20x8W (20x8W.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 0.0804 0.0307 0.008 0.498 0.410 5.895 0.056 1.824 31.542 0.08 47584. 0.5925 0.37 0.0195 0.0498 0.0787 0.0308 0.008 0.500 0.401 5.917 0.057 1.786 30.771 0.08 47609. 0.5720 0.74 0.0390 0.0971 0.0770 0.0309 0.008 0.502 0.392 5.933 0.057 1.746 29.999 0.08 47636. 0.5514 1.11 0.0585 0.1419 0.0751 0.0309 0.008 0.502 0.383 5.943 0.057 1.703 29.229 0.08 47665. 0.5307 1.48 0.0779 0.1842 0.0732 0.0310 0.008 0.503 0.373 5.945 0.057 1.659 28.460 0.08 47695. 0.5100 1.85 0.0974 0.2240 0.0711 0.0309 0.008 0.502 0.363 5.940 0.057 1.613 27.693 0.08 47727. 0.4893 2.21 0.1169 0.2614 0.0690 0.0309 0.008 0.501 0.352 5.925 0.057 1.565 26.927 0.08 47761. 0.4685 2.58 0.1364 0.2963 0.0668 0.0307 0.008 0.499 0.340 5.902 0.056 1.514 26.162 0.08 47797. 0.4478 2.95 0.1559 0.3287 0.0645 0.0306 0.008 0.496 0.329 5.869 0.056 1.462 25.398 0.08 47835. 0.4272 3.32 0.1754 0.3587 0.0621 0.0303 0.008 0.492 0.316 5.827 0.056 1.407 24.632 0.08 47874. 0.4065 3.69 0.1949 0.3861 0.0596 0.0301 0.008 0.488 0.304 5.773 0.055 1.351 23.865 0.08 47916. 0.3859 4.06 0.2144 0.4110 0.0570 0.0297 0.008 0.483 0.291 5.709 0.055 1.293 23.095 0.08 47959. 0.3653 4.43 0.2338 0.4334 0.0544 0.0293 0.008 0.476 0.277 5.633 0.054 1.233 22.320 0.08 48005. 0.3448 4.80 0.2533 0.4530 0.0516 0.0289 0.007 0.469 0.263 5.545 0.053 1.171 21.537 0.08 48053. 0.3242 5.17 0.2728 0.4699 0.0488 0.0284 0.007 0.460 0.249 5.445 0.052 1.108 20.744 0.08 48103. 0.3037 5.54 0.2923 0.4839 0.0460 0.0278 0.007 0.451 0.234 5.331 0.051 1.042 19.939 0.08 48155. 0.2832 5.91 0.3118 0.4949 0.0430 0.0271 0.007 0.440 0.219 5.204 0.050 0.976 19.116 0.08 48209. 0.2627 6.27 0.3313 0.5026 0.0400 0.0264 0.007 0.428 0.204 5.064 0.048 0.907 18.271 0.08 48266. 0.2421 6.64 0.3508 0.5067 0.0369 0.0256 0.007 0.415 0.188 4.909 0.047 0.838 17.398 0.08 48325. 0.2215 7.01 0.3703 0.5069 0.0338 0.0247 0.006 0.401 0.172 4.740 0.045 0.766 16.489 0.08 48387. 0.2008 7.38 0.3897 0.5027 0.0306 0.0237 0.006 0.385 0.156 4.555 0.044 0.694 15.535 0.08 48450. 0.1800 7.75 0.4092 0.4934 0.0274 0.0227 0.006 0.368 0.139 4.356 0.042 0.620 14.522 0.08 48516. 0.1591 8.12 0.4287 0.4783 0.0241 0.0216 0.006 0.350 0.123 4.141 0.040 0.546 13.436 0.08 48585. 0.1381 8.49 0.4482 0.4560 0.0207 0.0204 0.005 0.331 0.106 3.911 0.037 0.470 12.253 0.08 48656. 0.1168 8.86 0.4677 0.4250 0.0173 0.0191 0.005 0.310 0.088 3.665 0.035 0.393 10.945 0.08 48730. 0.0955 9.23 0.4872 0.3831 0.0139 0.0177 0.005 0.288 0.071 3.404 0.033 0.316 9.471 0.08 48806. 0.0741 9.60 0.5067 0.3270 0.0105 0.0163 0.004 0.264 0.054 3.127 0.030 0.238 7.773 0.08 48884. 0.0528 9.96 0.5261 0.2517 0.0071 0.0148 0.004 0.240 0.036 2.835 0.027 0.160 5.762 0.08 48964. 0.0321 10.33 0.5456 0.1496 0.0036 0.0132 0.003 0.214 0.018 2.529 0.024 0.082 3.302 0.08 49047. 0.0131 10.70 0.5651 0.0064 0.0001 0.0115 0.003 0.186 0.001 2.205 0.021 0.003 0.136 0.08 49126. 0.0001 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 0.0808 0.0275 0.057 1.784 1.648 42.221 0.202 7.332 17.709 0.16 95166. 0.6671 0.75 0.0197 0.0565 0.0791 0.0276 0.057 1.793 1.614 42.435 0.203 7.179 17.251 0.16 95218. 0.6430 1.49 0.0395 0.1100 0.0773 0.0277 0.057 1.800 1.578 42.601 0.203 7.017 16.796 0.16 95272. 0.6189 2.24 0.0592 0.1606 0.0755 0.0278 0.057 1.805 1.539 42.711 0.204 6.846 16.345 0.16 95331. 0.5949 2.99 0.0789 0.2083 0.0735 0.0278 0.057 1.807 1.499 42.759 0.204 6.667 15.899 0.16 95392. 0.5711 3.74 0.0986 0.2532 0.0714 0.0278 0.057 1.806 1.457 42.741 0.204 6.479 15.458 0.16 95457. 0.5473 4.48 0.1184 0.2952 0.0693 0.0278 0.057 1.802 1.412 42.651 0.204 6.283 15.021 0.16 95526. 0.5237 5.23 0.1381 0.3345 0.0670 0.0277 0.057 1.795 1.366 42.484 0.203 6.078 14.588 0.16 95599. 0.5003 5.98 0.1578 0.3711 0.0646 0.0275 0.057 1.785 1.319 42.235 0.202 5.865 14.160 0.16 95676. 0.4770 6.72 0.1775 0.4049 0.0622 0.0273 0.056 1.771 1.269 41.900 0.200 5.644 13.735 0.16 95756. 0.4539 7.47 0.1973 0.4361 0.0597 0.0270 0.056 1.753 1.217 41.475 0.198 5.415 13.312 0.16 95841. 0.4309 8.22 0.2170 0.4645 0.0571 0.0267 0.055 1.731 1.164 40.954 0.196 5.178 12.892 0.16 95930. 0.4081 8.97 0.2367 0.4903 0.0544 0.0263 0.054 1.705 1.109 40.333 0.193 4.934 12.473 0.16 96023. 0.3854 9.71 0.2564 0.5133 0.0516 0.0258 0.053 1.674 1.053 39.608 0.189 4.682 12.054 0.16 96120. 0.3628 10.46 0.2762 0.5335 0.0488 0.0252 0.052 1.639 0.995 38.775 0.185 4.424 11.634 0.16 96222. 0.3404 11.21 0.2959 0.5508 0.0458 0.0246 0.051 1.599 0.935 37.829 0.181 4.159 11.210 0.16 96329. 0.3180 11.95 0.3156 0.5650 0.0428 0.0239 0.049 1.554 0.874 36.767 0.176 3.887 10.780 0.16 96440. 0.2957 12.70 0.3353 0.5759 0.0398 0.0232 0.048 1.504 0.811 35.584 0.170 3.609 10.343 0.16 96556. 0.2733 13.45 0.3551 0.5833 0.0367 0.0223 0.046 1.449 0.748 34.277 0.164 3.326 9.893 0.16 96677. 0.2510 14.20 0.3748 0.5867 0.0335 0.0214 0.044 1.388 0.683 32.843 0.157 3.036 9.427 0.16 96802. 0.2285 14.94 0.3945 0.5856 0.0302 0.0204 0.042 1.322 0.616 31.279 0.149 2.742 8.939 0.16 96932. 0.2059 15.69 0.4142 0.5793 0.0269 0.0193 0.040 1.250 0.549 29.582 0.141 2.443 8.421 0.16 97068. 0.1831 16.44 0.4340 0.5666 0.0236 0.0181 0.037 1.173 0.481 27.752 0.133 2.140 7.862 0.16 97208. 0.1600 17.19 0.4537 0.5459 0.0202 0.0168 0.035 1.090 0.412 25.786 0.123 1.832 7.246 0.16 97353. 0.1365 17.93 0.4734 0.5152 0.0168 0.0154 0.032 1.001 0.342 23.685 0.113 1.522 6.553 0.16 97503. 0.1125 18.68 0.4931 0.4707 0.0133 0.0140 0.029 0.907 0.272 21.450 0.102 1.209 5.748 0.16 97658. 0.0879 19.43 0.5129 0.4070 0.0099 0.0124 0.026 0.806 0.201 19.082 0.091 0.894 4.779 0.16 97819. 0.0629 20.17 0.5326 0.3145 0.0064 0.0108 0.022 0.701 0.130 16.585 0.079 0.578 3.556 0.16 97983. 0.0376 20.92 0.5523 0.1755 0.0029 0.0091 0.019 0.590 0.059 13.957 0.067 0.262 1.913 0.16 98151. 0.0136 21.67 0.5720 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 0.0813 0.0263 0.183 3.836 3.731 136.170 0.433 16.595 12.427 0.24 142745. 0.7042 1.12 0.0197 0.0592 0.0796 0.0264 0.184 3.858 3.653 136.938 0.436 16.250 12.101 0.24 142822. 0.6785 2.23 0.0393 0.1153 0.0778 0.0265 0.184 3.875 3.571 137.542 0.438 15.886 11.777 0.24 142904. 0.6530 3.35 0.0590 0.1683 0.0759 0.0266 0.185 3.887 3.485 137.957 0.439 15.502 11.458 0.24 142991. 0.6276 4.47 0.0786 0.2182 0.0740 0.0266 0.185 3.893 3.395 138.164 0.440 15.099 11.144 0.24 143084. 0.6024 5.58 0.0983 0.2652 0.0719 0.0266 0.185 3.892 3.300 138.143 0.440 14.677 10.834 0.24 143181. 0.5774 6.70 0.1179 0.3093 0.0697 0.0266 0.185 3.885 3.200 137.877 0.439 14.236 10.528 0.24 143284. 0.5526 7.82 0.1376 0.3505 0.0675 0.0265 0.184 3.870 3.097 137.349 0.437 13.775 10.227 0.24 143393. 0.5280 8.93 0.1572 0.3889 0.0651 0.0263 0.183 3.847 2.989 136.541 0.435 13.297 9.930 0.24 143507. 0.5037 10.05 0.1769 0.4246 0.0627 0.0261 0.182 3.816 2.878 135.439 0.431 12.799 9.637 0.24 143628. 0.4796 11.17 0.1965 0.4576 0.0602 0.0259 0.180 3.776 2.762 134.027 0.427 12.285 9.347 0.24 143754. 0.4557 12.28 0.2162 0.4879 0.0576 0.0255 0.177 3.727 2.642 132.289 0.421 11.753 9.059 0.24 143887. 0.4320 13.40 0.2359 0.5155 0.0549 0.0251 0.175 3.669 2.519 130.209 0.414 11.204 8.774 0.24 144026. 0.4085 14.52 0.2555 0.5404 0.0521 0.0246 0.171 3.600 2.392 127.772 0.407 10.639 8.491 0.24 144172. 0.3852 15.63 0.2752 0.5625 0.0493 0.0241 0.168 3.521 2.261 124.963 0.398 10.058 8.207 0.24 144324. 0.3621 16.75 0.2948 0.5819 0.0464 0.0235 0.163 3.431 2.127 121.768 0.388 9.462 7.924 0.24 144483. 0.3391 17.87 0.3145 0.5983 0.0434 0.0228 0.158 3.329 1.990 118.173 0.376 8.852 7.638 0.24 144649. 0.3161 18.98 0.3341 0.6116 0.0403 0.0220 0.153 3.217 1.850 114.165 0.363 8.227 7.349 0.24 144822. 0.2932 20.10 0.3538 0.6216 0.0372 0.0212 0.147 3.092 1.706 109.731 0.349 7.590 7.053 0.24 145002. 0.2703 21.22 0.3734 0.6278 0.0340 0.0202 0.141 2.954 1.560 104.860 0.334 6.940 6.749 0.24 145189. 0.2473 22.33 0.3931 0.6298 0.0308 0.0192 0.133 2.805 1.412 99.542 0.317 6.279 6.432 0.24 145384. 0.2242 23.45 0.4127 0.6269 0.0275 0.0181 0.126 2.642 1.261 93.770 0.298 5.607 6.097 0.24 145585. 0.2008 24.57 0.4324 0.6179 0.0241 0.0169 0.117 2.466 1.107 87.537 0.279 4.925 5.737 0.24 145794. 0.1771 25.68 0.4520 0.6015 0.0207 0.0156 0.108 2.278 0.952 80.840 0.257 4.235 5.342 0.24 146011. 0.1529 26.80 0.4717 0.5752 0.0173 0.0142 0.099 2.076 0.795 73.676 0.235 3.537 4.896 0.24 146235. 0.1281 27.92 0.4914 0.5355 0.0139 0.0127 0.089 1.861 0.637 66.050 0.210 2.834 4.375 0.24 146466. 0.1025 29.03 0.5110 0.4761 0.0104 0.0112 0.078 1.633 0.478 57.966 0.185 2.126 3.740 0.24 146705. 0.0759 30.15 0.5307 0.3861 0.0069 0.0095 0.066 1.393 0.318 49.434 0.157 1.416 2.921 0.24 146950. 0.0483 31.27 0.5503 0.2434 0.0035 0.0078 0.054 1.140 0.158 40.458 0.129 0.704 1.775 0.24 147200. 0.0207 32.38 0.5700 -0.0130 -0.0001 0.0059 0.041 0.867 -0.006 30.756 0.098 -0.028 -0.092 0.24 147396. 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 0.0819 0.0257 0.424 6.676 6.683 315.918 0.754 29.726 9.595 0.32 190318. 0.7277 1.50 0.0198 0.0613 0.0802 0.0259 0.426 6.716 6.544 317.811 0.759 29.106 9.339 0.32 190422. 0.7009 2.99 0.0395 0.1193 0.0784 0.0260 0.428 6.747 6.396 319.300 0.762 28.451 9.086 0.32 190533. 0.6742 4.49 0.0593 0.1740 0.0765 0.0261 0.430 6.769 6.241 320.332 0.765 27.761 8.837 0.32 190650. 0.6477 5.99 0.0791 0.2256 0.0745 0.0261 0.430 6.780 6.078 320.854 0.766 27.037 8.593 0.32 190774. 0.6215 7.49 0.0988 0.2741 0.0724 0.0261 0.430 6.779 5.908 320.820 0.766 26.277 8.352 0.32 190906. 0.5956 8.98 0.1186 0.3197 0.0702 0.0261 0.429 6.766 5.729 320.186 0.764 25.482 8.115 0.32 191045. 0.5699 10.48 0.1384 0.3622 0.0679 0.0259 0.428 6.739 5.543 318.910 0.761 24.653 7.883 0.32 191191. 0.5445 11.98 0.1581 0.4020 0.0656 0.0258 0.425 6.697 5.349 316.953 0.757 23.791 7.654 0.32 191346. 0.5193 13.48 0.1779 0.4389 0.0631 0.0256 0.421 6.641 5.147 314.274 0.750 22.895 7.429 0.32 191508. 0.4945 14.97 0.1977 0.4731 0.0605 0.0253 0.417 6.568 4.939 310.835 0.742 21.967 7.207 0.32 191678. 0.4699 16.47 0.2174 0.5046 0.0579 0.0249 0.411 6.479 4.723 306.598 0.732 21.009 6.987 0.32 191857. 0.4455 17.97 0.2372 0.5333 0.0552 0.0245 0.404 6.371 4.501 301.525 0.720 20.019 6.770 0.32 192045. 0.4214 19.47 0.2570 0.5594 0.0524 0.0241 0.396 6.246 4.272 295.579 0.706 19.001 6.555 0.32 192241. 0.3975 20.96 0.2767 0.5828 0.0495 0.0235 0.387 6.101 4.036 288.721 0.689 17.954 6.341 0.32 192446. 0.3738 22.46 0.2965 0.6034 0.0465 0.0229 0.377 5.936 3.795 280.918 0.671 16.880 6.127 0.32 192661. 0.3502 23.96 0.3163 0.6210 0.0435 0.0221 0.365 5.750 3.547 272.135 0.650 15.779 5.913 0.32 192884. 0.3267 25.46 0.3360 0.6357 0.0404 0.0213 0.352 5.543 3.294 262.340 0.626 14.654 5.696 0.32 193117. 0.3033 26.95 0.3558 0.6470 0.0372 0.0205 0.337 5.314 3.036 251.503 0.600 13.505 5.476 0.32 193360. 0.2799 28.45 0.3756 0.6547 0.0340 0.0195 0.321 5.063 2.773 239.595 0.572 12.334 5.249 0.32 193612. 0.2564 29.95 0.3953 0.6583 0.0307 0.0184 0.304 4.788 2.505 226.595 0.541 11.141 5.014 0.32 193874. 0.2328 31.45 0.4151 0.6570 0.0274 0.0173 0.285 4.490 2.232 212.483 0.507 9.930 4.766 0.32 194146. 0.2089 32.94 0.4349 0.6497 0.0240 0.0160 0.265 4.168 1.956 197.243 0.471 8.702 4.499 0.32 194427. 0.1846 34.44 0.4546 0.6349 0.0206 0.0147 0.243 3.822 1.677 180.868 0.432 7.458 4.205 0.32 194719. 0.1597 35.94 0.4744 0.6099 0.0171 0.0133 0.219 3.452 1.394 163.355 0.390 6.201 3.871 0.32 195021. 0.1341 37.44 0.4942 0.5706 0.0136 0.0118 0.194 3.058 1.109 144.713 0.345 4.934 3.477 0.32 195333. 0.1074 38.93 0.5139 0.5097 0.0101 0.0102 0.168 2.640 0.823 124.957 0.298 3.660 2.986 0.32 195654. 0.0795 40.43 0.5337 0.4134 0.0066 0.0085 0.140 2.200 0.535 104.109 0.249 2.381 2.332 0.32 195985. 0.0501 41.93 0.5535 0.2510 0.0030 0.0067 0.110 1.736 0.247 82.174 0.196 1.100 1.365 0.32 196320. 0.0199 43.43 0.5732 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 0.0827 0.0255 0.821 10.346 10.543 612.017 1.169 46.894 7.813 0.40 237884. 0.7443 1.88 0.0198 0.0626 0.0810 0.0257 0.826 10.410 10.323 615.796 1.176 45.916 7.603 0.40 238015. 0.7167 3.76 0.0397 0.1218 0.0792 0.0258 0.830 10.460 10.091 618.766 1.182 44.883 7.397 0.40 238154. 0.6893 5.63 0.0595 0.1776 0.0772 0.0259 0.833 10.495 9.846 620.816 1.186 43.794 7.193 0.40 238302. 0.6622 7.51 0.0793 0.2303 0.0752 0.0259 0.834 10.512 9.589 621.846 1.188 42.650 6.994 0.40 238459. 0.6354 9.39 0.0991 0.2798 0.0731 0.0259 0.834 10.511 9.319 621.760 1.187 41.449 6.798 0.40 238624. 0.6088 11.27 0.1190 0.3262 0.0709 0.0258 0.832 10.489 9.036 620.469 1.185 40.193 6.606 0.40 238799. 0.5826 13.14 0.1388 0.3697 0.0686 0.0257 0.829 10.445 8.741 617.890 1.180 38.882 6.417 0.40 238984. 0.5566 15.02 0.1586 0.4104 0.0662 0.0256 0.823 10.378 8.435 613.944 1.173 37.518 6.231 0.40 239178. 0.5310 16.90 0.1785 0.4482 0.0637 0.0254 0.816 10.287 8.116 608.553 1.162 36.101 6.049 0.40 239383. 0.5056 18.78 0.1983 0.4832 0.0611 0.0251 0.807 10.170 7.786 601.640 1.149 34.634 5.870 0.40 239598. 0.4806 20.65 0.2181 0.5155 0.0584 0.0247 0.795 10.027 7.445 593.128 1.133 33.117 5.693 0.40 239823. 0.4558 22.53 0.2379 0.5452 0.0556 0.0243 0.782 9.854 7.093 582.941 1.113 31.551 5.519 0.40 240059. 0.4313 24.41 0.2578 0.5721 0.0528 0.0238 0.766 9.653 6.731 571.004 1.091 29.940 5.347 0.40 240307. 0.4070 26.29 0.2776 0.5964 0.0499 0.0232 0.747 9.420 6.359 557.245 1.064 28.283 5.176 0.40 240565. 0.3829 28.16 0.2974 0.6180 0.0469 0.0226 0.726 9.155 5.976 541.594 1.034 26.582 5.005 0.40 240835. 0.3590 30.04 0.3172 0.6367 0.0438 0.0218 0.703 8.858 5.585 523.981 1.001 24.841 4.834 0.40 241116. 0.3352 31.92 0.3371 0.6524 0.0407 0.0210 0.676 8.526 5.184 504.344 0.963 23.060 4.662 0.40 241409. 0.3114 33.80 0.3569 0.6650 0.0375 0.0201 0.647 8.158 4.775 482.622 0.922 21.241 4.488 0.40 241714. 0.2877 35.68 0.3767 0.6739 0.0342 0.0191 0.615 7.755 4.359 458.761 0.876 19.387 4.309 0.40 242032. 0.2639 37.55 0.3966 0.6789 0.0309 0.0180 0.580 7.315 3.934 432.715 0.826 17.500 4.124 0.40 242361. 0.2400 39.43 0.4164 0.6791 0.0275 0.0168 0.542 6.837 3.503 404.444 0.772 15.582 3.929 0.40 242703. 0.2157 41.31 0.4362 0.6735 0.0241 0.0156 0.501 6.321 3.066 373.921 0.714 13.637 3.719 0.40 243057. 0.1910 43.19 0.4560 0.6604 0.0206 0.0142 0.457 5.767 2.623 341.128 0.652 11.668 3.488 0.40 243424. 0.1657 45.06 0.4759 0.6371 0.0171 0.0128 0.410 5.174 2.176 306.065 0.585 9.679 3.225 0.40 243804. 0.1396 46.94 0.4957 0.5992 0.0135 0.0112 0.360 4.543 1.725 268.747 0.513 7.674 2.912 0.40 244196. 0.1122 48.82 0.5155 0.5386 0.0100 0.0095 0.307 3.875 1.272 229.207 0.438 5.657 2.517 0.40 244600. 0.0833 50.70 0.5354 0.4393 0.0064 0.0078 0.251 3.169 0.817 187.493 0.358 3.634 1.976 0.40 245016. 0.0524 52.57 0.5552 0.2630 0.0028 0.0060 0.193 2.427 0.361 143.597 0.274 1.607 1.141 0.40 245436. 0.0201 54.45 0.5750 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 0.0837 0.0255 1.420 14.917 15.365 1058.893 1.685 68.342 6.581 0.48 285439. 0.7568 2.24 0.0197 0.0629 0.0820 0.0257 1.429 15.009 15.047 1065.463 1.696 66.930 6.406 0.48 285596. 0.7290 4.48 0.0394 0.1224 0.0801 0.0258 1.436 15.082 14.712 1070.620 1.704 65.438 6.233 0.48 285764. 0.7014 6.72 0.0591 0.1786 0.0782 0.0259 1.440 15.132 14.359 1074.168 1.710 63.867 6.063 0.48 285941. 0.6740 8.96 0.0789 0.2316 0.0762 0.0259 1.443 15.157 13.987 1075.935 1.712 62.215 5.896 0.48 286129. 0.6470 11.20 0.0986 0.2815 0.0741 0.0259 1.443 15.154 13.597 1075.753 1.712 60.481 5.733 0.48 286327. 0.6202 13.44 0.1183 0.3284 0.0719 0.0259 1.440 15.122 13.190 1073.467 1.708 58.667 5.573 0.48 286537. 0.5938 15.68 0.1380 0.3724 0.0695 0.0258 1.433 15.058 12.764 1068.938 1.701 56.774 5.416 0.48 286758. 0.5677 17.92 0.1577 0.4135 0.0671 0.0256 1.424 14.961 12.321 1062.028 1.690 54.804 5.262 0.48 286990. 0.5419 20.16 0.1774 0.4518 0.0646 0.0254 1.412 14.828 11.861 1052.605 1.675 52.757 5.111 0.48 287235. 0.5164 22.40 0.1972 0.4874 0.0620 0.0251 1.395 14.658 11.384 1040.534 1.656 50.637 4.962 0.48 287491. 0.4912 24.64 0.2169 0.5204 0.0593 0.0247 1.375 14.449 10.892 1025.688 1.632 48.446 4.816 0.48 287761. 0.4663 26.88 0.2366 0.5507 0.0566 0.0243 1.352 14.199 10.383 1007.936 1.604 46.184 4.672 0.48 288042. 0.4417 29.12 0.2563 0.5784 0.0537 0.0238 1.324 13.906 9.860 987.151 1.571 43.856 4.530 0.48 288337. 0.4173 31.37 0.2760 0.6036 0.0508 0.0232 1.292 13.569 9.321 963.207 1.533 41.462 4.389 0.48 288646. 0.3932 33.61 0.2957 0.6260 0.0478 0.0226 1.255 13.185 8.769 935.984 1.490 39.005 4.249 0.48 288967. 0.3692 35.85 0.3154 0.6458 0.0447 0.0218 1.214 12.754 8.203 905.365 1.441 36.488 4.110 0.48 289302. 0.3453 38.09 0.3352 0.6628 0.0415 0.0210 1.168 12.273 7.625 871.240 1.387 33.914 3.969 0.48 289652. 0.3216 40.33 0.3549 0.6767 0.0383 0.0201 1.118 11.742 7.034 833.504 1.327 31.285 3.827 0.48 290015. 0.2978 42.57 0.3746 0.6872 0.0350 0.0191 1.062 11.158 6.431 792.066 1.261 28.605 3.683 0.48 290393. 0.2740 44.81 0.3943 0.6940 0.0317 0.0180 1.002 10.521 5.818 746.842 1.189 25.877 3.533 0.48 290785. 0.2500 47.05 0.4140 0.6964 0.0283 0.0168 0.936 9.829 5.194 697.763 1.111 23.104 3.376 0.48 291192. 0.2258 49.29 0.4337 0.6934 0.0249 0.0155 0.865 9.083 4.562 644.780 1.026 20.291 3.209 0.48 291613. 0.2011 51.53 0.4534 0.6835 0.0214 0.0142 0.788 8.281 3.921 587.860 0.936 17.442 3.026 0.48 292049. 0.1758 53.77 0.4732 0.6642 0.0178 0.0127 0.707 7.424 3.274 526.997 0.839 14.563 2.818 0.48 292501. 0.1496 56.01 0.4929 0.6316 0.0143 0.0111 0.620 6.511 2.621 462.215 0.736 11.660 2.572 0.48 292966. 0.1222 58.25 0.5126 0.5782 0.0107 0.0095 0.528 5.544 1.965 393.566 0.626 8.738 2.264 0.48 293447. 0.0931 60.49 0.5323 0.4889 0.0071 0.0077 0.431 4.524 1.305 321.133 0.511 5.806 1.844 0.48 293941. 0.0618 62.73 0.5520 0.3285 0.0035 0.0059 0.328 3.451 0.645 244.944 0.390 2.869 1.194 0.48 294443. 0.0281 64.97 0.5717 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 0.0849 0.0258 2.276 20.489 21.223 1696.900 2.315 94.400 5.673 0.56 332980. 0.7667 2.61 0.0197 0.0632 0.0832 0.0259 2.290 20.616 20.787 1707.403 2.329 92.460 5.522 0.56 333165. 0.7386 5.23 0.0394 0.1231 0.0814 0.0260 2.301 20.715 20.326 1715.594 2.340 90.410 5.374 0.56 333362. 0.7108 7.84 0.0591 0.1797 0.0794 0.0261 2.308 20.782 19.840 1721.158 2.348 88.248 5.228 0.56 333570. 0.6832 10.45 0.0788 0.2330 0.0774 0.0262 2.312 20.814 19.329 1723.812 2.352 85.975 5.086 0.56 333791. 0.6560 13.06 0.0985 0.2833 0.0752 0.0262 2.311 20.808 18.792 1723.285 2.351 83.588 4.946 0.56 334024. 0.6291 15.68 0.1182 0.3305 0.0730 0.0261 2.306 20.760 18.231 1719.326 2.345 81.090 4.809 0.56 334270. 0.6025 18.29 0.1379 0.3749 0.0706 0.0260 2.295 20.668 17.644 1711.713 2.335 78.482 4.675 0.56 334529. 0.5762 20.90 0.1577 0.4164 0.0682 0.0258 2.280 20.530 17.034 1700.223 2.319 75.766 4.544 0.56 334802. 0.5502 23.51 0.1774 0.4552 0.0656 0.0256 2.259 20.342 16.400 1684.648 2.298 72.946 4.415 0.56 335088. 0.5246 26.13 0.1971 0.4913 0.0630 0.0253 2.233 20.102 15.743 1664.781 2.271 70.023 4.289 0.56 335389. 0.4993 28.74 0.2168 0.5247 0.0603 0.0249 2.200 19.807 15.063 1640.415 2.238 67.001 4.165 0.56 335704. 0.4742 31.35 0.2365 0.5557 0.0575 0.0245 2.161 19.456 14.362 1611.341 2.198 63.883 4.043 0.56 336035. 0.4495 33.96 0.2562 0.5840 0.0546 0.0239 2.115 19.046 13.640 1577.363 2.152 60.671 3.922 0.56 336380. 0.4250 36.58 0.2759 0.6098 0.0516 0.0234 2.063 18.574 12.898 1538.276 2.098 57.369 3.803 0.56 336740. 0.4007 39.19 0.2956 0.6330 0.0486 0.0227 2.003 18.038 12.136 1493.892 2.038 53.980 3.685 0.56 337116. 0.3766 41.80 0.3153 0.6536 0.0454 0.0219 1.936 17.436 11.355 1444.021 1.970 50.508 3.567 0.56 337509. 0.3526 44.42 0.3350 0.6715 0.0423 0.0211 1.862 16.765 10.557 1388.489 1.894 46.956 3.448 0.56 337917. 0.3287 47.03 0.3547 0.6864 0.0390 0.0201 1.780 16.025 9.741 1327.132 1.810 43.328 3.329 0.56 338342. 0.3048 49.64 0.3744 0.6981 0.0357 0.0191 1.689 15.212 8.909 1259.800 1.719 39.629 3.208 0.56 338783. 0.2809 52.25 0.3941 0.7061 0.0323 0.0180 1.591 14.325 8.063 1186.360 1.618 35.863 3.083 0.56 339241. 0.2568 54.87 0.4138 0.7100 0.0288 0.0168 1.484 13.363 7.202 1106.700 1.510 32.035 2.952 0.56 339716. 0.2324 57.48 0.4336 0.7086 0.0253 0.0155 1.369 12.325 6.329 1020.742 1.392 28.151 2.812 0.56 340208. 0.2076 60.09 0.4533 0.7007 0.0218 0.0141 1.245 11.210 5.444 928.432 1.267 24.217 2.660 0.56 340717. 0.1821 62.70 0.4730 0.6837 0.0182 0.0126 1.113 10.019 4.550 829.760 1.132 20.240 2.487 0.56 341243. 0.1557 65.32 0.4927 0.6538 0.0146 0.0110 0.972 8.751 3.649 724.765 0.989 16.229 2.283 0.56 341787. 0.1280 67.93 0.5124 0.6035 0.0110 0.0093 0.823 7.408 2.741 613.530 0.837 12.192 2.026 0.56 342348. 0.0984 70.54 0.5321 0.5173 0.0073 0.0075 0.665 5.991 1.830 496.189 0.677 8.140 1.673 0.56 342924. 0.0664 73.15 0.5518 0.3579 0.0037 0.0057 0.500 4.501 0.917 372.797 0.509 4.080 1.116 0.56 343510. 0.0314 75.77 0.5715 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 0.0865 0.0262 3.454 27.212 28.222 2575.572 3.074 125.530 4.970 0.63 380503. 0.7746 2.99 0.0197 0.0635 0.0847 0.0264 3.475 27.378 27.644 2591.349 3.093 122.962 4.839 0.63 380717. 0.7464 5.98 0.0395 0.1235 0.0828 0.0265 3.491 27.507 27.033 2603.519 3.108 120.245 4.710 0.63 380944. 0.7184 8.97 0.0592 0.1803 0.0809 0.0266 3.502 27.592 26.389 2611.611 3.117 117.379 4.583 0.63 381185. 0.6907 11.97 0.0790 0.2339 0.0788 0.0266 3.507 27.630 25.711 2615.177 3.122 114.361 4.459 0.63 381440. 0.6634 14.96 0.0987 0.2844 0.0766 0.0266 3.505 27.616 24.998 2613.810 3.120 111.192 4.338 0.63 381709. 0.6363 17.95 0.1185 0.3320 0.0743 0.0265 3.496 27.545 24.252 2607.121 3.112 107.872 4.219 0.64 381993. 0.6096 20.94 0.1382 0.3767 0.0719 0.0264 3.480 27.415 23.472 2594.767 3.097 104.405 4.103 0.64 382292. 0.5832 23.93 0.1579 0.4185 0.0694 0.0262 3.455 27.221 22.660 2576.424 3.075 100.793 3.989 0.64 382607. 0.5571 26.92 0.1777 0.4577 0.0669 0.0260 3.422 26.960 21.816 2551.784 3.046 97.039 3.878 0.64 382938. 0.5314 29.91 0.1974 0.4942 0.0642 0.0256 3.380 26.630 20.942 2520.527 3.009 93.149 3.768 0.64 383285. 0.5060 32.91 0.2172 0.5282 0.0614 0.0252 3.329 26.227 20.037 2482.348 2.963 89.126 3.661 0.64 383648. 0.4808 35.90 0.2369 0.5596 0.0585 0.0248 3.268 25.747 19.104 2436.943 2.909 84.973 3.556 0.64 384028. 0.4559 38.89 0.2567 0.5885 0.0556 0.0242 3.197 25.188 18.142 2384.010 2.846 80.696 3.452 0.64 384426. 0.4313 41.88 0.2764 0.6149 0.0526 0.0236 3.116 24.546 17.153 2323.250 2.773 76.297 3.349 0.64 384841. 0.4069 44.87 0.2962 0.6387 0.0495 0.0229 3.023 23.818 16.138 2254.375 2.691 71.782 3.247 0.64 385274. 0.3827 47.86 0.3159 0.6600 0.0463 0.0221 2.920 23.002 15.098 2177.104 2.599 67.156 3.145 0.64 385726. 0.3586 50.85 0.3356 0.6786 0.0430 0.0213 2.804 22.094 14.034 2091.174 2.496 62.422 3.044 0.64 386195. 0.3345 53.85 0.3554 0.6944 0.0397 0.0203 2.677 21.092 12.947 1996.337 2.383 57.587 2.942 0.64 386684. 0.3105 56.84 0.3751 0.7070 0.0363 0.0192 2.538 19.993 11.838 1892.367 2.259 52.656 2.837 0.64 387191. 0.2864 59.83 0.3949 0.7161 0.0328 0.0181 2.386 18.796 10.709 1779.068 2.124 47.635 2.730 0.64 387717. 0.2621 62.82 0.4146 0.7211 0.0293 0.0168 2.221 17.499 9.562 1656.272 1.977 42.531 2.618 0.64 388263. 0.2376 65.81 0.4344 0.7211 0.0257 0.0155 2.044 16.100 8.397 1523.855 1.819 37.351 2.499 0.64 388828. 0.2125 68.80 0.4541 0.7146 0.0221 0.0141 1.853 14.599 7.218 1381.744 1.649 32.104 2.369 0.64 389413. 0.1867 71.79 0.4738 0.6993 0.0185 0.0125 1.649 12.995 6.025 1229.924 1.468 26.798 2.222 0.64 390017. 0.1600 74.79 0.4936 0.6711 0.0148 0.0109 1.433 11.289 4.822 1068.452 1.275 21.446 2.047 0.64 390641. 0.1319 77.78 0.5133 0.6222 0.0111 0.0091 1.204 9.482 3.611 897.470 1.071 16.060 1.825 0.64 391284. 0.1017 80.77 0.5331 0.5363 0.0073 0.0073 0.962 7.577 2.395 717.180 0.856 10.653 1.515 0.64 391945. 0.0688 83.76 0.5528 0.3714 0.0036 0.0054 0.708 5.575 1.176 527.651 0.630 5.233 1.011 0.64 392616. 0.0322 86.75 0.5726 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 0.0884 0.0269 5.045 35.333 36.507 3762.266 3.992 162.382 4.401 0.71 428000. 0.7802 3.37 0.0198 0.0634 0.0866 0.0270 5.074 35.537 35.765 3784.042 4.015 159.081 4.287 0.71 428244. 0.7521 6.75 0.0396 0.1235 0.0847 0.0271 5.097 35.693 34.978 3800.578 4.033 155.584 4.174 0.71 428503. 0.7243 10.12 0.0594 0.1803 0.0827 0.0272 5.111 35.792 34.148 3811.165 4.044 151.891 4.064 0.71 428778. 0.6967 13.49 0.0792 0.2340 0.0806 0.0273 5.116 35.829 33.273 3815.119 4.048 147.999 3.956 0.71 429069. 0.6694 16.87 0.0990 0.2847 0.0783 0.0272 5.112 35.798 32.353 3811.803 4.044 143.907 3.850 0.71 429376. 0.6424 20.24 0.1187 0.3324 0.0760 0.0272 5.097 35.693 31.388 3800.620 4.033 139.616 3.746 0.71 429699. 0.6157 23.61 0.1385 0.3773 0.0736 0.0270 5.070 35.509 30.380 3781.049 4.012 135.131 3.644 0.71 430040. 0.5893 26.99 0.1583 0.4194 0.0710 0.0268 5.032 35.242 29.329 3752.600 3.982 130.456 3.545 0.71 430399. 0.5632 30.36 0.1781 0.4589 0.0684 0.0265 4.982 34.887 28.236 3714.813 3.942 125.595 3.448 0.72 430775. 0.5375 33.74 0.1979 0.4958 0.0656 0.0262 4.918 34.440 27.103 3667.245 3.891 120.555 3.352 0.72 431170. 0.5120 37.11 0.2177 0.5301 0.0628 0.0258 4.840 33.898 25.931 3609.471 3.830 115.341 3.259 0.72 431584. 0.4868 40.48 0.2375 0.5620 0.0599 0.0253 4.749 33.255 24.721 3541.054 3.757 109.959 3.166 0.72 432016. 0.4619 43.86 0.2573 0.5914 0.0568 0.0247 4.642 32.509 23.474 3461.570 3.673 104.412 3.076 0.72 432468. 0.4372 47.23 0.2771 0.6183 0.0537 0.0241 4.520 31.655 22.192 3370.596 3.576 98.709 2.986 0.72 432940. 0.4127 50.60 0.2969 0.6428 0.0505 0.0233 4.382 30.688 20.875 3267.712 3.467 92.853 2.898 0.72 433431. 0.3884 53.98 0.3167 0.6648 0.0473 0.0225 4.228 29.606 19.526 3152.511 3.345 86.851 2.809 0.72 433944. 0.3642 57.35 0.3365 0.6841 0.0439 0.0216 4.056 28.405 18.145 3024.623 3.209 80.709 2.721 0.72 434476. 0.3400 60.72 0.3562 0.7007 0.0405 0.0206 3.867 27.082 16.734 2883.686 3.060 74.434 2.632 0.72 435030. 0.3159 64.10 0.3760 0.7142 0.0370 0.0195 3.660 25.633 15.295 2729.383 2.896 68.033 2.542 0.72 435605. 0.2916 67.47 0.3958 0.7244 0.0335 0.0183 3.435 24.055 13.830 2561.427 2.718 61.515 2.449 0.72 436202. 0.2672 70.84 0.4156 0.7305 0.0299 0.0170 3.191 22.348 12.340 2379.586 2.525 54.887 2.352 0.72 436820. 0.2424 74.22 0.4354 0.7317 0.0262 0.0156 2.928 20.508 10.827 2183.679 2.317 48.159 2.249 0.72 437460. 0.2171 77.59 0.4552 0.7266 0.0225 0.0141 2.647 18.535 9.295 1973.613 2.094 41.342 2.136 0.72 438122. 0.1911 80.97 0.4750 0.7127 0.0188 0.0125 2.346 16.429 7.745 1749.407 1.856 34.449 2.008 0.72 438806. 0.1639 84.34 0.4948 0.6859 0.0150 0.0108 2.027 14.193 6.181 1511.243 1.603 27.494 1.855 0.72 439512. 0.1353 87.71 0.5146 0.6380 0.0112 0.0090 1.689 11.828 4.607 1259.458 1.336 20.492 1.659 0.72 440239. 0.1045 91.09 0.5344 0.5512 0.0073 0.0071 1.334 9.340 3.026 994.539 1.055 13.462 1.380 0.72 440986. 0.0704 94.46 0.5542 0.3778 0.0035 0.0051 0.961 6.731 1.442 716.753 0.760 6.413 0.912 0.73 441743. 0.0321 97.83 0.5740 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 0.0908 0.0285 7.332 46.212 46.282 5467.403 5.221 205.860 3.839 0.79 475460. 0.7663 3.74 0.0197 0.0615 0.0890 0.0285 7.350 46.327 45.356 5481.029 5.234 201.745 3.753 0.79 475734. 0.7416 7.47 0.0395 0.1202 0.0870 0.0286 7.360 46.386 44.375 5488.068 5.241 197.379 3.667 0.79 476026. 0.7167 11.21 0.0592 0.1760 0.0850 0.0286 7.359 46.383 43.337 5487.638 5.240 192.762 3.582 0.79 476334. 0.6918 14.95 0.0789 0.2291 0.0828 0.0285 7.347 46.309 42.241 5478.857 5.232 187.890 3.497 0.79 476660. 0.6668 18.68 0.0986 0.2795 0.0806 0.0284 7.323 46.157 41.088 5460.872 5.215 182.760 3.413 0.79 477005. 0.6418 22.42 0.1184 0.3272 0.0782 0.0283 7.286 45.920 39.877 5432.915 5.188 177.374 3.329 0.79 477368. 0.6168 26.16 0.1381 0.3723 0.0757 0.0281 7.234 45.593 38.610 5394.247 5.151 171.738 3.247 0.79 477750. 0.5918 29.89 0.1578 0.4147 0.0731 0.0278 7.167 45.171 37.288 5344.206 5.103 165.858 3.165 0.79 478151. 0.5670 33.63 0.1776 0.4547 0.0704 0.0275 7.083 44.646 35.913 5282.123 5.044 159.741 3.084 0.79 478572. 0.5422 37.37 0.1973 0.4921 0.0676 0.0271 6.983 44.014 34.486 5207.319 4.973 153.394 3.004 0.79 479013. 0.5175 41.10 0.2170 0.5270 0.0647 0.0267 6.865 43.268 33.009 5119.120 4.888 146.824 2.925 0.80 479475. 0.4930 44.84 0.2368 0.5595 0.0617 0.0261 6.728 42.403 31.483 5016.834 4.791 140.038 2.846 0.80 479957. 0.4686 48.58 0.2565 0.5897 0.0587 0.0255 6.571 41.414 29.911 4899.745 4.679 133.044 2.769 0.80 480461. 0.4443 52.31 0.2762 0.6174 0.0555 0.0248 6.393 40.293 28.293 4767.178 4.552 125.848 2.692 0.80 480987. 0.4201 56.05 0.2959 0.6427 0.0522 0.0241 6.193 39.036 26.632 4618.472 4.410 118.460 2.615 0.80 481534. 0.3960 59.79 0.3157 0.6655 0.0489 0.0232 5.972 37.637 24.929 4452.955 4.252 110.885 2.539 0.80 482104. 0.3720 63.52 0.3354 0.6859 0.0455 0.0222 5.726 36.093 23.186 4270.171 4.078 103.131 2.463 0.80 482696. 0.3479 67.26 0.3551 0.7034 0.0420 0.0212 5.458 34.401 21.404 4069.992 3.887 95.207 2.385 0.80 483311. 0.3238 71.00 0.3749 0.7179 0.0384 0.0201 5.165 32.556 19.586 3851.749 3.678 87.121 2.306 0.80 483950. 0.2995 74.73 0.3946 0.7290 0.0348 0.0188 4.848 30.557 17.734 3615.252 3.452 78.882 2.225 0.80 484612. 0.2749 78.47 0.4143 0.7359 0.0311 0.0175 4.507 28.405 15.850 3360.598 3.209 70.501 2.139 0.80 485297. 0.2499 82.21 0.4341 0.7378 0.0273 0.0161 4.141 26.100 13.937 3087.884 2.949 61.990 2.047 0.80 486007. 0.2242 85.94 0.4538 0.7329 0.0235 0.0146 3.751 23.645 11.997 2797.474 2.671 53.362 1.945 0.80 486740. 0.1977 89.68 0.4735 0.7186 0.0197 0.0130 3.339 21.046 10.034 2489.988 2.378 44.631 1.828 0.80 487498. 0.1699 93.42 0.4932 0.6904 0.0158 0.0113 2.905 18.309 8.052 2166.202 2.069 35.814 1.686 0.80 488279. 0.1403 97.15 0.5130 0.6401 0.0119 0.0095 2.450 15.444 6.054 1827.184 1.745 26.930 1.503 0.80 489084. 0.1085 100.89 0.5327 0.5507 0.0079 0.0077 1.977 12.461 4.047 1474.237 1.408 18.001 1.245 0.80 489911. 0.0735 104.63 0.5524 0.3816 0.0040 0.0058 1.486 9.369 2.033 1108.416 1.058 9.042 0.832 0.81 490751. 0.0348 108.36 0.5722 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 0.0935 0.0331 11.346 65.011 57.713 8460.778 7.345 256.706 3.094 0.87 522875. 0.6896 4.12 0.0198 0.0551 0.0917 0.0329 11.288 64.676 56.587 8417.130 7.307 251.698 3.049 0.87 523182. 0.6730 8.24 0.0396 0.1086 0.0898 0.0327 11.216 64.266 55.388 8363.785 7.261 246.365 3.004 0.87 523508. 0.6558 12.37 0.0594 0.1603 0.0877 0.0325 11.131 63.778 54.116 8300.241 7.206 240.706 2.957 0.87 523854. 0.6382 16.49 0.0792 0.2103 0.0855 0.0322 11.031 63.206 52.769 8225.866 7.141 234.718 2.910 0.87 524219. 0.6201 20.61 0.0989 0.2585 0.0832 0.0318 10.916 62.546 51.348 8139.952 7.066 228.396 2.861 0.87 524605. 0.6015 24.73 0.1187 0.3049 0.0808 0.0315 10.784 61.792 49.852 8041.854 6.981 221.744 2.812 0.87 525012. 0.5824 28.86 0.1385 0.3493 0.0783 0.0310 10.636 60.940 48.284 7930.964 6.885 214.767 2.761 0.87 525439. 0.5629 32.98 0.1583 0.3918 0.0756 0.0305 10.469 59.985 46.644 7806.682 6.777 207.475 2.710 0.87 525889. 0.5430 37.10 0.1781 0.4323 0.0728 0.0300 10.283 58.923 44.936 7668.361 6.657 199.875 2.658 0.87 526360. 0.5227 41.22 0.1979 0.4708 0.0700 0.0294 10.078 57.746 43.160 7515.248 6.524 191.977 2.605 0.87 526853. 0.5021 45.35 0.2177 0.5072 0.0670 0.0287 9.852 56.450 41.320 7346.534 6.378 183.790 2.551 0.87 527369. 0.4811 49.47 0.2375 0.5414 0.0639 0.0280 9.604 55.028 39.416 7161.485 6.217 175.325 2.496 0.88 527908. 0.4598 53.59 0.2572 0.5735 0.0607 0.0272 9.333 53.475 37.453 6959.333 6.042 166.590 2.441 0.88 528471. 0.4383 57.71 0.2770 0.6033 0.0574 0.0264 9.038 51.784 35.431 6739.293 5.851 157.597 2.385 0.88 529057. 0.4164 61.84 0.2968 0.6309 0.0541 0.0254 8.717 49.949 33.353 6500.485 5.643 148.355 2.327 0.88 529668. 0.3943 65.96 0.3166 0.6560 0.0506 0.0244 8.371 47.963 31.222 6242.015 5.419 138.877 2.269 0.88 530302. 0.3719 70.08 0.3364 0.6787 0.0471 0.0233 7.996 45.818 29.040 5962.943 5.177 129.171 2.209 0.88 530962. 0.3492 74.20 0.3562 0.6980 0.0435 0.0222 7.600 43.546 26.809 5667.187 4.920 119.247 2.146 0.88 531647. 0.3259 78.33 0.3760 0.7105 0.0398 0.0210 7.211 41.316 24.528 5377.030 4.668 109.102 2.069 0.88 532357. 0.3006 82.45 0.3958 0.7181 0.0360 0.0198 6.798 38.951 22.204 5069.174 4.401 98.762 1.987 0.88 533093. 0.2746 86.57 0.4155 0.7200 0.0322 0.0186 6.360 36.442 19.838 4742.688 4.117 88.238 1.897 0.88 533854. 0.2479 90.69 0.4353 0.7146 0.0283 0.0172 5.900 33.807 17.434 4399.739 3.819 77.545 1.797 0.88 534642. 0.2202 94.82 0.4551 0.6996 0.0243 0.0158 5.419 31.049 14.995 4040.833 3.508 66.699 1.683 0.88 535455. 0.1912 98.94 0.4749 0.6719 0.0203 0.0144 4.919 28.183 12.527 3667.843 3.184 55.719 1.549 0.88 536296. 0.1609 103.06 0.4947 0.6262 0.0163 0.0128 4.403 25.229 10.033 3283.391 2.850 44.628 1.386 0.88 537162. 0.1288 107.18 0.5145 0.5547 0.0122 0.0113 3.875 22.203 7.521 2889.547 2.508 33.454 1.181 0.88 538054. 0.0950 111.31 0.5343 0.4443 0.0081 0.0097 3.338 19.124 4.997 2488.890 2.161 22.225 0.911 0.89 538969. 0.0597 115.43 0.5541 0.2715 0.0040 0.0082 2.794 16.007 2.465 2083.151 1.808 10.962 0.537 0.89 539899. 0.0247 119.55 0.5739