20x11E (20x11E.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 0.0874 0.0331 0.009 0.537 0.446 6.357 0.061 1.983 31.812 0.08 36675. 0.6232 0.45 0.0240 0.0617 0.0861 0.0335 0.009 0.544 0.439 6.433 0.061 1.953 30.958 0.08 36698. 0.6018 0.91 0.0480 0.1200 0.0847 0.0339 0.009 0.550 0.432 6.505 0.062 1.921 30.107 0.08 36723. 0.5804 1.36 0.0720 0.1750 0.0831 0.0342 0.009 0.555 0.424 6.570 0.063 1.885 29.263 0.08 36751. 0.5589 1.82 0.0960 0.2266 0.0815 0.0345 0.009 0.560 0.415 6.627 0.063 1.847 28.426 0.08 36780. 0.5375 2.27 0.1200 0.2750 0.0797 0.0348 0.009 0.564 0.406 6.675 0.064 1.807 27.598 0.08 36812. 0.5160 2.73 0.1440 0.3203 0.0777 0.0350 0.009 0.567 0.396 6.712 0.064 1.763 26.781 0.08 36847. 0.4946 3.18 0.1680 0.3624 0.0756 0.0351 0.009 0.569 0.386 6.735 0.064 1.716 25.975 0.08 36884. 0.4733 3.64 0.1920 0.4015 0.0734 0.0351 0.009 0.570 0.374 6.744 0.064 1.665 25.181 0.08 36923. 0.4520 4.09 0.2160 0.4376 0.0711 0.0351 0.009 0.569 0.362 6.736 0.064 1.612 24.397 0.08 36965. 0.4308 4.55 0.2400 0.4709 0.0685 0.0349 0.009 0.567 0.349 6.709 0.064 1.554 23.624 0.08 37010. 0.4097 5.00 0.2641 0.5012 0.0659 0.0347 0.009 0.563 0.336 6.663 0.064 1.494 22.860 0.08 37058. 0.3887 5.46 0.2881 0.5286 0.0630 0.0343 0.009 0.557 0.321 6.595 0.063 1.429 22.103 0.08 37108. 0.3676 5.91 0.3121 0.5532 0.0600 0.0339 0.009 0.550 0.306 6.503 0.062 1.361 21.349 0.08 37161. 0.3465 6.36 0.3361 0.5747 0.0569 0.0333 0.009 0.540 0.290 6.386 0.061 1.290 20.597 0.08 37217. 0.3254 6.82 0.3601 0.5932 0.0536 0.0325 0.008 0.528 0.273 6.244 0.060 1.215 19.840 0.08 37276. 0.3042 7.27 0.3841 0.6083 0.0501 0.0317 0.008 0.514 0.256 6.078 0.058 1.137 19.075 0.08 37338. 0.2829 7.73 0.4081 0.6198 0.0466 0.0307 0.008 0.498 0.237 5.888 0.056 1.056 18.293 0.08 37403. 0.2615 8.18 0.4321 0.6274 0.0429 0.0296 0.008 0.480 0.219 5.675 0.054 0.973 17.489 0.08 37470. 0.2400 8.64 0.4561 0.6306 0.0392 0.0283 0.007 0.460 0.200 5.439 0.052 0.888 16.652 0.08 37541. 0.2183 9.09 0.4801 0.6287 0.0353 0.0270 0.007 0.438 0.180 5.181 0.049 0.801 15.771 0.08 37614. 0.1964 9.55 0.5041 0.6208 0.0314 0.0255 0.007 0.414 0.160 4.902 0.047 0.713 14.832 0.08 37691. 0.1742 10.00 0.5281 0.6058 0.0275 0.0240 0.006 0.389 0.140 4.602 0.044 0.624 13.815 0.08 37770. 0.1518 10.46 0.5521 0.5820 0.0235 0.0223 0.006 0.362 0.120 4.283 0.041 0.533 12.695 0.08 37853. 0.1289 10.91 0.5761 0.5470 0.0195 0.0205 0.005 0.333 0.099 3.945 0.038 0.442 11.435 0.08 37938. 0.1058 11.37 0.6001 0.4975 0.0155 0.0187 0.005 0.303 0.079 3.589 0.034 0.351 9.985 0.08 38026. 0.0824 11.82 0.6241 0.4285 0.0115 0.0168 0.004 0.272 0.059 3.219 0.031 0.261 8.268 0.08 38118. 0.0588 12.28 0.6481 0.3318 0.0076 0.0148 0.004 0.240 0.039 2.835 0.027 0.171 6.165 0.08 38212. 0.0355 12.73 0.6721 0.1941 0.0037 0.0127 0.003 0.206 0.019 2.440 0.023 0.083 3.478 0.08 38310. 0.0140 13.18 0.6961 -0.0090 -0.0001 0.0106 0.003 0.172 -0.001 2.036 0.019 -0.003 -0.157 0.08 38409. 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 0.0878 0.0307 0.063 1.994 1.790 47.174 0.225 7.964 17.215 0.16 73348. 0.6758 0.91 0.0241 0.0669 0.0865 0.0311 0.064 2.022 1.763 47.837 0.228 7.844 16.720 0.16 73395. 0.6514 1.82 0.0482 0.1298 0.0850 0.0315 0.065 2.048 1.734 48.464 0.231 7.714 16.230 0.16 73446. 0.6271 2.74 0.0723 0.1889 0.0835 0.0319 0.066 2.073 1.703 49.041 0.234 7.573 15.747 0.16 73501. 0.6028 3.65 0.0963 0.2443 0.0818 0.0323 0.066 2.094 1.668 49.555 0.237 7.421 15.270 0.16 73561. 0.5787 4.56 0.1204 0.2960 0.0800 0.0325 0.067 2.113 1.632 49.992 0.239 7.257 14.803 0.16 73625. 0.5547 5.47 0.1445 0.3442 0.0781 0.0328 0.068 2.127 1.592 50.338 0.240 7.081 14.344 0.16 73694. 0.5310 6.39 0.1686 0.3890 0.0760 0.0329 0.068 2.137 1.549 50.577 0.241 6.892 13.895 0.16 73769. 0.5074 7.30 0.1927 0.4305 0.0737 0.0330 0.068 2.142 1.504 50.695 0.242 6.690 13.456 0.16 73848. 0.4841 8.21 0.2168 0.4689 0.0714 0.0330 0.068 2.142 1.455 50.677 0.242 6.474 13.026 0.16 73933. 0.4611 9.12 0.2408 0.5042 0.0688 0.0329 0.068 2.134 1.404 50.506 0.241 6.244 12.606 0.16 74023. 0.4382 10.03 0.2649 0.5365 0.0661 0.0327 0.067 2.120 1.349 50.170 0.240 6.000 12.194 0.16 74118. 0.4155 10.95 0.2890 0.5658 0.0633 0.0323 0.067 2.098 1.291 49.652 0.237 5.741 11.790 0.16 74220. 0.3930 11.86 0.3131 0.5923 0.0603 0.0319 0.066 2.068 1.229 48.936 0.234 5.467 11.392 0.16 74327. 0.3705 12.77 0.3372 0.6159 0.0571 0.0313 0.064 2.029 1.164 48.012 0.229 5.179 10.999 0.16 74439. 0.3482 13.68 0.3613 0.6364 0.0538 0.0305 0.063 1.981 1.096 46.878 0.224 4.877 10.609 0.16 74558. 0.3259 14.60 0.3853 0.6539 0.0503 0.0296 0.061 1.924 1.026 45.538 0.217 4.563 10.219 0.16 74682. 0.3037 15.51 0.4094 0.6680 0.0467 0.0286 0.059 1.859 0.953 43.995 0.210 4.239 9.825 0.16 74813. 0.2814 16.42 0.4335 0.6785 0.0430 0.0275 0.057 1.786 0.878 42.252 0.202 3.905 9.425 0.16 74949. 0.2591 17.33 0.4576 0.6848 0.0393 0.0262 0.054 1.704 0.801 40.313 0.192 3.563 9.013 0.16 75091. 0.2367 18.25 0.4817 0.6865 0.0354 0.0249 0.051 1.614 0.723 38.183 0.182 3.214 8.583 0.16 75239. 0.2141 19.16 0.5058 0.6827 0.0315 0.0233 0.048 1.516 0.643 35.866 0.171 2.859 8.129 0.16 75392. 0.1912 20.07 0.5298 0.6721 0.0276 0.0217 0.045 1.410 0.562 33.370 0.159 2.500 7.639 0.16 75552. 0.1680 20.98 0.5539 0.6531 0.0236 0.0200 0.041 1.298 0.481 30.703 0.147 2.138 7.100 0.16 75718. 0.1444 21.89 0.5780 0.6229 0.0196 0.0181 0.037 1.178 0.399 27.873 0.133 1.774 6.490 0.16 75890. 0.1202 22.81 0.6021 0.5776 0.0155 0.0162 0.033 1.052 0.317 24.894 0.119 1.410 5.777 0.16 76068. 0.0954 23.72 0.6262 0.5104 0.0116 0.0142 0.029 0.920 0.236 21.781 0.104 1.049 4.909 0.16 76252. 0.0699 24.63 0.6503 0.4100 0.0076 0.0121 0.025 0.784 0.155 18.551 0.089 0.691 3.797 0.16 76442. 0.0439 25.54 0.6743 0.2544 0.0037 0.0099 0.020 0.643 0.076 15.226 0.073 0.339 2.272 0.16 76637. 0.0184 26.46 0.6984 -0.0049 -0.0001 0.0077 0.016 0.500 -0.001 11.822 0.056 -0.005 -0.042 0.16 76836. 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 0.0882 0.0298 0.207 4.347 4.047 154.299 0.491 18.000 11.896 0.24 110020. 0.7021 1.37 0.0241 0.0694 0.0869 0.0302 0.210 4.413 3.986 156.627 0.499 17.730 11.543 0.24 110090. 0.6761 2.74 0.0482 0.1345 0.0854 0.0306 0.213 4.475 3.920 158.832 0.506 17.437 11.195 0.24 110167. 0.6503 4.11 0.0724 0.1956 0.0839 0.0310 0.216 4.532 3.849 160.869 0.512 17.120 10.852 0.24 110250. 0.6246 5.48 0.0965 0.2528 0.0822 0.0314 0.218 4.584 3.772 162.693 0.518 16.778 10.516 0.24 110340. 0.5992 6.85 0.1206 0.3061 0.0804 0.0317 0.220 4.628 3.689 164.255 0.523 16.409 10.187 0.24 110436. 0.5740 8.22 0.1447 0.3557 0.0784 0.0319 0.222 4.663 3.600 165.505 0.527 16.011 9.865 0.24 110541. 0.5491 9.59 0.1689 0.4017 0.0764 0.0321 0.223 4.688 3.504 166.391 0.530 15.585 9.551 0.24 110652. 0.5245 10.97 0.1930 0.4444 0.0741 0.0322 0.224 4.701 3.401 166.861 0.531 15.128 9.245 0.24 110772. 0.5002 12.34 0.2171 0.4838 0.0717 0.0322 0.224 4.701 3.291 166.861 0.531 14.640 8.947 0.24 110899. 0.4762 13.71 0.2412 0.5201 0.0692 0.0321 0.223 4.686 3.174 166.338 0.529 14.120 8.656 0.24 111035. 0.4525 15.08 0.2654 0.5534 0.0665 0.0319 0.222 4.656 3.050 165.243 0.526 13.568 8.373 0.24 111179. 0.4290 16.45 0.2895 0.5837 0.0636 0.0315 0.219 4.607 2.919 163.521 0.521 12.982 8.096 0.24 111331. 0.4058 17.82 0.3136 0.6112 0.0606 0.0311 0.216 4.539 2.779 161.115 0.513 12.363 7.824 0.24 111492. 0.3827 19.19 0.3377 0.6358 0.0574 0.0305 0.212 4.451 2.633 157.989 0.503 11.710 7.558 0.24 111662. 0.3598 20.56 0.3618 0.6575 0.0540 0.0297 0.207 4.343 2.479 154.137 0.491 11.027 7.295 0.24 111841. 0.3370 21.93 0.3860 0.6762 0.0505 0.0288 0.201 4.214 2.319 149.564 0.476 10.316 7.034 0.24 112028. 0.3143 23.30 0.4101 0.6917 0.0469 0.0278 0.193 4.065 2.154 144.283 0.459 9.582 6.772 0.24 112224. 0.2916 24.67 0.4342 0.7038 0.0432 0.0267 0.185 3.897 1.984 138.302 0.440 8.826 6.507 0.24 112429. 0.2689 26.04 0.4583 0.7121 0.0394 0.0254 0.177 3.709 1.810 131.636 0.419 8.051 6.237 0.24 112642. 0.2462 27.41 0.4825 0.7159 0.0356 0.0240 0.167 3.502 1.632 124.298 0.396 7.261 5.957 0.24 112865. 0.2233 28.78 0.5066 0.7145 0.0316 0.0224 0.156 3.277 1.452 116.307 0.370 6.458 5.662 0.24 113096. 0.2002 30.15 0.5307 0.7067 0.0277 0.0208 0.144 3.034 1.269 107.683 0.343 5.646 5.346 0.24 113337. 0.1767 31.52 0.5548 0.6908 0.0236 0.0190 0.132 2.774 1.085 98.455 0.313 4.826 4.999 0.24 113586. 0.1528 32.90 0.5790 0.6641 0.0196 0.0171 0.119 2.498 0.900 88.658 0.282 4.004 4.605 0.24 113845. 0.1282 34.27 0.6031 0.6222 0.0156 0.0151 0.105 2.207 0.715 78.334 0.249 3.182 4.142 0.24 114113. 0.1028 35.64 0.6272 0.5578 0.0116 0.0130 0.091 1.903 0.532 67.538 0.215 2.365 3.570 0.24 114389. 0.0764 37.01 0.6513 0.4573 0.0076 0.0109 0.076 1.587 0.350 56.334 0.179 1.557 2.818 0.24 114675. 0.0489 38.38 0.6755 0.2925 0.0037 0.0086 0.060 1.262 0.172 44.798 0.143 0.764 1.739 0.24 114970. 0.0211 39.75 0.6996 -0.0068 -0.0001 0.0064 0.044 0.929 -0.003 32.976 0.105 -0.013 -0.039 0.24 115268. 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 0.0887 0.0293 0.483 7.616 7.236 360.413 0.860 32.186 9.106 0.32 146688. 0.7187 1.85 0.0244 0.0715 0.0874 0.0298 0.491 7.737 7.127 366.136 0.874 31.702 8.829 0.32 146783. 0.6916 3.69 0.0487 0.1385 0.0859 0.0302 0.498 7.851 7.009 371.560 0.887 31.177 8.556 0.32 146886. 0.6646 5.54 0.0731 0.2013 0.0843 0.0306 0.505 7.957 6.881 376.572 0.899 30.607 8.288 0.32 146999. 0.6378 7.39 0.0975 0.2599 0.0826 0.0310 0.511 8.052 6.742 381.062 0.910 29.990 8.025 0.32 147120. 0.6114 9.23 0.1219 0.3144 0.0808 0.0313 0.516 8.133 6.593 384.907 0.919 29.324 7.769 0.32 147251. 0.5852 11.08 0.1462 0.3652 0.0788 0.0316 0.520 8.198 6.431 387.984 0.926 28.606 7.518 0.32 147392. 0.5594 12.93 0.1706 0.4122 0.0767 0.0317 0.523 8.244 6.258 390.160 0.931 27.835 7.275 0.32 147544. 0.5339 14.77 0.1950 0.4558 0.0744 0.0318 0.525 8.269 6.072 391.305 0.934 27.007 7.038 0.32 147706. 0.5088 16.62 0.2194 0.4960 0.0720 0.0318 0.525 8.268 5.873 391.286 0.934 26.123 6.808 0.32 147879. 0.4840 18.47 0.2437 0.5330 0.0694 0.0317 0.523 8.240 5.661 389.972 0.931 25.180 6.584 0.32 148063. 0.4596 20.31 0.2681 0.5669 0.0666 0.0315 0.519 8.183 5.436 387.236 0.924 24.177 6.367 0.32 148259. 0.4355 22.16 0.2925 0.5979 0.0637 0.0312 0.514 8.092 5.196 382.943 0.914 23.114 6.155 0.32 148466. 0.4116 24.01 0.3169 0.6259 0.0606 0.0307 0.506 7.965 4.943 376.954 0.900 21.987 5.948 0.32 148684. 0.3880 25.85 0.3412 0.6511 0.0573 0.0300 0.495 7.801 4.676 369.182 0.881 20.800 5.745 0.32 148915. 0.3645 27.70 0.3656 0.6734 0.0539 0.0293 0.482 7.599 4.397 359.615 0.859 19.558 5.546 0.32 149157. 0.3412 29.54 0.3900 0.6928 0.0503 0.0283 0.467 7.359 4.107 348.270 0.831 18.267 5.349 0.32 149412. 0.3180 31.39 0.4144 0.7089 0.0467 0.0273 0.449 7.082 3.807 335.172 0.800 16.933 5.152 0.32 149678. 0.2949 33.24 0.4387 0.7217 0.0429 0.0261 0.430 6.769 3.498 320.346 0.765 15.560 4.953 0.32 149956. 0.2718 35.08 0.4631 0.7307 0.0390 0.0247 0.407 6.420 3.182 303.822 0.725 14.154 4.750 0.32 150247. 0.2486 36.93 0.4875 0.7352 0.0351 0.0232 0.383 6.036 2.860 285.637 0.682 12.720 4.541 0.32 150549. 0.2253 38.78 0.5119 0.7345 0.0310 0.0216 0.356 5.617 2.532 265.836 0.635 11.264 4.321 0.32 150864. 0.2017 40.62 0.5362 0.7273 0.0270 0.0199 0.328 5.166 2.201 244.476 0.584 9.791 4.084 0.32 151191. 0.1778 42.47 0.5606 0.7117 0.0229 0.0180 0.297 4.683 1.868 221.629 0.529 8.308 3.822 0.32 151530. 0.1533 44.32 0.5850 0.6845 0.0188 0.0161 0.265 4.171 1.533 197.388 0.471 6.820 3.523 0.32 151881. 0.1280 46.16 0.6094 0.6407 0.0147 0.0140 0.230 3.632 1.200 171.867 0.410 5.335 3.166 0.32 152245. 0.1017 48.01 0.6337 0.5708 0.0106 0.0118 0.195 3.068 0.868 145.207 0.347 3.862 2.712 0.32 152621. 0.0741 49.86 0.6581 0.4565 0.0066 0.0096 0.158 2.485 0.541 117.582 0.281 2.408 2.089 0.32 153009. 0.0451 51.70 0.6825 0.2550 0.0027 0.0073 0.120 1.885 0.221 89.186 0.213 0.984 1.125 0.32 153409. 0.0155 53.55 0.7069 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 0.0893 0.0292 0.939 11.838 11.389 700.310 1.337 50.660 7.377 0.40 183351. 0.7304 2.29 0.0241 0.0717 0.0880 0.0296 0.954 12.030 11.222 711.640 1.359 49.915 7.152 0.40 183469. 0.7029 4.57 0.0483 0.1389 0.0866 0.0301 0.969 12.212 11.040 722.395 1.380 49.104 6.931 0.40 183597. 0.6757 6.86 0.0724 0.2018 0.0851 0.0305 0.982 12.380 10.842 732.357 1.399 48.225 6.715 0.40 183736. 0.6487 9.14 0.0965 0.2606 0.0834 0.0309 0.994 12.531 10.628 741.310 1.416 47.273 6.503 0.40 183886. 0.6220 11.43 0.1207 0.3154 0.0816 0.0312 1.004 12.662 10.397 749.023 1.431 46.245 6.296 0.40 184049. 0.5956 13.71 0.1448 0.3664 0.0796 0.0315 1.013 12.767 10.148 755.252 1.442 45.137 6.094 0.40 184223. 0.5696 16.00 0.1690 0.4137 0.0775 0.0317 1.019 12.843 9.880 759.745 1.451 43.946 5.898 0.40 184410. 0.5439 18.28 0.1931 0.4576 0.0753 0.0318 1.022 12.885 9.593 762.248 1.456 42.668 5.708 0.40 184610. 0.5187 20.57 0.2172 0.4981 0.0728 0.0318 1.023 12.890 9.285 762.504 1.456 41.301 5.523 0.40 184824. 0.4938 22.86 0.2414 0.5355 0.0703 0.0317 1.020 12.852 8.958 760.261 1.452 39.844 5.344 0.40 185051. 0.4693 25.14 0.2655 0.5698 0.0675 0.0315 1.013 12.767 8.609 755.270 1.442 38.293 5.170 0.40 185292. 0.4451 27.43 0.2896 0.6013 0.0646 0.0311 1.002 12.632 8.239 747.278 1.427 36.648 5.001 0.40 185547. 0.4211 29.71 0.3138 0.6299 0.0616 0.0307 0.987 12.442 7.848 736.011 1.406 34.906 4.836 0.40 185816. 0.3975 32.00 0.3379 0.6558 0.0583 0.0300 0.967 12.193 7.434 721.273 1.378 33.068 4.675 0.40 186100. 0.3740 34.28 0.3620 0.6789 0.0549 0.0293 0.943 11.884 7.002 703.026 1.343 31.143 4.517 0.40 186399. 0.3507 36.57 0.3862 0.6993 0.0514 0.0284 0.914 11.517 6.551 681.293 1.301 29.141 4.362 0.40 186712. 0.3275 38.86 0.4103 0.7166 0.0477 0.0273 0.880 11.091 6.086 656.118 1.253 27.068 4.207 0.40 187039. 0.3045 41.14 0.4344 0.7308 0.0440 0.0261 0.842 10.608 5.606 627.549 1.199 24.935 4.052 0.40 187381. 0.2814 43.43 0.4586 0.7414 0.0401 0.0248 0.799 10.069 5.114 595.641 1.138 22.749 3.895 0.40 187738. 0.2584 45.71 0.4827 0.7481 0.0362 0.0233 0.752 9.474 4.613 560.460 1.070 20.518 3.733 0.40 188110. 0.2352 48.00 0.5069 0.7500 0.0322 0.0218 0.700 8.826 4.103 522.090 0.997 18.250 3.564 0.40 188497. 0.2118 50.28 0.5310 0.7462 0.0281 0.0200 0.645 8.125 3.587 480.635 0.918 15.954 3.385 0.40 188899. 0.1881 52.57 0.5551 0.7348 0.0241 0.0182 0.585 7.374 3.066 436.230 0.833 13.640 3.188 0.40 189315. 0.1638 54.85 0.5793 0.7133 0.0200 0.0162 0.522 6.577 2.544 389.042 0.743 11.316 2.966 0.40 189747. 0.1388 57.14 0.6034 0.6772 0.0159 0.0141 0.455 5.735 2.022 339.285 0.648 8.994 2.703 0.40 190194. 0.1128 59.43 0.6275 0.6185 0.0118 0.0120 0.385 4.855 1.503 287.221 0.549 6.687 2.374 0.40 190655. 0.0854 61.71 0.6517 0.5214 0.0078 0.0097 0.313 3.942 0.991 233.173 0.445 4.407 1.927 0.41 191132. 0.0563 64.00 0.6758 0.3494 0.0038 0.0074 0.238 3.001 0.487 177.516 0.339 2.168 1.245 0.41 191623. 0.0255 66.28 0.6999 -0.0059 0.0000 0.0050 0.161 2.036 -0.005 120.418 0.230 -0.024 -0.020 0.41 192118. 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 0.0902 0.0292 1.626 17.077 16.550 1212.218 1.929 73.613 6.192 0.48 220007. 0.7391 2.74 0.0241 0.0721 0.0889 0.0297 1.652 17.359 16.310 1232.244 1.961 72.546 6.003 0.48 220149. 0.7113 5.48 0.0482 0.1398 0.0874 0.0302 1.678 17.627 16.049 1251.261 1.991 71.384 5.817 0.48 220303. 0.6837 8.22 0.0724 0.2031 0.0859 0.0306 1.702 17.875 15.765 1268.890 2.020 70.122 5.635 0.48 220471. 0.6564 10.96 0.0965 0.2623 0.0842 0.0310 1.723 18.098 15.457 1284.744 2.045 68.754 5.457 0.48 220651. 0.6294 13.70 0.1206 0.3174 0.0824 0.0313 1.741 18.291 15.124 1298.421 2.067 67.274 5.283 0.48 220846. 0.6028 16.45 0.1447 0.3687 0.0804 0.0316 1.756 18.447 14.765 1309.489 2.084 65.676 5.114 0.48 221056. 0.5766 19.19 0.1688 0.4164 0.0783 0.0318 1.767 18.560 14.379 1317.503 2.097 63.957 4.950 0.48 221281. 0.5507 21.93 0.1930 0.4605 0.0761 0.0319 1.773 18.623 13.964 1322.015 2.104 62.111 4.791 0.48 221522. 0.5252 24.67 0.2171 0.5014 0.0737 0.0319 1.774 18.631 13.519 1322.573 2.105 60.134 4.636 0.48 221778. 0.5001 27.41 0.2412 0.5391 0.0711 0.0318 1.768 18.577 13.045 1318.733 2.099 58.024 4.487 0.48 222051. 0.4754 30.15 0.2653 0.5738 0.0683 0.0316 1.757 18.455 12.540 1310.058 2.085 55.778 4.342 0.48 222341. 0.4511 32.89 0.2894 0.6057 0.0654 0.0312 1.738 18.258 12.004 1296.105 2.063 53.393 4.201 0.48 222647. 0.4270 35.63 0.3136 0.6348 0.0623 0.0308 1.712 17.981 11.436 1276.398 2.031 50.866 4.064 0.48 222971. 0.4032 38.37 0.3377 0.6611 0.0590 0.0302 1.677 17.617 10.836 1250.574 1.990 48.199 3.930 0.48 223312. 0.3796 41.11 0.3618 0.6848 0.0556 0.0294 1.634 17.166 10.208 1218.556 1.939 45.403 3.799 0.48 223670. 0.3561 43.85 0.3859 0.7057 0.0520 0.0285 1.583 16.628 9.553 1180.383 1.879 42.492 3.671 0.48 224046. 0.3329 46.59 0.4100 0.7238 0.0484 0.0274 1.524 16.005 8.876 1136.127 1.808 39.478 3.543 0.48 224439. 0.3097 49.34 0.4342 0.7388 0.0446 0.0262 1.456 15.297 8.178 1085.875 1.728 36.375 3.416 0.48 224850. 0.2866 52.08 0.4583 0.7504 0.0407 0.0248 1.381 14.506 7.462 1029.722 1.639 33.193 3.287 0.48 225278. 0.2634 54.82 0.4824 0.7582 0.0367 0.0233 1.298 13.633 6.732 967.784 1.540 29.944 3.155 0.48 225724. 0.2402 57.56 0.5065 0.7615 0.0326 0.0217 1.207 12.681 5.990 900.208 1.433 26.642 3.018 0.48 226188. 0.2167 60.30 0.5306 0.7592 0.0285 0.0199 1.109 11.652 5.238 827.176 1.316 23.297 2.872 0.48 226670. 0.1928 63.04 0.5547 0.7497 0.0244 0.0181 1.004 10.550 4.479 748.926 1.192 19.924 2.713 0.48 227170. 0.1684 65.78 0.5789 0.7305 0.0203 0.0161 0.893 9.379 3.718 665.753 1.060 16.537 2.533 0.48 227687. 0.1433 68.52 0.6030 0.6970 0.0161 0.0139 0.775 8.143 2.957 578.034 0.920 13.153 2.320 0.48 228223. 0.1171 71.26 0.6271 0.6413 0.0120 0.0117 0.652 6.850 2.201 486.235 0.774 9.788 2.053 0.49 228776. 0.0893 74.00 0.6512 0.5469 0.0079 0.0094 0.524 5.507 1.453 390.925 0.622 6.463 1.686 0.49 229348. 0.0596 76.74 0.6753 0.3747 0.0039 0.0071 0.393 4.124 0.719 292.776 0.466 3.198 1.114 0.49 229936. 0.0277 79.48 0.6995 0.0001 0.0000 0.0046 0.258 2.706 0.000 192.081 0.306 0.000 0.000 0.49 230529. 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 0.0912 0.0294 2.601 23.418 22.775 1939.470 2.646 101.303 5.326 0.56 256655. 0.7457 3.20 0.0241 0.0724 0.0899 0.0299 2.645 23.812 22.451 1972.095 2.690 99.863 5.164 0.56 256821. 0.7178 6.39 0.0482 0.1403 0.0884 0.0304 2.686 24.187 22.098 2003.088 2.733 98.290 5.004 0.56 257002. 0.6901 9.59 0.0723 0.2038 0.0869 0.0308 2.725 24.534 21.713 2031.827 2.772 96.578 4.847 0.56 257198. 0.6626 12.79 0.0965 0.2632 0.0852 0.0312 2.759 24.846 21.295 2057.685 2.807 94.719 4.694 0.56 257409. 0.6355 15.99 0.1206 0.3185 0.0834 0.0316 2.789 25.115 20.842 2079.997 2.838 92.705 4.545 0.56 257638. 0.6087 19.18 0.1447 0.3700 0.0815 0.0319 2.814 25.333 20.352 2098.065 2.862 90.527 4.400 0.56 257883. 0.5823 22.38 0.1688 0.4179 0.0793 0.0321 2.831 25.492 19.824 2111.166 2.880 88.179 4.259 0.56 258146. 0.5564 25.58 0.1929 0.4623 0.0771 0.0322 2.841 25.581 19.257 2118.569 2.890 85.654 4.123 0.56 258428. 0.5308 28.77 0.2170 0.5034 0.0746 0.0322 2.842 25.593 18.648 2119.540 2.891 82.947 3.991 0.56 258728. 0.5056 31.97 0.2411 0.5414 0.0720 0.0321 2.834 25.518 17.998 2113.358 2.883 80.054 3.863 0.56 259048. 0.4808 35.17 0.2653 0.5764 0.0693 0.0319 2.815 25.348 17.305 2099.318 2.864 76.972 3.739 0.56 259386. 0.4563 38.36 0.2894 0.6086 0.0663 0.0315 2.785 25.075 16.568 2076.703 2.833 73.696 3.619 0.56 259745. 0.4321 41.56 0.3135 0.6381 0.0632 0.0310 2.742 24.690 15.787 2044.750 2.789 70.222 3.502 0.56 260123. 0.4082 44.76 0.3376 0.6649 0.0599 0.0304 2.686 24.184 14.962 2002.852 2.732 66.551 3.388 0.56 260522. 0.3845 47.96 0.3617 0.6890 0.0564 0.0296 2.616 23.556 14.096 1950.865 2.661 62.701 3.277 0.56 260941. 0.3610 51.15 0.3858 0.7105 0.0528 0.0287 2.533 22.807 13.194 1888.848 2.577 58.688 3.168 0.56 261380. 0.3376 54.35 0.4100 0.7292 0.0491 0.0276 2.437 21.939 12.260 1816.922 2.479 54.531 3.060 0.56 261839. 0.3144 57.55 0.4341 0.7450 0.0452 0.0263 2.327 20.952 11.297 1735.229 2.367 50.248 2.953 0.56 262319. 0.2912 60.74 0.4582 0.7574 0.0413 0.0250 2.205 19.850 10.309 1643.925 2.243 45.855 2.844 0.56 262820. 0.2679 63.94 0.4823 0.7662 0.0372 0.0234 2.069 18.634 9.300 1543.203 2.105 41.367 2.733 0.56 263340. 0.2446 67.14 0.5064 0.7707 0.0331 0.0218 1.922 17.307 8.274 1433.299 1.955 36.803 2.618 0.56 263882. 0.2210 70.33 0.5305 0.7697 0.0290 0.0200 1.763 15.872 7.235 1314.512 1.793 32.180 2.496 0.56 264444. 0.1970 73.53 0.5546 0.7618 0.0248 0.0180 1.592 14.335 6.186 1187.228 1.620 27.516 2.363 0.56 265027. 0.1725 76.73 0.5788 0.7445 0.0205 0.0160 1.411 12.702 5.133 1051.933 1.435 22.831 2.213 0.56 265631. 0.1471 79.93 0.6029 0.7132 0.0163 0.0138 1.219 10.979 4.080 909.240 1.240 18.148 2.035 0.57 266256. 0.1206 83.12 0.6270 0.6597 0.0121 0.0115 1.019 9.176 3.033 759.913 1.037 13.492 1.810 0.57 266902. 0.0925 86.32 0.6511 0.5671 0.0080 0.0092 0.811 7.304 1.999 604.887 0.825 8.889 1.499 0.57 267568. 0.0622 89.52 0.6752 0.3928 0.0039 0.0068 0.597 5.376 0.983 445.269 0.607 4.371 1.001 0.57 268255. 0.0291 92.71 0.6993 -0.0084 -0.0001 0.0043 0.377 3.398 -0.013 281.409 0.384 -0.057 -0.021 0.57 268944. 0.0000 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 0.0924 0.0298 3.933 30.989 30.142 2933.049 3.501 134.073 4.661 0.63 293292. 0.7508 3.65 0.0241 0.0723 0.0911 0.0303 4.001 31.519 29.725 2983.212 3.561 132.215 4.519 0.63 293482. 0.7229 7.30 0.0482 0.1402 0.0897 0.0308 4.064 32.022 29.267 3030.882 3.618 130.181 4.380 0.63 293689. 0.6952 10.95 0.0723 0.2037 0.0882 0.0313 4.124 32.489 28.768 3075.099 3.671 127.961 4.243 0.63 293914. 0.6677 14.60 0.0964 0.2631 0.0865 0.0317 4.177 32.910 28.225 3114.896 3.718 125.543 4.110 0.63 294157. 0.6406 18.25 0.1205 0.3185 0.0847 0.0320 4.223 33.273 27.634 3149.247 3.759 122.917 3.980 0.64 294418. 0.6138 21.91 0.1446 0.3701 0.0827 0.0323 4.261 33.567 26.995 3177.078 3.792 120.072 3.854 0.64 294700. 0.5874 25.56 0.1687 0.4181 0.0806 0.0325 4.288 33.780 26.303 3197.273 3.816 116.997 3.731 0.64 295002. 0.5615 29.21 0.1928 0.4626 0.0783 0.0326 4.303 33.901 25.559 3208.721 3.830 113.686 3.613 0.64 295325. 0.5359 32.86 0.2169 0.5039 0.0759 0.0327 4.305 33.918 24.759 3210.293 3.832 110.130 3.498 0.64 295669. 0.5107 36.51 0.2410 0.5421 0.0732 0.0326 4.292 33.818 23.903 3200.890 3.821 106.323 3.387 0.64 296035. 0.4858 40.16 0.2651 0.5774 0.0705 0.0323 4.264 33.592 22.990 3179.430 3.795 102.260 3.280 0.64 296423. 0.4614 43.81 0.2892 0.6099 0.0675 0.0320 4.217 33.226 22.018 3144.839 3.754 97.938 3.176 0.64 296834. 0.4372 47.46 0.3132 0.6397 0.0643 0.0315 4.152 32.710 20.987 3095.963 3.696 93.349 3.075 0.64 297267. 0.4132 51.11 0.3373 0.6670 0.0610 0.0308 4.066 32.032 19.896 3031.846 3.619 88.496 2.976 0.64 297723. 0.3895 54.76 0.3614 0.6916 0.0575 0.0300 3.959 31.191 18.749 2952.219 3.524 83.398 2.881 0.64 298203. 0.3659 58.41 0.3855 0.7136 0.0538 0.0291 3.832 30.187 17.554 2857.188 3.411 78.080 2.787 0.64 298705. 0.3425 62.07 0.4096 0.7330 0.0500 0.0279 3.684 29.022 16.314 2746.938 3.279 72.566 2.694 0.64 299231. 0.3192 65.72 0.4337 0.7494 0.0461 0.0267 3.516 27.699 15.036 2621.690 3.129 66.880 2.601 0.64 299780. 0.2959 69.37 0.4578 0.7628 0.0421 0.0252 3.328 26.220 13.724 2481.697 2.962 61.044 2.508 0.64 300352. 0.2726 73.02 0.4819 0.7726 0.0379 0.0237 3.121 24.588 12.383 2327.251 2.778 55.080 2.413 0.64 300947. 0.2492 76.67 0.5060 0.7781 0.0338 0.0220 2.895 22.808 11.018 2158.723 2.577 49.010 2.315 0.64 301566. 0.2255 80.32 0.5301 0.7786 0.0295 0.0201 2.651 20.883 9.635 1976.573 2.359 42.858 2.211 0.64 302209. 0.2014 83.97 0.5542 0.7723 0.0252 0.0181 2.389 18.821 8.239 1781.387 2.126 36.648 2.098 0.64 302875. 0.1767 87.62 0.5783 0.7568 0.0209 0.0160 2.111 16.629 6.836 1573.917 1.879 30.408 1.970 0.65 303564. 0.1511 91.27 0.6024 0.7277 0.0167 0.0138 1.817 14.317 5.434 1355.104 1.618 24.169 1.819 0.65 304278. 0.1244 94.92 0.6265 0.6769 0.0124 0.0115 1.510 11.898 4.038 1126.123 1.344 17.962 1.626 0.65 305015. 0.0959 98.58 0.6506 0.5866 0.0081 0.0090 1.191 9.386 2.659 888.423 1.060 11.826 1.357 0.65 305776. 0.0649 102.23 0.6747 0.4118 0.0040 0.0065 0.863 6.801 1.304 643.714 0.768 5.800 0.919 0.65 306560. 0.0308 105.88 0.6988 -0.0131 -0.0001 0.0040 0.526 4.146 -0.024 392.429 0.468 -0.109 -0.028 0.65 307344. 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 0.0938 0.0305 5.720 40.057 38.754 4265.270 4.526 172.377 4.121 0.71 329914. 0.7527 4.12 0.0242 0.0722 0.0926 0.0310 5.816 40.733 38.234 4337.265 4.602 170.065 3.998 0.71 330130. 0.7253 8.23 0.0483 0.1400 0.0912 0.0315 5.908 41.378 37.662 4405.952 4.675 167.521 3.877 0.71 330364. 0.6981 12.35 0.0725 0.2035 0.0897 0.0319 5.994 41.978 37.035 4469.883 4.743 164.733 3.758 0.71 330619. 0.6710 16.47 0.0966 0.2629 0.0880 0.0323 6.072 42.521 36.350 4527.611 4.804 161.686 3.642 0.71 330894. 0.6441 20.59 0.1208 0.3184 0.0862 0.0327 6.139 42.990 35.603 4577.576 4.857 158.363 3.528 0.71 331191. 0.6176 24.70 0.1449 0.3701 0.0842 0.0330 6.193 43.370 34.791 4618.117 4.900 154.750 3.417 0.71 331511. 0.5913 28.82 0.1691 0.4182 0.0821 0.0332 6.232 43.647 33.911 4647.526 4.931 150.834 3.309 0.72 331853. 0.5654 32.94 0.1932 0.4628 0.0798 0.0333 6.255 43.802 32.960 4664.046 4.949 146.605 3.205 0.72 332220. 0.5399 37.06 0.2174 0.5043 0.0773 0.0333 6.257 43.820 31.936 4665.950 4.951 142.051 3.104 0.72 332610. 0.5147 41.17 0.2415 0.5428 0.0747 0.0332 6.238 43.684 30.838 4651.538 4.935 137.165 3.007 0.72 333026. 0.4899 45.29 0.2657 0.5783 0.0718 0.0330 6.194 43.381 29.663 4619.219 4.901 131.941 2.913 0.72 333466. 0.4654 49.41 0.2899 0.6111 0.0688 0.0326 6.125 42.894 28.411 4567.417 4.846 126.374 2.821 0.72 333932. 0.4412 53.52 0.3140 0.6413 0.0656 0.0321 6.027 42.209 27.081 4494.447 4.769 120.454 2.733 0.72 334423. 0.4172 57.64 0.3382 0.6689 0.0622 0.0314 5.899 41.312 25.671 4398.890 4.667 114.184 2.647 0.72 334941. 0.3935 61.76 0.3623 0.6940 0.0586 0.0306 5.740 40.198 24.188 4280.329 4.542 107.588 2.563 0.72 335484. 0.3698 65.88 0.3865 0.7165 0.0548 0.0296 5.550 38.870 22.639 4138.923 4.392 100.700 2.481 0.72 336054. 0.3463 69.99 0.4106 0.7364 0.0509 0.0284 5.331 37.331 21.032 3974.979 4.218 93.552 2.400 0.72 336649. 0.3229 74.11 0.4348 0.7535 0.0469 0.0271 5.081 35.582 19.374 3788.838 4.020 86.174 2.319 0.72 337271. 0.2995 78.23 0.4589 0.7676 0.0428 0.0256 4.802 33.630 17.670 3580.894 3.799 78.596 2.238 0.72 337919. 0.2760 82.35 0.4831 0.7781 0.0386 0.0239 4.495 31.476 15.928 3351.603 3.556 70.847 2.155 0.72 338593. 0.2524 86.46 0.5072 0.7846 0.0343 0.0222 4.159 29.128 14.154 3101.557 3.291 62.956 2.070 0.72 339294. 0.2285 90.58 0.5314 0.7859 0.0299 0.0202 3.797 26.592 12.355 2831.510 3.004 54.954 1.979 0.72 340021. 0.2041 94.70 0.5556 0.7805 0.0255 0.0182 3.409 23.877 10.539 2542.435 2.698 46.875 1.880 0.73 340774. 0.1791 98.81 0.5797 0.7658 0.0211 0.0160 2.998 20.995 8.713 2235.588 2.372 38.755 1.768 0.73 341555. 0.1531 102.93 0.6039 0.7370 0.0167 0.0137 2.565 17.962 6.887 1912.574 2.029 30.632 1.633 0.73 342361. 0.1257 107.05 0.6280 0.6850 0.0123 0.0113 2.113 14.796 5.070 1575.438 1.672 22.552 1.460 0.73 343195. 0.0964 111.17 0.6522 0.5900 0.0079 0.0088 1.645 11.521 3.274 1226.714 1.302 14.565 1.211 0.73 344055. 0.0643 115.28 0.6763 0.3985 0.0037 0.0062 1.166 8.165 1.511 869.419 0.922 6.722 0.788 0.73 344941. 0.0284 119.40 0.7005 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 0.0956 0.0324 8.354 52.657 48.728 6229.929 5.949 216.743 3.548 0.79 366517. 0.7266 4.54 0.0240 0.0689 0.0944 0.0329 8.462 53.336 48.112 6310.292 6.026 214.001 3.458 0.79 366756. 0.7037 9.09 0.0480 0.1342 0.0930 0.0333 8.564 53.975 47.430 6385.887 6.098 210.969 3.369 0.79 367016. 0.6807 13.63 0.0720 0.1960 0.0915 0.0336 8.656 54.559 46.679 6454.980 6.164 207.629 3.280 0.79 367297. 0.6575 18.18 0.0960 0.2544 0.0899 0.0339 8.738 55.073 45.854 6515.792 6.222 203.958 3.192 0.79 367602. 0.6341 22.72 0.1200 0.3093 0.0882 0.0342 8.806 55.502 44.950 6566.494 6.271 199.938 3.105 0.79 367932. 0.6107 27.27 0.1440 0.3609 0.0862 0.0344 8.858 55.828 43.963 6605.083 6.307 195.547 3.019 0.79 368285. 0.5873 31.81 0.1680 0.4092 0.0841 0.0345 8.890 56.034 42.889 6629.502 6.331 190.769 2.934 0.79 368665. 0.5638 36.36 0.1920 0.4544 0.0818 0.0346 8.901 56.103 41.724 6637.623 6.338 185.589 2.851 0.79 369070. 0.5403 40.90 0.2160 0.4966 0.0794 0.0345 8.887 56.015 40.466 6627.251 6.329 179.992 2.769 0.80 369503. 0.5169 45.45 0.2400 0.5358 0.0767 0.0344 8.846 55.752 39.112 6596.158 6.299 173.969 2.689 0.80 369962. 0.4935 49.99 0.2639 0.5722 0.0739 0.0341 8.773 55.296 37.660 6542.113 6.247 167.512 2.611 0.80 370449. 0.4701 54.53 0.2879 0.6059 0.0708 0.0337 8.667 54.626 36.109 6462.842 6.172 160.614 2.534 0.80 370964. 0.4468 59.08 0.3119 0.6369 0.0676 0.0331 8.523 53.721 34.457 6355.867 6.069 153.266 2.459 0.80 371507. 0.4235 63.62 0.3359 0.6653 0.0641 0.0324 8.340 52.563 32.703 6218.799 5.939 145.465 2.385 0.80 372079. 0.4002 68.17 0.3599 0.6912 0.0605 0.0315 8.114 51.142 30.854 6050.693 5.778 137.238 2.313 0.80 372679. 0.3769 72.71 0.3839 0.7145 0.0567 0.0305 7.847 49.460 28.918 5851.659 5.588 128.628 2.241 0.80 373307. 0.3536 77.26 0.4079 0.7352 0.0528 0.0293 7.539 47.518 26.905 5621.912 5.369 119.676 2.171 0.80 373964. 0.3303 81.80 0.4319 0.7531 0.0487 0.0279 7.190 45.319 24.825 5361.774 5.120 110.420 2.100 0.80 374649. 0.3070 86.35 0.4559 0.7679 0.0445 0.0264 6.801 42.868 22.684 5071.793 4.843 100.898 2.029 0.80 375363. 0.2835 90.89 0.4799 0.7792 0.0402 0.0248 6.374 40.174 20.491 4753.023 4.539 91.146 1.955 0.80 376106. 0.2597 95.44 0.5039 0.7862 0.0358 0.0229 5.909 37.246 18.256 4406.648 4.208 81.202 1.879 0.80 376877. 0.2355 99.98 0.5279 0.7877 0.0314 0.0210 5.410 34.099 15.985 4034.280 3.852 71.103 1.797 0.80 377677. 0.2108 104.53 0.5519 0.7821 0.0268 0.0189 4.879 30.749 13.689 3638.021 3.474 60.889 1.707 0.81 378505. 0.1853 109.07 0.5759 0.7662 0.0223 0.0168 4.319 27.220 11.377 3220.448 3.075 50.607 1.602 0.81 379363. 0.1586 113.61 0.5999 0.7351 0.0178 0.0145 3.734 23.537 9.061 2784.713 2.659 40.303 1.476 0.81 380250. 0.1303 118.16 0.6239 0.6795 0.0132 0.0122 3.131 19.733 6.752 2334.650 2.229 30.032 1.312 0.81 381166. 0.1000 122.70 0.6479 0.5810 0.0088 0.0098 2.514 15.846 4.464 1874.755 1.790 19.856 1.080 0.81 382111. 0.0669 127.25 0.6719 0.3969 0.0043 0.0073 1.891 11.919 2.212 1410.152 1.347 9.840 0.712 0.81 383084. 0.0310 131.79 0.6959 0.0009 0.0000 0.0049 1.265 7.974 0.003 943.380 0.901 0.014 0.002 0.81 384064. 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 0.0974 0.0380 13.034 74.684 60.065 9719.603 8.438 267.170 2.803 0.87 403101. 0.6373 5.01 0.0240 0.0605 0.0962 0.0383 13.113 75.133 59.365 9778.066 8.489 264.055 2.754 0.87 403363. 0.6225 10.02 0.0481 0.1188 0.0950 0.0384 13.176 75.497 58.583 9825.406 8.530 260.577 2.704 0.87 403650. 0.6073 15.02 0.0721 0.1749 0.0935 0.0386 13.222 75.759 57.714 9859.558 8.559 256.711 2.655 0.87 403962. 0.5918 20.03 0.0962 0.2288 0.0920 0.0387 13.247 75.906 56.751 9878.604 8.576 252.427 2.606 0.87 404299. 0.5759 25.04 0.1202 0.2806 0.0903 0.0387 13.250 75.921 55.687 9880.608 8.578 247.697 2.556 0.87 404664. 0.5597 30.05 0.1442 0.3303 0.0884 0.0386 13.227 75.791 54.518 9863.611 8.563 242.494 2.507 0.87 405056. 0.5431 35.06 0.1683 0.3777 0.0863 0.0384 13.176 75.499 53.236 9825.665 8.530 236.794 2.457 0.87 405477. 0.5260 40.07 0.1923 0.4229 0.0840 0.0382 13.095 75.031 51.838 9764.766 8.477 230.575 2.408 0.87 405927. 0.5086 45.07 0.2164 0.4660 0.0816 0.0379 12.980 74.371 50.319 9678.871 8.402 223.818 2.358 0.87 406407. 0.4907 50.08 0.2404 0.5067 0.0789 0.0374 12.828 73.503 48.675 9565.876 8.304 216.508 2.308 0.88 406917. 0.4724 55.09 0.2644 0.5452 0.0760 0.0369 12.637 72.410 46.905 9423.641 8.181 208.633 2.258 0.88 407458. 0.4536 60.10 0.2885 0.5814 0.0729 0.0362 12.404 71.075 45.006 9249.933 8.030 200.185 2.207 0.88 408030. 0.4343 65.11 0.3125 0.6153 0.0697 0.0354 12.126 69.479 42.975 9042.242 7.850 191.152 2.156 0.88 408633. 0.4146 70.11 0.3366 0.6467 0.0661 0.0344 11.799 67.604 40.812 8798.169 7.638 181.531 2.104 0.88 409267. 0.3943 75.12 0.3606 0.6757 0.0624 0.0333 11.421 65.441 38.524 8516.642 7.393 171.357 2.052 0.88 409933. 0.3736 80.13 0.3846 0.7020 0.0586 0.0321 10.996 63.004 36.124 8199.563 7.118 160.681 1.998 0.88 410630. 0.3524 85.14 0.4087 0.7249 0.0545 0.0307 10.530 60.336 33.623 7852.309 6.817 149.554 1.942 0.88 411358. 0.3304 90.15 0.4327 0.7441 0.0503 0.0292 10.024 57.439 31.031 7475.233 6.489 138.026 1.883 0.88 412118. 0.3077 95.16 0.4567 0.7591 0.0460 0.0277 9.480 54.318 28.360 7069.060 6.137 126.145 1.820 0.88 412909. 0.2843 100.16 0.4808 0.7680 0.0415 0.0260 8.909 51.048 25.619 6643.542 5.767 113.954 1.749 0.88 413731. 0.2597 105.17 0.5048 0.7704 0.0370 0.0242 8.307 47.599 22.820 6194.741 5.378 101.504 1.671 0.88 414585. 0.2342 110.18 0.5289 0.7651 0.0324 0.0224 7.670 43.950 19.976 5719.817 4.965 88.852 1.584 0.88 415470. 0.2077 115.19 0.5529 0.7498 0.0277 0.0204 7.004 40.134 17.098 5223.150 4.534 76.051 1.485 0.89 416386. 0.1801 120.20 0.5769 0.7205 0.0230 0.0184 6.317 36.194 14.199 4710.444 4.089 63.158 1.367 0.89 417335. 0.1512 125.20 0.6010 0.6715 0.0183 0.0164 5.616 32.177 11.295 4187.556 3.635 50.239 1.223 0.89 418314. 0.1206 130.21 0.6250 0.5942 0.0136 0.0143 4.909 28.130 8.401 3660.890 3.178 37.367 1.041 0.89 419326. 0.0885 135.22 0.6491 0.4744 0.0090 0.0123 4.208 24.109 5.536 3137.593 2.724 24.625 0.800 0.89 420370. 0.0552 140.23 0.6731 0.2891 0.0044 0.0103 3.520 20.168 2.722 2624.672 2.279 12.106 0.470 0.89 421445. 0.0228 145.24 0.6971 -0.0051 -0.0001 0.0083 2.844 16.297 -0.037 2120.902 1.841 -0.166 -0.008 0.89 422533. 0.0000 PROP RPM = 12000 V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM (mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - - 0.00 0.0000 0.0000 0.0970 0.0455 20.240 106.306 71.189 15092.655 12.010 316.647 2.139 0.95 439754. 0.5296 5.58 0.0246 0.0515 0.0960 0.0458 20.370 106.990 70.497 15189.873 12.088 313.570 2.105 0.95 440039. 0.5185 11.16 0.0491 0.1013 0.0949 0.0460 20.473 107.531 69.711 15266.578 12.149 310.073 2.071 0.95 440351. 0.5073 16.74 0.0737 0.1496 0.0937 0.0462 20.541 107.888 68.819 15317.301 12.189 306.109 2.038 0.95 440692. 0.4960 22.32 0.0982 0.1962 0.0924 0.0462 20.567 108.023 67.812 15336.521 12.204 301.628 2.006 0.95 441063. 0.4845 27.90 0.1228 0.2415 0.0908 0.0462 20.543 107.900 66.677 15318.953 12.190 296.578 1.974 0.95 441465. 0.4729 33.48 0.1473 0.2853 0.0891 0.0460 20.464 107.482 65.403 15259.724 12.143 290.911 1.944 0.95 441901. 0.4612 39.06 0.1719 0.3279 0.0871 0.0457 20.323 106.742 63.980 15154.674 12.060 284.583 1.915 0.95 442370. 0.4494 44.64 0.1964 0.3693 0.0850 0.0452 20.116 105.657 62.399 15000.569 11.937 277.552 1.887 0.95 442873. 0.4373 50.22 0.2210 0.4094 0.0826 0.0446 19.840 104.209 60.653 14795.019 11.773 269.786 1.859 0.95 443412. 0.4249 55.80 0.2455 0.4483 0.0800 0.0438 19.494 102.388 58.736 14536.509 11.568 261.258 1.833 0.95 443987. 0.4121 61.38 0.2701 0.4860 0.0771 0.0429 19.075 100.188 56.643 14224.099 11.319 251.948 1.806 0.96 444597. 0.3988 66.96 0.2946 0.5224 0.0741 0.0418 18.583 97.605 54.371 13857.316 11.027 241.842 1.780 0.96 445244. 0.3850 72.54 0.3192 0.5574 0.0707 0.0405 18.018 94.636 51.917 13435.801 10.692 230.927 1.753 0.96 445926. 0.3705 78.12 0.3437 0.5907 0.0671 0.0391 17.379 91.281 49.281 12959.590 10.313 219.204 1.725 0.96 446645. 0.3552 83.70 0.3683 0.6223 0.0633 0.0375 16.670 87.558 46.476 12430.962 9.892 206.727 1.696 0.96 447401. 0.3392 89.28 0.3929 0.6518 0.0593 0.0357 15.895 83.489 43.518 11853.221 9.432 193.570 1.665 0.96 448192. 0.3223 94.86 0.4174 0.6783 0.0551 0.0339 15.076 79.187 40.424 11242.446 8.946 179.808 1.631 0.96 449019. 0.3042 100.44 0.4420 0.7003 0.0507 0.0320 14.232 74.751 37.209 10612.764 8.445 165.505 1.590 0.96 449882. 0.2846 106.02 0.4665 0.7168 0.0462 0.0300 13.366 70.202 33.888 9966.830 7.931 150.733 1.542 0.96 450780. 0.2634 111.61 0.4911 0.7248 0.0415 0.0281 12.513 65.722 30.475 9330.859 7.425 135.551 1.481 0.96 451713. 0.2399 117.19 0.5156 0.7137 0.0367 0.0265 11.809 62.026 26.971 8806.037 7.008 119.966 1.389 0.96 452682. 0.2117 122.77 0.5402 0.6904 0.0319 0.0250 11.103 58.316 23.415 8279.377 6.589 104.150 1.283 0.97 453687. 0.1821 128.35 0.5647 0.6532 0.0270 0.0234 10.390 54.574 19.830 7748.074 6.166 88.205 1.161 0.97 454727. 0.1517 133.93 0.5893 0.5990 0.0221 0.0218 9.682 50.853 16.240 7219.746 5.745 72.237 1.020 0.97 455803. 0.1206 139.51 0.6138 0.5245 0.0173 0.0202 8.988 47.206 12.673 6702.077 5.333 56.369 0.858 0.97 456915. 0.0896 145.09 0.6384 0.4260 0.0125 0.0187 8.318 43.690 9.160 6202.797 4.936 40.742 0.670 0.97 458063. 0.0595 150.67 0.6629 0.3000 0.0078 0.0173 7.678 40.329 5.733 5725.717 4.556 25.500 0.454 0.97 459249. 0.0319 156.25 0.6875 0.1424 0.0033 0.0159 7.070 37.135 2.417 5272.233 4.196 10.751 0.208 0.97 460478. 0.0095 161.83 0.7120