19x12WE (19x12WE.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 0.1024 0.0420 0.008 0.527 0.425 6.240 0.060 1.893 30.927 0.08 36376. 0.6230 0.48 0.0268 0.0637 0.1012 0.0426 0.008 0.535 0.420 6.330 0.060 1.869 30.100 0.08 36404. 0.6025 0.96 0.0536 0.1238 0.0997 0.0432 0.009 0.542 0.414 6.418 0.061 1.842 29.272 0.08 36434. 0.5818 1.45 0.0804 0.1805 0.0982 0.0437 0.009 0.549 0.408 6.500 0.062 1.814 28.449 0.08 36466. 0.5610 1.93 0.1073 0.2338 0.0965 0.0443 0.009 0.556 0.401 6.577 0.063 1.782 27.632 0.08 36502. 0.5401 2.41 0.1341 0.2837 0.0946 0.0447 0.009 0.562 0.393 6.644 0.063 1.748 26.824 0.08 36541. 0.5193 2.89 0.1609 0.3303 0.0926 0.0451 0.009 0.566 0.385 6.701 0.064 1.710 26.027 0.08 36583. 0.4984 3.38 0.1877 0.3737 0.0904 0.0454 0.009 0.570 0.375 6.745 0.064 1.670 25.244 0.08 36628. 0.4777 3.86 0.2145 0.4141 0.0880 0.0456 0.009 0.573 0.366 6.774 0.065 1.626 24.474 0.08 36676. 0.4569 4.34 0.2413 0.4515 0.0854 0.0457 0.009 0.573 0.355 6.785 0.065 1.578 23.718 0.08 36728. 0.4363 4.82 0.2681 0.4860 0.0827 0.0456 0.009 0.573 0.343 6.776 0.065 1.527 22.977 0.08 36784. 0.4157 5.31 0.2950 0.5176 0.0797 0.0454 0.009 0.570 0.331 6.746 0.064 1.472 22.248 0.08 36843. 0.3952 5.79 0.3218 0.5465 0.0765 0.0450 0.009 0.566 0.318 6.691 0.064 1.413 21.532 0.08 36905. 0.3748 6.27 0.3486 0.5726 0.0731 0.0445 0.009 0.559 0.304 6.611 0.063 1.350 20.824 0.08 36972. 0.3543 6.75 0.3754 0.5958 0.0695 0.0438 0.009 0.550 0.288 6.503 0.062 1.283 20.122 0.08 37041. 0.3338 7.24 0.4022 0.6162 0.0656 0.0428 0.009 0.538 0.273 6.366 0.061 1.213 19.422 0.08 37115. 0.3132 7.72 0.4290 0.6334 0.0616 0.0417 0.008 0.524 0.256 6.200 0.059 1.138 18.717 0.08 37192. 0.2924 8.20 0.4559 0.6473 0.0574 0.0404 0.008 0.507 0.238 6.003 0.057 1.060 18.002 0.08 37273. 0.2714 8.68 0.4827 0.6575 0.0530 0.0389 0.008 0.488 0.220 5.778 0.055 0.978 17.269 0.08 37358. 0.2501 9.17 0.5095 0.6635 0.0484 0.0372 0.007 0.467 0.201 5.525 0.053 0.895 16.509 0.08 37446. 0.2286 9.65 0.5363 0.6646 0.0438 0.0353 0.007 0.444 0.182 5.247 0.050 0.808 15.710 0.08 37538. 0.2068 10.13 0.5631 0.6599 0.0390 0.0333 0.007 0.418 0.162 4.945 0.047 0.720 14.856 0.08 37634. 0.1846 10.61 0.5899 0.6481 0.0342 0.0311 0.006 0.390 0.142 4.620 0.044 0.631 13.928 0.08 37733. 0.1620 11.10 0.6167 0.6275 0.0293 0.0288 0.006 0.361 0.122 4.273 0.041 0.540 12.899 0.08 37836. 0.1389 11.58 0.6436 0.5955 0.0243 0.0263 0.005 0.330 0.101 3.905 0.037 0.449 11.731 0.08 37943. 0.1151 12.06 0.6704 0.5482 0.0194 0.0237 0.005 0.297 0.080 3.519 0.034 0.358 10.368 0.08 38054. 0.0908 12.54 0.6972 0.4797 0.0144 0.0210 0.004 0.263 0.060 3.117 0.030 0.267 8.722 0.08 38168. 0.0659 13.03 0.7240 0.3799 0.0095 0.0182 0.004 0.228 0.040 2.700 0.026 0.176 6.652 0.08 38285. 0.0409 13.51 0.7508 0.2313 0.0047 0.0153 0.003 0.192 0.020 2.272 0.022 0.087 3.906 0.08 38407. 0.0169 13.99 0.7776 -0.0005 0.0000 0.0124 0.002 0.155 0.000 1.836 0.018 0.000 -0.009 0.08 38531. 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 0.1028 0.0392 0.062 1.970 1.708 46.606 0.223 7.598 16.623 0.15 72751. 0.6709 0.97 0.0269 0.0686 0.1015 0.0399 0.064 2.002 1.687 47.380 0.226 7.502 16.146 0.15 72806. 0.6476 1.94 0.0539 0.1332 0.1001 0.0405 0.065 2.034 1.663 48.132 0.230 7.397 15.671 0.15 72867. 0.6241 2.91 0.0808 0.1938 0.0986 0.0411 0.066 2.064 1.637 48.849 0.233 7.282 15.201 0.15 72933. 0.6007 3.88 0.1077 0.2505 0.0968 0.0417 0.066 2.093 1.609 49.515 0.236 7.156 14.738 0.15 73004. 0.5773 4.85 0.1347 0.3035 0.0950 0.0422 0.067 2.118 1.578 50.112 0.239 7.019 14.282 0.15 73082. 0.5541 5.82 0.1616 0.3528 0.0930 0.0426 0.068 2.139 1.544 50.624 0.242 6.869 13.836 0.15 73167. 0.5310 6.79 0.1886 0.3986 0.0907 0.0429 0.068 2.157 1.508 51.031 0.244 6.706 13.399 0.15 73258. 0.5081 7.75 0.2155 0.4411 0.0884 0.0432 0.069 2.169 1.468 51.315 0.245 6.529 12.974 0.15 73355. 0.4854 8.72 0.2424 0.4803 0.0858 0.0433 0.069 2.175 1.425 51.455 0.246 6.337 12.559 0.15 73460. 0.4629 9.69 0.2694 0.5165 0.0830 0.0433 0.069 2.174 1.378 51.432 0.246 6.130 12.155 0.15 73572. 0.4407 10.66 0.2963 0.5498 0.0800 0.0431 0.069 2.165 1.328 51.227 0.245 5.908 11.761 0.15 73691. 0.4186 11.63 0.3232 0.5802 0.0767 0.0428 0.068 2.148 1.275 50.823 0.243 5.671 11.378 0.15 73817. 0.3967 12.60 0.3502 0.6078 0.0733 0.0422 0.067 2.122 1.218 50.205 0.240 5.417 11.002 0.15 73951. 0.3750 13.57 0.3771 0.6327 0.0697 0.0415 0.066 2.086 1.157 49.360 0.236 5.148 10.634 0.15 74092. 0.3533 14.54 0.4041 0.6547 0.0658 0.0406 0.065 2.040 1.093 48.274 0.230 4.862 10.271 0.15 74240. 0.3316 15.51 0.4310 0.6738 0.0617 0.0395 0.063 1.983 1.025 46.934 0.224 4.561 9.910 0.15 74396. 0.3099 16.48 0.4579 0.6898 0.0575 0.0381 0.061 1.916 0.954 45.339 0.216 4.246 9.549 0.15 74559. 0.2881 17.45 0.4849 0.7024 0.0530 0.0366 0.058 1.838 0.881 43.503 0.208 3.918 9.183 0.15 74730. 0.2662 18.42 0.5118 0.7113 0.0484 0.0349 0.056 1.751 0.805 41.436 0.198 3.580 8.809 0.15 74908. 0.2441 19.39 0.5387 0.7157 0.0438 0.0329 0.052 1.654 0.727 39.149 0.187 3.233 8.421 0.15 75094. 0.2217 20.36 0.5657 0.7148 0.0390 0.0308 0.049 1.549 0.647 36.651 0.175 2.879 8.010 0.15 75287. 0.1990 21.33 0.5926 0.7075 0.0341 0.0286 0.046 1.435 0.566 33.952 0.162 2.520 7.568 0.15 75487. 0.1759 22.29 0.6196 0.6919 0.0292 0.0261 0.042 1.313 0.485 31.063 0.148 2.156 7.079 0.15 75695. 0.1522 23.26 0.6465 0.6652 0.0242 0.0236 0.038 1.183 0.403 27.996 0.134 1.791 6.523 0.15 75910. 0.1278 24.23 0.6734 0.6231 0.0193 0.0208 0.033 1.047 0.320 24.767 0.118 1.425 5.865 0.15 76133. 0.1025 25.20 0.7004 0.5582 0.0143 0.0180 0.029 0.904 0.238 21.394 0.102 1.060 5.052 0.15 76363. 0.0762 26.17 0.7273 0.4569 0.0095 0.0151 0.024 0.756 0.157 17.898 0.085 0.699 3.982 0.15 76600. 0.0487 27.14 0.7542 0.2918 0.0047 0.0120 0.019 0.605 0.077 14.304 0.068 0.344 2.452 0.16 76845. 0.0211 28.11 0.7812 -0.0033 0.0000 0.0089 0.014 0.450 -0.001 10.637 0.051 -0.003 -0.026 0.16 77095. 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 0.1032 0.0381 0.205 4.306 3.858 152.818 0.486 17.159 11.450 0.23 109124. 0.6945 1.46 0.0270 0.0709 0.1019 0.0388 0.209 4.382 3.810 155.517 0.495 16.945 11.111 0.23 109207. 0.6697 2.91 0.0540 0.1376 0.1005 0.0394 0.212 4.456 3.757 158.147 0.503 16.710 10.774 0.23 109298. 0.6449 4.37 0.0810 0.2000 0.0990 0.0400 0.215 4.526 3.699 160.659 0.511 16.452 10.442 0.23 109397. 0.6202 5.83 0.1079 0.2584 0.0973 0.0406 0.219 4.592 3.635 162.999 0.519 16.169 10.115 0.23 109505. 0.5956 7.28 0.1349 0.3127 0.0954 0.0412 0.221 4.652 3.566 165.110 0.526 15.860 9.795 0.23 109622. 0.5712 8.74 0.1619 0.3633 0.0934 0.0416 0.224 4.703 3.490 166.931 0.531 15.522 9.482 0.23 109749. 0.5470 10.20 0.1889 0.4102 0.0912 0.0420 0.226 4.744 3.407 168.395 0.536 15.155 9.177 0.23 109886. 0.5231 11.65 0.2159 0.4536 0.0888 0.0422 0.227 4.774 3.317 169.437 0.539 14.755 8.880 0.23 110033. 0.4995 13.11 0.2429 0.4938 0.0862 0.0424 0.228 4.789 3.220 169.988 0.541 14.323 8.592 0.23 110191. 0.4761 14.56 0.2698 0.5308 0.0833 0.0424 0.228 4.789 3.115 169.980 0.541 13.857 8.313 0.23 110359. 0.4531 16.02 0.2968 0.5648 0.0803 0.0422 0.227 4.771 3.002 169.348 0.539 13.355 8.041 0.23 110538. 0.4303 17.48 0.3238 0.5960 0.0771 0.0419 0.225 4.734 2.882 168.033 0.535 12.817 7.778 0.23 110728. 0.4078 18.93 0.3508 0.6244 0.0736 0.0414 0.223 4.676 2.753 165.979 0.528 12.243 7.522 0.23 110929. 0.3854 20.39 0.3778 0.6500 0.0700 0.0407 0.219 4.596 2.615 163.141 0.519 11.634 7.272 0.23 111142. 0.3632 21.85 0.4048 0.6730 0.0661 0.0398 0.214 4.493 2.470 159.469 0.508 10.988 7.026 0.23 111365. 0.3410 23.30 0.4317 0.6931 0.0620 0.0386 0.208 4.365 2.317 154.916 0.493 10.306 6.784 0.23 111600. 0.3189 24.76 0.4587 0.7103 0.0577 0.0373 0.200 4.212 2.156 149.484 0.476 9.592 6.543 0.23 111845. 0.2967 26.22 0.4857 0.7243 0.0532 0.0357 0.192 4.035 1.990 143.209 0.456 8.850 6.302 0.23 112103. 0.2745 27.67 0.5127 0.7347 0.0486 0.0339 0.183 3.835 1.818 136.130 0.433 8.085 6.056 0.23 112371. 0.2522 29.13 0.5397 0.7411 0.0439 0.0320 0.172 3.614 1.641 128.279 0.408 7.300 5.803 0.23 112650. 0.2296 30.59 0.5667 0.7426 0.0391 0.0298 0.161 3.372 1.461 119.689 0.381 6.500 5.538 0.23 112941. 0.2067 32.04 0.5936 0.7380 0.0342 0.0275 0.148 3.110 1.279 110.394 0.351 5.687 5.253 0.23 113242. 0.1835 33.50 0.6206 0.7256 0.0293 0.0250 0.135 2.830 1.094 100.431 0.320 4.866 4.941 0.23 113555. 0.1596 34.96 0.6476 0.7027 0.0243 0.0224 0.120 2.531 0.908 89.843 0.286 4.040 4.585 0.23 113879. 0.1350 36.41 0.6746 0.6647 0.0193 0.0196 0.106 2.217 0.722 78.684 0.250 3.213 4.164 0.23 114214. 0.1093 37.87 0.7016 0.6037 0.0144 0.0167 0.090 1.888 0.537 67.017 0.213 2.390 3.636 0.23 114560. 0.0823 39.33 0.7286 0.5044 0.0095 0.0137 0.074 1.547 0.354 54.920 0.175 1.576 2.926 0.23 114917. 0.0538 40.78 0.7555 0.3330 0.0047 0.0106 0.057 1.197 0.174 42.481 0.135 0.776 1.862 0.23 115285. 0.0240 42.24 0.7825 -0.0033 0.0000 0.0074 0.040 0.839 -0.001 29.782 0.095 -0.005 -0.018 0.23 115660. 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 0.1037 0.0376 0.479 7.548 6.890 357.209 0.853 30.647 8.749 0.30 145494. 0.7092 1.94 0.0270 0.0723 0.1024 0.0383 0.488 7.687 6.805 363.763 0.868 30.269 8.485 0.30 145604. 0.6836 3.89 0.0540 0.1402 0.1010 0.0389 0.496 7.822 6.712 370.158 0.884 29.853 8.224 0.30 145726. 0.6580 5.83 0.0810 0.2036 0.0995 0.0396 0.505 7.951 6.609 376.272 0.898 29.396 7.967 0.30 145858. 0.6325 7.77 0.1080 0.2629 0.0978 0.0402 0.512 8.071 6.496 381.981 0.912 28.895 7.714 0.30 146003. 0.6072 9.72 0.1350 0.3181 0.0959 0.0407 0.519 8.181 6.373 387.144 0.924 28.346 7.466 0.30 146160. 0.5821 11.66 0.1620 0.3694 0.0939 0.0412 0.525 8.275 6.238 391.613 0.935 27.746 7.225 0.30 146329. 0.5573 13.61 0.1890 0.4169 0.0917 0.0416 0.530 8.351 6.091 395.232 0.944 27.093 6.990 0.30 146512. 0.5328 15.55 0.2161 0.4610 0.0893 0.0418 0.534 8.407 5.931 397.836 0.950 26.382 6.762 0.30 146709. 0.5086 17.49 0.2431 0.5016 0.0867 0.0420 0.535 8.437 5.758 399.260 0.953 25.611 6.541 0.30 146919. 0.4847 19.44 0.2701 0.5392 0.0838 0.0420 0.536 8.438 5.571 399.341 0.953 24.779 6.327 0.30 147144. 0.4612 21.38 0.2971 0.5737 0.0808 0.0418 0.534 8.408 5.370 397.920 0.950 23.884 6.121 0.30 147384. 0.4380 23.32 0.3241 0.6053 0.0776 0.0415 0.530 8.343 5.154 394.852 0.943 22.924 5.920 0.30 147638. 0.4151 25.27 0.3511 0.6343 0.0741 0.0410 0.523 8.241 4.923 390.005 0.931 21.899 5.726 0.30 147906. 0.3923 27.21 0.3781 0.6605 0.0704 0.0403 0.514 8.099 4.678 383.262 0.915 20.809 5.536 0.30 148190. 0.3698 29.16 0.4051 0.6840 0.0665 0.0394 0.502 7.914 4.419 374.507 0.894 19.654 5.352 0.30 148489. 0.3474 31.10 0.4321 0.7048 0.0624 0.0382 0.488 7.684 4.145 363.621 0.868 18.435 5.170 0.30 148802. 0.3250 33.04 0.4591 0.7228 0.0580 0.0369 0.470 7.409 3.857 350.606 0.837 17.157 4.990 0.30 149131. 0.3026 34.99 0.4861 0.7378 0.0536 0.0353 0.450 7.090 3.559 335.548 0.801 15.829 4.810 0.31 149474. 0.2802 36.93 0.5131 0.7494 0.0489 0.0335 0.427 6.731 3.251 318.534 0.760 14.459 4.629 0.31 149833. 0.2577 38.87 0.5401 0.7571 0.0442 0.0315 0.402 6.332 2.935 299.643 0.715 13.055 4.443 0.31 150206. 0.2350 40.82 0.5671 0.7602 0.0393 0.0293 0.374 5.894 2.613 278.952 0.666 11.622 4.249 0.31 150594. 0.2121 42.76 0.5942 0.7577 0.0344 0.0270 0.344 5.421 2.286 256.542 0.612 10.168 4.042 0.31 150997. 0.1887 44.70 0.6212 0.7477 0.0294 0.0244 0.312 4.913 1.956 232.502 0.555 8.698 3.815 0.31 151415. 0.1648 46.65 0.6482 0.7276 0.0244 0.0218 0.278 4.373 1.623 206.939 0.494 7.220 3.558 0.31 151847. 0.1400 48.59 0.6752 0.6929 0.0194 0.0189 0.241 3.803 1.291 179.983 0.430 5.741 3.253 0.31 152295. 0.1141 50.54 0.7022 0.6354 0.0144 0.0160 0.204 3.207 0.960 151.788 0.362 4.269 2.868 0.31 152757. 0.0868 52.48 0.7292 0.5386 0.0095 0.0129 0.164 2.589 0.633 122.544 0.293 2.814 2.341 0.31 153234. 0.0575 54.42 0.7562 0.3642 0.0047 0.0097 0.124 1.954 0.311 92.473 0.221 1.384 1.526 0.31 153726. 0.0263 56.37 0.7832 -0.0047 0.0000 0.0065 0.083 1.305 -0.003 61.761 0.147 -0.011 -0.019 0.31 154226. 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 0.1043 0.0374 0.930 11.728 10.828 693.771 1.325 48.162 7.079 0.38 181859. 0.7194 2.43 0.0270 0.0731 0.1030 0.0381 0.948 11.949 10.696 706.844 1.350 47.577 6.864 0.38 181997. 0.6932 4.86 0.0540 0.1417 0.1016 0.0387 0.965 12.165 10.551 719.613 1.374 46.933 6.651 0.38 182149. 0.6672 7.29 0.0810 0.2058 0.1001 0.0394 0.981 12.371 10.392 731.836 1.398 46.224 6.441 0.38 182315. 0.6412 9.72 0.1080 0.2656 0.0984 0.0400 0.997 12.565 10.217 743.264 1.420 45.444 6.235 0.38 182496. 0.6154 12.15 0.1350 0.3213 0.0966 0.0406 1.011 12.740 10.025 753.620 1.439 44.590 6.033 0.38 182692. 0.5899 14.58 0.1620 0.3730 0.0945 0.0411 1.023 12.891 9.814 762.608 1.456 43.655 5.837 0.38 182905. 0.5647 17.01 0.1890 0.4210 0.0923 0.0415 1.032 13.015 9.585 769.916 1.470 42.634 5.647 0.38 183134. 0.5399 19.44 0.2161 0.4654 0.0899 0.0417 1.040 13.105 9.335 775.219 1.481 41.523 5.462 0.38 183380. 0.5154 21.87 0.2431 0.5064 0.0873 0.0419 1.044 13.155 9.064 778.188 1.486 40.318 5.283 0.38 183643. 0.4912 24.30 0.2701 0.5443 0.0845 0.0419 1.044 13.160 8.771 778.496 1.487 39.015 5.110 0.38 183925. 0.4674 26.73 0.2971 0.5792 0.0814 0.0418 1.040 13.115 8.456 775.827 1.482 37.611 4.944 0.38 184225. 0.4439 29.15 0.3241 0.6112 0.0782 0.0415 1.032 13.015 8.117 769.890 1.470 36.105 4.782 0.38 184543. 0.4208 31.58 0.3511 0.6405 0.0747 0.0409 1.020 12.855 7.755 760.421 1.452 34.496 4.626 0.38 184879. 0.3978 34.01 0.3781 0.6672 0.0710 0.0402 1.002 12.631 7.371 747.189 1.427 32.784 4.474 0.38 185234. 0.3751 36.44 0.4051 0.6912 0.0671 0.0393 0.979 12.340 6.963 729.963 1.394 30.970 4.326 0.38 185608. 0.3525 38.87 0.4321 0.7126 0.0629 0.0381 0.950 11.977 6.531 708.503 1.353 29.052 4.181 0.38 186000. 0.3300 41.30 0.4591 0.7312 0.0586 0.0368 0.916 11.542 6.079 682.801 1.304 27.041 4.038 0.38 186411. 0.3075 43.73 0.4861 0.7470 0.0540 0.0352 0.876 11.039 5.610 653.026 1.247 24.951 3.896 0.38 186841. 0.2850 46.16 0.5131 0.7595 0.0494 0.0333 0.831 10.470 5.125 619.346 1.183 22.795 3.753 0.38 187289. 0.2624 48.59 0.5401 0.7684 0.0446 0.0313 0.780 9.837 4.628 581.917 1.111 20.584 3.607 0.38 187756. 0.2396 51.02 0.5671 0.7728 0.0397 0.0291 0.725 9.143 4.120 540.890 1.033 18.328 3.455 0.38 188241. 0.2166 53.45 0.5941 0.7719 0.0347 0.0267 0.666 8.392 3.605 496.424 0.948 16.037 3.294 0.38 188745. 0.1932 55.88 0.6211 0.7639 0.0297 0.0242 0.602 7.585 3.085 448.698 0.857 13.722 3.118 0.38 189268. 0.1691 58.31 0.6482 0.7463 0.0247 0.0214 0.534 6.727 2.561 397.926 0.760 11.393 2.920 0.38 189809. 0.1443 60.74 0.6752 0.7146 0.0196 0.0185 0.462 5.821 2.038 344.364 0.658 9.063 2.684 0.39 190368. 0.1183 63.17 0.7022 0.6605 0.0146 0.0155 0.387 4.874 1.516 288.323 0.551 6.744 2.385 0.39 190946. 0.0907 65.60 0.7292 0.5670 0.0096 0.0124 0.309 3.891 1.001 230.183 0.440 4.451 1.972 0.39 191542. 0.0609 68.03 0.7562 0.3925 0.0048 0.0092 0.229 2.880 0.494 170.393 0.325 2.199 1.316 0.39 192157. 0.0286 70.46 0.7832 0.0003 0.0000 0.0059 0.147 1.848 0.000 109.312 0.209 0.001 0.001 0.39 192781. 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 0.1050 0.0374 1.608 16.892 15.701 1199.137 1.908 69.840 5.939 0.45 218218. 0.7268 2.92 0.0270 0.0736 0.1038 0.0381 1.639 17.218 15.515 1222.230 1.945 69.009 5.757 0.45 218384. 0.7003 5.83 0.0540 0.1426 0.1024 0.0388 1.669 17.536 15.308 1244.807 1.981 68.091 5.578 0.45 218567. 0.6740 8.75 0.0810 0.2072 0.1009 0.0395 1.698 17.840 15.081 1266.441 2.016 67.078 5.401 0.45 218766. 0.6477 11.67 0.1081 0.2673 0.0992 0.0401 1.725 18.126 14.830 1286.688 2.048 65.963 5.228 0.45 218984. 0.6217 14.58 0.1351 0.3234 0.0973 0.0407 1.750 18.384 14.554 1305.061 2.077 64.738 5.058 0.45 219220. 0.5960 17.50 0.1621 0.3754 0.0953 0.0412 1.772 18.610 14.252 1321.036 2.102 63.395 4.893 0.45 219475. 0.5705 20.41 0.1891 0.4236 0.0931 0.0416 1.789 18.793 13.922 1334.062 2.123 61.927 4.733 0.45 219751. 0.5454 23.33 0.2161 0.4683 0.0907 0.0419 1.802 18.927 13.563 1343.568 2.138 60.326 4.579 0.45 220047. 0.5207 26.25 0.2431 0.5096 0.0881 0.0420 1.809 19.003 13.172 1348.966 2.147 58.587 4.429 0.45 220364. 0.4964 29.16 0.2701 0.5477 0.0853 0.0421 1.810 19.013 12.748 1349.683 2.148 56.705 4.284 0.45 220703. 0.4724 32.08 0.2972 0.5829 0.0822 0.0419 1.804 18.949 12.292 1345.162 2.141 54.674 4.145 0.45 221063. 0.4488 35.00 0.3242 0.6152 0.0789 0.0416 1.790 18.805 11.802 1334.884 2.125 52.493 4.010 0.45 221446. 0.4254 37.91 0.3512 0.6448 0.0754 0.0411 1.768 18.572 11.277 1318.386 2.098 50.161 3.880 0.46 221850. 0.4024 40.83 0.3782 0.6718 0.0717 0.0404 1.737 18.246 10.719 1295.255 2.061 47.677 3.754 0.46 222277. 0.3795 43.74 0.4052 0.6963 0.0677 0.0394 1.697 17.821 10.127 1265.087 2.013 45.043 3.631 0.46 222726. 0.3568 46.66 0.4322 0.7181 0.0635 0.0382 1.646 17.291 9.500 1227.466 1.954 42.258 3.511 0.46 223198. 0.3342 49.58 0.4592 0.7373 0.0591 0.0368 1.586 16.656 8.843 1182.355 1.882 39.336 3.392 0.46 223692. 0.3116 52.49 0.4863 0.7537 0.0546 0.0352 1.515 15.919 8.160 1130.046 1.799 36.297 3.275 0.46 224209. 0.2889 55.41 0.5133 0.7671 0.0499 0.0334 1.436 15.085 7.455 1070.837 1.704 33.160 3.158 0.46 224748. 0.2663 58.33 0.5403 0.7768 0.0450 0.0313 1.348 14.157 6.732 1004.998 1.600 29.942 3.038 0.46 225309. 0.2434 61.24 0.5673 0.7824 0.0401 0.0291 1.251 13.140 5.993 932.797 1.485 26.658 2.914 0.46 225892. 0.2203 64.16 0.5943 0.7828 0.0351 0.0266 1.146 12.038 5.243 854.512 1.360 23.323 2.783 0.46 226497. 0.1968 67.08 0.6213 0.7765 0.0300 0.0240 1.033 10.854 4.486 770.461 1.226 19.952 2.641 0.46 227125. 0.1727 69.99 0.6483 0.7608 0.0249 0.0212 0.913 9.594 3.723 681.021 1.084 16.560 2.480 0.46 227774. 0.1478 72.91 0.6754 0.7315 0.0198 0.0183 0.787 8.264 2.960 586.647 0.934 13.166 2.289 0.46 228446. 0.1216 75.82 0.7024 0.6800 0.0147 0.0152 0.654 6.873 2.201 487.893 0.777 9.788 2.046 0.46 229140. 0.0937 78.74 0.7294 0.5889 0.0097 0.0120 0.517 5.430 1.450 385.433 0.613 6.448 1.706 0.46 229856. 0.0634 81.66 0.7564 0.4131 0.0048 0.0087 0.376 3.945 0.712 280.072 0.446 3.169 1.154 0.47 230594. 0.0301 84.57 0.7834 -0.0073 0.0000 0.0054 0.231 2.429 -0.007 172.401 0.274 -0.033 -0.020 0.47 231342. 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 0.1059 0.0376 2.566 23.108 21.551 1913.775 2.611 95.860 5.108 0.53 254569. 0.7323 3.40 0.0270 0.0739 0.1047 0.0383 2.617 23.562 21.301 1951.358 2.662 94.749 4.951 0.53 254764. 0.7057 6.81 0.0540 0.1431 0.1033 0.0390 2.666 24.006 21.024 1988.128 2.712 93.516 4.796 0.53 254977. 0.6792 10.21 0.0811 0.2079 0.1018 0.0397 2.713 24.432 20.718 2023.399 2.760 92.154 4.644 0.53 255210. 0.6528 13.61 0.1081 0.2683 0.1001 0.0404 2.758 24.831 20.380 2056.440 2.805 90.650 4.495 0.53 255465. 0.6267 17.02 0.1351 0.3244 0.0983 0.0409 2.798 25.193 20.007 2086.460 2.846 88.993 4.349 0.53 255741. 0.6008 20.42 0.1621 0.3767 0.0963 0.0415 2.833 25.509 19.598 2112.604 2.882 87.172 4.208 0.53 256040. 0.5753 23.82 0.1891 0.4251 0.0941 0.0419 2.862 25.767 19.150 2133.971 2.911 85.178 4.070 0.53 256362. 0.5501 27.23 0.2162 0.4699 0.0917 0.0422 2.883 25.956 18.660 2149.627 2.932 82.999 3.937 0.53 256708. 0.5252 30.63 0.2432 0.5114 0.0891 0.0424 2.895 26.065 18.127 2158.627 2.945 80.628 3.809 0.53 257079. 0.5008 34.03 0.2702 0.5498 0.0862 0.0424 2.897 26.082 17.549 2160.027 2.947 78.056 3.685 0.53 257475. 0.4767 37.44 0.2972 0.5851 0.0832 0.0422 2.887 25.996 16.924 2152.925 2.937 75.278 3.565 0.53 257897. 0.4530 40.84 0.3242 0.6177 0.0799 0.0419 2.865 25.797 16.252 2136.471 2.915 72.290 3.450 0.53 258344. 0.4296 44.24 0.3513 0.6476 0.0763 0.0414 2.829 25.476 15.533 2109.916 2.878 69.091 3.339 0.53 258818. 0.4064 47.64 0.3783 0.6750 0.0726 0.0407 2.779 25.026 14.766 2072.590 2.827 65.681 3.231 0.53 259317. 0.3835 51.05 0.4053 0.6998 0.0686 0.0397 2.714 24.437 13.953 2023.847 2.761 62.061 3.127 0.53 259842. 0.3607 54.45 0.4323 0.7221 0.0643 0.0385 2.632 23.703 13.091 1963.008 2.678 58.230 3.025 0.53 260394. 0.3380 57.85 0.4594 0.7418 0.0599 0.0371 2.535 22.821 12.187 1889.992 2.578 54.207 2.925 0.53 260972. 0.3153 61.26 0.4864 0.7588 0.0553 0.0354 2.421 21.798 11.246 1805.262 2.463 50.022 2.826 0.53 261575. 0.2926 64.66 0.5134 0.7728 0.0505 0.0335 2.292 20.639 10.274 1709.303 2.332 45.699 2.726 0.53 262205. 0.2699 68.06 0.5404 0.7834 0.0456 0.0314 2.149 19.350 9.276 1602.556 2.186 41.262 2.626 0.54 262860. 0.2470 71.47 0.5674 0.7900 0.0406 0.0291 1.992 17.936 8.258 1485.452 2.026 36.732 2.522 0.54 263542. 0.2238 74.87 0.5945 0.7916 0.0355 0.0267 1.822 16.403 7.223 1358.452 1.853 32.129 2.412 0.54 264249. 0.2002 78.27 0.6215 0.7867 0.0304 0.0240 1.639 14.756 6.177 1222.068 1.667 27.476 2.293 0.54 264982. 0.1760 81.68 0.6485 0.7728 0.0252 0.0211 1.444 13.003 5.124 1076.916 1.469 22.793 2.158 0.54 265740. 0.1509 85.08 0.6755 0.7455 0.0200 0.0181 1.239 11.154 4.071 923.738 1.260 18.106 1.999 0.54 266525. 0.1245 88.48 0.7025 0.6964 0.0148 0.0150 1.024 9.218 3.022 763.445 1.041 13.440 1.795 0.54 267335. 0.0964 91.89 0.7296 0.6072 0.0098 0.0117 0.801 7.210 1.984 597.143 0.815 8.827 1.507 0.54 268171. 0.0656 95.29 0.7566 0.4297 0.0047 0.0084 0.571 5.146 0.966 426.151 0.581 4.298 1.029 0.54 269032. 0.0312 98.69 0.7836 -0.0223 -0.0001 0.0049 0.337 3.035 -0.028 251.328 0.343 -0.127 -0.051 0.54 269902. 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 0.1070 0.0379 3.867 30.466 28.429 2883.590 3.442 126.450 4.472 0.60 290911. 0.7363 3.88 0.0270 0.0738 0.1058 0.0387 3.944 31.075 28.110 2941.198 3.511 125.035 4.335 0.60 291133. 0.7098 7.77 0.0540 0.1430 0.1044 0.0394 4.020 31.671 27.757 2997.635 3.578 123.461 4.200 0.60 291377. 0.6833 11.65 0.0809 0.2077 0.1029 0.0401 4.093 32.244 27.364 3051.834 3.643 121.715 4.067 0.60 291643. 0.6570 15.53 0.1079 0.2680 0.1013 0.0408 4.161 32.781 26.929 3102.676 3.704 119.780 3.937 0.60 291934. 0.6309 19.41 0.1349 0.3242 0.0995 0.0414 4.223 33.270 26.448 3148.943 3.759 117.642 3.810 0.60 292249. 0.6050 23.30 0.1619 0.3765 0.0975 0.0419 4.277 33.696 25.919 3189.330 3.807 115.286 3.686 0.60 292591. 0.5795 27.18 0.1888 0.4249 0.0953 0.0424 4.321 34.046 25.337 3222.451 3.847 112.698 3.566 0.60 292960. 0.5544 31.06 0.2158 0.4699 0.0929 0.0427 4.354 34.304 24.700 3246.884 3.876 109.864 3.450 0.60 293356. 0.5296 34.95 0.2428 0.5115 0.0903 0.0429 4.373 34.455 24.004 3261.175 3.893 106.771 3.339 0.60 293780. 0.5051 38.83 0.2698 0.5500 0.0875 0.0429 4.377 34.484 23.249 3263.887 3.896 103.411 3.231 0.61 294233. 0.4811 42.71 0.2967 0.5855 0.0844 0.0428 4.363 34.376 22.431 3253.637 3.884 99.774 3.127 0.61 294715. 0.4574 46.60 0.3237 0.6183 0.0811 0.0424 4.330 34.117 21.550 3229.134 3.854 95.856 3.027 0.61 295226. 0.4340 50.48 0.3507 0.6485 0.0775 0.0419 4.277 33.695 20.606 3189.218 3.807 91.654 2.931 0.61 295767. 0.4108 54.36 0.3777 0.6762 0.0737 0.0412 4.201 33.100 19.597 3132.882 3.740 87.170 2.837 0.61 296337. 0.3879 58.24 0.4046 0.7014 0.0697 0.0402 4.102 32.321 18.526 3059.157 3.652 82.404 2.747 0.61 296937. 0.3651 62.13 0.4316 0.7241 0.0654 0.0390 3.979 31.347 17.391 2967.012 3.542 77.356 2.659 0.61 297567. 0.3424 66.01 0.4586 0.7443 0.0609 0.0375 3.830 30.177 16.198 2856.245 3.409 72.047 2.572 0.61 298227. 0.3197 69.89 0.4856 0.7620 0.0563 0.0359 3.658 28.817 14.954 2727.542 3.256 66.518 2.487 0.61 298916. 0.2970 73.78 0.5125 0.7767 0.0514 0.0339 3.462 27.276 13.669 2581.647 3.082 60.802 2.402 0.61 299634. 0.2742 77.66 0.5395 0.7883 0.0465 0.0318 3.244 25.560 12.349 2419.242 2.888 54.931 2.315 0.61 300382. 0.2513 81.54 0.5665 0.7959 0.0414 0.0295 3.005 23.677 11.001 2240.988 2.675 48.932 2.227 0.61 301159. 0.2281 85.42 0.5935 0.7989 0.0362 0.0269 2.746 21.633 9.630 2047.580 2.444 42.834 2.133 0.61 301966. 0.2044 89.31 0.6204 0.7956 0.0310 0.0242 2.467 19.438 8.243 1839.808 2.196 36.663 2.032 0.61 302802. 0.1802 93.19 0.6474 0.7838 0.0258 0.0213 2.171 17.101 6.846 1618.604 1.932 30.451 1.918 0.62 303667. 0.1550 97.07 0.6744 0.7591 0.0205 0.0182 1.857 14.634 5.447 1385.096 1.653 24.229 1.784 0.62 304561. 0.1286 100.96 0.7014 0.7135 0.0153 0.0150 1.530 12.051 4.054 1140.667 1.362 18.034 1.612 0.62 305485. 0.1002 104.84 0.7284 0.6289 0.0101 0.0117 1.189 9.372 2.676 887.009 1.059 11.904 1.368 0.62 306438. 0.0691 108.72 0.7553 0.4567 0.0050 0.0082 0.840 6.615 1.323 626.142 0.747 5.884 0.958 0.62 307419. 0.0340 112.60 0.7823 0.0004 0.0000 0.0047 0.482 3.799 0.001 359.558 0.429 0.003 0.001 0.62 308413. 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 0.1082 0.0384 5.585 39.112 36.398 4164.679 4.419 161.898 3.964 0.68 327240. 0.7386 4.37 0.0270 0.0736 0.1070 0.0392 5.698 39.902 36.009 4248.761 4.508 160.168 3.844 0.68 327490. 0.7124 8.73 0.0539 0.1426 0.1058 0.0400 5.809 40.678 35.574 4331.412 4.596 158.235 3.725 0.68 327764. 0.6862 13.10 0.0809 0.2071 0.1043 0.0407 5.915 41.426 35.090 4411.048 4.680 156.079 3.608 0.68 328064. 0.6601 17.46 0.1078 0.2674 0.1027 0.0414 6.016 42.130 34.550 4485.978 4.760 153.680 3.493 0.68 328392. 0.6341 21.83 0.1348 0.3235 0.1009 0.0420 6.108 42.772 33.952 4554.372 4.832 151.016 3.381 0.68 328748. 0.6084 26.19 0.1617 0.3757 0.0990 0.0426 6.188 43.334 33.289 4614.247 4.896 148.069 3.272 0.68 329133. 0.5830 30.56 0.1887 0.4242 0.0968 0.0431 6.254 43.797 32.558 4663.508 4.948 144.818 3.167 0.68 329548. 0.5580 34.92 0.2157 0.4692 0.0944 0.0434 6.303 44.140 31.755 4700.049 4.987 141.246 3.064 0.68 329995. 0.5333 39.29 0.2426 0.5108 0.0918 0.0436 6.332 44.344 30.876 4721.728 5.010 137.336 2.966 0.68 330473. 0.5090 43.65 0.2696 0.5494 0.0889 0.0436 6.338 44.388 29.918 4726.430 5.015 133.075 2.871 0.68 330984. 0.4850 48.02 0.2965 0.5852 0.0858 0.0435 6.319 44.253 28.879 4712.123 5.000 128.452 2.780 0.68 331527. 0.4613 52.38 0.3235 0.6182 0.0825 0.0432 6.272 43.923 27.756 4676.906 4.962 123.461 2.692 0.68 332104. 0.4380 56.75 0.3504 0.6486 0.0789 0.0426 6.194 43.380 26.551 4619.095 4.901 118.097 2.607 0.68 332713. 0.4149 61.11 0.3774 0.6766 0.0751 0.0419 6.084 42.611 25.261 4537.205 4.814 112.362 2.525 0.68 333356. 0.3920 65.48 0.4044 0.7021 0.0710 0.0409 5.941 41.602 23.889 4429.858 4.700 106.259 2.446 0.68 334032. 0.3692 69.84 0.4313 0.7253 0.0667 0.0397 5.760 40.341 22.434 4295.561 4.558 99.786 2.369 0.68 334742. 0.3465 74.21 0.4583 0.7461 0.0621 0.0382 5.544 38.823 20.901 4133.938 4.386 92.969 2.293 0.69 335485. 0.3238 78.57 0.4852 0.7643 0.0574 0.0364 5.292 37.058 19.303 3945.964 4.187 85.860 2.219 0.69 336261. 0.3011 82.94 0.5122 0.7798 0.0525 0.0345 5.006 35.056 17.649 3732.740 3.961 78.503 2.145 0.69 337070. 0.2782 87.31 0.5391 0.7921 0.0474 0.0323 4.687 32.826 15.948 3495.287 3.709 70.939 2.070 0.69 337912. 0.2552 91.67 0.5661 0.8008 0.0422 0.0299 4.338 30.377 14.210 3234.583 3.432 63.205 1.993 0.69 338787. 0.2320 96.04 0.5931 0.8049 0.0370 0.0272 3.958 27.720 12.441 2951.648 3.132 55.336 1.912 0.69 339694. 0.2082 100.40 0.6200 0.8030 0.0317 0.0244 3.551 24.865 10.650 2647.647 2.809 47.370 1.824 0.69 340634. 0.1839 104.77 0.6470 0.7929 0.0263 0.0215 3.116 21.825 8.845 2323.944 2.466 39.344 1.726 0.69 341607. 0.1586 109.13 0.6739 0.7704 0.0209 0.0183 2.658 18.616 7.037 1982.223 2.103 31.301 1.610 0.69 342613. 0.1319 113.50 0.7009 0.7273 0.0156 0.0150 2.179 15.257 5.236 1624.592 1.724 23.288 1.462 0.69 343651. 0.1033 117.86 0.7279 0.6454 0.0103 0.0116 1.681 11.774 3.452 1253.674 1.330 15.356 1.249 0.70 344722. 0.0717 122.23 0.7548 0.4736 0.0051 0.0081 1.170 8.195 1.700 872.655 0.926 7.564 0.884 0.70 345825. 0.0356 126.59 0.7818 -0.0061 0.0000 0.0045 0.649 4.545 -0.012 483.909 0.513 -0.053 -0.011 0.70 346940. 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 0.1096 0.0399 7.943 50.062 45.530 5922.866 5.656 202.519 3.487 0.75 363554. 0.7266 4.84 0.0269 0.0720 0.1085 0.0406 8.088 50.975 45.075 6030.892 5.759 200.493 3.390 0.75 363831. 0.7029 9.69 0.0538 0.1399 0.1073 0.0413 8.230 51.872 44.563 6137.073 5.860 198.214 3.293 0.75 364135. 0.6790 14.53 0.0808 0.2037 0.1059 0.0420 8.367 52.736 43.987 6239.340 5.958 195.656 3.198 0.75 364469. 0.6550 19.37 0.1077 0.2635 0.1044 0.0426 8.496 53.549 43.343 6335.528 6.050 192.790 3.103 0.75 364833. 0.6309 24.22 0.1346 0.3195 0.1026 0.0432 8.614 54.291 42.623 6423.240 6.134 189.588 3.010 0.75 365228. 0.6068 29.06 0.1615 0.3718 0.1007 0.0437 8.716 54.939 41.822 6499.879 6.207 186.024 2.918 0.75 365657. 0.5828 33.90 0.1884 0.4205 0.0986 0.0442 8.801 55.469 40.933 6562.685 6.267 182.070 2.829 0.76 366119. 0.5590 38.75 0.2153 0.4657 0.0962 0.0445 8.862 55.859 39.951 6608.755 6.311 177.704 2.742 0.76 366616. 0.5352 43.59 0.2423 0.5078 0.0936 0.0447 8.898 56.081 38.872 6635.091 6.336 172.903 2.657 0.76 367148. 0.5116 48.43 0.2692 0.5468 0.0908 0.0447 8.903 56.112 37.691 6638.679 6.339 167.649 2.575 0.76 367717. 0.4882 53.28 0.2961 0.5829 0.0877 0.0445 8.873 55.924 36.405 6616.519 6.318 161.929 2.496 0.76 368322. 0.4650 58.12 0.3230 0.6162 0.0843 0.0442 8.805 55.495 35.012 6565.763 6.270 155.733 2.419 0.76 368963. 0.4420 62.96 0.3499 0.6471 0.0807 0.0436 8.695 54.803 33.511 6483.797 6.192 149.056 2.344 0.76 369641. 0.4191 67.80 0.3769 0.6754 0.0768 0.0429 8.540 53.826 31.902 6368.291 6.081 141.901 2.272 0.76 370357. 0.3963 72.65 0.4038 0.7014 0.0727 0.0418 8.337 52.548 30.187 6217.079 5.937 134.271 2.202 0.76 371109. 0.3737 77.49 0.4307 0.7251 0.0683 0.0406 8.084 50.949 28.364 6027.882 5.756 126.165 2.134 0.76 371898. 0.3510 82.33 0.4576 0.7464 0.0637 0.0390 7.778 49.022 26.442 5799.894 5.538 117.612 2.068 0.76 372724. 0.3284 87.18 0.4845 0.7653 0.0588 0.0372 7.422 46.778 24.433 5534.448 5.285 108.676 2.002 0.76 373587. 0.3057 92.02 0.5114 0.7815 0.0538 0.0352 7.018 44.232 22.351 5233.196 4.997 99.416 1.937 0.76 374486. 0.2828 96.86 0.5384 0.7947 0.0487 0.0330 6.568 41.397 20.207 4897.724 4.677 89.883 1.871 0.76 375421. 0.2598 101.71 0.5653 0.8043 0.0434 0.0305 6.074 38.286 18.014 4529.633 4.325 80.124 1.804 0.77 376392. 0.2364 106.55 0.5922 0.8093 0.0380 0.0278 5.539 34.913 15.779 4130.664 3.944 70.186 1.733 0.77 377399. 0.2125 111.39 0.6191 0.8084 0.0325 0.0249 4.966 31.297 13.515 3702.853 3.536 60.113 1.655 0.77 378443. 0.1879 116.24 0.6460 0.7990 0.0270 0.0219 4.357 27.459 11.231 3248.676 3.102 49.954 1.568 0.77 379522. 0.1623 121.08 0.6729 0.7766 0.0215 0.0187 3.716 23.423 8.939 2771.212 2.646 39.762 1.463 0.77 380638. 0.1351 125.92 0.6999 0.7326 0.0160 0.0153 3.050 19.223 6.654 2274.270 2.172 29.596 1.327 0.77 381789. 0.1057 130.77 0.7268 0.6475 0.0106 0.0119 2.364 14.897 4.389 1762.516 1.683 19.521 1.129 0.77 382977. 0.0731 135.61 0.7537 0.4693 0.0052 0.0084 1.665 10.493 2.161 1241.483 1.186 9.611 0.789 0.78 384199. 0.0358 140.45 0.7806 -0.0075 0.0000 0.0048 0.959 6.047 -0.019 715.395 0.683 -0.085 -0.012 0.78 385436. 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 0.1112 0.0441 11.697 67.023 55.872 8722.545 7.572 248.521 2.905 0.83 399847. 0.6707 5.32 0.0269 0.0663 0.1102 0.0447 11.853 67.917 55.364 8838.931 7.673 246.258 2.841 0.83 400151. 0.6528 10.64 0.0538 0.1295 0.1090 0.0453 12.003 68.773 54.786 8950.328 7.770 243.688 2.776 0.83 400485. 0.6346 15.96 0.0807 0.1898 0.1077 0.0458 12.142 69.570 54.132 9054.070 7.860 240.778 2.712 0.83 400852. 0.6162 21.28 0.1075 0.2470 0.1062 0.0463 12.267 70.287 53.392 9147.355 7.941 237.488 2.647 0.83 401252. 0.5974 26.60 0.1344 0.3013 0.1046 0.0467 12.374 70.901 52.558 9227.272 8.010 233.780 2.584 0.83 401687. 0.5784 31.93 0.1613 0.3527 0.1027 0.0470 12.459 71.389 51.623 9290.731 8.065 229.617 2.520 0.83 402159. 0.5592 37.25 0.1882 0.4013 0.1006 0.0472 12.518 71.725 50.576 9334.483 8.103 224.964 2.458 0.83 402668. 0.5397 42.57 0.2151 0.4471 0.0983 0.0473 12.546 71.884 49.413 9355.241 8.121 219.787 2.396 0.83 403216. 0.5201 47.89 0.2420 0.4901 0.0958 0.0473 12.538 71.842 48.124 9349.673 8.117 214.057 2.335 0.83 403804. 0.5002 53.21 0.2688 0.5305 0.0929 0.0471 12.491 71.571 46.706 9314.454 8.086 207.749 2.274 0.83 404431. 0.4800 58.53 0.2957 0.5683 0.0899 0.0468 12.399 71.047 45.154 9246.283 8.027 200.844 2.215 0.83 405098. 0.4597 63.85 0.3226 0.6036 0.0865 0.0462 12.260 70.245 43.464 9141.950 7.936 193.328 2.156 0.83 405806. 0.4390 69.17 0.3495 0.6364 0.0829 0.0455 12.067 69.144 41.636 8998.543 7.812 185.196 2.099 0.83 406554. 0.4182 74.49 0.3764 0.6667 0.0789 0.0446 11.819 67.720 39.670 8813.254 7.651 176.450 2.042 0.83 407343. 0.3971 79.81 0.4033 0.6946 0.0748 0.0434 11.511 65.954 37.567 8583.404 7.451 167.096 1.985 0.84 408173. 0.3757 85.13 0.4302 0.7200 0.0703 0.0420 11.138 63.821 35.327 8305.883 7.210 157.133 1.929 0.84 409043. 0.3541 90.46 0.4570 0.7429 0.0656 0.0403 10.700 61.309 32.957 7978.893 6.927 146.593 1.873 0.84 409953. 0.3321 95.78 0.4839 0.7631 0.0606 0.0385 10.199 58.440 30.475 7605.536 6.603 135.551 1.817 0.84 410903. 0.3098 101.10 0.5108 0.7799 0.0555 0.0364 9.642 55.249 27.896 7190.244 6.242 124.083 1.760 0.84 411893. 0.2870 106.42 0.5377 0.7930 0.0502 0.0341 9.031 51.744 25.237 6734.123 5.846 112.255 1.700 0.84 412923. 0.2637 111.74 0.5646 0.8017 0.0448 0.0315 8.366 47.936 22.511 6238.529 5.416 100.127 1.637 0.84 413992. 0.2398 117.06 0.5915 0.8049 0.0393 0.0289 7.652 43.842 19.730 5705.779 4.953 87.760 1.568 0.84 415100. 0.2151 122.38 0.6183 0.8005 0.0336 0.0260 6.893 39.495 16.908 5139.959 4.462 75.209 1.492 0.84 416247. 0.1895 127.70 0.6452 0.7852 0.0280 0.0230 6.097 34.934 14.059 4546.471 3.947 62.534 1.403 0.85 417433. 0.1624 133.02 0.6721 0.7533 0.0223 0.0199 5.272 30.206 11.196 3931.125 3.413 49.801 1.292 0.85 418659. 0.1335 138.34 0.6990 0.6948 0.0166 0.0167 4.427 25.364 8.337 3300.955 2.866 37.084 1.146 0.85 419924. 0.1022 143.66 0.7259 0.5898 0.0109 0.0135 3.572 20.470 5.500 2664.009 2.313 24.465 0.936 0.85 421228. 0.0678 148.98 0.7528 0.3951 0.0054 0.0103 2.721 15.591 2.706 2029.072 1.761 12.038 0.605 0.85 422570. 0.0307 154.31 0.7797 -0.0061 -0.0001 0.0071 1.880 10.774 -0.028 1402.097 1.217 -0.125 -0.009 0.85 423933. 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 0.1119 0.0520 17.895 93.992 66.912 13344.392 10.619 297.624 2.274 0.90 436161. 0.5745 5.88 0.0272 0.0576 0.1110 0.0525 18.081 94.970 66.391 13483.326 10.730 295.305 2.233 0.90 436492. 0.5620 11.76 0.0545 0.1131 0.1100 0.0530 18.249 95.849 65.788 13608.125 10.829 292.623 2.193 0.90 436857. 0.5493 17.65 0.0817 0.1665 0.1088 0.0534 18.391 96.594 65.092 13713.897 10.913 289.528 2.153 0.90 437259. 0.5364 23.53 0.1090 0.2180 0.1075 0.0537 18.501 97.171 64.291 13795.826 10.978 285.965 2.114 0.90 437700. 0.5234 29.41 0.1362 0.2676 0.1060 0.0539 18.572 97.547 63.372 13849.105 11.021 281.879 2.075 0.91 438180. 0.5102 35.29 0.1635 0.3154 0.1042 0.0540 18.599 97.688 62.323 13869.155 11.037 277.215 2.038 0.91 438703. 0.4969 41.18 0.1907 0.3613 0.1022 0.0539 18.576 97.565 61.133 13851.757 11.023 271.920 2.002 0.91 439269. 0.4834 47.06 0.2180 0.4056 0.1000 0.0537 18.497 97.153 59.790 13793.178 10.976 265.946 1.966 0.91 439878. 0.4695 52.94 0.2452 0.4482 0.0975 0.0533 18.359 96.427 58.285 13690.186 10.894 259.252 1.931 0.91 440533. 0.4553 58.82 0.2724 0.4890 0.0947 0.0527 18.156 95.362 56.608 13538.988 10.774 251.793 1.896 0.91 441234. 0.4406 64.70 0.2997 0.5282 0.0916 0.0519 17.887 93.949 54.755 13338.358 10.614 243.551 1.862 0.91 441980. 0.4255 70.59 0.3269 0.5655 0.0882 0.0510 17.549 92.173 52.722 13086.157 10.414 234.506 1.827 0.91 442772. 0.4098 76.47 0.3542 0.6009 0.0845 0.0498 17.139 90.020 50.506 12780.478 10.170 224.652 1.792 0.91 443610. 0.3934 82.35 0.3814 0.6343 0.0804 0.0484 16.655 87.477 48.109 12419.523 9.883 213.989 1.757 0.91 444495. 0.3763 88.23 0.4087 0.6656 0.0761 0.0467 16.094 84.532 45.532 12001.311 9.550 202.524 1.721 0.91 445424. 0.3586 94.11 0.4359 0.6947 0.0715 0.0449 15.453 81.164 42.774 11523.255 9.170 190.260 1.684 0.91 446400. 0.3401 100.00 0.4631 0.7213 0.0666 0.0428 14.731 77.374 39.849 10985.051 8.742 177.250 1.645 0.91 447420. 0.3208 105.88 0.4904 0.7453 0.0615 0.0405 13.933 73.181 36.781 10389.755 8.268 163.602 1.606 0.92 448485. 0.3007 111.76 0.5176 0.7647 0.0562 0.0380 13.091 68.756 33.588 9761.626 7.768 149.401 1.561 0.92 449594. 0.2793 117.64 0.5449 0.7776 0.0506 0.0355 12.220 64.183 30.289 9112.350 7.251 134.725 1.508 0.92 450747. 0.2562 123.53 0.5721 0.7806 0.0450 0.0330 11.350 59.613 26.897 8463.435 6.735 119.640 1.441 0.92 451944. 0.2309 129.41 0.5994 0.7731 0.0392 0.0304 10.460 54.938 23.434 7799.785 6.207 104.236 1.363 0.92 453184. 0.2037 135.29 0.6266 0.7537 0.0333 0.0277 9.536 50.087 19.923 7111.126 5.659 88.616 1.271 0.92 454468. 0.1752 141.17 0.6539 0.7177 0.0274 0.0250 8.593 45.133 16.383 6407.666 5.099 72.871 1.160 0.92 455795. 0.1450 147.05 0.6811 0.6584 0.0215 0.0222 7.645 40.153 12.837 5700.751 4.537 57.097 1.021 0.93 457166. 0.1130 152.94 0.7083 0.5662 0.0156 0.0195 6.706 35.221 9.310 5000.449 3.979 41.410 0.844 0.93 458580. 0.0796 158.82 0.7356 0.4266 0.0098 0.0168 5.790 30.412 5.832 4317.677 3.436 25.943 0.613 0.93 460038. 0.0457 164.70 0.7628 0.2179 0.0041 0.0143 4.911 25.795 2.437 3662.184 2.914 10.841 0.302 0.93 461539. 0.0146 170.58 0.7901