427 lines
76 KiB
Plaintext
427 lines
76 KiB
Plaintext
21x12WE (21x12WE.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 0.0957 0.0368 0.012 0.762 0.593 9.021 0.086 2.637 29.809 0.08 44141. 0.6413
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0.49 0.0248 0.0627 0.0942 0.0373 0.012 0.772 0.584 9.131 0.087 2.597 29.004 0.08 44172. 0.6193
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0.99 0.0496 0.1219 0.0926 0.0377 0.012 0.780 0.574 9.234 0.088 2.554 28.203 0.08 44205. 0.5971
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1.48 0.0744 0.1777 0.0909 0.0381 0.013 0.788 0.564 9.327 0.089 2.507 27.410 0.08 44240. 0.5750
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1.97 0.0992 0.2302 0.0891 0.0384 0.013 0.795 0.552 9.409 0.090 2.457 26.625 0.08 44279. 0.5529
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2.47 0.1240 0.2794 0.0871 0.0387 0.013 0.801 0.540 9.477 0.090 2.402 25.850 0.08 44321. 0.5308
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2.96 0.1488 0.3253 0.0850 0.0389 0.013 0.805 0.527 9.528 0.091 2.344 25.086 0.08 44365. 0.5088
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3.45 0.1735 0.3682 0.0828 0.0390 0.013 0.808 0.513 9.560 0.091 2.282 24.335 0.08 44413. 0.4870
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3.94 0.1983 0.4080 0.0803 0.0391 0.013 0.809 0.498 9.571 0.091 2.215 23.596 0.08 44465. 0.4652
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4.44 0.2231 0.4448 0.0777 0.0390 0.013 0.808 0.482 9.557 0.091 2.143 22.868 0.08 44519. 0.4435
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4.93 0.2479 0.4788 0.0750 0.0388 0.013 0.804 0.465 9.516 0.091 2.067 22.152 0.08 44577. 0.4220
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5.42 0.2727 0.5099 0.0721 0.0385 0.013 0.798 0.447 9.446 0.090 1.987 21.446 0.08 44639. 0.4005
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5.92 0.2975 0.5381 0.0690 0.0381 0.013 0.790 0.427 9.344 0.089 1.901 20.748 0.08 44704. 0.3790
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6.41 0.3223 0.5635 0.0657 0.0376 0.012 0.778 0.407 9.207 0.088 1.811 20.055 0.08 44773. 0.3575
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6.90 0.3471 0.5860 0.0622 0.0369 0.012 0.764 0.386 9.034 0.086 1.716 19.366 0.08 44845. 0.3361
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7.40 0.3719 0.6054 0.0586 0.0360 0.012 0.746 0.363 8.824 0.084 1.616 18.675 0.08 44921. 0.3145
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7.89 0.3967 0.6217 0.0549 0.0350 0.012 0.725 0.340 8.578 0.082 1.512 17.978 0.08 45001. 0.2929
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8.38 0.4215 0.6345 0.0510 0.0339 0.011 0.701 0.316 8.298 0.079 1.405 17.269 0.08 45084. 0.2712
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8.87 0.4463 0.6435 0.0470 0.0326 0.011 0.675 0.291 7.983 0.076 1.295 16.541 0.08 45172. 0.2494
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9.37 0.4710 0.6483 0.0429 0.0312 0.010 0.645 0.266 7.634 0.073 1.182 15.785 0.08 45262. 0.2274
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9.86 0.4958 0.6481 0.0387 0.0296 0.010 0.613 0.240 7.254 0.069 1.066 14.992 0.08 45357. 0.2051
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10.35 0.5206 0.6421 0.0344 0.0279 0.009 0.578 0.213 6.841 0.065 0.949 14.146 0.08 45455. 0.1826
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10.85 0.5454 0.6291 0.0301 0.0261 0.009 0.541 0.187 6.398 0.061 0.830 13.229 0.08 45557. 0.1597
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11.34 0.5702 0.6073 0.0258 0.0242 0.008 0.501 0.160 5.927 0.057 0.710 12.217 0.08 45663. 0.1364
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11.83 0.5950 0.5744 0.0214 0.0221 0.007 0.459 0.133 5.427 0.052 0.589 11.074 0.08 45773. 0.1126
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12.33 0.6198 0.5267 0.0170 0.0200 0.007 0.414 0.105 4.903 0.047 0.469 9.747 0.08 45886. 0.0884
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12.82 0.6446 0.4584 0.0126 0.0178 0.006 0.368 0.078 4.356 0.042 0.348 8.157 0.09 46004. 0.0638
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13.31 0.6694 0.3601 0.0083 0.0155 0.005 0.320 0.052 3.788 0.036 0.229 6.171 0.09 46125. 0.0391
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13.80 0.6942 0.2155 0.0041 0.0131 0.004 0.271 0.025 3.205 0.031 0.112 3.562 0.09 46250. 0.0158
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14.30 0.7190 -0.0074 -0.0001 0.0106 0.003 0.220 -0.001 2.608 0.025 -0.003 -0.118 0.09 46377. 0.0000
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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 0.0960 0.0344 0.091 2.853 2.381 67.507 0.322 10.591 15.999 0.17 88281. 0.6898
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1.00 0.0252 0.0683 0.0946 0.0349 0.092 2.894 2.345 68.471 0.327 10.430 15.533 0.17 88343. 0.6646
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2.01 0.0504 0.1325 0.0930 0.0354 0.093 2.932 2.305 69.377 0.331 10.254 15.072 0.17 88410. 0.6394
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3.01 0.0756 0.1928 0.0913 0.0358 0.094 2.967 2.263 70.205 0.335 10.064 14.617 0.17 88483. 0.6143
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4.01 0.1009 0.2492 0.0894 0.0362 0.095 2.998 2.216 70.937 0.339 9.858 14.171 0.17 88562. 0.5895
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5.01 0.1261 0.3019 0.0874 0.0365 0.096 3.024 2.166 71.552 0.342 9.636 13.733 0.17 88647. 0.5648
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6.02 0.1513 0.3509 0.0852 0.0367 0.097 3.044 2.113 72.026 0.344 9.398 13.305 0.17 88739. 0.5404
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7.02 0.1765 0.3965 0.0829 0.0369 0.097 3.057 2.055 72.339 0.345 9.141 12.886 0.17 88837. 0.5162
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8.02 0.2017 0.4388 0.0804 0.0370 0.097 3.063 1.993 72.467 0.346 8.867 12.477 0.17 88942. 0.4922
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9.03 0.2269 0.4779 0.0778 0.0369 0.097 3.059 1.928 72.388 0.346 8.574 12.078 0.17 89055. 0.4685
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10.03 0.2521 0.5138 0.0749 0.0368 0.097 3.046 1.857 72.079 0.344 8.262 11.688 0.17 89174. 0.4451
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11.03 0.2773 0.5468 0.0719 0.0365 0.096 3.022 1.783 71.518 0.341 7.930 11.306 0.17 89301. 0.4218
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12.03 0.3026 0.5768 0.0687 0.0361 0.095 2.987 1.704 70.682 0.337 7.578 10.933 0.17 89435. 0.3987
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13.04 0.3278 0.6038 0.0653 0.0355 0.093 2.939 1.620 69.544 0.332 7.206 10.566 0.17 89576. 0.3757
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14.04 0.3530 0.6280 0.0618 0.0347 0.091 2.878 1.532 68.092 0.325 6.814 10.204 0.17 89725. 0.3529
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15.04 0.3782 0.6492 0.0581 0.0338 0.089 2.803 1.440 66.326 0.317 6.403 9.845 0.17 89882. 0.3300
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16.04 0.4034 0.6673 0.0542 0.0328 0.086 2.715 1.344 64.250 0.307 5.977 9.487 0.17 90046. 0.3073
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17.05 0.4286 0.6820 0.0502 0.0316 0.083 2.615 1.245 61.871 0.295 5.537 9.126 0.17 90218. 0.2845
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18.05 0.4538 0.6931 0.0461 0.0302 0.079 2.502 1.143 59.194 0.283 5.084 8.759 0.17 90398. 0.2616
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19.05 0.4791 0.7000 0.0419 0.0287 0.075 2.376 1.039 56.224 0.268 4.621 8.380 0.17 90585. 0.2387
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20.06 0.5043 0.7021 0.0376 0.0270 0.071 2.239 0.933 52.970 0.253 4.148 7.986 0.17 90780. 0.2155
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21.06 0.5295 0.6985 0.0333 0.0252 0.066 2.089 0.825 49.438 0.236 3.668 7.566 0.17 90983. 0.1920
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22.06 0.5547 0.6878 0.0289 0.0233 0.061 1.929 0.716 45.641 0.218 3.183 7.111 0.17 91193. 0.1681
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23.06 0.5799 0.6679 0.0244 0.0212 0.056 1.758 0.606 41.589 0.199 2.694 6.605 0.17 91411. 0.1436
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24.07 0.6051 0.6356 0.0200 0.0190 0.050 1.576 0.495 37.299 0.178 2.203 6.024 0.17 91638. 0.1185
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25.07 0.6303 0.5857 0.0155 0.0167 0.044 1.386 0.385 32.792 0.157 1.714 5.329 0.17 91872. 0.0924
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26.07 0.6555 0.5093 0.0111 0.0143 0.038 1.187 0.276 28.090 0.134 1.227 4.456 0.17 92114. 0.0654
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27.08 0.6808 0.3896 0.0068 0.0118 0.031 0.981 0.168 23.223 0.111 0.747 3.282 0.17 92363. 0.0376
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28.08 0.7060 0.1904 0.0025 0.0093 0.024 0.770 0.062 18.224 0.087 0.276 1.547 0.17 92620. 0.0108
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29.08 0.7312
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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 0.0965 0.0335 0.297 6.249 5.383 221.815 0.706 23.945 11.008 0.25 132417. 0.7136
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1.49 0.0249 0.0696 0.0951 0.0340 0.302 6.343 5.303 225.144 0.717 23.587 10.683 0.25 132509. 0.6874
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2.97 0.0498 0.1350 0.0935 0.0345 0.306 6.432 5.215 228.286 0.727 23.198 10.362 0.25 132609. 0.6612
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4.46 0.0747 0.1963 0.0918 0.0349 0.310 6.513 5.121 231.175 0.736 22.777 10.047 0.25 132717. 0.6352
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5.94 0.0996 0.2537 0.0900 0.0353 0.313 6.586 5.018 233.747 0.744 22.322 9.738 0.25 132834. 0.6095
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7.43 0.1245 0.3073 0.0880 0.0357 0.316 6.647 4.908 235.933 0.751 21.831 9.435 0.25 132960. 0.5841
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8.91 0.1494 0.3572 0.0859 0.0359 0.319 6.696 4.789 237.660 0.756 21.303 9.140 0.25 133095. 0.5589
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10.40 0.1743 0.4036 0.0836 0.0361 0.320 6.729 4.662 238.853 0.760 20.736 8.852 0.25 133240. 0.5341
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11.89 0.1992 0.4467 0.0811 0.0362 0.321 6.746 4.525 239.438 0.762 20.128 8.572 0.25 133395. 0.5095
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13.37 0.2241 0.4866 0.0785 0.0362 0.321 6.743 4.379 239.338 0.762 19.480 8.300 0.25 133560. 0.4853
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14.86 0.2491 0.5233 0.0757 0.0360 0.320 6.719 4.224 238.477 0.759 18.789 8.034 0.25 133736. 0.4614
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16.34 0.2740 0.5571 0.0728 0.0358 0.318 6.671 4.059 236.784 0.754 18.055 7.776 0.25 133923. 0.4377
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17.83 0.2989 0.5881 0.0696 0.0354 0.314 6.598 3.884 234.178 0.745 17.278 7.523 0.25 134120. 0.4143
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19.32 0.3238 0.6162 0.0663 0.0348 0.309 6.496 3.699 230.576 0.734 16.454 7.277 0.25 134328. 0.3911
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20.80 0.3487 0.6415 0.0628 0.0341 0.303 6.365 3.504 225.918 0.719 15.586 7.035 0.25 134547. 0.3680
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22.29 0.3736 0.6641 0.0592 0.0333 0.295 6.204 3.300 220.199 0.701 14.678 6.797 0.25 134777. 0.3450
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23.77 0.3985 0.6838 0.0554 0.0323 0.286 6.013 3.087 213.432 0.679 13.733 6.561 0.25 135019. 0.3221
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25.26 0.4234 0.7005 0.0514 0.0311 0.276 5.794 2.868 205.632 0.655 12.756 6.326 0.25 135271. 0.2993
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26.74 0.4483 0.7139 0.0474 0.0297 0.264 5.545 2.642 196.817 0.626 11.751 6.088 0.25 135535. 0.2765
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28.23 0.4732 0.7236 0.0432 0.0283 0.251 5.269 2.410 187.003 0.595 10.722 5.847 0.25 135810. 0.2536
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29.72 0.4981 0.7291 0.0390 0.0266 0.236 4.965 2.174 176.213 0.561 9.671 5.597 0.25 136097. 0.2306
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31.20 0.5230 0.7297 0.0347 0.0249 0.221 4.634 1.934 164.472 0.524 8.604 5.334 0.25 136394. 0.2073
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32.69 0.5479 0.7242 0.0303 0.0229 0.204 4.277 1.691 151.812 0.483 7.523 5.053 0.25 136703. 0.1836
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34.17 0.5728 0.7109 0.0259 0.0209 0.185 3.896 1.446 138.272 0.440 6.434 4.745 0.25 137024. 0.1594
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35.66 0.5977 0.6870 0.0215 0.0187 0.166 3.491 1.201 123.902 0.394 5.340 4.395 0.25 137356. 0.1345
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37.15 0.6226 0.6483 0.0171 0.0164 0.146 3.064 0.955 108.765 0.346 4.247 3.981 0.25 137699. 0.1087
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38.63 0.6475 0.5870 0.0127 0.0140 0.125 2.618 0.710 92.937 0.296 3.159 3.466 0.26 138054. 0.0816
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40.12 0.6724 0.4884 0.0084 0.0116 0.103 2.156 0.468 76.511 0.244 2.083 2.777 0.26 138420. 0.0531
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41.60 0.6973 0.3203 0.0041 0.0090 0.080 1.679 0.231 59.596 0.190 1.026 1.756 0.26 138797. 0.0236
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43.09 0.7222 -0.0043 0.0000 0.0064 0.057 1.190 -0.002 42.253 0.134 -0.009 -0.023 0.26 139179. 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 0.0971 0.0331 0.697 10.985 9.630 519.848 1.241 42.834 8.402 0.33 176548. 0.7285
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1.98 0.0249 0.0708 0.0957 0.0337 0.708 11.156 9.487 527.950 1.260 42.199 8.151 0.33 176671. 0.7015
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3.96 0.0498 0.1374 0.0941 0.0341 0.718 11.318 9.332 535.608 1.279 41.509 7.903 0.33 176804. 0.6745
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5.95 0.0748 0.1997 0.0924 0.0346 0.728 11.467 9.164 542.662 1.296 40.760 7.659 0.33 176949. 0.6478
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7.93 0.0997 0.2580 0.0906 0.0350 0.736 11.600 8.982 548.955 1.311 39.951 7.421 0.33 177105. 0.6214
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9.91 0.1246 0.3124 0.0886 0.0353 0.743 11.713 8.785 554.320 1.323 39.077 7.189 0.33 177274. 0.5953
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11.89 0.1495 0.3630 0.0865 0.0356 0.749 11.803 8.574 558.583 1.334 38.136 6.962 0.33 177455. 0.5696
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13.88 0.1744 0.4101 0.0842 0.0358 0.753 11.866 8.347 561.561 1.341 37.125 6.741 0.33 177649. 0.5442
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15.86 0.1994 0.4538 0.0817 0.0359 0.755 11.898 8.103 563.073 1.344 36.042 6.527 0.33 177856. 0.5191
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17.84 0.2243 0.4942 0.0791 0.0359 0.755 11.895 7.843 562.934 1.344 34.884 6.319 0.33 178077. 0.4945
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19.82 0.2492 0.5316 0.0763 0.0358 0.752 11.853 7.565 560.962 1.339 33.650 6.117 0.33 178312. 0.4701
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21.81 0.2741 0.5660 0.0733 0.0355 0.747 11.769 7.270 556.978 1.330 32.338 5.920 0.33 178561. 0.4460
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23.79 0.2990 0.5975 0.0702 0.0351 0.739 11.639 6.958 550.795 1.315 30.947 5.729 0.33 178825. 0.4223
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25.77 0.3240 0.6262 0.0668 0.0346 0.727 11.457 6.626 542.206 1.294 29.474 5.543 0.33 179103. 0.3987
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27.75 0.3489 0.6523 0.0633 0.0339 0.712 11.222 6.277 531.064 1.268 27.920 5.361 0.34 179396. 0.3753
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29.73 0.3738 0.6756 0.0596 0.0330 0.694 10.932 5.911 517.352 1.235 26.294 5.183 0.34 179704. 0.3521
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31.72 0.3987 0.6961 0.0558 0.0319 0.672 10.588 5.531 501.097 1.196 24.602 5.006 0.34 180026. 0.3290
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33.70 0.4236 0.7137 0.0518 0.0308 0.647 10.192 5.137 482.336 1.151 22.852 4.831 0.34 180364. 0.3060
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35.68 0.4486 0.7282 0.0477 0.0294 0.618 9.743 4.733 461.106 1.101 21.051 4.655 0.34 180716. 0.2830
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37.66 0.4735 0.7392 0.0435 0.0279 0.587 9.244 4.318 437.449 1.044 19.206 4.477 0.34 181084. 0.2599
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39.65 0.4984 0.7463 0.0393 0.0262 0.552 8.693 3.895 411.416 0.982 17.323 4.294 0.34 181466. 0.2368
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41.63 0.5233 0.7486 0.0349 0.0244 0.514 8.094 3.464 383.066 0.915 15.410 4.102 0.34 181864. 0.2133
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43.61 0.5482 0.7452 0.0305 0.0225 0.473 7.448 3.029 352.478 0.841 13.473 3.898 0.34 182276. 0.1895
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45.59 0.5732 0.7344 0.0261 0.0204 0.429 6.756 2.590 319.748 0.763 11.520 3.674 0.34 182704. 0.1652
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47.58 0.5981 0.7134 0.0217 0.0182 0.382 6.022 2.149 284.997 0.680 9.560 3.420 0.34 183147. 0.1401
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49.56 0.6230 0.6779 0.0172 0.0158 0.333 5.248 1.709 248.377 0.593 7.600 3.120 0.34 183606. 0.1140
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51.54 0.6479 0.6199 0.0128 0.0134 0.282 4.439 1.271 210.076 0.502 5.652 2.743 0.34 184079. 0.0864
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53.52 0.6729 0.5233 0.0084 0.0109 0.228 3.599 0.837 170.322 0.407 3.725 2.230 0.34 184568. 0.0570
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55.50 0.6978 0.3513 0.0042 0.0082 0.174 2.734 0.412 129.380 0.309 1.832 1.444 0.34 185072. 0.0259
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57.49 0.7227 -0.0070 -0.0001 0.0056 0.117 1.846 -0.005 87.376 0.209 -0.024 -0.028 0.34 185580. 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 0.0979 0.0331 1.358 17.125 15.166 1013.022 1.935 67.458 6.790 0.42 220672. 0.7389
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2.48 0.0249 0.0715 0.0964 0.0336 1.380 17.398 14.944 1029.222 1.966 66.471 6.586 0.42 220826. 0.7113
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4.95 0.0498 0.1387 0.0949 0.0341 1.401 17.657 14.702 1044.545 1.995 65.396 6.384 0.42 220993. 0.6840
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7.43 0.0747 0.2015 0.0932 0.0346 1.420 17.896 14.440 1058.673 2.022 64.230 6.187 0.42 221174. 0.6569
|
|
9.91 0.0996 0.2603 0.0914 0.0350 1.437 18.110 14.156 1071.295 2.046 62.967 5.994 0.42 221370. 0.6301
|
|
12.39 0.1246 0.3152 0.0894 0.0353 1.451 18.292 13.849 1082.076 2.067 61.601 5.805 0.42 221581. 0.6036
|
|
14.86 0.1495 0.3663 0.0872 0.0356 1.463 18.437 13.518 1090.668 2.083 60.129 5.622 0.42 221808. 0.5775
|
|
17.34 0.1744 0.4138 0.0849 0.0358 1.471 18.539 13.162 1096.711 2.095 58.546 5.444 0.42 222051. 0.5518
|
|
19.82 0.1993 0.4579 0.0825 0.0359 1.475 18.592 12.780 1099.840 2.101 56.847 5.271 0.42 222311. 0.5265
|
|
22.29 0.2242 0.4987 0.0798 0.0359 1.475 18.590 12.372 1099.689 2.100 55.031 5.103 0.42 222587. 0.5015
|
|
24.77 0.2491 0.5365 0.0770 0.0358 1.470 18.526 11.936 1095.898 2.093 53.093 4.940 0.42 222881. 0.4769
|
|
27.25 0.2740 0.5713 0.0740 0.0355 1.459 18.394 11.473 1088.106 2.078 51.032 4.782 0.42 223193. 0.4526
|
|
29.72 0.2989 0.6032 0.0709 0.0351 1.443 18.188 10.981 1075.948 2.055 48.845 4.629 0.42 223523. 0.4286
|
|
32.20 0.3239 0.6325 0.0675 0.0346 1.420 17.902 10.460 1059.013 2.023 46.528 4.480 0.42 223872. 0.4049
|
|
34.68 0.3488 0.6590 0.0640 0.0339 1.391 17.530 9.911 1036.998 1.981 44.083 4.335 0.42 224238. 0.3813
|
|
37.16 0.3737 0.6829 0.0602 0.0330 1.354 17.071 9.335 1009.857 1.929 41.521 4.193 0.42 224623. 0.3579
|
|
39.63 0.3986 0.7042 0.0564 0.0319 1.311 16.527 8.735 977.642 1.867 38.855 4.053 0.42 225027. 0.3347
|
|
42.11 0.4235 0.7226 0.0524 0.0307 1.261 15.897 8.115 940.423 1.796 36.097 3.914 0.42 225449. 0.3115
|
|
44.59 0.4484 0.7380 0.0483 0.0293 1.205 15.185 7.477 898.273 1.716 33.257 3.775 0.42 225890. 0.2884
|
|
47.06 0.4733 0.7500 0.0440 0.0278 1.142 14.390 6.823 851.276 1.626 30.347 3.635 0.42 226349. 0.2653
|
|
49.54 0.4982 0.7583 0.0397 0.0261 1.072 13.516 6.155 799.529 1.527 27.377 3.492 0.42 226827. 0.2420
|
|
52.02 0.5231 0.7622 0.0353 0.0243 0.997 12.563 5.476 743.154 1.419 24.358 3.342 0.42 227324. 0.2185
|
|
54.49 0.5481 0.7605 0.0309 0.0223 0.915 11.534 4.789 682.302 1.303 21.301 3.183 0.42 227840. 0.1947
|
|
56.97 0.5730 0.7518 0.0264 0.0201 0.828 10.433 4.096 617.165 1.179 18.218 3.010 0.42 228375. 0.1702
|
|
59.45 0.5979 0.7334 0.0219 0.0179 0.735 9.263 3.400 547.987 1.047 15.122 2.814 0.42 228929. 0.1450
|
|
61.93 0.6228 0.7009 0.0175 0.0155 0.637 8.031 2.704 475.070 0.907 12.028 2.582 0.42 229502. 0.1186
|
|
64.40 0.6477 0.6462 0.0130 0.0130 0.535 6.741 2.012 398.791 0.762 8.951 2.289 0.43 230094. 0.0907
|
|
66.88 0.6726 0.5527 0.0086 0.0104 0.429 5.403 1.328 319.607 0.610 5.908 1.885 0.43 230704. 0.0607
|
|
69.36 0.6975 0.3801 0.0042 0.0078 0.319 4.024 0.656 238.056 0.455 2.918 1.250 0.43 231334. 0.0283
|
|
71.83 0.7224 -0.0027 0.0000 0.0050 0.207 2.609 -0.003 154.363 0.295 -0.013 -0.008 0.43 231967. 0.0000
|
|
|
|
|
|
|
|
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 0.0988 0.0332 2.358 24.771 22.054 1758.387 2.799 98.096 5.689 0.50 264786. 0.7465
|
|
2.97 0.0249 0.0719 0.0974 0.0338 2.397 25.175 21.737 1787.087 2.844 96.685 5.517 0.50 264972. 0.7187
|
|
5.94 0.0498 0.1394 0.0959 0.0343 2.433 25.557 21.391 1814.244 2.887 95.145 5.348 0.50 265173. 0.6911
|
|
8.92 0.0747 0.2026 0.0942 0.0347 2.467 25.910 21.014 1839.303 2.927 93.471 5.182 0.50 265391. 0.6637
|
|
11.89 0.0996 0.2616 0.0924 0.0352 2.497 26.226 20.606 1861.697 2.963 91.654 5.020 0.50 265627. 0.6367
|
|
14.86 0.1245 0.3168 0.0904 0.0355 2.522 26.496 20.164 1880.848 2.993 89.687 4.862 0.50 265881. 0.6101
|
|
17.83 0.1495 0.3681 0.0882 0.0358 2.543 26.711 19.686 1896.129 3.018 87.564 4.709 0.50 266154. 0.5838
|
|
20.80 0.1744 0.4159 0.0859 0.0360 2.557 26.863 19.172 1906.906 3.035 85.276 4.560 0.50 266446. 0.5579
|
|
23.78 0.1993 0.4603 0.0835 0.0361 2.565 26.942 18.620 1912.538 3.044 82.820 4.416 0.50 266759. 0.5324
|
|
26.75 0.2242 0.5014 0.0808 0.0361 2.565 26.940 18.028 1912.377 3.044 80.190 4.276 0.50 267092. 0.5073
|
|
29.72 0.2491 0.5395 0.0780 0.0360 2.556 26.847 17.397 1905.783 3.033 77.381 4.140 0.50 267446. 0.4825
|
|
32.69 0.2740 0.5746 0.0750 0.0357 2.537 26.655 16.725 1892.130 3.011 74.391 4.009 0.50 267821. 0.4581
|
|
35.66 0.2989 0.6069 0.0718 0.0353 2.509 26.354 16.011 1870.774 2.977 71.216 3.882 0.50 268218. 0.4340
|
|
38.64 0.3238 0.6366 0.0684 0.0348 2.469 25.934 15.254 1840.997 2.930 67.850 3.758 0.50 268637. 0.4101
|
|
41.61 0.3487 0.6636 0.0648 0.0340 2.417 25.388 14.455 1802.251 2.868 64.294 3.638 0.50 269077. 0.3864
|
|
44.58 0.3736 0.6880 0.0610 0.0331 2.353 24.715 13.616 1754.433 2.792 60.566 3.520 0.50 269540. 0.3630
|
|
47.55 0.3985 0.7098 0.0571 0.0321 2.277 23.915 12.744 1697.632 2.702 56.683 3.405 0.50 270026. 0.3396
|
|
50.53 0.4234 0.7289 0.0531 0.0308 2.189 22.990 11.840 1631.971 2.597 52.664 3.291 0.50 270533. 0.3164
|
|
53.50 0.4484 0.7451 0.0489 0.0294 2.089 21.942 10.909 1557.583 2.479 48.525 3.177 0.50 271063. 0.2932
|
|
56.47 0.4733 0.7580 0.0446 0.0279 1.977 20.773 9.955 1474.615 2.347 44.280 3.062 0.51 271614. 0.2699
|
|
59.44 0.4982 0.7674 0.0403 0.0261 1.855 19.486 8.981 1383.239 2.201 39.947 2.945 0.51 272189. 0.2466
|
|
62.41 0.5231 0.7725 0.0358 0.0242 1.721 18.083 7.990 1283.671 2.043 35.541 2.823 0.51 272786. 0.2230
|
|
65.39 0.5480 0.7723 0.0313 0.0222 1.577 16.569 6.987 1176.178 1.872 31.078 2.694 0.51 273405. 0.1990
|
|
68.36 0.5729 0.7654 0.0268 0.0200 1.423 14.948 5.975 1061.101 1.689 26.576 2.554 0.51 274047. 0.1744
|
|
71.33 0.5978 0.7491 0.0222 0.0177 1.259 13.226 4.958 938.870 1.494 22.055 2.395 0.51 274712. 0.1490
|
|
74.30 0.6227 0.7190 0.0177 0.0153 1.086 11.411 3.942 810.024 1.289 17.535 2.207 0.51 275399. 0.1225
|
|
77.27 0.6476 0.6671 0.0131 0.0128 0.906 9.512 2.931 675.233 1.075 13.039 1.969 0.51 276110. 0.0942
|
|
80.25 0.6725 0.5758 0.0087 0.0101 0.718 7.541 1.932 535.314 0.852 8.593 1.637 0.51 276843. 0.0636
|
|
83.22 0.6974 0.4017 0.0043 0.0074 0.525 5.511 0.950 391.225 0.623 4.224 1.101 0.51 277598. 0.0300
|
|
86.19 0.7224 -0.0097 -0.0001 0.0046 0.326 3.427 -0.014 243.260 0.387 -0.061 -0.026 0.51 278354. 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 0.1000 0.0336 3.784 34.068 30.379 2821.485 3.849 135.128 4.884 0.58 308888. 0.7521
|
|
3.49 0.0250 0.0724 0.0986 0.0341 3.847 34.638 29.950 2868.634 3.913 133.215 4.735 0.58 309106. 0.7241
|
|
6.97 0.0501 0.1403 0.0971 0.0347 3.907 35.176 29.479 2913.240 3.974 131.123 4.590 0.58 309343. 0.6963
|
|
10.46 0.0751 0.2038 0.0954 0.0351 3.962 35.673 28.966 2954.383 4.030 128.841 4.447 0.58 309600. 0.6687
|
|
13.94 0.1001 0.2633 0.0935 0.0356 4.011 36.117 28.408 2991.128 4.080 126.359 4.308 0.58 309878. 0.6415
|
|
17.43 0.1252 0.3187 0.0915 0.0360 4.053 36.495 27.802 3022.490 4.123 123.664 4.172 0.58 310178. 0.6147
|
|
20.91 0.1502 0.3704 0.0894 0.0363 4.087 36.797 27.146 3047.439 4.157 120.747 4.040 0.58 310500. 0.5882
|
|
24.40 0.1753 0.4185 0.0871 0.0365 4.110 37.008 26.439 3064.932 4.181 117.600 3.913 0.58 310845. 0.5621
|
|
27.88 0.2003 0.4631 0.0846 0.0366 4.122 37.116 25.677 3073.889 4.193 114.212 3.789 0.58 311214. 0.5364
|
|
31.37 0.2253 0.5045 0.0819 0.0366 4.121 37.108 24.860 3073.242 4.192 110.578 3.669 0.58 311607. 0.5112
|
|
34.85 0.2504 0.5429 0.0790 0.0364 4.106 36.972 23.987 3061.947 4.177 106.692 3.553 0.58 312024. 0.4862
|
|
38.34 0.2754 0.5783 0.0759 0.0362 4.075 36.694 23.055 3038.966 4.146 102.549 3.441 0.59 312467. 0.4617
|
|
41.82 0.3004 0.6110 0.0727 0.0357 4.027 36.263 22.065 3003.249 4.097 98.144 3.332 0.59 312936. 0.4374
|
|
45.31 0.3255 0.6410 0.0692 0.0351 3.961 35.664 21.014 2953.621 4.029 93.469 3.227 0.59 313430. 0.4133
|
|
48.79 0.3505 0.6684 0.0655 0.0344 3.874 34.886 19.902 2889.182 3.941 88.526 3.124 0.59 313950. 0.3895
|
|
52.28 0.3756 0.6932 0.0617 0.0334 3.768 33.927 18.736 2809.782 3.833 83.339 3.025 0.59 314497. 0.3658
|
|
55.76 0.4006 0.7154 0.0577 0.0323 3.642 32.790 17.521 2715.574 3.705 77.935 2.927 0.59 315069. 0.3423
|
|
59.25 0.4256 0.7350 0.0536 0.0310 3.496 31.476 16.263 2606.767 3.556 72.338 2.830 0.59 315668. 0.3189
|
|
62.73 0.4507 0.7517 0.0493 0.0295 3.331 29.988 14.966 2483.589 3.388 66.571 2.733 0.59 316292. 0.2955
|
|
66.22 0.4757 0.7653 0.0449 0.0279 3.146 28.331 13.637 2346.295 3.201 60.656 2.636 0.59 316943. 0.2720
|
|
69.71 0.5007 0.7753 0.0404 0.0261 2.944 26.506 12.279 2195.177 2.995 54.617 2.537 0.59 317620. 0.2484
|
|
73.19 0.5258 0.7811 0.0359 0.0242 2.723 24.519 10.898 2030.601 2.770 48.474 2.434 0.59 318324. 0.2245
|
|
76.68 0.5508 0.7816 0.0313 0.0220 2.485 22.375 9.499 1853.025 2.528 42.253 2.325 0.59 319054. 0.2002
|
|
80.16 0.5759 0.7753 0.0266 0.0198 2.230 20.080 8.089 1663.032 2.269 35.978 2.206 0.59 319811. 0.1753
|
|
83.65 0.6009 0.7594 0.0220 0.0174 1.960 17.645 6.672 1461.357 1.994 29.676 2.071 0.59 320594. 0.1495
|
|
87.13 0.6259 0.7291 0.0173 0.0149 1.675 15.080 5.256 1248.922 1.704 23.379 1.909 0.59 321404. 0.1223
|
|
90.62 0.6510 0.6753 0.0127 0.0122 1.377 12.399 3.849 1026.875 1.401 17.118 1.700 0.60 322241. 0.0932
|
|
94.10 0.6760 0.5773 0.0081 0.0095 1.068 9.619 2.458 796.619 1.087 10.932 1.399 0.60 323104. 0.0613
|
|
97.59 0.7010 0.3787 0.0036 0.0067 0.751 6.759 1.093 559.784 0.764 4.860 0.885 0.60 323993. 0.0259
|
|
101.07 0.7261
|
|
|
|
|
|
|
|
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 0.1015 0.0341 5.741 45.234 40.257 4281.358 5.110 179.061 4.265 0.67 352973. 0.7561
|
|
3.95 0.0248 0.0717 0.1001 0.0347 5.838 45.997 39.708 4353.609 5.197 176.622 4.137 0.67 353221. 0.7284
|
|
7.90 0.0497 0.1390 0.0986 0.0352 5.930 46.720 39.107 4422.063 5.278 173.946 4.011 0.67 353490. 0.7009
|
|
11.86 0.0745 0.2021 0.0969 0.0357 6.015 47.388 38.448 4485.288 5.354 171.019 3.888 0.67 353783. 0.6736
|
|
15.81 0.0994 0.2611 0.0951 0.0362 6.091 47.986 37.731 4541.863 5.421 167.826 3.768 0.67 354099. 0.6467
|
|
19.76 0.1242 0.3163 0.0932 0.0366 6.156 48.498 36.950 4590.306 5.479 164.352 3.651 0.67 354439. 0.6201
|
|
23.71 0.1491 0.3678 0.0910 0.0369 6.208 48.907 36.102 4629.046 5.526 160.582 3.537 0.67 354805. 0.5939
|
|
27.67 0.1739 0.4157 0.0887 0.0371 6.244 49.197 35.186 4656.499 5.558 156.506 3.427 0.67 355197. 0.5680
|
|
31.62 0.1987 0.4603 0.0862 0.0372 6.264 49.351 34.198 4671.047 5.576 152.111 3.321 0.67 355616. 0.5426
|
|
35.57 0.2236 0.5017 0.0835 0.0372 6.264 49.352 33.136 4671.092 5.576 147.387 3.218 0.67 356062. 0.5175
|
|
39.52 0.2484 0.5402 0.0807 0.0371 6.243 49.182 31.998 4655.054 5.557 142.328 3.118 0.67 356536. 0.4928
|
|
43.48 0.2733 0.5758 0.0776 0.0368 6.197 48.826 30.784 4621.388 5.516 136.927 3.021 0.67 357038. 0.4684
|
|
47.43 0.2981 0.6088 0.0743 0.0364 6.127 48.268 29.491 4568.547 5.453 131.177 2.928 0.67 357569. 0.4443
|
|
51.38 0.3230 0.6391 0.0709 0.0358 6.028 47.489 28.118 4494.829 5.365 125.069 2.837 0.67 358129. 0.4204
|
|
55.33 0.3478 0.6669 0.0672 0.0351 5.899 46.474 26.664 4398.733 5.251 118.603 2.749 0.67 358718. 0.3967
|
|
59.28 0.3726 0.6923 0.0634 0.0341 5.739 45.218 25.136 4279.884 5.109 111.804 2.664 0.67 359336. 0.3732
|
|
63.24 0.3975 0.7153 0.0593 0.0330 5.550 43.724 23.541 4138.495 4.940 104.709 2.580 0.67 359983. 0.3498
|
|
67.19 0.4223 0.7356 0.0552 0.0317 5.330 41.996 21.886 3974.898 4.745 97.350 2.497 0.67 360660. 0.3265
|
|
71.14 0.4472 0.7533 0.0509 0.0302 5.082 40.037 20.180 3789.444 4.523 89.759 2.415 0.67 361366. 0.3032
|
|
75.09 0.4720 0.7680 0.0465 0.0286 4.804 37.850 18.427 3582.523 4.276 81.965 2.333 0.67 362102. 0.2798
|
|
79.05 0.4969 0.7795 0.0419 0.0267 4.499 35.442 16.636 3354.580 4.004 73.996 2.249 0.67 362867. 0.2563
|
|
83.00 0.5217 0.7870 0.0373 0.0248 4.165 32.817 14.812 3106.151 3.708 65.883 2.163 0.68 363661. 0.2326
|
|
86.95 0.5465 0.7897 0.0327 0.0226 3.806 29.983 12.962 2837.906 3.388 57.657 2.072 0.68 364485. 0.2084
|
|
90.90 0.5714 0.7862 0.0280 0.0203 3.421 26.949 11.095 2550.696 3.045 49.350 1.973 0.68 365339. 0.1836
|
|
94.86 0.5962 0.7742 0.0232 0.0179 3.011 23.725 9.217 2245.585 2.680 40.997 1.862 0.68 366223. 0.1579
|
|
98.81 0.6211 0.7494 0.0185 0.0153 2.580 20.327 7.338 1923.923 2.297 32.639 1.730 0.68 367136. 0.1309
|
|
102.76 0.6459 0.7037 0.0138 0.0127 2.129 16.771 5.467 1587.407 1.895 24.318 1.562 0.68 368079. 0.1021
|
|
106.71 0.6708 0.6197 0.0091 0.0099 1.660 13.081 3.616 1238.154 1.478 16.083 1.325 0.68 369053. 0.0704
|
|
110.66 0.6956 0.4496 0.0045 0.0070 1.178 9.284 1.795 878.706 1.049 7.986 0.927 0.68 370055. 0.0347
|
|
114.62 0.7204 0.0043 0.0000 0.0041 0.684 5.389 0.010 510.109 0.609 0.043 0.008 0.68 371060. 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 0.1033 0.0353 8.454 59.208 51.834 6304.510 6.689 230.557 3.729 0.75 397035. 0.7502
|
|
4.44 0.0248 0.0706 0.1019 0.0358 8.584 60.117 51.159 6401.301 6.792 227.555 3.625 0.75 397315. 0.7244
|
|
8.88 0.0496 0.1371 0.1004 0.0363 8.708 60.980 50.415 6493.190 6.889 224.244 3.522 0.75 397619. 0.6987
|
|
13.32 0.0744 0.1997 0.0988 0.0368 8.822 61.778 49.597 6578.194 6.980 220.606 3.420 0.75 397949. 0.6729
|
|
17.76 0.0992 0.2585 0.0970 0.0372 8.924 62.493 48.700 6654.325 7.060 216.618 3.319 0.75 398306. 0.6473
|
|
22.20 0.1241 0.3135 0.0951 0.0376 9.011 63.105 47.720 6719.449 7.130 212.259 3.221 0.75 398690. 0.6217
|
|
26.64 0.1489 0.3650 0.0929 0.0379 9.080 63.592 46.653 6771.296 7.185 207.512 3.125 0.75 399103. 0.5964
|
|
31.08 0.1737 0.4131 0.0906 0.0381 9.129 63.932 45.494 6807.498 7.223 202.358 3.031 0.75 399546. 0.5713
|
|
35.53 0.1985 0.4579 0.0881 0.0382 9.153 64.102 44.240 6825.647 7.242 196.782 2.940 0.75 400019. 0.5464
|
|
39.97 0.2233 0.4995 0.0854 0.0382 9.150 64.080 42.889 6823.283 7.240 190.771 2.851 0.75 400523. 0.5217
|
|
44.41 0.2481 0.5382 0.0825 0.0380 9.116 63.842 41.438 6797.963 7.213 184.316 2.765 0.75 401058. 0.4973
|
|
48.85 0.2729 0.5742 0.0794 0.0378 9.048 63.366 39.885 6747.271 7.159 177.408 2.681 0.75 401625. 0.4731
|
|
53.29 0.2977 0.6074 0.0761 0.0373 8.943 62.629 38.229 6668.774 7.076 170.041 2.600 0.75 402224. 0.4492
|
|
57.73 0.3225 0.6381 0.0726 0.0367 8.797 61.606 36.466 6559.841 6.960 162.201 2.521 0.75 402855. 0.4254
|
|
62.17 0.3474 0.6664 0.0689 0.0359 8.607 60.274 34.597 6418.042 6.810 153.886 2.445 0.75 403520. 0.4018
|
|
66.61 0.3722 0.6923 0.0650 0.0349 8.371 58.627 32.628 6242.620 6.624 145.128 2.371 0.75 404217. 0.3784
|
|
71.05 0.3970 0.7158 0.0609 0.0338 8.092 56.666 30.569 6033.880 6.402 135.973 2.298 0.76 404947. 0.3550
|
|
75.49 0.4218 0.7368 0.0566 0.0324 7.768 54.398 28.432 5792.357 6.146 126.464 2.226 0.76 405709. 0.3317
|
|
79.93 0.4466 0.7553 0.0522 0.0309 7.401 51.828 26.224 5518.637 5.855 116.644 2.155 0.76 406504. 0.3084
|
|
84.37 0.4714 0.7709 0.0477 0.0292 6.991 48.961 23.954 5213.410 5.532 106.549 2.084 0.76 407332. 0.2850
|
|
88.81 0.4962 0.7832 0.0431 0.0273 6.541 45.806 21.632 4877.470 5.175 96.219 2.012 0.76 408193. 0.2614
|
|
93.25 0.5210 0.7918 0.0384 0.0253 6.050 42.372 19.265 4511.805 4.787 85.692 1.937 0.76 409087. 0.2375
|
|
97.69 0.5458 0.7956 0.0336 0.0230 5.522 38.671 16.863 4117.666 4.369 75.007 1.858 0.76 410014. 0.2131
|
|
102.14 0.5707 0.7931 0.0288 0.0207 4.957 34.717 14.435 3696.665 3.922 64.208 1.771 0.76 410974. 0.1880
|
|
106.58 0.5955 0.7817 0.0239 0.0182 4.359 30.530 11.992 3250.870 3.449 53.341 1.673 0.76 411967. 0.1619
|
|
111.02 0.6203 0.7571 0.0190 0.0156 3.732 26.135 9.545 2782.906 2.953 42.455 1.556 0.76 412993. 0.1343
|
|
115.46 0.6451 0.7105 0.0142 0.0129 3.079 21.563 7.106 2296.052 2.436 31.608 1.404 0.77 414052. 0.1046
|
|
119.90 0.6699 0.6232 0.0093 0.0100 2.406 16.851 4.690 1794.317 1.904 20.863 1.186 0.77 415145. 0.0717
|
|
124.34 0.6947 0.4459 0.0046 0.0072 1.720 12.043 2.313 1282.393 1.361 10.287 0.818 0.77 416271. 0.0348
|
|
128.78 0.7195 -0.0077 0.0000 0.0043 1.022 7.158 -0.023 762.194 0.809 -0.102 -0.014 0.77 417397. 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 0.1053 0.0393 12.905 81.341 65.256 9623.585 9.190 290.257 3.076 0.83 441067. 0.6942
|
|
4.93 0.0248 0.0650 0.1040 0.0396 13.028 82.112 64.463 9714.799 9.277 286.730 3.010 0.83 441378. 0.6752
|
|
9.85 0.0495 0.1271 0.1026 0.0400 13.138 82.806 63.581 9796.892 9.355 282.809 2.944 0.83 441717. 0.6558
|
|
14.78 0.0743 0.1864 0.1010 0.0403 13.233 83.403 62.605 9867.607 9.423 278.469 2.878 0.83 442084. 0.6362
|
|
19.71 0.0991 0.2429 0.0993 0.0405 13.309 83.885 61.528 9924.634 9.477 273.679 2.812 0.83 442482. 0.6163
|
|
24.63 0.1239 0.2966 0.0974 0.0407 13.364 84.232 60.344 9965.585 9.516 268.411 2.746 0.83 442911. 0.5961
|
|
29.56 0.1486 0.3475 0.0953 0.0408 13.394 84.421 59.046 9987.961 9.538 262.638 2.681 0.83 443372. 0.5757
|
|
34.48 0.1734 0.3956 0.0930 0.0408 13.396 84.431 57.630 9989.172 9.539 256.337 2.617 0.83 443866. 0.5550
|
|
39.41 0.1982 0.4410 0.0905 0.0407 13.365 84.239 56.089 9966.502 9.517 249.485 2.553 0.83 444394. 0.5342
|
|
44.34 0.2230 0.4838 0.0878 0.0405 13.299 83.822 54.421 9917.165 9.470 242.065 2.489 0.84 444956. 0.5130
|
|
49.26 0.2477 0.5239 0.0849 0.0401 13.193 83.156 52.622 9838.352 9.395 234.062 2.426 0.84 445554. 0.4917
|
|
54.19 0.2725 0.5615 0.0818 0.0397 13.045 82.218 50.689 9727.307 9.289 225.465 2.364 0.84 446186. 0.4702
|
|
59.12 0.2973 0.5965 0.0784 0.0391 12.848 80.982 48.621 9581.126 9.149 216.266 2.302 0.84 446855. 0.4484
|
|
64.04 0.3220 0.6290 0.0749 0.0383 12.601 79.422 46.415 9396.547 8.973 206.452 2.240 0.84 447560. 0.4265
|
|
68.97 0.3468 0.6591 0.0711 0.0374 12.297 77.508 44.068 9170.118 8.757 196.015 2.180 0.84 448300. 0.4043
|
|
73.90 0.3716 0.6866 0.0671 0.0363 11.935 75.227 41.590 8900.251 8.499 184.991 2.119 0.84 449077. 0.3819
|
|
78.82 0.3964 0.7116 0.0629 0.0350 11.516 72.585 38.993 8587.680 8.201 173.439 2.059 0.84 449890. 0.3593
|
|
83.75 0.4211 0.7338 0.0586 0.0336 11.045 69.613 36.289 8235.990 7.865 161.413 1.998 0.84 450739. 0.3364
|
|
88.68 0.4459 0.7528 0.0540 0.0320 10.519 66.300 33.491 7844.083 7.491 148.969 1.937 0.84 451624. 0.3131
|
|
93.60 0.4707 0.7684 0.0494 0.0303 9.943 62.667 30.611 7414.197 7.080 136.156 1.873 0.84 452545. 0.2895
|
|
98.53 0.4955 0.7800 0.0446 0.0283 9.316 58.718 27.659 6947.015 6.634 123.026 1.806 0.84 453503. 0.2654
|
|
103.45 0.5202 0.7869 0.0398 0.0263 8.640 54.457 24.646 6442.914 6.153 109.627 1.735 0.84 454496. 0.2407
|
|
108.38 0.5450 0.7877 0.0348 0.0241 7.919 49.914 21.585 5905.404 5.639 96.011 1.658 0.85 455526. 0.2152
|
|
113.31 0.5698 0.7803 0.0298 0.0218 7.158 45.118 18.487 5337.978 5.097 82.231 1.571 0.85 456591. 0.1887
|
|
118.23 0.5945 0.7612 0.0248 0.0194 6.364 40.111 15.366 4745.559 4.532 68.347 1.469 0.85 457694. 0.1609
|
|
123.16 0.6193 0.7249 0.0197 0.0169 5.543 34.938 12.235 4133.618 3.947 54.423 1.343 0.85 458832. 0.1312
|
|
128.09 0.6441 0.6615 0.0147 0.0143 4.705 29.655 9.112 3508.491 3.350 40.530 1.178 0.85 460007. 0.0994
|
|
133.01 0.6689 0.5528 0.0097 0.0117 3.859 24.321 6.014 2877.432 2.748 26.751 0.948 0.85 461219. 0.0650
|
|
137.94 0.6936 0.3614 0.0048 0.0092 3.015 19.003 2.963 2248.316 2.147 13.177 0.598 0.85 462466. 0.0287
|
|
142.87 0.7184 -0.0061 -0.0001 0.0066 2.177 13.722 -0.035 1623.423 1.550 -0.155 -0.010 0.85 463723. 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 0.1064 0.0476 20.829 119.350 79.818 15532.555 13.484 355.032 2.331 0.92 485113. 0.5818
|
|
5.50 0.0251 0.0553 0.1053 0.0479 20.938 119.973 78.964 15613.690 13.555 351.230 2.294 0.92 485456. 0.5695
|
|
11.00 0.0503 0.1089 0.1040 0.0480 21.015 120.414 77.997 15671.011 13.604 346.931 2.257 0.92 485831. 0.5571
|
|
16.50 0.0754 0.1608 0.1026 0.0481 21.055 120.641 76.909 15700.520 13.630 342.090 2.222 0.92 486239. 0.5444
|
|
22.01 0.1006 0.2110 0.1009 0.0481 21.052 120.627 75.689 15698.711 13.628 336.663 2.187 0.92 486682. 0.5316
|
|
27.51 0.1257 0.2596 0.0991 0.0480 21.004 120.347 74.327 15662.374 13.597 330.604 2.152 0.92 487162. 0.5185
|
|
33.01 0.1509 0.3066 0.0971 0.0478 20.905 119.781 72.814 15588.697 13.533 323.875 2.119 0.92 487680. 0.5051
|
|
38.51 0.1760 0.3520 0.0949 0.0474 20.752 118.909 71.141 15475.132 13.434 316.437 2.085 0.92 488236. 0.4914
|
|
44.01 0.2012 0.3959 0.0924 0.0470 20.544 117.712 69.303 15319.377 13.299 308.258 2.052 0.92 488831. 0.4773
|
|
49.51 0.2263 0.4382 0.0897 0.0464 20.275 116.174 67.291 15119.270 13.125 299.310 2.019 0.92 489466. 0.4627
|
|
55.01 0.2515 0.4788 0.0868 0.0456 19.945 114.281 65.102 14872.933 12.911 289.572 1.985 0.92 490142. 0.4476
|
|
60.51 0.2766 0.5178 0.0836 0.0447 19.550 112.021 62.731 14578.764 12.656 279.028 1.952 0.92 490858. 0.4319
|
|
66.02 0.3018 0.5549 0.0802 0.0436 19.090 109.381 60.177 14235.117 12.358 267.668 1.917 0.92 491616. 0.4156
|
|
71.52 0.3269 0.5902 0.0766 0.0424 18.559 106.339 57.435 13839.281 12.014 255.470 1.882 0.92 492415. 0.3986
|
|
77.02 0.3521 0.6234 0.0727 0.0410 17.955 102.881 54.504 13389.193 11.623 242.433 1.846 0.92 493255. 0.3809
|
|
82.52 0.3772 0.6545 0.0685 0.0395 17.279 99.006 51.397 12884.880 11.186 228.613 1.809 0.92 494136. 0.3624
|
|
88.02 0.4024 0.6833 0.0642 0.0378 16.532 94.726 48.132 12327.901 10.702 214.092 1.771 0.92 495059. 0.3433
|
|
93.52 0.4275 0.7093 0.0596 0.0359 15.725 90.102 44.726 11726.154 10.180 198.940 1.730 0.92 496022. 0.3233
|
|
99.02 0.4527 0.7305 0.0549 0.0340 14.890 85.317 41.191 11103.378 9.639 183.217 1.683 0.93 497026. 0.3017
|
|
104.52 0.4778 0.7468 0.0501 0.0320 14.013 80.295 37.546 10449.857 9.072 167.005 1.630 0.93 498070. 0.2790
|
|
110.03 0.5030 0.7541 0.0451 0.0301 13.151 75.353 33.801 9806.662 8.513 150.345 1.563 0.93 499155. 0.2540
|
|
115.53 0.5281 0.7504 0.0400 0.0281 12.304 70.499 29.971 9174.940 7.965 133.311 1.482 0.93 500280. 0.2266
|
|
121.03 0.5533 0.7368 0.0348 0.0261 11.423 65.454 26.081 8518.330 7.395 116.008 1.389 0.93 501446. 0.1982
|
|
126.53 0.5784 0.7102 0.0295 0.0241 10.522 60.291 22.149 7846.394 6.812 98.518 1.280 0.93 502653. 0.1684
|
|
132.03 0.6036 0.6666 0.0243 0.0220 9.610 55.065 18.196 7166.386 6.221 80.936 1.152 0.93 503900. 0.1373
|
|
137.53 0.6287 0.6004 0.0190 0.0199 8.701 49.858 14.246 6488.646 5.633 63.366 0.996 0.93 505189. 0.1050
|
|
143.03 0.6539 0.5044 0.0138 0.0179 7.808 44.741 10.326 5822.682 5.055 45.929 0.804 0.94 506518. 0.0722
|
|
148.54 0.6790 0.3689 0.0086 0.0159 6.942 39.779 6.467 5176.944 4.494 28.764 0.567 0.94 507889. 0.0403
|
|
154.04 0.7042 0.1817 0.0036 0.0140 6.113 35.026 2.704 4558.441 3.957 12.025 0.269 0.94 509301. 0.0124
|
|
159.54 0.7293
|
|
|
|
|
|
|