20x15E (20x15E.dat) v2022-0915 Simulation Date: 09/22/2022 AIRFOIL AERO DATA GENERATED USING: POLAR DIAGRAMS ====== PERFORMANCE DATA (versus advance ratio and MPH) ====== DEFINITIONS: J=V/nD (advance ratio) Ct=T/(rho * n**2 * D**4) (thrust coef.) Cp=P/(rho * n**3 * D**5) (power coef.) Pe=Ct*J/Cp (efficiency) V (model speed in MPH) Mach (at prop tip) Reyn (at 75% of span) FOM (Figure of Merit) PROP RPM = 1000 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 0.1008 0.0431 0.011 0.700 0.514 8.277 0.079 2.286 28.157 0.08 36633. 0.5922 0.59 0.0309 0.0702 0.0999 0.0440 0.011 0.714 0.510 8.447 0.081 2.267 27.362 0.08 36663. 0.5730 1.17 0.0618 0.1363 0.0990 0.0449 0.012 0.729 0.505 8.620 0.082 2.245 26.558 0.08 36696. 0.5536 1.76 0.0927 0.1982 0.0979 0.0458 0.012 0.743 0.499 8.794 0.084 2.221 25.751 0.08 36733. 0.5338 2.34 0.1236 0.2561 0.0967 0.0467 0.012 0.758 0.493 8.965 0.086 2.193 24.947 0.08 36774. 0.5139 2.93 0.1545 0.3099 0.0953 0.0475 0.012 0.772 0.486 9.130 0.087 2.162 24.149 0.08 36819. 0.4940 3.51 0.1854 0.3597 0.0938 0.0484 0.012 0.785 0.478 9.285 0.089 2.127 23.363 0.08 36869. 0.4740 4.10 0.2163 0.4058 0.0921 0.0491 0.013 0.797 0.469 9.425 0.090 2.088 22.590 0.08 36923. 0.4541 4.68 0.2473 0.4483 0.0901 0.0497 0.013 0.807 0.460 9.546 0.091 2.044 21.835 0.08 36982. 0.4343 5.27 0.2782 0.4873 0.0880 0.0502 0.013 0.815 0.449 9.642 0.092 1.995 21.098 0.08 37045. 0.4145 5.85 0.3091 0.5230 0.0856 0.0506 0.013 0.821 0.436 9.708 0.093 1.940 20.381 0.08 37114. 0.3949 6.44 0.3400 0.5557 0.0829 0.0507 0.013 0.823 0.423 9.738 0.093 1.880 19.685 0.08 37188. 0.3754 7.02 0.3709 0.5854 0.0799 0.0507 0.013 0.822 0.408 9.727 0.093 1.813 19.008 0.08 37267. 0.3561 7.61 0.4018 0.6122 0.0767 0.0504 0.013 0.817 0.391 9.669 0.092 1.740 18.351 0.08 37350. 0.3367 8.20 0.4327 0.6363 0.0732 0.0498 0.013 0.808 0.373 9.559 0.091 1.660 17.710 0.08 37439. 0.3174 8.78 0.4636 0.6576 0.0694 0.0489 0.013 0.794 0.354 9.392 0.090 1.573 17.083 0.08 37533. 0.2981 9.37 0.4945 0.6760 0.0653 0.0477 0.012 0.775 0.333 9.167 0.088 1.480 16.464 0.08 37633. 0.2786 9.95 0.5254 0.6913 0.0609 0.0463 0.012 0.751 0.310 8.885 0.085 1.381 15.847 0.08 37737. 0.2590 10.54 0.5563 0.7032 0.0563 0.0445 0.011 0.723 0.287 8.550 0.082 1.277 15.225 0.08 37846. 0.2393 11.12 0.5872 0.7113 0.0515 0.0425 0.011 0.690 0.263 8.164 0.078 1.168 14.588 0.08 37960. 0.2193 11.71 0.6181 0.7148 0.0466 0.0403 0.010 0.653 0.237 7.731 0.074 1.056 13.927 0.08 38080. 0.1991 12.29 0.6490 0.7128 0.0415 0.0378 0.010 0.613 0.212 7.254 0.069 0.941 13.227 0.08 38204. 0.1785 12.88 0.6800 0.7041 0.0363 0.0351 0.009 0.569 0.185 6.736 0.064 0.824 12.471 0.08 38333. 0.1575 13.46 0.7109 0.6867 0.0311 0.0322 0.008 0.522 0.158 6.179 0.059 0.705 11.635 0.08 38467. 0.1359 14.05 0.7418 0.6580 0.0258 0.0291 0.007 0.472 0.132 5.587 0.053 0.585 10.683 0.08 38605. 0.1137 14.63 0.7727 0.6134 0.0205 0.0258 0.007 0.420 0.105 4.964 0.047 0.465 9.561 0.08 38749. 0.0907 15.22 0.8036 0.5459 0.0153 0.0225 0.006 0.365 0.078 4.314 0.041 0.346 8.182 0.08 38897. 0.0670 15.80 0.8345 0.4429 0.0101 0.0190 0.005 0.308 0.051 3.643 0.035 0.228 6.392 0.08 39050. 0.0425 16.39 0.8654 0.2801 0.0050 0.0154 0.004 0.250 0.025 2.956 0.028 0.113 3.898 0.08 39208. 0.0182 16.98 0.8963 0.0033 0.0000 0.0118 0.003 0.191 0.000 2.260 0.022 0.001 0.044 0.08 39370. 0.0000 PROP RPM = 2000 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 0.1011 0.0403 0.083 2.619 2.062 61.960 0.296 9.173 15.096 0.16 73265. 0.6360 1.18 0.0311 0.0755 0.1003 0.0413 0.085 2.678 2.045 63.378 0.303 9.098 14.637 0.16 73325. 0.6142 2.35 0.0621 0.1462 0.0993 0.0422 0.087 2.740 2.026 64.828 0.310 9.013 14.176 0.16 73392. 0.5920 3.53 0.0932 0.2122 0.0983 0.0432 0.089 2.801 2.005 66.288 0.317 8.916 13.716 0.16 73466. 0.5697 4.70 0.1242 0.2735 0.0971 0.0441 0.091 2.862 1.980 67.733 0.323 8.807 13.259 0.16 73549. 0.5474 5.88 0.1553 0.3302 0.0957 0.0450 0.093 2.922 1.952 69.133 0.330 8.684 12.808 0.16 73640. 0.5250 7.06 0.1863 0.3826 0.0942 0.0459 0.094 2.978 1.921 70.455 0.336 8.544 12.366 0.16 73740. 0.5028 8.23 0.2174 0.4308 0.0924 0.0466 0.096 3.029 1.886 71.662 0.342 8.387 11.934 0.16 73849. 0.4808 9.41 0.2484 0.4750 0.0905 0.0473 0.098 3.073 1.846 72.713 0.347 8.210 11.514 0.16 73967. 0.4590 10.59 0.2795 0.5155 0.0883 0.0479 0.099 3.109 1.802 73.567 0.351 8.013 11.107 0.16 74096. 0.4374 11.76 0.3105 0.5525 0.0859 0.0483 0.099 3.135 1.752 74.176 0.354 7.794 10.714 0.16 74234. 0.4161 12.94 0.3416 0.5862 0.0832 0.0485 0.100 3.148 1.697 74.496 0.356 7.550 10.335 0.16 74383. 0.3950 14.11 0.3726 0.6169 0.0803 0.0485 0.100 3.147 1.637 74.477 0.356 7.281 9.969 0.16 74542. 0.3742 15.29 0.4037 0.6447 0.0770 0.0482 0.099 3.130 1.571 74.073 0.354 6.986 9.617 0.16 74711. 0.3536 16.47 0.4347 0.6697 0.0734 0.0477 0.098 3.095 1.498 73.239 0.350 6.663 9.277 0.16 74890. 0.3331 17.64 0.4658 0.6921 0.0696 0.0468 0.096 3.040 1.419 71.936 0.343 6.312 8.947 0.16 75080. 0.3127 18.82 0.4968 0.7117 0.0654 0.0457 0.094 2.965 1.334 70.149 0.335 5.934 8.626 0.16 75280. 0.2923 20.00 0.5279 0.7285 0.0610 0.0442 0.091 2.869 1.244 67.891 0.324 5.533 8.311 0.16 75491. 0.2719 21.17 0.5589 0.7423 0.0563 0.0424 0.087 2.755 1.149 65.183 0.311 5.112 7.997 0.16 75711. 0.2515 22.35 0.5900 0.7526 0.0515 0.0404 0.083 2.622 1.051 62.050 0.296 4.674 7.681 0.16 75942. 0.2310 23.52 0.6210 0.7589 0.0465 0.0381 0.078 2.473 0.949 58.513 0.279 4.222 7.358 0.16 76182. 0.2103 24.70 0.6521 0.7603 0.0414 0.0355 0.073 2.307 0.845 54.597 0.261 3.759 7.021 0.16 76432. 0.1894 25.88 0.6832 0.7558 0.0362 0.0328 0.067 2.127 0.739 50.323 0.240 3.288 6.662 0.16 76693. 0.1680 27.05 0.7142 0.7435 0.0310 0.0298 0.061 1.932 0.632 45.718 0.218 2.811 6.269 0.16 76963. 0.1462 28.23 0.7453 0.7206 0.0257 0.0266 0.055 1.725 0.524 40.809 0.195 2.330 5.823 0.16 77243. 0.1236 29.41 0.7763 0.6826 0.0204 0.0232 0.048 1.506 0.416 35.631 0.170 1.850 5.295 0.16 77532. 0.1002 30.58 0.8074 0.6212 0.0151 0.0197 0.041 1.277 0.309 30.220 0.144 1.373 4.633 0.16 77831. 0.0755 31.76 0.8384 0.5206 0.0100 0.0160 0.033 1.041 0.203 24.624 0.118 0.903 3.739 0.16 78140. 0.0494 32.93 0.8695 0.3457 0.0049 0.0123 0.025 0.799 0.100 18.897 0.090 0.444 2.394 0.16 78458. 0.0222 34.11 0.9005 -0.0018 0.0000 0.0085 0.018 0.553 0.000 13.087 0.062 -0.002 -0.012 0.17 78783. 0.0000 PROP RPM = 3000 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 0.1014 0.0392 0.273 5.730 4.655 203.377 0.647 20.705 10.381 0.24 109896. 0.6571 1.77 0.0311 0.0779 0.1006 0.0402 0.279 5.868 4.618 208.271 0.663 20.539 10.056 0.24 109986. 0.6340 3.54 0.0622 0.1508 0.0997 0.0411 0.286 6.009 4.575 213.284 0.679 20.351 9.730 0.24 110086. 0.6106 5.30 0.0933 0.2186 0.0987 0.0421 0.293 6.152 4.527 218.341 0.695 20.137 9.405 0.24 110198. 0.5871 7.07 0.1244 0.2815 0.0975 0.0431 0.300 6.293 4.473 223.356 0.711 19.894 9.082 0.24 110322. 0.5635 8.84 0.1556 0.3396 0.0961 0.0440 0.306 6.430 4.411 228.229 0.726 19.618 8.765 0.24 110459. 0.5401 10.61 0.1867 0.3931 0.0946 0.0449 0.312 6.560 4.340 232.844 0.741 19.307 8.455 0.24 110609. 0.5168 12.37 0.2178 0.4423 0.0929 0.0457 0.318 6.679 4.261 237.074 0.755 18.954 8.153 0.24 110773. 0.4938 14.14 0.2489 0.4873 0.0909 0.0464 0.323 6.784 4.172 240.779 0.766 18.559 7.860 0.24 110952. 0.4710 15.91 0.2800 0.5284 0.0887 0.0470 0.327 6.869 4.073 243.813 0.776 18.115 7.576 0.24 111145. 0.4486 17.68 0.3111 0.5660 0.0863 0.0475 0.330 6.931 3.961 246.016 0.783 17.620 7.303 0.24 111354. 0.4265 19.45 0.3422 0.6002 0.0836 0.0477 0.332 6.965 3.838 247.228 0.787 17.071 7.041 0.24 111577. 0.4047 21.21 0.3733 0.6314 0.0807 0.0477 0.332 6.967 3.701 247.282 0.787 16.464 6.789 0.24 111816. 0.3832 22.98 0.4045 0.6596 0.0774 0.0475 0.330 6.931 3.551 246.016 0.783 15.797 6.548 0.24 112071. 0.3620 24.75 0.4356 0.6852 0.0738 0.0469 0.326 6.854 3.387 243.272 0.774 15.066 6.315 0.24 112342. 0.3410 26.52 0.4667 0.7081 0.0699 0.0461 0.320 6.731 3.209 238.912 0.760 14.271 6.091 0.24 112627. 0.3201 28.28 0.4978 0.7284 0.0657 0.0449 0.312 6.561 3.016 232.885 0.741 13.416 5.874 0.24 112929. 0.2993 30.05 0.5289 0.7460 0.0613 0.0434 0.302 6.346 2.812 225.227 0.717 12.507 5.663 0.24 113246. 0.2786 31.82 0.5600 0.7608 0.0566 0.0417 0.290 6.086 2.597 216.009 0.688 11.553 5.454 0.24 113578. 0.2579 33.59 0.5911 0.7723 0.0517 0.0396 0.275 5.784 2.374 205.308 0.654 10.561 5.245 0.24 113925. 0.2371 35.35 0.6222 0.7802 0.0467 0.0373 0.259 5.443 2.144 193.200 0.615 9.537 5.034 0.24 114287. 0.2163 37.12 0.6534 0.7837 0.0416 0.0347 0.241 5.065 1.908 179.761 0.572 8.489 4.815 0.24 114664. 0.1952 38.89 0.6845 0.7816 0.0364 0.0318 0.221 4.651 1.668 165.072 0.525 7.421 4.584 0.24 115056. 0.1737 40.66 0.7156 0.7724 0.0311 0.0288 0.200 4.204 1.426 149.218 0.475 6.341 4.333 0.24 115462. 0.1518 42.43 0.7467 0.7533 0.0257 0.0255 0.177 3.727 1.181 132.298 0.421 5.255 4.050 0.24 115884. 0.1292 44.19 0.7778 0.7198 0.0204 0.0221 0.153 3.224 0.937 114.428 0.364 4.169 3.715 0.25 116320. 0.1055 45.96 0.8089 0.6634 0.0151 0.0185 0.128 2.698 0.695 95.746 0.305 3.091 3.292 0.25 116770. 0.0805 47.73 0.8400 0.5668 0.0099 0.0147 0.102 2.153 0.456 76.414 0.243 2.030 2.709 0.25 117235. 0.0537 49.50 0.8711 0.3885 0.0049 0.0109 0.076 1.595 0.224 56.623 0.180 0.994 1.790 0.25 117714. 0.0248 51.26 0.9023 -0.0060 0.0000 0.0070 0.049 1.029 -0.002 36.537 0.116 -0.010 -0.027 0.25 118201. 0.0000 PROP RPM = 4000 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 0.1018 0.0387 0.638 10.051 8.307 475.659 1.136 36.951 7.922 0.32 146523. 0.6698 2.36 0.0311 0.0793 0.1010 0.0397 0.654 10.300 8.243 487.458 1.164 36.663 7.670 0.32 146643. 0.6460 4.72 0.0623 0.1533 0.1001 0.0406 0.670 10.556 8.169 499.564 1.193 36.336 7.417 0.32 146777. 0.6219 7.07 0.0934 0.2222 0.0991 0.0416 0.686 10.815 8.085 511.795 1.222 35.963 7.165 0.32 146926. 0.5978 9.43 0.1245 0.2860 0.0979 0.0426 0.703 11.071 7.990 523.948 1.251 35.539 6.917 0.32 147092. 0.5736 11.79 0.1556 0.3449 0.0966 0.0436 0.718 11.321 7.881 535.779 1.279 35.056 6.672 0.32 147275. 0.5495 14.15 0.1868 0.3990 0.0951 0.0445 0.734 11.559 7.758 547.012 1.306 34.508 6.433 0.32 147475. 0.5257 16.51 0.2179 0.4486 0.0934 0.0454 0.747 11.777 7.619 557.339 1.331 33.887 6.200 0.32 147694. 0.5021 18.86 0.2490 0.4941 0.0915 0.0461 0.760 11.969 7.461 566.423 1.352 33.188 5.975 0.32 147933. 0.4788 21.22 0.2801 0.5357 0.0893 0.0467 0.770 12.127 7.285 573.906 1.370 32.403 5.757 0.32 148191. 0.4559 23.58 0.3113 0.5736 0.0869 0.0471 0.777 12.243 7.088 579.408 1.383 31.526 5.548 0.32 148469. 0.4334 25.94 0.3424 0.6081 0.0842 0.0474 0.781 12.309 6.869 582.535 1.391 30.551 5.348 0.32 148768. 0.4112 28.30 0.3735 0.6396 0.0812 0.0474 0.782 12.317 6.626 582.887 1.392 29.472 5.156 0.32 149087. 0.3894 30.65 0.4046 0.6682 0.0779 0.0472 0.778 12.257 6.359 580.068 1.385 28.283 4.972 0.32 149427. 0.3678 33.01 0.4358 0.6940 0.0744 0.0467 0.769 12.123 6.066 573.698 1.370 26.980 4.796 0.32 149788. 0.3465 35.37 0.4669 0.7173 0.0704 0.0458 0.756 11.906 5.747 563.436 1.345 25.562 4.626 0.32 150170. 0.3254 37.73 0.4980 0.7381 0.0662 0.0447 0.736 11.604 5.403 549.147 1.311 24.033 4.463 0.32 150573. 0.3043 40.09 0.5291 0.7564 0.0618 0.0432 0.712 11.218 5.038 530.911 1.267 22.408 4.304 0.32 150995. 0.2834 42.44 0.5603 0.7719 0.0570 0.0414 0.682 10.753 4.654 508.891 1.215 20.701 4.148 0.32 151439. 0.2625 44.80 0.5914 0.7843 0.0522 0.0393 0.648 10.212 4.255 483.266 1.154 18.926 3.993 0.32 151902. 0.2417 47.16 0.6225 0.7934 0.0471 0.0370 0.609 9.598 3.843 454.215 1.084 17.093 3.837 0.32 152386. 0.2207 49.52 0.6536 0.7983 0.0419 0.0343 0.566 8.915 3.421 421.922 1.007 15.216 3.677 0.32 152889. 0.1995 51.88 0.6848 0.7981 0.0367 0.0315 0.518 8.169 2.991 386.577 0.923 13.304 3.509 0.32 153412. 0.1781 54.23 0.7159 0.7912 0.0313 0.0283 0.467 7.362 2.556 348.388 0.832 11.370 3.328 0.33 153955. 0.1561 56.59 0.7470 0.7751 0.0260 0.0250 0.412 6.500 2.119 307.596 0.734 9.424 3.124 0.33 154517. 0.1334 58.95 0.7781 0.7453 0.0206 0.0215 0.355 5.589 1.682 264.481 0.631 7.480 2.884 0.33 155099. 0.1097 61.31 0.8093 0.6934 0.0153 0.0179 0.294 4.636 1.248 219.379 0.524 5.550 2.580 0.33 155700. 0.0846 63.67 0.8404 0.6017 0.0101 0.0141 0.232 3.649 0.821 172.690 0.412 3.651 2.156 0.33 156320. 0.0573 66.02 0.8715 0.4247 0.0050 0.0102 0.167 2.639 0.404 124.879 0.298 1.797 1.467 0.33 156959. 0.0274 68.38 0.9026 0.0003 0.0000 0.0062 0.102 1.613 0.000 76.339 0.182 0.001 0.001 0.33 157609. 0.0000 PROP RPM = 5000 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 0.1023 0.0385 1.239 15.621 13.041 924.073 1.765 58.007 6.401 0.40 183147. 0.6782 2.95 0.0311 0.0801 0.1015 0.0395 1.271 16.017 12.943 947.511 1.810 57.572 6.196 0.40 183297. 0.6540 5.90 0.0623 0.1549 0.1007 0.0405 1.303 16.424 12.832 971.595 1.856 57.075 5.990 0.40 183464. 0.6295 8.85 0.0934 0.2244 0.0997 0.0415 1.336 16.836 12.704 995.972 1.902 56.508 5.785 0.40 183651. 0.6050 11.80 0.1246 0.2888 0.0985 0.0425 1.368 17.247 12.558 1020.236 1.949 55.859 5.583 0.40 183858. 0.5805 14.75 0.1557 0.3481 0.0972 0.0435 1.400 17.647 12.392 1043.904 1.994 55.118 5.384 0.40 184087. 0.5561 17.70 0.1869 0.4026 0.0957 0.0444 1.430 18.027 12.202 1066.426 2.037 54.275 5.190 0.40 184338. 0.5319 20.65 0.2180 0.4526 0.0940 0.0453 1.458 18.378 11.987 1087.183 2.076 53.317 5.001 0.40 184612. 0.5080 23.60 0.2492 0.4984 0.0921 0.0461 1.483 18.688 11.743 1105.503 2.111 52.235 4.818 0.40 184911. 0.4844 26.54 0.2803 0.5402 0.0900 0.0467 1.503 18.944 11.469 1120.669 2.140 51.016 4.642 0.40 185234. 0.4612 29.49 0.3115 0.5783 0.0876 0.0472 1.518 19.134 11.162 1131.918 2.162 49.651 4.473 0.40 185583. 0.4384 32.44 0.3426 0.6131 0.0849 0.0474 1.527 19.245 10.820 1138.466 2.174 48.128 4.311 0.40 185957. 0.4160 35.39 0.3737 0.6448 0.0819 0.0475 1.528 19.263 10.441 1139.509 2.176 46.440 4.156 0.40 186357. 0.3940 38.34 0.4049 0.6736 0.0786 0.0473 1.521 19.174 10.022 1134.258 2.166 44.578 4.008 0.40 186783. 0.3722 41.29 0.4360 0.6998 0.0750 0.0467 1.505 18.966 9.563 1121.951 2.143 42.535 3.866 0.40 187235. 0.3507 44.24 0.4672 0.7234 0.0711 0.0459 1.478 18.627 9.062 1101.899 2.104 40.306 3.730 0.40 187714. 0.3294 47.19 0.4983 0.7446 0.0668 0.0447 1.440 18.152 8.521 1073.814 2.051 37.902 3.599 0.40 188218. 0.3082 50.14 0.5295 0.7633 0.0623 0.0432 1.392 17.544 7.946 1037.841 1.982 35.343 3.473 0.40 188747. 0.2872 53.09 0.5606 0.7794 0.0576 0.0414 1.333 16.808 7.341 994.295 1.899 32.653 3.349 0.40 189302. 0.2662 56.04 0.5918 0.7926 0.0527 0.0393 1.265 15.950 6.711 943.524 1.802 29.853 3.226 0.40 189883. 0.2452 58.99 0.6229 0.8025 0.0476 0.0369 1.188 14.975 6.061 885.887 1.692 26.961 3.103 0.40 190488. 0.2242 61.94 0.6541 0.8086 0.0423 0.0342 1.102 13.891 5.395 821.744 1.569 23.998 2.978 0.41 191118. 0.2029 64.89 0.6852 0.8098 0.0370 0.0313 1.008 12.703 4.717 751.474 1.435 20.980 2.847 0.41 191773. 0.1814 67.84 0.7163 0.8047 0.0316 0.0281 0.906 11.419 4.030 675.496 1.290 17.925 2.706 0.41 192453. 0.1594 70.79 0.7475 0.7908 0.0262 0.0248 0.797 10.046 3.339 594.288 1.135 14.852 2.548 0.41 193157. 0.1366 73.73 0.7786 0.7638 0.0208 0.0212 0.682 8.595 2.649 508.417 0.971 11.781 2.363 0.41 193885. 0.1128 76.68 0.8098 0.7153 0.0154 0.0174 0.561 7.075 1.963 418.557 0.799 8.733 2.128 0.41 194637. 0.0875 79.63 0.8409 0.6270 0.0101 0.0136 0.437 5.503 1.289 325.519 0.622 5.733 1.796 0.41 195414. 0.0598 82.58 0.8721 0.4499 0.0049 0.0096 0.309 3.892 0.631 230.247 0.440 2.806 1.243 0.41 196214. 0.0290 85.53 0.9032 -0.0087 -0.0001 0.0056 0.179 2.256 -0.007 133.474 0.255 -0.030 -0.023 0.41 197024. 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 0.1029 0.0385 2.142 22.500 18.885 1597.243 2.542 83.998 5.363 0.48 219766. 0.6837 3.54 0.0311 0.0805 0.1021 0.0395 2.197 23.081 18.750 1638.453 2.608 83.399 5.190 0.48 219945. 0.6594 7.08 0.0623 0.1557 0.1013 0.0405 2.254 23.679 18.595 1680.880 2.675 82.712 5.018 0.48 220146. 0.6348 10.62 0.0934 0.2256 0.1003 0.0416 2.312 24.285 18.418 1723.912 2.744 81.923 4.846 0.48 220371. 0.6101 14.16 0.1246 0.2902 0.0992 0.0426 2.369 24.889 18.214 1766.832 2.812 81.017 4.676 0.48 220619. 0.5855 17.70 0.1557 0.3498 0.0980 0.0436 2.426 25.481 17.981 1808.797 2.879 79.979 4.509 0.48 220894. 0.5609 21.24 0.1869 0.4046 0.0965 0.0446 2.479 26.044 17.714 1848.820 2.942 78.791 4.346 0.48 221195. 0.5366 24.78 0.2180 0.4548 0.0948 0.0455 2.529 26.566 17.409 1885.816 3.001 77.436 4.187 0.48 221525. 0.5126 28.31 0.2492 0.5007 0.0930 0.0463 2.573 27.027 17.063 1918.584 3.054 75.898 4.034 0.48 221883. 0.4889 31.85 0.2803 0.5427 0.0908 0.0469 2.609 27.411 16.673 1945.848 3.097 74.161 3.886 0.48 222272. 0.4656 35.39 0.3115 0.5810 0.0884 0.0474 2.637 27.699 16.234 1966.261 3.129 72.208 3.745 0.48 222690. 0.4427 38.93 0.3426 0.6160 0.0858 0.0477 2.653 27.870 15.743 1978.423 3.149 70.024 3.609 0.48 223140. 0.4201 42.47 0.3738 0.6479 0.0828 0.0478 2.656 27.905 15.197 1980.914 3.153 67.595 3.480 0.48 223621. 0.3980 46.01 0.4049 0.6769 0.0795 0.0476 2.645 27.784 14.593 1972.334 3.139 64.911 3.356 0.48 224133. 0.3761 49.55 0.4360 0.7033 0.0759 0.0470 2.617 27.489 13.930 1951.331 3.106 61.959 3.238 0.48 224676. 0.3545 53.09 0.4672 0.7273 0.0719 0.0462 2.570 27.000 13.204 1916.677 3.050 58.733 3.125 0.48 225250. 0.3331 56.63 0.4983 0.7488 0.0677 0.0450 2.505 26.312 12.421 1867.815 2.973 55.247 3.016 0.48 225856. 0.3119 60.17 0.5295 0.7679 0.0631 0.0435 2.421 25.427 11.585 1804.973 2.873 51.532 2.911 0.48 226492. 0.2907 63.71 0.5606 0.7846 0.0583 0.0417 2.318 24.352 10.706 1728.692 2.751 47.622 2.809 0.48 227159. 0.2697 67.25 0.5918 0.7984 0.0533 0.0395 2.199 23.097 9.790 1639.584 2.609 43.546 2.708 0.48 227857. 0.2486 70.79 0.6229 0.8092 0.0482 0.0371 2.063 21.670 8.843 1538.277 2.448 39.335 2.608 0.49 228584. 0.2275 74.33 0.6541 0.8162 0.0429 0.0344 1.912 20.080 7.872 1425.410 2.269 35.016 2.505 0.49 229341. 0.2062 77.87 0.6852 0.8187 0.0375 0.0314 1.746 18.336 6.883 1301.652 2.072 30.616 2.398 0.49 230127. 0.1846 81.40 0.7164 0.8152 0.0320 0.0282 1.566 16.450 5.881 1167.744 1.859 26.159 2.284 0.49 230943. 0.1625 84.94 0.7475 0.8033 0.0265 0.0247 1.374 14.433 4.873 1024.536 1.631 21.674 2.157 0.49 231788. 0.1397 88.48 0.7787 0.7788 0.0211 0.0210 1.171 12.298 3.865 873.032 1.389 17.190 2.008 0.49 232662. 0.1158 92.02 0.8098 0.7335 0.0156 0.0172 0.958 10.064 2.864 714.436 1.137 12.739 1.818 0.49 233565. 0.0903 95.56 0.8409 0.6489 0.0102 0.0133 0.738 7.751 1.879 550.193 0.876 8.357 1.549 0.49 234497. 0.0623 99.10 0.8721 0.4734 0.0050 0.0092 0.512 5.381 0.918 381.994 0.608 4.081 1.090 0.49 235457. 0.0306 102.64 0.9032 -0.0136 -0.0001 0.0051 0.283 2.973 -0.014 211.077 0.336 -0.062 -0.030 0.50 236428. 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 0.1036 0.0387 3.418 30.773 25.872 2548.593 3.477 115.080 4.604 0.56 256379. 0.6871 4.16 0.0314 0.0813 0.1029 0.0397 3.508 31.585 25.698 2615.855 3.569 114.304 4.456 0.56 256589. 0.6627 8.32 0.0628 0.1572 0.1020 0.0408 3.601 32.424 25.497 2685.278 3.663 113.409 4.307 0.56 256826. 0.6380 12.49 0.0942 0.2276 0.1011 0.0418 3.696 33.276 25.264 2755.853 3.759 112.374 4.158 0.56 257090. 0.6132 16.65 0.1256 0.2928 0.1000 0.0429 3.790 34.128 24.995 2826.398 3.856 111.178 4.011 0.56 257383. 0.5883 20.81 0.1570 0.3528 0.0988 0.0440 3.883 34.962 24.685 2895.494 3.950 109.797 3.867 0.56 257707. 0.5636 24.97 0.1884 0.4079 0.0974 0.0450 3.971 35.759 24.327 2961.496 4.040 108.206 3.726 0.56 258063. 0.5391 29.13 0.2198 0.4584 0.0957 0.0459 4.053 36.496 23.916 3022.557 4.123 106.380 3.589 0.56 258453. 0.5149 33.30 0.2512 0.5046 0.0938 0.0467 4.126 37.149 23.447 3076.654 4.197 104.294 3.457 0.56 258877. 0.4911 37.46 0.2825 0.5468 0.0917 0.0474 4.186 37.692 22.914 3121.625 4.258 101.923 3.329 0.56 259337. 0.4676 41.62 0.3139 0.5852 0.0893 0.0479 4.231 38.098 22.312 3155.193 4.304 99.245 3.207 0.56 259832. 0.4445 45.78 0.3453 0.6204 0.0866 0.0482 4.258 38.337 21.636 3175.006 4.331 96.238 3.091 0.56 260365. 0.4218 49.94 0.3767 0.6524 0.0836 0.0483 4.263 38.381 20.882 3178.686 4.336 92.881 2.980 0.56 260934. 0.3995 54.11 0.4081 0.6816 0.0802 0.0480 4.243 38.203 20.044 3163.885 4.316 89.158 2.874 0.56 261541. 0.3774 58.27 0.4395 0.7082 0.0765 0.0475 4.195 37.774 19.122 3128.354 4.268 85.053 2.772 0.56 262185. 0.3557 62.43 0.4709 0.7323 0.0725 0.0466 4.117 37.070 18.111 3070.080 4.188 80.557 2.676 0.56 262866. 0.3341 66.59 0.5023 0.7541 0.0681 0.0454 4.007 36.082 17.017 2988.235 4.077 75.694 2.583 0.56 263583. 0.3126 70.76 0.5337 0.7735 0.0634 0.0438 3.866 34.814 15.851 2883.243 3.933 70.506 2.494 0.56 264338. 0.2913 74.92 0.5651 0.7904 0.0585 0.0418 3.696 33.278 14.623 2756.020 3.760 65.043 2.407 0.56 265128. 0.2700 79.08 0.5965 0.8046 0.0534 0.0396 3.497 31.486 13.343 2607.597 3.557 59.347 2.321 0.57 265954. 0.2487 83.24 0.6279 0.8157 0.0481 0.0370 3.271 29.450 12.019 2439.027 3.327 53.462 2.235 0.57 266815. 0.2273 87.40 0.6593 0.8231 0.0427 0.0342 3.019 27.185 10.662 2251.384 3.071 47.425 2.148 0.57 267712. 0.2058 91.57 0.6907 0.8258 0.0371 0.0311 2.743 24.702 9.279 2045.806 2.791 41.275 2.057 0.57 268643. 0.1839 95.73 0.7221 0.8225 0.0315 0.0277 2.445 22.019 7.880 1823.558 2.488 35.048 1.960 0.57 269610. 0.1614 99.89 0.7535 0.8104 0.0259 0.0241 2.127 19.152 6.472 1586.111 2.164 28.785 1.851 0.57 270610. 0.1381 104.05 0.7848 0.7849 0.0203 0.0203 1.791 16.122 5.065 1335.205 1.821 22.529 1.721 0.57 271645. 0.1136 108.21 0.8162 0.7361 0.0147 0.0163 1.439 12.955 3.671 1072.940 1.464 16.326 1.552 0.57 272715. 0.0872 112.38 0.8476 0.6409 0.0092 0.0122 1.075 9.682 2.300 801.843 1.094 10.230 1.301 0.58 273818. 0.0579 116.54 0.8790 0.4264 0.0039 0.0080 0.704 6.337 0.966 524.855 0.716 4.296 0.835 0.58 274953. 0.0241 120.70 0.9104 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 0.1043 0.0390 5.148 40.559 34.045 3838.856 4.582 151.434 4.023 0.63 292984. 0.6886 4.71 0.0311 0.0805 0.1037 0.0401 5.284 41.632 33.837 3940.412 4.704 150.508 3.895 0.63 293222. 0.6647 9.43 0.0622 0.1557 0.1029 0.0411 5.425 42.743 33.596 4045.580 4.829 149.433 3.767 0.63 293489. 0.6405 14.14 0.0933 0.2256 0.1021 0.0422 5.569 43.877 33.315 4152.888 4.957 148.183 3.639 0.63 293787. 0.6161 18.86 0.1245 0.2903 0.1011 0.0433 5.714 45.014 32.988 4260.587 5.086 146.729 3.512 0.64 294118. 0.5917 23.57 0.1556 0.3500 0.0999 0.0444 5.856 46.134 32.607 4366.560 5.212 145.037 3.387 0.64 294483. 0.5674 28.29 0.1867 0.4049 0.0986 0.0454 5.992 47.209 32.166 4468.326 5.334 143.075 3.265 0.64 294885. 0.5433 33.00 0.2178 0.4552 0.0970 0.0464 6.119 48.211 31.657 4563.104 5.447 140.809 3.147 0.64 295324. 0.5194 37.71 0.2489 0.5013 0.0952 0.0473 6.233 49.106 31.071 4647.829 5.548 138.203 3.032 0.64 295802. 0.4959 42.43 0.2800 0.5435 0.0932 0.0480 6.329 49.860 30.401 4719.230 5.633 135.224 2.922 0.64 296321. 0.4727 47.14 0.3111 0.5820 0.0908 0.0486 6.402 50.437 29.640 4773.850 5.698 131.841 2.816 0.64 296880. 0.4498 51.86 0.3423 0.6173 0.0882 0.0489 6.448 50.799 28.782 4808.135 5.739 128.023 2.715 0.64 297480. 0.4274 56.57 0.3734 0.6495 0.0853 0.0490 6.462 50.909 27.820 4818.484 5.752 123.742 2.619 0.64 298122. 0.4052 61.29 0.4045 0.6789 0.0820 0.0488 6.439 50.728 26.748 4801.349 5.731 118.976 2.527 0.64 298806. 0.3834 66.00 0.4356 0.7058 0.0783 0.0483 6.374 50.220 25.563 4753.337 5.674 113.705 2.439 0.64 299531. 0.3618 70.72 0.4667 0.7303 0.0743 0.0475 6.264 49.354 24.261 4671.302 5.576 107.913 2.356 0.64 300299. 0.3404 75.43 0.4978 0.7525 0.0700 0.0463 6.106 48.110 22.847 4553.567 5.435 101.621 2.276 0.64 301107. 0.3191 80.14 0.5289 0.7725 0.0654 0.0448 5.901 46.493 21.332 4400.496 5.253 94.884 2.199 0.64 301957. 0.2979 84.86 0.5601 0.7902 0.0605 0.0429 5.650 44.516 19.731 4213.383 5.029 87.764 2.124 0.64 302847. 0.2768 89.57 0.5912 0.8053 0.0553 0.0406 5.356 42.195 18.058 3993.764 4.767 80.320 2.051 0.65 303778. 0.2557 94.29 0.6223 0.8176 0.0500 0.0381 5.020 39.548 16.324 3743.224 4.468 72.609 1.978 0.65 304748. 0.2345 99.00 0.6534 0.8265 0.0446 0.0352 4.644 36.592 14.542 3463.382 4.134 64.681 1.904 0.65 305757. 0.2131 103.72 0.6845 0.8313 0.0390 0.0321 4.232 33.343 12.722 3155.933 3.767 56.587 1.828 0.65 306806. 0.1913 108.43 0.7156 0.8307 0.0333 0.0287 3.785 29.823 10.876 2822.747 3.369 48.376 1.748 0.65 307894. 0.1691 113.14 0.7468 0.8225 0.0276 0.0251 3.307 26.054 9.015 2465.957 2.944 40.100 1.658 0.65 309020. 0.1461 117.86 0.7779 0.8027 0.0219 0.0212 2.800 22.061 7.152 2088.100 2.492 31.814 1.554 0.65 310184. 0.1219 122.57 0.8090 0.7635 0.0162 0.0172 2.269 17.879 5.301 1692.220 2.020 23.579 1.421 0.66 311387. 0.0960 127.29 0.8401 0.6863 0.0107 0.0130 1.719 13.545 3.476 1282.003 1.530 15.463 1.230 0.66 312628. 0.0673 132.00 0.8712 0.5164 0.0052 0.0088 1.156 9.105 1.695 861.801 1.029 7.541 0.892 0.66 313906. 0.0341 136.72 0.9023 -0.0204 -0.0001 0.0044 0.583 4.592 -0.033 434.589 0.519 -0.145 -0.034 0.66 315193. 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 0.1052 0.0400 7.505 52.556 43.443 5596.185 5.938 193.237 3.521 0.71 329580. 0.6809 5.29 0.0311 0.0793 0.1046 0.0410 7.695 53.891 43.209 5738.384 6.089 192.192 3.415 0.71 329847. 0.6586 10.59 0.0621 0.1536 0.1040 0.0420 7.893 55.279 42.934 5886.176 6.245 190.969 3.308 0.71 330146. 0.6360 15.88 0.0932 0.2229 0.1032 0.0431 8.097 56.701 42.611 6037.562 6.406 189.533 3.201 0.71 330479. 0.6130 21.18 0.1242 0.2873 0.1023 0.0442 8.301 58.134 42.231 6190.165 6.568 187.844 3.094 0.71 330850. 0.5900 26.47 0.1553 0.3469 0.1012 0.0453 8.504 59.551 41.785 6341.063 6.728 185.858 2.989 0.71 331260. 0.5668 31.77 0.1864 0.4018 0.0999 0.0463 8.699 60.920 41.261 6486.794 6.883 183.530 2.885 0.72 331710. 0.5437 37.06 0.2174 0.4523 0.0984 0.0473 8.882 62.203 40.650 6623.436 7.028 180.812 2.784 0.72 332204. 0.5207 42.35 0.2485 0.4986 0.0967 0.0482 9.047 63.359 39.940 6746.559 7.158 177.655 2.685 0.72 332741. 0.4979 47.65 0.2795 0.5410 0.0947 0.0489 9.188 64.344 39.122 6851.393 7.270 174.013 2.590 0.72 333323. 0.4753 52.94 0.3106 0.5798 0.0925 0.0495 9.297 65.109 38.184 6932.841 7.356 169.841 2.498 0.72 333951. 0.4529 58.24 0.3417 0.6153 0.0899 0.0499 9.368 65.604 37.117 6985.571 7.412 165.098 2.410 0.72 334625. 0.4308 63.53 0.3727 0.6478 0.0870 0.0500 9.393 65.778 35.914 7004.113 7.432 159.745 2.326 0.72 335347. 0.4089 68.83 0.4038 0.6774 0.0837 0.0499 9.364 65.580 34.566 6983.019 7.409 153.751 2.245 0.72 336115. 0.3873 74.12 0.4348 0.7046 0.0801 0.0494 9.276 64.960 33.069 6917.030 7.339 147.090 2.168 0.72 336931. 0.3658 79.41 0.4659 0.7294 0.0761 0.0486 9.121 63.873 31.417 6801.237 7.216 139.741 2.095 0.72 337794. 0.3445 84.71 0.4970 0.7521 0.0717 0.0474 8.895 62.291 29.614 6632.771 7.038 131.725 2.025 0.72 338703. 0.3233 90.00 0.5280 0.7725 0.0670 0.0458 8.599 60.217 27.678 6411.929 6.803 123.110 1.958 0.72 339658. 0.3022 95.30 0.5591 0.7908 0.0620 0.0439 8.235 57.668 25.624 6140.531 6.515 113.977 1.893 0.73 340658. 0.2811 100.59 0.5901 0.8066 0.0568 0.0416 7.806 54.666 23.473 5820.849 6.176 104.406 1.829 0.73 341704. 0.2600 105.89 0.6212 0.8197 0.0514 0.0390 7.316 51.232 21.238 5455.248 5.788 94.469 1.766 0.73 342794. 0.2388 111.18 0.6523 0.8297 0.0459 0.0360 6.767 47.390 18.937 5046.134 5.354 84.234 1.702 0.73 343927. 0.2173 116.47 0.6833 0.8357 0.0402 0.0328 6.163 43.163 16.584 4596.056 4.877 73.766 1.637 0.73 345105. 0.1955 121.77 0.7144 0.8366 0.0344 0.0293 5.509 38.579 14.193 4107.867 4.359 63.132 1.567 0.73 346326. 0.1732 127.06 0.7454 0.8302 0.0285 0.0256 4.807 33.667 11.780 3584.892 3.804 52.398 1.490 0.73 347590. 0.1501 132.36 0.7765 0.8128 0.0227 0.0217 4.065 28.467 9.361 3031.168 3.216 41.637 1.401 0.74 348897. 0.1257 137.65 0.8076 0.7763 0.0168 0.0175 3.288 23.025 6.953 2451.677 2.601 30.928 1.286 0.74 350247. 0.0995 142.95 0.8386 0.7023 0.0111 0.0132 2.484 17.399 4.577 1852.610 1.966 20.360 1.121 0.74 351639. 0.0703 148.24 0.8697 0.5355 0.0055 0.0089 1.665 11.659 2.255 1241.483 1.317 10.031 0.824 0.74 353072. 0.0363 153.53 0.9007 0.0003 0.0000 0.0045 0.837 5.863 0.001 624.279 0.662 0.003 0.000 0.74 354520. 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 0.1060 0.0432 11.112 70.039 54.072 8286.425 7.913 240.514 2.960 0.79 366165. 0.6385 5.87 0.0310 0.0742 0.1056 0.0441 11.357 71.583 53.825 8469.171 8.087 239.415 2.883 0.79 366460. 0.6205 11.74 0.0620 0.1444 0.1050 0.0451 11.611 73.184 53.533 8658.498 8.268 238.116 2.804 0.79 366790. 0.6020 17.62 0.0930 0.2105 0.1043 0.0461 11.870 74.815 53.186 8851.493 8.453 236.573 2.725 0.79 367159. 0.5831 23.49 0.1240 0.2725 0.1035 0.0471 12.129 76.448 52.773 9044.751 8.637 234.734 2.646 0.79 367569. 0.5640 29.36 0.1550 0.3306 0.1025 0.0481 12.383 78.049 52.280 9234.104 8.818 232.542 2.568 0.79 368022. 0.5447 35.23 0.1860 0.3847 0.1014 0.0490 12.625 79.576 51.694 9414.767 8.990 229.933 2.490 0.79 368521. 0.5253 41.11 0.2170 0.4351 0.1000 0.0499 12.849 80.984 50.999 9581.343 9.150 226.843 2.414 0.80 369067. 0.5058 46.98 0.2481 0.4819 0.0984 0.0507 13.045 82.223 50.181 9727.972 9.290 223.203 2.340 0.80 369662. 0.4862 52.85 0.2791 0.5253 0.0965 0.0513 13.207 83.241 49.224 9848.428 9.405 218.948 2.267 0.80 370308. 0.4666 58.72 0.3101 0.5654 0.0944 0.0517 13.325 83.983 48.115 9936.223 9.488 214.015 2.196 0.80 371005. 0.4470 64.60 0.3411 0.6026 0.0919 0.0520 13.390 84.392 46.840 9984.619 9.535 208.344 2.128 0.80 371753. 0.4272 70.47 0.3721 0.6368 0.0890 0.0520 13.392 84.410 45.387 9986.757 9.537 201.882 2.061 0.80 372555. 0.4074 76.34 0.4031 0.6684 0.0858 0.0517 13.324 83.980 43.746 9935.778 9.488 194.583 1.997 0.80 373408. 0.3875 82.21 0.4341 0.6973 0.0822 0.0512 13.175 83.043 41.909 9824.938 9.382 186.411 1.935 0.80 374315. 0.3675 88.09 0.4651 0.7238 0.0782 0.0502 12.938 81.545 39.869 9647.792 9.213 177.338 1.874 0.80 375273. 0.3472 93.96 0.4961 0.7479 0.0738 0.0490 12.605 79.450 37.631 9399.879 8.976 167.381 1.816 0.80 376283. 0.3268 99.83 0.5271 0.7697 0.0691 0.0473 12.178 76.753 35.212 9080.838 8.672 156.623 1.759 0.80 377344. 0.3062 105.70 0.5581 0.7892 0.0640 0.0453 11.657 73.471 32.637 8692.498 8.301 145.171 1.703 0.81 378455. 0.2854 111.58 0.5891 0.8060 0.0587 0.0429 11.048 69.631 29.929 8238.156 7.867 133.125 1.648 0.81 379616. 0.2645 117.45 0.6201 0.8200 0.0532 0.0402 10.354 65.257 27.109 7720.716 7.373 120.580 1.593 0.81 380826. 0.2433 123.32 0.6511 0.8306 0.0475 0.0372 9.579 60.376 24.196 7143.249 6.821 107.625 1.536 0.81 382085. 0.2217 129.19 0.6821 0.8371 0.0416 0.0339 8.729 55.020 21.211 6509.562 6.216 94.346 1.478 0.81 383392. 0.1997 135.07 0.7132 0.8378 0.0356 0.0303 7.811 49.233 18.171 5824.854 5.562 80.826 1.415 0.81 384746. 0.1770 140.94 0.7442 0.8303 0.0296 0.0265 6.833 43.068 15.097 5095.442 4.866 67.150 1.344 0.82 386148. 0.1532 146.81 0.7752 0.8097 0.0235 0.0225 5.806 36.593 12.008 4329.363 4.134 53.411 1.258 0.82 387597. 0.1279 152.68 0.8062 0.7664 0.0175 0.0184 4.742 29.889 8.927 3536.201 3.377 39.706 1.145 0.82 389094. 0.1004 158.56 0.8372 0.6796 0.0115 0.0142 3.658 23.055 5.879 2727.675 2.605 26.151 0.978 0.82 390636. 0.0695 164.43 0.8682 0.4935 0.0057 0.0100 2.571 16.204 2.894 1917.092 1.831 12.871 0.685 0.82 392224. 0.0342 170.30 0.8992 -0.0033 0.0000 0.0058 1.495 9.423 -0.011 1114.844 1.065 -0.048 -0.004 0.83 393832. 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 0.1065 0.0503 17.251 98.845 65.707 12863.973 11.167 292.265 2.317 0.87 402754. 0.5510 6.47 0.0311 0.0643 0.1061 0.0512 17.565 100.643 65.468 13097.975 11.371 291.202 2.267 0.87 403075. 0.5382 12.95 0.0621 0.1258 0.1057 0.0522 17.888 102.493 65.183 13338.723 11.580 289.935 2.216 0.87 403436. 0.5250 19.42 0.0932 0.1843 0.1051 0.0531 18.213 104.357 64.840 13581.396 11.790 288.410 2.165 0.87 403840. 0.5116 25.89 0.1243 0.2400 0.1044 0.0541 18.533 106.193 64.426 13820.216 11.998 286.565 2.114 0.87 404288. 0.4979 32.36 0.1553 0.2928 0.1036 0.0550 18.839 107.944 63.922 14048.126 12.195 284.323 2.064 0.87 404786. 0.4841 38.84 0.1864 0.3429 0.1026 0.0558 19.119 109.549 63.310 14256.976 12.377 281.601 2.014 0.87 405333. 0.4702 45.31 0.2175 0.3904 0.1014 0.0565 19.361 110.938 62.569 14437.823 12.534 278.308 1.966 0.87 405934. 0.4562 51.78 0.2485 0.4355 0.1000 0.0571 19.554 112.041 61.679 14581.376 12.658 274.347 1.919 0.88 406589. 0.4421 58.25 0.2796 0.4784 0.0982 0.0574 19.684 112.787 60.617 14678.435 12.743 269.624 1.873 0.88 407301. 0.4278 64.73 0.3107 0.5190 0.0962 0.0576 19.740 113.105 59.363 14719.870 12.779 264.044 1.829 0.88 408070. 0.4135 71.20 0.3418 0.5577 0.0938 0.0575 19.710 112.933 57.896 14697.487 12.759 257.521 1.787 0.88 408897. 0.3988 77.67 0.3728 0.5943 0.0911 0.0571 19.585 112.221 56.201 14604.828 12.679 249.982 1.745 0.88 409783. 0.3839 84.14 0.4039 0.6290 0.0880 0.0565 19.358 110.917 54.263 14435.108 12.531 241.362 1.705 0.88 410728. 0.3685 90.62 0.4350 0.6616 0.0844 0.0555 19.018 108.973 52.070 14182.028 12.312 231.609 1.665 0.88 411731. 0.3526 97.09 0.4660 0.6921 0.0804 0.0541 18.559 106.341 49.613 13839.485 12.014 220.680 1.626 0.88 412792. 0.3360 103.56 0.4971 0.7205 0.0760 0.0524 17.974 102.991 46.894 13403.559 11.636 208.587 1.587 0.88 413911. 0.3188 110.03 0.5282 0.7466 0.0712 0.0504 17.267 98.936 43.936 12875.782 11.178 195.429 1.548 0.88 415086. 0.3010 116.51 0.5592 0.7703 0.0661 0.0480 16.442 94.209 40.769 12260.611 10.644 181.341 1.508 0.89 416316. 0.2825 122.98 0.5903 0.7914 0.0607 0.0452 15.506 88.845 37.422 11562.607 10.038 166.452 1.468 0.89 417602. 0.2635 129.45 0.6214 0.8085 0.0550 0.0423 14.483 82.988 33.921 10800.300 9.376 150.882 1.425 0.89 418942. 0.2434 135.93 0.6524 0.8206 0.0491 0.0390 13.380 76.666 30.294 9977.591 8.662 134.749 1.377 0.89 420335. 0.2224 142.40 0.6835 0.8258 0.0431 0.0356 12.215 69.988 26.565 9108.470 7.907 118.159 1.323 0.89 421781. 0.2000 148.87 0.7146 0.8202 0.0369 0.0321 11.013 63.104 22.754 8212.592 7.129 101.209 1.257 0.89 423279. 0.1759 155.34 0.7456 0.8021 0.0306 0.0285 9.757 55.907 18.894 7275.876 6.316 84.040 1.178 0.90 424829. 0.1502 161.82 0.7767 0.7651 0.0243 0.0247 8.467 48.513 15.014 6313.656 5.481 66.780 1.079 0.90 426431. 0.1226 168.29 0.8078 0.6977 0.0181 0.0209 7.167 41.065 11.143 5344.283 4.639 49.563 0.946 0.90 428084. 0.0926 174.76 0.8389 0.5798 0.0119 0.0172 5.882 33.702 7.318 4386.119 3.808 32.552 0.757 0.90 429788. 0.0601 181.23 0.8699 0.3731 0.0058 0.0135 4.638 26.577 3.581 3458.815 3.003 15.927 0.470 0.91 431542. 0.0261 187.71 0.9010 -0.0059 -0.0001 0.0101 3.449 19.761 -0.041 2571.742 2.233 -0.181 -0.007 0.91 433332. 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 0.1041 0.0570 25.376 133.282 76.400 18922.645 15.058 339.828 1.831 0.95 439463. 0.4696 7.37 0.0324 0.0580 0.1038 0.0580 25.811 135.571 76.178 19247.557 15.317 338.841 1.795 0.95 439822. 0.4597 14.73 0.0648 0.1135 0.1034 0.0590 26.272 137.988 75.914 19590.732 15.590 337.665 1.758 0.95 440227. 0.4493 22.10 0.0972 0.1665 0.1030 0.0601 26.748 140.491 75.594 19946.078 15.873 336.242 1.719 0.95 440683. 0.4385 29.47 0.1297 0.2170 0.1024 0.0612 27.230 143.022 75.201 20305.477 16.159 334.496 1.680 0.95 441192. 0.4274 36.83 0.1621 0.2649 0.1018 0.0623 27.703 145.507 74.716 20658.256 16.439 332.335 1.640 0.95 441758. 0.4160 44.20 0.1945 0.3103 0.1009 0.0633 28.149 147.851 74.112 20991.082 16.704 329.651 1.601 0.95 442384. 0.4045 51.57 0.2269 0.3534 0.0999 0.0642 28.548 149.943 73.363 21287.980 16.940 326.321 1.563 0.95 443073. 0.3928 58.93 0.2593 0.3943 0.0987 0.0649 28.873 151.651 72.438 21530.555 17.133 322.205 1.526 0.96 443828. 0.3810 66.30 0.2917 0.4332 0.0971 0.0654 29.098 152.834 71.303 21698.482 17.267 317.156 1.490 0.96 444651. 0.3692 73.67 0.3241 0.4705 0.0952 0.0656 29.195 153.340 69.923 21770.344 17.324 311.019 1.457 0.96 445543. 0.3574 81.03 0.3565 0.5063 0.0930 0.0655 29.134 153.020 68.264 21724.869 17.288 303.637 1.425 0.96 446505. 0.3455 88.40 0.3890 0.5409 0.0903 0.0649 28.888 151.731 66.290 21541.836 17.142 294.859 1.396 0.96 447539. 0.3334 95.77 0.4214 0.5745 0.0871 0.0639 28.435 149.352 63.971 21204.078 16.874 284.543 1.368 0.96 448644. 0.3211 103.13 0.4538 0.6070 0.0835 0.0624 27.764 145.828 61.286 20703.863 16.476 272.602 1.343 0.96 449821. 0.3084 110.50 0.4862 0.6385 0.0793 0.0604 26.869 141.124 58.222 20035.984 15.944 258.973 1.318 0.96 451068. 0.2951 117.87 0.5186 0.6687 0.0746 0.0579 25.755 135.272 54.794 19205.143 15.283 243.724 1.294 0.96 452384. 0.2810 125.23 0.5510 0.6974 0.0695 0.0549 24.440 128.370 51.039 18225.240 14.503 227.020 1.270 0.97 453768. 0.2662 132.60 0.5834 0.7241 0.0640 0.0516 22.950 120.540 47.000 17113.518 13.619 209.054 1.246 0.97 455218. 0.2505 139.97 0.6158 0.7484 0.0582 0.0479 21.305 111.902 42.721 15887.138 12.643 190.022 1.220 0.97 456733. 0.2339 147.33 0.6483 0.7672 0.0521 0.0440 19.581 102.848 38.238 14601.798 11.620 170.082 1.188 0.97 458312. 0.2155 154.70 0.6807 0.7780 0.0457 0.0400 17.810 93.544 33.591 13280.813 10.569 149.415 1.147 0.97 459954. 0.1951 162.07 0.7131 0.7712 0.0392 0.0363 16.141 84.778 28.803 12036.316 9.578 128.114 1.085 0.98 461658. 0.1709 169.43 0.7455 0.7358 0.0326 0.0330 14.679 77.098 23.906 10945.899 8.710 106.333 0.991 0.98 463423. 0.1421 176.80 0.7779 0.6768 0.0259 0.0297 13.230 69.491 18.993 9865.957 7.851 84.483 0.873 0.98 465249. 0.1116 184.17 0.8103 0.5870 0.0193 0.0266 11.827 62.121 14.137 8819.580 7.018 62.881 0.727 0.98 467136. 0.0802 191.53 0.8427 0.4579 0.0128 0.0236 10.499 55.142 9.412 7828.795 6.230 41.864 0.545 0.99 469084. 0.0491 198.90 0.8752 0.2795 0.0067 0.0208 9.269 48.686 4.885 6912.189 5.501 21.730 0.321 0.99 471099. 0.0208 206.27 0.9076 0.0389 0.0008 0.0183 8.131 42.709 0.575 6063.629 4.825 2.558 0.043 0.99 473220. 0.0010 213.63 0.9400