will be highlighted, and you

can then pick either Edit or Delete to modify the convergence criteria

set.

Solution Controls

General Information About Using the Solution Controls Dialog Box

You can use the Solution Controls dialog box if you are performing a static or full transient analysis.

The Solution Controls dialog box consists of five tabbed “pages,” each of which contains a set of related

solution controls. The tabs, in order from left to right, include:

• Basic

• Transient

• Sol'n Options

• Nonlinear

• Advanced NL

Each set of controls is logically grouped on a tab; the most basic controls appear on the first tab, with

each subsequent tab providing more advanced controls. The Transient tab contains transient analysis

controls; it is available only when you choose a transient analysis and remains grayed out when you

choose a static analysis.

Once you are satisfied with the settings on the Basic tab, you do not need to progress through the

remaining tabs unless you want to change some of the advanced controls. As soon as you click OK on

any tab of the dialog box, the settings are applied to the ANSYS database and the dialog box closes.

Note

Whether you make changes to only one or to multiple tabbed pages, your changes are applied

to the ANSYS database only when you click OK to close the dialog box.



Solution Controls

Basic Tab

Use the Basic tab to specify the options described below. The controls that appear on the Basic tab

provide the minimum amount of data that ANSYS needs for the analysis.

Analysis Options [ANTYPE, NLGEOM]--Specifies the type of analysis that you want to

perform. (The “large deformation effects” referred to below include large

deflection, large rotation, and/or large strain, depending on the element

type being used.) You can choose one of these options:

• Small Displacement Static: Performs a linear static analysis (that is, a

static analysis in which large deformation effects are ignored).

• Large Displacement Static: Performs a nonlinear static analysis (that

is, a static analysis in which large deformation effects are included).

• Small Displacement Transient: Performs a linear full transient analysis

(that is, a full transient analysis in which large deformation effects are

ignored).

• Large Displacement Transient: Performs a nonlinear full transient

analysis (that is, a full transient analysis in which large deformation

effects are included).

• Restart Current Analysis: Restarts the current analysis.

Time Control Controls various time settings.

In the Time at end of loadstep [TIME] entry box, specify a time

value for ANSYS to associate with the boundary conditions at the

end of the load step.



Click the Automatic time stepping [AUTOTS] drop down list box

to turn automatic time stepping on, off, or have ANSYS automatically

switch it on and off between substeps of a load step as needed.

Determine how you want to control the number of substeps that

are taken within a load step. You can choose either Number of

substeps or Time increment:

• Number of substeps [NSUBST]: Indicates that you want to specify a

specific number of substeps to be taken within this load step. If you

choose this option, you can use the Number of substeps, Max no. of

substeps, and Min no. of substeps entry boxes to specify starting

values and limits for substeps. How these limits are interpreted by

ANSYS depends on what option you selected in the Automatic time

stepping drop down list box:

– Number of substeps: If automatic time stepping is turned off, spe-

cifies the number of substeps to be taken this load step (that is, the

time step size or frequency increment). If automatic time stepping

is turned on, specifies the size of the first substep.

– Max no. of substeps: Specifies the maximum number of substeps

to be taken (that is, the minimum time step size) if automatic time

stepping is turned on.

– Min no. of substeps: Specifies the minimum number of substeps

to be taken (that is, the maximum time step size) if automatic time

stepping is turned on.

• Time increment [DELTIM]: Indicates that you want to specify the time

step size for this load step. If you choose this option, you can use the

Time step size, Minimum time step, and Maximum time step entry

boxes to specify starting values and limits for time steps. How these

limits are interpreted by ANSYS depends on what option you selected

in the Automatic time stepping drop down list box:

– Time step size: If automatic time stepping is turned off, specifies

the time step size for this load step. If automatic time stepping is

turned on, specifies the starting time substep.

– Minimum time step: Specifies the minimum time step size (if

automatic time stepping is turned on).

– Maximum time step: Specifies the maximum time step size (if

automatic time stepping is turned on).

Write Items to Results File [OUTRES]--Specifies the solution data that you want ANSYS to write to

the results file (database). You can choose one of these options:

• All solution items: Writes all solution items to the database.

• Basic quantities: Writes only the following solution items to the

database: nodal DOF solution; nodal reaction loads; element nodal



Solution Controls

loads and input constraint and force loads; element nodal stresses;

element nodal gradients; and element nodal fluxes.

• User selected: Writes only selected solution items. If you select this

option, use the list box to choose the specific solution items that you

want ANSYS to write to the database. Ctrl-click on each item to select

it; to unselect a selected item, Ctrl-click on it again.

Use the Frequency drop down list box to indicate how frequently

you want ANSYS to write the selected solution items to the database.

You can choose one of these options: Write every substep, Do not

write any substeps, Write last substep only, Write every Nth

substep, or Write N number of substeps.

For more information about the controls on the Basic tab, see Loading and The General Postprocessor

(POST1) in the Basic Analysis Guide.

Transient Tab

Use the Transient tab to specify the options described below.

Full Transient Options Specifies the transient options that you want to include in the analysis.

You can set one or more of these options:

• Transient effects [TIMINT]: Includes transient effects (for example,

structural inertia).

• Stepped loading/Ramped loading [KBC]: Choose between stepped

loading or ramped loading by clicking the desired button. When

loading is stepped, loads are step changed at the first substep of this

load step to the values of this load step (that is, the same values are

used for all substeps). When loading is ramped, loads are linearly inter-



polated for each substep from the values of the previous load step to

the values of this load step.

Damping Coefficients Specifies various damping options. One form of the viscous damping

matrix [C] is given by α[M] + β[K], where [M] is the mass matrix and [K]

is the stiffness matrix. You can specify values for one or both of the fol-

lowing:

• Mass matrix multiplier (ALPHA) [ALPHAD]: Defines the mass matrix

multiplier, α, for damping.

• Stiffness matrix multiplier (BETA) [BETAD]: Defines the stiffness

matrix multiplier, β, in the damping expression described above.

Midstep Criterion Specifies the midstep residual criterion to be used in the analysis [MIDTOL

command]:

• Midstep Criterion: Activate midstep residual criterion.

• Tol/Ref for Bisection: Midstep residual tolerance (if > 0) or reference

value (if < 0) used for bisection.

• Include Response Frequency: Calculate response frequency and

consider it in the automatic time stepping.

Time Integration Specifies time integration method and parameters.

• Algorithm [TRNOPT]: Choose the Newmark algorithm or the HHT al-

gorithm.

Integration parameters can be set by choosing one of these two

options:

• Amplitude decay [TINTP]: Defines an amplitude decay for the

second order transient integration. If you choose this option, use

the GAMMA entry box to specify the factor.

• Integration parameters: Allows individual input of each integra-

tion parameter. If you choose this option, use the ALPHA and

DELTA entry boxes to specify the Newmark parameters. If the

HHT algorithm was selected, use ALPHAM and ALPHAF to specify

additional HHT parameters.

For more information about the controls on the Transient tab, see Transient Dynamic Analysis in the

Structural Analysis Guide.



Solution Controls

Sol'n Options Tab

Use the Sol'n Options tab to specify the options described below.

Equation Solvers [EQSLV]--Specifies the type of equation solver that you want to use. You

can choose one of these options:

• Program chosen solver: ANSYS selects a solver for you, based on the

physics of the problem.

• Sparse direct: This direct elimination solver is suited for analyses in

which robustness and solution speed are required (nonlinear analyses),

and for linear analyses in which iterative solvers are slow to converge

(especially for ill-conditioned matrices, such as poorly shaped elements).

Memory use is medium; disk use is high.

• Pre-Condition CG: This iterative solver is suited for analyses in which

solution speed is crucial, such as in linear analyses of large models.

Especially well suited for bulky structures modeled with solid elements.

Memory use is medium; disk use is low. If you choose this option, use

the slider to set the accuracy level for convergence for the solver. The

accuracy level can vary from 1 (fastest setting, fewer number of itera-

tions) to 5 (slowest setting, accurate, more number of iterations).

For detailed information on these solvers, see the Basic Analysis

Guide.

Restart Control [RESCONTROL]--Restarts an analysis from any point. In the Number of

restart files to write entry box, indicate the maximum number of restart

files that you want ANSYS to write for a load step.

Click the Frequency drop down list box and choose how frequently

you want restart files to be written to the ANSYS database. You can

choose one of these options: Write every substep, Do not write

any files, Write last substep only, Write every Nth substep, or

Write N number of substeps.



For more information about the controls on the Sol'n Options tab, see Solution in the Basic Analysis

Guide.

Nonlinear Tab

Use the Nonlinear tab to specify the options described below.

Nonlinear Options Controls several nonlinear options and how they are used in the analysis.

You can set one or both of these options:

• Line search [LNSRCH]: Activates a line search to be used with the

Newton-Raphson method. Line search is an alternative to adaptive

descent. You can turn line search on or off, or have ANSYS automatically

switch line searching on and off between substeps of a load step as

needed. This setting, which is recommended, can be very efficient for

analyses in which a line search is needed only at certain substeps.

• DOF solution predictor [PRED]: Activates a predictor on the degree

of freedom solution. You can turn the predictor on for all substeps of

a load step except the first substep, on for all substeps including the

first substep, off for all substeps, or have ANSYS automatically switch

a predictor on and off between substeps of a load step as needed.

Equilibrium Iterations [NEQIT]--In the Maximum number of iterations entry box, specify the

maximum number of equilibrium iterations that you want to allow per

substep.

Creep Option [RATE]--Specifies whether the effect of creep strain rate will be used in

the solution of a load step. You can turn creep calculation on or off. The

default is off. This option must be on to perform an implicit creep analysis.

RATE works only when performing an implicit creep analysis with the

following elements: LINK180, SHELL181, PLANE182, PLANE183, SOLID185,



Solution Controls

SOLID186, SOLID187, SOLSH190, BEAM188, BEAM189, SHELL208, and

SHELL209.

Set convergence criteria [CNVTOL]--Sets convergence values for the analysis. Click the Set con-

vergence criteria button to access the Nonlinear Convergence Criteria

dialog box. The dialog box contains a Help button that you can click for

more information.

Cutback Control [CUTCONTROL]--Provides control over bisections, or cutbacks, in substep

size. Under Limits on physical values to perform bisection, specify

limits for cutbacks. When any of these limits is exceeded, a cutback occurs.

You can specify values for one or more of these limits:

• Plastic strain ratio: A cutback occurs if the equivalent plastic strain

within a substep exceeds this limit.

• Explicit creep ratio: A cutback occurs if the equivalent explicit creep

ratio within a substep exceeds this limit.

• Implicit creep ratio: A cutback occurs if the equivalent implicit creep

ratio within a substep exceeds this limit.

• Incremental displacement: A cutback occurs if the incremental dis-

placement within the solution field in a substep exceeds this limit.

• Points per cycle: A cutback occurs if the number of solution points

per cycle exceeds this limit.

You can also choose one of these options:

• Cutback according to predicted number of iterations: ANSYS uses

an internal auto time step scheme to predict the number of iterations

for nonlinear convergence and performs a cutback before reaching

the number of iterations specified in the Maximum number of itera-

tions entry box (described above). This is the recommended setting.

• Always iterate to n equilibrium iterations: A nonconvergent solution

iterates to the number of iterations specified in the Maximum number

of iterations entry box (described above) before ANSYS invokes a

cutback.

For more information about the controls on the Nonlinear tab, see Nonlinear Structural Analysis in the

Structural Analysis Guide.



Advanced NL Tab

Use the Advanced NL tab to specify the options described below.

Termination Criteria [NCNV]--Determines what happens if the analysis fails to converge or

specified limits are met. Click the Program behavior upon nonconver-

gence drop down list box and choose one of these options: Do not

terminate analysis, Terminate analysis and Exit, or Terminate but Do

Not Exit.

Limits on physical values to stop analysis-- You can also specify

limits for one or more of the following physical values:

• Nodal DOF sol'n: Terminates if the largest nodal DOF solution value

(displacement, temperature, and so on) exceeds this limit.

• Cumulative iter: Terminates if the cumulative iteration number exceeds

this limit.

• Elapsed time: Terminates if the elapsed time (in seconds) exceeds this

limit.

• CPU time: Terminates if the CPU time (in seconds) exceeds this limit.

Arc-length Options [ARCLEN, ARCTRM]--Controls activation and termination of the arc-length

method. Click the Activate arc-length method check box to activate it,

and then use the Max multiplier and Min multiplier entry boxes to



Solution Controls

specify the maximum and minimum multipliers of the reference arc-

length radius.

Note

You cannot use the arc-length method with the fol-

lowing controls: automatic time stepping, line search,

and the DOF solution predictor. If you activate the

arc-length method after you set any of these con-

trols, a warning message appears. If you choose to

proceed with the arc-length method activation, AN-

SYS disables your automatic time stepping, line

search, and DOF solution predictor settings.

Arc-length termination: Click the drop down list box to specify the

basis of solution termination. You can choose one of these options:

• Do not terminate analysis: Does not use arc-length option settings

as the basis for terminating the analysis.

• Terminate at first limit point: Terminates the analysis if the first limit

point has been reached. (The first limit point is that point in the re-

sponse history at which the tangent stiffness matrix becomes singular;

in other words, the point at which the structure becomes unstable.)

• Terminate at <direction> limit: Terminates the analysis when the

displacement in the chosen direction first equals or exceeds a specified

limit. The direction can be UX, UY, UZ, ROTX, ROTY, or ROTZ. If you

select one of these options, specify the maximum desired displacement

(absolute value) in the Displacement limit entry box. (For rotational

degrees of freedom, specify the limit in radians rather than in degrees.)

Then, click the Pick node button and use the picker to pick a node.

Mechanical APDL calculates the displacement at the picked node and

compares it to the specified limit. When the calculated displacement

equals or exceeds the specified limit, the analysis terminates.

For more information about the controls on the Advanced NL tab, see Nonlinear Structural Analysis in

the Structural Analysis Guide.



MeshTool

ANSYS Function Provides a shortcut to the most commonly used meshing controls, as

well as to the meshing operations that users perform most frequently.

Attribute Controls Sets attributes to be used for meshing. Pressing the Global option

button causes an option menu of available choices (Global , Volumes ,

Areas , Lines , KeyPoints ) to appear. After selecting an option, press

the Set button to specify attributes.

SmartSizing Controls Pressing the button activates SmartSizing. The position of the slider

control determines the overall element size level for meshing, which can

vary from 1 (fine mesh) to 10 (coarse mesh). The slider control is active

only when SmartSizing has been activated. SmartSizing is recommended

for free meshing operations; it cannot be used for mapped meshing.

[SMRTSIZE]

Local Mesh Sizing Controls Provide more control over element size specifications.



MeshTool

• Global: Controls the setting and clearing of global element edge

lengths. Pressing the Set button opens a dialog box for setting the

global edge length; pressing the Clear button clears this specification.

[ESIZE]

• Areas: Controls the setting and clearing of edge lengths on selected

unmeshed areas [AESIZE]. Pressing the Set button opens a dialog box

for selecting areas, followed by a dialog box for setting the edge lengh;

pressing the Clear button opens a dialog box for selecting areas to

be cleared of edge length settings.

• Lines: Controls the setting and clearing of the divisions and spacing

ratios on selected unmeshed lines. [LESIZE]

– Pressing the Set button opens a picking dialog for selecting lines,

followed by a dialog box for setting divisions.

– Pressing the Clear button opens a picking dialog for selecting lines

to be cleared of divisions.

– Pressing the Copy button opens a picking dialog to let you copy

line divisions (including spacing ratios) from one line onto other

unmeshed lines.

1. Pick the line from which divisions will be copied.

2. Pick OK in the picking menu.

3. Pick the lines to which the divisions should be copied.

4. Pick OK in the picking menu. If previously-set line divisions exist,

the copied divisions overwrite them.

– Pressing the Flip button opens a picking dialog to let you flip the

spacing ratio of line divisions (from one end to the other) on an

unmeshed line.

1. Pick the line to be flipped.

2. Pick OK in the picking menu.

• Layer: Controls the setting and clearing of layer-mesh controls on lines

for 2-D area meshing. Pressing the Set button opens a picking dialog

for selecting lines, followed by a dialog box for setting layer-mesh

control parameters. Pressing the Clear button opens a picking dialog

for selecting lines; layer-mesh control settings are then removed

without altering the existing line division and spacing ratio settings

for the picked lines. [LESIZE]

• Keypt: Controls the setting and clearing of the edge lengths of the

elements near a selected keypoint or keypoints. Pressing the Set button

opens a picking dialog for selecting keypoints, followed by a dialog

box for setting edge lengths. Pressing the Clear button opens a picking

dialog for selecting the keypoints for which you wish to clear the

keypoint sizing specifications. [KESIZE]



Meshing Controls Mesh: Controls which type of solid model entity is being meshed.

Pressing the option button causes an option menu of available choices

(Volumes , Areas , Lines , and Keypoints ) to appear.

•

• Shape: Controls the shape of the elements used to create a mesh

(quadrilateral, triangle, hexahedral, or tetrahedral). The shape choices

that are presented at a particular time in the MeshTool depend on

what type of solid model entity you are meshing (volume , area , etc.;

see Mesh above) and which meshing type you select (free or mapped;

see Mesher below). If you are meshing lines or keypoints (see

Mesh above), the Shape control is inactive. [MSHAPE]

• Mesher: Controls which type of meshing (free or mapped) is used to

mesh a solid model. If you are meshing lines or keypoints (see Mesh

above), the Mesher control is inactive. Also see the [MSHKEY] com-

mand description.

An additional option in the Mesher section is active if you are

either

1. meshing an area (See Mesh above) and you are using mapped

meshing, or

2. meshing a volume (see Mesh above) and you are using hex

sweeping.

Pressing the options button causes an option menu of available

choices to appear. The choices in this options menu depend upon

if you are area map meshing or volume hex sweeping.

If you are area map meshing (option 1. above), the available

choices will be “3/4 sided” and “pick cornrs.” Choose “3/4 sided”

if you are meshing a 3-- 4-- sided area. Doing so causes a picking

dialog to open when you start the meshing operation (see Mesh

below). Use the picking dialog to pick the area to be meshed.

Choose “Pick cornrs” if you are meshing an area that is bounded

by more than four lines. Doing so will cause a series of picking

dialog boxes to open when you start the meshing operation (see

Mesh below). Use the first picking dialog to pick an area, then

use the second to pick three or four corners of the area. These

corners will be used as the keypoints that define the corners of

the mapped mesh. ANSYS internally concatenates all lines between

the specified keypoints, then meshes the area with all quadrilateral

elements. Also see the AMAP command description.

If you are volume hex sweeping (option 2 above), the available

choices will be “Auto Src/Trg” and “Pick Src/Trg.” Choose “Auto

Src/Trg” for most sweepable volumes. Doing so will cause a picking

dialog to open when you start the sweeping operation (see Sweep

below). Use the picking dialog to pick the volume or volumes to

be swept. When the “Auto Src/Trg” option is chosen, ANSYS intern-

ally attempts to determine which direction the volume can be



MeshTool

swept. In addition, this option allows more than one volume to

be swept at once. Also see the VSWEEP command description.

Choose “Pick Src/Trg” if you first tried “Auto Src/Trg” and ANSYS

could not automatically internally determine the source and target.

In addition, use “Pick Src/Trg” if you want to specify a bias in the

sweep direction or a specific number of element layers in the

sweep direction, both of which are ignored by the “Auto Src/Trg”

option. Choosing the “Pick Src/Trg” option will cause a series of

picking dialog boxes to open when you start the meshing opera-

tion (see Sweep below). Use the first picking dialog to pick a

volume to sweep. Use the second dialog to pick the source area

for sweeping. Finally use the third dialog to pick the target area

for sweeping. This option allows only one volume to be swept at

a time.

• MESH: Starts the meshing operation. Also see the [VMESH, AMESH,

LMESH, KMESH, AMAP] command descriptions.

• SWEEP: Appears in place of the MESH button if Volumes, Hex, and

Sweep is chosen. When chosen, SWEEP issues the VSWEEP command.

See the VSWEEP command descriptions.

• CLEAR: Clears the selected volumes, areas, lines, and keypoints of their

associated nodes and elements. Pressing the CLEAR button opens a

picking dialog box that lets you select the entity to be cleared.

[VCLEAR, ACLEAR, LCLEAR, KCLEAR]

Refinement Controls Refine at:: Controls the general location at which mesh refinement

occurs. Pressing the option button causes an option menu of available

•

choices ( Nodes , Elements , KeyPoints , Lines , Areas , and AllElems ) to appear.

• Refine: Starts the refinement operation. Pressing the Refine button

opens a picking dialog box that lets you select the specific area(s),

line(s), etc. at which you want refinement to occur. Once you've made

your selection, additional dialog boxes are opened to let you set various

refinement options. [AREFINE, LREFINE, KREFINE, EREFINE, NREFINE]



Model Query Picker

ANSYS Function Displays existing information or computes simple geometric/loading in-

formation by picking items in the ANSYS window.

Pick Indicator Enables selection or deselection of items in the active workspace. The

selection in the On Entities: box will determine the type of item (point,

line, area, volume, etc.) that will be selected or deselected by each indi-

vidual pick.

Selection Method You can select individual items (Single), or multiple items within ad-

justable geometrical areas (Box, Polygon, Circle, Loop).

Query Item: You can use the Query Picker to display existing information or to calcu-

late simple geometric, DOF or loading information. The following

items/parameters can be queried:

• Attributes : Displays coordinates, attributes, properties and node

listings (as applicable) for the entities selected in the On Entities: op-

tion.

• Distance Between: Computes distance between two picked nodes or

keypoints.



Model Query Picker

• Angle Between: Computes included angle between three nodes or

keypoints (center, from, to). The angle is displayed in degrees or radians

according to the List Option: Selection.

• Length: Determines length of the selected line.

• Area: Determines the area of the selection.

• Volume: Determines volume of the selection.

• Constraints: Lists constraints for the lines, areas, nodes or keypoints.

• Point Loads: Lists force loads on the nodes or the keypoints.

• Surface Loads: Lists surface loads on one or more nodes, elements,

lines or areas.

• Body Loads: Lists body loads on one or more nodes, elements or

keypoints.

• Initial Conditions: Lists initial conditions for one or more nodes.

On Entities: Lists the specifics of the Query Item: selection.

• Nodes : One or more nodes

• Keypoints : One or more Keypoints

• Lines : One or more lines

• Areas : One or more areas

• Volumes : One or more volumes

• Elements : One or more elements

List Option: Determines the display/measuring system to be used to present the

queried information.

• DSYS Coordinate System

• Layer

• Radius

• RKEY

• Degrees

• Radians

• DISP

• VEL



• Load Labels

Selection Tracking Displays a running count of the number of items picked, the minimum

and maximum number required and the specific label identifier (line,

area, node, or keypoint number, etc.) for the last item picked.

Keyboard Entry Options List of Items: List of all entities selected (default).•

• Min, Max, Inc: Allows you to specify a range and increment of entities

selected.

Generate 3D Annotation Applies the queried information to the model as 3D annotation.

Contact Wizard

You can use the Contact Wizard to create a contact pair for either rigid-to-flexible or flexible-to-flexible

contact. In addition, you can use the wizard to create contact pairs for surface-based constraints. As

you progress through the various dialog boxes in the wizard, remember that the contact pair isn't actually

created until you complete all of the requirements and click the Create button. At any point before

you click Create, you can click the Cancel button to abort the process. You can also return to previous

dialog boxes (and change your settings) by clicking the Back button.

Contact Wizard: Select Target

Use this dialog box to define the target surface.

Target Surface: Select the Target Surface type.

• For 2-D analysis this can be lines, body (areas), nodes, or nodal com-

ponents. TARGE169 is the 2-D target surface element.

• For 3-D analysis this can be areas, body (volumes), nodes, or nodal

components. TARGE170 is the 3-D target surface element.

Target Type: Select the Target Type. For rigid-to-flexible contact, the target surface

must be either Rigid or Rigid w/ Pilot (with a pilot node). For a surface-

based constraint (force-distributed or rigid constraint), you must use the

Pilot Node Only option.

Pick Target ... Click this to launch the target picker. Pick the target surface or nodes

and then click OK to return to this dialog. For rigid-to-flexible analysis,

the picker will only let you select unmeshed surfaces or nodes as the

target.

Next After you have selected the target surface and its parameters, click Next

to continue.

Contact Wizard: Define Pilot Node

Use this dialog box to define the pilot node for a rigid-to-flexible contact pair or surface-based constraint.



Contact Wizard

Pilot Name: (Optional) You can specify a name for a nodal component that will contain

the pilot node. This allows easier interaction with the pilot node later on.

Definition Mode: You can define the pilot node in several ways.

• Allow the program to automatically define the pilot node at the

centroid of selected geometric entities (keypoints, lines, or areas).

Target entities are considered for rigid-to-flexible contact, and contact

entities are considered for a surface-based constraint.

• Pick an existing keypoint, node, or working plane location.

• Type in coordinates in the active coordinate system.

Pick Entity ... Click this to launch the pilot node location picker. Pick the keypoint,

node, or working plane location and then click OK to return to this dialog.

Only one entity or location is allowed.

Next After you have selected the pilot node, click Next to continue.

Contact Wizard: Select Contact

Use this dialog box to define the contact surface.

Contact Surface: Select the Contact Surface type.

• For 2-D analysis this can be keypoints (node-to-surface contact only),

lines, body (areas), nodes, or nodal components.

• For 3-D analysis this can be lines (node-to-surface contact only), areas,

body (volumes), nodes, or nodal components.

Contact Element Type: This option determines the specific element type that will be used. For

Surface-to-Surface contact, CONTA172 (2–D) or CONTA174 (3-D) will be

used as the contact element type. For Node-to-Surface contact, CONTA175

will be used (2-D or 3-D).

Pick Contact ... Click this to launch the contact picker. Pick the keypoints, lines, surface,

or nodes and then click OK to return to this dialog. Note that in a 2-D

analysis, only lines and keypoints that are part of areas are valid selections

and, therefore, only these are shown.

Next After you have selected the contact surface and its parameters, click Next

to continue.

Contact Wizard: Set Parameters and Create

Flexible-to-Flexible or Rigid-to-Flexible Contact Pair

Use this dialog box to specify parameters for your contact analysis and create the contact pair. This

dialog provides some of the most commonly used parameters. The Optional settings button lets you

select additional parameters.



The Contact Wizard automatically detects which degrees of freedom are active in your model (based

on element type):

• If only structural degrees of freedom are detected, thermal, electric, and magnetic options for contact

are ignored and KEYOPT(1) is set to 0.

• If structural and thermal degrees of freedom are detected, electric and magnetic contact options are

ignored and KEYOPT(1) is set to 1.

• If only the thermal degree of freedom is detected, thermal options are available and KEYOPT(1) is set

to 2. Heat generation due to friction is ignored.

• If structural, thermal, and electric degrees of freedom are detected, all contact options except mag-

netic are available and KEYOPT(1) is set to 3.

• If thermal and electric degrees of freedom are detected, all structural and magnetic contact options

are ignored and KEYOPT(1) is set to 4.

• If structural and electric degrees of freedom are detected, all thermal and magnetic options are ignored

and KEYOPT(1) is set to 5.

• If only the electric degree of freedom is detected, electric options are available and KEYOPT(1) is set

to 6.

• If only the magnetic degree of freedom is detected, magnetic options are available and KEYOPT(1)

is set to 7.

Create symmetric pair When on, two companion (symmetric) contact pairs will be created in-

stead of a single pair. The contact surface of each pair is identical to the

target surface of its companion pair, and vice versa. Although they will

use different real constant and element type IDs, both pairs will have the

same settings. This symmetric pair capability is applicable to flexible-to-

flexible contact only.

Include initial penetration When on, initial penetration includes the geometrical penetration. When

off, initial penetration is excluded.

Friction: Select the material ID and then set the coefficient of friction (any non-

negative value). You can use this to create a new material ID. Also, a

coefficient of friction value entered here will overwrite any previously

entered value.

Only isotropic friction can be defined through the Contact Wizard.

For a detailed description of the friction model and information on

how to define orthotropic friction (available for 3-D contact only),

see Choosing a Friction Model.

Thermal Contact Conduct-

ance:

For a thermal analysis, input the thermal conductance between the two

contacting surfaces. You can input a constant value or a table. The drop-

down list box lists all tables that have been defined.

Electric Contact Conduct-

ance:

For an electric current conduction analysis, input the electrical conduct-

ance between two contacting surfaces if KEYOPT(1) = 3 or 4, or input the

electrical capacitance per unit area between two contacting surfaces for

piezoelectric (KEYOPT(1) = 5) or electrostatic (KEYOPT(1) = 6) analyses.



Contact Wizard

You can input a constant value or a table. The drop-down list box lists

all the tables that have been defined.

Magnetic Contact Per-

meance:

For a magnetic field analysis, input the magnetic permeance at the con-

tact interface. You can input a constant value or a table. The drop-down

list box lists all the tables that have been defined.

Optional settings ... This button launches the Contact Parameters dialog box. These settings

provide a finer degree of control over your contact analysis.

Create Click this button to create the contact pair.

Contact Wizard: Set Parameters and Create

Surface-based Constraint Contact Pair (Pilot Node Only)

Use this dialog box to specify parameters for your analysis and create the contact pair that will support

a surface-based constraint.

Constraint Surface Type: The constraint surface type is either Rigid Constraint or Force-distributed

Constraint. See Surface-based Constraints for more information.

Boundary Conditions on

Target:

The boundary conditions on the pilot node (target) can be either user-

specified or set automatically based on the dimensionality of the model.

Constrained DOF Set on

Target:

Only checked degrees of freedom will be constrained according to the

constraint surface type. The All DOFs button sets all available degrees

of freedom to be included in the constrained DOF set.

Create Click this button to create the contact pair.

Flip Normals

This dialog box indicates that the contact pair was created and lists the real set ID for the contact pair.

At this point, you should check the normals for the contact pair.

The node order of the target surface elements is critical because it defines contact direction. For 2-D

contact, the associated contact elements must lie to the right of the target surface when moving from

the first node to the second node along the target surface line.

For 3-D contact, the target element numbering should be such that the surface's outward normal points

toward the contact surface. The outward normal is determined by the right-hand rule.

If the element normals do not point toward the contact surface, click Flip Target Normals to reverse

the direction of the surface normals. Click Finish when you have verified that the direction of the normals

is correct.

Finish

This dialog box indicates that the contact pair was created and lists the real set ID for the contact pair.

Each contact pair is identified via the same real constant number.



Contact Properties

The following are the tabs on the Contact Properties dialog box for creating a contact pair.

• Basic

• Friction

• Initial Adjustment

• Misc

• Rigid target

• Thermal

• Electric

• Magnetic

• Constraint

• ID

Note

Not all of the above tabs will be available at all times. The tabs that are presented in the GUI

and the options shown on each tab will vary depending on the type of contact pair you

define, and the location from which you access the Contact Properties dialog (from the

Contact Wizard or from the Contact Manager).

Contact Properties: Basic

The Basic tab contains general properties related to contact behavior and convergence.

You should first try running your contact analysis using the default settings, then change settings only

if you encounter difficulties or have special situations in your analysis.

Use the questions below to assist you in determining if you need to change any of the default settings

based on special situations.

These questions are intended only as hints to guide you in your decision to adjust any of the

contact properties and may not cover all possible uses of these parameters. You are advised to

review the information in the linked sections (shown below) even if the questions do not apply

directly to your situation. The linked sections provide a more complete description on how the

parameters can be used.

For this dialog box, the <auto> option indicates that you are choosing a default value, the factor radio

button indicates that you are setting a scaling factor, and the constant radio button indicates that you

are setting a constant.



Contact Properties

Adjust this tab entry ...Question

Normal penalty stiffness [FKN]Are you modeling slender structures or other bending dom-

inated problems?Contact algorithm [KEYOPT(2)

= 0, 1]

Penetration tolerance [FTOLN]Does your model exhibit a highly varying mesh density?

Does your solution diverge due to chattering?

Pinball region [PINB]Are you experiencing spurious contact because a target

segment is far from a contact element, even though penetra-

tion exists?

Behavior of contact surface [KEY-

OPT(12)]

Is the contact surface behavior other than standard unilateral

contact (that is, other than when normal pressure equals zero

if separation occurs)?

Contact stiffness update [KEY-

OPT(10)]

Do you need to account for large strain effects (for example,

necking down) that change the underlying element's stiff-

ness?

Do you need to update the normal or tangential contact

stiffness more often than at each load step?

Contact algorithm [KEYOPT(2)]Does your model have very distorted elements, a high coef-

ficient of friction, and/or poor convergence behavior when

using the default augmented Lagrange method?

Contact algorithm [KEYOPT(2) = 2]Do you need to build multipoint constraints (MPC) for assem-

blies?

Contact algorithm [KEYOPT(2) = 3,

4]

Is the amount of penetration in your model not acceptable?

Allowable tensile contact pressure

[TNOP]

If you are using the Lagrange/penalty algorithm (KEYOPT(2)

= 3) or pure Lagrange multiplier method (KEYOPT(2) = 4),

does your solution diverge due to chattering?

Location of contact detection [KEY-

OPT(4)]

Are you modeling corner, point-to-surface, or edge-to-surface

contact and using CONTA171, CONTA172, CONTA173, or

CONTA174?

Contact normal [KEYOPT(4)]Is the contact region smoother than the target surface (using

CONTA175)?

Type of constraint [TARGE170, KEY-

OPT(5)]

If you are using the MPC algorithm, do you need to constrain

any rotational degrees of freedom?

Related Elements: CONTA171, CONTA172, CONTA173, CONTA174, CONTA175

Contact Properties: Friction

The Friction tab contains parameters related to static and dynamic friction at the contact interface.















The Material ID and Friction Coefficient entries replicate the entries on the Contact Properties: Set

Parameters and Create dialog box. Use these entries on the Friction tab to create a new material ID

or to enter a revised friction coefficient that will overwrite the existing one. (Note that only isotropic

friction is available through this dialog box. See Choosing a Friction Model for information on how to

define orthotropic friction, which is available for 3-D contact only.)

Adjust this tab entry ...Question

Tangent penalty stiffness [FKT]Does your analysis involve tangential (sliding) contact stiffness

that is significantly different from the normal contact stiffness?

Allowable elastic slip [SLTO]Are you updating contact stiffness at each iteration [KEYOPT(10)

= 2] and have a need to enhance convergence even though

accuracy may be compromised?

Contact cohesion [COHE]Do you need to include sliding resistance in your simulation

when there is zero normal pressure?

Maximum friction stress [TAU-

MAX]

Does your analysis involve a bulk metal forming process or

similar situation where the contact pressure can become very

large?

Stiffness matrix [NROPT ]Do frictional stresses have a substantial influence on the overall

displacement field?

Is the magnitude of the frictional stresses highly solution depend-

ent?

Are you having convergence problems with contact simulations

that involve friction?

Static/dynamic ratio [FACT]Are the static and dynamic coefficients of friction unequal?

Exponential decay coefficient

[DC]

If the static and dynamic coefficients of friction are unequal,

should a friction decay time be simulated?


Contact Properties: Initial Adjustment

The Initial Adjustment tab contains advanced penetration and surface offset parameter settings.







Contact Properties









Initial penetration [KEYOPT(9)]Does your model contain an initial geometric penetra-

tion such that contact forces would immediately be

“stepped” to a large value (such as an interference fit)?

Contact surface offset [CNOF]Are you modeling initial interference contact problems

(such as shrink fit assemblies)?

Automatic contact adjustment [KEY-

OPT(5)]

Do you need to prevent rigid body motion before

contact occurs?

Initial contact closure [ICONT]Do you need to prevent rigid body motion before

contact occurs?

Lower boundary - Initial Allowable Pen-

etration Range [PMIN]


contact occurs?

Upper boundary - Initial Allowable Pen-

etration Range [PMAX]


contact occurs?


Contact Properties: Miscellaneous

Use the Miscellaneous tab to specify the following settings for your contact analysis.

If the factor button is checked, the value entered into the field is used as a scaling factor. If the constant

button is checked, the value entered is used as a constant.

Contact opening stiffness This sets a constant value or scaling factor for the FKOP real constant.

For modeling either no-separation or bonded contact, you may need to

set this value. This provides a stiffness factor applied when contact opens.

If a constant value is not selected, the true contact opening stiffness

equals FKOP* the contact stiffness applied when contact closes. The de-

fault FKOP value is 1.

No separation and bonded contact generate a "pull-back" force when

contact opening occurs, and that force may not completely prevent

separation. To reduce separation, define a larger value for FKOP.

Also, in some cases separation is expected but a connection must

be maintained to prevent rigid body motion. In such instances, you

can specify a small value for FKOP to maintain the connection

between the contact surfaces while allowing separation to occur

(this is a "weak spring" effect). This setting is ignored for Standard

and Rough settings for Behavior of contact surface (Basic tab).



Target edge extension

factor

This sets the value for real constant TOLS, which is used to add a small

tolerance that will internally extend the edge of the target surface. TOLS

is expressed in percentage units. A small value is usually efficient. The

default value is 10 for small deflection and 2 for large deflection.

Pressure penetration cri-

terion

When a fluid pressure penetration load is applied at the contact interface,

the pressure penetration criterion (real constant PPCN) is used to determ-

ine when the pressure penetrates. When the contact pressure is less than

the criterion, fluid pressure starts to penetrate. When the contact pressure

is greater than the criterion, fluid pressure is cut off.

Fluid penetration acting

time


the fluid pressure can be ramped linearly over a time period, during one

or several substeps. To implement this ramping option, enter a fluid

penetration acting time (real constant FPAT). You can enter a fraction of

the time increment of the load step (factor) or an absolute acting time

(constant).

Fluid penetration load re-

mains constant


you can indicate whether the fluid penetration load varies during itera-

tions based on the current contact status (default), or whether it remains

constant over the substep.

Asymmetric contact selec-

tion

When there are several contact pairs involved in the model, and the

graphical picking of contact and target surfaces is difficult, you can just

define the symmetric contact pairs. When you choose this option, ANSYS

internally selects which asymmetric pairs are to be used at the solution

stage.

Beam/shell thickness ef-

fect

By default, ANSYS does not account for the element thickness, beams

and shells are discretized at their mid-surface, and the penetration dis-

tance is calculated from the mid-surface. You can account for the thick-

ness of shells (2-D and 3-D) and beams (2-D) by using this option. When

this option is active, the distance of contact is calculated from either the

top or the bottom surface and

• For rigid-to-flexible contact, ANSYS will automatically shift the contact

surface to the bottom or top of the shell/beam surface.

• For flexible-to-flexible contact, ANSYS will automatically shift both the

contact and target surface (if they are attached to shell/beam elements).

When building your model geometry, if you are going to account

for thickness, remember the offsets which may come from either

contact surface or target surface or from both. When you specify a

contact offset and activate this option, it is defined from the top or

bottom of the shell/beam, not the mid-surface. When used with

SHELL181, SHELL208, or SHELL209, changes in thickness during de-

formation are also taken into account.

Element time increment Time step control is an automatic time stepping feature that predicts

when the status of a contact element will change or cuts the current

time step back. Select one of four actions to control time stepping:



Contact Properties

No control: The time step size is unaffected by the prediction. This

setting is appropriate for most analyses when automatic time stepping

is activated and a small time step size is allowed.

•

• Automatic bisection: Time step size is bisected if too much penetration

occurs during an iteration, or if the contact status changes dramatically.

• Maintain reasonable: Predict a reasonable increment for the next

substep.

• Achieve minimum: Predict a minimal time increment for the next

substep.

• Use Impact Constraints: Activate energy and momentum conserving

contact in transient dynamic analysis.

Superelement usage The surface-to-surface contact elements can model a rigid body (or one

linear elastic body) contacting another linear elastic body undergoing

small motions. These elastic bodies can be modeled using superelements,

which greatly reduces the number of degrees of freedom involved in the

contact iteration. Remember that any contact or target nodes must be

one of the master nodes of the superelements.

Since the superelement consists only of a group of retained nodal

degrees of freedom, it has no surface geometry on which ANSYS

can define a contact and target surface. Therefore, the contact and

target surface must be defined on the surface of the original ele-

ments before they are assembled into a superelement. Information

taken from the superelement includes nodal connection and as-

sembly stiffness, but no material property or stress states (whether

axisymmetric, plane stress, or plane strain). One restriction is that

the material property set used for the contact elements must be the

same as the one used for the original elements before they were

assembled into superelements.

The following selections are valid:

• No superelement used

• Axisymmetric

• Plane strain or plane stress with unit thickness

• Plane stress with thickness input - The thickness (real constant

R2) is set through the field below.

Note

The above bulleted options are not available if you

are using CONTA175. However, the Contact Wizard

does provide the Contact Model capability, which

allows you to base the contact model either on

contact force or contact traction.



Contact model -- For the CONTA175 element, the

contact model can be either contact force based

(KEYOPT(3) = 0, default) or contact traction based

(KEYOPT(3) = 1). For the contact traction based

model, ANSYS can determine the area associated

with contact nodes. For the single point contact case,

a unit area will be used which is equivalent to the

contact force based model.

Contact Properties: Rigid Target

Use the Rigid target tab to specify the following settings for your contact analysis.

Boundary condition on tar-

get nodes

The boundary conditions on the target can be either automatically con-

strained or user specified.

For the Auto constrained option (the default), ANSYS checks the

boundary conditions for each target surface. If all of the conditions

listed below are met, then ANSYS treats the target nodes along the

respective degree of freedom as fixed:

• There are no explicit boundary conditions or prescribed forces for target

surface nodes.

• Target surface nodes are not connected to other elements.

• No constraint equations or node couplings have been used to constrain

target surface nodes.

At the end of each load step, ANSYS release the constraint conditions

that were set internally.

The constraint conditions stored in the result file (Jobname.RST )

and the database file (Jobname.DB ) may be updated due to this

change. You should carefully verify whether the current constraint

conditions are as expected before restarting an analysis or resolving

the problem in interactive mode.

If you wish to control the constraint conditions of target nodes, select

User specified.

Area elements have Defines whether 3–D rigid target surfaces were meshed with high-order

(midside nodes) or low-order target elements.

Pilot Node You can define or modify the pilot node using these options:

• Pilot Name (optional) - You can specify a name for a nodal component

that will contain the pilot node. This allows easier interaction with the

pilot node later on.

• Pilot Node - You can create or modify (delete/move) a pilot node using

one of the listed methods. The definition methods include an automatic

method (at centroid of target elements), picking methods (pick existing



Contact Properties

keypoint, node, or working plane location), and direct input of coordin-

ates in the active coordinate system. Pick Choose location ... to launch

the pilot node location picker or input the node coordinates. The pilot

node is not created or modified until after you pick OK in the Contact

Properties dialog.

Contact Properties: Thermal

Use the Thermal tab to specify the following settings for your contact analysis.

Thermal Contact Conduct-

ance

This sets the real constant TCC.

The conductive heat transfer between two contacting surfaces is

given by:

q = TCC X (Tt - Tc)

where:

q is the heat flux per area,

TCC is the thermal contact conductance coeffi-

cient, and

Tt and Tc are the temperatures of the contact

points on the target and contact surfaces.

TCC can be input as a constant value or as a table.

In a table, TCC can be a function of temperature,

pressure, time, and location. The drop-down list box

lists all tables that have been defined.

Stephan-Boltzmann con-

stant

This sets the real constant SBCT used to model radiation.

Heat transfer through radiation is given by:

q = RDVF x EMIS x SBCT [(Te + TOFFST)4 - (Tc +

TOFFST)4]

where:

TOFFST is the temperature offset from absolute zero to zero

(defined through the TOFFST command.)

EMIS is the surface emissivity.

RDVF is the radiation view factor.

Radiation View factor This sets the real constant RDVF. The radiation view factor can be input

as a constant value or as a table. In a table, RDVF can be a function of

temperature, gap distance, time, and location. The drop-down list box

lists all tables that have been defined.

Emissivity This sets the surface emissivity (MP,EMIS).

Frictional heating factor This sets the real constant FHTG used to model heat generation due to

frictional sliding.



The rate of frictional dissipation is given by:

q = FHTG x τ x V

where:

τ is the equivalent frictional stress.

V is the sliding rate.

FHTG is the fraction of frictional dissipated energy converted

into heat (defaults to 1).

Dissipation weight factor This sets the real constant FWGT used to model heat generation due to

frictional sliding. It is the weight factor for the distribution of heat

between the contact and target surfaces (defaults to 0.5).

The amount of frictional dissipation on contact and target surfaces

is given by:

qc = FWGT x FHTG x τ x V

and

qT = (1 - FWGT) x FHTG x t x V

where:

qc is the amount of frictional dissipation on the contact side.

qT is the amount of frictional dissipation on the target side

FWGT defaults to 0.5.

Thermal contact behavior This sets KEYOPT(3) for target elements TARGE169 and TARGE170. There

are two options for thermal contact behavior:

• Based on Contact Status (KEYOPT(3) = 0). This is the default option.

• Treated as Free Surface (KEYOPT(3) = 1).

For KEYOPT(3) = 0, the thermal contact behavior depends on contact

status as follows:

• Closed Contact -- Thermal contact conduction transfers heat between

two contacting surfaces.

• Frictional Sliding -- Frictional dissipated energy generates the heat to

both the contact and target surfaces.

• Near-Field Contact -- Both heat convection and radiation between the

contact and target surfaces is taken into account. The external flux

value contributes to the contact surface.

• Far-Field Contact -- Heat convection and radiation between the contact

surface and the environment is taken into account. The external flux

value only contributes to both contact and target surfaces.



Contact Properties

If you choose the free surface contact behavior, ANSYS considers both free surface radiation and con-

vection as long as open contact is detected. In this case, there is no convection or radiation heat

transfer between the contact and target surfaces.

Contact Properties (Constraint Type): Constraint

The Constraint tab contains general parameters related to the behavior of surface-based constraint

contact pairs. Surface-based constraints are used to couple the motion of nodes on the contact surface

to a single pilot node on the target surface. A surface-based constraint requires the multipoint constraint

(MPC) contact algorithm (KEYOPT(2) = 2). (This KEYOPT is set automatically if you use the Contact Wizard

to create the contact pair.)

Constraint surface type When the multipoint constraint (MPC) algorithm is used, KEYOPT(4) de-

termines the surface-based constraint type. Two types are available:

• Force-distributed constraint surface - In this type of constraint, forces

or displacements applied on the pilot node are distributed to contact

nodes (in an average sense) through shape functions (similar to a

constraint defined by the RBE3 command).

• Rigid constraint surface - In this type of constraint, the contact nodes

are constrained to the rigid body motion defined by the pilot node

(similar to a constraint defined by the CERIG command).

Boundary conditions on

target

The boundary conditions on the target node can be either automatically

constrained or user specified.

For the Auto constrained option (the default), ANSYS checks the

boundary conditions for the target node. If all of the conditions listed

below are met, then ANSYS treats the target node along the respect-

ive degree of freedom as fixed.

• There are no explicit boundary conditions or prescribed forces for the

target node.

• The target node is not connected to other elements.

• No user-specified constraint equations or node couplings have been

used to constrain the target node.

At the end of each load step, ANSYS release the constraint conditions

that were set internally.

The constraint conditions stored in the result file (Jobname.RST )

and the database file (Jobname.DB ) may be updated due to this

change. You should carefully verify whether the current constraint

conditions are as expected before restarting an analysis or resolving

the problem in interactive mode.

If you wish to control the constraint conditions of the target node,

select User specified.



Constrained DOF set on

target

KEYOPT(4) of the target element is used to specify the degrees of freedom

to be constrained. A checked box indicates the DOF is active, and an

empty box indicates the DOF is inactive.

Pilot Node You can modify the pilot node using these options:

• Pilot Name (optional) - You can specify a name for a nodal component

that will contain the pilot node. This allows easier interaction with the

pilot node later on.

• Pilot Node - You can modify a pilot node using one of the listed

methods. The definition methods include an automatic method (at

centroid of contact elements), picking methods (pick existing keypoint,

node, or working plane location), and direct input of coordinates in

the active coordinate system. Pick Choose location ... to launch the

pilot node location picker or input the node coordinates. The pilot

node is not modified until after you pick OK in the Contact Properties

dialog.

Contact Properties: ID

Use the Identification tab to specify ID numbers for your contact pair. By default ANSYS will assign the

numbers shown in the various fields.

Contact pair real set ID A contact pair must share the same real constant set number. You can

use this field to assign any number that you wish, or accept the value

shown. After the contact pair is created, you cannot change this number.

Target element type ID ANSYS automatically creates this ID.

Contact element type ID ANSYS automatically creates this ID.

If you are creating symmetric contact pairs in the Contact Wizard, the following fields are also shown.

Companion contact pair

real set ID

The companion pair must use a different real constant set number. You

can use this field to assign any number that you wish, or accept the value

shown. After the contact pair is created, you cannot change this number.

Companion target element

type ID

ANSYS automatically creates this ID.

Companion contact ele-

ment type ID

ANSYS automatically creates this ID.



Contact Properties

Define Material Model Behavior

Use the Define Material Model Behavior dialog box to specify material properties, material models

and model combinations. There is a pull down menu bar, and two interactive scrollable tree structure

windows, as described below:

Material Allows you to specify a unique material model number, or allows you to

exit the Define Material Model Behavior dialog box. Choices are as

follows:

• New Model: Opens a dialog box where you specify a unique ID number

for the material model you are defining. You do not need to choose

this option when you define the first model. ANSYS automatically as-

signs number 1 to this model.

• Exit: Closes the Define Material Model Behavior dialog box. All set-

tings are retained if you open this dialog box again in the current

ANSYS session.

Edit Allows you to copy or delete material models.

• Copy: Opens a dialog box where you copy the contents of an existing

material model to a new material model by specifying model numbers

(for example, copy the contents of existing Material Model Number 1

to become the contents of new Material Model Number 3). The copied

material model is listed in the Material Models Defined window (de-

scribed below) with its new number. Its contents are identical to the

model whose contents you copied.

• Delete: Deletes a material model after you highlight its name in the

Material Models Defined window (described below).

Material Models Defined Displays a list of each material model number you have specified in the

Material Models Available tree structure window (described below).

This list appears after you have chosen OK in the material data input



dialog box associated with your chosen material property or model. The

Material Models Defined tree structure window displays the number

of each model, along with a small icon to the left of each item. If you

double-click on the item, a list appears of the material properties that

you entered for that item. The list appears indented below the model

number. Double-clicking on any listed material name displays the associ-

ated material data input dialog box, where you can edit the data.

Material Models Available Displays a list of material categories (for example, Structural, Thermal,

Electromagnetics). When you double-click on a category , sub-categories

appear indented and below the category (for example, under Structural

are categories Linear and Nonlinear, and others). If you double-click fur-

ther on the subcategories, you will eventually see a vertical list of mater-

ial models that are included under that category (for example, under

Hyperelastic are categories Mooney-Rivlin, Ogden, Neo-Hookean, and

others). This logical, top-down arrangement of material categories is in-

tended to assist you in choosing the appropriate model for your analysis.

Once you have decided which model you will use, you then choose it

by double-clicking on the item. A dialog box appears that prompts you

for the required input data for that property or model only (for example,

material constants associated with the Ogden model). When you click

on OK in the dialog box, the material number is listed in the Material

Models Defined tree structure window.

For a structural analysis, several inelastic material models (listed by

double-clicking on the following in the tree structure: Structural,

Nonlinear, Inelastic) require you to input values for elastic material

properties (elastic modulus and/or Poisson's ratio) in addition to the

inelastic constants that are specific to the model (for example, Yield

Stress and Tangent Modulus for the Bilinear Isotropic Hardening

model). In these instances, you must enter the elastic material

properties before you enter the inelastic constants. If you try to enter

the inelastic constants first, a Note appears stating that you must

first enter the elastic properties. After you click on OK in the Note,

a dialog box appears that prompts you for the elastic material

properties. After you enter these properties and click on OK, a dialog

box appears that prompts you for the inelastic constants associated

with the specific model you chose.

When entering constants for a combination model (for example, Bi-

linear Kinematic and Chaboche), after you enter constants for the

first model and click on the OK button, the material input dialog

box for the second model then appears where you can enter the

constants for the second model.

Video Demonstrations for PC Users

Video demonstrations are available that show basic techniques on defining material models, displaying

material properties, and material curve fitting. If you are a PC user, you can view one of these videos

by pointing your Internet Explorer browser to one of the following URL addresses:

• Defining One Material Model: http://www.ansys.com/staticassets/ANSYS/staticas-sets/techmedia/one_material.html



Define Material Model Behavior

• Adding a Temperature Dependent Material Model: http://www.ansys.com/staticassets/AN-SYS/staticassets/techmedia/add_temp_material.html

• Graphing a Temperature Dependent Material Property: http://www.ansys.com/staticassets/AN-SYS/staticassets/techmedia/graph_temp_material.html

• Material Curve Fitting: http://www.ansys.com/staticassets/ANSYS/staticassets/tech-media/material_curve_fitting.html

For more information about the Define Material Model Behavior dialog box, see:

• Material Model Interface in the Basic Analysis Guide (includes examples).

• Using Tree Structures in the Operations Guide.

• Material Curve Fitting in the Structural Analysis Guide.

For more information about data input dialog boxes, see Entering Material Data in the Basic Analysis

Guide.

Define Material ID

Define Material ID text field -- Allows you to specify a unique ID number for the material model you

are defining. After you choose OK in this dialog box, all subsequent material information that you enter

is assigned to this number. If you then specify another ID number and choose OK, material information

that you enter is assigned to this latest ID number. The ID number that appears in the field by default

is one number higher than the highest Material Model Number that appears in the Material Models

Defined window. When you define the first model, it is not necessary for you to use this dialog box.

ANSYS automatically assigns Material Model Number 1 to the first model.

For more information related to the Define Material ID dialog box, see the MP and TB commands in

the Command Reference.



BeamTool

ANSYS Function Use the BeamTool to create beam cross sections. You may select a pre-

defined cross section shape or define an arbitrary shape.

ID The ID number of the cross section [SECTYPE].

Name The name of the cross section, 8 alphanumeric characters maximum

[SECTYPE].

Sub-Type The cross section subtype. Clicking the Sub-Type button displays a drop-

down list of predefined shapes.

• RECT creates a rectangular cross section.

• QUAD creates a quadrilateral cross section.

• CSOLID creates a circular solid cross section.

• CTUBE creates a circular hollow cross section.

• CHAN creates a U-shaped cross section.

• I creates an I-shaped cross section.

• Z creates a Z-shaped cross section.

• L creates an L-shaped cross section.

• T creates a T-shaped cross section.



BeamTool

• HATS creates a hat-shaped cross section.

• HREC creates a hollow rectangular cross section.

• ASEC creates a user-defined shape for a cross section.

Section Offsets The section offset for the cross sec-

tion [SECOFFSET]. Selecting the Off-

Offset To

set To button displays a drop-down

list with the following options:

• Centroid : Beam node will be

offset to centroid (default).

• Shear Cen : Beam node will be

offset to Shear Center.

• Origin : Beam node will be offset

to origin of the cross section.

• Location : Beam node is offset to

the user-specified location set in

the Offset-Y and Offset-Z fields:

Offset-Y, Offset-Z Values that locate the node with re-

spect to the default origin of cross

section when the Location option

is chosen.

Section Shape The shape of the cross section.

Dimension Labels Geometry information for each dimension [SECDATA]:

Rectangular Cross Section Dimensions

• B = Width

• H = Height

• Nb = Number of cells along width, default

= 2

• Nh = Number of cells along height, default

= 2



Quadrilaterial Cross Section Dimensions

• yI, zI, yJ, zJ, yK, zK, yL, zL = Coordinate

location of various points

• Ng = Number of cells along g, default = 2

• Nh = Number of cells along h, default = 2

Note

Degeneration to triangle is

permitted by specifying the

same coordinates for nodes

along an edge.

Circular Solid Cross Section Dimensions

• R = Radius

• N = Number of divisions along the circumfer-

ence

• T = Number of divisions through the radius

Hollow Circular Cross Section Dimensions

• Ri = Inner radius of the tube

• Ro = Outer radius of the tube

• N = Number of cells along the circumfer-

ence; default = 8

Channel Cross Section Dimensions

• W1, W2 = Lengths of the flanges

• W3 = Overall depth

• t1, t2 = Flange thicknesses

• t3 = Web thickness



BeamTool

I-shaped Cross Section Dimensions

• W1,W2 = Width of the top and bottom

flanges


• t1,t2 = Flange thicknesses

• t3 = Web thickness

Z-shaped Cross Section Dimensions

• W1,W2 = Flange lengths


• t1,t2 = Flange thicknesses

• t3 = Stem thickness

L-shaped Cross Section Dimensions

• W1, W2 = Leg lengths

• t1, t2 = Leg thicknesses

T-shaped Cross Section Dimensions

• W1 = Flange width


• t1 = Flange thickness

• t2 = Stem thickness



Hat-shaped Cross Section Dimensions

• W1,W2 = Width of the brim

• W3 = Width of the top of the hat


• t1,t2 = Thickness of the brim

• t3 = Thickness of the top of the hat

• t4,t5 = Web thicknesses

Hollow Rectangular Cross Section Dimen-

sions

• W1 = Outer width of the box

• W2 = Outer height of the box

• t1, t2, t3, t4 = Wall thicknesses

Arbitrary Cross Section Dimensions

• A = Area of section

• Iyy = Moment of inertia about the y axis

• Iyz = Product of inertia

• Izz = Moment of inertia about the z axis

• Iw = Warping constant

• J = Torsional constant

• CGy = Y coordinate of centroid

• CGz = Z coordinate of centroid

• SHy = y coordinate of shear center

• SHz = z coordinate of shear center

The SECPLOT command cannot display

the plot of an arbitrary section (ASEC)



BeamTool

subtype. However, consider issuing the

/ESHAPE command to display the orient-

ation of the section.

Mesh Refinement Sets mesh refinement level for thin-walled sections. Values are 0 (the

default - no mesh refinement) to 5 (high level of mesh refinement).

Action Buttons Preview: Displays a sample cross section using the specified shape and

dimension information without applying this information to the ANSYS

database.

Meshview: Same as Preview except section mesh is also displayed.

2-D and 3-D Annotation

ANSYS Function Use a variation of this dialog for annotating your ANSYS display with text

and graphics. 2-D Annotation can be considered an overlay of your exist-

ing ANSYS display. As such, the underlying display can change without

changing the defined annotation. 3-D annotation is applied directly to

the XYZ coordinates of the hot spot of the anchor item you choose, and

will remain attached (within reason) even when the model is rotated,

moved, or resized.

Annotation Entity Select an entity from the list of annotation entities from the top pull

down menu on the dialog box.

3-D2-D

TextText

LinesLines

AreasRect-angle

Sym-bols

Circles

Ar-rows

Arcs

Bit-maps

Polygon

Op-tions

Wedges

Pies

Symbols

Dimen-sions

Arrows

Bitmaps



3-D2-D

Options

Note

Each Annotation Entity is initiated, generated and

closed (saved) in a specific manner. The ANSYS status

bar will contain instructions (prompts) for each step

in the annotation process.

Annotation Anchor Available for 3-D annotations only. Use this pull-down menu to choose

the item to apply your annotation to. You can apply 3-D annotations to

any of the standard ANSYS geometry and analysis model items (nodes,

elements, keypoints, lines, areas and volumes), to XYZ coordinates that

you specify, or to “picked” points in free space. Your Annotation Entity

will be applied to the centroid of the anchor item (if applicable), and will

remain attached (within reason) even when the model is rotated, moved,

or resized.

Annotation Controls This area will change according to the annotation entity you choose. The

following defines the controls available for each entity. When you choose

“Options ”, the anchor type is grayed out and does not apply.

Areas Annotation areas attach the first

vertex of your area to the item, point,

or centroid of your defined anchor.

Subsequent picks create lines that

define the sides, and a final double-

click closes the sides to create an

area.

Choose Rectangle , Circle ,

Pie , Polygon , or Wedge to

annotate shapes. With the op-

tion shown in this box, you can

create 2-D annotation shapes of

different interior and exterior

color, and with solid or dashed

borders of different widths.

Color The

fill

col-

or

of

your

defined

area

(if

Filled

is




chosen

be-

low).

Hollow / Filled Areas

and

shaptes

can

be

full

opaque,

or

only

an

edge

line.

If

Hol-

low

is

chosen,

the

col-

or

and

line

type

will

be

de-

term-

ined

by

the

se-

lec-

tions

that

fol-

low

for

Edge

Col-

or

and

Edge

Line

Type

(Sol-

id

or

Dashed).



Show Edge Val-

id

only

if

Filled

is

chosen.

Show-

ing

the

edge

al-

lows

you

to

ap-

ply

a

dif-

fer-

ent

col-

or

to

the

out-

line

of

an

area.

Edge Color Se-

lect

the

col-

or

to

be

ap-

plied

to

filled

area

or

shapes

and

to

the

out-

line

if

Hol-

low




is

se-

lec-

ted.

Solid / Dashed Defines

the

edge

as

a

sol-

id

or

dashed

line.

Edge Width This

slider

bar

al-

lows

you

to

vary

the

width

of

your

edge

in

pro-

por-

tion

to

the

size

of

your

area

or

shape.

Ad-

just

width

be-

fore

de-

fin-

ing

the

area

or

shape.



Arrows or Symbols Annotation Arrows attach the head

or tail to the item, point, or entity's

centroid, as defined by your anchor.

Your initial click starts the arrow, and

subsequent clicks allow you to apply

"bends" to the arrow tail. The final

right mouse click applies the arrow-

head and finishes the annotation.

Unlike Bitmap Files, which are

placed on your model at a fixed

size and color, Symbols can be

sized and defined according to

your requirements. Symbolswill not change size when you

alter the view of your model, but

can be modified using the Op-tion sizing capability.

Type De-

term-

ines

the

dir-

ec-

tion

of

the

ar-

row's

con-

struc-

tion

(as

you

pick)

-

-

head

to

tail

or

tail

to

head.

The

avail-

able

sym-

bols

are:

ar-rows ,




dashes ,

circles ,

tri-anglesor

stars .

Size Use

this

slider

to

ad-

just

the

over-

all

size

(height

and

width)

of

your

sym-

bols

or

the

size

of

the

ar-

row

head,

al-

low-

ing

you

to

spe-

cify

the

pro-

por-

tions.

Modi-

fy

this

set-

ting

for

very

short

or



very

long

lines

so

that

ar-

rows

and

sym-

bols

are

pro-

por-

tion-

al

to

the

line

length.

Color Choose

the

ar-

row

or

sym-

bol

col-

or

from

the

pull-

down

menu.

Width Move

the

slider

to

the

de-

sired

line

width

be-

fore

de-

fin-

ing

the

ar-

row

or




sym-

bol.

The

thick-

ness

of

the

nor-

mal

ar-

row

or

sym-

bol

will

be

the

same

as

the

line

thick-

ness

you

se-

lect

with

this

slider.

Move

the

slider

to

the

de-

sired

line

width

be-

fore

de-

fin-

ing

the

hol-lowar-rowheador

dashsym-



bols .

This

slider

does

not

af-

fect

the

circle ,

sol-idar-rowhead ,

and

star .

Orientation These

check

boxes

de-

term-

ine

the

way

an-

nota-

tion

lines

and

ar-

rows

are

gen-

er-

ated.

De-

pend-

ing

on

the

an-

chor

se-

lec-

tion,

you

can

gen-

er-

ate

an-




nota-

tion

from

the

an-

chor

to

the

view,

from

the

view

to

the

an-

chor,

or

between

two

of

the

an-

chor

items

chosen.

The

term

“view”

is

used

to

de-

scribe

a

point

in

3-

D

space

from

which,

or

to

which

you

draw

the

line

or

ar-

row.



Bitmaps Bitmaps are applied to the item,

point, or entity's centroid, as defined

by your anchor. Bitmaps are automat-

ically applied when you pick on the

graphics window.

Bitmap Name You

can

choose

from

the

sev-

en

sup-

plied

bit-

map

en-

tit-

ies

(Two

AN-

SYS

lo-

gos,

a

clamp

and

four

3-

D-

dir-

ec-

tion-

al

ar-

rows),

or

sup-

ply

your

own

bit-

maps.

You

must

des-

ig-

nate

your

bit-

map

be-




fore-

hand

(Util-

ity

Menu

>PlotCtrls>

An-

not-

ate>

Load

Bit-

map)

in

either

JPEG,

PNG

or

Win-

dows

BMP

format.

The

bit-

map

file

will

then

ap-

pear

in

this

pull-

down

se-

lec-

tion

box.

Note

Your

im-

por-

ted

bit-

maps

oc-

cupy

the

num-

ber

of



pixels

they

were

gen-

er-

ated

at,

and

can-

not

be

res-

ized

once

they

are

placed

in

the

graph-

ics

win-

dow

(even

if

you

res-

ize

your

mod-

el).

Dimensions Horizontal

Vertical

Slanting

Angular

Radial

6

2

7

10 fee

Dimension Settings




Color Choose

a

col-

or

from

the

pull-

down

menu.

The

sub-

sequently

defined

di-

men-

sion

lines

and

text

will

be

of

the

col-

or

chosen.

Inline / Parallel Text Choose

wheth-

er

your

text

will

fol-

low

the

same

slope

as

the

di-

men-

sion

lines

(per-

pen-

dic-

u-

lar

to

the

ex-

ten-



sion

lines

for

all

but

An-

gu-

lar

and

Ra-

di-

al

types),

or

be

par-

al-

lel

to

the

ex-

ten-

sion

lines.

Lines or Arcs You pick the starting point of your

line in the Graphics window, or define

it via coordinates in the input area.

You can draw lines between two

picked anchor entities, between two

points, or from a picked point in

space to any anchor entity or defined

point. Each subsequent right mouse

click allows you to create vertices and

angles, and a right mouse click ends

the line.

Color Choose

a

line

col-

or

from

the

pull-

down

menu.

Solid / Dashed Choose

either

sol-

id

(de-




fault)

or

dashed

lines.

Width You

can

vary

the

thick-

ness

of

your

line

by

a

factor

of

10.

Orientation These

check

boxes

de-

term-

ine

the

way

an-

nota-

tion

lines

and

ar-

rows

are

gen-

er-

ated.

Op-

tions

are

avail-

able,

de-

pend-

ing

on

the

an-

chor

se-

lec-



tion,

to

gen-

er-

ate

the

an-

nota-

tion

from

the

an-

chor

to

the

view,

from

the

view

to

the

an-

chor,

or

between

two

of

the

item

types

chosen

for

the

an-

chor.

The

term

view

is

used

to

de-

scribe

a

point

in

3-

D

space

from

which,

or




to

which

you

draw

the

line

or

ar-

row.

Options You can modify your annotation

items individually or all at once. The

ANNOTATION ANCHOR pull down box

is grayed out when Options is selec-

ted from the ANNOTATON ENTITY list.

Modify Buttons Copy:

You

•

must

first

"box

se-

lect"

the

item(s)

you

want

to

copy.

The

prompt

in

the

in-

put

win-

dow

tells

you

to

pick

the

first

and

second

corners.

You

then

click

to

place

the

copied



an-

nota-

tion

item

any-

where

in

the

graph-

ics

screen

(there

is

no

defined

an-

chor

loc-

a-

tion).

Mul-

tiple

clicks

will

place

mul-

tiple

cop-

ies.

• Move:

After

se-

lect-

ing

the

item,

you

use

the

mouse

to

move

it

any-

where

in

the

graph-

ics

win-

dow.

Sub-




sequent

ro-

ta-

tions,

res-

iz-

ings

or

tran-

la-

tions

will

an-

chor

the

item(s)

to

the

xyz

co-

ordin-

ates.

• Res-

ize:

After

se-

lect-

ing

the

item,

you

move

the

mouse

to

change

its

size.

Al-

though

they

can

be

copied

and

moved,

Bit-

map

File

An-

nota-

tions



can-

not

be

res-

ized.

• De-

lete:

Un-

like

all

of

the

pre-

vi-

ous

"Op-

tion

Modi-

fy

But-

tons",

does

not

re-

quire

that

you

se-

lect

the

item.

The

de-

lete

func-

tion

auto-

mat-

ic-

ally

de-

letes

the

ap-

pro-

pri-

ate

an-

nota-

tion

when

you




pick

it.

• Box

De-

lete:

Auto-

mat-

ic-

ally

de-

letes

all

of

the

en-

closed

items

when

you

com-

plete

the

se-

lec-

tion

box.

Al-

though

some

items

dis-

ap-

pear,

oth-

ers

(bit-

maps)

re-

quire

that

you

replot

in

or-

der

to

see

the

item

ac-

tu-

ally



re-

moved.

Draw / Erase Grid En-

able

grid

vis-

ib-

il-

ity

to

aid

in

pla-

cing

your

an-

nota-

tion.

2-

D

An-

nota-

tion

en-

tit-

ies

can

be

placed

more

pre-

cisely

us-

ing

the

grid.

(See

Snap,

be-

low.)

The

grid

does

not

need

to

be

vis-

ible

for

snap-




ping

to

be

en-

abled.

Enable Snap Lets

you

pick

loc-

a-

tions

at

the

in-

ter-

sec-

tion

of

the

grid

lines.

This

is

sim-

il-

ar

to

pick-

ing

points

on

a

work-

ing

plane.

Picked

loc-

a-

tions

that

fall

between

grid

lines

will

be

re-

dir-

ec-

ted

to

the



nearest

grid

in-

ter-

sec-

tion.

Snap Increment Con-

trols

the

size

of

the

grid

squares,

and

the

"dens-

ity"

of

the

snap

point

loc-

a-

tions.

Snap

point

loc-

a-

tions

are

the

in-

ter-

sec-

tion

of

grid

lines.

Save / Restore You

can

use

these

but-

tons

to

save

and

re-

store

an-




nota-

tion

from

a

sep-

ar-

ate

an-

nota-

tion

file.

Be-

cause

an-

nota-

tion

is

not

saved

with

the

data-

base,

you

will

need

to

save

an-

nota-

tion

en-

tit-

ies

to

a

file

if

you

plan

on

us-

ing

the

cur-

rent

an-

nota-

tion

in

an-

oth-



er

ses-

sion.

The

en-

tit-

ies

are

saved

in

glossterms

of

AN-

SYS

com-

mands,

and

can

be

re-

stored

at

any

time.

The

an-

nota-

tion

file

name

is

dis-

played

be-

low

these

but-

tons.

Delete All Auto-

mat-

ic-

ally

de-

letes

all

an-

nota-

tion

items

(both

2-

D




and

3-

D)

from

your

graph-

ics

win-

dow.

YOU

CAN-

NOT

RE-

COV-

ER

THIS

OP-

ER-

A-

TION

VIA

THE

UNDO

BUT-

TON

Text Choose the entity to use for annotat-

ing. Bitmap text is the default, but

you can also use graphics entities

such as lines, polygons, arrows etc. If

bitmap fonts are not enabled, this

dialog box will provide additional

controls for creating “stroke text”

fonts. You can use the provided con-

trols to create stroke text and modify

it as desired.

Setting Bitmap Text Option

To create bitmap text, you must

first enable bitmap fonts (Utility

Menu> PlotCtrls> Annotation>

Enable Bitmap Font). This loads

the fonts that are available on

your system. You then select the

desired font (Utility Menu>

PlotCtrls> Annotation> Select

Anno/Graph Font). The font you

select will also be used for your

charting and legend annotations.

Setting Stroke Text Option

Unlike Bitmap Text, which ac-

cesses your system fonts, Stroke-



Text characters are drawn by AN-

SYS. Although you are limited in

the construction and make up of

the type face, the vector nature

of the characters allows them to

be modified and customized

more easily. Stroke text annota-

tions do not size proportionately.

That is you can make the text il-

legible by independently modify-

ing one size parameter, or by us-

ing the ANNOTATION OPTIONS

sizing capability.

Color You

choose

from

the

col-

or

pal-

let

to

de-

glosster-

mine

the

col-

or

of

your

text.

Size Move

the

slider

to

the

de-

sired

text

size.

A

text

size

value

of

1

cor-

res-

ponds

to

ap-




prox-

im-

ately

5%

of

your

Graph-

ics

Win-

dow

height,

while

a

value

of

10

cor-

res-

ponds

to

ap-

prox-

im-

ately

20%.

NOTE

:

Al-

though

3-

D

text

an-

nota-

tion

re-

mains

anchored

when

you

trans-

late,

ro-

tate

or

res-

ize

your

mod-

el,

the

text



size

does

not

change

auto-

mat-

ic-

ally.

Use

the

“Op-

tions”

set-

ting

to

res-

ize

your

text

if

you

modi-

fy

your

mod-

el.

Thickness You

can

vary

the

thick-

ness

of

the

text

lines

by

a

factor

of

10.

This

op-

tion

is

only

avail-

able

when

en-

abled

bit-




map

fonts

is

dis-

abled.

Slant You

can

make

your

text

look

as

though

it

is

it-

alicized

by

chan-

ging

the

slant.

The

num-

bers

dis-

played

(0

-

45)

cor-

res-

pond

to

de-

grees.

This

op-

tion

is

only

avail-

able

when

en-

abled

bit-

map

fonts

is

dis-

abled.



Justification Buttons Con-

trols

how

the

text

is

jus-

ti-

fied

with-

in

the

picked

start-

ing

and

end-

ing

loc-

a-

tions

for

2-

D

only.

• Left

Jus-

ti-

fied:

The

text

will

start

at

the

first

picked

loc-

a-

tion

and

ex-

tend

as

far

as

ne-

ces-

sary

to

the

right.




• Centered:

The

cen-

ter

of

the

text

will

be

halfway

between

the

first

and

second

picked

loc-

a-

tion.

The

text

will

be

dis-

played

as

you

type

it,

and

will

al-

tern-

ately

move

to

the

left

and

right

as

you

build

the

text

string.

• Right

Jus-

ti-

fied:

The

text



will

end

at

the

second

picked

loc-

a-

tion.

Text Path Buttons • Ex-

act

Path:

The

text

you

define

will

fol-

low

the

path

from

the

first

point

that

you

pick

to

the

second

point

(de-

fault).

• Ap-

prox-

im-

ate

Path:

Al-

lows

some

tol-

er-

ance

when

you

are

try-

ing




to

define

text

that

is

ex-

actly

ho-

ri-

zont-

al

or

ver-

tic-

al.

Picked

path

lines

with-

in

5

de-

grees

of

be-

ing

ver-

tic-

al

or

ho-

ri-

zont-

al

will

be

made

in-

to

purely

ho-

ri-

zont-

al

or

ver-

tic-

al

text

paths.



Select Entities: Lines - By Length or by Radius

Selection Criteria By Length/Rad: Select line by length or by radius.

Selection Type By Length or By Radius: Indicate whether lines are selected by length

or by radius.

Range Criteria Min, Max, Inc: The minimum value and maximum value of the length

or radius of the line(s) to be selected and Inc indicates the value increment

within the range.

Selection Function Setting From Full: Select a new set of entities from the entire model.•

• Reselect: Replace the current set of entities with a subset of those

entities.

• Also Select: Select additional entities to add to the currently selected

set of entities.

• Unselect: Unselect entities from the currently selected set of entities.

Selection Function Action Selection function actions execute immediately.

• Sele All: Select all entities.

• Invert: Unselect the currently selected set of entities, and select

the currently unselected set of entities.

• Sele None: Unselect all entities.

• Sele Belo: Selects all items directly associated with and below the

selected items of the specified entity type.



Select Entities: Lines - By Length or by Radius

Action Buttons Options within your current window that are not selected will not be

plotted. You can act upon the unselected options using Selection Function

Settings: From Full or Also Select.

• Plot: If you press the Plot button, an entity plot occurs for the entity

that is featured on the drop down. For instance, if the drop down dis-

plays "Nodes", an NPLOT occurs.

• Replot: If you press the Replot button, ANSYS issues a “/REPLOT”

command. If your most recent plot was an “EPLOT”, then pressing

Replot reissues the EPLOT command.

Select Entities: Elements

Selection Criteria By Elem Name: Select elements that have a previously defined [ET]

name or number.

•

• Adjacent to: Select elements that are adjacent to the specified element.

Only elements of the same dimensionality adjacent to lateral faces are

considered. Progression continues until edge of model or until more

than two elements are adjacent at a face.

Element Name Element number to which the selected elements are to be adjacent (for

example, SOLID185 or 185).



entities.


set of entities.






















Select Entities: Elements

Select Entities: By Attributes

Entity Type Nodes [NSEL]•

• Elements [ESEL]

• Volumes [VSEL]

• Areas [ASEL]

• Lines [LSEL]

• Keypoints [KSEL]

Selection Criteria Select entities by attributes.

Attachment Criteria Master node num: Select nodes with a master DOF.•

• Coupled set num: Select nodes with a coupled DOF.

• Constraint eq num: Select nodes that are subject to constraint equa-

tions.

• THXY rot angle: Select nodes whose nodal coordinate systems have

been rotated by the given THXY angle.

• THYZ rot angle: Select nodes whose nodal coordinate systems have

been rotated by the given THYZ angle.



• THZX rot angle: Select nodes whose nodal coordinate systems have

been rotated by the given THZX angle.

• Min,Max,Inc: Minimum and maximum values of the specified attributes

and increment to advance from the minimum to the maximum value.

Inc does not apply to the rotation angles.

• Material num: Material number associated with an entity.

• Elem type num: Element type number associated with an entity.

• Real set num: Real constant set number associated with an entity.

• Elem CS num: Element coordinate system number associated with an

entity.

• No. of divisions: Number of divisions within the line.

• Spacing ratio: Spacing ratio of line divisions.

• Section ID num: Associated with an entity.

• Layer num: Only for composite elements.

• LS-DYNA Part ID: Only for ANSYS LS-DYNA.



entities.


set of entities.




• Invert: Unselect the currently selected set of entities, and select the

currently unselected set of entities.


• Sele Belo: Selects all items directly associated with and below the se-

lected items of the specified entity type.






Select Entities: By Attributes







Select Entities: Attached to Other Entities


• Elements [ESEL]

• Volumes [VSEL]

• Areas [ASEL]

• Lines [LSEL]


Selection Criteria Select entities that are attached to

other entities. You must select entit-

Attached to

ies to be used in defining attachment

criteria before entering this dialog

box.



Attachment Criteria Nodes: Select entities [ESLN, KSLN] based on their connectivity to the

currently selected set of nodes.

•

• Nodes, all: Select entities [ESLN] that are fully defined by nodes in

the currently selected set of nodes.

• Elements: Select all entities [NSLE] contained in the currently selected

set of elements.

• Keypoints: Select all entities [NSLK, LSLK] contained in the currently

selected set of keypoints.

• Keypoints, all: Select entities [LSLK] only if all of each lines keypoints

are in the currently selected set of keypoints.

• Lines: Select entities [ESLL, ASLL, KSLL] contained in the currently

selected set of lines.

• Lines, all: Select all entities [NSLL, ASLL] contained in the currently

selected set of lines.

• Lines, interior: Select all entities [NSLL] contained in the currently

selected set of lines, except those at the endpoints of the lines.

• Areas: Select entities [ESLA, LSLA, VSLA] contained in the currently

selected set of areas.

• Areas, all: Select all entities [NSLA, VSLA] contained within the cur-

rently selected set of areas.

• Areas, interior: Select all entities [NSLA] contained within the currently

selected set of areas, except those on the edges of the areas.

• Volumes: Select entities [ESLV, ASLV] based on those currently meshed

in the currently selected set of volumes.

• Volumes, all: Select all entities [NSLV] contained within the currently

selected set of volumes.

• Volumes, interior: Select all entities [NSLV] contained within the

currently selected set of volumes, except those on the exterior surfaces

of the volumes.



entities.


set of entities.





Select Entities: Attached to Other Entities

Sele All: Select all entities.•















Select Entities: By Location


• Volumes [VSEL]

• Areas [ASEL]



• Lines [LSEL]


Selection Criteria Select entity by location.

Location Settings X,Y,Z Coordinates: Selects the Cartesian coordinate to use to specify

location for area selection. Interpreted as R, Θ, Z for cylindrical coordin-

•

ate system or R, Θ, Φ for spherical coordinate system. One coordinate

at a time is specified. You must specify the coordinate system before

entering this dialog box.

• Min,Max: The minimum value and maximum value of the specified

coordinate. Areas with "hot spot" within the specified range will be

selected.



entities.


set of entities.




















Select Entities: By Location

Select Entities


• Elements [ESEL]

• Volumes [VSEL]

• Areas [ASEL]

• Lines [LSEL]


Selection Criteria By Num/Pick : Select an entity by keyboard entry or by graphical

picking.

•

• Exterior : Select entity type on exterior of currently selected item.

You must select entities to be used before entering this dialog box.

• By Results : Select entities having solution results within a chosen

range. You must save solution results in an element table [ETABLE]

before you can choose these elements.

• Live Elem's : Select elements that have not been previously "killed"

[EKILL], or that have been previously "born" [EALIVE] after being

"killed." See the discussion on element birth and death in the Advanced

Analysis Guide.

• By Hard Points : Select those entities which are hard points.

• Concatenated : Select concatenated entity.





entities.


set of entities.


















CrankSlot_Rigid.inp

/batch/prep7! Turn off shape checking because checks already performed inside WB mesher.! See help system for more information.SHPP,OFF,,NOWARN/nolistetcon,set ! allow ANSYS to choose best KEYOP's for 180x elements/com,*********** Nodes for the whole assembly ***********nblock,3(1i8,3e20.9e3) 1 0.000000000E+000 3.529175918E+001 -5.000000000E+000 2 2.378511247E+001 1.380297652E+001 5.000000000E+000 3 2.380153982E+001 6.877452408E+001 1.500000000E+001 4 -4.717895070E-016 1.100000000E+002 5.000000000E+000 5 1.525181166E-017 1.189641309E-016 9.761159461E-017 6 4.760307959E+001 2.754904870E+001 1.000000000E+001-1/com,*********** Elements for Part 1 ***********/com,*********** Send Body as a Rigid Body ***********et,1,MASS21keyo,1,3,0 ! 3D Mass With Rotary Intertiakeyo,1,2,1 ! Moments of inertia in nodal coordinatesr,1,5.62959624417329e-004,5.62959624417329e-004,5.62959624417329e-004,4.27915117762894,5.64969611751201e-002,4.32626430862063local,11,0,0.,35.2917591780688,-4.99999999999951,0.,0.,0.nrot,1



CrankSlot_Rigid.inp

csys,0mat,1real,1type,1en,1,1/com,*********** Elements for Part 2 ***********/com,*********** Send Body as a Rigid Body ***********et,2,MASS21keyo,2,3,0 ! 3D Mass With Rotary Intertiakeyo,2,2,1 ! Moments of inertia in nodal coordinatesr,2,7.59817488346602e-005,7.59817488346602e-005,7.59817488346602e-005,2.21486141701566e-003,3.27365368251796e-002,3.36826963131752e-002local,11,0,23.7851124732216,13.8029765212764,4.99999999999951,29.9821797972594,-1.63487457250109e-008,4.06547904138105e-009nrot,2csys,0mat,2real,2type,2en,2,2/com,*********** Elements for Part 3 ***********/com,*********** Send Body as a Rigid Body ***********et,3,MASS21keyo,3,3,0 ! 3D Mass With Rotary Intertiakeyo,3,2,1 ! Moments of inertia in nodal coordinatesr,3,1.23324499502402e-004,1.23324499502402e-004,1.23324499502402e-004,0.123369407044669,3.4970850903802e-003,0.124808744493488local,11,0,23.8015398171524,68.7745240829644,14.9999999999985,29.9999986025964,3.45291420136837e-009,-1.90838113503191e-007nrot,3csys,0mat,3real,3type,3en,3,3/com,*********** Elements for Part 4 ***********/com,*********** Send Body as a Rigid Body ***********et,4,MASS21keyo,4,3,0 ! 3D Mass With Rotary Intertiakeyo,4,2,1 ! Moments of inertia in nodal coordinatesr,4,1.84961267480099e-005,1.84961267480099e-005,1.84961267480099e-005,1.48440380137047e-003,1.48440385658378e-003,2.259733717427e-004local,11,0,-4.71789506988333e-016,110.000000028382,4.99999999999951,0.,0.,0.nrot,4csys,0mat,4real,4type,4en,4,4/com,*********** Elements for Part 5 ***********/com,*********** Send Body as a Rigid Body ***********et,5,MASS21keyo,5,3,0 ! 3D Mass With Rotary Intertiakeyo,5,2,1 ! Moments of inertia in nodal coordinatesr,5,1.23307511653399e-005,1.23307511653399e-005,1.23307511653399e-005,4.816704325156e-004,4.8167043256163e-004,1.50648999123811e-004local,11,0,1.52518116573376e-017,1.18964130927233e-016,9.76115946069606e-017,0.,0.,0.nrot,5csys,0mat,5real,5type,5en,5,5/com,*********** Elements for Part 6 ***********/com,*********** Send Body as a Rigid Body ***********et,6,MASS21keyo,6,3,0 ! 3D Mass With Rotary Intertiakeyo,6,2,1 ! Moments of inertia in nodal coordinatesr,6,1.23307511653399e-005,1.23307511653399e-005,1.23307511653399e-005,4.81670360832402e-004,4.81670377213366e-004,1.5064896426044e-004local,11,0,47.6030795911263,27.5490486999112,9.99999999999894,0.,0.,0.nrot,6csys,0mat,6real,6type,6en,6,6/com,*********** Send Materials ***********MP,DENS,1,7.85e-009, ! ton/mm³



MP,NUXY,1,0.3,MP,EX,1,200000., ! ton/s²·mmMP,ALPX,1,1.2e-005, ! 1/°CMP,C,1,434000000., ! mm²/s²·°CMP,KXX,1,60.5, ! ton·mm/s³·°CMP,MURX,1,10000.,MP,RSVX,1,1.7e-004, ! Ohm·mm

MP,DENS,2,7.85e-009, ! ton/mm³MP,NUXY,2,0.3,MP,EX,2,200000., ! ton/s²·mmMP,ALPX,2,1.2e-005, ! 1/°CMP,C,2,434000000., ! mm²/s²·°CMP,KXX,2,60.5, ! ton·mm/s³·°CMP,MURX,2,10000.,MP,RSVX,2,1.7e-004, ! Ohm·mm





! get the diagonal of the bounding box. Needed later for other things*get,_xmin,node,,mnloc,x*get,_ymin,node,,mnloc,y*get,_zmin,node,,mnloc,z*get,_xmax,node,,mxloc,x*get,_ymax,node,,mxloc,y*get,_zmax,node,,mxloc,z_ASMDIAG=(_xmax-_xmin)*(_xmax-_xmin)+(_ymax-_ymin)*(_ymax-_ymin)+(_zmax-_zmin)*(_zmax-_zmin)_ASMDIAG=SQRT(_ASMDIAG)/golistnsel,all/com,*********** Create Joint "Revolute - Base To Bolt1" ***********local,12,0,0.,3.06151588455594e-016,-5.00000000000001,0.,0.,180.csys,0 ! reset coordinate system back to global! Setup Joint Connection For Reference Set! ********* Create Target to Connect To Rigid Body Mass Node *********** *set,tid,8*set,cid,7et,tid,170



CrankSlot_Rigid.inp

keyo,tid,2,1 ! Don't fix the pilot nodekeyo,tid,4,0 ! Create CE's for all DOFstype,tidmat ,cidreal,cidtshape,piloen,14,1tshape! ********* End of Create Target to Connect To Rigid Body Mass Node *********** n,7,0.,3.06151588455594e-016,-5.00000000000001*set,_npilot,7_npilot38a=_npilotmat,7real,7type,8en,15,1,7csys,12nrot,_npilot ! rotate joint node into joint coordinate systemcsys,0 ! reset coordinate system back to global! Setup Joint Connection For Mobile Set! ********* Create Target to Connect To Rigid Body Mass Node *********** *set,tid,10*set,cid,9et,tid,170keyo,tid,2,1 ! Don't fix the pilot nodekeyo,tid,4,0 ! Create CE's for all DOFstype,tidmat ,cidreal,cidtshape,piloen,16,5tshape! ********* End of Create Target to Connect To Rigid Body Mass Node *********** n,8,0.,3.06151588455594e-016,-5.00000000000001*set,_npilot,8_npilot38b=_npilotmat,9real,9type,10en,17,5,8csys,12nrot,_npilot ! rotate joint node into joint coordinate systemcsys,0 ! reset coordinate system back to global/com, Real Contact Set For Above Joint Is 11! Joint Element Type Declaration and Definition using MPC184*set,_jid,11et,_jid,184keyo,_jid,1,6 ! Revolute Jointkeyo,_jid,4,1 ! Z Axis is revolute axissectype,_jid, joint, revo, _wbjointsecjoint,,12,12mat,_jidreal,_jidtype,_jidsecnum,_jiden,7,_npilot38a,_npilot38b ! body to body joint/com,*********** Create Joint "Fixed - Rod1 To Bolt1" ***********local,13,0,0.,3.06151588455594e-016,5.00000000000001,0.,0.,0.csys,0 ! reset coordinate system back to global! Setup Joint Connection For Reference Set! ********* Create Target to Connect To Rigid Body Mass Node *********** *set,tid,13*set,cid,12et,tid,170keyo,tid,2,1 ! Don't fix the pilot nodekeyo,tid,4,0 ! Create CE's for all DOFstype,tidmat ,cidreal,cidtshape,piloen,18,2tshape



! ********* End of Create Target to Connect To Rigid Body Mass Node *********** n,9,0.,3.06151588455594e-016,5.00000000000001*set,_npilot,9_npilot40a=_npilotmat,12real,12type,13en,19,2,9csys,13nrot,_npilot ! rotate joint node into joint coordinate systemcsys,0 ! reset coordinate system back to global! Setup Joint Connection For Mobile Setn,10,0.,3.06151588455594e-016,5.00000000000001*set,_npilot,10_npilot40b=_npilotmat,9real,9type,10en,20,5,10csys,13nrot,_npilot ! rotate joint node into joint coordinate systemcsys,0 ! reset coordinate system back to global! Joint Element Type Declaration and Definition using TARGE170*set,tid,15*set,cid,14et,tid,170keyo,tid,2,1 ! Don't fix the pilot nodekeyo,tid,4,0 ! Create CE's for all DOFsmat,cidreal,cidtype,tidtshape,piloen,8,_npilot40a ! create pilot node for rigid linktshapetype,tiden,21,_npilot40a,_npilot40bcsys,0/com,*********** Create Joint "Fixed - Rod1 To Bolt2" ***********local,14,0,47.6030788398054,27.5490488527501,5.,0.,0.,0.csys,0 ! reset coordinate system back to global! Setup Joint Connection For Reference Setn,11,47.6030788398054,27.5490488527501,5.*set,_npilot,11_npilot42a=_npilotmat,12real,12type,13en,22,2,11csys,14nrot,_npilot ! rotate joint node into joint coordinate systemcsys,0 ! reset coordinate system back to global! Setup Joint Connection For Mobile Set! ********* Create Target to Connect To Rigid Body Mass Node *********** *set,tid,17*set,cid,16et,tid,170keyo,tid,2,1 ! Don't fix the pilot nodekeyo,tid,4,0 ! Create CE's for all DOFstype,tidmat ,cidreal,cidtshape,piloen,23,6tshape! ********* End of Create Target to Connect To Rigid Body Mass Node *********** n,12,47.6030788398054,27.5490488527501,5.*set,_npilot,12_npilot42b=_npilotmat,16real,16type,17en,24,6,12



CrankSlot_Rigid.inp

csys,14nrot,_npilot ! rotate joint node into joint coordinate systemcsys,0 ! reset coordinate system back to global! Joint Element Type Declaration and Definition using TARGE170*set,tid,19*set,cid,18et,tid,170keyo,tid,2,1 ! Don't fix the pilot nodekeyo,tid,4,0 ! Create CE's for all DOFsmat,cidreal,cidtype,tidtshape,piloen,9,_npilot42a ! create pilot node for rigid linktshapetype,tiden,25,_npilot42a,_npilot42bcsys,0/com,*********** Create Joint "Fixed - Rod2 To Bolt3" ***********local,15,0,1.45519152283668e-014,110.,15.,0.,0.,0.csys,0 ! reset coordinate system back to global! Setup Joint Connection For Reference Set! ********* Create Target to Connect To Rigid Body Mass Node *********** *set,tid,21*set,cid,20et,tid,170keyo,tid,2,1 ! Don't fix the pilot nodekeyo,tid,4,0 ! Create CE's for all DOFstype,tidmat ,cidreal,cidtshape,piloen,26,3tshape! ********* End of Create Target to Connect To Rigid Body Mass Node *********** n,13,1.45519152283668e-014,110.,15.*set,_npilot,13_npilot44a=_npilotmat,20real,20type,21en,27,3,13csys,15nrot,_npilot ! rotate joint node into joint coordinate systemcsys,0 ! reset coordinate system back to global! Setup Joint Connection For Mobile Set! ********* Create Target to Connect To Rigid Body Mass Node *********** *set,tid,23*set,cid,22et,tid,170keyo,tid,2,1 ! Don't fix the pilot nodekeyo,tid,4,0 ! Create CE's for all DOFstype,tidmat ,cidreal,cidtshape,piloen,28,4tshape! ********* End of Create Target to Connect To Rigid Body Mass Node *********** n,14,1.45519152283668e-014,110.,15.*set,_npilot,14_npilot44b=_npilotmat,22real,22type,23en,29,4,14csys,15nrot,_npilot ! rotate joint node into joint coordinate systemcsys,0 ! reset coordinate system back to global! Joint Element Type Declaration and Definition using TARGE170*set,tid,25*set,cid,24



et,tid,170keyo,tid,2,1 ! Don't fix the pilot nodekeyo,tid,4,0 ! Create CE's for all DOFsmat,cidreal,cidtype,tidtshape,piloen,10,_npilot44a ! create pilot node for rigid linktshapetype,tiden,30,_npilot44a,_npilot44bcsys,0/com,*********** Create Joint "Cylindrical - Rod2 To Bolt2" ***********local,16,0,47.6030788398054,27.5490488527501,15.,0.,0.,0.csys,0 ! reset coordinate system back to global! Setup Joint Connection For Reference Setn,15,47.6030788398054,27.5490488527501,15.*set,_npilot,15_npilot46a=_npilotmat,20real,20type,21en,31,3,15csys,16nrot,_npilot ! rotate joint node into joint coordinate systemcsys,0 ! reset coordinate system back to global! Setup Joint Connection For Mobile Setn,16,47.6030788398054,27.5490488527501,15.*set,_npilot,16_npilot46b=_npilotmat,16real,16type,17en,32,6,16csys,16nrot,_npilot ! rotate joint node into joint coordinate systemcsys,0 ! reset coordinate system back to global/com, Real Contact Set For Above Joint Is 26! Joint Element Type Declaration and Definition using MPC184*set,_jid,26et,_jid,184keyo,_jid,1,11 ! Cylindrical Jointkeyo,_jid,4,1 ! Z Axis is revolute axissectype,_jid, joint, cyli, _wbjointsecjoint,,16,16mat,_jidreal,_jidtype,_jidsecnum,_jiden,11,_npilot46a,_npilot46b ! body to body joint/com,*********** Create Joint "Slot - Base To Bolt3" ***********local,17,0,4.57554378011943e-017,110.000000097686,-10.,-90.,0.,180.csys,0 ! reset coordinate system back to global! Setup Joint Connection For Reference Setn,17,4.57554378011943e-017,110.000000097686,-10.*set,_npilot,17_npilot53a=_npilotmat,7real,7type,8en,33,1,17csys,17nrot,_npilot ! rotate joint node into joint coordinate systemcsys,0 ! reset coordinate system back to global! Setup Joint Connection For Mobile Setn,18,4.57554378011943e-017,110.000000097686,-10.*set,_npilot,18_npilot53b=_npilotmat,22real,22type,23en,34,4,18



CrankSlot_Rigid.inp

csys,17nrot,_npilot ! rotate joint node into joint coordinate systemcsys,0 ! reset coordinate system back to global/com, Real Contact Set For Above Joint Is 27! Joint Element Type Declaration and Definition using MPC184*set,_jid,27et,_jid,184keyo,_jid,1,8 ! Slot Jointsectype,_jid, joint, slot, _wbjointsecjoint,,17,17mat,_jidreal,_jidtype,_jidsecnum,_jiden,12,_npilot53a,_npilot53b ! body to body joint/com,*********** Create Joint "Fixed - Ground To Base" ***********local,18,0,0.,-100.,-5.,0.,90.,0.csys,0 ! reset coordinate system back to global! Setup Joint Connection For Mobile Setn,19,0.,-100.,-5.*set,_npilot,19_npilot55b=_npilotmat,7real,7type,8en,35,1,19csys,18nrot,_npilot ! rotate joint node into joint coordinate systemcsys,0 ! reset coordinate system back to globald,19,all ! body to ground Direct D/com,*********** Set Reference Temperature ***********tref,22./com,*********** Create Joint Drivers **********

*DIM,_loadvari109,TABLE,1,1,1,TIME! Time values_loadvari109(1,0) = 1.! Load values_loadvari109(1,1) = 25./com,*********** Send User Defined Coordinate System(s) ***********local,12,0,0.,3.06151588455594e-016,-5.00000000000001,0.,0.,180.local,13,0,0.,3.06151588455594e-016,5.00000000000001,0.,0.,0.local,14,0,47.6030788398054,27.5490488527501,5.,0.,0.,0.local,15,0,1.45519152283668e-014,110.,15.,0.,0.,0.local,16,0,47.6030788398054,27.5490488527501,15.,0.,0.,0.local,17,0,4.57554378011943e-017,110.000000097686,-10.,-90.,0.,180.local,18,0,0.,-100.,-5.,0.,90.,0.csys,0/gst,on,onfini*get,_numnode,node,0,count*get,_numelem,elem,0,count/go/com,--- Number of total nodes = %_numnode%/com,--- Number of total elements = %_numelem%/com,****************************************************************************/com,************************* SOLUTION ********************************/com,****************************************************************************/soluantype,4 ! transient analysisnlgeom,on ! Turn on Large Deformation Effectssolc,on,on ! Turn on solution control with ability to use contact time predictionkbc,1 ! stepped BC's/com, Avg ratio= 1, totalParts=6, thickParts=0, thickPcent= 0eqsl,sparse,,,,,1resc,,none ! Do not keep any restart filescntr,print,1 ! print out contact info and also make no initial contact an errortrnopt,full,,,,,hht ! HHT time integration methodtintp,0.1 ! Numerical Dampingnldiag,cont,iter ! print out contact info each equilibrium iteration/com,****************************************************/com,******************* SOLVE FOR LS 1 ****************



/nopr/gopresel,s,type,,11dj,all,dmgz,%_loadvari109%esel,allautots,off ! User turned off automatic time steppingnsub,100,100,100time,1.timint,on ! Turn on time integration effectsoutres,eraseoutres,all,noneoutres,nsol,-100outres,rsol,-100outres,nload,-100outres,strs,-100outres,epel,-100outres,eppl,-100outres,v,-100outres,a,-100esel,s,mat,,11esel,a,mat,,26esel,a,mat,,27esel,a,mat,,1esel,a,mat,,2esel,a,mat,,3esel,a,mat,,4esel,a,mat,,5esel,a,mat,,6cm,_elmisc,elemesel,alloutres,misc,-100,_elmisclnsr,off ! Line search turned OFF by user! *********** WB SOLVE COMMAND ***********solvefini

/post26nsol,2,3,u,y,uynsol,3,3,u,x,uxnsol,4,3,u,z,uzprod,5,2,2,,squyprod,6,3,3,,squxprod,7,4,4,,squzadd,8,5,6,7,sqsumsqrt,9,8,,,utotprvar,9

/com/com Time history plot of total displacement of node 2 of Rigid Body 2 /com

/xrange,0,1/yrange,0,80.956/axlab,x,TIME/axlab,y,TOTAL DISPLACEMENT OF RIGID ROD2plvar,9

finish

CrankSlot_flexible.inp

/batch/prep7! Turn off shape checking because checks already performed inside WB mesher.! See help system for more information.SHPP,OFF,,NOWARN/nolistetcon,set ! allow ANSYS to choose best KEYOP's for 180x elements/com,*********** Nodes for the whole assembly ***********nblock,3(1i8,3e20.9e3)




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433 5.222247650E+001 2.563563169E+001 1.500000000E+001 434 5.113861275E+001 2.401351495E+001 1.250000000E+001 435 4.760307884E+001 2.254904885E+001 1.750000000E+001 436 4.951649600E+001 2.292965119E+001 1.500000000E+001 437 4.760307884E+001 2.254904885E+001 1.250000000E+001 438 4.406754493E+001 2.401351495E+001 1.750000000E+001 439 4.568966168E+001 2.292965119E+001 1.500000000E+001 440 4.406754493E+001 2.401351495E+001 1.250000000E+001 441 4.260307884E+001 2.754904885E+001 1.750000000E+001 442 4.298368118E+001 2.563563169E+001 1.500000000E+001 443 4.260307884E+001 2.754904885E+001 1.250000000E+001 444 4.406754493E+001 3.108458276E+001 1.750000000E+001 445 4.298368118E+001 2.946246601E+001 1.500000000E+001 446 4.406754493E+001 3.108458276E+001 1.250000000E+001 447 4.760307884E+001 3.254904885E+001 1.750000000E+001 448 4.568966168E+001 3.216844652E+001 1.500000000E+001 449 4.760307884E+001 3.254904885E+001 1.250000000E+001 450 5.113861275E+001 3.108458276E+001 1.750000000E+001 451 4.951649600E+001 3.216844652E+001 1.500000000E+001 452 5.113861275E+001 3.108458276E+001 1.250000000E+001 453 5.222247650E+001 2.946246601E+001 1.500000000E+001 454 4.955197804E+001 3.215358921E+001 1.000000000E+001 455 4.572525697E+001 3.218303040E+001 1.000000000E+001 456 4.299853848E+001 2.949794805E+001 1.000000000E+001 457 4.296909729E+001 2.567122698E+001 1.000000000E+001 458 4.565417964E+001 2.294450849E+001 1.000000000E+001 459 4.948090071E+001 2.291506730E+001 1.000000000E+001 460 5.220761920E+001 2.560014966E+001 1.000000000E+001 461 -5.000000000E+000 1.186602540E+002 1.750000000E+001 462 -1.752404736E+000 1.205352540E+002 1.500000000E+001 463 -5.000000000E+000 1.186602540E+002 1.250000000E+001 464 -8.247595264E+000 1.167852540E+002 1.500000000E+001 465 -8.247595264E+000 1.167852540E+002 1.000000000E+001 466 -1.752404736E+000 1.205352540E+002 1.000000000E+001 467 5.223706039E+001 2.942687073E+001 1.000000000E+001 468 4.633981550E+000 1.118778219E+002 1.000000000E+001 469 -4.717895070E-016 1.100000000E+002 5.000000000E+000 470 1.525181166E-017 1.189641309E-016 9.761159461E-017 471 4.760307959E+001 2.754904870E+001 1.000000000E+001-1/com,*********** Elements for Part 1 ***********/com,*********** Send Body as a Rigid Body ***********et,1,MASS21keyo,1,3,0 ! 3D Mass With Rotary Intertiakeyo,1,2,1 ! Moments of inertia in nodal coordinatesr,1,5.62959624417329e-004,5.62959624417329e-004,5.62959624417329e-004,4.27915117762894,5.64969611751201e-002,4.32626430862063local,11,0,0.,35.2917591780688,-4.99999999999951,0.,0.,0.nrot,1csys,0mat,1real,1type,1en,1,1/com,*********** Elements for Part 2 ***********/com,*********** Send Body as a Rigid Body ***********et,2,MASS21keyo,2,3,0 ! 3D Mass With Rotary Intertiakeyo,2,2,1 ! Moments of inertia in nodal coordinatesr,2,7.59817488346602e-005,7.59817488346602e-005,7.59817488346602e-005,2.21486141701566e-003,3.27365368251796e-002,3.36826963131752e-002local,11,0,23.7851124732216,13.8029765212764,4.99999999999951,29.9821797972594,-1.63487457250109e-008,4.06547904138105e-009nrot,2csys,0mat,2real,2type,2en,2,2/com,*********** Elements for Part 3 ***********et,3,186keyo,3,2,1eblock,10(15i8) 3 3 3 3 0 90 115 116 91 109 124 123 108 164 411



0 0 0 0 0 179 383 204 426 215 395 382 412 409 379 4 3 3 3 0 32 39 38 33 116 91 90 115 246 278 0 0 0 0 0 247 273 179 383 164 411 407 381 384 410 5 3 3 3 0 18 127 70 71 135 134 80 81 453 148 0 0 0 0 0 305 144 467 192 341 189 430 452 306 303 6 3 3 3 0 18 71 70 127 21 51 52 27 144 305 0 0 0 0 0 148 453 240 291 244 260 431 301 304 450 7 3 3 3 0 18 71 85 133 135 81 84 136 144 302 0 0 0 0 0 177 433 189 342 213 460 430 303 345 434 8 3 3 3 0 18 133 85 71 21 22 50 51 433 177 0 0 0 0 0 302 144 263 241 290 240 431 432 346 301 9 3 3 3 0 98 130 131 99 101 139 138 100 145 442 0 0 0 0 0 174 359 190 457 211 387 358 443 440 355 10 3 3 3 0 24 47 46 25 131 99 98 130 242 286 0 0 0 0 0 243 266 174 359 145 442 438 357 360 441 11 3 3 3 0 97 129 130 98 102 140 139 101 146 445 0 0 0 0 0 145 362 191 456 190 388 361 446 443 358 12 3 3 3 0 25 46 45 26 130 98 97 129 243 285 0 0 0 0 0 239 267 145 362 146 445 441 360 363 444 13 3 3 3 0 5 128 129 97 10 141 140 102 147 448 0 0 0 0 0 146 151 193 455 191 196 152 449 446 361 14 3 3 3 0 5 97 129 128 15 45 26 28 151 146 0 0 0 0 0 448 147 230 239 268 232 153 363 444 447 15 3 3 3 0 5 70 127 128 10 80 134 141 154 148 0 0 0 0 0 451 147 198 192 454 193 152 306 452 449 16 3 3 3 0 5 128 127 70 15 28 27 52 147 451 0 0 0 0 0 148 154 232 269 244 231 153 447 450 304 17 3 3 3 0 19 112 62 63 120 119 72 73 422 149 0 0 0 0 0 329 181 468 195 333 219 399 421 330 327 18 3 3 3 0 19 63 62 112 29 59 60 35 181 329 0 0 0 0 0 149 422 245 299 248 259 400 325 328 419 19 3 3 3 0 6 142 83 62 11 143 82 72 171 462 0 0 0 0 0 331 150 210 466 332 194 168 463 343 330 20 3 3 3 0 6 62 83 142 14 60 61 20 150 331 0 0 0 0 0 462 171 233 300 261 235 170 328 344 461 21 3 3 3 0 6 62 112 113 11 72 119 126 150 149 0 0 0 0 0 420 166 194 195 423 206 168 330 421 418 22 3 3 3 0 6 113 112 62 14 36 35 60 166 420 0 0 0 0 0 149 150 234 276 248 233 170 416 419 328 23 3 3 3 0 3 5 97 96 8 10 102 103 155 151 0 0 0 0 0 365 159 197 196 389 200 157 152 361 364 24 3 3 3 0 3 96 97 5 17 44 45 15 159 365 0 0 0 0 0 151 155 226 284 230 225 158 366 363 153 25 3 3 3 0 3 69 70 5 8 79 80 10 156 308 0 0 0 0 0 154 155 199 340 198 197 157 309 306 152 26 3 3 3 0 3 5 70 69 17 15 52 53 155 154 0 0 0 0 0 308 156 225 231 292 227 158 153 304 307 27 3 3 3 0 3 95 68 69 8 104 78 79 160 161 0 0 0 0 0 311 156 201 202 339 199 157 367 312 309 28 3 3 3 0 3 69 68 95 17 53 54 43 156 311 0 0 0 0 0 161 160 227 293 236 224 158 307 310 369 29 3 3 3 0 67 68 95 94 77 78 104 105 314 161 0 0 0 0 0 371 162 338 202 391 203 315 312 367 370 30 3 3 3 0 42 55 54 43 94 67 68 95 237 294 0 0 0 0 0 236 282 162 314 161 371 372 313 310 369 31 3 3 3 0 66 67 94 93 76 77 105 106 317 162 0 0 0 0 0 374 188 337 203 392 222 318 315 370 373 32 3 3 3 0 41 56 55 42 93 66 67 94 238 295 0 0 0 0 0 237 281 188 317 162 374 375 316 313 372 33 3 3 3 0 7 114 115 90 12 125 124 109 165 414 0 0 0 0 0 164 163 207 425 204 205 167 415 412 382 34 3 3 3 0 7 90 115 114 13 38 33 34 163 164 0 0 0 0 0 414 165 249 247 274 251 169 384 410 413 35 3 3 3 0 6 113 114 7 11 126 125 12 166 417 0 0 0 0 0 165 173 206 424 207 208 168 418 415 167 36 3 3 3 0 6 7 114 113 14 13 34 36 173 165 0 0 0 0 0 417 166 252 251 275 234 170 169 413 416 37 3 3 3 0 6 7 111 142 11 12 110 143 173 172 0 0 0 0 0 464 171 208 209 465 210 168 167 397 463 38 3 3 3 0 6 142 111 7 14 20 37 13 171 464 0 0 0 0 0 172 173 235 262 250 252 170 461 398 169 39 3 3 3 0 88 137 138 100 89 132 131 99 212 458




0 0 0 0 0 211 386 175 439 174 356 353 437 440 355 40 3 3 3 0 23 48 47 24 132 89 99 131 253 287 0 0 0 0 0 242 265 175 356 174 439 435 354 357 438 41 3 3 3 0 84 136 137 87 85 133 132 86 213 459 0 0 0 0 0 214 351 177 436 176 348 345 434 437 347 42 3 3 3 0 22 50 49 23 133 85 86 132 241 289 0 0 0 0 0 254 264 177 348 176 436 432 346 349 435 43 3 3 3 0 4 91 116 117 9 108 123 122 178 179 0 0 0 0 0 408 180 216 215 427 217 183 379 409 406 44 3 3 3 0 4 117 116 91 16 31 32 39 180 408 0 0 0 0 0 179 178 256 272 246 255 184 404 407 381 45 3 3 3 0 4 117 118 64 9 122 121 74 180 405 0 0 0 0 0 182 185 217 428 218 221 183 406 403 324 46 3 3 3 0 4 64 118 117 16 58 30 31 185 182 0 0 0 0 0 405 180 229 257 271 256 184 322 401 404 47 3 3 3 0 19 63 64 118 120 73 74 121 181 326 0 0 0 0 0 182 402 219 334 218 429 399 327 324 403 48 3 3 3 0 19 118 64 63 29 30 58 59 402 182 0 0 0 0 0 326 181 270 257 298 245 400 401 322 325 49 3 3 3 0 4 64 65 92 9 74 75 107 185 323 0 0 0 0 0 187 186 221 335 223 220 183 324 321 376 50 3 3 3 0 4 92 65 64 16 40 57 58 186 187 0 0 0 0 0 323 185 228 258 297 229 184 378 319 322 51 3 3 3 0 65 66 93 92 75 76 106 107 320 188 0 0 0 0 0 377 187 336 222 393 223 321 318 373 376 52 3 3 3 0 40 57 56 41 92 65 66 93 258 296 0 0 0 0 0 238 280 187 320 188 377 378 319 316 375 53 3 3 3 0 3 96 95 95 8 103 104 104 159 368 0 0 0 0 0 95 160 200 390 104 201 157 364 367 367 54 3 3 3 0 3 95 96 96 17 43 44 44 160 368 0 0 0 0 0 96 159 224 283 44 226 158 369 366 366 55 3 3 3 0 7 90 111 111 12 109 110 110 163 385 0 0 0 0 0 111 172 205 396 110 209 167 382 397 397 56 3 3 3 0 7 111 90 90 13 37 38 38 172 385 0 0 0 0 0 90 163 250 277 38 249 169 398 384 384 57 3 3 3 0 86 89 132 132 87 88 137 137 350 175 0 0 0 0 0 132 176 352 212 137 214 347 353 437 437 58 3 3 3 0 23 49 48 48 132 86 89 89 254 288 0 0 0 0 0 48 253 176 350 89 175 435 349 354 354 59 3 3 3 0 4 92 91 91 9 107 108 108 186 380 0 0 0 0 0 91 178 220 394 108 216 183 376 379 379 60 3 3 3 0 4 91 92 92 16 39 40 40 178 380 0 0 0 0 0 92 186 255 279 40 228 184 381 378 378-1/com,*********** Elements for Part 4 ***********/com,*********** Send Body as a Rigid Body ***********et,4,MASS21keyo,4,3,0 ! 3D Mass With Rotary Intertiakeyo,4,2,1 ! Moments of inertia in nodal coordinatesr,4,1.84961267480099e-005,1.84961267480099e-005,1.84961267480099e-005,1.48440380137047e-003,1.48440385658378e-003,2.259733717427e-004local,11,0,-4.71789506988333e-016,110.000000028382,4.99999999999951,0.,0.,0.nrot,469csys,0mat,4real,4type,4en,61,469/com,*********** Elements for Part 5 ***********/com,*********** Send Body as a Rigid Body ***********et,5,MASS21keyo,5,3,0 ! 3D Mass With Rotary Intertiakeyo,5,2,1 ! Moments of inertia in nodal coordinatesr,5,1.23307511653399e-005,1.23307511653399e-005,1.23307511653399e-005,4.816704325156e-004,4.8167043256163e-004,1.50648999123811e-004local,11,0,1.52518116573376e-017,1.18964130927233e-016,9.76115946069606e-017,0.,0.,0.nrot,470csys,0mat,5real,5type,5en,62,470/com,*********** Elements for Part 6 ***********/com,*********** Send Body as a Rigid Body ***********



et,6,MASS21keyo,6,3,0 ! 3D Mass With Rotary Intertiakeyo,6,2,1 ! Moments of inertia in nodal coordinatesr,6,1.23307511653399e-005,1.23307511653399e-005,1.23307511653399e-005,4.81670360832402e-004,4.81670377213366e-004,1.5064896426044e-004local,11,0,47.6030795911263,27.5490486999112,9.99999999999894,0.,0.,0.nrot,471csys,0mat,6real,6type,6en,63,471/com,*********** Send Materials ***********MP,DENS,1,7.85e-009, ! ton/mm³MP,NUXY,1,0.3,MP,EX,1,200000., ! ton/s²·mmMP,ALPX,1,1.2e-005, ! 1/°CMP,C,1,434000000., ! mm²/s²·°CMP,KXX,1,60.5, ! ton·mm/s³·°CMP,MURX,1,10000.,MP,RSVX,1,1.7e-004, ! Ohm·mm






! get the diagonal of the bounding box. Needed later for other things*get,_xmin,node,,mnloc,x*get,_ymin,node,,mnloc,y*get,_zmin,node,,mnloc,z*get,_xmax,node,,mxloc,x*get,_ymax,node,,mxloc,y




*get,_zmax,node,,mxloc,z_ASMDIAG=(_xmax-_xmin)*(_xmax-_xmin)+(_ymax-_ymin)*(_ymax-_ymin)+(_zmax-_zmin)*(_zmax-_zmin)_ASMDIAG=SQRT(_ASMDIAG)/golistnsel,all/com,*********** Create Joint "Revolute - Base To Bolt1" ***********local,12,0,0.,3.06151588455594e-016,-5.00000000000001,0.,0.,-180.csys,0 ! reset coordinate system back to global! Setup Joint Connection For Reference Set! ********* Create Target to Connect To Rigid Body Mass Node *********** *set,tid,8*set,cid,7et,tid,170keyo,tid,2,1 ! Don't fix the pilot nodekeyo,tid,4,0 ! Create CE's for all DOFstype,tidmat ,cidreal,cidtshape,piloen,71,1tshape! ********* End of Create Target to Connect To Rigid Body Mass Node *********** n,472,0.,3.06151588455594e-016,-5.00000000000001*set,_npilot,472_npilot471a=_npilotmat,7real,7type,8en,72,1,472csys,12nrot,_npilot ! rotate joint node into joint coordinate systemcsys,0 ! reset coordinate system back to global! Setup Joint Connection For Mobile Set! ********* Create Target to Connect To Rigid Body Mass Node *********** *set,tid,10*set,cid,9et,tid,170keyo,tid,2,1 ! Don't fix the pilot nodekeyo,tid,4,0 ! Create CE's for all DOFstype,tidmat ,cidreal,cidtshape,piloen,73,470tshape! ********* End of Create Target to Connect To Rigid Body Mass Node *********** n,473,0.,3.06151588455594e-016,-5.00000000000001*set,_npilot,473_npilot471b=_npilotmat,9real,9type,10en,74,470,473csys,12nrot,_npilot ! rotate joint node into joint coordinate systemcsys,0 ! reset coordinate system back to global/com, Real Contact Set For Above Joint Is 11! Joint Element Type Declaration and Definition using MPC184*set,_jid,11et,_jid,184keyo,_jid,1,6 ! Revolute Jointkeyo,_jid,4,1 ! Z Axis is revolute axissectype,_jid, joint, revo, _wbjointsecjoint,,12,12mat,_jidreal,_jidtype,_jidsecnum,_jiden,64,_npilot471a,_npilot471b ! body to body joint/com,*********** Create Joint "Fixed - Rod1 To Bolt1" ***********local,13,0,0.,3.06151588455594e-016,5.00000000000001,0.,0.,0.csys,0 ! reset coordinate system back to global



! Setup Joint Connection For Reference Set! ********* Create Target to Connect To Rigid Body Mass Node *********** *set,tid,13*set,cid,12et,tid,170keyo,tid,2,1 ! Don't fix the pilot nodekeyo,tid,4,0 ! Create CE's for all DOFstype,tidmat ,cidreal,cidtshape,piloen,75,2tshape! ********* End of Create Target to Connect To Rigid Body Mass Node *********** n,474,0.,3.06151588455594e-016,5.00000000000001*set,_npilot,474_npilot472a=_npilotmat,12real,12type,13en,76,2,474csys,13nrot,_npilot ! rotate joint node into joint coordinate systemcsys,0 ! reset coordinate system back to global! Setup Joint Connection For Mobile Setn,475,0.,3.06151588455594e-016,5.00000000000001*set,_npilot,475_npilot472b=_npilotmat,9real,9type,10en,77,470,475csys,13nrot,_npilot ! rotate joint node into joint coordinate systemcsys,0 ! reset coordinate system back to global! Joint Element Type Declaration and Definition using TARGE170*set,tid,15*set,cid,14et,tid,170keyo,tid,2,1 ! Don't fix the pilot nodekeyo,tid,4,0 ! Create CE's for all DOFsmat,cidreal,cidtype,tidtshape,piloen,65,_npilot472a ! create pilot node for rigid linktshapetype,tiden,78,_npilot472a,_npilot472bcsys,0/com,*********** Create Joint "Fixed - Rod1 To Bolt2" ***********local,14,0,47.6030788398054,27.5490488527501,5.,0.,0.,0.csys,0 ! reset coordinate system back to global! Setup Joint Connection For Reference Setn,476,47.6030788398054,27.5490488527501,5.*set,_npilot,476_npilot473a=_npilotmat,12real,12type,13en,79,2,476csys,14nrot,_npilot ! rotate joint node into joint coordinate systemcsys,0 ! reset coordinate system back to global! Setup Joint Connection For Mobile Set! ********* Create Target to Connect To Rigid Body Mass Node *********** *set,tid,17*set,cid,16et,tid,170keyo,tid,2,1 ! Don't fix the pilot nodekeyo,tid,4,0 ! Create CE's for all DOFstype,tid




mat ,cidreal,cidtshape,piloen,80,471tshape! ********* End of Create Target to Connect To Rigid Body Mass Node *********** n,477,47.6030788398054,27.5490488527501,5.*set,_npilot,477_npilot473b=_npilotmat,16real,16type,17en,81,471,477csys,14nrot,_npilot ! rotate joint node into joint coordinate systemcsys,0 ! reset coordinate system back to global! Joint Element Type Declaration and Definition using TARGE170*set,tid,19*set,cid,18et,tid,170keyo,tid,2,1 ! Don't fix the pilot nodekeyo,tid,4,0 ! Create CE's for all DOFsmat,cidreal,cidtype,tidtshape,piloen,66,_npilot473a ! create pilot node for rigid linktshapetype,tiden,82,_npilot473a,_npilot473bcsys,0/com,*********** Create Joint "Fixed - Rod2 To Bolt3" ***********local,15,0,1.45519152283668e-014,110.,15.,0.,0.,0.csys,0 ! reset coordinate system back to global! Setup Joint Connection For Reference Set*set,tid,21*set,cid,20et,cid,174et,tid,170keyo,tid,2,1 ! Don't fix the pilot nodekeyo,tid,4,0 ! Activate all DOF's due to either large deformation or CERIG stylekeyo,cid,12,5 ! Bonded Contact keyo,cid,4,2 ! Rigid CERIG style loadkeyo,cid,2,2 ! MPC style contacteblock,10(15i8) 83 20 20 20 0 119 120 19 112 468 399 422 421 84 20 20 20 0 112 19 29 35 422 400 259 419 85 20 20 20 0 112 113 126 119 420 418 423 421 86 20 20 20 0 35 36 113 112 276 416 420 419 87 20 20 20 0 113 114 125 126 417 415 424 418 88 20 20 20 0 36 34 114 113 275 413 417 416 89 20 20 20 0 114 115 124 125 414 412 425 415 90 20 20 20 0 34 33 115 114 274 410 414 413 91 20 20 20 0 115 116 123 124 411 409 426 412 92 20 20 20 0 33 32 116 115 273 407 411 410 93 20 20 20 0 116 117 122 123 408 406 427 409 94 20 20 20 0 32 31 117 116 272 404 408 407 95 20 20 20 0 117 118 121 122 405 403 428 406 96 20 20 20 0 31 30 118 117 271 401 405 404 97 20 20 20 0 118 19 120 121 402 399 429 403 98 20 20 20 0 30 29 19 118 270 400 402 401-1*set,_npilot,478_npilot474a=_npilotn,_npilot,1.45519152283668e-014,110.,15.type,tidmat ,cidreal,cidtshape,piloen,99,_npilottshape



csys,15nrot,_npilot ! rotate joint node into joint coordinate systemcsys,0 ! reset coordinate system back to global! Setup Joint Connection For Mobile Set! ********* Create Target to Connect To Rigid Body Mass Node *********** *set,tid,23*set,cid,22et,tid,170keyo,tid,2,1 ! Don't fix the pilot nodekeyo,tid,4,0 ! Create CE's for all DOFstype,tidmat ,cidreal,cidtshape,piloen,100,469tshape! ********* End of Create Target to Connect To Rigid Body Mass Node *********** n,479,1.45519152283668e-014,110.,15.*set,_npilot,479_npilot474b=_npilotmat,22real,22type,23en,101,469,479csys,15nrot,_npilot ! rotate joint node into joint coordinate systemcsys,0 ! reset coordinate system back to global! Joint Element Type Declaration and Definition using TARGE170*set,tid,25*set,cid,24et,tid,170keyo,tid,2,1 ! Don't fix the pilot nodekeyo,tid,4,0 ! Create CE's for all DOFsmat,cidreal,cidtype,tidtshape,piloen,67,_npilot474a ! create pilot node for rigid linktshapetype,tiden,102,_npilot474a,_npilot474bcsys,0/com,*********** Create Joint "Cylindrical - Rod2 To Bolt2" ***********local,16,0,47.6030788398054,27.5490488527501,15.,0.,0.,0.csys,0 ! reset coordinate system back to global! Setup Joint Connection For Reference Set*set,tid,27*set,cid,26et,cid,174et,tid,170keyo,tid,2,1 ! Don't fix the pilot nodekeyo,tid,4,0 ! Activate all DOF's due to either large deformation or CERIG stylekeyo,cid,12,5 ! Bonded Contact keyo,cid,4,2 ! Rigid CERIG style loadkeyo,cid,2,2 ! MPC style contacteblock,10(15i8) 103 26 26 26 0 134 135 18 127 467 430 453 452 104 26 26 26 0 127 18 21 27 453 431 260 450 105 26 26 26 0 127 128 141 134 451 449 454 452 106 26 26 26 0 27 28 128 127 269 447 451 450 107 26 26 26 0 128 129 140 141 448 446 455 449 108 26 26 26 0 28 26 129 128 268 444 448 447 109 26 26 26 0 129 130 139 140 445 443 456 446 110 26 26 26 0 26 25 130 129 267 441 445 444 111 26 26 26 0 130 131 138 139 442 440 457 443 112 26 26 26 0 25 24 131 130 266 438 442 441 113 26 26 26 0 131 132 137 138 439 437 458 440 114 26 26 26 0 24 23 132 131 265 435 439 438 115 26 26 26 0 132 133 136 137 436 434 459 437 116 26 26 26 0 23 22 133 132 264 432 436 435 117 26 26 26 0 133 18 135 136 433 430 460 434




118 26 26 26 0 22 21 18 133 263 431 433 432-1*set,_npilot,480_npilot475a=_npilotn,_npilot,47.6030788398054,27.5490488527501,15.type,tidmat ,cidreal,cidtshape,piloen,119,_npilottshapecsys,16nrot,_npilot ! rotate joint node into joint coordinate systemcsys,0 ! reset coordinate system back to global! Setup Joint Connection For Mobile Setn,481,47.6030788398054,27.5490488527501,15.*set,_npilot,481_npilot475b=_npilotmat,16real,16type,17en,120,471,481csys,16nrot,_npilot ! rotate joint node into joint coordinate systemcsys,0 ! reset coordinate system back to global/com, Real Contact Set For Above Joint Is 28! Joint Element Type Declaration and Definition using MPC184*set,_jid,28et,_jid,184keyo,_jid,1,11 ! Cylindrical Jointkeyo,_jid,4,1 ! Z Axis is revolute axissectype,_jid, joint, cyli, _wbjointsecjoint,,16,16mat,_jidreal,_jidtype,_jidsecnum,_jiden,68,_npilot475a,_npilot475b ! body to body joint/com,*********** Create Joint "Slot - Base To Bolt3" ***********local,17,0,4.57554378011943e-017,110.000000097686,-10.,-90.,0.,180.csys,0 ! reset coordinate system back to global! Setup Joint Connection For Reference Setn,482,4.57554378011943e-017,110.000000097686,-10.*set,_npilot,482_npilot476a=_npilotmat,7real,7type,8en,121,1,482csys,17nrot,_npilot ! rotate joint node into joint coordinate systemcsys,0 ! reset coordinate system back to global! Setup Joint Connection For Mobile Setn,483,4.57554378011943e-017,110.000000097686,-10.*set,_npilot,483_npilot476b=_npilotmat,22real,22type,23en,122,469,483csys,17nrot,_npilot ! rotate joint node into joint coordinate systemcsys,0 ! reset coordinate system back to global/com, Real Contact Set For Above Joint Is 29! Joint Element Type Declaration and Definition using MPC184*set,_jid,29et,_jid,184keyo,_jid,1,8 ! Slot Jointsectype,_jid, joint, slot, _wbjointsecjoint,,17,17mat,_jidreal,_jid



type,_jidsecnum,_jiden,69,_npilot476a,_npilot476b ! body to body joint/com,*********** Create Joint "Fixed - Ground To Base" ***********local,18,0,0.,-100.,-5.,0.,90.,0.csys,0 ! reset coordinate system back to global! Setup Joint Connection For Mobile Setn,484,0.,-100.,-5.*set,_npilot,484_npilot477b=_npilotmat,7real,7type,8en,123,1,484csys,18nrot,_npilot ! rotate joint node into joint coordinate systemcsys,0 ! reset coordinate system back to globald,484,all ! body to ground Direct D/com,*********** Set Reference Temperature ***********tref,22./com,*********** Create Joint Drivers **********

*DIM,_loadvari493,TABLE,1,1,1,TIME! Time values_loadvari493(1,0) = 1.! Load values_loadvari493(1,1) = 25./com,*********** Send User Defined Coordinate System(s) ***********local,12,0,0.,3.06151588455594e-016,-5.00000000000001,0.,0.,-180.local,13,0,0.,3.06151588455594e-016,5.00000000000001,0.,0.,0.local,14,0,47.6030788398054,27.5490488527501,5.,0.,0.,0.local,15,0,1.45519152283668e-014,110.,15.,0.,0.,0.local,16,0,47.6030788398054,27.5490488527501,15.,0.,0.,0.local,17,0,4.57554378011943e-017,110.000000097686,-10.,-90.,0.,180.local,18,0,0.,-100.,-5.,0.,90.,0.csys,0/gst,on,onfini*get,_numnode,node,0,count*get,_numelem,elem,0,count/go/com,--- Number of total nodes = %_numnode%/com,--- Number of total elements = %_numelem%/com,****************************************************************************/com,************************* SOLUTION ********************************/com,****************************************************************************/soluantype,4 ! transient analysisnlgeom,on ! Turn on Large Deformation Effectssolc,on,on ! Turn on solution control with ability to use contact time predictionkbc,1 ! stepped BC's/com, Avg ratio= 1, totalParts=6, thickParts=0, thickPcent= 0eqsl,sparse,,,,,1resc,,none ! Do not keep any restart filescntr,print,1 ! print out contact info and also make no initial contact an errortrnopt,full,,,,,hht ! HHT time integration methodtintp,0.1 ! Numerical Dampingnldiag,cont,iter ! print out contact info each equilibrium iteration/com,****************************************************/com,******************* SOLVE FOR LS 1 ****************/nopr/gopresel,s,type,,11dj,all,dmgz,%_loadvari493%esel,allautots,off ! User turned off automatic time steppingnsub,100,100,100time,1.timint,on ! Turn on time integration effectsoutres,eraseoutres,all,noneoutres,nsol,-100




outres,rsol,-100outres,nload,-100outres,strs,-100outres,epel,-100outres,eppl,-100outres,v,-100outres,a,-100esel,s,mat,,11esel,a,mat,,28esel,a,mat,,29esel,a,mat,,1esel,a,mat,,2esel,a,mat,,4esel,a,mat,,5esel,a,mat,,6cm,_elmisc,elemesel,alloutres,misc,-100,_elmisclnsr,off ! Line search turned OFF by user

! *********** WB SOLVE COMMAND ***********

solvefini

CrankSlot_FlexibleCMS.inp

/batch/prep7! Turn off shape checking because checks already performed inside WB mesher.! See help system for more information.SHPP,OFF,,NOWARN/nolistetcon,set ! allow ANSYS to choose best KEYOP's for 180x elements/com,*********** Nodes for the whole assembly ***********nblock,3(1i8,3e20.9e3) 1 0.000000000E+000 3.529175918E+001 -5.000000000E+000 2 2.378511247E+001 1.380297652E+001 5.000000000E+000 3 3.747472964E+001 4.559062494E+001 1.500000000E+001 4 2.963480264E+000 1.004528103E+002 1.500000000E+001 5 4.418837782E+001 3.642574588E+001 1.500000000E+001 6 -1.379888426E+000 1.165590246E+002 1.500000000E+001 7 -5.887184641E+000 1.140364304E+002 1.500000000E+001 8 3.747472964E+001 4.559062494E+001 1.000000000E+001 9 2.963480264E+000 1.004528103E+002 1.000000000E+001 10 4.418837782E+001 3.642574588E+001 1.000000000E+001 11 -1.379888426E+000 1.165590246E+002 1.000000000E+001 12 -5.887184641E+000 1.140364304E+002 1.000000000E+001 13 -5.887184641E+000 1.140364304E+002 2.000000000E+001 14 -1.379888426E+000 1.165590246E+002 2.000000000E+001 15 4.418837782E+001 3.642574588E+001 2.000000000E+001 16 2.963480264E+000 1.004528103E+002 2.000000000E+001 17 3.747472964E+001 4.559062494E+001 2.000000000E+001 18 5.260307884E+001 2.754904885E+001 1.500000000E+001 19 5.000000000E+000 1.100000000E+002 1.500000000E+001 20 -5.000000000E+000 1.186602540E+002 2.000000000E+001 21 5.260307884E+001 2.754904885E+001 2.000000000E+001 22 5.113861275E+001 2.401351495E+001 2.000000000E+001 23 4.760307884E+001 2.254904885E+001 2.000000000E+001 24 4.406754493E+001 2.401351495E+001 2.000000000E+001 25 4.260307884E+001 2.754904885E+001 2.000000000E+001 26 4.406754493E+001 3.108458276E+001 2.000000000E+001 27 5.113861275E+001 3.108458276E+001 2.000000000E+001 28 4.760307884E+001 3.254904885E+001 2.000000000E+001 29 5.000000000E+000 1.100000000E+002 2.000000000E+001 30 3.535533906E+000 1.064644661E+002 2.000000000E+001 31 1.357163622E-014 1.050000000E+002 2.000000000E+001 32 -3.535533906E+000 1.064644661E+002 2.000000000E+001 33 -5.000000000E+000 1.100000000E+002 2.000000000E+001 34 -3.535533906E+000 1.135355339E+002 2.000000000E+001



35 3.535533906E+000 1.135355339E+002 2.000000000E+001 36 1.135119017E-014 1.150000000E+002 2.000000000E+001 37 -1.149519053E+001 1.149102540E+002 2.000000000E+001 38 -7.894998101E+000 1.086745378E+002 2.000000000E+001 39 -4.294805673E+000 1.024388216E+002 2.000000000E+001 40 2.905579182E+000 8.996738923E+001 2.000000000E+001 41 1.010596404E+001 7.749595683E+001 2.000000000E+001 42 1.730634889E+001 6.502452443E+001 2.000000000E+001 43 2.450673375E+001 5.255309202E+001 2.000000000E+001 44 3.170711860E+001 4.008165962E+001 2.000000000E+001 45 3.530731103E+001 3.384594342E+001 2.000000000E+001 46 3.890750346E+001 2.761022722E+001 2.000000000E+001 47 4.250769588E+001 2.137451102E+001 2.000000000E+001 48 4.610788831E+001 1.513879481E+001 2.000000000E+001 49 5.260307884E+001 1.888879481E+001 2.000000000E+001 50 5.909826937E+001 2.263879481E+001 2.000000000E+001 51 5.549807694E+001 2.887451102E+001 2.000000000E+001 52 5.189788451E+001 3.511022722E+001 2.000000000E+001 53 4.469749966E+001 4.758165962E+001 2.000000000E+001 54 3.749711480E+001 6.005309202E+001 2.000000000E+001 55 3.029672995E+001 7.252452443E+001 2.000000000E+001 56 2.309634509E+001 8.499595683E+001 2.000000000E+001 57 1.589596024E+001 9.746738923E+001 2.000000000E+001 58 1.229576781E+001 1.037031054E+002 2.000000000E+001 59 8.695575383E+000 1.099388216E+002 2.000000000E+001 60 5.095382956E+000 1.161745378E+002 2.000000000E+001 61 1.495190528E+000 1.224102540E+002 2.000000000E+001 62 5.095382956E+000 1.161745378E+002 1.500000000E+001 63 8.695575383E+000 1.099388216E+002 1.500000000E+001 64 1.229576781E+001 1.037031054E+002 1.500000000E+001 65 1.589596024E+001 9.746738923E+001 1.500000000E+001 66 2.309634509E+001 8.499595683E+001 1.500000000E+001 67 3.029672995E+001 7.252452443E+001 1.500000000E+001 68 3.749711480E+001 6.005309202E+001 1.500000000E+001 69 4.469749966E+001 4.758165962E+001 1.500000000E+001 70 5.189788451E+001 3.511022722E+001 1.500000000E+001 71 5.549807694E+001 2.887451102E+001 1.500000000E+001 72 5.095382956E+000 1.161745378E+002 1.000000000E+001 73 8.695575383E+000 1.099388216E+002 1.000000000E+001 74 1.229576781E+001 1.037031054E+002 1.000000000E+001 75 1.589596024E+001 9.746738923E+001 1.000000000E+001 76 2.309634509E+001 8.499595683E+001 1.000000000E+001 77 3.029672995E+001 7.252452443E+001 1.000000000E+001 78 3.749711480E+001 6.005309202E+001 1.000000000E+001 79 4.469749966E+001 4.758165962E+001 1.000000000E+001 80 5.189788451E+001 3.511022722E+001 1.000000000E+001 81 5.549807694E+001 2.887451102E+001 1.000000000E+001 82 1.495190528E+000 1.224102540E+002 1.000000000E+001 83 1.495190528E+000 1.224102540E+002 1.500000000E+001 84 5.909826937E+001 2.263879481E+001 1.000000000E+001 85 5.909826937E+001 2.263879481E+001 1.500000000E+001 86 5.260307884E+001 1.888879481E+001 1.500000000E+001 87 5.260307884E+001 1.888879481E+001 1.000000000E+001 88 4.610788831E+001 1.513879481E+001 1.000000000E+001 89 4.610788831E+001 1.513879481E+001 1.500000000E+001 90 -7.894998101E+000 1.086745378E+002 1.500000000E+001 91 -4.294805673E+000 1.024388216E+002 1.500000000E+001 92 2.905579182E+000 8.996738923E+001 1.500000000E+001 93 1.010596404E+001 7.749595683E+001 1.500000000E+001 94 1.730634889E+001 6.502452443E+001 1.500000000E+001 95 2.450673375E+001 5.255309202E+001 1.500000000E+001 96 3.170711860E+001 4.008165962E+001 1.500000000E+001 97 3.530731103E+001 3.384594342E+001 1.500000000E+001 98 3.890750346E+001 2.761022722E+001 1.500000000E+001 99 4.250769588E+001 2.137451102E+001 1.500000000E+001 100 4.250769588E+001 2.137451102E+001 1.000000000E+001 101 3.890750346E+001 2.761022722E+001 1.000000000E+001 102 3.530731103E+001 3.384594342E+001 1.000000000E+001 103 3.170711860E+001 4.008165962E+001 1.000000000E+001 104 2.450673375E+001 5.255309202E+001 1.000000000E+001 105 1.730634889E+001 6.502452443E+001 1.000000000E+001 106 1.010596404E+001 7.749595683E+001 1.000000000E+001




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395 -6.094901887E+000 1.055566797E+002 1.000000000E+001 396 -9.695094315E+000 1.117923959E+002 1.000000000E+001 397 -1.149519053E+001 1.149102540E+002 1.250000000E+001 398 -1.149519053E+001 1.149102540E+002 1.750000000E+001 399 5.000000000E+000 1.100000000E+002 1.250000000E+001 400 5.000000000E+000 1.100000000E+002 1.750000000E+001 401 3.535533906E+000 1.064644661E+002 1.750000000E+001 402 4.619397663E+000 1.080865828E+002 1.500000000E+001 403 3.535533906E+000 1.064644661E+002 1.250000000E+001 404 1.412674773E-014 1.050000000E+002 1.750000000E+001 405 1.913417162E+000 1.053806023E+002 1.500000000E+001 406 1.412674773E-014 1.050000000E+002 1.250000000E+001 407 -3.535533906E+000 1.064644661E+002 1.750000000E+001 408 -1.913417162E+000 1.053806023E+002 1.500000000E+001 409 -3.535533906E+000 1.064644661E+002 1.250000000E+001 410 -5.000000000E+000 1.100000000E+002 1.750000000E+001 411 -4.619397663E+000 1.080865828E+002 1.500000000E+001 412 -5.000000000E+000 1.100000000E+002 1.250000000E+001 413 -3.535533906E+000 1.135355339E+002 1.750000000E+001 414 -4.619397663E+000 1.119134172E+002 1.500000000E+001 415 -3.535533906E+000 1.135355339E+002 1.250000000E+001 416 1.301652471E-014 1.150000000E+002 1.750000000E+001 417 -1.913417162E+000 1.146193977E+002 1.500000000E+001 418 1.301652471E-014 1.150000000E+002 1.250000000E+001 419 3.535533906E+000 1.135355339E+002 1.750000000E+001 420 1.913417162E+000 1.146193977E+002 1.500000000E+001 421 3.535533906E+000 1.135355339E+002 1.250000000E+001 422 4.619397663E+000 1.119134172E+002 1.500000000E+001 423 1.948899197E+000 1.146045404E+002 1.000000000E+001 424 -1.877821874E+000 1.146339816E+002 1.000000000E+001 425 -4.604540359E+000 1.119488992E+002 1.000000000E+001 426 -4.633981550E+000 1.081221781E+002 1.000000000E+001 427 -1.948899197E+000 1.053954596E+002 1.000000000E+001 428 1.877821874E+000 1.053660184E+002 1.000000000E+001 429 4.604540359E+000 1.080511008E+002 1.000000000E+001 430 5.260307884E+001 2.754904885E+001 1.250000000E+001 431 5.260307884E+001 2.754904885E+001 1.750000000E+001 432 5.113861275E+001 2.401351495E+001 1.750000000E+001 433 5.222247650E+001 2.563563169E+001 1.500000000E+001 434 5.113861275E+001 2.401351495E+001 1.250000000E+001 435 4.760307884E+001 2.254904885E+001 1.750000000E+001 436 4.951649600E+001 2.292965119E+001 1.500000000E+001 437 4.760307884E+001 2.254904885E+001 1.250000000E+001 438 4.406754493E+001 2.401351495E+001 1.750000000E+001 439 4.568966168E+001 2.292965119E+001 1.500000000E+001 440 4.406754493E+001 2.401351495E+001 1.250000000E+001 441 4.260307884E+001 2.754904885E+001 1.750000000E+001 442 4.298368118E+001 2.563563169E+001 1.500000000E+001 443 4.260307884E+001 2.754904885E+001 1.250000000E+001 444 4.406754493E+001 3.108458276E+001 1.750000000E+001 445 4.298368118E+001 2.946246601E+001 1.500000000E+001 446 4.406754493E+001 3.108458276E+001 1.250000000E+001 447 4.760307884E+001 3.254904885E+001 1.750000000E+001 448 4.568966168E+001 3.216844652E+001 1.500000000E+001 449 4.760307884E+001 3.254904885E+001 1.250000000E+001 450 5.113861275E+001 3.108458276E+001 1.750000000E+001 451 4.951649600E+001 3.216844652E+001 1.500000000E+001 452 5.113861275E+001 3.108458276E+001 1.250000000E+001 453 5.222247650E+001 2.946246601E+001 1.500000000E+001 454 4.955197804E+001 3.215358921E+001 1.000000000E+001 455 4.572525697E+001 3.218303040E+001 1.000000000E+001 456 4.299853848E+001 2.949794805E+001 1.000000000E+001 457 4.296909729E+001 2.567122698E+001 1.000000000E+001 458 4.565417964E+001 2.294450849E+001 1.000000000E+001 459 4.948090071E+001 2.291506730E+001 1.000000000E+001 460 5.220761920E+001 2.560014966E+001 1.000000000E+001 461 -5.000000000E+000 1.186602540E+002 1.750000000E+001 462 -1.752404736E+000 1.205352540E+002 1.500000000E+001 463 -5.000000000E+000 1.186602540E+002 1.250000000E+001 464 -8.247595264E+000 1.167852540E+002 1.500000000E+001 465 -8.247595264E+000 1.167852540E+002 1.000000000E+001 466 -1.752404736E+000 1.205352540E+002 1.000000000E+001



467 5.223706039E+001 2.942687073E+001 1.000000000E+001 468 4.633981550E+000 1.118778219E+002 1.000000000E+001 469 -4.717895070E-016 1.100000000E+002 5.000000000E+000 470 1.525181166E-017 1.189641309E-016 9.761159461E-017 471 4.760307959E+001 2.754904870E+001 1.000000000E+001-1/com,*********** Elements for Part 1 ***********/com,*********** Send Body as a Rigid Body ***********et,1,MASS21keyo,1,3,0 ! 3D Mass With Rotary Intertiakeyo,1,2,1 ! Moments of inertia in nodal coordinatesr,1,5.62959624417329e-004,5.62959624417329e-004,5.62959624417329e-004,4.27915117762894,5.64969611751201e-002,4.32626430862063local,11,0,0.,35.2917591780688,-4.99999999999951,0.,0.,0.nrot,1csys,0mat,1real,1type,1en,1,1/com,*********** Elements for Part 2 ***********/com,*********** Send Body as a Rigid Body ***********et,2,MASS21keyo,2,3,0 ! 3D Mass With Rotary Intertiakeyo,2,2,1 ! Moments of inertia in nodal coordinatesr,2,7.59817488346602e-005,7.59817488346602e-005,7.59817488346602e-005,2.21486141701566e-003,3.27365368251796e-002,3.36826963131752e-002local,11,0,23.7851124732216,13.8029765212764,4.99999999999951,29.9821797972594,-1.63487457250109e-008,4.06547904138105e-009nrot,2csys,0mat,2real,2type,2en,2,2/com,*********** Elements for Part 3 ***********et,3,186keyo,3,2,1eblock,10(15i8) 3 3 3 3 0 90 115 116 91 109 124 123 108 164 411 0 0 0 0 0 179 383 204 426 215 395 382 412 409 379 4 3 3 3 0 32 39 38 33 116 91 90 115 246 278 0 0 0 0 0 247 273 179 383 164 411 407 381 384 410 5 3 3 3 0 18 127 70 71 135 134 80 81 453 148 0 0 0 0 0 305 144 467 192 341 189 430 452 306 303 6 3 3 3 0 18 71 70 127 21 51 52 27 144 305 0 0 0 0 0 148 453 240 291 244 260 431 301 304 450 7 3 3 3 0 18 71 85 133 135 81 84 136 144 302 0 0 0 0 0 177 433 189 342 213 460 430 303 345 434 8 3 3 3 0 18 133 85 71 21 22 50 51 433 177 0 0 0 0 0 302 144 263 241 290 240 431 432 346 301 9 3 3 3 0 98 130 131 99 101 139 138 100 145 442 0 0 0 0 0 174 359 190 457 211 387 358 443 440 355 10 3 3 3 0 24 47 46 25 131 99 98 130 242 286 0 0 0 0 0 243 266 174 359 145 442 438 357 360 441 11 3 3 3 0 97 129 130 98 102 140 139 101 146 445 0 0 0 0 0 145 362 191 456 190 388 361 446 443 358 12 3 3 3 0 25 46 45 26 130 98 97 129 243 285 0 0 0 0 0 239 267 145 362 146 445 441 360 363 444 13 3 3 3 0 5 128 129 97 10 141 140 102 147 448 0 0 0 0 0 146 151 193 455 191 196 152 449 446 361 14 3 3 3 0 5 97 129 128 15 45 26 28 151 146 0 0 0 0 0 448 147 230 239 268 232 153 363 444 447 15 3 3 3 0 5 70 127 128 10 80 134 141 154 148 0 0 0 0 0 451 147 198 192 454 193 152 306 452 449 16 3 3 3 0 5 128 127 70 15 28 27 52 147 451 0 0 0 0 0 148 154 232 269 244 231 153 447 450 304 17 3 3 3 0 19 112 62 63 120 119 72 73 422 149 0 0 0 0 0 329 181 468 195 333 219 399 421 330 327 18 3 3 3 0 19 63 62 112 29 59 60 35 181 329 0 0 0 0 0 149 422 245 299 248 259 400 325 328 419 19 3 3 3 0 6 142 83 62 11 143 82 72 171 462 0 0 0 0 0 331 150 210 466 332 194 168 463 343 330 20 3 3 3 0 6 62 83 142 14 60 61 20 150 331




0 0 0 0 0 462 171 233 300 261 235 170 328 344 461 21 3 3 3 0 6 62 112 113 11 72 119 126 150 149 0 0 0 0 0 420 166 194 195 423 206 168 330 421 418 22 3 3 3 0 6 113 112 62 14 36 35 60 166 420 0 0 0 0 0 149 150 234 276 248 233 170 416 419 328 23 3 3 3 0 3 5 97 96 8 10 102 103 155 151 0 0 0 0 0 365 159 197 196 389 200 157 152 361 364 24 3 3 3 0 3 96 97 5 17 44 45 15 159 365 0 0 0 0 0 151 155 226 284 230 225 158 366 363 153 25 3 3 3 0 3 69 70 5 8 79 80 10 156 308 0 0 0 0 0 154 155 199 340 198 197 157 309 306 152 26 3 3 3 0 3 5 70 69 17 15 52 53 155 154 0 0 0 0 0 308 156 225 231 292 227 158 153 304 307 27 3 3 3 0 3 95 68 69 8 104 78 79 160 161 0 0 0 0 0 311 156 201 202 339 199 157 367 312 309 28 3 3 3 0 3 69 68 95 17 53 54 43 156 311 0 0 0 0 0 161 160 227 293 236 224 158 307 310 369 29 3 3 3 0 67 68 95 94 77 78 104 105 314 161 0 0 0 0 0 371 162 338 202 391 203 315 312 367 370 30 3 3 3 0 42 55 54 43 94 67 68 95 237 294 0 0 0 0 0 236 282 162 314 161 371 372 313 310 369 31 3 3 3 0 66 67 94 93 76 77 105 106 317 162 0 0 0 0 0 374 188 337 203 392 222 318 315 370 373 32 3 3 3 0 41 56 55 42 93 66 67 94 238 295 0 0 0 0 0 237 281 188 317 162 374 375 316 313 372 33 3 3 3 0 7 114 115 90 12 125 124 109 165 414 0 0 0 0 0 164 163 207 425 204 205 167 415 412 382 34 3 3 3 0 7 90 115 114 13 38 33 34 163 164 0 0 0 0 0 414 165 249 247 274 251 169 384 410 413 35 3 3 3 0 6 113 114 7 11 126 125 12 166 417 0 0 0 0 0 165 173 206 424 207 208 168 418 415 167 36 3 3 3 0 6 7 114 113 14 13 34 36 173 165 0 0 0 0 0 417 166 252 251 275 234 170 169 413 416 37 3 3 3 0 6 7 111 142 11 12 110 143 173 172 0 0 0 0 0 464 171 208 209 465 210 168 167 397 463 38 3 3 3 0 6 142 111 7 14 20 37 13 171 464 0 0 0 0 0 172 173 235 262 250 252 170 461 398 169 39 3 3 3 0 88 137 138 100 89 132 131 99 212 458 0 0 0 0 0 211 386 175 439 174 356 353 437 440 355 40 3 3 3 0 23 48 47 24 132 89 99 131 253 287 0 0 0 0 0 242 265 175 356 174 439 435 354 357 438 41 3 3 3 0 84 136 137 87 85 133 132 86 213 459 0 0 0 0 0 214 351 177 436 176 348 345 434 437 347 42 3 3 3 0 22 50 49 23 133 85 86 132 241 289 0 0 0 0 0 254 264 177 348 176 436 432 346 349 435 43 3 3 3 0 4 91 116 117 9 108 123 122 178 179 0 0 0 0 0 408 180 216 215 427 217 183 379 409 406 44 3 3 3 0 4 117 116 91 16 31 32 39 180 408 0 0 0 0 0 179 178 256 272 246 255 184 404 407 381 45 3 3 3 0 4 117 118 64 9 122 121 74 180 405 0 0 0 0 0 182 185 217 428 218 221 183 406 403 324 46 3 3 3 0 4 64 118 117 16 58 30 31 185 182 0 0 0 0 0 405 180 229 257 271 256 184 322 401 404 47 3 3 3 0 19 63 64 118 120 73 74 121 181 326 0 0 0 0 0 182 402 219 334 218 429 399 327 324 403 48 3 3 3 0 19 118 64 63 29 30 58 59 402 182 0 0 0 0 0 326 181 270 257 298 245 400 401 322 325 49 3 3 3 0 4 64 65 92 9 74 75 107 185 323 0 0 0 0 0 187 186 221 335 223 220 183 324 321 376 50 3 3 3 0 4 92 65 64 16 40 57 58 186 187 0 0 0 0 0 323 185 228 258 297 229 184 378 319 322 51 3 3 3 0 65 66 93 92 75 76 106 107 320 188 0 0 0 0 0 377 187 336 222 393 223 321 318 373 376 52 3 3 3 0 40 57 56 41 92 65 66 93 258 296 0 0 0 0 0 238 280 187 320 188 377 378 319 316 375 53 3 3 3 0 3 96 95 95 8 103 104 104 159 368 0 0 0 0 0 95 160 200 390 104 201 157 364 367 367 54 3 3 3 0 3 95 96 96 17 43 44 44 160 368 0 0 0 0 0 96 159 224 283 44 226 158 369 366 366 55 3 3 3 0 7 90 111 111 12 109 110 110 163 385 0 0 0 0 0 111 172 205 396 110 209 167 382 397 397 56 3 3 3 0 7 111 90 90 13 37 38 38 172 385



0 0 0 0 0 90 163 250 277 38 249 169 398 384 384 57 3 3 3 0 86 89 132 132 87 88 137 137 350 175 0 0 0 0 0 132 176 352 212 137 214 347 353 437 437 58 3 3 3 0 23 49 48 48 132 86 89 89 254 288 0 0 0 0 0 48 253 176 350 89 175 435 349 354 354 59 3 3 3 0 4 92 91 91 9 107 108 108 186 380 0 0 0 0 0 91 178 220 394 108 216 183 376 379 379 60 3 3 3 0 4 91 92 92 16 39 40 40 178 380 0 0 0 0 0 92 186 255 279 40 228 184 381 378 378-1/com,*********** Elements for Part 4 ***********/com,*********** Send Body as a Rigid Body ***********et,4,MASS21keyo,4,3,0 ! 3D Mass With Rotary Intertiakeyo,4,2,1 ! Moments of inertia in nodal coordinatesr,4,1.84961267480099e-005,1.84961267480099e-005,1.84961267480099e-005,1.48440380137047e-003,1.48440385658378e-003,2.259733717427e-004local,11,0,-4.71789506988333e-016,110.000000028382,4.99999999999951,0.,0.,0.nrot,469csys,0mat,4real,4type,4en,61,469/com,*********** Elements for Part 5 ***********/com,*********** Send Body as a Rigid Body ***********et,5,MASS21keyo,5,3,0 ! 3D Mass With Rotary Intertiakeyo,5,2,1 ! Moments of inertia in nodal coordinatesr,5,1.23307511653399e-005,1.23307511653399e-005,1.23307511653399e-005,4.816704325156e-004,4.8167043256163e-004,1.50648999123811e-004local,11,0,1.52518116573376e-017,1.18964130927233e-016,9.76115946069606e-017,0.,0.,0.nrot,470csys,0mat,5real,5type,5en,62,470/com,*********** Elements for Part 6 ***********/com,*********** Send Body as a Rigid Body ***********et,6,MASS21keyo,6,3,0 ! 3D Mass With Rotary Intertiakeyo,6,2,1 ! Moments of inertia in nodal coordinatesr,6,1.23307511653399e-005,1.23307511653399e-005,1.23307511653399e-005,4.81670360832402e-004,4.81670377213366e-004,1.5064896426044e-004local,11,0,47.6030795911263,27.5490486999112,9.99999999999894,0.,0.,0.nrot,471csys,0mat,6real,6type,6en,63,471/com,*********** Send Materials ***********MP,DENS,1,7.85e-009, ! ton/mm³MP,NUXY,1,0.3,MP,EX,1,200000., ! ton/s²·mmMP,ALPX,1,1.2e-005, ! 1/°CMP,C,1,434000000., ! mm²/s²·°CMP,KXX,1,60.5, ! ton·mm/s³·°CMP,MURX,1,10000.,MP,RSVX,1,1.7e-004, ! Ohm·mm


MP,DENS,3,7.85e-009, ! ton/mm³MP,NUXY,3,0.3,MP,EX,3,200000., ! ton/s²·mmMP,ALPX,3,1.2e-005, ! 1/°C




MP,C,3,434000000., ! mm²/s²·°CMP,KXX,3,60.5, ! ton·mm/s³·°CMP,MURX,3,10000.,MP,RSVX,3,1.7e-004, ! Ohm·mm




! get the diagonal of the bounding box. Needed later for other things*get,_xmin,node,,mnloc,x*get,_ymin,node,,mnloc,y*get,_zmin,node,,mnloc,z*get,_xmax,node,,mxloc,x*get,_ymax,node,,mxloc,y*get,_zmax,node,,mxloc,z_ASMDIAG=(_xmax-_xmin)*(_xmax-_xmin)+(_ymax-_ymin)*(_ymax-_ymin)+(_zmax-_zmin)*(_zmax-_zmin)_ASMDIAG=SQRT(_ASMDIAG)/com,*********** Send Named Selection as Element Component ***********esel,noneesel,a,mat,,3cm,VANE,elemesel,all/golistnsel,all/com,*********** Create Joint "Revolute - Base To Bolt1" ***********local,12,0,0.,3.06151588455594e-016,-5.00000000000001,0.,0.,-180.csys,0 ! reset coordinate system back to global! Setup Joint Connection For Reference Set! ********* Create Target to Connect To Rigid Body Mass Node *********** *set,tid,8*set,cid,7et,tid,170keyo,tid,2,1 ! Don't fix the pilot nodekeyo,tid,4,0 ! Create CE's for all DOFstype,tidmat ,cidreal,cidtshape,piloen,71,1tshape! ********* End of Create Target to Connect To Rigid Body Mass Node *********** n,472,0.,3.06151588455594e-016,-5.00000000000001*set,_npilot,472_npilot601a=_npilotmat,7real,7type,8en,72,1,472



csys,12nrot,_npilot ! rotate joint node into joint coordinate systemcsys,0 ! reset coordinate system back to global! Setup Joint Connection For Mobile Set! ********* Create Target to Connect To Rigid Body Mass Node *********** *set,tid,10*set,cid,9et,tid,170keyo,tid,2,1 ! Don't fix the pilot nodekeyo,tid,4,0 ! Create CE's for all DOFstype,tidmat ,cidreal,cidtshape,piloen,73,470tshape! ********* End of Create Target to Connect To Rigid Body Mass Node *********** n,473,0.,3.06151588455594e-016,-5.00000000000001*set,_npilot,473_npilot601b=_npilotmat,9real,9type,10en,74,470,473csys,12nrot,_npilot ! rotate joint node into joint coordinate systemcsys,0 ! reset coordinate system back to global/com, Real Contact Set For Above Joint Is 11! Joint Element Type Declaration and Definition using MPC184*set,_jid,11et,_jid,184keyo,_jid,1,6 ! Revolute Jointkeyo,_jid,4,1 ! Z Axis is revolute axissectype,_jid, joint, revo, _wbjointsecjoint,,12,12mat,_jidreal,_jidtype,_jidsecnum,_jiden,64,_npilot601a,_npilot601b ! body to body joint/com,*********** Create Joint "Fixed - Rod1 To Bolt1" ***********local,13,0,0.,3.06151588455594e-016,5.00000000000001,0.,0.,0.csys,0 ! reset coordinate system back to global! Setup Joint Connection For Reference Set! ********* Create Target to Connect To Rigid Body Mass Node *********** *set,tid,13*set,cid,12et,tid,170keyo,tid,2,1 ! Don't fix the pilot nodekeyo,tid,4,0 ! Create CE's for all DOFstype,tidmat ,cidreal,cidtshape,piloen,75,2tshape! ********* End of Create Target to Connect To Rigid Body Mass Node *********** n,474,0.,3.06151588455594e-016,5.00000000000001*set,_npilot,474_npilot602a=_npilotmat,12real,12type,13en,76,2,474csys,13nrot,_npilot ! rotate joint node into joint coordinate systemcsys,0 ! reset coordinate system back to global! Setup Joint Connection For Mobile Setn,475,0.,3.06151588455594e-016,5.00000000000001*set,_npilot,475_npilot602b=_npilotmat,9




real,9type,10en,77,470,475csys,13nrot,_npilot ! rotate joint node into joint coordinate systemcsys,0 ! reset coordinate system back to global! Joint Element Type Declaration and Definition using TARGE170*set,tid,15*set,cid,14et,tid,170keyo,tid,2,1 ! Don't fix the pilot nodekeyo,tid,4,0 ! Create CE's for all DOFsmat,cidreal,cidtype,tidtshape,piloen,65,_npilot602a ! create pilot node for rigid linktshapetype,tiden,78,_npilot602a,_npilot602bcsys,0/com,*********** Create Joint "Fixed - Rod1 To Bolt2" ***********local,14,0,47.6030788398054,27.5490488527501,5.,0.,0.,0.csys,0 ! reset coordinate system back to global! Setup Joint Connection For Reference Setn,476,47.6030788398054,27.5490488527501,5.*set,_npilot,476_npilot603a=_npilotmat,12real,12type,13en,79,2,476csys,14nrot,_npilot ! rotate joint node into joint coordinate systemcsys,0 ! reset coordinate system back to global! Setup Joint Connection For Mobile Set! ********* Create Target to Connect To Rigid Body Mass Node *********** *set,tid,17*set,cid,16et,tid,170keyo,tid,2,1 ! Don't fix the pilot nodekeyo,tid,4,0 ! Create CE's for all DOFstype,tidmat ,cidreal,cidtshape,piloen,80,471tshape! ********* End of Create Target to Connect To Rigid Body Mass Node *********** n,477,47.6030788398054,27.5490488527501,5.*set,_npilot,477_npilot603b=_npilotmat,16real,16type,17en,81,471,477csys,14nrot,_npilot ! rotate joint node into joint coordinate systemcsys,0 ! reset coordinate system back to global! Joint Element Type Declaration and Definition using TARGE170*set,tid,19*set,cid,18et,tid,170keyo,tid,2,1 ! Don't fix the pilot nodekeyo,tid,4,0 ! Create CE's for all DOFsmat,cidreal,cidtype,tidtshape,piloen,66,_npilot603a ! create pilot node for rigid linktshapetype,tid



en,82,_npilot603a,_npilot603bcsys,0/com,*********** Create Joint "Fixed - Rod2 To Bolt3" ***********local,15,0,1.45519152283668e-014,110.,15.,0.,0.,0.csys,0 ! reset coordinate system back to global! Setup Joint Connection For Reference Set*set,tid,21*set,cid,20et,cid,174et,tid,170keyo,tid,2,1 ! Don't fix the pilot nodekeyo,tid,4,0 ! Activate all DOF's due to either large deformation or CERIG stylekeyo,cid,12,5 ! Bonded Contact keyo,cid,4,2 ! Rigid CERIG style loadkeyo,cid,2,2 ! MPC style contacteblock,10(15i8) 83 20 20 20 0 119 120 19 112 468 399 422 421 84 20 20 20 0 112 19 29 35 422 400 259 419 85 20 20 20 0 112 113 126 119 420 418 423 421 86 20 20 20 0 35 36 113 112 276 416 420 419 87 20 20 20 0 113 114 125 126 417 415 424 418 88 20 20 20 0 36 34 114 113 275 413 417 416 89 20 20 20 0 114 115 124 125 414 412 425 415 90 20 20 20 0 34 33 115 114 274 410 414 413 91 20 20 20 0 115 116 123 124 411 409 426 412 92 20 20 20 0 33 32 116 115 273 407 411 410 93 20 20 20 0 116 117 122 123 408 406 427 409 94 20 20 20 0 32 31 117 116 272 404 408 407 95 20 20 20 0 117 118 121 122 405 403 428 406 96 20 20 20 0 31 30 118 117 271 401 405 404 97 20 20 20 0 118 19 120 121 402 399 429 403 98 20 20 20 0 30 29 19 118 270 400 402 401-1*set,_npilot,478_npilot604a=_npilotn,_npilot,1.45519152283668e-014,110.,15.type,tidmat ,cidreal,cidtshape,piloen,99,_npilottshapecsys,15nrot,_npilot ! rotate joint node into joint coordinate systemcsys,0 ! reset coordinate system back to global! Setup Joint Connection For Mobile Set! ********* Create Target to Connect To Rigid Body Mass Node *********** *set,tid,23*set,cid,22et,tid,170keyo,tid,2,1 ! Don't fix the pilot nodekeyo,tid,4,0 ! Create CE's for all DOFstype,tidmat ,cidreal,cidtshape,piloen,100,469tshape! ********* End of Create Target to Connect To Rigid Body Mass Node *********** n,479,1.45519152283668e-014,110.,15.*set,_npilot,479_npilot604b=_npilotmat,22real,22type,23en,101,469,479csys,15nrot,_npilot ! rotate joint node into joint coordinate systemcsys,0 ! reset coordinate system back to global! Joint Element Type Declaration and Definition using TARGE170*set,tid,25




*set,cid,24et,tid,170keyo,tid,2,1 ! Don't fix the pilot nodekeyo,tid,4,0 ! Create CE's for all DOFsmat,cidreal,cidtype,tidtshape,piloen,67,_npilot604a ! create pilot node for rigid linktshapetype,tiden,102,_npilot604a,_npilot604bcsys,0/com,*********** Create Joint "Cylindrical - Rod2 To Bolt2" ***********local,16,0,47.6030788398054,27.5490488527501,15.,0.,0.,0.csys,0 ! reset coordinate system back to global! Setup Joint Connection For Reference Set*set,tid,27*set,cid,26et,cid,174et,tid,170keyo,tid,2,1 ! Don't fix the pilot nodekeyo,tid,4,0 ! Activate all DOF's due to either large deformation or CERIG stylekeyo,cid,12,5 ! Bonded Contact keyo,cid,4,2 ! Rigid CERIG style loadkeyo,cid,2,2 ! MPC style contacteblock,10(15i8) 103 26 26 26 0 134 135 18 127 467 430 453 452 104 26 26 26 0 127 18 21 27 453 431 260 450 105 26 26 26 0 127 128 141 134 451 449 454 452 106 26 26 26 0 27 28 128 127 269 447 451 450 107 26 26 26 0 128 129 140 141 448 446 455 449 108 26 26 26 0 28 26 129 128 268 444 448 447 109 26 26 26 0 129 130 139 140 445 443 456 446 110 26 26 26 0 26 25 130 129 267 441 445 444 111 26 26 26 0 130 131 138 139 442 440 457 443 112 26 26 26 0 25 24 131 130 266 438 442 441 113 26 26 26 0 131 132 137 138 439 437 458 440 114 26 26 26 0 24 23 132 131 265 435 439 438 115 26 26 26 0 132 133 136 137 436 434 459 437 116 26 26 26 0 23 22 133 132 264 432 436 435 117 26 26 26 0 133 18 135 136 433 430 460 434 118 26 26 26 0 22 21 18 133 263 431 433 432-1*set,_npilot,480_npilot605a=_npilotn,_npilot,47.6030788398054,27.5490488527501,15.type,tidmat ,cidreal,cidtshape,piloen,119,_npilottshapecsys,16nrot,_npilot ! rotate joint node into joint coordinate systemcsys,0 ! reset coordinate system back to global! Setup Joint Connection For Mobile Setn,481,47.6030788398054,27.5490488527501,15.*set,_npilot,481_npilot605b=_npilotmat,16real,16type,17en,120,471,481csys,16nrot,_npilot ! rotate joint node into joint coordinate systemcsys,0 ! reset coordinate system back to global/com, Real Contact Set For Above Joint Is 28! Joint Element Type Declaration and Definition using MPC184*set,_jid,28et,_jid,184



keyo,_jid,1,11 ! Cylindrical Jointkeyo,_jid,4,1 ! Z Axis is revolute axissectype,_jid, joint, cyli, _wbjointsecjoint,,16,16mat,_jidreal,_jidtype,_jidsecnum,_jiden,68,_npilot605a,_npilot605b ! body to body joint/com,*********** Create Joint "Slot - Base To Bolt3" ***********local,17,0,4.57554378011943e-017,110.000000097686,-10.,-90.,0.,180.csys,0 ! reset coordinate system back to global! Setup Joint Connection For Reference Setn,482,4.57554378011943e-017,110.000000097686,-10.*set,_npilot,482_npilot606a=_npilotmat,7real,7type,8en,121,1,482csys,17nrot,_npilot ! rotate joint node into joint coordinate systemcsys,0 ! reset coordinate system back to global! Setup Joint Connection For Mobile Setn,483,4.57554378011943e-017,110.000000097686,-10.*set,_npilot,483_npilot606b=_npilotmat,22real,22type,23en,122,469,483csys,17nrot,_npilot ! rotate joint node into joint coordinate systemcsys,0 ! reset coordinate system back to global/com, Real Contact Set For Above Joint Is 29! Joint Element Type Declaration and Definition using MPC184*set,_jid,29et,_jid,184keyo,_jid,1,8 ! Slot Jointsectype,_jid, joint, slot, _wbjointsecjoint,,17,17mat,_jidreal,_jidtype,_jidsecnum,_jiden,69,_npilot606a,_npilot606b ! body to body joint/com,*********** Create Joint "Fixed - Ground To Base" ***********local,18,0,0.,-100.,-5.,0.,90.,0.csys,0 ! reset coordinate system back to global! Setup Joint Connection For Mobile Setn,484,0.,-100.,-5.*set,_npilot,484_npilot607b=_npilotmat,7real,7type,8en,123,1,484csys,18nrot,_npilot ! rotate joint node into joint coordinate systemcsys,0 ! reset coordinate system back to globald,484,all ! body to ground Direct D/com,*********** Set Reference Temperature ***********tref,22./com,*********** Create Joint Drivers **********

*DIM,_loadvari617,TABLE,1,1,1,TIME! Time values_loadvari617(1,0) = 1.! Load values_loadvari617(1,1) = 25./com,*********** Send User Defined Coordinate System(s) ***********local,12,0,0.,3.06151588455594e-016,-5.00000000000001,0.,0.,-180.




local,13,0,0.,3.06151588455594e-016,5.00000000000001,0.,0.,0.local,14,0,47.6030788398054,27.5490488527501,5.,0.,0.,0.local,15,0,1.45519152283668e-014,110.,15.,0.,0.,0.local,16,0,47.6030788398054,27.5490488527501,15.,0.,0.,0.local,17,0,4.57554378011943e-017,110.000000097686,-10.,-90.,0.,180.local,18,0,0.,-100.,-5.,0.,90.,0.csys,0/com,*********** Create Components for CMS ***********nsel,none ! create nodal component of master nodesnsel,a,node,,478,! add pilot node attached to this bodynsel,a,node,,480,! add pilot node attached to this bodycm,VANE_master,nodeesel,s,elem,,VANEnsle ! select any nodes touching these bodies in the user componentesln ! add in any touching elements such as contact and surf effectesel,a,elem,,99,! add target element attached to this bodyesel,a,elem,,119,! add target element attached to this bodycm,VANE_slave,elemallsel/gst,on,onfini*get,_numnode,node,0,count*get,_numelem,elem,0,count/go/com,--- Number of total nodes = %_numnode%/com,--- Number of total elements = %_numelem%/com,****************************************************************************/com,************************* SOLUTION ********************************/com,****************************************************************************/soluantype,4 ! transient analysisnlgeom,on ! Turn on Large Deformation Effectssolc,on,on ! Turn on solution control with ability to use contact time predictionkbc,1 ! stepped BC's/com, Avg ratio= 1, totalParts=6, thickParts=0, thickPcent= 0eqsl,sparse,,,,,1resc,,none ! Do not keep any restart filescntr,print,1 ! print out contact info and also make no initial contact an errortrnopt,full,,,,,hht ! HHT time integration methodtintp,0.1 ! Numerical Dampingnldiag,cont,iter ! print out contact info each equilibrium iteration/com,****************************************************/com,******************* SOLVE FOR LS 1 ****************/nopr/gopresel,s,type,,11dj,all,dmgz,%_loadvari617%esel,allautots,off ! User turned off automatic time steppingnsub,100,100,100time,1.timint,on ! Turn on time integration effectsoutres,eraseoutres,all,noneoutres,nsol,-100outres,rsol,-100outres,nload,-100outres,strs,-100outres,epel,-100outres,eppl,-100outres,v,-100outres,a,-100esel,s,mat,,11esel,a,mat,,28esel,a,mat,,29esel,a,mat,,1esel,a,mat,,2esel,a,mat,,4esel,a,mat,,5esel,a,mat,,6cm,_elmisc,elemesel,all



outres,misc,-100,_elmisclnsr,off ! Line search turned OFF by user! ****** Begin Command Snippet ******! Commands inserted into this file will be executed just prior to the Ansys SOLVE command.! These commands may supercede command settings set by Workbench.

! Active UNIT system in Workbench when this object was created: Metric (mm, kg, N, C, s, mV, mA)

!!!!! save the full modelfini/filnam,fullsave

!!!!! perform substructure generation/clear,nostart/filnam,vaneresu,full,db

/soluantype,subst ! substructure analysis typeseopt,vane,2 ! substructure and option for stiffness and masscmsopt,fix,12 ! cms options and number of modes

cmse,s,VANE_master ! select the substructure nodesm,all,all ! specify master dofs for superelement

cmse,s,VANE_slave ! select the substructure elements nsle ! select nodel for substructure elementssave

solve ! solve the substructurefini

!!!!! perform use pass solution/clear,nostart/filnam,useresu,full,db

/prep7cmse,u,VANE_slave ! unselect the flexible elementsnelecmse,a,VANE_master ! make sure the master nodes are selected

se_itype=etyiqr(0,14)+1et,se_itype,50 ! define substructure element type using available itype numbertype,se_itypemat,1se,vane ! define substructure elementfini

/soluantype,transientsolvefini

!!!!! expand the solution/clear,nostart/filnam,vaneresu

/soluexpass,onseexp,vane,use ! substructure name and the use pass jobname numexp,all,,,yes ! Expand all time pointssolvefini

!!!!! merge results file




/clear,nostart/filnam,fullresume/delete

/post1nsubsteps=100 ! number of time points*do,j,1,nsubsteps file,use set,1,j file,vane append,1,j reswrite,file ! file name for results file*enddo

:next

! ****** End Command Snippet ******! *********** WB SOLVE COMMAND ***********solve/com,****************************************************/com,*************** FINISHED SOLVE FOR LS 1 **************set,_DS_PROGRESS ! turn off progress updates to avoid virus scanning bugfini

Modal Analysis Using WorkBench - Output File

ANSYS Multiphysics

*-------------------------------------------------------------* | | | W E L C O M E T O T H E A N S Y S P R O G R A M | | | *-------------------------------------------------------------*

*************************************************************** * ANSYS 14.0 LEGAL NOTICES * *************************************************************** * * * COPYRIGHT AND TRADEMARK INFORMATION * * * * Copyright 2011 SAS IP, Inc. All rights reserved. * * Unauthorized use, distribution or duplication is * * prohibited. * * * * See the ANSYS, Inc. online documentation or the ANSYS, Inc. * * documentation CD for the complete Legal Notice. * * * *************************************************************** * * * DISCLAIMER NOTICE * * * * THIS ANSYS SOFTWARE PRODUCT AND PROGRAM DOCUMENTATION * * EMBODY TRADE SECRETS AND CONFIDENTIAL AND PROPRIETARY * * INFORMATION OF ANSYS, INC., ITS SUBSIDIARIES, OR LICENSORS. * * The software products and documentation are furnished by * * ANSYS, Inc. or its subsidiaries under a software license * * agreement that contains provisions concerning * * non-disclosure, copying, length and nature of use, * * compliance with exporting laws, warranties, disclaimers, * * limitations of liability, and remedies, and other * * provisions. The software products and documentation may be * * used, disclosed, transferred, or copied only in accordance *



* with the terms and conditions of that software license * * agreement. * * * * ANSYS, Inc. and ANSYS Europe, Ltd. are UL registered * * ISO 9001:2000 Companies. * * * *************************************************************** * * * U.S. GOVERNMENT RIGHTS * * * * For U.S. Government users, except as specifically granted * * by the ANSYS, Inc. software license agreement, the use, * * duplication, or disclosure by the United States Government * * is subject to restrictions stated in the ANSYS, Inc. * * software license agreement and FAR 12.212 (for non-DOD * * licenses). * * * ***************************************************************

***** ANSYS COMMAND LINE ARGUMENTS ***** BATCH MODE REQUESTED (-b) = NOLIST INPUT FILE COPY MODE (-c) = COPY 2 PARALLEL CPUS REQUESTED START-UP FILE MODE = NOREAD STOP FILE MODE = NOREAD

00000000 VERSION=WINDOWS x64 RELEASE= 14.0BETA UP20110626 CURRENT JOBNAME=file 17:59:36 JUN 28, 2011 CP= 0.499

PARAMETER _DS_PROGRESS = 999.0000000

/INPUT FILE= ds.dat LINE= 0

DO NOT WRITE ELEMENT RESULTS INTO DATABASE

*GET _WALLSTRT FROM ACTI ITEM=TIME WALL VALUE= 17.9936111

TITLE= disk_v14--Modal with Omega (C5) (D5)

SET PARAMETER DIMENSIONS ON _WB_PROJECTSCRATCH_DIR TYPE=STRI DIMENSIONS= 248 1 1

PARAMETER _WB_PROJECTSCRATCH_DIR(1) = D:\afbeley\WB projects\Rotordynamics Projects\Disk for Chap7 in RG\_ProjectScratch\ScrC5CC\

SET PARAMETER DIMENSIONS ON _WB_USERFILES_DIR TYPE=STRI DIMENSIONS= 248 1 1

PARAMETER _WB_USERFILES_DIR(1) = D:\afbeley\WB projects\Rotordynamics Projects\Disk for Chap7 in RG\disk_v14_files\user_files\ --- Data in consistent MKS units.

MKS UNITS SPECIFIED FOR INTERNAL LENGTH (l) = METER (M) MASS (M) = KILOGRAM (KG) TIME (t) = SECOND (SEC) TEMPERATURE (T) = CELSIUS (C) TOFFSET = 273.0 CHARGE (Q) = COULOMB FORCE (f) = NEWTON (N) (KG-M/SEC2) HEAT = JOULE (N-M)

PRESSURE = PASCAL (NEWTON/M**2) ENERGY (W) = JOULE (N-M) POWER (P) = WATT (N-M/SEC) CURRENT (i) = AMPERE (COULOMBS/SEC) CAPACITANCE (C) = FARAD




INDUCTANCE (L) = HENRY MAGNETIC FLUX = WEBER RESISTANCE (R) = OHM ELECTRIC POTENTIAL = VOLT

INPUT UNITS ARE ALSO SET TO MKS 1

***** ANSYS - ENGINEERING ANALYSIS SYSTEM RELEASE 14.0BETA ***** ANSYS Multiphysics 00000000 VERSION=WINDOWS x64 17:59:37 JUN 28, 2011 CP= 0.764

disk_v14--Modal with Omega (C5) (D5)

** WARNING: PRE-RELEASE VERSION OF ANSYS 14.0BETA ANSYS,INC TESTING IS NOT COMPLETE - CHECK RESULTS CAREFULLY **

***** ANSYS ANALYSIS DEFINITION (PREP7) ***** *********** Nodes for the whole assembly *********** *********** Elements for Body 1 "Surface Body" *********** *********** Send User Defined Coordinate System(s) *********** *********** Set Reference Temperature *********** *********** Send Materials *********** *********** Send Sheet Properties *********** *********** Fixed Supports *********** *********** Define Rotational Velocity ***********

***** ROUTINE COMPLETED ***** CP = 0.764

--- Number of total nodes = 912 --- Number of contact elements = 0 --- Number of spring elements = 0 --- Number of solid elements = 836 --- Number of total elements = 836

*GET _WALLBSOL FROM ACTI ITEM=TIME WALL VALUE= 17.9938889

***** ANSYS SOLUTION ROUTINE *****

PERFORM A MODAL ANALYSIS THIS WILL BE A NEW ANALYSIS

USE SYM. BLOCK LANCZOS MODE EXTRACTION METHOD FOR DAMPED SYSTEM EXTRACT 10 MODES COMPUTE COMPLEX MODE SHAPES: Yes NORMALIZE THE MODE SHAPES TO THE MASS MATRIX

CORIOLIS IN STATIONARY REF. FRAME: GYROSCOPIC DAMPING MATRIX ACTIVATED.

ERASE THE CURRENT DATABASE OUTPUT CONTROL TABLE.

WRITE ALL ITEMS TO THE DATABASE WITH A FREQUENCY OF NONE FOR ALL APPLICABLE ENTITIES

WRITE NSOL ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL FOR ALL APPLICABLE ENTITIES

WRITE NLOA ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL FOR ALL APPLICABLE ENTITIES

EXPAND ALL EXTRACTED MODES DO NOT CALCULATE ELEMENT RESULTS

CMOMEGA on component= cm_rotvelcity113



OMEGAX, OMEGAY, OMEGAZ= 0.0000 0.0000 753.98 X1, Y1, Z1= 0.33210E-18 0.24354E-17 0.0000

*GET ANSINTER_ FROM ACTI ITEM=INT VALUE= 0.00000000

*IF ANSINTER_ ( = 0.00000 ) NE 0 ( = 0.00000 ) THEN

*ENDIF

***** ANSYS SOLVE COMMAND *****

*** WARNING *** CP = 0.764 TIME= 17:59:38 Element shape checking is currently inactive. Issue SHPP,ON or SHPP,WARN to reactivate, if desired.

*** WARNING *** CP = 0.764 TIME= 17:59:38 Make sure that the rotating element component 1 (component name CM_ROTVE) is axisymmetric about the axis of spin defined by the CMOMEGA command to correctly account for the gyroscopic effect in the stationary reference frame (CORIOLIS, ON,,, ON).

*** WARNING *** CP = 0.764 TIME= 17:59:38 SHELL181 will generate a gyroscopic damping matrix contribution (stationary frame ON in CORIOLIS command) in a dynamic analysis. The element matrix will be non-symmetric.

*** NOTE *** CP = 0.764 TIME= 17:59:38 The model data was checked and warning messages were found. Please review output or errors file ( D:\afbeley\WB projects\Rotordynamics Projects\Disk for Chap7 in RG\_ProjectScratch\ScrC5CC\file.err ) for these warning messages.

*** SELECTION OF ELEMENT TECHNOLOGIES FOR APPLICABLE ELEMENTS *** --- GIVE SUGGESTIONS AND RESET THE KEY OPTIONS ---

ELEMENT TYPE 1 IS SHELL181. IT IS ASSOCIATED WITH ELASTOPLASTIC MATERIALS ONLY. KEYOPT(8)=2 IS SUGGESTED AND KEYOPT(3)=2 IS SUGGESTED FOR HIGHER ACCURACY OF MEMBRANE STRESSES; OTHERWISE, KEYOPT(3)=0 IS SUGGESTED. KEYOPT(8) HAS BEEN RESET BUT KEYOPT(3) CAN NOT BE RESET HERE. PLEASE RESET IT MANUALLY IF NECESSARY. KEYOPT(1-12)= 0 0 2 0 0 0 0 2 0 0 0 0

ELEMENT TYPE 1 HAS KEYOPT(3)=2. FOR THE SPECIFIED ANALYSIS TYPE, LUMPED MASS MATRIX OPTION (LUMPM, ON) IS SUGGESTED.

1




S O L U T I O N O P T I O N S

PROBLEM DIMENSIONALITY. . . . . . . . . . . . .3-D DEGREES OF FREEDOM. . . . . . UX UY UZ ROTX ROTY ROTZ ANALYSIS TYPE . . . . . . . . . . . . . . . . .MODAL EXTRACTION METHOD. . . . . . . . . . . . . .BLOCK LANCZOS OFFSET TEMPERATURE FROM ABSOLUTE ZERO . . . . . 273.15 NUMBER OF MODES TO EXTRACT. . . . . . . . . . . 10 GLOBALLY ASSEMBLED MATRIX . . . . . . . . . . .UNSYMMETRIC NUMBER OF MODES TO EXPAND . . . . . . . . . . .ALL ELEMENT RESULTS CALCULATION . . . . . . . . . .OFF

L O A D S T E P O P T I O N S




LOAD STEP NUMBER. . . . . . . . . . . . . . . . 1 CORIOLIS EFFECT IN STATIONARY REF. FRAME . . . ON PRINT OUTPUT CONTROLS . . . . . . . . . . . . .NO PRINTOUT DATABASE OUTPUT CONTROLS ITEM FREQUENCY COMPONENT ALL NONE NSOL ALL NLOA ALL

**** CENTER OF MASS, MASS, AND MASS MOMENTS OF INERTIA ****

CALCULATIONS ASSUME ELEMENT MASS AT ELEMENT CENTROID

TOTAL MASS = 0.13946E-01

MOM. OF INERTIA MOM. OF INERTIA CENTER OF MASS ABOUT ORIGIN ABOUT CENTER OF MASS

XC = -0.14425E-17 IXX = 0.8787E-05 IXX = 0.8787E-05 YC = -0.39859E-19 IYY = 0.8787E-05 IYY = 0.8787E-05 ZC = 0.0000 IZZ = 0.1757E-04 IZZ = 0.1757E-04 IXY = -0.2068E-23 IXY = -0.2068E-23 IYZ = 0.000 IYZ = 0.000 IZX = 0.000 IZX = 0.000

*** MASS SUMMARY BY ELEMENT TYPE ***

TYPE MASS 1 0.139458E-01

Range of element maximum matrix coefficients in global coordinates Maximum = 48540958.7 at element 72. Minimum = 28019921.8 at element 476.

*** ELEMENT MATRIX FORMULATION TIMES TYPE NUMBER ENAME TOTAL CP AVE CP

1 836 SHELL181 0.343 0.000411 Time at end of element matrix formulation CP = 1.1544075.

BLOCK LANCZOS CALCULATION OF UP TO 10 EIGENVECTORS. NUMBER OF EQUATIONS = 5016 MAXIMUM WAVEFRONT = 54 MAXIMUM MODES STORED = 10 MINIMUM EIGENVALUE = 0.00000E+00 MAXIMUM EIGENVALUE = 0.10000E+31

Memory allocated for solver = 15.259 MB Memory required for in-core = 9.910 MB Optimal memory required for out-of-core = 6.307 MB Minimum memory required for out-of-core = 4.456 MB

*** NOTE *** CP = 1.232 TIME= 17:59:40 The Block Lanczos solver is currently running in the in-core memory mode. This memory mode uses the most amount of memory in order to avoid using the hard drive as much as possible, which most often results in the fastest solution time. This mode is recommended if enough physical memory is present to accommodate all of the solver data.

LANCZOS CYCLE NUMBER = 1

new shift: 7.5552D+05 modes still needed: 10

FREQUENCIES AT CURRENT LANCZOS CYCLE 1 0.67026351E+03 2 0.67026351E+03 3 0.67361940E+03 4 0.77976094E+03 5 0.77976094E+03 6 0.12006490E+04



7 0.12006490E+04 8 0.19407295E+04 9 0.19407295E+04 10 0.29429750E+04 11 0.29429750E+04 12 0.43994338E+04 13 0.45625299E+04

number of steps : 8 eigenvalues found : 13 total no. eigenvalues: 13

LANCZOS CYCLE NUMBER = 2

new shift: 3.4193D+08 modes still needed: 01




*** UNDAMPED FREQUENCIES FROM BLOCK LANCZOS ITERATION ***

MODE FREQUENCY (HERTZ)

1 670.2635085229 2 670.2635085236 3 673.6194007885 4 779.7609391426 5 779.7609391516 6 1200.649004484 7 1200.649004485 8 1940.729531196 9 1940.729531217 10 2942.975037442

Time at end of state-space matrix formulation CP = 1.57561016.

***** DAMPED FREQUENCIES FROM REDUCED DAMPED EIGENSOLVER *****

MODE COMPLEX FREQUENCY (HERTZ) MODAL DAMPING RATIO

1 0.0000000 561.14834 j 0.0000000 0.0000000 -561.14834 j 0.0000000 2 0.0000000 576.05641 j 0.0000000 0.0000000 -576.05641 j 0.0000000 3 0.0000000 673.61940 j 0.0000000 0.0000000 -673.61940 j 0.0000000 4 0.0000000 800.59610 j 0.0000000 0.0000000 -800.59610 j 0.0000000 5 0.0000000 893.28099 j 0.0000000 0.0000000 -893.28099 j 0.0000000 6 0.0000000 1055.4993 j 0.0000000 0.0000000 -1055.4993 j 0.0000000 7 0.0000000 1518.0098 j 0.0000000 0.0000000 -1518.0098 j 0.0000000 8 0.0000000 1613.7789 j 0.0000000 0.0000000 -1613.7789 j 0.0000000 9 0.0000000 2481.1639 j 0.0000000 0.0000000 -2481.1639 j 0.0000000 10 0.0000000 2942.9750 j 0.0000000 0.0000000 -2942.9750 j 0.0000000

Time at end of eigenproblem resolution CP = 1.57561016.

Time at end of mode shape normalization CP = 1.66921079. 1







***** PARTICIPATION FACTOR CALCULATION ***** X DIRECTION CUMULATIVE RATIO EFF.MASS MODE FREQUENCY PERIOD PARTIC.FACTOR RATIO EFFECTIVE MASS MASS FRACTION TO TOTAL MASS 1 561.148 0.17821E-02 0.23818E-18 0.000017 0.567320E-37 0.273319E-09 0.406802E-35 2 576.056 0.17359E-02 0.56246E-18 0.000039 0.316357E-36 0.179744E-08 0.226847E-34 3 673.619 0.14845E-02 0.20648E-18 0.000014 0.426339E-37 0.200284E-08 0.305710E-35 4 800.596 0.12491E-02 0.11640E-18 0.000008 0.135486E-37 0.206811E-08 0.971517E-36 5 893.281 0.11195E-02 0.84092E-18 0.000058 0.707147E-36 0.547495E-08 0.507066E-34 6 1055.50 0.94742E-03 0.53740E-18 0.000037 0.288799E-36 0.686631E-08 0.207086E-34 7 1518.01 0.65876E-03 0.26518E-16 0.001841 0.703224E-33 0.339481E-05 0.504253E-31 8 1613.78 0.61966E-03 0.10841E-17 0.000075 0.117531E-35 0.340047E-05 0.842768E-34 9 2481.16 0.40304E-03 -0.26366E-16 0.001830 0.695151E-33 0.674952E-05 0.498465E-31 10 2942.98 0.33979E-03 0.14407E-13 1.000000 0.207565E-27 1.00000 0.148837E-25 ----------------------------------------------------------------------------------------------------------------- sum 0.207567E-27 0.148838E-25 -----------------------------------------------------------------------------------------------------------------

***** PARTICIPATION FACTOR CALCULATION ***** Y DIRECTION CUMULATIVE RATIO EFF.MASS MODE FREQUENCY PERIOD PARTIC.FACTOR RATIO EFFECTIVE MASS MASS FRACTION TO TOTAL MASS 1 561.148 0.17821E-02 0.81650E-19 0.000004 0.666679E-38 0.135918E-10 0.478049E-36 2 576.056 0.17359E-02 -0.31956E-18 0.000014 0.102118E-36 0.221783E-09 0.732248E-35 3 673.619 0.14845E-02 0.65938E-19 0.000003 0.434777E-38 0.230647E-09 0.311761E-36 4 800.596 0.12491E-02 0.73206E-19 0.000003 0.535916E-38 0.241572E-09 0.384284E-36 5 893.281 0.11195E-02 -0.14021E-18 0.000006 0.196588E-37 0.281651E-09 0.140965E-35 6 1055.50 0.94742E-03 -0.15389E-18 0.000007 0.236822E-37 0.329933E-09 0.169815E-35 7 1518.01 0.65876E-03 0.20158E-16 0.000910 0.406357E-33 0.828780E-06 0.291382E-31 8 1613.78 0.61966E-03 0.16806E-18 0.000008 0.282444E-37 0.828837E-06 0.202529E-35 9 2481.16 0.40304E-03 -0.19302E-16 0.000872 0.372582E-33 0.158843E-05 0.267164E-31 10 2942.98 0.33979E-03 0.22147E-13 1.000000 0.490502E-27 1.00000 0.351719E-25 ----------------------------------------------------------------------------------------------------------------- sum 0.490503E-27 0.351720E-25 -----------------------------------------------------------------------------------------------------------------

***** PARTICIPATION FACTOR CALCULATION ***** Z DIRECTION CUMULATIVE RATIO EFF.MASS MODE FREQUENCY PERIOD PARTIC.FACTOR RATIO EFFECTIVE MASS MASS FRACTION TO TOTAL MASS 1 561.148 0.17821E-02 -0.82563E-13 0.000000 0.681666E-26 0.667793E-24 0.488795E-24 2 576.056 0.17359E-02 -0.21313E-12 0.000000 0.454251E-25 0.511785E-23 0.325725E-23 3 673.619 0.14845E-02 0.10103 1.000000 0.102078E-01 1.00000 0.731957 4 800.596 0.12491E-02 0.11815E-13 0.000000 0.139588E-27 1.00000 0.100093E-25 5 893.281 0.11195E-02 0.82368E-13 0.000000 0.678443E-26 1.00000 0.486484E-24 6 1055.50 0.94742E-03 0.55819E-13 0.000000 0.311578E-26 1.00000 0.223420E-24 7 1518.01 0.65876E-03 0.53365E-11 0.000000 0.284780E-22 1.00000 0.204204E-20 8 1613.78 0.61966E-03 0.32991E-14 0.000000 0.108842E-28 1.00000 0.780461E-27 9 2481.16 0.40304E-03 0.12473E-13 0.000000 0.155573E-27 1.00000 0.111555E-25 10 2942.98 0.33979E-03 -0.27025E-13 0.000000 0.730367E-27 1.00000 0.523717E-25 ----------------------------------------------------------------------------------------------------------------- sum 0.102078E-01 0.731957 -----------------------------------------------------------------------------------------------------------------1






***** PARTICIPATION FACTOR CALCULATION ***** X DIRECTION CUMULATIVE RATIO EFF.MASS MODE FREQUENCY PERIOD PARTIC.FACTOR RATIO EFFECTIVE MASS MASS FRACTION TO TOTAL MASS IMAGINARY COMPONENT

1 561.148 0.17821E-02 0.11640E-18 0.004389 0.135486E-37 0.967114E-05 0.971517E-36 2 576.056 0.17359E-02 -0.53740E-18 0.020265 0.288799E-36 0.215819E-03 0.207086E-34 3 673.619 0.14845E-02 -0.36210E-27 0.000000 0.131115E-54 0.215819E-03 0.940170E-53 4 800.596 0.12491E-02 0.23818E-18 0.008982 0.567320E-37 0.256314E-03 0.406802E-35 5 893.281 0.11195E-02 -0.10841E-17 0.040882 0.117531E-35 0.109526E-02 0.842768E-34 6 1055.50 0.94742E-03 -0.56246E-18 0.021210 0.316357E-36 0.132108E-02 0.226847E-34 7 1518.01 0.65876E-03 0.26366E-16 0.994244 0.695151E-33 0.497527 0.498465E-31 8 1613.78 0.61966E-03 -0.84092E-18 0.031711 0.707147E-36 0.498032 0.507066E-34 9 2481.16 0.40304E-03 -0.26518E-16 1.000000 0.703224E-33 1.00000 0.504253E-31 10 2942.98 0.33979E-03 0.10575E-28 0.000000 0.111828E-57 1.00000 0.801871E-56 ----------------------------------------------------------------------------------------------------------------- sum 0.140093E-32 0.100455E-30 -----------------------------------------------------------------------------------------------------------------

***** PARTICIPATION FACTOR CALCULATION ***** Y DIRECTION CUMULATIVE RATIO EFF.MASS MODE FREQUENCY PERIOD PARTIC.FACTOR RATIO EFFECTIVE MASS MASS FRACTION TO TOTAL MASS IMAGINARY COMPONENT

1 561.148 0.17821E-02 0.73206E-19 0.003632 0.535917E-38 0.687844E-05 0.384284E-36 2 576.056 0.17359E-02 0.15389E-18 0.007634 0.236822E-37 0.372743E-04 0.169815E-35 3 673.619 0.14845E-02 -0.34820E-27 0.000000 0.121242E-54 0.372743E-04 0.869377E-53 4 800.596 0.12491E-02 0.81650E-19 0.004050 0.666680E-38 0.458311E-04 0.478050E-36 5 893.281 0.11195E-02 -0.16806E-18 0.008337 0.282444E-37 0.820825E-04 0.202529E-35 6 1055.50 0.94742E-03 0.31956E-18 0.015853 0.102118E-36 0.213150E-03 0.732248E-35 7 1518.01 0.65876E-03 0.19302E-16 0.957541 0.372582E-33 0.478419 0.267164E-31 8 1613.78 0.61966E-03 0.14021E-18 0.006955 0.196588E-37 0.478445 0.140965E-35 9 2481.16 0.40304E-03 -0.20158E-16 1.000000 0.406357E-33 1.00000 0.291382E-31 10 2942.98 0.33979E-03 0.65231E-29 0.000000 0.425506E-58 1.00000 0.305113E-56 ----------------------------------------------------------------------------------------------------------------- sum 0.779125E-33 0.558679E-31 -----------------------------------------------------------------------------------------------------------------

***** PARTICIPATION FACTOR CALCULATION ***** Z DIRECTION CUMULATIVE RATIO EFF.MASS MODE FREQUENCY PERIOD PARTIC.FACTOR RATIO EFFECTIVE MASS MASS FRACTION TO TOTAL MASS IMAGINARY COMPONENT

1 561.148 0.17821E-02 -0.16579E-13 0.007000 0.274858E-27 0.481446E-04 0.197090E-25 2 576.056 0.17359E-02 0.30612E-12 0.129253 0.937069E-25 0.164620E-01 0.671934E-23 3 673.619 0.14845E-02 0.87077E-25 0.000000 0.758243E-50 0.164620E-01 0.543705E-48 4 800.596 0.12491E-02 0.60670E-13 0.025617 0.368081E-26 0.171067E-01 0.263936E-24 5 893.281 0.11195E-02 -0.16100E-13 0.006798 0.259196E-27 0.171521E-01 0.185859E-25 6 1055.50 0.94742E-03 -0.39769E-13 0.016792 0.158155E-26 0.174291E-01 0.113406E-24 7 1518.01 0.65876E-03 -0.17396E-13 0.007345 0.302618E-27 0.174822E-01 0.216995E-25 8 1613.78 0.61966E-03 -0.13384E-13 0.005651 0.179128E-27 0.175135E-01 0.128446E-25 9 2481.16 0.40304E-03 -0.23683E-11 1.000000 0.560902E-23 0.999998 0.402200E-21 10 2942.98 0.33979E-03 -0.31135E-14 0.001315 0.969359E-29 1.00000 0.695088E-27 ----------------------------------------------------------------------------------------------------------------- sum 0.570902E-23 0.409371E-21 -----------------------------------------------------------------------------------------------------------------

*** ANSYS BINARY FILE STATISTICS BUFFER SIZE USED= 16384




15.250 MB WRITTEN ON ELEMENT MATRIX FILE: file.emat 3.188 MB WRITTEN ON ASSEMBLED MATRIX FILE: file.full 0.938 MB WRITTEN ON MODAL MATRIX FILE: file.mode 1.500 MB WRITTEN ON RESULTS FILE: file.rst *************** Write FE CONNECTORS *********

WRITE OUT CONSTRAINT EQUATIONS TO FILE= file.ce

FINISH SOLUTION PROCESSING


*GET _WALLASOL FROM ACTI ITEM=TIME WALL VALUE= 17.9944444 1




***** ANSYS RESULTS INTERPRETATION (POST1) *****

*** NOTE *** CP = 1.685 TIME= 17:59:40 Reading results into the database (SET command) will update the current displacement and force boundary conditions in the database with the values from the results file for that load set. Note that any subsequent solutions will use these values unless action is taken to either SAVE the current values or not overwrite them (/EXIT,NOSAVE).

Set Encoding of XML File to:ISO-8859-1

Set Output of XML File to: PARM, , , , , , , , , , , , , , , , , , ,

DATABASE WRITTEN ON FILE parm.xml

EXIT THE ANSYS POST1 DATABASE PROCESSOR


PRINTOUT RESUMED BY /GOP

*GET _WALLDONE FROM ACTI ITEM=TIME WALL VALUE= 17.9944444

PARAMETER _PREPTIME = 1.000000000

PARAMETER _SOLVTIME = 2.000000000

PARAMETER _POSTTIME = 0.000000000

PARAMETER _TOTALTIM = 3.000000000

EXIT ANSYS WITHOUT SAVING DATABASE

NUMBER OF WARNING MESSAGES ENCOUNTERED= 3 NUMBER OF ERROR MESSAGES ENCOUNTERED= 0

+--------------------- A N S Y S S T A T I S T I C S ------------------------+



Release: 14.0BETA Build: UP20110626 Platform: WINDOWS x64 Date Run: 06/28/2011 Time: 17:59Windows Process ID: 5116

Compiler: Intel(R) FORTRAN Compiler Version 11.1.0 (Build: 20100414) Microsoft(R) Visual C/C++ Compiler Version 15.0 (Build: 30729) Intel(R) Math Kernel Library Version 10.3.3 Product Build 20110314

Number of cores: 2 (Shared Memory Parallel)

GPU Acceleration: Not Requested

Job Name: fileWorking Directory: D:\afbeley\WB projects\Rotordynamics Projects\Disk for Chap7 in RG\_ProjectScratch\ScrC5CC

Elapsed time spent pre-processing model (/PREP7) : 0.7 secondsElapsed time spent solution - preprocessing : 0.3 secondsElapsed time spent computing solution : 1.8 secondsElapsed time spent solution - postprocessing : 0.0 secondsElapsed time spent post-processing model (/POST1) : 0.0 seconds

Maximum total memory used : 563.0 MbytesMaximum total memory allocated : 1028.0 Mbytes

+------------------ E N D A N S Y S S T A T I S T I C S -------------------+

*---------------------------------------------------------------------------* | | | ANSYS RUN COMPLETED | | | |---------------------------------------------------------------------------| | | | Release 14.0BETA UP20110626 WINDOWS x64 | | | |---------------------------------------------------------------------------| | | | Database Requested(-db) 512 MB Scratch Memory Requested 512 MB | | Maximum Database Used 1 MB Maximum Scratch Memory Used 48 MB | | | |---------------------------------------------------------------------------| | | | CP Time (sec) = 1.856 Time = 17:59:40 | | Elapsed Time (sec) = 32.000 Date = 06/28/2011 | | | *---------------------------------------------------------------------------*

Modal Analysis Using WorkBench - Input File

/batch/config,noeldb,1 ! force off writing results to database*get,_wallstrt,active,,time,wall! ANSYS input file written by Workbench version 14.0 Internal! File used for geometry attach: D:\afbeley\WB projects\Rotordynamics Projects\Disk for Chap7 in RG\disk_v14_files\dp0\Geom\DM\Geom.agdb/title,disk_v14--Modal with Omega (C5) (D5)*DIM,_wb_ProjectScratch_dir,string,248_wb_ProjectScratch_dir(1) = 'D:\afbeley\WB projects\Rotordynamics Projects\Disk for Chap7 in RG\_ProjectScratch\ScrC5CC\'*DIM,_wb_userfiles_dir,string,248_wb_userfiles_dir(1) = 'D:\afbeley\WB projects\Rotordynamics Projects\Disk for Chap7 in RG\disk_v14_files\user_files\'/com,--- Data in consistent MKS units./units,MKS/nopr/wb,file,start ! signify a WB generated input file/prep7! Turn off shape checking because checks already performed inside WB mesher.! See help system for more information.SHPP,OFF,,NOWARN/nolistetcon,set ! allow ANSYS to choose best KEYOP's for 180x elements/com,*********** Nodes for the whole assembly ***********




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1 1 1 1 0 0 0 0 4 0 592 740 739 749 750 1 1 1 1 0 0 0 0 4 0 593 750 749 759 760 1 1 1 1 0 0 0 0 4 0 594 760 759 769 770 1 1 1 1 0 0 0 0 4 0 595 770 769 779 780 1 1 1 1 0 0 0 0 4 0 596 780 779 789 790 1 1 1 1 0 0 0 0 4 0 597 790 789 799 800 1 1 1 1 0 0 0 0 4 0 598 800 799 809 810 1 1 1 1 0 0 0 0 4 0 599 810 809 819 820 1 1 1 1 0 0 0 0 4 0 600 820 819 829 830 1 1 1 1 0 0 0 0 4 0 601 830 829 839 840 1 1 1 1 0 0 0 0 4 0 602 840 839 849 850 1 1 1 1 0 0 0 0 4 0 603 850 849 859 860 1 1 1 1 0 0 0 0 4 0 604 860 859 869 870 1 1 1 1 0 0 0 0 4 0 605 870 869 879 880 1 1 1 1 0 0 0 0 4 0 606 880 879 889 890 1 1 1 1 0 0 0 0 4 0 607 890 889 899 900 1 1 1 1 0 0 0 0 4 0 608 900 899 909 910 1 1 1 1 0 0 0 0 4 0 609 911 910 160 161 1 1 1 1 0 0 0 0 4 0 610 161 160 170 171 1 1 1 1 0 0 0 0 4 0 611 171 170 180 181 1 1 1 1 0 0 0 0 4 0 612 181 180 190 191 1 1 1 1 0 0 0 0 4 0 613 191 190 200 201 1 1 1 1 0 0 0 0 4 0 614 201 200 210 211 1 1 1 1 0 0 0 0 4 0 615 211 210 220 221 1 1 1 1 0 0 0 0 4 0 616 221 220 230 231 1 1 1 1 0 0 0 0 4 0 617 231 230 240 241 1 1 1 1 0 0 0 0 4 0 618 241 240 250 251 1 1 1 1 0 0 0 0 4 0 619 251 250 260 261 1 1 1 1 0 0 0 0 4 0 620 261 260 270 271 1 1 1 1 0 0 0 0 4 0 621 271 270 280 281 1 1 1 1 0 0 0 0 4 0 622 281 280 290 291 1 1 1 1 0 0 0 0 4 0 623 291 290 300 301 1 1 1 1 0 0 0 0 4 0 624 301 300 310 311 1 1 1 1 0 0 0 0 4 0 625 311 310 320 321 1 1 1 1 0 0 0 0 4 0 626 321 320 330 331 1 1 1 1 0 0 0 0 4 0 627 331 330 340 341 1 1 1 1 0 0 0 0 4 0 628 341 340 350 351 1 1 1 1 0 0 0 0 4 0 629 351 350 360 361 1 1 1 1 0 0 0 0 4 0 630 361 360 370 371 1 1 1 1 0 0 0 0 4 0 631 371 370 380 381 1 1 1 1 0 0 0 0 4 0 632 381 380 390 391 1 1 1 1 0 0 0 0 4 0 633 391 390 400 401 1 1 1 1 0 0 0 0 4 0 634 401 400 410 411 1 1 1 1 0 0 0 0 4 0 635 411 410 420 421 1 1 1 1 0 0 0 0 4 0 636 421 420 430 431 1 1 1 1 0 0 0 0 4 0 637 431 430 440 441 1 1 1 1 0 0 0 0 4 0 638 441 440 450 451 1 1 1 1 0 0 0 0 4 0 639 451 450 460 461 1 1 1 1 0 0 0 0 4 0 640 461 460 470 471 1 1 1 1 0 0 0 0 4 0 641 471 470 480 481 1 1 1 1 0 0 0 0 4 0 642 481 480 490 491 1 1 1 1 0 0 0 0 4 0 643 491 490 500 501 1 1 1 1 0 0 0 0 4 0 644 501 500 510 511 1 1 1 1 0 0 0 0 4 0 645 511 510 520 521 1 1 1 1 0 0 0 0 4 0 646 521 520 530 531 1 1 1 1 0 0 0 0 4 0 647 531 530 540 541 1 1 1 1 0 0 0 0 4 0 648 541 540 550 551 1 1 1 1 0 0 0 0 4 0 649 551 550 560 561 1 1 1 1 0 0 0 0 4 0 650 561 560 570 571 1 1 1 1 0 0 0 0 4 0 651 571 570 580 581 1 1 1 1 0 0 0 0 4 0 652 581 580 590 591 1 1 1 1 0 0 0 0 4 0 653 591 590 600 601 1 1 1 1 0 0 0 0 4 0 654 601 600 610 611 1 1 1 1 0 0 0 0 4 0 655 611 610 620 621 1 1 1 1 0 0 0 0 4 0 656 621 620 630 631 1 1 1 1 0 0 0 0 4 0 657 631 630 640 641 1 1 1 1 0 0 0 0 4 0 658 641 640 650 651 1 1 1 1 0 0 0 0 4 0 659 651 650 660 661 1 1 1 1 0 0 0 0 4 0 660 661 660 670 671 1 1 1 1 0 0 0 0 4 0 661 671 670 680 681 1 1 1 1 0 0 0 0 4 0 662 681 680 690 691 1 1 1 1 0 0 0 0 4 0 663 691 690 700 701




1 1 1 1 0 0 0 0 4 0 664 701 700 710 711 1 1 1 1 0 0 0 0 4 0 665 711 710 720 721 1 1 1 1 0 0 0 0 4 0 666 721 720 730 731 1 1 1 1 0 0 0 0 4 0 667 731 730 740 741 1 1 1 1 0 0 0 0 4 0 668 741 740 750 751 1 1 1 1 0 0 0 0 4 0 669 751 750 760 761 1 1 1 1 0 0 0 0 4 0 670 761 760 770 771 1 1 1 1 0 0 0 0 4 0 671 771 770 780 781 1 1 1 1 0 0 0 0 4 0 672 781 780 790 791 1 1 1 1 0 0 0 0 4 0 673 791 790 800 801 1 1 1 1 0 0 0 0 4 0 674 801 800 810 811 1 1 1 1 0 0 0 0 4 0 675 811 810 820 821 1 1 1 1 0 0 0 0 4 0 676 821 820 830 831 1 1 1 1 0 0 0 0 4 0 677 831 830 840 841 1 1 1 1 0 0 0 0 4 0 678 841 840 850 851 1 1 1 1 0 0 0 0 4 0 679 851 850 860 861 1 1 1 1 0 0 0 0 4 0 680 861 860 870 871 1 1 1 1 0 0 0 0 4 0 681 871 870 880 881 1 1 1 1 0 0 0 0 4 0 682 881 880 890 891 1 1 1 1 0 0 0 0 4 0 683 891 890 900 901 1 1 1 1 0 0 0 0 4 0 684 901 900 910 911 1 1 1 1 0 0 0 0 4 0 685 912 911 161 162 1 1 1 1 0 0 0 0 4 0 686 162 161 171 172 1 1 1 1 0 0 0 0 4 0 687 172 171 181 182 1 1 1 1 0 0 0 0 4 0 688 182 181 191 192 1 1 1 1 0 0 0 0 4 0 689 192 191 201 202 1 1 1 1 0 0 0 0 4 0 690 202 201 211 212 1 1 1 1 0 0 0 0 4 0 691 212 211 221 222 1 1 1 1 0 0 0 0 4 0 692 222 221 231 232 1 1 1 1 0 0 0 0 4 0 693 232 231 241 242 1 1 1 1 0 0 0 0 4 0 694 242 241 251 252 1 1 1 1 0 0 0 0 4 0 695 252 251 261 262 1 1 1 1 0 0 0 0 4 0 696 262 261 271 272 1 1 1 1 0 0 0 0 4 0 697 272 271 281 282 1 1 1 1 0 0 0 0 4 0 698 282 281 291 292 1 1 1 1 0 0 0 0 4 0 699 292 291 301 302 1 1 1 1 0 0 0 0 4 0 700 302 301 311 312 1 1 1 1 0 0 0 0 4 0 701 312 311 321 322 1 1 1 1 0 0 0 0 4 0 702 322 321 331 332 1 1 1 1 0 0 0 0 4 0 703 332 331 341 342 1 1 1 1 0 0 0 0 4 0 704 342 341 351 352 1 1 1 1 0 0 0 0 4 0 705 352 351 361 362 1 1 1 1 0 0 0 0 4 0 706 362 361 371 372 1 1 1 1 0 0 0 0 4 0 707 372 371 381 382 1 1 1 1 0 0 0 0 4 0 708 382 381 391 392 1 1 1 1 0 0 0 0 4 0 709 392 391 401 402 1 1 1 1 0 0 0 0 4 0 710 402 401 411 412 1 1 1 1 0 0 0 0 4 0 711 412 411 421 422 1 1 1 1 0 0 0 0 4 0 712 422 421 431 432 1 1 1 1 0 0 0 0 4 0 713 432 431 441 442 1 1 1 1 0 0 0 0 4 0 714 442 441 451 452 1 1 1 1 0 0 0 0 4 0 715 452 451 461 462 1 1 1 1 0 0 0 0 4 0 716 462 461 471 472 1 1 1 1 0 0 0 0 4 0 717 472 471 481 482 1 1 1 1 0 0 0 0 4 0 718 482 481 491 492 1 1 1 1 0 0 0 0 4 0 719 492 491 501 502 1 1 1 1 0 0 0 0 4 0 720 502 501 511 512 1 1 1 1 0 0 0 0 4 0 721 512 511 521 522 1 1 1 1 0 0 0 0 4 0 722 522 521 531 532 1 1 1 1 0 0 0 0 4 0 723 532 531 541 542 1 1 1 1 0 0 0 0 4 0 724 542 541 551 552 1 1 1 1 0 0 0 0 4 0 725 552 551 561 562 1 1 1 1 0 0 0 0 4 0 726 562 561 571 572 1 1 1 1 0 0 0 0 4 0 727 572 571 581 582 1 1 1 1 0 0 0 0 4 0 728 582 581 591 592 1 1 1 1 0 0 0 0 4 0 729 592 591 601 602 1 1 1 1 0 0 0 0 4 0 730 602 601 611 612 1 1 1 1 0 0 0 0 4 0 731 612 611 621 622 1 1 1 1 0 0 0 0 4 0 732 622 621 631 632 1 1 1 1 0 0 0 0 4 0 733 632 631 641 642 1 1 1 1 0 0 0 0 4 0 734 642 641 651 652 1 1 1 1 0 0 0 0 4 0 735 652 651 661 662



1 1 1 1 0 0 0 0 4 0 736 662 661 671 672 1 1 1 1 0 0 0 0 4 0 737 672 671 681 682 1 1 1 1 0 0 0 0 4 0 738 682 681 691 692 1 1 1 1 0 0 0 0 4 0 739 692 691 701 702 1 1 1 1 0 0 0 0 4 0 740 702 701 711 712 1 1 1 1 0 0 0 0 4 0 741 712 711 721 722 1 1 1 1 0 0 0 0 4 0 742 722 721 731 732 1 1 1 1 0 0 0 0 4 0 743 732 731 741 742 1 1 1 1 0 0 0 0 4 0 744 742 741 751 752 1 1 1 1 0 0 0 0 4 0 745 752 751 761 762 1 1 1 1 0 0 0 0 4 0 746 762 761 771 772 1 1 1 1 0 0 0 0 4 0 747 772 771 781 782 1 1 1 1 0 0 0 0 4 0 748 782 781 791 792 1 1 1 1 0 0 0 0 4 0 749 792 791 801 802 1 1 1 1 0 0 0 0 4 0 750 802 801 811 812 1 1 1 1 0 0 0 0 4 0 751 812 811 821 822 1 1 1 1 0 0 0 0 4 0 752 822 821 831 832 1 1 1 1 0 0 0 0 4 0 753 832 831 841 842 1 1 1 1 0 0 0 0 4 0 754 842 841 851 852 1 1 1 1 0 0 0 0 4 0 755 852 851 861 862 1 1 1 1 0 0 0 0 4 0 756 862 861 871 872 1 1 1 1 0 0 0 0 4 0 757 872 871 881 882 1 1 1 1 0 0 0 0 4 0 758 882 881 891 892 1 1 1 1 0 0 0 0 4 0 759 892 891 901 902 1 1 1 1 0 0 0 0 4 0 760 902 901 911 912 1 1 1 1 0 0 0 0 4 0 761 77 912 162 152 1 1 1 1 0 0 0 0 4 0 762 152 162 172 151 1 1 1 1 0 0 0 0 4 0 763 151 172 182 150 1 1 1 1 0 0 0 0 4 0 764 150 182 192 149 1 1 1 1 0 0 0 0 4 0 765 149 192 202 148 1 1 1 1 0 0 0 0 4 0 766 148 202 212 147 1 1 1 1 0 0 0 0 4 0 767 147 212 222 146 1 1 1 1 0 0 0 0 4 0 768 146 222 232 145 1 1 1 1 0 0 0 0 4 0 769 145 232 242 144 1 1 1 1 0 0 0 0 4 0 770 144 242 252 143 1 1 1 1 0 0 0 0 4 0 771 143 252 262 142 1 1 1 1 0 0 0 0 4 0 772 142 262 272 141 1 1 1 1 0 0 0 0 4 0 773 141 272 282 140 1 1 1 1 0 0 0 0 4 0 774 140 282 292 139 1 1 1 1 0 0 0 0 4 0 775 139 292 302 138 1 1 1 1 0 0 0 0 4 0 776 138 302 312 137 1 1 1 1 0 0 0 0 4 0 777 137 312 322 136 1 1 1 1 0 0 0 0 4 0 778 136 322 332 135 1 1 1 1 0 0 0 0 4 0 779 135 332 342 134 1 1 1 1 0 0 0 0 4 0 780 134 342 352 133 1 1 1 1 0 0 0 0 4 0 781 133 352 362 132 1 1 1 1 0 0 0 0 4 0 782 132 362 372 131 1 1 1 1 0 0 0 0 4 0 783 131 372 382 130 1 1 1 1 0 0 0 0 4 0 784 130 382 392 129 1 1 1 1 0 0 0 0 4 0 785 129 392 402 128 1 1 1 1 0 0 0 0 4 0 786 128 402 412 127 1 1 1 1 0 0 0 0 4 0 787 127 412 422 126 1 1 1 1 0 0 0 0 4 0 788 126 422 432 125 1 1 1 1 0 0 0 0 4 0 789 125 432 442 124 1 1 1 1 0 0 0 0 4 0 790 124 442 452 123 1 1 1 1 0 0 0 0 4 0 791 123 452 462 122 1 1 1 1 0 0 0 0 4 0 792 122 462 472 121 1 1 1 1 0 0 0 0 4 0 793 121 472 482 120 1 1 1 1 0 0 0 0 4 0 794 120 482 492 119 1 1 1 1 0 0 0 0 4 0 795 119 492 502 118 1 1 1 1 0 0 0 0 4 0 796 118 502 512 117 1 1 1 1 0 0 0 0 4 0 797 117 512 522 116 1 1 1 1 0 0 0 0 4 0 798 116 522 532 115 1 1 1 1 0 0 0 0 4 0 799 115 532 542 114 1 1 1 1 0 0 0 0 4 0 800 114 542 552 113 1 1 1 1 0 0 0 0 4 0 801 113 552 562 112 1 1 1 1 0 0 0 0 4 0 802 112 562 572 111 1 1 1 1 0 0 0 0 4 0 803 111 572 582 110 1 1 1 1 0 0 0 0 4 0 804 110 582 592 109 1 1 1 1 0 0 0 0 4 0 805 109 592 602 108 1 1 1 1 0 0 0 0 4 0 806 108 602 612 107 1 1 1 1 0 0 0 0 4 0 807 107 612 622 106




1 1 1 1 0 0 0 0 4 0 808 106 622 632 105 1 1 1 1 0 0 0 0 4 0 809 105 632 642 104 1 1 1 1 0 0 0 0 4 0 810 104 642 652 103 1 1 1 1 0 0 0 0 4 0 811 103 652 662 102 1 1 1 1 0 0 0 0 4 0 812 102 662 672 101 1 1 1 1 0 0 0 0 4 0 813 101 672 682 100 1 1 1 1 0 0 0 0 4 0 814 100 682 692 99 1 1 1 1 0 0 0 0 4 0 815 99 692 702 98 1 1 1 1 0 0 0 0 4 0 816 98 702 712 97 1 1 1 1 0 0 0 0 4 0 817 97 712 722 96 1 1 1 1 0 0 0 0 4 0 818 96 722 732 95 1 1 1 1 0 0 0 0 4 0 819 95 732 742 94 1 1 1 1 0 0 0 0 4 0 820 94 742 752 93 1 1 1 1 0 0 0 0 4 0 821 93 752 762 92 1 1 1 1 0 0 0 0 4 0 822 92 762 772 91 1 1 1 1 0 0 0 0 4 0 823 91 772 782 90 1 1 1 1 0 0 0 0 4 0 824 90 782 792 89 1 1 1 1 0 0 0 0 4 0 825 89 792 802 88 1 1 1 1 0 0 0 0 4 0 826 88 802 812 87 1 1 1 1 0 0 0 0 4 0 827 87 812 822 86 1 1 1 1 0 0 0 0 4 0 828 86 822 832 85 1 1 1 1 0 0 0 0 4 0 829 85 832 842 84 1 1 1 1 0 0 0 0 4 0 830 84 842 852 83 1 1 1 1 0 0 0 0 4 0 831 83 852 862 82 1 1 1 1 0 0 0 0 4 0 832 82 862 872 81 1 1 1 1 0 0 0 0 4 0 833 81 872 882 80 1 1 1 1 0 0 0 0 4 0 834 80 882 892 79 1 1 1 1 0 0 0 0 4 0 835 79 892 902 78 1 1 1 1 0 0 0 0 4 0 836 78 902 912 77-1/wb,elem,end ! done creating elements/com,*********** Send User Defined Coordinate System(s) ***********csys,0toffst,273.15, ! Temperature offset from absolute zero/com,*********** Set Reference Temperature ***********tref,22./wb,mat,start ! starting to send materials/com,*********** Send Materials ***********MP,DENS,1,2800, ! kg m^-3MP,ALPX,1,2.3e-05, ! C^-1MP,C,1,875, ! J kg^-1 C^-1MPTEMP,,,,,,,,MPTEMP,1,-100MPTEMP,2,0MPTEMP,3,100MPTEMP,4,200MPDATA,KXX,1, ,114,144,165,175, ! W m^-1 C^-1MPTEMP,,,,,,,,MPTEMP,,,,,,,,MPTEMP,1,0MPTEMP,2,20MPTEMP,3,100MPDATA,RSVX,1, ,2.43e-08,2.67e-08,3.63e-08, ! kg m^3 A^-2 s^-3MPTEMP,,,,,,,,MP,EX,1,72000000000, ! PaMP,NUXY,1,0.33,MP,MURX,1,1,

/wb,mat,end ! done sending materials/com,*********** Send Sheet Properties ***********sectype,1,shellsecdata,8.e-004secoff,mid!************************* Model Summary ********************!Surface Body, Aluminum Alloy, matid, 1!************************* End Model Summary ********************! get the diagonal of the bounding box. Needed later for other things*get,_xmin,node,,mnloc,x*get,_ymin,node,,mnloc,y*get,_zmin,node,,mnloc,z*get,_xmax,node,,mxloc,x*get,_ymax,node,,mxloc,y



*get,_zmax,node,,mxloc,z_ASMDIAG=(_xmax-_xmin)*(_xmax-_xmin)+(_ymax-_ymin)*(_ymax-_ymin)+(_zmax-_zmin)*(_zmax-_zmin)_ASMDIAG=SQRT(_ASMDIAG)/wb,contact,start ! starting to send contact/wb,contact,end ! done creating contacts/golist/wb,load,start ! starting to send loads/com,*********** Fixed Supports ***********CMBLOCK,_FIXEDSU,NODE, 76(8i10) 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 61 62 63 64 65 66 67 68 69 70 71 72 73 74 75 76cmsel,s,_FIXEDSUd,all,allnsel,allnsel,all/com,*********** Define Rotational Velocity ***********esel,allcm,cm_rotvelcity113,elem/gst,on,onfini*get,_numnode,node,0,count*get,_numelem,elem,0,count/go/wb,load,end ! done creating loads/com,--- Number of total nodes = %_numnode%/com,--- Number of contact elements = 0/com,--- Number of spring elements = 0/com,--- Number of solid elements = 836/com,--- Number of total elements = %_numelem%*get,_wallbsol,active,,time,wall/soluantype,2 ! modal analysismodopt,qrdamp,10,,,on ! calculate complex eigen solutioncoriolis,yes,,,yes,nooutres,eraseoutres,all,noneoutres,nsol,alloutres,nload,allmxpand ! default expand in case of complex solutioncmom,cm_rotvelcity113,0.,0.,753.9822,3.32095941451108e-019,2.43537023730813e-018,0.! *********** WB SOLVE COMMAND ***********! check interactive state*get,ANSINTER_,active,,int*if,ANSINTER_,ne,0,then/eof*endifsolve/com *************** Write FE CONNECTORS ********* CEWRITE,file,ce,,INTEfini*get,_wallasol,active,,time,wall/post1xmlo,ENCODING,ISO-8859-1xmlo,parm/xml,parm,xmlfini/gopr*get,_walldone,active,,time,wall_preptime=(_wallbsol-_wallstrt)*3600_solvtime=(_wallasol-_wallbsol)*3600_posttime=(_walldone-_wallasol)*3600_totaltim=(_walldone-_wallstrt)*3600/wb,file,end ! done with WB generated input


