575 lines
102 KiB
Plaintext
575 lines
102 KiB
Plaintext
15x12 (15x12.dat)
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v2022-0915
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Simulation Date: 09/22/2022
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AIRFOIL AERO DATA GENERATED USING: POLAR DIAGRAMS
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====== PERFORMANCE DATA (versus advance ratio and MPH) ======
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DEFINITIONS:
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J=V/nD (advance ratio)
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Ct=T/(rho * n**2 * D**4) (thrust coef.)
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Cp=P/(rho * n**3 * D**5) (power coef.)
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Pe=Ct*J/Cp (efficiency)
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V (model speed in MPH)
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Mach (at prop tip)
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Reyn (at 75% of span)
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FOM (Figure of Merit)
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PROP RPM = 1000
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V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
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(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
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0.00 0.0000 0.0000 0.1167 0.0591 0.004 0.228 0.188 2.695 0.026 0.838 31.690 0.06 26743. 0.5379
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0.48 0.0337 0.0647 0.1158 0.0603 0.004 0.232 0.187 2.749 0.026 0.831 30.822 0.06 26768. 0.5211
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0.96 0.0674 0.1257 0.1147 0.0615 0.004 0.237 0.185 2.804 0.027 0.823 29.943 0.06 26796. 0.5039
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1.44 0.1011 0.1830 0.1135 0.0627 0.004 0.242 0.183 2.859 0.027 0.815 29.057 0.06 26828. 0.4864
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1.92 0.1348 0.2365 0.1121 0.0639 0.004 0.246 0.181 2.912 0.028 0.805 28.171 0.06 26863. 0.4687
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2.39 0.1685 0.2864 0.1105 0.0650 0.004 0.251 0.178 2.964 0.028 0.793 27.291 0.06 26903. 0.4508
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2.87 0.2022 0.3327 0.1087 0.0661 0.004 0.255 0.175 3.011 0.029 0.780 26.420 0.06 26946. 0.4328
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3.35 0.2359 0.3756 0.1067 0.0670 0.004 0.258 0.172 3.053 0.029 0.765 25.562 0.06 26993. 0.4148
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3.83 0.2696 0.4151 0.1043 0.0678 0.004 0.261 0.168 3.089 0.029 0.749 24.720 0.06 27044. 0.3967
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4.31 0.3033 0.4514 0.1017 0.0684 0.004 0.263 0.164 3.115 0.030 0.730 23.894 0.06 27100. 0.3787
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4.79 0.3371 0.4846 0.0988 0.0687 0.004 0.265 0.159 3.132 0.030 0.709 23.086 0.06 27160. 0.3606
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5.27 0.3708 0.5147 0.0956 0.0688 0.004 0.265 0.154 3.136 0.030 0.686 22.295 0.06 27225. 0.3424
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5.75 0.4045 0.5420 0.0920 0.0686 0.004 0.264 0.148 3.127 0.030 0.660 21.519 0.06 27294. 0.3242
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6.22 0.4382 0.5663 0.0880 0.0681 0.004 0.262 0.142 3.103 0.030 0.632 20.755 0.06 27367. 0.3059
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6.70 0.4719 0.5877 0.0837 0.0672 0.004 0.259 0.135 3.062 0.029 0.601 20.002 0.06 27445. 0.2875
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7.18 0.5056 0.6062 0.0791 0.0659 0.004 0.254 0.128 3.004 0.029 0.567 19.254 0.06 27528. 0.2690
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7.66 0.5393 0.6215 0.0741 0.0643 0.004 0.248 0.120 2.930 0.028 0.532 18.507 0.06 27614. 0.2503
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8.14 0.5730 0.6335 0.0689 0.0623 0.004 0.240 0.111 2.838 0.027 0.494 17.754 0.06 27705. 0.2315
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8.62 0.6067 0.6418 0.0634 0.0599 0.004 0.231 0.102 2.732 0.026 0.455 16.987 0.06 27801. 0.2125
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9.10 0.6404 0.6459 0.0578 0.0573 0.004 0.221 0.093 2.610 0.025 0.415 16.196 0.06 27900. 0.1934
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9.58 0.6741 0.6451 0.0520 0.0543 0.003 0.209 0.084 2.475 0.024 0.373 15.368 0.06 28004. 0.1741
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10.05 0.7078 0.6385 0.0461 0.0510 0.003 0.197 0.074 2.326 0.022 0.330 14.487 0.06 28112. 0.1545
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10.53 0.7415 0.6247 0.0400 0.0475 0.003 0.183 0.065 2.164 0.021 0.287 13.529 0.06 28225. 0.1345
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11.01 0.7752 0.6016 0.0339 0.0437 0.003 0.168 0.055 1.989 0.019 0.243 12.462 0.06 28341. 0.1140
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11.49 0.8089 0.5660 0.0277 0.0395 0.002 0.152 0.045 1.802 0.017 0.199 11.236 0.06 28462. 0.0929
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11.97 0.8426 0.5128 0.0214 0.0352 0.002 0.135 0.035 1.602 0.015 0.154 9.772 0.06 28586. 0.0710
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12.45 0.8763 0.4333 0.0151 0.0305 0.002 0.118 0.024 1.392 0.013 0.108 7.940 0.06 28715. 0.0485
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12.93 0.9100 0.3117 0.0088 0.0257 0.002 0.099 0.014 1.171 0.011 0.063 5.500 0.06 28848. 0.0256
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13.41 0.9438 0.1152 0.0025 0.0206 0.001 0.079 0.004 0.940 0.009 0.018 1.959 0.06 28984. 0.0049
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13.88 0.9775
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PROP RPM = 2000
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V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
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(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
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0.00 0.0000 0.0000 0.1172 0.0533 0.026 0.822 0.756 19.442 0.093 3.364 17.645 0.12 53486. 0.6003
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0.94 0.0332 0.0709 0.1163 0.0545 0.027 0.840 0.751 19.885 0.095 3.339 17.122 0.12 53535. 0.5803
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1.89 0.0665 0.1374 0.1153 0.0558 0.027 0.859 0.744 20.338 0.097 3.310 16.595 0.12 53591. 0.5600
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2.83 0.0997 0.1995 0.1141 0.0570 0.028 0.879 0.737 20.794 0.099 3.277 16.068 0.12 53653. 0.5395
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3.78 0.1329 0.2573 0.1128 0.0583 0.028 0.898 0.728 21.244 0.101 3.238 15.545 0.12 53722. 0.5189
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4.72 0.1661 0.3110 0.1113 0.0595 0.029 0.916 0.718 21.678 0.104 3.195 15.028 0.12 53799. 0.4982
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5.66 0.1994 0.3606 0.1096 0.0606 0.030 0.933 0.707 22.085 0.105 3.145 14.521 0.12 53883. 0.4776
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6.61 0.2326 0.4063 0.1076 0.0616 0.030 0.949 0.694 22.454 0.107 3.088 14.025 0.12 53976. 0.4571
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7.55 0.2658 0.4483 0.1053 0.0625 0.031 0.962 0.680 22.771 0.109 3.024 13.542 0.12 54076. 0.4368
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8.50 0.2991 0.4869 0.1028 0.0632 0.031 0.973 0.664 23.025 0.110 2.952 13.072 0.12 54185. 0.4166
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9.44 0.3323 0.5222 0.1000 0.0636 0.031 0.981 0.645 23.202 0.111 2.871 12.617 0.12 54303. 0.3965
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10.38 0.3655 0.5543 0.0969 0.0639 0.031 0.984 0.625 23.288 0.111 2.781 12.177 0.12 54429. 0.3766
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11.33 0.3987 0.5835 0.0934 0.0638 0.031 0.983 0.603 23.271 0.111 2.681 11.749 0.12 54564. 0.3568
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12.27 0.4320 0.6098 0.0896 0.0635 0.031 0.978 0.578 23.138 0.110 2.572 11.334 0.12 54707. 0.3371
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13.22 0.4652 0.6333 0.0854 0.0628 0.031 0.967 0.551 22.876 0.109 2.452 10.930 0.12 54859. 0.3175
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14.16 0.4984 0.6540 0.0809 0.0617 0.030 0.950 0.522 22.479 0.107 2.323 10.536 0.12 55019. 0.2978
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15.10 0.5317 0.6720 0.0761 0.0602 0.029 0.927 0.491 21.945 0.105 2.184 10.149 0.12 55189. 0.2782
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16.05 0.5649 0.6871 0.0710 0.0584 0.029 0.899 0.458 21.278 0.102 2.038 9.767 0.12 55366. 0.2586
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16.99 0.5981 0.6992 0.0657 0.0562 0.027 0.866 0.424 20.483 0.098 1.885 9.386 0.12 55552. 0.2390
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17.94 0.6313 0.7079 0.0602 0.0537 0.026 0.827 0.388 19.566 0.093 1.727 9.002 0.12 55746. 0.2195
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18.88 0.6646 0.7127 0.0545 0.0508 0.025 0.783 0.352 18.532 0.088 1.565 8.610 0.12 55949. 0.1998
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19.82 0.6978 0.7129 0.0487 0.0477 0.023 0.735 0.314 17.384 0.083 1.398 8.203 0.12 56160. 0.1799
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20.77 0.7310 0.7075 0.0428 0.0442 0.022 0.682 0.276 16.126 0.077 1.229 7.771 0.12 56378. 0.1598
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21.71 0.7643 0.6950 0.0368 0.0405 0.020 0.624 0.238 14.760 0.070 1.057 7.301 0.12 56605. 0.1392
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22.66 0.7975 0.6727 0.0307 0.0365 0.018 0.562 0.198 13.288 0.063 0.883 6.773 0.12 56841. 0.1180
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23.60 0.8307 0.6365 0.0246 0.0321 0.016 0.495 0.159 11.715 0.056 0.707 6.152 0.12 57084. 0.0959
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24.54 0.8639 0.5789 0.0185 0.0276 0.013 0.424 0.119 10.044 0.048 0.530 5.380 0.12 57335. 0.0726
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25.49 0.8972 0.4854 0.0123 0.0227 0.011 0.350 0.079 8.282 0.040 0.353 4.345 0.12 57593. 0.0479
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26.43 0.9304 0.3236 0.0061 0.0177 0.009 0.272 0.040 6.437 0.031 0.176 2.793 0.12 57860. 0.0217
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27.38 0.9636 0.0027 0.0000 0.0124 0.006 0.191 0.000 4.515 0.022 0.001 0.022 0.12 58132. 0.0000
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PROP RPM = 3000
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V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
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(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
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0.00 0.0000 0.0000 0.1175 0.0510 0.084 1.767 1.706 62.732 0.200 7.590 12.337 0.18 80228. 0.6304
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1.42 0.0333 0.0744 0.1167 0.0522 0.086 1.810 1.694 64.261 0.205 7.534 11.955 0.18 80302. 0.6086
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2.84 0.0667 0.1441 0.1157 0.0535 0.088 1.855 1.679 65.829 0.210 7.470 11.571 0.18 80386. 0.5866
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4.26 0.1000 0.2090 0.1145 0.0548 0.090 1.899 1.663 67.411 0.215 7.396 11.188 0.18 80479. 0.5643
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5.68 0.1333 0.2692 0.1132 0.0561 0.092 1.943 1.644 68.976 0.220 7.311 10.809 0.18 80584. 0.5421
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7.10 0.1666 0.3249 0.1117 0.0573 0.095 1.986 1.622 70.490 0.224 7.214 10.436 0.18 80699. 0.5199
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8.52 0.2000 0.3762 0.1100 0.0585 0.096 2.026 1.597 71.916 0.229 7.102 10.071 0.18 80826. 0.4978
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9.94 0.2333 0.4234 0.1080 0.0595 0.098 2.063 1.568 73.213 0.233 6.975 9.715 0.18 80965. 0.4759
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11.36 0.2666 0.4667 0.1058 0.0604 0.100 2.094 1.536 74.337 0.237 6.831 9.371 0.18 81117. 0.4543
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12.78 0.2999 0.5064 0.1033 0.0612 0.101 2.120 1.499 75.245 0.240 6.669 9.037 0.18 81281. 0.4329
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14.20 0.3333 0.5426 0.1004 0.0617 0.102 2.138 1.458 75.890 0.242 6.486 8.716 0.18 81459. 0.4117
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15.62 0.3666 0.5757 0.0973 0.0620 0.102 2.148 1.413 76.227 0.243 6.283 8.405 0.18 81649. 0.3908
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17.04 0.3999 0.6056 0.0938 0.0619 0.102 2.147 1.362 76.210 0.243 6.058 8.106 0.18 81852. 0.3701
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18.46 0.4333 0.6327 0.0900 0.0616 0.102 2.135 1.306 75.795 0.241 5.811 7.818 0.18 82068. 0.3495
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19.88 0.4666 0.6571 0.0858 0.0609 0.100 2.111 1.246 74.940 0.239 5.540 7.538 0.18 82297. 0.3291
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21.30 0.4999 0.6787 0.0812 0.0598 0.099 2.074 1.180 73.618 0.234 5.247 7.268 0.18 82540. 0.3088
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22.72 0.5332 0.6977 0.0764 0.0584 0.096 2.024 1.109 71.823 0.229 4.933 7.004 0.18 82795. 0.2885
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24.14 0.5666 0.7140 0.0713 0.0565 0.093 1.960 1.035 69.567 0.221 4.602 6.746 0.18 83062. 0.2684
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25.56 0.5999 0.7274 0.0659 0.0544 0.090 1.884 0.957 66.871 0.213 4.257 6.491 0.18 83343. 0.2484
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26.98 0.6332 0.7377 0.0604 0.0518 0.085 1.796 0.877 63.751 0.203 3.899 6.236 0.18 83636. 0.2284
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28.40 0.6665 0.7445 0.0547 0.0489 0.081 1.697 0.794 60.223 0.192 3.531 5.979 0.18 83941. 0.2084
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29.82 0.6999 0.7472 0.0488 0.0458 0.075 1.586 0.709 56.298 0.179 3.155 5.715 0.18 84259. 0.1883
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31.24 0.7332 0.7447 0.0429 0.0423 0.070 1.465 0.623 51.986 0.165 2.772 5.437 0.18 84589. 0.1679
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32.66 0.7665 0.7356 0.0369 0.0384 0.063 1.333 0.536 47.295 0.151 2.383 5.137 0.18 84932. 0.1471
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34.08 0.7998 0.7175 0.0308 0.0343 0.057 1.190 0.447 42.237 0.134 1.989 4.802 0.18 85286. 0.1256
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35.50 0.8332 0.6862 0.0246 0.0299 0.049 1.037 0.358 36.824 0.117 1.592 4.408 0.18 85653. 0.1032
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36.92 0.8665 0.6338 0.0185 0.0253 0.042 0.875 0.268 31.070 0.099 1.193 3.916 0.19 86031. 0.0793
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38.35 0.8998 0.5443 0.0123 0.0203 0.034 0.704 0.178 24.997 0.080 0.794 3.238 0.19 86422. 0.0535
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39.77 0.9332 0.3776 0.0061 0.0151 0.025 0.525 0.089 18.632 0.059 0.396 2.166 0.19 86823. 0.0253
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41.19 0.9665 0.0015 0.0000 0.0098 0.016 0.338 0.000 12.003 0.038 0.001 0.008 0.19 87233. 0.0000
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PROP RPM = 4000
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V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
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(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
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0.00 0.0000 0.0000 0.1178 0.0497 0.195 3.065 3.041 145.045 0.346 13.528 9.511 0.24 106968. 0.6488
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1.90 0.0334 0.0766 0.1170 0.0510 0.199 3.143 3.020 148.731 0.355 13.431 9.208 0.24 107067. 0.6259
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3.79 0.0668 0.1481 0.1160 0.0523 0.205 3.223 2.994 152.517 0.364 13.319 8.905 0.24 107179. 0.6028
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5.69 0.1002 0.2146 0.1149 0.0536 0.210 3.304 2.965 156.340 0.373 13.190 8.603 0.24 107304. 0.5795
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7.59 0.1335 0.2763 0.1136 0.0549 0.215 3.384 2.932 160.131 0.382 13.042 8.305 0.24 107444. 0.5563
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9.48 0.1669 0.3331 0.1121 0.0562 0.220 3.461 2.894 163.806 0.391 12.870 8.012 0.24 107598. 0.5331
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11.38 0.2003 0.3855 0.1104 0.0574 0.224 3.535 2.849 167.276 0.399 12.674 7.726 0.24 107768. 0.5102
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13.28 0.2337 0.4336 0.1084 0.0584 0.229 3.601 2.799 170.440 0.407 12.450 7.448 0.24 107954. 0.4874
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15.18 0.2671 0.4776 0.1062 0.0594 0.232 3.660 2.742 173.194 0.413 12.194 7.180 0.24 108157. 0.4650
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17.07 0.3005 0.5180 0.1037 0.0602 0.235 3.707 2.677 175.432 0.419 11.906 6.921 0.24 108377. 0.4429
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18.97 0.3339 0.5548 0.1009 0.0607 0.237 3.741 2.604 177.041 0.423 11.582 6.671 0.24 108614. 0.4211
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20.87 0.3672 0.5883 0.0977 0.0610 0.239 3.759 2.523 177.912 0.425 11.221 6.431 0.24 108868. 0.3996
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22.76 0.4006 0.6188 0.0942 0.0610 0.239 3.760 2.433 177.935 0.425 10.820 6.201 0.24 109140. 0.3783
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24.66 0.4340 0.6464 0.0904 0.0607 0.237 3.740 2.333 176.999 0.423 10.378 5.979 0.24 109429. 0.3573
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26.56 0.4674 0.6712 0.0862 0.0600 0.235 3.698 2.225 175.007 0.418 9.895 5.766 0.24 109736. 0.3364
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28.45 0.5008 0.6935 0.0816 0.0589 0.231 3.632 2.107 171.891 0.410 9.371 5.559 0.24 110060. 0.3157
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30.35 0.5342 0.7131 0.0767 0.0575 0.225 3.542 1.981 167.635 0.400 8.811 5.360 0.24 110402. 0.2951
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32.25 0.5676 0.7302 0.0716 0.0556 0.218 3.429 1.848 162.270 0.387 8.219 5.165 0.24 110760. 0.2746
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34.14 0.6009 0.7445 0.0662 0.0534 0.209 3.293 1.709 155.839 0.372 7.601 4.974 0.24 111135. 0.2544
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36.04 0.6343 0.7560 0.0606 0.0509 0.199 3.135 1.565 148.384 0.354 6.962 4.784 0.24 111527. 0.2341
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37.94 0.6677 0.7641 0.0549 0.0480 0.188 2.957 1.417 139.939 0.334 6.305 4.594 0.24 111936. 0.2140
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39.83 0.7011 0.7684 0.0491 0.0448 0.175 2.758 1.266 130.532 0.312 5.632 4.400 0.24 112361. 0.1937
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41.73 0.7345 0.7679 0.0431 0.0412 0.161 2.540 1.112 120.185 0.287 4.947 4.197 0.24 112803. 0.1732
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43.63 0.7679 0.7613 0.0370 0.0373 0.146 2.302 0.956 108.922 0.260 4.252 3.981 0.25 113261. 0.1522
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45.53 0.8013 0.7463 0.0309 0.0332 0.130 2.045 0.798 96.766 0.231 3.549 3.739 0.25 113735. 0.1307
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47.42 0.8346 0.7188 0.0247 0.0287 0.112 1.770 0.638 83.746 0.200 2.839 3.457 0.25 114225. 0.1081
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49.32 0.8680 0.6709 0.0185 0.0240 0.094 1.477 0.478 69.902 0.167 2.127 3.103 0.25 114732. 0.0839
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51.22 0.9014 0.5857 0.0123 0.0190 0.074 1.168 0.318 55.284 0.132 1.414 2.608 0.25 115254. 0.0575
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53.11 0.9348 0.4183 0.0061 0.0137 0.054 0.844 0.158 39.958 0.095 0.704 1.797 0.25 115791. 0.0280
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55.01 0.9682 -0.0005 0.0000 0.0082 0.032 0.507 0.000 23.989 0.057 0.000 -0.002 0.25 116337. 0.0000
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PROP RPM = 5000
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V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
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(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
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0.00 0.0000 0.0000 0.1182 0.0490 0.374 4.719 4.766 279.132 0.533 21.197 7.744 0.30 133707. 0.6613
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2.39 0.0337 0.0786 0.1173 0.0503 0.384 4.843 4.732 286.495 0.547 21.048 7.492 0.30 133832. 0.6375
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4.78 0.0674 0.1518 0.1164 0.0516 0.394 4.971 4.693 294.069 0.562 20.876 7.239 0.30 133973. 0.6135
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7.18 0.1010 0.2199 0.1153 0.0530 0.405 5.101 4.649 301.729 0.576 20.677 6.988 0.30 134131. 0.5894
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9.57 0.1347 0.2827 0.1140 0.0543 0.415 5.229 4.597 309.331 0.591 20.446 6.740 0.30 134307. 0.5653
|
|
11.96 0.1684 0.3407 0.1125 0.0556 0.425 5.354 4.537 316.708 0.605 20.179 6.497 0.30 134503. 0.5413
|
|
14.35 0.2021 0.3939 0.1108 0.0568 0.434 5.472 4.468 323.673 0.618 19.872 6.260 0.30 134718. 0.5176
|
|
16.75 0.2358 0.4427 0.1088 0.0579 0.443 5.579 4.388 330.024 0.630 19.519 6.031 0.30 134954. 0.4942
|
|
19.14 0.2695 0.4874 0.1066 0.0589 0.450 5.672 4.298 335.547 0.641 19.117 5.810 0.30 135211. 0.4711
|
|
21.53 0.3031 0.5282 0.1040 0.0597 0.456 5.748 4.195 340.022 0.649 18.661 5.596 0.30 135490. 0.4484
|
|
23.92 0.3368 0.5655 0.1012 0.0603 0.460 5.802 4.080 343.224 0.656 18.148 5.392 0.30 135791. 0.4260
|
|
26.31 0.3705 0.5994 0.0980 0.0606 0.463 5.831 3.951 344.928 0.659 17.574 5.195 0.30 136114. 0.4040
|
|
28.71 0.4042 0.6302 0.0944 0.0606 0.463 5.830 3.808 344.908 0.659 16.937 5.007 0.30 136460. 0.3822
|
|
31.10 0.4379 0.6581 0.0905 0.0602 0.460 5.797 3.649 342.943 0.655 16.233 4.827 0.30 136827. 0.3607
|
|
33.49 0.4716 0.6832 0.0862 0.0595 0.454 5.728 3.476 338.838 0.647 15.462 4.653 0.30 137217. 0.3394
|
|
35.88 0.5052 0.7058 0.0815 0.0584 0.446 5.620 3.288 332.462 0.635 14.627 4.486 0.30 137629. 0.3183
|
|
38.28 0.5389 0.7258 0.0766 0.0568 0.434 5.474 3.088 323.794 0.618 13.734 4.325 0.30 138063. 0.2973
|
|
40.67 0.5726 0.7432 0.0713 0.0549 0.420 5.289 2.876 312.900 0.598 12.792 4.169 0.30 138518. 0.2765
|
|
43.06 0.6063 0.7580 0.0658 0.0526 0.402 5.069 2.655 299.867 0.573 11.808 4.015 0.30 138995. 0.2559
|
|
45.45 0.6400 0.7699 0.0602 0.0500 0.382 4.814 2.426 284.779 0.544 10.791 3.864 0.30 139493. 0.2354
|
|
47.84 0.6737 0.7787 0.0543 0.0470 0.359 4.525 2.191 267.699 0.511 9.746 3.712 0.30 140012. 0.2150
|
|
50.24 0.7073 0.7836 0.0484 0.0437 0.333 4.204 1.951 248.683 0.475 8.677 3.558 0.30 140552. 0.1944
|
|
52.63 0.7410 0.7839 0.0423 0.0400 0.305 3.850 1.706 227.775 0.435 7.589 3.397 0.31 141113. 0.1736
|
|
55.02 0.7747 0.7780 0.0361 0.0360 0.275 3.466 1.458 205.022 0.392 6.485 3.225 0.31 141695. 0.1523
|
|
57.41 0.8084 0.7635 0.0299 0.0317 0.242 3.051 1.207 180.473 0.345 5.369 3.034 0.31 142298. 0.1304
|
|
59.81 0.8421 0.7359 0.0237 0.0271 0.207 2.607 0.954 154.192 0.294 4.244 2.807 0.31 142921. 0.1073
|
|
62.20 0.8757 0.6860 0.0174 0.0222 0.169 2.134 0.700 126.262 0.241 3.115 2.516 0.31 143564. 0.0824
|
|
64.59 0.9094 0.5926 0.0111 0.0170 0.130 1.636 0.447 96.794 0.185 1.986 2.093 0.31 144227. 0.0547
|
|
66.98 0.9431 0.3922 0.0048 0.0116 0.088 1.115 0.194 65.930 0.126 0.864 1.336 0.31 144909. 0.0230
|
|
69.37 0.9768
|
|
|
|
|
|
|
|
PROP RPM = 6000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1185 0.0486 0.641 6.736 6.884 478.204 0.761 30.620 6.529 0.36 160444. 0.6701
|
|
2.85 0.0334 0.0789 0.1177 0.0499 0.658 6.917 6.838 491.007 0.781 30.414 6.316 0.36 160592. 0.6461
|
|
5.70 0.0669 0.1525 0.1168 0.0512 0.676 7.103 6.784 504.201 0.802 30.176 6.103 0.36 160760. 0.6218
|
|
8.55 0.1003 0.2209 0.1157 0.0526 0.694 7.291 6.722 517.567 0.824 29.900 5.891 0.36 160948. 0.5975
|
|
11.40 0.1338 0.2840 0.1145 0.0539 0.712 7.478 6.650 530.860 0.845 29.579 5.682 0.36 161157. 0.5731
|
|
14.25 0.1672 0.3422 0.1131 0.0552 0.729 7.660 6.566 543.796 0.865 29.206 5.477 0.36 161389. 0.5490
|
|
17.10 0.2007 0.3957 0.1114 0.0565 0.746 7.833 6.470 556.051 0.885 28.776 5.277 0.36 161645. 0.5251
|
|
19.96 0.2341 0.4448 0.1095 0.0576 0.761 7.991 6.358 567.278 0.903 28.282 5.084 0.36 161925. 0.5015
|
|
22.81 0.2676 0.4896 0.1073 0.0586 0.774 8.130 6.231 577.108 0.918 27.716 4.897 0.36 162231. 0.4782
|
|
25.66 0.3010 0.5307 0.1048 0.0595 0.785 8.243 6.087 585.161 0.931 27.074 4.718 0.36 162562. 0.4553
|
|
28.51 0.3345 0.5682 0.1020 0.0600 0.793 8.326 5.924 591.052 0.941 26.350 4.546 0.36 162919. 0.4328
|
|
31.36 0.3679 0.6023 0.0989 0.0604 0.797 8.373 5.742 594.390 0.946 25.538 4.381 0.36 163302. 0.4107
|
|
34.21 0.4014 0.6334 0.0954 0.0604 0.798 8.379 5.539 594.788 0.947 24.635 4.224 0.36 163712. 0.3888
|
|
37.06 0.4348 0.6617 0.0915 0.0601 0.794 8.338 5.314 591.866 0.942 23.637 4.072 0.36 164148. 0.3672
|
|
39.91 0.4683 0.6872 0.0873 0.0595 0.785 8.245 5.068 585.281 0.932 22.543 3.928 0.36 164611. 0.3459
|
|
42.76 0.5017 0.7102 0.0827 0.0584 0.771 8.097 4.801 574.789 0.915 21.355 3.788 0.36 165099. 0.3247
|
|
45.61 0.5352 0.7308 0.0777 0.0569 0.751 7.893 4.515 560.331 0.892 20.081 3.654 0.36 165613. 0.3037
|
|
48.46 0.5686 0.7489 0.0725 0.0551 0.727 7.635 4.212 542.004 0.863 18.735 3.525 0.36 166153. 0.2830
|
|
51.31 0.6021 0.7645 0.0671 0.0528 0.697 7.325 3.896 519.958 0.828 17.329 3.398 0.36 166719. 0.2624
|
|
54.17 0.6355 0.7775 0.0614 0.0502 0.663 6.964 3.568 494.336 0.787 15.872 3.274 0.36 167310. 0.2419
|
|
57.02 0.6690 0.7875 0.0556 0.0473 0.624 6.554 3.232 465.253 0.740 14.374 3.150 0.37 167925. 0.2215
|
|
59.87 0.7024 0.7940 0.0497 0.0440 0.580 6.097 2.887 432.804 0.689 12.841 3.025 0.37 168566. 0.2011
|
|
62.72 0.7359 0.7964 0.0437 0.0403 0.532 5.594 2.536 397.070 0.632 11.279 2.897 0.37 169231. 0.1804
|
|
65.57 0.7693 0.7934 0.0375 0.0364 0.480 5.045 2.179 358.126 0.570 9.694 2.760 0.37 169921. 0.1594
|
|
68.42 0.8028 0.7829 0.0313 0.0321 0.424 4.452 1.819 316.056 0.503 8.090 2.610 0.37 170635. 0.1377
|
|
71.27 0.8362 0.7610 0.0251 0.0275 0.363 3.817 1.455 270.965 0.431 6.473 2.436 0.37 171373. 0.1149
|
|
74.12 0.8697 0.7204 0.0188 0.0227 0.299 3.141 1.090 222.988 0.355 4.848 2.217 0.37 172136. 0.0905
|
|
76.97 0.9031 0.6434 0.0125 0.0175 0.231 2.427 0.724 172.305 0.274 3.222 1.907 0.37 172921. 0.0635
|
|
79.82 0.9366 0.4800 0.0062 0.0121 0.160 1.679 0.360 119.154 0.190 1.603 1.372 0.37 173730. 0.0322
|
|
82.67 0.9700 -0.0022 0.0000 0.0065 0.085 0.898 -0.001 63.727 0.101 -0.004 -0.006 0.37 174548. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 7000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1189 0.0484 1.014 9.130 9.403 756.104 1.031 41.824 5.641 0.42 187177. 0.6766
|
|
3.33 0.0335 0.0796 0.1182 0.0497 1.042 9.379 9.343 776.745 1.060 41.556 5.455 0.42 187351. 0.6523
|
|
6.66 0.0669 0.1538 0.1173 0.0511 1.070 9.636 9.272 798.051 1.089 41.244 5.270 0.42 187546. 0.6277
|
|
9.99 0.1004 0.2226 0.1163 0.0524 1.099 9.897 9.191 819.675 1.118 40.880 5.086 0.42 187765. 0.6031
|
|
13.31 0.1339 0.2862 0.1151 0.0538 1.128 10.157 9.095 841.223 1.148 40.455 4.904 0.42 188010. 0.5785
|
|
16.64 0.1674 0.3448 0.1136 0.0552 1.156 10.411 8.984 862.227 1.176 39.961 4.726 0.42 188281. 0.5541
|
|
19.97 0.2008 0.3986 0.1120 0.0564 1.183 10.652 8.855 882.167 1.203 39.387 4.553 0.42 188579. 0.5300
|
|
23.30 0.2343 0.4479 0.1101 0.0576 1.208 10.873 8.706 900.472 1.228 38.724 4.385 0.42 188907. 0.5061
|
|
26.63 0.2678 0.4930 0.1080 0.0586 1.229 11.067 8.535 916.542 1.250 37.963 4.224 0.42 189264. 0.4827
|
|
29.96 0.3013 0.5343 0.1055 0.0595 1.247 11.226 8.340 929.758 1.268 37.096 4.069 0.42 189651. 0.4596
|
|
33.28 0.3347 0.5720 0.1027 0.0601 1.260 11.344 8.119 939.489 1.282 36.115 3.920 0.42 190068. 0.4369
|
|
36.61 0.3682 0.6063 0.0996 0.0605 1.267 11.412 7.872 945.105 1.289 35.013 3.778 0.42 190516. 0.4146
|
|
39.94 0.4017 0.6377 0.0961 0.0605 1.269 11.422 7.595 945.980 1.290 33.784 3.642 0.42 190996. 0.3926
|
|
43.27 0.4352 0.6661 0.0922 0.0602 1.263 11.368 7.290 941.499 1.284 32.424 3.512 0.42 191506. 0.3709
|
|
46.60 0.4686 0.6919 0.0880 0.0596 1.249 11.243 6.954 931.106 1.270 30.929 3.387 0.42 192046. 0.3494
|
|
49.93 0.5021 0.7153 0.0833 0.0585 1.226 11.041 6.588 914.406 1.247 29.304 3.268 0.42 192617. 0.3281
|
|
53.25 0.5356 0.7362 0.0784 0.0570 1.195 10.762 6.196 891.298 1.216 27.561 3.153 0.42 193219. 0.3070
|
|
56.58 0.5691 0.7547 0.0731 0.0551 1.156 10.408 5.782 861.934 1.176 25.717 3.042 0.42 193850. 0.2862
|
|
59.91 0.6025 0.7708 0.0677 0.0529 1.108 9.980 5.348 826.559 1.128 23.789 2.935 0.42 194511. 0.2655
|
|
63.24 0.6360 0.7843 0.0620 0.0503 1.053 9.483 4.899 785.402 1.071 21.791 2.829 0.42 195202. 0.2450
|
|
66.57 0.6695 0.7951 0.0561 0.0473 0.991 8.919 4.437 738.655 1.008 19.735 2.724 0.43 195921. 0.2245
|
|
69.90 0.7029 0.8025 0.0501 0.0439 0.921 8.289 3.964 686.468 0.936 17.631 2.619 0.43 196670. 0.2040
|
|
73.22 0.7364 0.8060 0.0440 0.0402 0.843 7.595 3.482 628.972 0.858 15.487 2.511 0.43 197448. 0.1833
|
|
76.55 0.7699 0.8043 0.0379 0.0362 0.759 6.838 2.992 566.289 0.773 13.310 2.397 0.43 198254. 0.1622
|
|
79.88 0.8034 0.7955 0.0316 0.0319 0.669 6.020 2.497 498.556 0.680 11.107 2.272 0.43 199088. 0.1404
|
|
83.21 0.8368 0.7759 0.0253 0.0273 0.571 5.143 1.998 425.941 0.581 8.885 2.127 0.43 199951. 0.1176
|
|
86.54 0.8703 0.7381 0.0189 0.0223 0.468 4.210 1.496 348.661 0.476 6.653 1.946 0.43 200842. 0.0931
|
|
89.87 0.9038 0.6648 0.0126 0.0171 0.358 3.224 0.993 267.010 0.364 4.419 1.688 0.43 201760. 0.0658
|
|
93.19 0.9373 0.5039 0.0062 0.0116 0.243 2.190 0.493 181.373 0.247 2.194 1.233 0.43 202704. 0.0339
|
|
96.52 0.9707 -0.0070 0.0000 0.0059 0.123 1.111 -0.003 92.038 0.126 -0.015 -0.017 0.44 203657. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 8000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1194 0.0483 1.512 11.912 12.329 1127.500 1.346 54.841 4.960 0.48 213908. 0.6813
|
|
3.80 0.0335 0.0800 0.1187 0.0497 1.554 12.243 12.255 1158.792 1.383 54.509 4.797 0.48 214106. 0.6569
|
|
7.61 0.0670 0.1545 0.1178 0.0511 1.597 12.585 12.167 1191.163 1.422 54.121 4.633 0.48 214329. 0.6322
|
|
11.41 0.1004 0.2237 0.1169 0.0525 1.642 12.933 12.065 1224.091 1.461 53.666 4.471 0.48 214579. 0.6074
|
|
15.22 0.1339 0.2875 0.1157 0.0539 1.686 13.280 11.945 1256.970 1.500 53.132 4.310 0.48 214858. 0.5827
|
|
19.02 0.1674 0.3463 0.1143 0.0553 1.729 13.620 11.805 1289.094 1.539 52.506 4.153 0.48 215167. 0.5582
|
|
22.82 0.2009 0.4003 0.1127 0.0566 1.770 13.943 11.640 1319.660 1.575 51.776 4.001 0.48 215509. 0.5340
|
|
26.63 0.2343 0.4498 0.1109 0.0578 1.807 14.240 11.450 1347.791 1.609 50.928 3.853 0.48 215883. 0.5100
|
|
30.43 0.2678 0.4951 0.1088 0.0588 1.841 14.502 11.230 1372.563 1.638 49.951 3.711 0.48 216291. 0.4865
|
|
34.24 0.3013 0.5365 0.1063 0.0597 1.868 14.718 10.978 1393.021 1.663 48.831 3.575 0.48 216734. 0.4633
|
|
38.04 0.3348 0.5744 0.1036 0.0604 1.888 14.878 10.692 1408.201 1.681 47.560 3.444 0.48 217211. 0.4405
|
|
41.85 0.3682 0.6089 0.1004 0.0607 1.900 14.973 10.370 1417.143 1.692 46.128 3.319 0.48 217724. 0.4181
|
|
45.65 0.4017 0.6404 0.0970 0.0608 1.903 14.991 10.010 1418.890 1.694 44.526 3.200 0.48 218273. 0.3960
|
|
49.45 0.4352 0.6691 0.0931 0.0605 1.894 14.924 9.611 1412.511 1.686 42.749 3.086 0.48 218856. 0.3743
|
|
53.26 0.4687 0.6951 0.0888 0.0599 1.874 14.761 9.171 1397.163 1.668 40.793 2.977 0.48 219475. 0.3527
|
|
57.06 0.5021 0.7187 0.0842 0.0588 1.840 14.498 8.692 1372.232 1.638 38.663 2.873 0.48 220129. 0.3313
|
|
60.87 0.5356 0.7399 0.0792 0.0573 1.794 14.132 8.178 1337.557 1.597 36.374 2.773 0.48 220817. 0.3102
|
|
64.67 0.5691 0.7589 0.0739 0.0554 1.734 13.665 7.633 1293.365 1.544 33.950 2.677 0.48 221539. 0.2893
|
|
68.47 0.6026 0.7754 0.0684 0.0531 1.663 13.101 7.062 1240.027 1.480 31.413 2.583 0.48 222295. 0.2685
|
|
72.28 0.6360 0.7895 0.0627 0.0505 1.580 12.445 6.471 1177.899 1.406 28.783 2.492 0.49 223085. 0.2479
|
|
76.08 0.6695 0.8009 0.0568 0.0475 1.485 11.699 5.862 1107.274 1.322 26.074 2.401 0.49 223909. 0.2274
|
|
79.89 0.7030 0.8092 0.0507 0.0441 1.379 10.865 5.239 1028.385 1.228 23.301 2.310 0.49 224765. 0.2069
|
|
83.69 0.7365 0.8137 0.0446 0.0404 1.262 9.947 4.603 941.431 1.124 20.474 2.218 0.49 225654. 0.1861
|
|
87.49 0.7700 0.8133 0.0383 0.0363 1.135 8.945 3.957 846.599 1.011 17.603 2.120 0.49 226576. 0.1650
|
|
91.30 0.8034 0.8061 0.0320 0.0319 0.998 7.862 3.304 744.096 0.888 14.697 2.014 0.49 227530. 0.1432
|
|
95.10 0.8369 0.7887 0.0256 0.0272 0.850 6.700 2.645 634.172 0.757 11.765 1.892 0.49 228517. 0.1203
|
|
98.91 0.8704 0.7539 0.0192 0.0222 0.694 5.464 1.982 517.160 0.617 8.818 1.739 0.49 229535. 0.0958
|
|
102.71 0.9039 0.6847 0.0128 0.0169 0.528 4.157 1.319 393.504 0.470 5.868 1.521 0.50 230585. 0.0683
|
|
106.52 0.9373 0.5287 0.0064 0.0113 0.354 2.787 0.658 263.790 0.315 2.929 1.132 0.50 231664. 0.0359
|
|
110.32 0.9708 0.0042 0.0000 0.0055 0.172 1.357 0.002 128.446 0.153 0.011 0.009 0.50 232753. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 9000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1199 0.0484 2.156 15.102 15.671 1608.080 1.706 69.706 4.420 0.54 240635. 0.6845
|
|
4.28 0.0335 0.0802 0.1192 0.0498 2.217 15.528 15.583 1653.415 1.754 69.313 4.275 0.54 240857. 0.6601
|
|
8.56 0.0670 0.1550 0.1185 0.0512 2.280 15.969 15.479 1700.439 1.804 68.851 4.129 0.54 241107. 0.6354
|
|
12.85 0.1005 0.2244 0.1175 0.0526 2.345 16.420 15.356 1748.398 1.855 68.305 3.984 0.54 241388. 0.6107
|
|
17.13 0.1340 0.2884 0.1164 0.0541 2.409 16.871 15.211 1796.415 1.906 67.661 3.841 0.54 241702. 0.5860
|
|
21.41 0.1675 0.3474 0.1151 0.0555 2.472 17.313 15.040 1843.446 1.956 66.900 3.701 0.54 242050. 0.5614
|
|
25.69 0.2010 0.4015 0.1136 0.0568 2.532 17.734 14.839 1888.315 2.004 66.005 3.564 0.54 242435. 0.5371
|
|
29.97 0.2345 0.4511 0.1118 0.0581 2.588 18.123 14.604 1929.723 2.047 64.959 3.433 0.54 242856. 0.5131
|
|
34.26 0.2680 0.4965 0.1097 0.0592 2.637 18.466 14.331 1966.301 2.086 63.746 3.306 0.54 243316. 0.4895
|
|
38.54 0.3015 0.5380 0.1073 0.0601 2.678 18.751 14.017 1996.637 2.118 62.349 3.184 0.54 243815. 0.4664
|
|
42.82 0.3350 0.5760 0.1045 0.0608 2.708 18.964 13.659 2019.309 2.143 60.755 3.068 0.54 244353. 0.4435
|
|
47.10 0.3685 0.6106 0.1014 0.0612 2.726 19.092 13.254 2032.909 2.157 58.952 2.957 0.54 244931. 0.4211
|
|
51.39 0.4019 0.6423 0.0979 0.0613 2.730 19.121 12.799 2036.043 2.160 56.929 2.851 0.54 245550. 0.3990
|
|
55.67 0.4354 0.6712 0.0941 0.0610 2.719 19.040 12.293 2027.361 2.151 54.677 2.750 0.54 246208. 0.3772
|
|
59.95 0.4689 0.6974 0.0898 0.0604 2.690 18.836 11.734 2005.635 2.128 52.194 2.654 0.54 246906. 0.3556
|
|
64.23 0.5024 0.7213 0.0851 0.0593 2.642 18.501 11.125 1969.972 2.090 49.484 2.561 0.54 247643. 0.3342
|
|
68.51 0.5359 0.7428 0.0801 0.0578 2.575 18.033 10.469 1920.117 2.037 46.567 2.473 0.54 248419. 0.3130
|
|
72.80 0.5694 0.7621 0.0748 0.0559 2.489 17.434 9.774 1856.402 1.970 43.473 2.388 0.54 249233. 0.2920
|
|
77.08 0.6029 0.7791 0.0692 0.0536 2.386 16.711 9.045 1779.371 1.888 40.232 2.306 0.55 250086. 0.2712
|
|
81.36 0.6364 0.7937 0.0634 0.0509 2.266 15.867 8.289 1689.557 1.793 36.868 2.225 0.55 250976. 0.2506
|
|
85.64 0.6699 0.8056 0.0575 0.0478 2.129 14.908 7.510 1587.392 1.684 33.404 2.146 0.55 251904. 0.2300
|
|
89.92 0.7034 0.8146 0.0514 0.0443 1.976 13.836 6.712 1473.224 1.563 29.854 2.066 0.55 252870. 0.2094
|
|
94.21 0.7369 0.8200 0.0451 0.0406 1.807 12.653 5.898 1347.340 1.430 26.233 1.985 0.55 253872. 0.1886
|
|
98.49 0.7704 0.8207 0.0388 0.0364 1.623 11.364 5.071 1210.017 1.284 22.555 1.901 0.55 254910. 0.1674
|
|
102.77 0.8039 0.8149 0.0324 0.0320 1.424 9.969 4.233 1061.550 1.126 18.830 1.809 0.55 255986. 0.1456
|
|
107.05 0.8374 0.7993 0.0259 0.0272 1.210 8.474 3.388 902.307 0.957 15.070 1.703 0.55 257097. 0.1226
|
|
111.34 0.8709 0.7669 0.0194 0.0221 0.983 6.882 2.538 732.766 0.777 11.291 1.571 0.56 258244. 0.0979
|
|
115.62 0.9044 0.7008 0.0129 0.0167 0.742 5.199 1.687 553.576 0.587 7.506 1.383 0.56 259426. 0.0703
|
|
119.90 0.9379 0.5475 0.0064 0.0110 0.490 3.433 0.840 365.592 0.388 3.734 1.042 0.56 260642. 0.0373
|
|
124.18 0.9714 -0.0041 0.0000 0.0051 0.227 1.591 -0.003 169.367 0.180 -0.013 -0.008 0.56 261864. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 10000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1205 0.0486 2.970 18.721 19.437 2214.908 2.115 86.455 3.980 0.59 267358. 0.6864
|
|
4.76 0.0335 0.0803 0.1199 0.0500 3.055 19.256 19.337 2278.241 2.176 86.010 3.850 0.60 267604. 0.6622
|
|
9.52 0.0670 0.1552 0.1191 0.0514 3.144 19.813 19.218 2344.153 2.239 85.482 3.719 0.60 267881. 0.6377
|
|
14.28 0.1005 0.2246 0.1182 0.0529 3.234 20.383 19.077 2411.607 2.303 84.854 3.588 0.60 268193. 0.6130
|
|
19.04 0.1340 0.2887 0.1172 0.0544 3.325 20.956 18.909 2479.359 2.368 84.105 3.459 0.60 268541. 0.5884
|
|
23.80 0.1675 0.3477 0.1160 0.0559 3.414 21.519 18.708 2545.946 2.431 83.213 3.333 0.60 268928. 0.5639
|
|
28.56 0.2010 0.4019 0.1145 0.0573 3.500 22.058 18.470 2609.673 2.492 82.155 3.210 0.60 269354. 0.5397
|
|
33.32 0.2346 0.4515 0.1127 0.0586 3.579 22.556 18.189 2668.690 2.548 80.907 3.091 0.60 269823. 0.5158
|
|
38.08 0.2681 0.4970 0.1107 0.0597 3.649 22.999 17.861 2721.018 2.598 79.447 2.977 0.60 270334. 0.4922
|
|
42.84 0.3016 0.5386 0.1084 0.0607 3.707 23.367 17.481 2764.636 2.640 77.756 2.868 0.60 270889. 0.4691
|
|
47.60 0.3351 0.5766 0.1056 0.0614 3.752 23.645 17.044 2797.505 2.671 75.814 2.763 0.60 271488. 0.4463
|
|
52.36 0.3686 0.6114 0.1026 0.0618 3.778 23.815 16.548 2817.626 2.691 73.605 2.664 0.60 272132. 0.4239
|
|
57.11 0.4021 0.6432 0.0991 0.0620 3.786 23.861 15.989 2823.034 2.696 71.117 2.569 0.60 272821. 0.4018
|
|
61.87 0.4356 0.6723 0.0952 0.0617 3.771 23.766 15.364 2811.837 2.685 68.338 2.478 0.60 273554. 0.3800
|
|
66.63 0.4691 0.6987 0.0909 0.0611 3.731 23.517 14.673 2782.315 2.657 65.264 2.392 0.60 274331. 0.3584
|
|
71.39 0.5026 0.7228 0.0863 0.0600 3.665 23.102 13.917 2733.200 2.610 61.901 2.309 0.60 275151. 0.3370
|
|
76.15 0.5361 0.7447 0.0812 0.0585 3.573 22.518 13.101 2664.118 2.544 58.274 2.230 0.60 276015. 0.3158
|
|
80.91 0.5696 0.7643 0.0758 0.0565 3.454 21.769 12.235 2575.528 2.459 54.420 2.155 0.60 276922. 0.2948
|
|
85.67 0.6031 0.7817 0.0702 0.0542 3.310 20.862 11.326 2468.212 2.357 50.377 2.081 0.61 277872. 0.2740
|
|
90.43 0.6366 0.7968 0.0643 0.0514 3.142 19.803 10.382 2342.933 2.237 46.177 2.010 0.61 278863. 0.2533
|
|
95.19 0.6701 0.8093 0.0583 0.0483 2.951 18.598 9.408 2200.326 2.101 41.848 1.939 0.61 279896. 0.2327
|
|
99.95 0.7037 0.8190 0.0521 0.0448 2.737 17.250 8.410 2040.883 1.949 37.409 1.869 0.61 280970. 0.2120
|
|
104.71 0.7372 0.8252 0.0458 0.0409 2.501 15.764 7.392 1865.017 1.781 32.879 1.798 0.61 282085. 0.1912
|
|
109.47 0.7707 0.8270 0.0394 0.0367 2.244 14.142 6.356 1673.115 1.598 28.273 1.723 0.61 283241. 0.1699
|
|
114.23 0.8042 0.8225 0.0329 0.0322 1.965 12.388 5.307 1465.593 1.400 23.607 1.643 0.61 284437. 0.1480
|
|
118.99 0.8377 0.8087 0.0263 0.0273 1.667 10.506 4.248 1242.962 1.187 18.897 1.550 0.62 285673. 0.1250
|
|
123.75 0.8712 0.7786 0.0197 0.0221 1.349 8.502 3.183 1005.891 0.961 14.158 1.435 0.62 286948. 0.1002
|
|
128.51 0.9047 0.7158 0.0131 0.0166 1.013 6.384 2.116 755.286 0.721 9.411 1.271 0.62 288263. 0.0723
|
|
133.27 0.9382 0.5661 0.0065 0.0108 0.660 4.161 1.052 492.352 0.470 4.678 0.969 0.62 289616. 0.0389
|
|
138.03 0.9717 -0.0075 0.0000 0.0048 0.292 1.841 -0.006 217.786 0.208 -0.026 -0.012 0.62 290969. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 11000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1211 0.0490 3.987 22.843 23.633 2972.893 2.581 105.121 3.606 0.65 294077. 0.6857
|
|
5.24 0.0335 0.0801 0.1205 0.0504 4.101 23.497 23.525 3057.978 2.655 104.638 3.489 0.65 294346. 0.6620
|
|
10.47 0.0670 0.1548 0.1198 0.0519 4.220 24.180 23.395 3146.913 2.732 104.061 3.372 0.65 294650. 0.6380
|
|
15.71 0.1005 0.2242 0.1190 0.0534 4.343 24.883 23.239 3238.328 2.811 103.368 3.255 0.65 294992. 0.6138
|
|
20.95 0.1341 0.2883 0.1181 0.0549 4.466 25.592 23.051 3330.591 2.891 102.532 3.139 0.66 295374. 0.5896
|
|
26.18 0.1676 0.3473 0.1169 0.0564 4.589 26.292 22.825 3421.700 2.970 101.524 3.026 0.66 295798. 0.5654
|
|
31.42 0.2011 0.4015 0.1155 0.0579 4.706 26.965 22.553 3509.354 3.047 100.314 2.915 0.66 296267. 0.5415
|
|
36.66 0.2346 0.4512 0.1139 0.0592 4.816 27.593 22.228 3590.980 3.117 98.871 2.808 0.66 296782. 0.5178
|
|
41.89 0.2681 0.4967 0.1119 0.0604 4.913 28.152 21.845 3663.809 3.181 97.166 2.704 0.66 297345. 0.4944
|
|
47.13 0.3016 0.5383 0.1096 0.0614 4.995 28.622 21.397 3724.956 3.234 95.172 2.605 0.66 297956. 0.4714
|
|
52.37 0.3352 0.5764 0.1069 0.0622 5.058 28.980 20.878 3771.534 3.274 92.865 2.511 0.66 298616. 0.4488
|
|
57.60 0.3687 0.6113 0.1039 0.0627 5.097 29.204 20.284 3800.698 3.299 90.224 2.421 0.66 299326. 0.4265
|
|
62.84 0.4022 0.6432 0.1005 0.0628 5.109 29.273 19.611 3809.716 3.307 87.231 2.335 0.66 300085. 0.4045
|
|
68.08 0.4357 0.6724 0.0966 0.0626 5.091 29.168 18.857 3795.999 3.295 83.875 2.253 0.66 300893. 0.3827
|
|
73.31 0.4692 0.6991 0.0923 0.0619 5.038 28.870 18.019 3757.206 3.262 80.148 2.175 0.66 301749. 0.3612
|
|
78.55 0.5027 0.7235 0.0876 0.0609 4.951 28.366 17.099 3691.602 3.205 76.057 2.101 0.66 302654. 0.3398
|
|
83.79 0.5362 0.7456 0.0825 0.0593 4.826 27.651 16.105 3598.625 3.124 71.634 2.030 0.66 303607. 0.3186
|
|
89.02 0.5698 0.7656 0.0771 0.0574 4.665 26.731 15.046 3478.898 3.020 66.924 1.962 0.67 304607. 0.2976
|
|
94.26 0.6033 0.7834 0.0714 0.0550 4.470 25.614 13.933 3333.524 2.894 61.976 1.896 0.67 305653. 0.2768
|
|
99.50 0.6368 0.7990 0.0654 0.0522 4.242 24.309 12.776 3163.582 2.746 56.828 1.832 0.67 306746. 0.2561
|
|
104.74 0.6703 0.8121 0.0593 0.0490 3.983 22.821 11.582 2969.972 2.578 51.516 1.769 0.67 307884. 0.2355
|
|
109.97 0.7038 0.8225 0.0531 0.0454 3.692 21.157 10.357 2753.395 2.390 46.066 1.706 0.67 309067. 0.2148
|
|
115.21 0.7373 0.8295 0.0466 0.0415 3.372 19.320 9.105 2514.415 2.183 40.499 1.642 0.67 310295. 0.1939
|
|
120.45 0.7709 0.8323 0.0401 0.0372 3.022 17.316 7.832 2253.570 1.956 34.836 1.576 0.67 311568. 0.1726
|
|
125.68 0.8044 0.8292 0.0335 0.0325 2.644 15.148 6.541 1971.422 1.711 29.095 1.505 0.68 312886. 0.1506
|
|
130.92 0.8379 0.8170 0.0268 0.0275 2.238 12.822 5.237 1668.662 1.449 23.295 1.424 0.68 314247. 0.1274
|
|
136.16 0.8714 0.7893 0.0201 0.0222 1.805 10.344 3.925 1346.201 1.169 17.457 1.322 0.68 315651. 0.1025
|
|
141.39 0.9049 0.7296 0.0134 0.0166 1.348 7.725 2.609 1005.330 0.873 11.605 1.177 0.68 317098. 0.0744
|
|
146.63 0.9384 0.5837 0.0066 0.0107 0.869 4.978 1.297 647.835 0.562 5.768 0.908 0.68 318587. 0.0404
|
|
151.87 0.9719 -0.0097 0.0000 0.0045 0.369 2.111 -0.009 274.795 0.239 -0.039 -0.014 0.69 320072. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 12000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1217 0.0502 5.297 27.824 28.262 3950.283 3.144 125.712 3.245 0.71 320792. 0.6748
|
|
5.71 0.0335 0.0788 0.1212 0.0516 5.444 28.595 28.150 4059.791 3.231 125.211 3.145 0.71 321084. 0.6527
|
|
11.43 0.0670 0.1525 0.1206 0.0530 5.598 29.403 28.015 4174.523 3.322 124.610 3.044 0.71 321414. 0.6302
|
|
17.14 0.1006 0.2211 0.1199 0.0545 5.757 30.236 27.851 4292.690 3.416 123.880 2.943 0.71 321785. 0.6075
|
|
22.85 0.1341 0.2848 0.1190 0.0560 5.917 31.077 27.650 4412.125 3.511 122.988 2.842 0.71 322200. 0.5847
|
|
28.57 0.1676 0.3436 0.1180 0.0575 6.075 31.909 27.405 4530.206 3.605 121.896 2.744 0.72 322661. 0.5619
|
|
34.28 0.2011 0.3978 0.1167 0.0590 6.228 32.710 27.105 4643.909 3.696 120.564 2.647 0.72 323172. 0.5392
|
|
39.99 0.2346 0.4477 0.1151 0.0603 6.370 33.456 26.743 4749.890 3.780 118.953 2.554 0.72 323733. 0.5166
|
|
45.71 0.2681 0.4936 0.1132 0.0615 6.497 34.123 26.309 4844.566 3.855 117.024 2.463 0.72 324347. 0.4942
|
|
51.42 0.3017 0.5356 0.1110 0.0625 6.603 34.684 25.796 4924.211 3.919 114.739 2.376 0.72 325013. 0.4721
|
|
57.13 0.3352 0.5742 0.1084 0.0633 6.685 35.112 25.195 4985.061 3.967 112.066 2.292 0.72 325734. 0.4501
|
|
62.85 0.3687 0.6095 0.1055 0.0638 6.736 35.382 24.501 5023.398 3.997 108.979 2.212 0.72 326510. 0.4283
|
|
68.56 0.4022 0.6418 0.1020 0.0640 6.753 35.468 23.708 5035.587 4.007 105.454 2.135 0.72 327339. 0.4067
|
|
74.27 0.4357 0.6714 0.0982 0.0637 6.729 35.345 22.814 5018.112 3.993 101.477 2.062 0.72 328223. 0.3853
|
|
79.98 0.4692 0.6985 0.0939 0.0631 6.662 34.990 21.816 4967.718 3.953 97.038 1.992 0.72 329159. 0.3639
|
|
85.70 0.5028 0.7231 0.0892 0.0620 6.547 34.386 20.717 4881.873 3.885 92.148 1.925 0.72 330149. 0.3427
|
|
91.41 0.5363 0.7456 0.0840 0.0604 6.383 33.524 19.524 4759.566 3.788 86.843 1.861 0.72 331191. 0.3216
|
|
97.12 0.5698 0.7660 0.0786 0.0584 6.171 32.410 18.250 4601.408 3.662 81.177 1.799 0.73 332284. 0.3006
|
|
102.84 0.6033 0.7843 0.0728 0.0560 5.912 31.054 16.909 4408.837 3.508 75.212 1.740 0.73 333427. 0.2798
|
|
108.55 0.6368 0.8004 0.0668 0.0531 5.610 29.466 15.512 4183.373 3.329 68.997 1.682 0.73 334621. 0.2591
|
|
114.26 0.6703 0.8141 0.0606 0.0499 5.265 27.655 14.068 3926.271 3.124 62.575 1.625 0.73 335865. 0.2384
|
|
119.98 0.7039 0.8252 0.0542 0.0462 4.879 25.628 12.585 3638.515 2.895 55.979 1.569 0.73 337158. 0.2177
|
|
125.69 0.7374 0.8331 0.0476 0.0422 4.453 23.391 11.069 3320.877 2.643 49.236 1.512 0.73 338500. 0.1968
|
|
131.40 0.7709 0.8369 0.0410 0.0378 3.988 20.948 9.526 2974.084 2.367 42.370 1.453 0.74 339890. 0.1754
|
|
137.12 0.8044 0.8350 0.0343 0.0330 3.485 18.306 7.959 2599.028 2.068 35.404 1.389 0.74 341329. 0.1533
|
|
142.83 0.8379 0.8243 0.0274 0.0279 2.946 15.474 6.376 2196.883 1.748 28.360 1.316 0.74 342815. 0.1300
|
|
148.54 0.8715 0.7981 0.0206 0.0225 2.373 12.462 4.780 1769.257 1.408 21.263 1.226 0.74 344348. 0.1048
|
|
154.26 0.9050 0.7397 0.0137 0.0167 1.768 9.286 3.180 1318.420 1.049 14.143 1.094 0.74 345928. 0.0763
|
|
159.97 0.9385 0.5935 0.0068 0.0108 1.136 5.969 1.581 847.446 0.674 7.033 0.846 0.75 347552. 0.0416
|
|
165.68 0.9720 -0.0107 0.0000 0.0046 0.481 2.526 -0.012 358.576 0.285 -0.052 -0.015 0.75 349169. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 13000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1222 0.0529 7.109 34.466 33.315 5300.982 3.894 148.185 2.851 0.77 347502. 0.6436
|
|
6.19 0.0335 0.0751 0.1218 0.0543 7.292 35.354 33.204 5437.565 3.994 147.690 2.770 0.77 347816. 0.6243
|
|
12.38 0.0670 0.1458 0.1213 0.0557 7.484 36.285 33.070 5580.774 4.099 147.094 2.688 0.77 348171. 0.6046
|
|
18.56 0.1005 0.2120 0.1207 0.0572 7.682 37.243 32.906 5728.146 4.208 146.364 2.606 0.77 348570. 0.5847
|
|
24.75 0.1340 0.2739 0.1199 0.0587 7.881 38.208 32.702 5876.614 4.317 145.460 2.524 0.77 349017. 0.5646
|
|
30.94 0.1675 0.3315 0.1190 0.0602 8.076 39.157 32.449 6022.487 4.424 144.334 2.444 0.77 349515. 0.5446
|
|
37.13 0.2011 0.3850 0.1179 0.0615 8.263 40.061 32.135 6161.586 4.526 142.935 2.366 0.78 350066. 0.5245
|
|
43.31 0.2346 0.4347 0.1164 0.0628 8.434 40.892 31.747 6289.419 4.620 141.209 2.289 0.78 350672. 0.5046
|
|
49.50 0.2681 0.4809 0.1147 0.0639 8.584 41.620 31.273 6401.395 4.702 139.103 2.216 0.78 351336. 0.4847
|
|
55.69 0.3016 0.5236 0.1126 0.0649 8.707 42.215 30.704 6492.890 4.769 136.569 2.145 0.78 352058. 0.4649
|
|
61.88 0.3351 0.5633 0.1101 0.0655 8.796 42.647 30.027 6559.379 4.818 133.562 2.076 0.78 352839. 0.4451
|
|
68.07 0.3686 0.5999 0.1072 0.0659 8.846 42.888 29.237 6596.461 4.846 130.045 2.010 0.78 353679. 0.4252
|
|
74.25 0.4021 0.6337 0.1039 0.0659 8.851 42.911 28.324 6599.935 4.848 125.987 1.947 0.78 354579. 0.4052
|
|
80.44 0.4356 0.6647 0.1001 0.0656 8.805 42.689 27.286 6565.793 4.823 121.369 1.885 0.78 355538. 0.3852
|
|
86.63 0.4691 0.6932 0.0958 0.0648 8.704 42.198 26.120 6490.318 4.768 116.180 1.825 0.78 356555. 0.3649
|
|
92.82 0.5026 0.7193 0.0911 0.0636 8.543 41.419 24.827 6370.528 4.680 110.430 1.768 0.78 357630. 0.3445
|
|
99.00 0.5361 0.7429 0.0859 0.0620 8.321 40.344 23.418 6205.168 4.558 104.162 1.712 0.78 358761. 0.3240
|
|
105.19 0.5697 0.7644 0.0803 0.0599 8.039 38.977 21.907 5994.850 4.404 97.444 1.658 0.79 359947. 0.3035
|
|
111.38 0.6032 0.7836 0.0745 0.0573 7.699 37.327 20.312 5741.073 4.217 90.349 1.605 0.79 361189. 0.2829
|
|
117.57 0.6367 0.8005 0.0684 0.0544 7.302 35.405 18.646 5445.405 4.000 82.939 1.553 0.79 362485. 0.2623
|
|
123.76 0.6702 0.8150 0.0621 0.0510 6.851 33.218 16.922 5109.159 3.753 75.268 1.502 0.79 363834. 0.2417
|
|
129.94 0.7037 0.8269 0.0556 0.0473 6.348 30.776 15.148 4733.584 3.477 67.378 1.451 0.79 365237. 0.2210
|
|
136.13 0.7372 0.8354 0.0489 0.0431 5.793 28.086 13.332 4319.716 3.173 59.302 1.400 0.79 366692. 0.1999
|
|
142.32 0.7707 0.8398 0.0421 0.0386 5.188 25.154 11.481 3868.885 2.842 51.069 1.346 0.80 368200. 0.1784
|
|
148.51 0.8042 0.8381 0.0352 0.0338 4.537 21.995 9.601 3382.956 2.485 42.705 1.287 0.80 369759. 0.1560
|
|
154.69 0.8377 0.8265 0.0282 0.0286 3.841 18.624 7.697 2864.443 2.104 34.236 1.219 0.80 371370. 0.1323
|
|
160.88 0.8712 0.7976 0.0212 0.0231 3.107 15.062 5.776 2316.656 1.702 25.691 1.131 0.80 373031. 0.1063
|
|
167.07 0.9048 0.7324 0.0141 0.0174 2.339 11.339 3.845 1743.963 1.281 17.102 1.000 0.80 374742. 0.0767
|
|
173.26 0.9383 0.5722 0.0070 0.0115 1.545 7.490 1.913 1151.959 0.846 8.511 0.753 0.81 376502. 0.0408
|
|
179.45 0.9718 -0.0093 -0.0001 0.0054 0.731 3.546 -0.014 545.453 0.401 -0.063 -0.012 0.81 378258. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 14000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1226 0.0584 9.793 44.088 38.758 7302.585 4.981 172.395 2.407 0.83 374207. 0.5862
|
|
6.67 0.0335 0.0686 0.1222 0.0597 10.018 45.100 38.650 7470.167 5.095 171.915 2.347 0.83 374543. 0.5707
|
|
13.34 0.0671 0.1336 0.1218 0.0612 10.254 46.163 38.522 7646.327 5.216 171.346 2.285 0.83 374923. 0.5548
|
|
20.00 0.1006 0.1950 0.1213 0.0626 10.497 47.258 38.366 7827.710 5.339 170.651 2.223 0.83 375350. 0.5386
|
|
26.67 0.1341 0.2527 0.1207 0.0641 10.741 48.358 38.171 8009.848 5.463 169.782 2.161 0.83 375829. 0.5224
|
|
33.34 0.1677 0.3071 0.1199 0.0655 10.979 49.428 37.924 8187.103 5.584 168.684 2.101 0.83 376361. 0.5061
|
|
40.01 0.2012 0.3582 0.1189 0.0668 11.201 50.429 37.610 8352.913 5.697 167.289 2.042 0.83 376952. 0.4899
|
|
46.68 0.2347 0.4063 0.1177 0.0680 11.399 51.319 37.214 8500.226 5.798 165.526 1.986 0.84 377603. 0.4738
|
|
53.34 0.2682 0.4517 0.1161 0.0690 11.563 52.055 36.718 8622.268 5.881 163.323 1.932 0.84 378316. 0.4578
|
|
60.01 0.3018 0.4945 0.1142 0.0697 11.684 52.603 36.109 8712.902 5.943 160.612 1.880 0.84 379093. 0.4418
|
|
66.68 0.3353 0.5350 0.1119 0.0701 11.756 52.928 35.372 8766.785 5.980 157.332 1.830 0.84 379935. 0.4258
|
|
73.35 0.3688 0.5731 0.1091 0.0702 11.773 53.003 34.495 8779.308 5.988 153.433 1.782 0.84 380843. 0.4094
|
|
80.02 0.4024 0.6089 0.1058 0.0699 11.729 52.804 33.470 8746.330 5.966 148.873 1.736 0.84 381815. 0.3928
|
|
86.69 0.4359 0.6424 0.1021 0.0693 11.618 52.307 32.289 8663.882 5.910 143.620 1.690 0.84 382851. 0.3757
|
|
93.35 0.4694 0.6736 0.0979 0.0682 11.437 51.489 30.949 8528.400 5.817 137.660 1.646 0.84 383951. 0.3582
|
|
100.02 0.5030 0.7026 0.0931 0.0667 11.181 50.336 29.452 8337.551 5.687 131.002 1.602 0.84 385113. 0.3401
|
|
106.69 0.5365 0.7292 0.0879 0.0647 10.850 48.848 27.810 8090.937 5.519 123.698 1.559 0.85 386336. 0.3216
|
|
113.36 0.5700 0.7535 0.0824 0.0623 10.447 47.033 26.041 7790.340 5.314 115.831 1.516 0.85 387620. 0.3027
|
|
120.03 0.6036 0.7754 0.0764 0.0595 9.975 44.907 24.166 7438.308 5.074 107.491 1.474 0.85 388962. 0.2834
|
|
126.69 0.6371 0.7948 0.0702 0.0563 9.437 42.483 22.202 7036.818 4.800 98.755 1.431 0.85 390363. 0.2638
|
|
133.36 0.6706 0.8117 0.0638 0.0527 8.834 39.769 20.163 6587.275 4.493 89.686 1.388 0.85 391822. 0.2439
|
|
140.03 0.7041 0.8253 0.0571 0.0487 8.172 36.788 18.061 6093.505 4.156 80.336 1.344 0.85 393338. 0.2235
|
|
146.70 0.7377 0.8345 0.0503 0.0445 7.456 33.565 15.905 5559.667 3.792 70.745 1.298 0.86 394910. 0.2024
|
|
153.37 0.7712 0.8374 0.0433 0.0399 6.691 30.125 13.702 4989.738 3.403 60.946 1.246 0.86 396538. 0.1803
|
|
160.03 0.8047 0.8322 0.0362 0.0350 5.877 26.457 11.461 4382.274 2.989 50.976 1.186 0.86 398221. 0.1571
|
|
166.70 0.8383 0.8140 0.0291 0.0299 5.018 22.589 9.188 3741.628 2.552 40.867 1.114 0.86 399960. 0.1321
|
|
173.37 0.8718 0.7727 0.0218 0.0246 4.123 18.562 6.892 3074.528 2.097 30.654 1.017 0.86 401753. 0.1044
|
|
180.04 0.9053 0.6866 0.0145 0.0191 3.204 14.423 4.582 2388.918 1.629 20.380 0.870 0.87 403599. 0.0728
|
|
186.71 0.9389 0.4977 0.0072 0.0135 2.272 10.227 2.271 1693.967 1.155 10.101 0.608 0.87 405498. 0.0358
|
|
193.37 0.9724 -0.0121 -0.0001 0.0080 1.338 6.022 -0.031 997.431 0.680 -0.140 -0.014 0.87 407408. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 15000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1219 0.0655 13.501 56.729 44.259 10067.613 6.409 196.863 1.994 0.89 400952. 0.5189
|
|
7.16 0.0336 0.0612 0.1216 0.0668 13.778 57.892 44.155 10273.930 6.541 196.401 1.949 0.89 401309. 0.5067
|
|
14.32 0.0672 0.1195 0.1213 0.0682 14.072 59.129 44.035 10493.444 6.680 195.869 1.903 0.89 401713. 0.4941
|
|
21.48 0.1008 0.1749 0.1209 0.0697 14.379 60.419 43.892 10722.390 6.826 195.233 1.857 0.89 402167. 0.4812
|
|
28.64 0.1344 0.2273 0.1204 0.0712 14.691 61.732 43.716 10955.430 6.974 194.447 1.810 0.89 402675. 0.4681
|
|
35.81 0.1680 0.2768 0.1198 0.0727 15.000 63.027 43.492 11185.269 7.121 193.451 1.764 0.89 403242. 0.4550
|
|
42.97 0.2017 0.3237 0.1190 0.0741 15.291 64.252 43.204 11402.569 7.259 192.171 1.719 0.89 403869. 0.4419
|
|
50.13 0.2353 0.3682 0.1180 0.0754 15.551 65.343 42.832 11596.307 7.382 190.519 1.675 0.89 404561. 0.4289
|
|
57.29 0.2689 0.4105 0.1167 0.0764 15.763 66.234 42.356 11754.410 7.483 188.400 1.634 0.90 405320. 0.4161
|
|
64.45 0.3025 0.4510 0.1150 0.0771 15.911 66.857 41.752 11864.974 7.553 185.714 1.596 0.90 406150. 0.4034
|
|
71.61 0.3361 0.4899 0.1129 0.0775 15.982 67.154 41.000 11917.587 7.587 182.368 1.560 0.90 407050. 0.3908
|
|
78.77 0.3697 0.5274 0.1104 0.0774 15.964 67.079 40.081 11904.335 7.579 178.281 1.527 0.90 408023. 0.3782
|
|
85.93 0.4033 0.5635 0.1074 0.0769 15.850 66.601 38.980 11819.465 7.525 173.385 1.496 0.90 409067. 0.3653
|
|
93.09 0.4369 0.5983 0.1038 0.0758 15.635 65.698 37.687 11659.329 7.423 167.630 1.466 0.90 410182. 0.3521
|
|
100.25 0.4705 0.6316 0.0997 0.0743 15.319 64.369 36.195 11423.360 7.272 160.996 1.437 0.90 411366. 0.3382
|
|
107.42 0.5041 0.6633 0.0951 0.0723 14.901 62.613 34.508 11111.743 7.074 153.492 1.409 0.90 412619. 0.3237
|
|
114.58 0.5377 0.6932 0.0899 0.0697 14.385 60.445 32.638 10726.973 6.829 145.173 1.380 0.91 413939. 0.3084
|
|
121.74 0.5714 0.7212 0.0843 0.0668 13.777 57.890 30.607 10273.669 6.540 136.138 1.351 0.91 415324. 0.2924
|
|
128.90 0.6050 0.7470 0.0783 0.0634 13.084 54.979 28.438 9756.988 6.211 126.494 1.322 0.91 416772. 0.2758
|
|
136.06 0.6386 0.7707 0.0721 0.0597 12.313 51.739 26.155 9181.977 5.845 116.338 1.292 0.91 418284. 0.2585
|
|
143.22 0.6722 0.7917 0.0655 0.0556 11.469 48.192 23.776 8552.467 5.445 105.755 1.261 0.91 419858. 0.2405
|
|
150.38 0.7058 0.8097 0.0587 0.0512 10.556 44.356 21.316 7871.764 5.011 94.815 1.228 0.91 421493. 0.2218
|
|
157.54 0.7394 0.8218 0.0517 0.0466 9.603 40.349 18.784 7160.596 4.559 83.552 1.190 0.92 423188. 0.2017
|
|
164.70 0.7730 0.8229 0.0446 0.0419 8.638 36.295 16.185 6441.246 4.101 71.992 1.140 0.92 424943. 0.1794
|
|
171.87 0.8066 0.8083 0.0373 0.0372 7.670 32.230 13.529 5719.865 3.641 60.178 1.073 0.92 426758. 0.1544
|
|
179.03 0.8402 0.7751 0.0298 0.0324 6.673 28.038 10.834 4975.752 3.168 48.191 0.988 0.92 428631. 0.1272
|
|
186.19 0.8738 0.7119 0.0224 0.0274 5.658 23.776 8.114 4219.447 2.686 36.090 0.872 0.93 430562. 0.0972
|
|
193.35 0.9074 0.5979 0.0148 0.0225 4.643 19.511 5.385 3462.542 2.204 23.952 0.705 0.93 432550. 0.0640
|
|
200.51 0.9411 0.3923 0.0074 0.0177 3.643 15.307 2.673 2716.513 1.729 11.888 0.446 0.93 434594. 0.0285
|
|
207.67 0.9747 0.0003 0.0000 0.0129 2.667 11.204 0.001 1988.424 1.266 0.006 0.000 0.93 436672. 0.0000
|
|
|
|
|
|
|