20x15C (20x15C.dat) v2022-0915 Simulation Date: 08/22/2023 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 0.0904 0.0391 0.010 0.635 0.461 7.513 0.072 2.050 27.817 0.08 33408. 0.5540 0.61 0.0321 0.0720 0.0899 0.0401 0.010 0.651 0.458 7.707 0.074 2.039 26.980 0.08 33434. 0.5359 1.22 0.0642 0.1394 0.0894 0.0412 0.011 0.669 0.456 7.909 0.076 2.027 26.130 0.08 33463. 0.5175 1.83 0.0964 0.2022 0.0887 0.0423 0.011 0.686 0.452 8.118 0.078 2.012 25.273 0.08 33496. 0.4987 2.43 0.1285 0.2605 0.0879 0.0434 0.011 0.704 0.448 8.330 0.080 1.995 24.417 0.08 33533. 0.4797 3.04 0.1606 0.3143 0.0870 0.0445 0.011 0.722 0.444 8.540 0.082 1.974 23.566 0.08 33574. 0.4606 3.65 0.1927 0.3637 0.0859 0.0455 0.012 0.739 0.438 8.744 0.084 1.949 22.728 0.08 33620. 0.4414 4.26 0.2249 0.4090 0.0846 0.0465 0.012 0.755 0.432 8.936 0.085 1.920 21.906 0.08 33670. 0.4222 4.87 0.2570 0.4503 0.0831 0.0474 0.012 0.770 0.424 9.109 0.087 1.885 21.105 0.08 33725. 0.4031 5.48 0.2891 0.4879 0.0814 0.0482 0.012 0.782 0.415 9.256 0.088 1.845 20.327 0.08 33785. 0.3841 6.08 0.3212 0.5221 0.0793 0.0488 0.013 0.792 0.404 9.370 0.089 1.799 19.574 0.08 33850. 0.3652 6.69 0.3533 0.5529 0.0769 0.0492 0.013 0.798 0.392 9.442 0.090 1.745 18.846 0.08 33920. 0.3463 7.30 0.3855 0.5807 0.0743 0.0493 0.013 0.800 0.379 9.466 0.090 1.684 18.143 0.08 33995. 0.3275 7.91 0.4176 0.6055 0.0713 0.0491 0.013 0.798 0.363 9.437 0.090 1.616 17.463 0.08 34076. 0.3088 8.52 0.4497 0.6275 0.0679 0.0487 0.013 0.790 0.346 9.350 0.089 1.541 16.804 0.08 34161. 0.2902 9.13 0.4818 0.6466 0.0643 0.0479 0.012 0.778 0.328 9.207 0.088 1.459 16.162 0.08 34252. 0.2716 9.73 0.5140 0.6628 0.0605 0.0469 0.012 0.761 0.308 9.009 0.086 1.372 15.532 0.08 34348. 0.2531 10.34 0.5461 0.6760 0.0565 0.0456 0.012 0.740 0.288 8.757 0.084 1.280 14.908 0.08 34449. 0.2347 10.95 0.5782 0.6858 0.0522 0.0440 0.011 0.715 0.266 8.455 0.081 1.184 14.286 0.08 34555. 0.2163 11.56 0.6103 0.6920 0.0478 0.0422 0.011 0.685 0.244 8.103 0.077 1.085 13.656 0.08 34665. 0.1979 12.17 0.6424 0.6941 0.0433 0.0401 0.010 0.651 0.221 7.703 0.074 0.983 13.012 0.08 34781. 0.1794 12.78 0.6746 0.6912 0.0387 0.0378 0.010 0.613 0.197 7.257 0.069 0.878 12.341 0.08 34902. 0.1609 13.38 0.7067 0.6823 0.0340 0.0352 0.009 0.572 0.173 6.765 0.065 0.771 11.628 0.08 35027. 0.1421 13.99 0.7388 0.6658 0.0292 0.0324 0.008 0.527 0.149 6.230 0.059 0.663 10.853 0.08 35157. 0.1229 14.60 0.7709 0.6390 0.0244 0.0294 0.008 0.478 0.124 5.651 0.054 0.553 9.983 0.08 35293. 0.1033 15.21 0.8031 0.5979 0.0195 0.0262 0.007 0.425 0.099 5.032 0.048 0.442 8.968 0.08 35433. 0.0830 15.82 0.8352 0.5356 0.0146 0.0228 0.006 0.370 0.074 4.373 0.042 0.331 7.723 0.08 35577. 0.0618 16.43 0.8673 0.4390 0.0097 0.0192 0.005 0.311 0.049 3.677 0.035 0.220 6.096 0.08 35727. 0.0398 17.03 0.8994 0.2813 0.0048 0.0154 0.004 0.249 0.024 2.949 0.028 0.109 3.767 0.08 35880. 0.0173 17.64 0.9316 -0.0036 0.0000 0.0114 0.003 0.185 0.000 2.190 0.021 -0.001 -0.047 0.08 36038. 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 0.0907 0.0354 0.073 2.300 1.850 54.433 0.260 8.228 15.414 0.16 66816. 0.6150 1.24 0.0327 0.0808 0.0903 0.0365 0.075 2.369 1.841 56.047 0.268 8.188 14.896 0.16 66868. 0.5929 2.47 0.0653 0.1559 0.0897 0.0376 0.077 2.440 1.830 57.743 0.276 8.139 14.374 0.16 66928. 0.5704 3.71 0.0980 0.2253 0.0891 0.0387 0.080 2.514 1.817 59.498 0.284 8.082 13.851 0.16 66995. 0.5477 4.95 0.1306 0.2892 0.0883 0.0399 0.082 2.590 1.801 61.285 0.293 8.012 13.331 0.16 67070. 0.5249 6.19 0.1633 0.3476 0.0874 0.0411 0.085 2.665 1.783 63.067 0.301 7.929 12.820 0.16 67155. 0.5022 7.42 0.1959 0.4009 0.0863 0.0422 0.087 2.739 1.760 64.803 0.309 7.829 12.320 0.16 67248. 0.4795 8.66 0.2286 0.4492 0.0850 0.0433 0.089 2.808 1.734 66.442 0.317 7.711 11.834 0.16 67351. 0.4571 9.90 0.2613 0.4930 0.0834 0.0442 0.091 2.871 1.702 67.928 0.324 7.570 11.364 0.16 67465. 0.4350 11.13 0.2939 0.5326 0.0816 0.0450 0.093 2.924 1.665 69.199 0.330 7.406 10.913 0.16 67588. 0.4131 12.37 0.3266 0.5683 0.0795 0.0457 0.094 2.966 1.622 70.189 0.335 7.214 10.480 0.16 67722. 0.3916 13.61 0.3592 0.6005 0.0771 0.0461 0.095 2.993 1.572 70.832 0.338 6.993 10.067 0.16 67866. 0.3703 14.84 0.3919 0.6294 0.0743 0.0463 0.095 3.003 1.515 71.068 0.339 6.741 9.672 0.16 68022. 0.3493 16.08 0.4245 0.6553 0.0712 0.0461 0.095 2.994 1.452 70.849 0.338 6.458 9.295 0.16 68187. 0.3286 17.32 0.4572 0.6783 0.0678 0.0457 0.094 2.965 1.382 70.155 0.335 6.146 8.934 0.16 68364. 0.3081 18.56 0.4899 0.6985 0.0640 0.0449 0.093 2.915 1.306 68.983 0.329 5.809 8.587 0.16 68551. 0.2879 19.79 0.5225 0.7160 0.0601 0.0438 0.090 2.846 1.225 67.345 0.322 5.450 8.251 0.16 68748. 0.2680 21.03 0.5552 0.7306 0.0559 0.0425 0.088 2.758 1.140 65.255 0.312 5.071 7.924 0.16 68956. 0.2482 22.27 0.5878 0.7421 0.0516 0.0408 0.084 2.651 1.051 62.728 0.300 4.677 7.602 0.16 69174. 0.2287 23.50 0.6205 0.7503 0.0471 0.0389 0.080 2.526 0.960 59.777 0.285 4.269 7.282 0.16 69403. 0.2093 24.74 0.6531 0.7547 0.0424 0.0367 0.076 2.384 0.865 56.413 0.269 3.850 6.959 0.16 69641. 0.1899 25.98 0.6858 0.7546 0.0377 0.0343 0.071 2.225 0.769 52.646 0.251 3.421 6.626 0.16 69890. 0.1705 27.21 0.7185 0.7489 0.0329 0.0316 0.065 2.049 0.671 48.485 0.231 2.985 6.277 0.16 70149. 0.1509 28.45 0.7511 0.7358 0.0280 0.0286 0.059 1.857 0.572 43.940 0.210 2.542 5.899 0.16 70417. 0.1308 29.69 0.7838 0.7124 0.0231 0.0254 0.052 1.649 0.471 39.023 0.186 2.095 5.474 0.16 70696. 0.1102 30.93 0.8164 0.6736 0.0181 0.0220 0.045 1.426 0.370 33.749 0.161 1.644 4.969 0.16 70984. 0.0886 32.16 0.8491 0.6096 0.0131 0.0183 0.038 1.189 0.268 28.137 0.134 1.193 4.324 0.16 71283. 0.0657 33.40 0.8817 0.4991 0.0082 0.0145 0.030 0.939 0.167 22.213 0.106 0.742 3.408 0.16 71590. 0.0409 34.64 0.9144 0.2856 0.0033 0.0104 0.021 0.677 0.066 16.010 0.076 0.295 1.881 0.17 71907. 0.0142 35.87 0.9470 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 0.0909 0.0340 0.236 4.964 4.173 176.176 0.561 18.563 10.745 0.24 100222. 0.6440 1.84 0.0324 0.0836 0.0905 0.0350 0.244 5.118 4.154 181.645 0.578 18.478 10.373 0.24 100300. 0.6203 3.68 0.0647 0.1612 0.0900 0.0361 0.251 5.280 4.131 187.402 0.597 18.375 9.999 0.24 100389. 0.5962 5.52 0.0971 0.2328 0.0894 0.0373 0.259 5.448 4.103 193.375 0.616 18.252 9.625 0.24 100488. 0.5720 7.36 0.1295 0.2984 0.0887 0.0385 0.267 5.620 4.070 199.474 0.635 18.104 9.255 0.24 100600. 0.5478 9.19 0.1618 0.3584 0.0878 0.0397 0.276 5.792 4.030 205.583 0.654 17.925 8.891 0.24 100725. 0.5236 11.03 0.1942 0.4129 0.0868 0.0408 0.284 5.961 3.982 211.563 0.673 17.710 8.536 0.24 100863. 0.4997 12.87 0.2265 0.4623 0.0855 0.0419 0.291 6.121 3.924 217.248 0.692 17.454 8.193 0.24 101015. 0.4761 14.71 0.2589 0.5070 0.0840 0.0429 0.298 6.267 3.856 222.453 0.708 17.150 7.861 0.24 101183. 0.4529 16.55 0.2913 0.5474 0.0823 0.0438 0.304 6.395 3.775 226.971 0.722 16.792 7.544 0.24 101365. 0.4300 18.39 0.3236 0.5837 0.0802 0.0445 0.309 6.496 3.681 230.582 0.734 16.374 7.241 0.24 101563. 0.4076 20.23 0.3560 0.6165 0.0778 0.0450 0.313 6.566 3.572 233.063 0.742 15.890 6.952 0.24 101776. 0.3855 22.07 0.3884 0.6460 0.0751 0.0452 0.314 6.599 3.448 234.205 0.745 15.338 6.678 0.24 102005. 0.3638 23.91 0.4207 0.6725 0.0721 0.0451 0.314 6.588 3.308 233.843 0.744 14.716 6.417 0.24 102250. 0.3424 25.74 0.4531 0.6963 0.0687 0.0447 0.311 6.533 3.154 231.887 0.738 14.029 6.169 0.24 102511. 0.3214 27.58 0.4855 0.7174 0.0651 0.0440 0.306 6.433 2.986 228.321 0.727 13.283 5.932 0.24 102787. 0.3008 29.42 0.5178 0.7359 0.0612 0.0430 0.299 6.288 2.807 223.171 0.710 12.486 5.705 0.24 103078. 0.2804 31.26 0.5502 0.7518 0.0571 0.0418 0.290 6.099 2.618 216.482 0.689 11.646 5.486 0.24 103385. 0.2604 33.10 0.5826 0.7650 0.0528 0.0402 0.279 5.869 2.421 208.302 0.663 10.769 5.272 0.24 103707. 0.2407 34.94 0.6149 0.7753 0.0483 0.0383 0.266 5.597 2.217 198.671 0.632 9.861 5.061 0.24 104044. 0.2211 36.78 0.6473 0.7823 0.0437 0.0362 0.252 5.286 2.007 187.627 0.597 8.927 4.852 0.24 104396. 0.2017 38.62 0.6796 0.7855 0.0391 0.0338 0.235 4.936 1.792 175.202 0.558 7.972 4.640 0.24 104763. 0.1822 40.46 0.7120 0.7840 0.0343 0.0311 0.216 4.548 1.573 161.427 0.514 6.998 4.420 0.24 105145. 0.1627 42.29 0.7444 0.7765 0.0294 0.0282 0.196 4.123 1.351 146.331 0.466 6.010 4.188 0.24 105541. 0.1428 44.13 0.7767 0.7607 0.0245 0.0251 0.174 3.661 1.126 129.954 0.414 5.011 3.932 0.25 105952. 0.1224 45.97 0.8091 0.7325 0.0196 0.0217 0.151 3.165 0.900 112.341 0.358 4.004 3.635 0.25 106378. 0.1012 47.81 0.8415 0.6840 0.0147 0.0180 0.125 2.636 0.673 93.556 0.298 2.994 3.263 0.25 106818. 0.0786 49.65 0.8738 0.5981 0.0097 0.0142 0.099 2.076 0.446 73.680 0.235 1.985 2.748 0.25 107272. 0.0539 51.49 0.9062 0.4283 0.0048 0.0102 0.071 1.488 0.221 52.819 0.168 0.983 1.897 0.25 107740. 0.0262 53.33 0.9386 -0.0089 -0.0001 0.0060 0.042 0.874 -0.003 31.009 0.099 -0.012 -0.038 0.25 108215. 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 0.0912 0.0332 0.548 8.634 7.441 408.594 0.975 33.097 8.260 0.32 133628. 0.6610 2.45 0.0324 0.0858 0.0908 0.0343 0.566 8.911 7.409 421.710 1.007 32.954 7.968 0.32 133732. 0.6363 4.91 0.0648 0.1652 0.0903 0.0354 0.584 9.203 7.370 435.548 1.040 32.782 7.675 0.32 133849. 0.6113 7.36 0.0972 0.2383 0.0898 0.0366 0.603 9.508 7.323 449.942 1.074 32.574 7.382 0.32 133982. 0.5861 9.82 0.1296 0.3053 0.0891 0.0378 0.623 9.819 7.266 464.680 1.109 32.321 7.093 0.32 134132. 0.5609 12.27 0.1620 0.3664 0.0882 0.0390 0.643 10.132 7.198 479.485 1.145 32.015 6.809 0.32 134298. 0.5359 14.73 0.1944 0.4218 0.0872 0.0402 0.662 10.439 7.115 494.022 1.179 31.645 6.532 0.32 134483. 0.5112 17.18 0.2268 0.4719 0.0860 0.0413 0.681 10.732 7.015 507.893 1.213 31.201 6.264 0.32 134686. 0.4868 19.64 0.2592 0.5172 0.0845 0.0424 0.698 11.002 6.895 520.644 1.243 30.671 6.007 0.32 134910. 0.4628 22.09 0.2916 0.5580 0.0828 0.0433 0.713 11.237 6.754 531.773 1.270 30.043 5.761 0.32 135153. 0.4393 24.55 0.3240 0.5947 0.0808 0.0440 0.725 11.426 6.589 540.745 1.291 29.306 5.526 0.32 135418. 0.4162 27.00 0.3564 0.6279 0.0784 0.0445 0.734 11.559 6.397 547.011 1.306 28.452 5.304 0.32 135703. 0.3935 29.46 0.3888 0.6577 0.0757 0.0448 0.738 11.623 6.176 550.062 1.313 27.472 5.093 0.32 136009. 0.3713 31.91 0.4212 0.6845 0.0727 0.0447 0.737 11.611 5.928 549.489 1.312 26.367 4.893 0.32 136336. 0.3495 34.37 0.4536 0.7087 0.0693 0.0444 0.731 11.518 5.652 545.066 1.301 25.142 4.704 0.32 136685. 0.3281 36.82 0.4860 0.7302 0.0656 0.0437 0.720 11.342 5.353 536.747 1.281 23.810 4.523 0.32 137054. 0.3070 39.28 0.5184 0.7493 0.0617 0.0427 0.703 11.085 5.033 524.589 1.252 22.386 4.351 0.32 137443. 0.2864 41.73 0.5509 0.7658 0.0575 0.0414 0.682 10.749 4.695 508.698 1.214 20.882 4.186 0.32 137854. 0.2661 44.19 0.5833 0.7798 0.0532 0.0398 0.656 10.337 4.342 489.183 1.168 19.312 4.026 0.32 138284. 0.2461 46.64 0.6157 0.7910 0.0487 0.0379 0.625 9.850 3.976 466.147 1.113 17.685 3.869 0.32 138735. 0.2263 49.10 0.6481 0.7993 0.0441 0.0358 0.590 9.291 3.600 439.677 1.050 16.012 3.714 0.32 139205. 0.2067 51.55 0.6805 0.8040 0.0394 0.0333 0.550 8.660 3.215 409.850 0.978 14.299 3.558 0.32 139696. 0.1871 54.00 0.7129 0.8045 0.0346 0.0307 0.505 7.961 2.822 376.738 0.899 12.553 3.398 0.33 140206. 0.1675 56.46 0.7453 0.7994 0.0297 0.0277 0.457 7.193 2.424 340.417 0.813 10.782 3.230 0.33 140736. 0.1475 58.91 0.7777 0.7867 0.0248 0.0245 0.404 6.360 2.021 300.978 0.719 8.990 3.046 0.33 141286. 0.1270 61.37 0.8101 0.7625 0.0198 0.0210 0.347 5.463 1.615 258.533 0.617 7.186 2.834 0.33 141855. 0.1057 63.82 0.8425 0.7192 0.0148 0.0174 0.286 4.506 1.208 213.237 0.509 5.375 2.570 0.33 142443. 0.0829 66.28 0.8749 0.6392 0.0098 0.0134 0.222 3.493 0.802 165.290 0.395 3.566 2.200 0.33 143050. 0.0578 68.73 0.9073 0.4728 0.0049 0.0094 0.154 2.429 0.398 114.950 0.274 1.769 1.569 0.33 143675. 0.0290 71.19 0.9397 -0.0077 0.0000 0.0051 0.083 1.315 -0.003 62.252 0.149 -0.015 -0.025 0.33 144307. 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 0.0915 0.0329 1.058 13.338 11.664 789.010 1.507 51.881 6.705 0.40 167032. 0.6718 3.07 0.0324 0.0871 0.0911 0.0339 1.093 13.775 11.618 814.897 1.556 51.675 6.466 0.40 167161. 0.6466 6.14 0.0649 0.1677 0.0907 0.0351 1.130 14.238 11.562 842.289 1.609 51.426 6.226 0.40 167309. 0.6211 9.22 0.0973 0.2418 0.0902 0.0363 1.168 14.722 11.493 870.870 1.663 51.122 5.986 0.40 167475. 0.5954 12.29 0.1298 0.3097 0.0895 0.0375 1.207 15.218 11.410 900.227 1.719 50.751 5.749 0.40 167661. 0.5697 15.36 0.1622 0.3714 0.0887 0.0387 1.247 15.718 11.308 929.817 1.776 50.297 5.516 0.40 167870. 0.5442 18.43 0.1946 0.4274 0.0877 0.0400 1.286 16.211 11.183 958.972 1.832 49.743 5.289 0.40 168101. 0.5190 21.50 0.2271 0.4780 0.0865 0.0411 1.323 16.683 11.033 986.897 1.885 49.073 5.070 0.40 168356. 0.4941 24.58 0.2595 0.5236 0.0851 0.0422 1.358 17.119 10.851 1012.676 1.934 48.267 4.860 0.40 168635. 0.4697 27.65 0.2920 0.5647 0.0834 0.0431 1.388 17.501 10.635 1035.297 1.977 47.305 4.659 0.40 168940. 0.4458 30.72 0.3244 0.6018 0.0814 0.0439 1.413 17.812 10.380 1053.674 2.012 46.171 4.468 0.40 169271. 0.4224 33.79 0.3568 0.6351 0.0791 0.0444 1.430 18.032 10.083 1066.700 2.037 44.847 4.287 0.40 169629. 0.3994 36.86 0.3893 0.6652 0.0764 0.0447 1.439 18.144 9.740 1073.334 2.050 43.323 4.116 0.40 170013. 0.3769 39.94 0.4217 0.6923 0.0734 0.0447 1.439 18.134 9.352 1072.744 2.049 41.597 3.954 0.40 170423. 0.3548 43.01 0.4542 0.7167 0.0700 0.0443 1.427 17.994 8.921 1064.462 2.033 39.678 3.801 0.40 170859. 0.3331 46.08 0.4866 0.7386 0.0663 0.0437 1.406 17.722 8.450 1048.377 2.002 37.588 3.656 0.40 171322. 0.3118 49.15 0.5190 0.7580 0.0623 0.0427 1.374 17.320 7.947 1024.603 1.957 35.347 3.518 0.40 171811. 0.2909 52.22 0.5515 0.7751 0.0582 0.0414 1.332 16.792 7.414 993.345 1.897 32.979 3.385 0.40 172325. 0.2704 55.30 0.5839 0.7897 0.0538 0.0398 1.280 16.141 6.858 954.829 1.824 30.503 3.258 0.40 172864. 0.2503 58.37 0.6164 0.8017 0.0493 0.0379 1.219 15.371 6.281 909.257 1.737 27.937 3.133 0.40 173429. 0.2304 61.44 0.6488 0.8109 0.0446 0.0357 1.149 14.484 5.687 856.809 1.636 25.295 3.010 0.41 174019. 0.2106 64.51 0.6812 0.8168 0.0398 0.0332 1.070 13.484 5.079 797.637 1.523 22.590 2.888 0.41 174633. 0.1909 67.58 0.7137 0.8187 0.0350 0.0305 0.981 12.372 4.459 731.889 1.398 19.832 2.763 0.41 175273. 0.1712 70.66 0.7461 0.8155 0.0300 0.0275 0.885 11.152 3.829 659.715 1.260 17.033 2.633 0.41 175937. 0.1511 73.73 0.7786 0.8052 0.0250 0.0242 0.780 9.827 3.193 581.297 1.110 14.201 2.491 0.41 176626. 0.1306 76.80 0.8110 0.7841 0.0200 0.0207 0.666 8.399 2.551 496.863 0.949 11.347 2.329 0.41 177338. 0.1091 79.87 0.8434 0.7448 0.0150 0.0169 0.545 6.875 1.907 406.717 0.777 8.484 2.127 0.41 178075. 0.0862 82.94 0.8759 0.6698 0.0099 0.0130 0.417 5.262 1.264 311.269 0.594 5.623 1.842 0.41 178836. 0.0608 86.01 0.9083 0.5067 0.0049 0.0088 0.283 3.567 0.625 211.038 0.403 2.781 1.344 0.41 179619. 0.0312 89.09 0.9408 -0.0167 -0.0001 0.0044 0.142 1.791 -0.010 105.937 0.202 -0.045 -0.043 0.41 180407. 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 0.0918 0.0327 1.820 19.117 16.857 1357.070 2.160 74.980 5.634 0.48 200434. 0.6786 3.71 0.0327 0.0884 0.0915 0.0338 1.881 19.757 16.797 1402.506 2.232 74.712 5.432 0.48 200590. 0.6531 7.42 0.0653 0.1701 0.0911 0.0350 1.946 20.437 16.723 1450.766 2.309 74.385 5.228 0.48 200768. 0.6273 11.13 0.0980 0.2452 0.0906 0.0362 2.013 21.149 16.633 1501.313 2.389 73.982 5.025 0.48 200968. 0.6012 14.84 0.1306 0.3139 0.0900 0.0375 2.083 21.883 16.521 1553.432 2.472 73.484 4.824 0.48 201194. 0.5752 18.55 0.1633 0.3763 0.0892 0.0387 2.154 22.626 16.382 1606.167 2.556 72.869 4.626 0.48 201446. 0.5494 22.26 0.1959 0.4328 0.0883 0.0400 2.224 23.361 16.212 1658.312 2.639 72.109 4.434 0.48 201726. 0.5238 25.98 0.2286 0.4838 0.0872 0.0412 2.291 24.067 16.002 1708.419 2.719 71.178 4.248 0.48 202035. 0.4986 29.69 0.2612 0.5297 0.0858 0.0423 2.353 24.720 15.748 1754.814 2.793 70.045 4.070 0.48 202374. 0.4739 33.40 0.2939 0.5711 0.0841 0.0433 2.408 25.295 15.441 1795.632 2.858 68.682 3.900 0.48 202744. 0.4497 37.11 0.3265 0.6083 0.0821 0.0441 2.453 25.763 15.076 1828.871 2.911 67.058 3.739 0.48 203146. 0.4259 40.82 0.3592 0.6417 0.0798 0.0447 2.484 26.096 14.647 1852.500 2.948 65.150 3.586 0.48 203580. 0.4027 44.53 0.3919 0.6719 0.0771 0.0450 2.500 26.267 14.150 1864.616 2.968 62.941 3.442 0.48 204047. 0.3799 48.24 0.4245 0.6992 0.0740 0.0449 2.499 26.254 13.585 1863.707 2.966 60.426 3.306 0.48 204545. 0.3575 51.95 0.4572 0.7238 0.0706 0.0446 2.479 26.046 12.955 1848.939 2.943 57.623 3.178 0.48 205076. 0.3356 55.66 0.4898 0.7459 0.0668 0.0439 2.441 25.640 12.266 1820.128 2.897 54.561 3.057 0.48 205638. 0.3141 59.37 0.5225 0.7656 0.0628 0.0429 2.384 25.040 11.527 1777.495 2.829 51.274 2.941 0.48 206232. 0.2930 63.08 0.5551 0.7830 0.0585 0.0415 2.308 24.250 10.746 1721.426 2.740 47.797 2.831 0.48 206857. 0.2723 66.79 0.5878 0.7980 0.0541 0.0398 2.216 23.277 9.928 1652.332 2.630 44.159 2.725 0.48 207513. 0.2519 70.50 0.6204 0.8105 0.0495 0.0379 2.106 22.125 9.080 1570.591 2.500 40.387 2.622 0.49 208199. 0.2318 74.22 0.6531 0.8202 0.0447 0.0356 1.980 20.800 8.206 1476.528 2.350 36.501 2.521 0.49 208916. 0.2119 77.93 0.6858 0.8267 0.0398 0.0330 1.838 19.305 7.311 1370.427 2.181 32.522 2.420 0.49 209663. 0.1920 81.64 0.7184 0.8294 0.0349 0.0302 1.680 17.645 6.399 1252.554 1.994 28.464 2.317 0.49 210440. 0.1720 85.35 0.7511 0.8270 0.0298 0.0271 1.506 15.822 5.473 1123.188 1.788 24.345 2.210 0.49 211247. 0.1517 89.06 0.7837 0.8175 0.0247 0.0237 1.318 13.843 4.536 982.663 1.564 20.178 2.094 0.49 212084. 0.1308 92.77 0.8164 0.7971 0.0196 0.0200 1.115 11.712 3.592 831.409 1.323 15.979 1.960 0.49 212950. 0.1090 96.48 0.8490 0.7575 0.0144 0.0162 0.898 9.438 2.645 670.000 1.066 11.767 1.791 0.49 213845. 0.0855 100.19 0.8817 0.6785 0.0093 0.0120 0.669 7.032 1.700 499.205 0.795 7.562 1.545 0.49 214769. 0.0591 103.90 0.9143 0.4916 0.0041 0.0077 0.429 4.508 0.761 319.994 0.509 3.386 1.079 0.50 215720. 0.0276 107.61 0.9470 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 0.0922 0.0327 2.891 26.030 23.035 2155.750 2.941 102.459 4.847 0.56 233833. 0.6824 4.33 0.0326 0.0887 0.0919 0.0338 2.988 26.907 22.964 2228.423 3.040 102.143 4.674 0.56 234015. 0.6571 8.66 0.0653 0.1707 0.0916 0.0350 3.092 27.843 22.876 2305.947 3.146 101.754 4.500 0.56 234222. 0.6314 12.98 0.0979 0.2462 0.0911 0.0362 3.202 28.829 22.768 2387.528 3.257 101.271 4.325 0.56 234455. 0.6055 17.31 0.1306 0.3151 0.0906 0.0375 3.315 29.849 22.632 2472.075 3.372 100.666 4.152 0.56 234718. 0.5796 21.64 0.1632 0.3778 0.0899 0.0388 3.430 30.888 22.461 2558.096 3.490 99.908 3.983 0.56 235011. 0.5538 25.97 0.1959 0.4345 0.0890 0.0401 3.545 31.921 22.248 2643.652 3.606 98.959 3.817 0.56 235337. 0.5282 30.29 0.2285 0.4857 0.0880 0.0414 3.656 32.920 21.983 2726.380 3.719 97.779 3.657 0.56 235697. 0.5030 34.62 0.2611 0.5318 0.0867 0.0426 3.760 33.851 21.655 2803.513 3.825 96.323 3.504 0.56 236092. 0.4783 38.95 0.2938 0.5732 0.0851 0.0436 3.851 34.678 21.256 2871.942 3.918 94.549 3.357 0.56 236523. 0.4541 43.28 0.3264 0.6105 0.0832 0.0445 3.927 35.358 20.776 2928.322 3.995 92.412 3.218 0.56 236992. 0.4303 47.60 0.3591 0.6441 0.0809 0.0451 3.982 35.853 20.206 2969.244 4.051 89.876 3.087 0.56 237498. 0.4071 51.93 0.3917 0.6745 0.0782 0.0454 4.012 36.121 19.540 2991.499 4.081 86.914 2.963 0.56 238042. 0.3842 56.26 0.4244 0.7019 0.0752 0.0454 4.013 36.134 18.777 2992.515 4.082 83.521 2.846 0.56 238624. 0.3618 60.59 0.4570 0.7267 0.0717 0.0451 3.984 35.872 17.922 2970.825 4.053 79.715 2.736 0.56 239243. 0.3398 64.91 0.4896 0.7491 0.0680 0.0444 3.924 35.331 16.983 2926.065 3.992 75.538 2.632 0.56 239900. 0.3183 69.24 0.5223 0.7692 0.0639 0.0434 3.833 34.516 15.971 2858.583 3.900 71.040 2.534 0.56 240593. 0.2971 73.57 0.5549 0.7871 0.0596 0.0420 3.713 33.435 14.898 2769.025 3.777 66.267 2.440 0.56 241322. 0.2763 77.90 0.5876 0.8026 0.0551 0.0404 3.565 32.096 13.773 2658.098 3.626 61.264 2.350 0.56 242088. 0.2559 82.22 0.6202 0.8157 0.0505 0.0384 3.388 30.506 12.605 2526.453 3.447 56.067 2.263 0.57 242889. 0.2357 86.55 0.6528 0.8262 0.0456 0.0361 3.184 28.673 11.400 2374.647 3.239 50.708 2.178 0.57 243725. 0.2157 90.88 0.6855 0.8337 0.0407 0.0335 2.954 26.602 10.165 2203.167 3.006 45.214 2.093 0.57 244597. 0.1957 95.21 0.7181 0.8376 0.0356 0.0306 2.699 24.300 8.904 2012.457 2.745 39.607 2.007 0.57 245504. 0.1757 99.53 0.7508 0.8368 0.0305 0.0274 2.418 21.770 7.623 1802.981 2.460 33.909 1.918 0.57 246445. 0.1554 103.86 0.7834 0.8295 0.0253 0.0239 2.112 19.021 6.327 1575.278 2.149 28.142 1.822 0.57 247421. 0.1344 108.19 0.8161 0.8119 0.0201 0.0202 1.784 16.060 5.020 1330.039 1.814 22.327 1.712 0.57 248431. 0.1125 112.52 0.8487 0.7765 0.0148 0.0162 1.432 12.898 3.707 1068.194 1.457 16.490 1.574 0.58 249475. 0.0889 116.85 0.8813 0.7038 0.0096 0.0120 1.061 9.551 2.396 790.988 1.079 10.658 1.374 0.58 250552. 0.0624 121.17 0.9140 0.5271 0.0044 0.0076 0.671 6.037 1.094 500.009 0.682 4.865 0.992 0.58 251661. 0.0304 125.50 0.9466 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 0.0926 0.0329 4.344 34.221 30.212 3238.999 3.866 134.382 4.231 0.63 267231. 0.6822 4.92 0.0325 0.0881 0.0923 0.0340 4.489 35.363 30.135 3347.124 3.995 134.039 4.084 0.63 267437. 0.6577 9.84 0.0650 0.1698 0.0921 0.0352 4.644 36.588 30.040 3462.999 4.134 133.617 3.934 0.63 267671. 0.6327 14.76 0.0974 0.2450 0.0917 0.0365 4.808 37.883 29.921 3585.584 4.280 133.088 3.785 0.63 267935. 0.6074 19.69 0.1299 0.3138 0.0912 0.0378 4.980 39.233 29.770 3713.411 4.433 132.418 3.636 0.64 268232. 0.5821 24.61 0.1624 0.3765 0.0906 0.0391 5.155 40.617 29.578 3844.373 4.589 131.564 3.490 0.64 268564. 0.5568 29.53 0.1949 0.4332 0.0899 0.0404 5.331 42.004 29.334 3975.665 4.746 130.477 3.347 0.64 268933. 0.5318 34.45 0.2274 0.4845 0.0889 0.0417 5.503 43.358 29.024 4103.771 4.899 129.098 3.208 0.64 269340. 0.5070 39.37 0.2598 0.5307 0.0877 0.0430 5.665 44.633 28.635 4224.486 5.043 127.368 3.074 0.64 269787. 0.4827 44.29 0.2923 0.5722 0.0863 0.0441 5.811 45.780 28.152 4333.013 5.172 125.222 2.947 0.64 270276. 0.4587 49.21 0.3248 0.6097 0.0845 0.0450 5.933 46.742 27.562 4424.126 5.281 122.597 2.826 0.64 270806. 0.4352 54.14 0.3573 0.6434 0.0823 0.0457 6.024 47.464 26.853 4492.432 5.362 119.440 2.711 0.64 271380. 0.4122 59.06 0.3898 0.6739 0.0797 0.0461 6.079 47.890 26.014 4532.789 5.411 115.708 2.603 0.64 271996. 0.3895 63.98 0.4223 0.7016 0.0767 0.0462 6.090 47.977 25.042 4540.956 5.420 111.387 2.501 0.64 272656. 0.3672 68.90 0.4547 0.7266 0.0734 0.0459 6.054 47.695 23.943 4514.343 5.389 106.499 2.406 0.64 273358. 0.3453 73.82 0.4872 0.7493 0.0696 0.0453 5.970 47.038 22.728 4452.159 5.314 101.095 2.315 0.64 274103. 0.3239 78.74 0.5197 0.7699 0.0656 0.0443 5.840 46.010 21.412 4354.817 5.198 95.241 2.230 0.64 274889. 0.3028 83.66 0.5522 0.7882 0.0613 0.0430 5.664 44.621 20.010 4223.322 5.041 89.003 2.149 0.64 275716. 0.2820 88.58 0.5847 0.8043 0.0568 0.0413 5.443 42.883 18.534 4058.821 4.845 82.440 2.071 0.65 276584. 0.2616 93.51 0.6171 0.8182 0.0521 0.0393 5.180 40.807 16.998 3862.395 4.610 75.605 1.996 0.65 277493. 0.2414 98.43 0.6496 0.8297 0.0472 0.0370 4.875 38.405 15.410 3634.974 4.339 68.542 1.923 0.65 278441. 0.2214 103.35 0.6821 0.8384 0.0422 0.0344 4.529 35.683 13.778 3377.354 4.031 61.287 1.850 0.65 279430. 0.2015 108.27 0.7146 0.8438 0.0371 0.0314 4.144 32.649 12.112 3090.253 3.689 53.872 1.778 0.65 280457. 0.1815 113.19 0.7471 0.8450 0.0319 0.0282 3.721 29.312 10.415 2774.377 3.312 46.328 1.703 0.65 281524. 0.1612 118.11 0.7795 0.8403 0.0266 0.0247 3.259 25.679 8.696 2430.533 2.901 38.681 1.623 0.65 282630. 0.1404 123.03 0.8120 0.8268 0.0213 0.0210 2.762 21.762 6.961 2059.733 2.459 30.961 1.533 0.66 283775. 0.1186 127.96 0.8445 0.7978 0.0160 0.0169 2.231 17.573 5.216 1663.319 1.985 23.200 1.422 0.66 284957. 0.0953 132.88 0.8770 0.7376 0.0106 0.0126 1.667 13.134 3.470 1243.111 1.484 15.436 1.266 0.66 286178. 0.0692 137.80 0.9095 0.5927 0.0053 0.0082 1.075 8.468 1.734 801.473 0.957 7.711 0.981 0.66 287434. 0.0379 142.72 0.9420 0.0016 0.0000 0.0034 0.452 3.562 0.002 337.175 0.402 0.008 0.003 0.66 288689. 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 0.0930 0.0340 6.374 44.636 38.393 4752.830 5.043 170.772 3.664 0.71 300626. 0.6660 5.54 0.0325 0.0861 0.0928 0.0350 6.578 46.067 38.315 4905.221 5.205 170.424 3.543 0.71 300857. 0.6434 11.08 0.0650 0.1662 0.0925 0.0362 6.798 47.607 38.219 5069.237 5.379 169.998 3.420 0.71 301120. 0.6202 16.63 0.0975 0.2402 0.0922 0.0375 7.032 49.244 38.098 5243.568 5.564 169.461 3.296 0.71 301417. 0.5968 22.17 0.1301 0.3082 0.0919 0.0388 7.277 50.960 37.943 5426.240 5.757 168.772 3.172 0.71 301750. 0.5732 27.71 0.1626 0.3704 0.0914 0.0401 7.529 52.726 37.742 5614.312 5.957 167.878 3.049 0.71 302123. 0.5496 33.25 0.1951 0.4270 0.0907 0.0415 7.783 54.505 37.481 5803.748 6.158 166.713 2.929 0.72 302537. 0.5261 38.79 0.2276 0.4783 0.0899 0.0428 8.032 56.248 37.140 5989.374 6.355 165.201 2.813 0.72 302994. 0.5029 44.34 0.2601 0.5249 0.0889 0.0440 8.267 57.897 36.703 6164.929 6.541 163.254 2.700 0.72 303497. 0.4800 49.88 0.2926 0.5670 0.0875 0.0452 8.480 59.384 36.146 6323.213 6.709 160.779 2.593 0.72 304047. 0.4573 55.42 0.3251 0.6051 0.0858 0.0461 8.658 60.634 35.451 6456.385 6.850 157.685 2.490 0.72 304644. 0.4350 60.96 0.3576 0.6397 0.0838 0.0468 8.792 61.574 34.597 6556.436 6.957 153.888 2.393 0.72 305290. 0.4130 66.50 0.3902 0.6710 0.0813 0.0473 8.872 62.131 33.571 6615.787 7.020 149.324 2.302 0.72 305985. 0.3912 72.05 0.4227 0.6995 0.0784 0.0473 8.889 62.248 32.366 6628.161 7.033 143.963 2.215 0.72 306729. 0.3697 77.59 0.4552 0.7255 0.0750 0.0471 8.837 61.886 30.987 6589.700 6.992 137.829 2.133 0.72 307522. 0.3483 83.13 0.4877 0.7490 0.0713 0.0464 8.716 61.036 29.448 6499.175 6.896 130.986 2.055 0.72 308362. 0.3272 88.67 0.5202 0.7702 0.0672 0.0454 8.525 59.702 27.770 6357.147 6.745 123.522 1.981 0.72 309250. 0.3063 94.21 0.5527 0.7892 0.0629 0.0440 8.267 57.898 25.973 6165.005 6.541 115.527 1.911 0.72 310184. 0.2857 99.76 0.5852 0.8061 0.0583 0.0423 7.945 55.637 24.075 5924.295 6.286 107.084 1.843 0.73 311164. 0.2653 105.30 0.6177 0.8206 0.0535 0.0403 7.559 52.934 22.092 5636.455 5.980 98.263 1.778 0.73 312189. 0.2451 110.84 0.6503 0.8328 0.0485 0.0379 7.111 49.800 20.038 5302.725 5.626 89.127 1.714 0.73 313260. 0.2251 116.38 0.6828 0.8424 0.0434 0.0352 6.603 46.245 17.924 4924.190 5.225 79.727 1.651 0.73 314375. 0.2051 121.92 0.7153 0.8488 0.0382 0.0322 6.037 42.279 15.761 4501.857 4.777 70.105 1.588 0.73 315535. 0.1850 127.47 0.7478 0.8512 0.0328 0.0288 5.413 37.911 13.557 4036.778 4.283 60.301 1.523 0.73 316738. 0.1645 133.01 0.7803 0.8481 0.0274 0.0252 4.734 33.153 11.320 3530.158 3.746 50.353 1.454 0.74 317986. 0.1436 138.55 0.8128 0.8366 0.0219 0.0213 4.001 28.019 9.060 2983.502 3.166 40.299 1.377 0.74 319277. 0.1216 144.09 0.8453 0.8104 0.0164 0.0171 3.217 22.529 6.785 2398.892 2.545 30.182 1.283 0.74 320610. 0.0980 149.63 0.8779 0.7537 0.0109 0.0127 2.386 16.711 4.508 1779.372 1.888 20.050 1.149 0.74 321986. 0.0716 155.18 0.9104 0.6118 0.0054 0.0081 1.514 10.606 2.239 1129.294 1.198 9.960 0.899 0.74 323403. 0.0395 160.72 0.9429 -0.0223 -0.0001 0.0032 0.599 4.192 -0.031 446.344 0.474 -0.139 -0.032 0.75 324804. 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 0.0933 0.0370 9.540 60.127 47.563 7113.707 6.793 211.561 3.033 0.79 334019. 0.6136 6.16 0.0325 0.0795 0.0931 0.0381 9.815 61.860 47.486 7318.797 6.989 211.220 2.943 0.79 334275. 0.5950 12.32 0.0651 0.1540 0.0930 0.0393 10.112 63.736 47.395 7540.725 7.201 210.811 2.851 0.79 334566. 0.5758 18.48 0.0976 0.2234 0.0927 0.0405 10.430 65.740 47.280 7777.875 7.427 210.302 2.757 0.79 334895. 0.5562 24.64 0.1301 0.2877 0.0924 0.0418 10.765 67.852 47.133 8027.667 7.666 209.648 2.663 0.79 335265. 0.5364 30.80 0.1626 0.3470 0.0921 0.0432 11.112 70.036 46.940 8286.030 7.913 208.789 2.569 0.79 335677. 0.5165 36.96 0.1952 0.4014 0.0916 0.0445 11.462 72.242 46.683 8547.137 8.162 207.647 2.477 0.79 336135. 0.4966 43.12 0.2277 0.4514 0.0909 0.0458 11.805 74.407 46.341 8803.198 8.406 206.125 2.388 0.80 336642. 0.4769 49.29 0.2602 0.4972 0.0900 0.0471 12.129 76.446 45.887 9044.450 8.637 204.106 2.301 0.80 337199. 0.4573 55.45 0.2928 0.5393 0.0888 0.0482 12.417 78.263 45.293 9259.468 8.842 201.462 2.219 0.80 337808. 0.4381 61.61 0.3253 0.5781 0.0873 0.0491 12.654 79.754 44.527 9435.811 9.011 198.056 2.140 0.80 338471. 0.4190 67.77 0.3578 0.6139 0.0854 0.0498 12.821 80.812 43.561 9560.983 9.130 193.759 2.067 0.80 339189. 0.4001 73.93 0.3903 0.6472 0.0831 0.0501 12.906 81.342 42.371 9623.746 9.190 188.465 1.997 0.80 339961. 0.3814 80.09 0.4229 0.6781 0.0803 0.0501 12.895 81.273 40.944 9615.545 9.182 182.117 1.931 0.80 340789. 0.3626 86.25 0.4554 0.7068 0.0770 0.0496 12.783 80.566 39.282 9531.958 9.102 174.725 1.869 0.80 341671. 0.3437 92.41 0.4879 0.7333 0.0734 0.0488 12.569 79.222 37.402 9372.860 8.950 166.365 1.810 0.80 342607. 0.3248 98.57 0.5205 0.7575 0.0693 0.0476 12.258 77.262 35.330 9140.964 8.729 157.148 1.753 0.80 343596. 0.3057 104.73 0.5530 0.7796 0.0649 0.0460 11.855 74.717 33.092 8839.953 8.442 147.194 1.698 0.81 344637. 0.2866 110.89 0.5855 0.7993 0.0602 0.0441 11.363 71.619 30.714 8473.315 8.091 136.615 1.644 0.81 345729. 0.2673 117.05 0.6180 0.8165 0.0553 0.0419 10.787 67.988 28.217 8043.803 7.681 125.510 1.591 0.81 346872. 0.2480 123.21 0.6506 0.8311 0.0502 0.0393 10.129 63.842 25.621 7553.288 7.213 113.963 1.539 0.81 348065. 0.2285 129.37 0.6831 0.8428 0.0450 0.0365 9.391 59.190 22.942 7002.929 6.687 102.045 1.486 0.81 349308. 0.2088 135.53 0.7156 0.8512 0.0396 0.0333 8.574 54.039 20.193 6393.480 6.105 89.817 1.433 0.81 350599. 0.1889 141.69 0.7481 0.8555 0.0341 0.0298 7.678 48.394 17.386 5725.545 5.467 77.332 1.377 0.82 351940. 0.1685 147.86 0.7807 0.8544 0.0285 0.0260 6.706 42.267 14.532 5000.738 4.775 64.639 1.318 0.82 353328. 0.1474 154.02 0.8132 0.8439 0.0228 0.0220 5.666 35.710 11.642 4224.883 4.034 51.785 1.250 0.82 354765. 0.1251 160.18 0.8457 0.8175 0.0171 0.0177 4.560 28.743 8.729 3400.590 3.247 38.825 1.164 0.82 356249. 0.1009 166.34 0.8783 0.7570 0.0114 0.0132 3.401 21.435 5.804 2536.045 2.422 25.818 1.038 0.82 357780. 0.0734 172.50 0.9108 0.6028 0.0057 0.0085 2.202 13.877 2.886 1641.775 1.568 12.835 0.797 0.83 359356. 0.0397 178.66 0.9433 -0.0211 -0.0001 0.0037 0.963 6.067 -0.043 717.796 0.685 -0.190 -0.027 0.83 360917. 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 0.0932 0.0431 14.786 84.721 57.473 11025.837 9.572 255.638 2.364 0.87 367414. 0.5258 6.79 0.0326 0.0686 0.0930 0.0442 15.136 86.728 57.389 11287.072 9.799 255.266 2.306 0.87 367697. 0.5126 13.57 0.0652 0.1336 0.0929 0.0453 15.518 88.918 57.294 11572.076 10.046 254.844 2.246 0.87 368017. 0.4987 20.36 0.0977 0.1949 0.0927 0.0465 15.929 91.269 57.180 11878.015 10.312 254.335 2.183 0.87 368379. 0.4844 27.15 0.1303 0.2523 0.0924 0.0477 16.365 93.769 57.038 12203.347 10.594 253.704 2.120 0.87 368785. 0.4697 33.94 0.1629 0.3059 0.0922 0.0491 16.821 96.381 56.855 12543.257 10.889 252.891 2.056 0.87 369238. 0.4548 40.72 0.1955 0.3556 0.0918 0.0504 17.286 99.048 56.613 12890.339 11.190 251.813 1.992 0.87 369741. 0.4397 47.51 0.2281 0.4018 0.0912 0.0518 17.747 101.688 56.286 13234.037 11.489 250.361 1.929 0.87 370297. 0.4246 54.30 0.2606 0.4447 0.0905 0.0531 18.185 104.195 55.846 13560.244 11.772 248.401 1.868 0.88 370909. 0.4095 61.09 0.2932 0.4845 0.0896 0.0542 18.575 106.432 55.253 13851.434 12.025 245.768 1.809 0.88 371578. 0.3946 67.87 0.3258 0.5218 0.0883 0.0551 18.892 108.246 54.469 14087.465 12.230 242.279 1.754 0.88 372306. 0.3797 74.66 0.3584 0.5570 0.0866 0.0557 19.106 109.474 53.450 14247.316 12.368 237.747 1.702 0.88 373095. 0.3650 81.45 0.3910 0.5903 0.0845 0.0560 19.192 109.967 52.160 14311.485 12.424 232.007 1.653 0.88 373945. 0.3503 88.24 0.4235 0.6220 0.0820 0.0558 19.129 109.608 50.572 14264.746 12.383 224.943 1.608 0.88 374857. 0.3355 95.02 0.4561 0.6524 0.0789 0.0552 18.907 108.333 48.680 14098.788 12.239 216.528 1.566 0.88 375829. 0.3206 101.81 0.4887 0.6815 0.0754 0.0540 18.522 106.129 46.496 13811.989 11.990 206.816 1.527 0.88 376862. 0.3055 108.60 0.5213 0.7093 0.0714 0.0525 17.984 103.046 44.049 13410.729 11.642 195.929 1.490 0.88 377955. 0.2901 115.38 0.5538 0.7356 0.0671 0.0505 17.304 99.149 41.369 12903.534 11.202 184.008 1.454 0.89 379105. 0.2744 122.17 0.5864 0.7601 0.0624 0.0481 16.494 94.510 38.487 12299.873 10.678 171.191 1.419 0.89 380312. 0.2583 128.96 0.6190 0.7827 0.0574 0.0454 15.568 89.200 35.434 11608.719 10.078 157.612 1.384 0.89 381576. 0.2418 135.75 0.6516 0.8029 0.0522 0.0424 14.533 83.273 32.236 10837.373 9.408 143.386 1.349 0.89 382894. 0.2247 142.53 0.6842 0.8202 0.0469 0.0391 13.398 76.769 28.915 9990.987 8.673 128.614 1.313 0.89 384268. 0.2071 149.32 0.7167 0.8342 0.0413 0.0355 12.167 69.713 25.491 9072.606 7.876 113.382 1.274 0.90 385696. 0.1888 156.11 0.7493 0.8440 0.0356 0.0316 10.841 62.119 21.981 8084.378 7.018 97.771 1.233 0.90 387177. 0.1696 162.90 0.7819 0.8478 0.0298 0.0275 9.428 54.023 18.402 7030.667 6.103 81.851 1.187 0.90 388711. 0.1494 169.68 0.8145 0.8343 0.0239 0.0234 8.003 45.857 14.757 5968.016 5.181 65.640 1.122 0.90 390298. 0.1264 176.47 0.8471 0.7931 0.0179 0.0192 6.566 37.622 11.067 4896.256 4.251 49.224 1.025 0.90 391937. 0.1001 183.26 0.8796 0.7049 0.0119 0.0149 5.100 29.220 7.356 3802.793 3.301 32.719 0.877 0.91 393627. 0.0698 190.05 0.9122 0.5092 0.0059 0.0106 3.632 20.810 3.649 2708.281 2.351 16.231 0.611 0.91 395367. 0.0342 196.83 0.9448 -0.0136 -0.0001 0.0063 2.169 12.427 -0.056 1617.332 1.404 -0.251 -0.016 0.91 397118. 0.0000