Curvas Kt Kq de B Series Wageningen

115
K.r, and Efficiency Curves for the Wageningen B-Series Propellers by 0'1 " . D. Ray P. Kinley Department of Naval Architecture and Marine Engineering College of Engineering The University of Michigan Ann Arbor, Michigan 48109

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Transcript of Curvas Kt Kq de B Series Wageningen

  • K.r, ~ and Efficiency Curves for

    the Wageningen B-Series Propellers

    by 0'1 ~. " . M.M."Bern~tsas

    D. Ray

    P. Kinley

    Department of Naval Architecture and Marine Engineering College of Engineering

    The University of Michigan Ann Arbor, Michigan 48109

  • j j j j j j j j j j j j j j j j j j j j

    J

    j j j j j j j j j j

    j j j j j

    j j j

    j

    j j j j

  • ABSTRACT

    The B-series propellers were designed and tested at the Netherlands Ship Model Basin in Wageningen. The open-water characteristics of 120 propeller models of the B-series were tested at N.S.M.B. and analyzed with multiple polynomial regression analysis [1]. The derived polynomials express the thrust and torque coefficients in terms of the number of blades, the blade area ratio, the pitch-diameter ratio and the advance coefficient. The Rey-nolds number effect and the effect of variation of blade thickness on the B-series propeller characteristics have also been evaluated at N.S.M.B. In this report the polynomials derived in [1] are used to plot the open water propel-ler characteristics for Reynolds number 2.0x10 6 and for the ranges of number of blades, blade area ratio and pitch-diameter ratio recommended by N.S.M.B. The extent of applicability of the regression polynomials is also discussed.

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  • ACKNOWLEDGEMENTS

    This report was prepared in fulfillment of the requirements for the de-sign project in the graduate computer-aided design course, NA 574, of the Dp.-partment of Naval Architecture and Marine Engineering of the University of Michigan. Computer funds were provided by the department. Thanks are due to Professor R.F. Beck for his constructive comments and Mrs. Paula Bousley for the excellent typing and editing of this report.

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  • TABLE OF CONTENTS

    ABSTRACT .......................................................... ..

    ACKN'OWLEDGEMENTS

    LIST OF FIGURES

    NOMENCLATURE

    INTRODUCTION

    ~, ~ POLYNOMIALS AND REYNOLDS NUMBER CORRECTIONS LIMITATIONS OF APPLICABILITY OF THE REGRESSION POLYNOMIALS REFERENCES . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FIGU'RES ............................................................. .

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    Page

    iii

    v

    ix xii

    3

    6

    6

    7

  • LIST OF FIGURES

    Figure No. Page

    1. Propeller with 2 blades and AE/Ao = 0.30..................... 7 2. Propeller with 2 blades and AE/Ao = 0.35..................... 8 3. Propeller with 2 blades and AEiAo = 0.40..................... 9 4. Propeller with 2 blades and AE/Ao = 0.45..................... 10 S. Propeller with 2 blades and AE/Ao = 0.50..................... 11 6. Propeller with 2 blades and AE/Ao = 0.55..................... 12 7. Propeller with 2 blades and AE/Ao = 0.60 ' 13 8. Propeller with 2 blades and AE/Ao = 0.65..................... 14 9. Propeller with 2 blades and AEiAo = 0.70..................... 15

    10. 11. 12.

    13. 14. 15. 16.

    17.

    18.

    19. 20.

    21.

    22. 23.

    24. 25.

    26. 27.

    28. 29. 30. 31. 32.

    Propeller with 2 blades and AE/Ao = 0.75 Propeller with 2 blades and AE/Ao = 0.80 Propeller with 2 blades and AE/Ao = 0.85

    " Propeller with 2 blades and AE/Ao = 0.90 Propeller with 2 blades and AE/Ao = 0.95 Propeller with 2 blades and AE/Ao = 1.00 Propeller with 2 blades and AE/Ao = 1.05

    Propeller with 3 blades and AE/Ao = 0.30 Propeller with 3 blades and AEiAo = 0.35 Propeller with 3 blades and AE/Ao = 0.40 Propeller with 3 blades and AE/Ao = 0.45 Propeller with 3 blades and AE/Ao = 0.50 Propeller with 3 blades and AE/Ao = 0.55 Propeller with 3 blades and AE/Ao = 0.60 Propeller with 3 blades and AE/Ao = 0.65 Propeller with 3 blades and AE/Ao = 0.70 Propeller with 3 blades and AE/Ao = 0.75 Propeller with 3 blades and AE/Ao = 0.80 Propeller with 3 blades and AE/Ao = 0.85 Propeller with 3 blades and AE/Ao = 0.90 Propeller with 3 blades and AE/Ao = 0.95 Propeller with 3 blades and AE/Ao = 1.00 Propeller with 3 blades and AE/Ao = 1.05

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    16 17

    18

    19 20 21

    22

    23 24

    25 26 27

    28 29

    30

    31 32 33 34

    35 36

    37 38

  • Figure No.

    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.

    Propeller with 4 blades and AE/Ao = 0.30 Propeller with 4 blades and AE/Ao = 0.35 Propeller with 4 blades and AE/Ao = 0.40 Propeller with 4 blades and AE/Ao = 0.45 Propeller with 4 blades and AEiAo = 0.50 propeller with 4 blades and AE/Ao = 0.55 Propeller with 4 blades and AE/Ao = 0.60 Propeller with 4 blades and AE/Ao = 0.65 Propeller with 4 blades and AE/Ao = 0.70 Propeller with 4 blades and AE/Ao = 0.75 Propeller with 4 blades and AE/Ao = 0.80 Propeller with 4 blades and AE/Ao 0.85 Propeller with 4 blades and AE/Ao = 0.90 Propeller with 4 blades and AE/Ao = 0.95 Propeller with 4 blades and AE/Ao = 1.00 Propeller with 4 blades and AE/Ao = 1.05

    Propeller with 5 blades and AE/Ao = 0.30 Propeller with 5 blades and AE/Ao = 0.35 Propeller with 5 blades and AE/Ao = 0.40 Propeller with 5 blades and AE/Ao = 0.45 Propeller with 5 blades and AE/Ao = 0.50 Propeller with 5 blades and AE/Ao = 0.55 Propeller with 5 blades and AE/Ao = 0.60 Propeller with 5 blades and AE/Ao = 0.65 Propeller with 5 blades and AE/Ao = 0.70 Propeller with 5 blades and AEiAo = 0.75 Propeller with 5 blades and AE/Ao = 0.80 Propeller with 5 blades and AE/Ao = 0.85 Propeller with 5 blades and AE/Ao = 0.90 Propeller with 5 blades and AE/Ao = 0.95

    Propeller with 5 blades and AE/Ao = 1.00 Propeller with 5 blades and AE/Ao = 1.05 .

    Propeller with 6 blades and AE/Ao = 0.30 Propeller with 6 blades and AE/Ao = 0.35

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    Page

    39

    40 41

    42

    43 44

    45 46

    47

    48

    49

    SO 51

    52

    53 54

    55 56 57 58 59 60 61 62

    63 64

    65 66

    67 68

    69

    70

    71

    72

  • Figure No.

    67. 68. 69. 70. 71.

    72.

    73. 74. 75. 76. 77.

    78.

    79. 80.

    Propeller with 6 blades and AE/Ao = 0.40 Propeller with 6 blades and AE/Ao = 0.45 Propeller with 6 blades and AE/Ao = 0.50 Propeller with 6 blades and AE/Ao = 0.55 Propeller with 6 blades and AElAo = 0.60 Propeller with 6 blades and AE/Ao = 0.65 Propeller with 6 blades and AE/Ao = 0.70 Propeller with 6 blades and AE/Ao = 0.75 Propeller with 6 blades and AE/Ao = 0.80 Propeller with 6 blades and AE/Ao = 0.85 Propeller with 6 blades and AE/Ao = 0.90 Propeller with 6 blades and AE/Ao = 0.95 Propeller with 6 blades and AE/Ao = 1.00 Propeller with 6 blades and AE/Ao = 1.05

    Page

    73 74

    75 76 77

    78

    79 80 81

    82

    83

    84 85

    86

    81. Propeller with 7 blades and AE/Ao = 0.30..................... g7 82. Propeller with 7 blades and AE/Aa = 0.35..................... 88 83.

    84.

    85. 86.

    Propeller with 7 blades and AE/Ao = 0.40 Propeller with 7 blades and AE/Ao = 0.45 Propeller with 7 blades and AE/Ao = 0.50 Propeller with 7 blades and AE/Ao = 0.55

    89

    90 91 92

    87. Propeller with 7 blades and AE/Ao = 0.60..................... 93 88. Propeller with 7 blades and AE/Ao = 0.65..................... 94 89. Propeller with 7 blades and AE/Ao = 0.70..................... 95 90. Propeller with 7 blades and AE/Ao = 0.75..................... 96 91. Propeller with 7 blades and AE/Ao = 0.80..................... 97 92. Propeller with 7 blades and AElAo = 0.85..................... 98 93. Propeller with 7 blades and AElAo = 0.90..................... 99 94. Propeller with 7 blades and AE/Ao = 0.95..................... 100 95. Propeller with 7 blades and AE/Ao = 1.00..................... 101 96. Propeller with 7 blades and AE/Ao = 1.05..................... 102

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  • D

    J

    n

    P/D Q Re

    Greek Symbols

    n

    p

    NOMENCLATURE

    blade area ratio coefficient in the ~ polynomial expression coefficient in the KT polynomial expression propeller diameter advance coefficient torque coefficient

    thrust coefficient propeller revolutions per second pitch-diameter ratio propeller torque Reynolds number propeller thrust thickness to cord ratio for propeller blades speed of advance number of blades

    open-water propeller efficiency fluid density

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  • INTRODUCTION

    The open-water propeller characteristics conventionally are presented in the form of the thrust and torque coefficients KT and KQ in terms of the advance coefficient J where

    T Krr = pn2D4 (1)

    KQ = _Q-pn2D5 (2 )

    J VA

    = nD (3 )

    where

    T is the propeller thrust, Q is the propeller torque, p is the fluid density, n is the number of propeller revolutions per second, D is the propeller diameter and

    VA is the speed of a~vance.

    The open-water efficiency of the propeller is

    (4 )

    The thrust and torque coefficients can be written as:

    AE t , Z , Re , -) Ao c (5)

    and

    ~ fQ(J , P AE

    , Z , Re , ~) -D Ao c

    (6)

    where P/D is the pitch diameter ratio

    AE/Ao is the blade area ratio Z is the number of propeller blades

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  • Re is the Reynolds number of a characteristic radius (0.75 R) tic is the ratio of the maximum propeller blade thickness to the

    length of the cord at a characteristic radius (0.75 R)

    KT and KQ can be expressed in terms of polynomials of J, and Z (see Table 1) [1].

    P D

    The Reynolds number effect on the propeller characteristics has been taken into account using Lerbs method [2]. The Reynolds number corrections for ~ and KQ 'are polynomial expressions of Re, P/D, AEiAo and J (see Table 2).

    Finally the effect of variation of blade thickness on propeller charac-teristics can be represented as a change in the Reynolds number and need not be formulated in a polynomial form (1].

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  • K.r, ~ POLYNOMIALS AND REYNOLDS NUMBER CORRECTIONS

    The polynomials for KT and ~ derived with multiple regression analy-sis are

    KT = 2: cT s,t,u,v (J)S (P/D)t (AEiAo)U (Z)V (7) s,t,u,v

    Ko = 2: cQ s,t,u,v (J)S (P/O)t (AEiAo)U ( Z)V (8) s,t,u,v

    The coefficients CT s,t,u,v and CQ s,t,u,v and terms s,t,u,v are given in Table 1.

    For Reynolds number greater than 2x10 6 the open water propeller charac-teristics should be corrected. The corrections

    AKT(Re, J, P/O, AEiAo, z) (9)

    and

    AKQ(Re, J, P/O, AEiAo, z) ( 10)

    are given in Table 2.

    -3-

  • TABLE 1

    Coefficients and terms of the ~ and Kg polynomials for the Wageningen B-screw Series for Rn=2x106. Reproduced from [ 1]

    K.r= 2: cT .(J)S.(P/D)t.(AE/Ao)u.(zV) s,t,u,v Kg= s,t,u,v cQ .(J)S.(P/D)t.(AE/Ao)u.(zV) s,t,u,v

    T s t U v cQ s t u v K.r Cs,t,u,v (J) (P/D) (AE/Ao) (Z) s,t,u,v (J) (P/D) (AE/Ao) ( z)

    +0.00880496 0 0 0 0 +0.00379368 0 0 0 0 -0.204554 1 0 0 0 +0.00886523 2 0 0 0 +0.166351 0 1 0 0 -0.032241 1 1 0 0 +0.158114 0 2 0 0 +0.00344778 0 2 0 0 -0.147581 2 0 1 0 -0.0408811 0 1 1 0 -0.481497 1 1 1 0 -0.108009 1 1 1 0 +0.415437 0 2 1 0 -0.0885381 2 1 1 0 +0.0144043 0 0 0 1 +0.188561 0 2 1 0 -0.0530054 2 0 0 1 -0.00370871 1 0 0 1 +0.0143481 0 1 0 1 +0.00513696 0 1 0 1 +0.0606826 1 1 0 1 +0.0209449 1 1 0 1 -0.0125894 0 0 1 1 +0.00474319 2 1 0 1 +0.0109689 1 0 1 1 -0.00723408 2 0 1 1 -0.133698 0 3 0 0 +0.00438388 1 1 1 1 +0.00638407 0 6 0 0 -0.0269403 0 2 1 1 -0.00132718 2 6 0 0 +0.0558082 3 0 1 0 +0.168496 3 0 1 0 +0.0161886 0 3 1 0 -0.0507214 0 0 2 0 +0.00318086 1 3 1 0 +0.0854559 2 0 2 0 +0.015896 0 0 2 0 -0.0504475 3 0 2 0 +0.0471729 1 0 2 0 +0.010465 1 6 2 0 +0.0196283 3 0 2 0 -0.00648272 2 6 2 0 -0.0502782 0 1 2 0 -0.00841728 0 3 0 1 -0.030055 3 1 2 0 +0.0168424 1 3 0 1 +0.0417122 2 2 2 0 -0.00102296 3 3 0 1 -0.0397722 0 3 2 0 -0.0317791 0 3 1 1 -0.00350024 0 6 2 0 +0.018604 1 0 2 1 -0.0106854 3 0 0 1 -0.00410798 0 2 2 1 +0.00110903 3 3 0 1 -0.000606848 0 0 0 2 -0.000313912 0 6 0 1 -0.0049819 1 0 0 2 +0.0035985 3 0 1 1 +0.0025983 2 0 0 2 -0.00142121 0 6 1 1 -0.000560528 3 0 0 2 -0.00383637 1 0 2 1 -0.00163652 1 2 0 2 +0.0126803 0 2 2 1 -0.000328787 1 6 0 2 -0.00318278 2 3 2 1 +0.000116502 2 6 0 2 +0.00334268 0 6 2 1 +0.000690904 0 0 1 2 -0.00183491 1 1 0 2 +0.00421749 0 3 1 2 +0.000112451 3 2 0 2 +0.0000565229 3 6 1 2 -0.0000297228 3 6 0 2 -0.00146564 0 3 2 2 +0.000269551 1 0 1 2

    +0.00083265 2 0 1 2 +0.00155334 0 2 1 2 +0.000302683 0 6 1 2 -0.0001843 0 0 2 2

    2 x 10 6 -0.000425399 0 3 2 2

    Rn = +0.0000869243 3 3 2 2 -0.0004659 0 6 2 2 +0.0000554194 1 6 2 2

    -4-

  • TABLE 2

    Polynomials for Reynolds number effect (above Rn = 2x106) on KT and KQ

    ~KT = 0.000353485

    -0.00333758(AE/Ao)J2 -0.00478125(AE/AO) (P/D)J +0.000257792(logRn-0.301)2(AE/Ao)J2 +0.0000643192(logRn-0.301)(P/D)6J2 -0.0000110636(logRn-0.301)2(p/D)6J 2 -0.0000276305(logRn-0.301)2 z (AE/Ao )J2 +0.0000954(logRn-0.301)z(AE/AO) (P/D)J +0.0000032049(logRn-0.301)Z2(AEiAo) (P/D)3J

    ~~ = -0.000591412

    +0.00696898(P/D) -0.0000666654z(P/D)6 +0.0160818(AE/Ao)2 -0.000938091(logRn-0.301) (P/D) -0.00059593(logRn-0.301)(P/D)2 +0.0000782099{logRn-0.301)2(p/D)2 +0.0000052199(logRn-0.301)z(AE/Ao)J2 -0.00000088528(logRn-0.301)2 z (AE/Ao) (P/D)J +0.0000230171(logRn-0.301)z(P/D)6 -0.00000184341(logRn-0.301)2 z (P/D)6 -0.00400252(logRn-0.301) (AE/AO) 2 +0.000220915(logRn-0.301)2(AE/Ao)2

  • LIMITATIONS OF APPLICABILITY OF THE REGRESSION POLYNOMIALS

    The derived regression polynomials can be used to evaluate the thrust and torque coefficients for

    and

    0.5 ( PID ( 1.40

    ( 11 )

    (12)

    ( 13 )

    However, at the extremes of the above ranges the results are not fully reliable. For instance the thrust coefficient ~ displays a local maximum for low values of J, high number of blades, low blade area ratio and high pitch-diameter ratio. This minor error is due to regression analysis.

    96 open-water propeller characteristics curves are included in this re-port. For each set of blades between 2 and 7, sixteen graphs have been plot-ted for blade area ratio varying between 0.30 and 1.05 in steps of 0.05 and pitch diameter ratio varying between 0.50 and 1.40 in steps of 0.10. These graphs have been plotted with the aid of the Michigan Computer Center plotting routines which are included in the public file *PLOTSYS [3].

    REFERENCES

    1. Oosterveld, M.W.C. and P. Van Oosanen, "Further Computer-Analyzed Data of the Wageningen B-Screw Series," IV International Symposium on Ship Auto-mation, Genova, Italy, Nov. 1974.

    2. Lerbs, H.W., "On the Effect of Scale and Roughness on Free Running Pro-pellers," Journal ASME, 1951.

    3. MTS Volume 11: "Plot Description System," University of Michigan Compu-ting Center, 1978.

    -6-

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