Chapter 9 2D 實體結構分析 Analysis of 2D Structural Solids.
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Transcript of Chapter 9 2D 實體結構分析 Analysis of 2D Structural Solids.
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Contents9.1 何謂 2D結構 ?
When is a Structure Modeled as 2D?
9.2 PLANE42: 2D實體結構元素PLANE42: 2D Structural Solid Element
9.3 實例 : 平面應力問題Example: Plane Stress Case
9.4 實例 : 平面應變問題Example: Plane Strain Case
9.5 實例 : 軸對稱問題Example: Axisymmetric Case
9.6 2D實體元素瀏覽Overview of 2D Solid Elements
9.7 練習題 : 懸臂樑的 2D分析2D Analysis of a Cantilevel Beam
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9.1.1 平面應力問題0 zyyzzxxzz
EE
G
EE
EE
yxz
zyyzzxxz
xyxy
yxy
yxx
0Fixed pin hole, 0.8 in diameter
Tapered pressure load: 50 to 500 psi approximates a 130 lb pin load force
6 in
2 in
4 in
2 in
0.4 in radius
Thickness = 1/2 in
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9.2.2 PLANE42輸入資料Element Name PLANE42
Nodes I, J, K, L
Degrees of Freedom UX, UY
Real Constant None, if KEYOPT (3) = 0, 1, 2Thickness, if KEYOPT (3) = 3
Material Properties EX, NUXY, GXY, ALPX, DENS, DAMP, etc.
Surface Loads Pressure: face 1 (JI), face 2 (KJ), face 3 (LK), face 4 (IL)
Body Loads Temperature -- T(I), T(J), T(K), T(L)
Special Features Plasticity, Creep, Stress stiffening,Large deflection, Large strain, etc.
KEYOPT(1) Key for element coordinate system:0 -- Element C.S. is parallel to the global C.S.1 -- Element C.S. is based on the element I-J side
KEYOPT(2) Key to include extra shapes:0 -- Include extra displacement shapes1 -- Suppress extra displacement shapes
KEYOPT(3) 0 -- Plane stress1 -- Axisymmetric2 -- Plane strain3 -- Plane stress with thickness input
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9.3.1 問題描述
Fixed pin hole, 0.8 in diameter
Tapered pressure load: 50 to 500 psi approximates a 130 lb pin load force
6 in
2 in
4 in
2 in
0.4 in radius
Thickness = 1/2 in
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9.3.2 ANSYS Procedure (1/5)01
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FINISH
/CLEAR
/TITLE, Corner Bracket (in-lbf-s)
/PREP7
ET, 1, PLANE82,,, 3
R, 1, 0.5
MP, EX, 1, 30E6
MP, NUXY, 1, 0.27
RECTNG, 0, 6, -1, 1
RECTNG, 4, 6, -3, -1
PCIRC, 1
WPOFFS, 5, -3
PCIRC, 1
AADD, ALL
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9.3.2 ANSYS Procedure (2/5)18
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WPOFFS, -5, 3
PCIRC, 0.4
WPOFFS, 5, -3
PCIRC, 0.4
ASBA, 5, ALL
LFILLT, 8, 17, 0.4
AL, 12, 13, 14
AADD, ALL
APLOT
/PNUM, LINE, ON
/PNUM, KP, ON
LPLOT
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9.3.2 ANSYS Procedure (4/5)36
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/SOLU
DK, 7, ALL, 0,, 1
DK, 9, ALL, 0,, 1
DK, 10, ALL, 0,, 1
DK, 12, ALL, 0,, 1
SFL, 10, PRES, 50, 500
SFL, 11, PRES, 500, 50
/PBC, U,, ON
/PSF, PRES, NORM, 2
APLOT
SOLVE
FINISH
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9.4.2 ANSYS Procedure (1/6)01
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FINISH
/CLEAR
/TITLE, STRESSES IN A LONG CYLINDER
/UNITS, BIN
/PREP7
ET, 1, PLANE42,,, 2
MP, EX, 1, 30E6
MP, DENS, 1, .00073
MP, NUXY, 1, 0.3
CSYS, 1
K, 1, 4, 0
K, 2, 8, 0
K, 3, 4, 45
K, 4, 8, 45
A, 3, 1, 2, 4
ESIZE, .25
MSHKEY, 1
MSHAPE, 0, 2D
AMESH, 1
NROTAT, ALL
FINISH
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9.4.2 ANSYS Procedure (2/6)27
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/SOLU
NSEL, S, LOC, Y, 0
NSEL, A, LOC, Y, 45
D, ALL, UY, 0
NSEL, S, LOC, X, 4
SF, ALL, PRES, 30000
ALLSEL
/PBC, U,, ON
/PSF, PRES, NORM, 2
EPLOT
SOLVE
NSEL, S, LOC, X, 4
SF, ALL, PRES, 0
ALLSEL
OMEGA,,, 1000
SOLVE
FINISH
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9.4.2 ANSYS Procedure (3/6)50
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/POST1
SET, 1
PLDISP, 2
RSYS, 1
PLNSOL, S, X
PLNSOL, S, Y
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9.4.2 ANSYS Procedure (4/6)
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PATH, R-DIR, 2
PPATH, 1,, 4, 0
PPATH, 2,, 8, 0
PDEF, R-STRESS, S, X
PDEF, H-STRESS, S, Y
/GRID, 1
/AXLAB, Y, STRESS
/TITLE, STRESS UNDER PRESSURE
PLPATH, R-STRESS, H-STRESS
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9.4.2 ANSYS Procedure (6/6)73
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PDEF, R-STRESS, S, X
PDEF, H-STRESS, S, Y
/TITLE, STRESS UNDER ROTATION
PLPATH, R-STRESS, H-STRESS
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9.5.2 ANSYS Procedure (1/6)01
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FINISH
/CLEAR
/TITLE, STRESSES IN A LONG CYLINDER
/UNITS, BIN
/PREP7
ET, 1, PLANE42,,, 1
MP, EX, 1, 30E6
MP, DENS, 1, .00073
MP, NUXY, 1, 0.3
K, 1, 4, 0
K, 2, 8, 0
K, 3, 4, 1
K, 4, 8, 1
A, 3, 1, 2, 4
ESIZE, .25 MSHK, 1
MSHA, 0, 2D
AMESH, 1
FINISH
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9.5.2 ANSYS Procedure (2/6)25
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/SOLU
NSEL, S, LOC, Y, 0
NSEL, A, LOC, Y, 1
D, ALL, UY, 0
NSEL, S, LOC, X, 4
SF, ALL, PRES, 30000
ALLSEL
/PBC, U,, ON
/PSF, PRES, NORM, 2
EPLOT
SOLVE
NSEL, S, LOC, X, 4
SF, ALL, PRES, 0
ALLSEL
OMEGA,, 1000
SOLVE
FINISH
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9.5.2 ANSYS Procedure (3/6)48
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/POST1
SET, 1
PLDISP, 2
PLNSOL, S, X
PLNSOL, S, Z
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9.5.2 ANSYS Procedure (4/6)
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PATH, R-DIR, 2
PPATH, 1,, 4, 0
PPATH, 2,, 8, 0
PDEF, R-STRESS, S, X
PDEF, H-STRESS, S, Z
/GRID, 1
/AXLAB, Y, STRESS
/TITLE, STRESS UNDER PRESSURE
PLPATH, R-STRESS, H-STRESS
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9.5.2 ANSYS Procedure (6/6)70
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PDEF, R-STRESS, S, X
PDEF, H-STRESS, S, Z
/TITLE, STRESS UNDER ROTATION
PLPATH, R-STRESS, H-STRESS