18.1x10 (181x10.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 0.0423 0.007 0.417 0.345 4.929 0.047 1.533 31.710 0.07 39306. 0.6035 0.43 0.0248 0.0576 0.0992 0.0427 0.007 0.421 0.339 4.981 0.048 1.508 30.880 0.07 39335. 0.5830 0.85 0.0497 0.1121 0.0974 0.0431 0.007 0.425 0.333 5.029 0.048 1.482 30.051 0.07 39365. 0.5624 1.28 0.0745 0.1636 0.0956 0.0435 0.007 0.429 0.327 5.072 0.048 1.454 29.226 0.07 39399. 0.5416 1.70 0.0993 0.2120 0.0935 0.0438 0.007 0.432 0.320 5.109 0.049 1.423 28.405 0.07 39434. 0.5208 2.13 0.1241 0.2574 0.0914 0.0441 0.007 0.434 0.313 5.137 0.049 1.390 27.591 0.07 39473. 0.5000 2.55 0.1490 0.2998 0.0890 0.0442 0.007 0.436 0.305 5.157 0.049 1.355 26.784 0.07 39514. 0.4792 2.98 0.1738 0.3393 0.0865 0.0443 0.007 0.437 0.296 5.167 0.049 1.317 25.983 0.07 39559. 0.4583 3.40 0.1986 0.3760 0.0839 0.0443 0.007 0.437 0.287 5.165 0.049 1.276 25.191 0.07 39606. 0.4374 3.83 0.2235 0.4098 0.0810 0.0442 0.007 0.435 0.277 5.149 0.049 1.232 24.405 0.07 39656. 0.4165 4.26 0.2483 0.4408 0.0780 0.0439 0.007 0.433 0.267 5.119 0.049 1.186 23.626 0.07 39710. 0.3955 4.68 0.2731 0.4690 0.0747 0.0435 0.007 0.429 0.256 5.073 0.048 1.137 22.851 0.07 39766. 0.3745 5.11 0.2980 0.4943 0.0713 0.0430 0.007 0.424 0.244 5.011 0.048 1.085 22.080 0.07 39826. 0.3535 5.53 0.3228 0.5168 0.0678 0.0423 0.007 0.417 0.232 4.933 0.047 1.031 21.309 0.07 39889. 0.3326 5.96 0.3476 0.5364 0.0640 0.0415 0.006 0.409 0.219 4.838 0.046 0.974 20.536 0.07 39955. 0.3116 6.38 0.3724 0.5529 0.0602 0.0405 0.006 0.399 0.206 4.726 0.045 0.916 19.757 0.07 40024. 0.2906 6.81 0.3973 0.5662 0.0562 0.0394 0.006 0.389 0.192 4.598 0.044 0.855 18.966 0.07 40097. 0.2696 7.23 0.4221 0.5759 0.0521 0.0382 0.006 0.376 0.178 4.452 0.043 0.793 18.158 0.07 40173. 0.2485 7.66 0.4469 0.5819 0.0479 0.0368 0.006 0.363 0.164 4.290 0.041 0.729 17.326 0.07 40252. 0.2274 8.09 0.4718 0.5835 0.0436 0.0353 0.006 0.348 0.149 4.112 0.039 0.664 16.460 0.07 40335. 0.2061 8.51 0.4966 0.5802 0.0392 0.0336 0.005 0.331 0.134 3.916 0.037 0.597 15.548 0.07 40421. 0.1847 8.94 0.5214 0.5710 0.0348 0.0318 0.005 0.313 0.119 3.702 0.035 0.529 14.575 0.07 40510. 0.1630 9.36 0.5462 0.5548 0.0303 0.0298 0.005 0.293 0.103 3.472 0.033 0.460 13.518 0.07 40603. 0.1410 9.79 0.5711 0.5298 0.0257 0.0277 0.004 0.273 0.088 3.225 0.031 0.390 12.347 0.07 40699. 0.1186 10.21 0.5959 0.4934 0.0210 0.0254 0.004 0.250 0.072 2.961 0.028 0.320 11.018 0.07 40799. 0.0958 10.64 0.6207 0.4416 0.0164 0.0230 0.004 0.227 0.056 2.680 0.026 0.249 9.467 0.07 40902. 0.0726 11.07 0.6456 0.3682 0.0117 0.0205 0.003 0.202 0.040 2.384 0.023 0.177 7.591 0.07 41008. 0.0492 11.49 0.6704 0.2628 0.0070 0.0178 0.003 0.175 0.024 2.073 0.020 0.106 5.218 0.07 41118. 0.0261 11.92 0.6952 0.1064 0.0023 0.0150 0.002 0.148 0.008 1.748 0.017 0.035 2.036 0.07 41230. 0.0058 12.34 0.7200 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 0.1012 0.0382 0.048 1.507 1.385 35.659 0.170 6.160 17.617 0.14 78612. 0.6721 0.84 0.0245 0.0632 0.0997 0.0387 0.048 1.526 1.363 36.110 0.172 6.065 17.126 0.14 78667. 0.6483 1.68 0.0491 0.1227 0.0980 0.0392 0.049 1.544 1.340 36.532 0.174 5.961 16.640 0.14 78728. 0.6245 2.52 0.0736 0.1788 0.0961 0.0396 0.050 1.560 1.315 36.914 0.176 5.850 16.160 0.14 78794. 0.6008 3.36 0.0981 0.2314 0.0942 0.0399 0.050 1.574 1.288 37.248 0.178 5.730 15.686 0.14 78864. 0.5771 4.21 0.1227 0.2806 0.0920 0.0402 0.050 1.586 1.259 37.523 0.179 5.600 15.219 0.14 78940. 0.5536 5.05 0.1472 0.3266 0.0897 0.0405 0.051 1.594 1.228 37.730 0.180 5.461 14.761 0.14 79022. 0.5302 5.89 0.1717 0.3694 0.0873 0.0406 0.051 1.600 1.194 37.856 0.181 5.312 14.310 0.14 79109. 0.5070 6.73 0.1963 0.4091 0.0847 0.0406 0.051 1.601 1.158 37.890 0.181 5.153 13.868 0.14 79202. 0.4839 7.57 0.2208 0.4458 0.0819 0.0406 0.051 1.598 1.120 37.821 0.181 4.982 13.433 0.14 79301. 0.4609 8.41 0.2454 0.4796 0.0789 0.0404 0.050 1.591 1.079 37.636 0.180 4.801 13.007 0.14 79406. 0.4381 9.25 0.2699 0.5106 0.0757 0.0400 0.050 1.577 1.036 37.326 0.178 4.608 12.589 0.14 79517. 0.4154 10.09 0.2944 0.5388 0.0724 0.0396 0.049 1.559 0.990 36.886 0.176 4.405 12.177 0.14 79634. 0.3928 10.93 0.3190 0.5642 0.0689 0.0389 0.049 1.535 0.942 36.313 0.173 4.191 11.770 0.14 79757. 0.3704 11.78 0.3435 0.5868 0.0652 0.0382 0.048 1.505 0.892 35.605 0.170 3.969 11.368 0.14 79887. 0.3481 12.62 0.3680 0.6066 0.0614 0.0373 0.047 1.469 0.841 34.762 0.166 3.739 10.968 0.14 80023. 0.3260 13.46 0.3926 0.6235 0.0575 0.0362 0.045 1.428 0.787 33.783 0.161 3.501 10.568 0.14 80165. 0.3040 14.30 0.4171 0.6372 0.0535 0.0350 0.044 1.380 0.732 32.666 0.156 3.256 10.166 0.14 80314. 0.2820 15.14 0.4416 0.6476 0.0494 0.0337 0.042 1.327 0.676 31.409 0.150 3.006 9.758 0.15 80469. 0.2600 15.98 0.4662 0.6543 0.0452 0.0322 0.040 1.268 0.618 30.013 0.143 2.749 9.339 0.15 80631. 0.2380 16.82 0.4907 0.6568 0.0409 0.0305 0.038 1.203 0.559 28.474 0.136 2.487 8.906 0.15 80800. 0.2159 17.66 0.5152 0.6543 0.0365 0.0287 0.036 1.132 0.499 26.794 0.128 2.220 8.450 0.15 80975. 0.1935 18.50 0.5398 0.6458 0.0320 0.0268 0.033 1.055 0.438 24.971 0.119 1.949 7.961 0.15 81157. 0.1709 19.35 0.5643 0.6297 0.0275 0.0247 0.031 0.972 0.377 23.006 0.110 1.675 7.425 0.15 81345. 0.1477 20.19 0.5889 0.6036 0.0230 0.0224 0.028 0.883 0.314 20.901 0.100 1.398 6.820 0.15 81540. 0.1239 21.03 0.6134 0.5635 0.0184 0.0200 0.025 0.788 0.251 18.658 0.089 1.118 6.113 0.15 81742. 0.0994 21.87 0.6379 0.5030 0.0138 0.0175 0.022 0.688 0.188 16.282 0.078 0.838 5.247 0.15 81950. 0.0738 22.71 0.6625 0.4102 0.0091 0.0148 0.018 0.582 0.125 13.779 0.066 0.557 4.120 0.15 82165. 0.0473 23.55 0.6870 0.2609 0.0045 0.0120 0.015 0.472 0.062 11.158 0.053 0.276 2.527 0.15 82385. 0.0204 24.39 0.7115 -0.0049 -0.0001 0.0090 0.011 0.355 -0.001 8.408 0.040 -0.004 -0.046 0.15 82603. 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 0.1017 0.0367 0.155 3.252 3.130 115.425 0.367 13.923 12.300 0.22 117914. 0.7055 1.28 0.0249 0.0669 0.1001 0.0372 0.157 3.297 3.081 117.034 0.373 13.706 11.942 0.22 117999. 0.6796 2.56 0.0497 0.1299 0.0984 0.0377 0.159 3.340 3.028 118.538 0.377 13.470 11.588 0.22 118092. 0.6537 3.84 0.0746 0.1890 0.0965 0.0381 0.161 3.378 2.971 119.906 0.382 13.216 11.239 0.22 118192. 0.6280 5.12 0.0995 0.2444 0.0945 0.0385 0.162 3.412 2.909 121.105 0.385 12.941 10.897 0.22 118300. 0.6025 6.39 0.1243 0.2960 0.0924 0.0388 0.164 3.440 2.843 122.099 0.389 12.645 10.561 0.22 118416. 0.5772 7.67 0.1492 0.3442 0.0900 0.0390 0.165 3.461 2.771 122.850 0.391 12.327 10.232 0.22 118541. 0.5522 8.95 0.1741 0.3889 0.0875 0.0392 0.165 3.474 2.694 123.318 0.393 11.985 9.910 0.22 118674. 0.5274 10.23 0.1990 0.4304 0.0849 0.0392 0.166 3.478 2.612 123.460 0.393 11.618 9.596 0.22 118816. 0.5028 11.51 0.2238 0.4687 0.0820 0.0392 0.165 3.472 2.524 123.234 0.392 11.226 9.289 0.22 118968. 0.4784 12.79 0.2487 0.5040 0.0789 0.0390 0.164 3.454 2.430 122.599 0.390 10.808 8.990 0.22 119129. 0.4543 14.07 0.2736 0.5363 0.0757 0.0386 0.163 3.424 2.330 121.522 0.387 10.364 8.697 0.22 119299. 0.4304 15.35 0.2984 0.5658 0.0723 0.0381 0.161 3.380 2.225 119.984 0.382 9.896 8.410 0.22 119479. 0.4067 16.62 0.3233 0.5925 0.0687 0.0375 0.158 3.324 2.114 117.975 0.376 9.405 8.129 0.22 119668. 0.3832 17.90 0.3482 0.6163 0.0650 0.0367 0.155 3.254 1.999 115.489 0.368 8.894 7.853 0.22 119867. 0.3600 19.18 0.3730 0.6374 0.0611 0.0357 0.151 3.170 1.880 112.522 0.358 8.364 7.579 0.22 120076. 0.3369 20.46 0.3979 0.6555 0.0571 0.0347 0.146 3.073 1.757 109.069 0.347 7.816 7.308 0.22 120295. 0.3140 21.74 0.4228 0.6706 0.0530 0.0334 0.141 2.962 1.631 105.125 0.335 7.254 7.036 0.22 120523. 0.2913 23.02 0.4477 0.6824 0.0488 0.0320 0.135 2.837 1.501 100.685 0.320 6.677 6.762 0.22 120762. 0.2686 24.30 0.4725 0.6905 0.0445 0.0304 0.128 2.698 1.368 95.745 0.305 6.087 6.482 0.22 121011. 0.2458 25.58 0.4974 0.6945 0.0401 0.0287 0.121 2.544 1.233 90.299 0.287 5.485 6.194 0.22 121270. 0.2230 26.86 0.5223 0.6936 0.0356 0.0268 0.113 2.376 1.095 84.345 0.268 4.873 5.891 0.22 121539. 0.1999 28.13 0.5471 0.6865 0.0310 0.0247 0.104 2.194 0.956 77.883 0.248 4.251 5.566 0.22 121818. 0.1764 29.41 0.5720 0.6716 0.0265 0.0225 0.095 1.998 0.814 70.916 0.226 3.622 5.208 0.22 122108. 0.1524 30.69 0.5969 0.6459 0.0218 0.0202 0.085 1.788 0.672 63.450 0.202 2.987 4.800 0.22 122408. 0.1275 31.97 0.6217 0.6045 0.0171 0.0176 0.074 1.564 0.528 55.498 0.177 2.347 4.313 0.22 122718. 0.1016 33.25 0.6466 0.5385 0.0125 0.0150 0.063 1.326 0.383 47.077 0.150 1.706 3.694 0.22 123038. 0.0742 34.53 0.6715 0.4298 0.0078 0.0121 0.051 1.077 0.239 38.215 0.122 1.064 2.840 0.22 123368. 0.0450 35.81 0.6964 0.2353 0.0031 0.0092 0.039 0.815 0.096 28.938 0.092 0.425 1.499 0.22 123705. 0.0150 37.09 0.7212 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 0.1022 0.0359 0.359 5.663 5.595 267.987 0.640 24.886 9.469 0.29 157212. 0.7261 1.70 0.0247 0.0684 0.1007 0.0364 0.365 5.745 5.509 271.888 0.649 24.503 9.190 0.29 157326. 0.6992 3.39 0.0495 0.1326 0.0990 0.0369 0.370 5.822 5.415 275.544 0.658 24.088 8.914 0.29 157448. 0.6725 5.09 0.0742 0.1929 0.0971 0.0374 0.374 5.893 5.314 278.878 0.666 23.639 8.643 0.29 157581. 0.6460 6.79 0.0990 0.2493 0.0951 0.0378 0.378 5.955 5.205 281.813 0.673 23.154 8.378 0.29 157725. 0.6197 8.48 0.1237 0.3019 0.0930 0.0381 0.381 6.007 5.088 284.267 0.679 22.631 8.118 0.29 157879. 0.5936 10.18 0.1485 0.3510 0.0907 0.0384 0.384 6.046 4.961 286.147 0.683 22.068 7.864 0.29 158044. 0.5679 11.88 0.1732 0.3966 0.0882 0.0385 0.385 6.072 4.826 287.358 0.686 21.464 7.617 0.29 158221. 0.5424 13.57 0.1980 0.4389 0.0855 0.0386 0.386 6.081 4.680 287.801 0.687 20.816 7.375 0.29 158410. 0.5172 15.27 0.2227 0.4780 0.0827 0.0385 0.385 6.072 4.524 287.374 0.686 20.123 7.140 0.29 158611. 0.4923 16.97 0.2475 0.5141 0.0796 0.0383 0.384 6.043 4.358 285.980 0.683 19.383 6.912 0.29 158824. 0.4677 18.66 0.2722 0.5473 0.0764 0.0380 0.380 5.991 4.181 283.540 0.677 18.598 6.689 0.29 159049. 0.4434 20.36 0.2970 0.5776 0.0730 0.0375 0.375 5.917 3.995 280.003 0.668 17.769 6.471 0.29 159287. 0.4193 22.06 0.3217 0.6052 0.0694 0.0369 0.369 5.818 3.799 275.344 0.657 16.899 6.259 0.29 159538. 0.3955 23.75 0.3465 0.6301 0.0657 0.0361 0.361 5.696 3.596 269.548 0.643 15.993 6.050 0.29 159802. 0.3719 25.45 0.3712 0.6522 0.0618 0.0352 0.352 5.549 3.384 262.605 0.627 15.054 5.845 0.29 160078. 0.3486 27.15 0.3960 0.6716 0.0579 0.0341 0.341 5.378 3.166 254.502 0.608 14.084 5.643 0.29 160368. 0.3255 28.84 0.4207 0.6881 0.0538 0.0329 0.329 5.182 2.942 245.228 0.585 13.086 5.441 0.29 160670. 0.3026 30.54 0.4455 0.7015 0.0496 0.0315 0.315 4.961 2.712 234.768 0.560 12.062 5.239 0.29 160986. 0.2797 32.24 0.4702 0.7115 0.0453 0.0299 0.299 4.714 2.477 223.111 0.533 11.016 5.035 0.29 161315. 0.2568 33.93 0.4949 0.7178 0.0409 0.0282 0.282 4.443 2.237 210.247 0.502 9.948 4.825 0.29 161657. 0.2339 35.63 0.5197 0.7195 0.0364 0.0263 0.263 4.145 1.992 196.168 0.468 8.862 4.606 0.29 162013. 0.2108 37.33 0.5444 0.7158 0.0319 0.0242 0.243 3.822 1.744 180.873 0.432 7.759 4.374 0.29 162383. 0.1873 39.02 0.5692 0.7050 0.0273 0.0220 0.220 3.473 1.493 164.367 0.392 6.642 4.121 0.29 162765. 0.1632 40.72 0.5939 0.6844 0.0227 0.0197 0.197 3.099 1.240 146.665 0.350 5.514 3.834 0.29 163162. 0.1384 42.42 0.6187 0.6496 0.0180 0.0171 0.171 2.700 0.984 127.794 0.305 4.378 3.493 0.29 163572. 0.1124 44.11 0.6434 0.5923 0.0133 0.0144 0.145 2.278 0.728 107.796 0.257 3.238 3.063 0.29 163995. 0.0847 45.81 0.6682 0.4952 0.0086 0.0116 0.116 1.833 0.472 86.731 0.207 2.097 2.466 0.29 164431. 0.0549 47.51 0.6929 0.3157 0.0039 0.0087 0.087 1.366 0.216 64.667 0.154 0.961 1.516 0.29 164878. 0.0228 49.20 0.7177 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 0.1029 0.0356 0.695 8.765 8.800 518.479 0.990 39.144 7.699 0.36 196505. 0.7404 2.13 0.0248 0.0697 0.1013 0.0361 0.706 8.897 8.666 526.302 1.005 38.545 7.468 0.36 196647. 0.7127 4.26 0.0497 0.1351 0.0996 0.0366 0.716 9.021 8.520 533.638 1.019 37.896 7.241 0.36 196802. 0.6852 6.38 0.0745 0.1964 0.0978 0.0371 0.725 9.134 8.361 540.335 1.032 37.192 7.019 0.36 196969. 0.6579 8.51 0.0993 0.2537 0.0958 0.0375 0.733 9.234 8.190 546.235 1.043 36.431 6.801 0.36 197149. 0.6310 10.64 0.1241 0.3073 0.0936 0.0378 0.739 9.317 8.006 551.172 1.053 35.610 6.588 0.36 197344. 0.6043 12.77 0.1490 0.3571 0.0913 0.0381 0.744 9.381 7.807 554.966 1.060 34.726 6.381 0.36 197552. 0.5780 14.89 0.1738 0.4034 0.0888 0.0383 0.748 9.423 7.593 557.426 1.065 33.776 6.179 0.36 197774. 0.5520 17.02 0.1986 0.4464 0.0861 0.0383 0.749 9.439 7.364 558.350 1.066 32.756 5.982 0.36 198012. 0.5263 19.15 0.2234 0.4861 0.0832 0.0383 0.748 9.425 7.119 557.538 1.065 31.663 5.791 0.36 198265. 0.5009 21.28 0.2483 0.5228 0.0802 0.0381 0.744 9.379 6.856 554.796 1.060 30.497 5.605 0.36 198533. 0.4758 23.40 0.2731 0.5566 0.0769 0.0377 0.738 9.297 6.578 549.963 1.050 29.258 5.425 0.36 198817. 0.4510 25.53 0.2979 0.5876 0.0735 0.0373 0.728 9.178 6.284 542.940 1.037 27.949 5.249 0.36 199116. 0.4266 27.66 0.3227 0.6158 0.0699 0.0366 0.716 9.022 5.975 533.676 1.019 26.577 5.078 0.36 199432. 0.4024 29.79 0.3476 0.6413 0.0661 0.0358 0.700 8.827 5.653 522.141 0.997 25.146 4.911 0.36 199763. 0.3785 31.91 0.3724 0.6641 0.0622 0.0349 0.682 8.593 5.320 508.312 0.971 23.662 4.747 0.36 200111. 0.3549 34.04 0.3972 0.6843 0.0582 0.0338 0.660 8.320 4.975 492.167 0.940 22.129 4.585 0.36 200475. 0.3315 36.17 0.4220 0.7016 0.0540 0.0325 0.635 8.007 4.621 473.680 0.905 20.553 4.425 0.36 200856. 0.3083 38.30 0.4469 0.7159 0.0498 0.0311 0.607 7.655 4.257 452.823 0.865 18.936 4.264 0.36 201253. 0.2852 40.43 0.4717 0.7271 0.0454 0.0295 0.576 7.262 3.885 429.574 0.820 17.282 4.102 0.36 201667. 0.2622 42.55 0.4965 0.7345 0.0410 0.0277 0.542 6.828 3.506 403.911 0.771 15.596 3.937 0.36 202098. 0.2390 44.68 0.5214 0.7377 0.0365 0.0258 0.504 6.353 3.120 375.821 0.718 13.879 3.766 0.36 202546. 0.2157 46.81 0.5462 0.7355 0.0319 0.0237 0.463 5.837 2.729 345.301 0.659 12.137 3.584 0.36 203010. 0.1919 48.94 0.5710 0.7265 0.0273 0.0214 0.419 5.280 2.332 312.361 0.597 10.373 3.386 0.36 203492. 0.1676 51.06 0.5958 0.7079 0.0226 0.0190 0.372 4.683 1.931 277.034 0.529 8.591 3.162 0.37 203990. 0.1425 53.19 0.6207 0.6751 0.0179 0.0164 0.321 4.046 1.528 239.374 0.457 6.796 2.895 0.37 204506. 0.1160 55.32 0.6455 0.6193 0.0131 0.0137 0.267 3.372 1.123 199.471 0.381 4.996 2.554 0.37 205038. 0.0877 57.45 0.6703 0.5212 0.0084 0.0108 0.211 2.662 0.718 157.446 0.301 3.195 2.070 0.37 205586. 0.0569 59.57 0.6951 0.3293 0.0037 0.0078 0.152 1.918 0.315 113.432 0.217 1.402 1.261 0.37 206148. 0.0229 61.70 0.7200 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 0.1038 0.0355 1.199 12.597 12.775 894.218 1.423 56.825 6.480 0.43 235791. 0.7508 2.54 0.0247 0.0699 0.1022 0.0361 1.218 12.791 12.584 907.972 1.445 55.972 6.286 0.43 235960. 0.7229 5.07 0.0493 0.1356 0.1005 0.0366 1.235 12.972 12.375 920.879 1.466 55.046 6.095 0.43 236145. 0.6951 7.61 0.0740 0.1971 0.0987 0.0370 1.251 13.139 12.150 932.676 1.484 54.042 5.908 0.43 236345. 0.6676 10.15 0.0987 0.2547 0.0967 0.0375 1.265 13.285 11.905 943.097 1.501 52.955 5.726 0.43 236560. 0.6405 12.69 0.1233 0.3085 0.0945 0.0378 1.276 13.409 11.642 951.850 1.515 51.782 5.547 0.43 236792. 0.6136 15.22 0.1480 0.3586 0.0922 0.0381 1.286 13.504 11.357 958.632 1.526 50.518 5.374 0.43 237040. 0.5871 17.76 0.1727 0.4052 0.0898 0.0382 1.292 13.567 11.052 963.113 1.533 49.158 5.205 0.43 237306. 0.5609 20.30 0.1974 0.4485 0.0871 0.0383 1.294 13.593 10.723 964.950 1.536 47.698 5.040 0.43 237589. 0.5351 22.83 0.2220 0.4886 0.0842 0.0383 1.292 13.577 10.372 963.794 1.534 46.134 4.881 0.43 237890. 0.5096 25.37 0.2467 0.5257 0.0812 0.0381 1.286 13.514 9.996 959.310 1.527 44.463 4.726 0.43 238209. 0.4844 27.91 0.2714 0.5599 0.0779 0.0378 1.276 13.400 9.597 951.217 1.514 42.686 4.576 0.43 238547. 0.4596 30.44 0.2960 0.5913 0.0745 0.0373 1.260 13.232 9.175 939.332 1.495 40.809 4.430 0.43 238904. 0.4350 32.98 0.3207 0.6200 0.0709 0.0367 1.239 13.010 8.732 923.562 1.470 38.838 4.288 0.43 239280. 0.4108 35.52 0.3454 0.6462 0.0672 0.0359 1.212 12.733 8.269 903.854 1.439 36.782 4.150 0.43 239674. 0.3868 38.06 0.3700 0.6697 0.0633 0.0350 1.180 12.399 7.790 880.170 1.401 34.649 4.014 0.43 240088. 0.3632 40.59 0.3947 0.6907 0.0592 0.0339 1.143 12.009 7.294 852.471 1.357 32.445 3.881 0.43 240521. 0.3398 43.13 0.4194 0.7089 0.0551 0.0326 1.101 11.561 6.784 820.715 1.306 30.176 3.749 0.43 240973. 0.3166 45.67 0.4441 0.7244 0.0508 0.0312 1.053 11.056 6.261 784.857 1.249 27.849 3.618 0.44 241446. 0.2935 48.20 0.4687 0.7368 0.0465 0.0296 0.999 10.493 5.726 744.854 1.185 25.468 3.487 0.44 241937. 0.2705 50.74 0.4934 0.7459 0.0421 0.0278 0.940 9.870 5.180 700.671 1.115 23.039 3.353 0.44 242449. 0.2474 53.28 0.5181 0.7510 0.0376 0.0259 0.875 9.189 4.624 652.283 1.038 20.566 3.215 0.44 242981. 0.2241 55.82 0.5427 0.7512 0.0330 0.0238 0.804 8.448 4.059 599.679 0.954 18.055 3.070 0.44 243532. 0.2005 58.35 0.5674 0.7453 0.0283 0.0216 0.728 7.648 3.487 542.877 0.864 15.511 2.914 0.44 244104. 0.1764 60.89 0.5921 0.7309 0.0236 0.0191 0.646 6.789 2.909 481.923 0.767 12.940 2.738 0.44 244696. 0.1514 63.43 0.6167 0.7039 0.0189 0.0166 0.559 5.873 2.327 416.907 0.664 10.350 2.532 0.44 245307. 0.1252 65.96 0.6414 0.6567 0.0141 0.0138 0.467 4.902 1.742 347.971 0.554 7.749 2.271 0.44 245939. 0.0972 68.50 0.6661 0.5725 0.0094 0.0109 0.369 3.878 1.157 275.316 0.438 5.147 1.906 0.44 246590. 0.0665 71.04 0.6908 0.4071 0.0047 0.0079 0.267 2.806 0.574 199.183 0.317 2.553 1.307 0.44 247258. 0.0321 73.57 0.7154 -0.0203 -0.0001 0.0047 0.158 1.665 -0.016 118.178 0.188 -0.073 -0.063 0.44 247860. 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 0.1048 0.0357 1.912 17.215 17.558 1425.683 1.945 78.098 5.586 0.50 275066. 0.7588 2.97 0.0247 0.0705 0.1032 0.0362 1.942 17.486 17.298 1448.126 1.976 76.942 5.418 0.50 275265. 0.7305 5.93 0.0494 0.1366 0.1015 0.0367 1.970 17.740 17.015 1469.190 2.004 75.683 5.253 0.50 275482. 0.7024 8.90 0.0742 0.1986 0.0997 0.0372 1.996 17.972 16.708 1488.436 2.031 74.316 5.091 0.50 275716. 0.6746 11.86 0.0989 0.2566 0.0977 0.0377 2.019 18.177 16.375 1505.427 2.054 72.834 4.933 0.50 275969. 0.6472 14.83 0.1236 0.3108 0.0956 0.0380 2.038 18.350 16.014 1519.698 2.073 71.232 4.780 0.50 276241. 0.6201 17.80 0.1483 0.3612 0.0932 0.0383 2.053 18.483 15.626 1530.750 2.088 69.502 4.630 0.50 276533. 0.5933 20.76 0.1731 0.4082 0.0907 0.0385 2.063 18.571 15.207 1538.050 2.098 67.640 4.484 0.50 276845. 0.5669 23.73 0.1978 0.4518 0.0880 0.0385 2.067 18.608 14.757 1541.044 2.102 65.637 4.343 0.50 277177. 0.5409 26.70 0.2225 0.4923 0.0852 0.0385 2.064 18.585 14.274 1539.163 2.100 63.489 4.206 0.50 277531. 0.5152 29.66 0.2472 0.5297 0.0821 0.0383 2.054 18.497 13.758 1531.866 2.090 61.193 4.073 0.50 277906. 0.4898 32.63 0.2719 0.5642 0.0788 0.0380 2.037 18.338 13.208 1518.694 2.072 58.750 3.945 0.50 278302. 0.4648 35.59 0.2967 0.5961 0.0753 0.0375 2.011 18.104 12.627 1499.351 2.045 56.165 3.820 0.50 278721. 0.4400 38.56 0.3214 0.6252 0.0717 0.0369 1.976 17.794 12.017 1473.684 2.010 53.450 3.698 0.51 279162. 0.4156 41.53 0.3461 0.6518 0.0679 0.0361 1.933 17.407 11.380 1441.615 1.967 50.617 3.580 0.51 279625. 0.3915 44.49 0.3708 0.6758 0.0640 0.0351 1.882 16.942 10.719 1403.085 1.914 47.676 3.465 0.51 280110. 0.3677 47.46 0.3956 0.6973 0.0599 0.0340 1.821 16.398 10.035 1358.033 1.853 44.637 3.352 0.51 280618. 0.3442 50.43 0.4203 0.7162 0.0557 0.0327 1.752 15.774 9.332 1306.395 1.782 41.508 3.240 0.51 281149. 0.3208 53.39 0.4450 0.7324 0.0514 0.0312 1.674 15.070 8.610 1248.101 1.703 38.297 3.129 0.51 281703. 0.2976 56.36 0.4697 0.7456 0.0470 0.0296 1.587 14.285 7.871 1183.083 1.614 35.011 3.018 0.51 282280. 0.2745 59.32 0.4944 0.7555 0.0425 0.0278 1.490 13.418 7.117 1111.284 1.516 31.658 2.905 0.51 282879. 0.2512 62.29 0.5192 0.7616 0.0379 0.0258 1.385 12.469 6.350 1032.663 1.409 28.245 2.789 0.51 283503. 0.2278 65.26 0.5439 0.7631 0.0332 0.0237 1.270 11.437 5.571 947.209 1.292 24.778 2.667 0.51 284149. 0.2041 68.22 0.5686 0.7586 0.0285 0.0214 1.147 10.323 4.781 854.948 1.166 21.265 2.536 0.51 284819. 0.1798 71.19 0.5933 0.7457 0.0238 0.0189 1.014 9.128 3.983 755.961 1.031 17.715 2.390 0.51 285513. 0.1546 74.15 0.6181 0.7206 0.0190 0.0163 0.872 7.853 3.178 650.394 0.887 14.138 2.217 0.51 286229. 0.1281 77.12 0.6428 0.6752 0.0141 0.0135 0.722 6.502 2.371 538.482 0.735 10.546 1.997 0.51 286969. 0.0997 80.09 0.6675 0.5918 0.0093 0.0105 0.564 5.078 1.563 420.560 0.574 6.951 1.686 0.51 287732. 0.0683 83.05 0.6922 0.4212 0.0045 0.0074 0.398 3.586 0.758 297.015 0.405 3.370 1.157 0.51 288514. 0.0326 86.02 0.7169 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 0.1060 0.0360 2.880 22.692 23.197 2147.798 2.564 103.181 4.899 0.57 314330. 0.7649 3.39 0.0247 0.0705 0.1044 0.0366 2.926 23.056 22.861 2182.262 2.605 101.687 4.752 0.57 314558. 0.7365 6.77 0.0494 0.1368 0.1028 0.0371 2.970 23.398 22.495 2214.609 2.643 100.056 4.607 0.57 314806. 0.7084 10.16 0.0741 0.1989 0.1009 0.0376 3.009 23.710 22.095 2244.163 2.679 98.280 4.466 0.57 315074. 0.6805 13.54 0.0988 0.2570 0.0990 0.0380 3.044 23.986 21.662 2270.255 2.710 96.350 4.328 0.57 315364. 0.6530 16.93 0.1235 0.3112 0.0968 0.0384 3.074 24.218 21.192 2292.177 2.736 94.260 4.193 0.57 315676. 0.6258 20.32 0.1482 0.3618 0.0945 0.0387 3.097 24.397 20.684 2309.177 2.756 92.001 4.063 0.58 316010. 0.5990 23.70 0.1729 0.4090 0.0920 0.0389 3.112 24.516 20.136 2320.453 2.770 89.563 3.936 0.58 316367. 0.5725 27.09 0.1976 0.4528 0.0893 0.0390 3.118 24.566 19.546 2325.163 2.775 86.939 3.813 0.58 316748. 0.5465 30.47 0.2222 0.4935 0.0864 0.0389 3.114 24.537 18.912 2322.453 2.772 84.122 3.694 0.58 317153. 0.5207 33.86 0.2469 0.5311 0.0833 0.0387 3.100 24.422 18.234 2311.502 2.759 81.106 3.578 0.58 317583. 0.4953 37.25 0.2716 0.5660 0.0800 0.0384 3.073 24.211 17.512 2291.602 2.735 77.894 3.466 0.58 318037. 0.4702 40.63 0.2963 0.5981 0.0765 0.0379 3.034 23.902 16.747 2262.301 2.700 74.492 3.358 0.58 318516. 0.4454 44.02 0.3210 0.6277 0.0728 0.0373 2.982 23.491 15.943 2223.363 2.654 70.916 3.252 0.58 319020. 0.4210 47.41 0.3457 0.6547 0.0690 0.0364 2.916 22.976 15.103 2174.672 2.596 67.180 3.150 0.58 319550. 0.3969 50.79 0.3704 0.6792 0.0650 0.0355 2.838 22.358 14.231 2116.153 2.526 63.300 3.050 0.58 320105. 0.3730 54.18 0.3951 0.7012 0.0609 0.0343 2.746 21.635 13.329 2047.720 2.444 59.289 2.952 0.58 320686. 0.3494 57.56 0.4198 0.7208 0.0566 0.0330 2.641 20.806 12.400 1969.287 2.351 55.157 2.856 0.58 321293. 0.3260 60.95 0.4445 0.7376 0.0523 0.0315 2.522 19.871 11.447 1880.750 2.245 50.916 2.761 0.58 321926. 0.3028 64.34 0.4692 0.7517 0.0478 0.0299 2.390 18.828 10.471 1782.016 2.127 46.575 2.665 0.58 322584. 0.2796 67.72 0.4939 0.7626 0.0433 0.0280 2.244 17.676 9.475 1672.998 1.997 42.143 2.569 0.58 323270. 0.2563 71.11 0.5186 0.7699 0.0386 0.0260 2.083 16.415 8.460 1553.632 1.855 37.630 2.470 0.58 323982. 0.2329 74.49 0.5433 0.7728 0.0339 0.0239 1.909 15.044 7.429 1423.904 1.700 33.044 2.366 0.58 324720. 0.2091 77.88 0.5680 0.7700 0.0292 0.0215 1.722 13.564 6.384 1283.850 1.532 28.396 2.255 0.58 325485. 0.1847 81.27 0.5927 0.7595 0.0243 0.0190 1.520 11.977 5.328 1133.585 1.353 23.698 2.132 0.58 326276. 0.1595 84.65 0.6174 0.7372 0.0195 0.0163 1.305 10.284 4.263 973.331 1.162 18.962 1.987 0.59 327094. 0.1330 88.04 0.6420 0.6958 0.0146 0.0135 1.077 8.489 3.193 803.437 0.959 14.203 1.803 0.59 327938. 0.1044 91.42 0.6667 0.6180 0.0097 0.0105 0.837 6.597 2.123 624.409 0.745 9.441 1.542 0.59 328808. 0.0728 94.81 0.6914 0.4554 0.0048 0.0073 0.586 4.615 1.055 436.839 0.521 4.693 1.096 0.59 329701. 0.0365 98.20 0.7161 -0.0274 -0.0002 0.0040 0.316 2.493 -0.033 235.947 0.282 -0.147 -0.064 0.59 330463. 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 0.1074 0.0365 4.160 29.135 29.756 3102.324 3.292 132.357 4.350 0.65 353577. 0.7693 3.81 0.0247 0.0705 0.1059 0.0371 4.228 29.612 29.337 3153.130 3.346 130.491 4.220 0.65 353835. 0.7410 7.63 0.0494 0.1368 0.1042 0.0377 4.292 30.060 28.877 3200.815 3.396 128.445 4.092 0.65 354116. 0.7128 11.44 0.0741 0.1989 0.1024 0.0382 4.351 30.469 28.375 3244.380 3.442 126.210 3.967 0.65 354419. 0.6850 15.25 0.0989 0.2571 0.1004 0.0386 4.402 30.830 27.827 3282.826 3.483 123.775 3.845 0.65 354747. 0.6575 19.06 0.1236 0.3114 0.0983 0.0390 4.446 31.133 27.232 3315.094 3.517 121.129 3.726 0.65 355100. 0.6303 22.88 0.1483 0.3621 0.0960 0.0393 4.479 31.368 26.588 3340.101 3.544 118.262 3.610 0.65 355478. 0.6035 26.69 0.1730 0.4093 0.0935 0.0395 4.501 31.524 25.891 3356.672 3.562 115.162 3.498 0.65 355882. 0.5771 30.50 0.1977 0.4533 0.0907 0.0396 4.511 31.589 25.139 3363.591 3.569 111.819 3.390 0.65 356313. 0.5510 34.31 0.2224 0.4941 0.0878 0.0395 4.505 31.551 24.331 3359.615 3.565 108.224 3.285 0.65 356772. 0.5253 38.13 0.2472 0.5320 0.0847 0.0393 4.484 31.401 23.465 3343.545 3.548 104.370 3.183 0.65 357258. 0.4999 41.94 0.2719 0.5671 0.0814 0.0390 4.445 31.126 22.540 3314.354 3.517 100.258 3.085 0.65 357772. 0.4747 45.75 0.2966 0.5996 0.0778 0.0385 4.387 30.723 21.560 3271.366 3.471 95.898 2.989 0.65 358314. 0.4500 49.56 0.3213 0.6294 0.0741 0.0378 4.310 30.186 20.528 3214.246 3.410 91.310 2.897 0.65 358884. 0.4255 53.38 0.3460 0.6568 0.0702 0.0370 4.215 29.516 19.450 3142.842 3.335 86.513 2.807 0.65 359483. 0.4013 57.19 0.3707 0.6818 0.0662 0.0360 4.100 28.710 18.329 3057.056 3.244 81.527 2.719 0.65 360111. 0.3774 61.00 0.3955 0.7044 0.0620 0.0348 3.965 27.768 17.169 2956.794 3.137 76.369 2.634 0.65 360767. 0.3538 64.82 0.4202 0.7244 0.0577 0.0334 3.811 26.690 15.974 2841.936 3.015 71.054 2.549 0.65 361452. 0.3303 68.63 0.4449 0.7420 0.0532 0.0319 3.637 25.473 14.747 2712.355 2.878 65.595 2.466 0.65 362167. 0.3070 72.44 0.4696 0.7567 0.0487 0.0302 3.444 24.116 13.491 2567.910 2.725 60.006 2.383 0.65 362911. 0.2837 76.25 0.4943 0.7685 0.0441 0.0283 3.230 22.619 12.207 2408.493 2.555 54.298 2.299 0.65 363685. 0.2604 80.07 0.5190 0.7768 0.0393 0.0263 2.996 20.980 10.900 2234.001 2.370 48.483 2.213 0.65 364488. 0.2369 83.88 0.5437 0.7808 0.0345 0.0241 2.742 19.200 9.571 2044.427 2.169 42.572 2.123 0.66 365321. 0.2130 87.69 0.5685 0.7794 0.0297 0.0216 2.467 17.278 8.224 1839.819 1.952 36.580 2.027 0.66 366184. 0.1885 91.50 0.5932 0.7705 0.0248 0.0191 2.173 15.217 6.862 1620.352 1.719 30.520 1.921 0.66 367077. 0.1631 95.32 0.6179 0.7503 0.0198 0.0163 1.859 13.020 5.488 1386.345 1.471 24.410 1.795 0.66 367999. 0.1364 99.13 0.6426 0.7113 0.0148 0.0134 1.527 10.690 4.107 1138.311 1.208 18.270 1.637 0.66 368951. 0.1075 102.94 0.6673 0.6361 0.0098 0.0103 1.176 8.236 2.725 876.991 0.931 12.123 1.410 0.66 369932. 0.0754 106.76 0.6920 0.4740 0.0049 0.0071 0.809 5.665 1.347 603.264 0.640 5.992 1.013 0.66 370938. 0.0381 110.57 0.7168 -0.0566 -0.0003 0.0036 0.410 2.871 -0.079 305.728 0.324 -0.350 -0.117 0.66 371679. 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 0.1091 0.0375 5.861 36.943 37.313 4370.785 4.174 165.969 3.872 0.72 392805. 0.7668 4.27 0.0249 0.0704 0.1076 0.0381 5.953 37.520 36.803 4439.061 4.239 163.701 3.760 0.72 393095. 0.7396 8.54 0.0498 0.1366 0.1060 0.0386 6.039 38.061 36.241 4503.101 4.300 161.199 3.650 0.72 393410. 0.7124 12.80 0.0747 0.1988 0.1041 0.0391 6.117 38.555 35.623 4561.523 4.356 158.450 3.542 0.72 393752. 0.6853 17.07 0.0996 0.2572 0.1022 0.0396 6.186 38.990 34.946 4612.926 4.405 155.440 3.436 0.72 394121. 0.6585 21.34 0.1245 0.3118 0.1000 0.0399 6.244 39.352 34.207 4655.840 4.446 152.154 3.332 0.72 394519. 0.6318 25.61 0.1494 0.3628 0.0977 0.0402 6.288 39.630 33.403 4688.702 4.477 148.578 3.231 0.72 394946. 0.6054 29.88 0.1743 0.4103 0.0951 0.0404 6.316 39.809 32.531 4709.818 4.498 144.699 3.133 0.72 395403. 0.5793 34.14 0.1992 0.4546 0.0924 0.0405 6.326 39.873 31.588 4717.426 4.505 140.502 3.037 0.72 395890. 0.5534 38.41 0.2241 0.4958 0.0894 0.0404 6.316 39.807 30.570 4709.691 4.497 135.977 2.944 0.72 396408. 0.5277 42.68 0.2490 0.5340 0.0862 0.0402 6.282 39.597 29.477 4684.824 4.474 131.116 2.854 0.72 396958. 0.5023 46.95 0.2739 0.5694 0.0828 0.0398 6.224 39.229 28.309 4641.272 4.432 125.918 2.766 0.72 397538. 0.4772 51.21 0.2988 0.6021 0.0791 0.0393 6.139 38.694 27.068 4577.989 4.372 120.399 2.682 0.72 398151. 0.4523 55.48 0.3237 0.6323 0.0753 0.0386 6.027 37.988 25.761 4494.433 4.292 114.584 2.600 0.72 398795. 0.4278 59.75 0.3486 0.6601 0.0713 0.0377 5.888 37.109 24.393 4390.375 4.192 108.498 2.520 0.72 399472. 0.4035 64.02 0.3735 0.6854 0.0672 0.0366 5.720 36.055 22.969 4265.693 4.073 102.168 2.442 0.72 400180. 0.3795 68.29 0.3984 0.7084 0.0628 0.0353 5.525 34.826 21.496 4120.278 3.935 95.615 2.366 0.72 400922. 0.3557 72.55 0.4233 0.7289 0.0584 0.0339 5.302 33.420 19.978 3953.997 3.776 88.860 2.292 0.72 401696. 0.3321 76.82 0.4482 0.7469 0.0538 0.0323 5.051 31.837 18.417 3766.678 3.597 81.921 2.218 0.73 402502. 0.3085 81.09 0.4731 0.7622 0.0492 0.0305 4.772 30.074 16.819 3558.150 3.398 74.813 2.144 0.73 403342. 0.2851 85.36 0.4980 0.7745 0.0444 0.0286 4.463 28.131 15.187 3328.248 3.178 67.551 2.070 0.73 404215. 0.2615 89.63 0.5229 0.7833 0.0395 0.0264 4.126 26.006 13.523 3076.862 2.938 60.152 1.994 0.73 405121. 0.2377 93.89 0.5478 0.7878 0.0346 0.0241 3.760 23.700 11.832 2803.976 2.678 52.629 1.914 0.73 406061. 0.2134 98.16 0.5727 0.7868 0.0296 0.0215 3.366 21.213 10.117 2509.739 2.397 45.002 1.828 0.73 407034. 0.1885 102.43 0.5976 0.7780 0.0245 0.0188 2.943 18.549 8.383 2194.514 2.096 37.287 1.733 0.73 408040. 0.1626 106.70 0.6225 0.7572 0.0194 0.0159 2.493 15.712 6.634 1858.940 1.775 29.509 1.619 0.73 409080. 0.1352 110.96 0.6474 0.7155 0.0143 0.0129 2.017 12.712 4.877 1504.025 1.436 21.692 1.471 0.73 410152. 0.1053 115.23 0.6723 0.6316 0.0091 0.0097 1.517 9.561 3.118 1131.195 1.080 13.868 1.250 0.73 411257. 0.0716 119.50 0.6972 0.4367 0.0040 0.0064 0.995 6.272 1.364 742.076 0.709 6.067 0.834 0.74 412387. 0.0316 123.77 0.7221 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 0.1110 0.0402 8.365 47.929 45.948 6237.632 5.415 204.375 3.341 0.79 432008. 0.7342 4.69 0.0249 0.0670 0.1096 0.0407 8.464 48.500 45.355 6311.947 5.480 201.738 3.259 0.79 432326. 0.7115 9.38 0.0498 0.1307 0.1080 0.0411 8.555 49.019 44.696 6379.527 5.538 198.806 3.178 0.79 432674. 0.6887 14.08 0.0747 0.1911 0.1062 0.0415 8.635 49.475 43.967 6438.764 5.590 195.563 3.097 0.79 433051. 0.6657 18.77 0.0995 0.2483 0.1043 0.0418 8.701 49.853 43.163 6488.040 5.632 191.989 3.017 0.79 433459. 0.6427 23.46 0.1244 0.3022 0.1022 0.0421 8.751 50.142 42.280 6525.640 5.665 188.063 2.939 0.79 433899. 0.6195 28.15 0.1493 0.3531 0.0998 0.0422 8.783 50.328 41.315 6549.786 5.686 183.768 2.861 0.79 434371. 0.5962 32.84 0.1742 0.4009 0.0973 0.0423 8.795 50.395 40.263 6558.578 5.694 179.088 2.784 0.79 434877. 0.5728 37.53 0.1991 0.4457 0.0945 0.0422 8.784 50.329 39.120 6549.958 5.686 174.004 2.709 0.79 435416. 0.5493 42.23 0.2240 0.4877 0.0915 0.0420 8.746 50.112 37.883 6521.763 5.662 168.503 2.635 0.79 435989. 0.5257 46.92 0.2488 0.5269 0.0883 0.0417 8.679 49.729 36.550 6471.822 5.618 162.575 2.562 0.79 436597. 0.5020 51.61 0.2737 0.5633 0.0849 0.0412 8.580 49.163 35.121 6398.157 5.554 156.220 2.490 0.79 437239. 0.4783 56.30 0.2986 0.5971 0.0812 0.0406 8.448 48.404 33.601 6299.390 5.469 149.456 2.419 0.79 437916. 0.4546 60.99 0.3235 0.6284 0.0773 0.0398 8.280 47.446 31.995 6174.730 5.360 142.313 2.350 0.79 438628. 0.4310 65.68 0.3484 0.6572 0.0732 0.0388 8.078 46.286 30.311 6023.749 5.229 134.824 2.282 0.79 439376. 0.4073 70.38 0.3733 0.6836 0.0690 0.0377 7.840 44.921 28.557 5846.122 5.075 127.023 2.216 0.80 440159. 0.3838 75.07 0.3981 0.7075 0.0646 0.0364 7.565 43.349 26.739 5641.523 4.898 118.937 2.150 0.80 440977. 0.3604 79.76 0.4230 0.7289 0.0601 0.0349 7.254 41.566 24.864 5409.546 4.696 110.593 2.085 0.80 441831. 0.3370 84.45 0.4479 0.7479 0.0554 0.0332 6.906 39.570 22.935 5149.737 4.471 102.014 2.020 0.80 442721. 0.3136 89.14 0.4728 0.7641 0.0506 0.0313 6.520 37.359 20.958 4861.978 4.221 93.220 1.955 0.80 443647. 0.2902 93.83 0.4977 0.7772 0.0458 0.0293 6.096 34.931 18.937 4545.979 3.946 84.230 1.889 0.80 444609. 0.2665 98.53 0.5226 0.7869 0.0408 0.0271 5.634 32.284 16.875 4201.587 3.647 75.062 1.822 0.80 445607. 0.2426 103.22 0.5475 0.7922 0.0357 0.0247 5.135 29.422 14.779 3829.063 3.324 65.736 1.751 0.80 446642. 0.2182 107.91 0.5723 0.7916 0.0306 0.0221 4.599 26.349 12.651 3429.139 2.977 56.272 1.673 0.80 447713. 0.1929 112.60 0.5972 0.7827 0.0254 0.0194 4.027 23.075 10.497 3003.014 2.607 46.692 1.585 0.80 448821. 0.1665 117.29 0.6221 0.7606 0.0201 0.0165 3.423 19.613 8.324 2552.433 2.216 37.023 1.479 0.81 449965. 0.1383 121.98 0.6470 0.7158 0.0148 0.0134 2.789 15.980 6.137 2079.747 1.805 27.297 1.338 0.81 451145. 0.1075 126.68 0.6719 0.6259 0.0095 0.0102 2.130 12.202 3.946 1588.001 1.379 17.551 1.127 0.81 452360. 0.0726 131.37 0.6968 0.4250 0.0042 0.0070 1.449 8.303 1.758 1080.557 0.938 7.821 0.738 0.81 453603. 0.0317 136.06 0.7216 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 0.1130 0.0465 12.564 65.992 55.633 9369.118 7.456 247.458 2.693 0.86 471183. 0.6512 5.09 0.0247 0.0590 0.1116 0.0468 12.647 66.424 54.982 9430.548 7.505 244.559 2.644 0.86 471527. 0.6357 10.18 0.0495 0.1158 0.1101 0.0471 12.710 66.757 54.249 9477.806 7.542 241.300 2.596 0.86 471903. 0.6199 15.26 0.0742 0.1705 0.1085 0.0472 12.752 66.977 53.430 9509.025 7.567 237.656 2.549 0.86 472312. 0.6039 20.35 0.0990 0.2232 0.1066 0.0473 12.770 67.073 52.518 9522.633 7.578 233.600 2.501 0.86 472755. 0.5877 25.44 0.1237 0.2738 0.1046 0.0472 12.763 67.035 51.508 9517.167 7.574 229.108 2.455 0.86 473234. 0.5711 30.53 0.1484 0.3223 0.1023 0.0471 12.728 66.851 50.395 9491.043 7.553 224.156 2.408 0.86 473747. 0.5542 35.62 0.1732 0.3688 0.0998 0.0469 12.663 66.511 49.173 9442.801 7.514 218.721 2.362 0.86 474298. 0.5369 40.71 0.1979 0.4132 0.0971 0.0465 12.566 66.004 47.838 9370.834 7.457 212.784 2.315 0.86 474885. 0.5192 45.79 0.2226 0.4555 0.0942 0.0460 12.435 65.315 46.386 9273.109 7.379 206.324 2.269 0.86 475510. 0.5009 50.88 0.2474 0.4956 0.0910 0.0454 12.267 64.431 44.813 9147.501 7.279 199.328 2.222 0.86 476172. 0.4822 55.97 0.2721 0.5337 0.0875 0.0446 12.059 63.337 43.119 8992.246 7.156 191.793 2.175 0.86 476871. 0.4630 61.06 0.2969 0.5695 0.0839 0.0437 11.809 62.028 41.308 8806.320 7.008 183.740 2.128 0.87 477609. 0.4433 66.15 0.3216 0.6032 0.0800 0.0426 11.519 60.501 39.390 8589.540 6.835 175.205 2.080 0.87 478384. 0.4232 71.23 0.3463 0.6346 0.0759 0.0414 11.187 58.757 37.372 8342.009 6.638 166.231 2.032 0.87 479197. 0.4027 76.32 0.3711 0.6637 0.0716 0.0400 10.814 56.798 35.266 8063.795 6.417 156.861 1.984 0.87 480049. 0.3819 81.41 0.3958 0.6905 0.0672 0.0385 10.399 54.620 33.078 7754.667 6.171 147.130 1.935 0.87 480938. 0.3607 86.50 0.4205 0.7149 0.0626 0.0368 9.942 52.221 30.816 7414.060 5.900 137.069 1.885 0.87 481866. 0.3393 91.59 0.4453 0.7368 0.0578 0.0350 9.442 49.595 28.486 7041.223 5.603 126.706 1.835 0.87 482832. 0.3175 96.67 0.4700 0.7560 0.0530 0.0329 8.898 46.737 26.094 6635.470 5.280 116.068 1.784 0.87 483836. 0.2954 101.76 0.4948 0.7715 0.0480 0.0308 8.317 43.684 23.645 6202.011 4.935 105.174 1.729 0.87 484879. 0.2726 106.85 0.5195 0.7822 0.0429 0.0285 7.702 40.454 21.144 5743.441 4.570 94.050 1.670 0.87 485961. 0.2489 111.94 0.5442 0.7856 0.0378 0.0262 7.065 37.108 18.595 5268.427 4.192 82.710 1.601 0.87 487082. 0.2238 117.03 0.5690 0.7816 0.0325 0.0237 6.390 33.565 16.005 4765.312 3.792 71.189 1.523 0.88 488241. 0.1976 122.12 0.5937 0.7668 0.0272 0.0210 5.682 29.842 13.380 4236.823 3.372 59.515 1.432 0.88 489440. 0.1699 127.20 0.6185 0.7360 0.0218 0.0183 4.944 25.968 10.728 3686.727 2.934 47.719 1.320 0.88 490677. 0.1401 132.29 0.6432 0.6794 0.0164 0.0155 4.183 21.973 8.057 3119.633 2.483 35.838 1.171 0.88 491953. 0.1078 137.38 0.6679 0.5782 0.0109 0.0126 3.407 17.896 5.378 2540.787 2.022 23.921 0.960 0.88 493267. 0.0722 142.47 0.6927 0.3914 0.0055 0.0097 2.623 13.776 2.702 1955.837 1.556 12.019 0.627 0.88 494614. 0.0334 147.56 0.7174 -0.0012 0.0000 0.0067 1.812 9.519 -0.006 1351.426 1.075 -0.025 -0.002 0.88 495854. 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 0.1127 0.0541 18.567 90.017 65.127 13845.045 10.170 289.684 2.134 0.93 510451. 0.5582 5.55 0.0249 0.0511 0.1116 0.0544 18.685 90.592 64.481 13933.547 10.235 286.812 2.099 0.93 510816. 0.5464 11.10 0.0498 0.1005 0.1103 0.0547 18.780 91.054 63.750 14004.590 10.287 283.558 2.065 0.93 511216. 0.5344 16.65 0.0747 0.1482 0.1089 0.0549 18.847 91.375 62.923 14053.917 10.323 279.882 2.031 0.93 511652. 0.5222 22.20 0.0996 0.1944 0.1072 0.0550 18.878 91.526 61.992 14077.122 10.341 275.740 1.997 0.93 512126. 0.5098 27.75 0.1245 0.2390 0.1054 0.0549 18.868 91.476 60.945 14069.541 10.335 271.086 1.965 0.93 512640. 0.4972 33.30 0.1495 0.2822 0.1034 0.0548 18.809 91.195 59.774 14026.207 10.303 265.873 1.933 0.93 513193. 0.4845 38.85 0.1744 0.3240 0.1011 0.0544 18.697 90.648 58.465 13942.079 10.241 260.054 1.902 0.93 513788. 0.4715 44.40 0.1993 0.3644 0.0986 0.0539 18.523 89.805 57.011 13812.452 10.146 253.585 1.872 0.94 514426. 0.4582 49.95 0.2242 0.4036 0.0958 0.0532 18.283 88.642 55.401 13633.617 10.015 246.425 1.843 0.94 515106. 0.4447 55.50 0.2491 0.4416 0.0928 0.0523 17.974 87.143 53.631 13403.116 9.845 238.549 1.815 0.94 515829. 0.4309 61.05 0.2740 0.4784 0.0894 0.0512 17.594 85.302 51.697 13119.871 9.637 229.947 1.787 0.94 516595. 0.4166 66.60 0.2989 0.5139 0.0858 0.0499 17.144 83.121 49.604 12784.386 9.391 220.639 1.760 0.94 517404. 0.4018 72.15 0.3238 0.5481 0.0819 0.0484 16.627 80.615 47.363 12399.035 9.108 210.671 1.733 0.94 518256. 0.3865 77.70 0.3487 0.5808 0.0778 0.0467 16.049 77.809 44.988 11967.471 8.791 200.105 1.705 0.94 519151. 0.3707 83.25 0.3736 0.6120 0.0735 0.0449 15.412 74.723 42.490 11492.802 8.442 188.996 1.677 0.94 520089. 0.3544 88.81 0.3985 0.6416 0.0690 0.0429 14.721 71.371 39.882 10977.202 8.063 177.396 1.648 0.94 521068. 0.3374 94.36 0.4235 0.6692 0.0643 0.0407 13.976 67.760 37.173 10421.854 7.655 165.345 1.618 0.94 522090. 0.3198 99.91 0.4484 0.6948 0.0595 0.0384 13.179 63.898 34.372 9827.823 7.219 152.885 1.586 0.94 523155. 0.3015 105.46 0.4733 0.7180 0.0545 0.0359 12.332 59.791 31.487 9196.235 6.755 140.056 1.553 0.94 524261. 0.2825 111.01 0.4982 0.7384 0.0494 0.0333 11.436 55.445 28.529 8527.756 6.264 126.896 1.517 0.95 525410. 0.2627 116.56 0.5231 0.7529 0.0441 0.0307 10.527 51.038 25.500 7849.983 5.766 113.425 1.473 0.95 526601. 0.2412 122.11 0.5480 0.7527 0.0387 0.0282 9.689 46.976 22.397 7225.210 5.307 99.624 1.406 0.95 527834. 0.2157 127.66 0.5729 0.7350 0.0333 0.0259 8.907 43.182 19.231 6641.682 4.879 85.541 1.313 0.95 529110. 0.1867 133.21 0.5978 0.7019 0.0277 0.0236 8.109 39.314 16.023 6046.766 4.442 71.268 1.202 0.95 530428. 0.1560 138.76 0.6227 0.6477 0.0221 0.0213 7.304 35.410 12.784 5446.323 4.001 56.864 1.065 0.95 531788. 0.1234 144.31 0.6476 0.5643 0.0165 0.0189 6.500 31.515 9.533 4847.248 3.561 42.402 0.892 0.95 533190. 0.0893 149.86 0.6726 0.4403 0.0109 0.0166 5.708 27.672 6.289 4256.085 3.126 27.973 0.670 0.95 534632. 0.0545 155.41 0.6975 0.2584 0.0053 0.0144 4.931 23.905 3.075 3676.752 2.701 13.678 0.379 0.96 536112. 0.0216 160.96 0.7224 -0.0161 -0.0003 0.0120 4.123 19.988 -0.154 3074.188 2.258 -0.686 -0.023 0.96 537533. 0.0000