19x12E (19x12E.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 0.0952 0.0384 0.008 0.483 0.395 5.712 0.055 1.759 31.396 0.08 33270. 0.6097 0.48 0.0268 0.0646 0.0941 0.0390 0.008 0.490 0.391 5.800 0.055 1.738 30.546 0.08 33294. 0.5896 0.96 0.0536 0.1256 0.0928 0.0396 0.008 0.498 0.385 5.887 0.056 1.714 29.695 0.08 33320. 0.5693 1.45 0.0804 0.1830 0.0914 0.0402 0.008 0.505 0.380 5.970 0.057 1.689 28.846 0.08 33349. 0.5489 1.93 0.1072 0.2368 0.0899 0.0407 0.008 0.511 0.373 6.048 0.058 1.661 28.003 0.08 33380. 0.5284 2.41 0.1340 0.2872 0.0882 0.0412 0.008 0.517 0.366 6.118 0.058 1.630 27.168 0.08 33414. 0.5079 2.89 0.1608 0.3342 0.0864 0.0416 0.008 0.522 0.359 6.179 0.059 1.596 26.344 0.08 33451. 0.4874 3.38 0.1876 0.3779 0.0844 0.0419 0.008 0.527 0.351 6.229 0.059 1.560 25.534 0.08 33492. 0.4670 3.86 0.2144 0.4184 0.0823 0.0422 0.008 0.530 0.342 6.265 0.060 1.520 24.737 0.08 33535. 0.4466 4.34 0.2412 0.4558 0.0799 0.0423 0.008 0.531 0.332 6.286 0.060 1.477 23.956 0.08 33581. 0.4263 4.82 0.2680 0.4903 0.0774 0.0423 0.008 0.531 0.321 6.287 0.060 1.430 23.190 0.08 33631. 0.4060 5.30 0.2948 0.5218 0.0747 0.0422 0.008 0.530 0.310 6.268 0.060 1.379 22.438 0.08 33684. 0.3859 5.79 0.3216 0.5505 0.0717 0.0419 0.008 0.526 0.298 6.227 0.059 1.325 21.700 0.08 33740. 0.3658 6.27 0.3484 0.5764 0.0686 0.0415 0.008 0.521 0.285 6.160 0.059 1.267 20.972 0.08 33800. 0.3457 6.75 0.3752 0.5994 0.0652 0.0408 0.008 0.513 0.271 6.068 0.058 1.205 20.251 0.08 33863. 0.3255 7.23 0.4020 0.6194 0.0617 0.0400 0.008 0.503 0.256 5.948 0.057 1.139 19.533 0.08 33930. 0.3053 7.72 0.4288 0.6363 0.0579 0.0390 0.008 0.490 0.241 5.800 0.055 1.070 18.812 0.08 34000. 0.2849 8.20 0.4556 0.6499 0.0540 0.0378 0.008 0.475 0.224 5.622 0.054 0.997 18.082 0.08 34073. 0.2643 8.68 0.4824 0.6596 0.0498 0.0364 0.007 0.458 0.207 5.416 0.052 0.921 17.334 0.08 34150. 0.2435 9.16 0.5092 0.6652 0.0456 0.0349 0.007 0.438 0.189 5.184 0.050 0.842 16.560 0.08 34230. 0.2225 9.64 0.5360 0.6658 0.0412 0.0332 0.007 0.416 0.171 4.927 0.047 0.761 15.746 0.08 34314. 0.2011 10.13 0.5628 0.6605 0.0367 0.0313 0.006 0.393 0.152 4.647 0.044 0.678 14.878 0.08 34401. 0.1794 10.61 0.5897 0.6482 0.0321 0.0292 0.006 0.367 0.133 4.344 0.041 0.594 13.936 0.08 34491. 0.1572 11.09 0.6165 0.6269 0.0275 0.0271 0.005 0.340 0.114 4.021 0.038 0.508 12.892 0.08 34585. 0.1346 11.57 0.6433 0.5941 0.0229 0.0248 0.005 0.311 0.095 3.679 0.035 0.422 11.709 0.08 34682. 0.1114 12.06 0.6701 0.5460 0.0182 0.0223 0.004 0.281 0.076 3.319 0.032 0.336 10.331 0.08 34783. 0.0877 12.54 0.6969 0.4767 0.0136 0.0198 0.004 0.249 0.056 2.944 0.028 0.250 8.673 0.08 34887. 0.0635 13.02 0.7237 0.3765 0.0089 0.0172 0.003 0.216 0.037 2.555 0.024 0.165 6.596 0.08 34994. 0.0393 13.50 0.7505 0.2284 0.0044 0.0145 0.003 0.182 0.018 2.157 0.021 0.082 3.858 0.08 35105. 0.0161 13.98 0.7773 -0.0003 0.0000 0.0118 0.002 0.148 0.000 1.752 0.017 0.000 -0.005 0.08 35219. 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 0.0955 0.0357 0.057 1.795 1.587 42.472 0.203 7.060 16.950 0.15 66539. 0.6595 0.97 0.0269 0.0699 0.0944 0.0364 0.058 1.827 1.568 43.228 0.206 6.976 16.456 0.15 66587. 0.6364 1.94 0.0539 0.1356 0.0932 0.0370 0.059 1.858 1.547 43.971 0.210 6.883 15.962 0.15 66639. 0.6132 2.91 0.0808 0.1972 0.0918 0.0376 0.060 1.889 1.525 44.689 0.213 6.781 15.473 0.15 66697. 0.5900 3.88 0.1077 0.2547 0.0903 0.0382 0.061 1.917 1.499 45.365 0.217 6.669 14.991 0.15 66761. 0.5669 4.84 0.1346 0.3083 0.0886 0.0387 0.062 1.943 1.472 45.985 0.220 6.546 14.516 0.15 66830. 0.5438 5.81 0.1616 0.3581 0.0868 0.0391 0.062 1.966 1.441 46.532 0.222 6.411 14.050 0.15 66904. 0.5209 6.78 0.1885 0.4043 0.0848 0.0395 0.063 1.986 1.408 46.986 0.224 6.264 13.595 0.15 66985. 0.4982 7.75 0.2154 0.4469 0.0826 0.0398 0.063 2.000 1.372 47.329 0.226 6.104 13.151 0.15 67072. 0.4758 8.72 0.2424 0.4863 0.0802 0.0400 0.064 2.009 1.333 47.541 0.227 5.930 12.719 0.15 67166. 0.4535 9.69 0.2693 0.5224 0.0777 0.0400 0.064 2.012 1.291 47.603 0.227 5.741 12.298 0.15 67266. 0.4315 10.66 0.2962 0.5556 0.0749 0.0400 0.064 2.007 1.245 47.494 0.227 5.537 11.889 0.15 67373. 0.4097 11.63 0.3231 0.5858 0.0720 0.0397 0.063 1.995 1.196 47.198 0.225 5.319 11.491 0.15 67487. 0.3880 12.60 0.3501 0.6131 0.0688 0.0393 0.063 1.974 1.143 46.698 0.223 5.084 11.102 0.15 67607. 0.3666 13.57 0.3770 0.6376 0.0654 0.0387 0.062 1.943 1.087 45.980 0.220 4.834 10.721 0.15 67734. 0.3452 14.53 0.4039 0.6593 0.0618 0.0379 0.060 1.903 1.027 45.032 0.215 4.569 10.347 0.15 67869. 0.3239 15.50 0.4308 0.6780 0.0580 0.0369 0.059 1.853 0.964 43.841 0.209 4.289 9.975 0.15 68010. 0.3025 16.47 0.4578 0.6936 0.0540 0.0357 0.057 1.792 0.898 42.402 0.202 3.994 9.604 0.15 68158. 0.2810 17.44 0.4847 0.7057 0.0499 0.0343 0.055 1.721 0.829 40.727 0.194 3.686 9.229 0.15 68313. 0.2595 18.41 0.5116 0.7140 0.0456 0.0327 0.052 1.641 0.757 38.827 0.185 3.368 8.846 0.15 68475. 0.2377 19.38 0.5386 0.7179 0.0412 0.0309 0.049 1.552 0.684 36.713 0.175 3.042 8.449 0.15 68643. 0.2158 20.35 0.5655 0.7164 0.0367 0.0289 0.046 1.454 0.609 34.397 0.164 2.709 8.030 0.15 68819. 0.1935 21.32 0.5924 0.7083 0.0321 0.0268 0.043 1.348 0.533 31.887 0.152 2.370 7.579 0.15 69001. 0.1709 22.29 0.6193 0.6919 0.0274 0.0246 0.039 1.234 0.456 29.196 0.139 2.028 7.082 0.15 69191. 0.1477 23.26 0.6463 0.6644 0.0228 0.0222 0.035 1.113 0.378 26.336 0.126 1.683 6.516 0.15 69387. 0.1238 24.22 0.6732 0.6213 0.0181 0.0196 0.031 0.986 0.301 23.323 0.111 1.338 5.850 0.15 69590. 0.0991 25.19 0.7001 0.5554 0.0135 0.0170 0.027 0.853 0.224 20.174 0.096 0.995 5.028 0.15 69800. 0.0734 26.16 0.7271 0.4532 0.0089 0.0142 0.023 0.715 0.147 16.912 0.081 0.655 3.952 0.15 70016. 0.0468 27.13 0.7540 0.2882 0.0044 0.0114 0.018 0.573 0.072 13.561 0.065 0.322 2.423 0.16 70240. 0.0201 28.10 0.7809 -0.0031 0.0000 0.0085 0.014 0.429 -0.001 10.148 0.048 -0.003 -0.025 0.16 70468. 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 0.0959 0.0346 0.186 3.915 3.584 138.952 0.442 15.944 11.701 0.23 99806. 0.6841 1.46 0.0270 0.0724 0.0948 0.0353 0.190 3.989 3.542 141.586 0.451 15.756 11.348 0.23 99878. 0.6596 2.91 0.0540 0.1404 0.0935 0.0359 0.193 4.062 3.496 144.183 0.459 15.548 10.996 0.23 99957. 0.6349 4.37 0.0809 0.2039 0.0921 0.0366 0.197 4.133 3.444 146.694 0.467 15.320 10.649 0.23 100045. 0.6103 5.82 0.1079 0.2632 0.0906 0.0372 0.200 4.200 3.388 149.070 0.475 15.068 10.307 0.23 100140. 0.5859 7.28 0.1349 0.3183 0.0890 0.0377 0.203 4.262 3.325 151.257 0.481 14.792 9.972 0.23 100244. 0.5616 8.74 0.1619 0.3694 0.0871 0.0382 0.205 4.316 3.257 153.194 0.488 14.489 9.644 0.23 100356. 0.5375 10.19 0.1888 0.4167 0.0852 0.0386 0.208 4.362 3.183 154.819 0.493 14.157 9.325 0.23 100478. 0.5138 11.65 0.2158 0.4603 0.0830 0.0389 0.209 4.397 3.102 156.064 0.497 13.796 9.014 0.23 100609. 0.4903 13.10 0.2428 0.5006 0.0806 0.0391 0.210 4.419 3.013 156.862 0.499 13.403 8.713 0.23 100750. 0.4671 14.56 0.2698 0.5375 0.0781 0.0392 0.211 4.427 2.917 157.144 0.500 12.977 8.421 0.23 100901. 0.4442 16.02 0.2967 0.5714 0.0753 0.0391 0.210 4.419 2.814 156.842 0.499 12.517 8.138 0.23 101062. 0.4216 17.47 0.3237 0.6024 0.0723 0.0389 0.209 4.392 2.703 155.896 0.496 12.022 7.864 0.23 101233. 0.3992 18.93 0.3507 0.6304 0.0691 0.0384 0.207 4.346 2.584 154.247 0.491 11.492 7.597 0.23 101414. 0.3771 20.38 0.3777 0.6558 0.0657 0.0379 0.204 4.278 2.457 151.846 0.483 10.927 7.338 0.23 101606. 0.3552 21.84 0.4046 0.6783 0.0621 0.0371 0.199 4.188 2.322 148.650 0.473 10.326 7.084 0.23 101808. 0.3333 23.30 0.4316 0.6980 0.0583 0.0360 0.194 4.074 2.179 144.610 0.460 9.691 6.834 0.23 102020. 0.3115 24.75 0.4586 0.7146 0.0543 0.0348 0.187 3.936 2.029 139.714 0.445 9.023 6.586 0.23 102243. 0.2897 26.21 0.4856 0.7281 0.0501 0.0334 0.180 3.775 1.872 133.993 0.427 8.327 6.337 0.23 102476. 0.2678 27.67 0.5125 0.7380 0.0458 0.0318 0.171 3.592 1.710 127.488 0.406 7.608 6.085 0.23 102720. 0.2458 29.12 0.5395 0.7438 0.0413 0.0300 0.161 3.387 1.544 120.234 0.383 6.869 5.826 0.23 102974. 0.2236 30.58 0.5665 0.7446 0.0368 0.0280 0.151 3.163 1.375 112.267 0.357 6.115 5.554 0.23 103238. 0.2011 32.03 0.5935 0.7393 0.0322 0.0258 0.139 2.919 1.203 103.621 0.330 5.349 5.264 0.23 103513. 0.1783 33.49 0.6204 0.7261 0.0275 0.0235 0.127 2.658 1.029 94.336 0.300 4.575 4.945 0.23 103798. 0.1549 34.95 0.6474 0.7022 0.0228 0.0211 0.113 2.379 0.854 84.457 0.269 3.796 4.584 0.23 104093. 0.1308 36.40 0.6744 0.6632 0.0181 0.0185 0.099 2.086 0.678 74.036 0.236 3.017 4.156 0.23 104398. 0.1057 37.86 0.7014 0.6012 0.0135 0.0157 0.085 1.779 0.504 63.139 0.201 2.243 3.622 0.23 104714. 0.0794 39.31 0.7283 0.5008 0.0089 0.0129 0.070 1.461 0.332 51.842 0.165 1.477 2.906 0.23 105040. 0.0517 40.77 0.7553 0.3291 0.0044 0.0100 0.054 1.134 0.163 40.236 0.128 0.727 1.841 0.23 105377. 0.0230 42.23 0.7823 -0.0032 0.0000 0.0071 0.038 0.800 -0.001 28.406 0.090 -0.005 -0.017 0.23 105720. 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 0.0963 0.0341 0.435 6.853 6.402 324.326 0.774 28.474 8.953 0.30 133070. 0.6995 1.94 0.0270 0.0739 0.0952 0.0348 0.444 6.988 6.327 330.719 0.790 28.143 8.677 0.30 133167. 0.6741 3.89 0.0540 0.1432 0.0940 0.0354 0.452 7.122 6.245 337.028 0.805 27.777 8.404 0.30 133273. 0.6486 5.83 0.0810 0.2079 0.0926 0.0361 0.460 7.251 6.154 343.139 0.819 27.372 8.134 0.30 133389. 0.6232 7.77 0.1080 0.2681 0.0911 0.0367 0.468 7.373 6.054 348.932 0.833 26.927 7.869 0.30 133516. 0.5979 9.72 0.1350 0.3241 0.0894 0.0373 0.475 7.486 5.944 354.276 0.846 26.437 7.609 0.30 133655. 0.5729 11.66 0.1620 0.3760 0.0876 0.0378 0.481 7.586 5.823 359.026 0.857 25.899 7.356 0.30 133806. 0.5482 13.60 0.1890 0.4239 0.0856 0.0382 0.487 7.671 5.690 363.028 0.867 25.310 7.109 0.30 133968. 0.5237 15.55 0.2160 0.4682 0.0835 0.0385 0.491 7.736 5.546 366.121 0.874 24.667 6.870 0.30 134144. 0.4996 17.49 0.2430 0.5090 0.0811 0.0387 0.494 7.779 5.388 368.141 0.879 23.967 6.639 0.30 134332. 0.4759 19.43 0.2700 0.5465 0.0785 0.0388 0.495 7.796 5.218 368.921 0.881 23.208 6.415 0.30 134534. 0.4525 21.37 0.2970 0.5808 0.0757 0.0387 0.494 7.782 5.033 368.298 0.879 22.387 6.198 0.30 134749. 0.4294 23.32 0.3240 0.6122 0.0728 0.0385 0.491 7.736 4.834 366.120 0.874 21.504 5.989 0.30 134977. 0.4067 25.26 0.3510 0.6408 0.0695 0.0381 0.486 7.655 4.622 362.248 0.865 20.557 5.787 0.30 135220. 0.3842 27.20 0.3780 0.6667 0.0661 0.0375 0.478 7.534 4.394 356.563 0.851 19.546 5.590 0.30 135476. 0.3619 29.15 0.4050 0.6898 0.0625 0.0367 0.468 7.374 4.153 348.954 0.833 18.473 5.398 0.30 135746. 0.3397 31.09 0.4320 0.7101 0.0587 0.0357 0.455 7.170 3.898 339.306 0.810 17.336 5.210 0.30 136030. 0.3177 33.03 0.4590 0.7276 0.0546 0.0344 0.439 6.922 3.629 327.583 0.782 16.141 5.024 0.30 136327. 0.2956 34.98 0.4860 0.7421 0.0504 0.0330 0.421 6.632 3.349 313.861 0.749 14.895 4.839 0.31 136639. 0.2735 36.92 0.5130 0.7531 0.0460 0.0314 0.400 6.302 3.059 298.230 0.712 13.608 4.653 0.31 136965. 0.2513 38.86 0.5400 0.7602 0.0416 0.0295 0.377 5.933 2.762 280.777 0.670 12.286 4.462 0.31 137304. 0.2290 40.81 0.5670 0.7626 0.0370 0.0275 0.351 5.527 2.459 261.584 0.624 10.936 4.263 0.31 137657. 0.2064 42.75 0.5940 0.7593 0.0324 0.0253 0.323 5.087 2.150 240.735 0.575 9.565 4.051 0.31 138024. 0.1835 44.69 0.6210 0.7485 0.0277 0.0230 0.293 4.613 1.839 218.325 0.521 8.179 3.820 0.31 138405. 0.1600 46.64 0.6480 0.7275 0.0230 0.0204 0.261 4.109 1.526 194.462 0.464 6.786 3.558 0.31 138799. 0.1357 48.58 0.6750 0.6918 0.0182 0.0178 0.227 3.577 1.212 169.278 0.404 5.392 3.248 0.31 139207. 0.1104 50.52 0.7020 0.6331 0.0136 0.0150 0.192 3.020 0.901 142.929 0.341 4.007 2.858 0.31 139629. 0.0838 52.47 0.7290 0.5352 0.0089 0.0122 0.155 2.443 0.593 115.606 0.276 2.638 2.327 0.31 140064. 0.0553 54.41 0.7560 0.3602 0.0044 0.0092 0.117 1.850 0.291 87.532 0.209 1.296 1.510 0.31 140513. 0.0252 56.35 0.7830 -0.0044 0.0000 0.0062 0.079 1.245 -0.002 58.908 0.141 -0.010 -0.018 0.31 140971. 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 0.0969 0.0339 0.844 10.637 10.059 629.228 1.202 44.743 7.251 0.38 166331. 0.7102 2.43 0.0270 0.0748 0.0958 0.0346 0.861 10.852 9.944 641.977 1.226 44.231 7.026 0.38 166452. 0.6842 4.86 0.0540 0.1449 0.0945 0.0352 0.878 11.065 9.817 654.571 1.250 43.665 6.802 0.38 166584. 0.6582 7.29 0.0810 0.2103 0.0932 0.0359 0.894 11.272 9.676 666.783 1.273 43.038 6.582 0.38 166730. 0.6323 9.72 0.1080 0.2711 0.0917 0.0365 0.910 11.468 9.520 678.377 1.296 42.347 6.365 0.38 166889. 0.6065 12.15 0.1350 0.3276 0.0900 0.0371 0.924 11.649 9.349 689.090 1.316 41.585 6.154 0.38 167063. 0.5811 14.57 0.1620 0.3800 0.0882 0.0376 0.937 11.810 9.161 698.635 1.334 40.747 5.947 0.38 167251. 0.5559 17.00 0.1890 0.4284 0.0862 0.0381 0.948 11.946 8.954 706.706 1.350 39.829 5.747 0.38 167455. 0.5311 19.43 0.2160 0.4730 0.0841 0.0384 0.956 12.053 8.729 712.983 1.362 38.825 5.553 0.38 167674. 0.5066 21.86 0.2430 0.5142 0.0817 0.0386 0.962 12.123 8.483 717.136 1.370 37.731 5.365 0.38 167910. 0.4826 24.29 0.2700 0.5520 0.0791 0.0387 0.964 12.152 8.216 718.834 1.373 36.543 5.184 0.38 168163. 0.4589 26.72 0.2970 0.5867 0.0763 0.0386 0.963 12.133 7.926 717.753 1.371 35.257 5.009 0.38 168432. 0.4355 29.15 0.3240 0.6185 0.0733 0.0384 0.957 12.063 7.615 713.588 1.363 33.872 4.840 0.38 168718. 0.4125 31.58 0.3510 0.6475 0.0701 0.0380 0.947 11.936 7.281 706.061 1.348 32.385 4.677 0.38 169021. 0.3898 34.01 0.3780 0.6737 0.0667 0.0374 0.932 11.747 6.924 694.932 1.327 30.799 4.519 0.38 169342. 0.3672 36.44 0.4050 0.6973 0.0630 0.0366 0.912 11.495 6.545 679.980 1.299 29.112 4.366 0.38 169680. 0.3449 38.86 0.4320 0.7182 0.0592 0.0356 0.886 11.173 6.143 660.976 1.262 27.324 4.215 0.38 170035. 0.3227 41.29 0.4590 0.7364 0.0551 0.0343 0.855 10.782 5.720 637.841 1.218 25.443 4.068 0.38 170408. 0.3004 43.72 0.4860 0.7516 0.0508 0.0329 0.819 10.324 5.279 610.716 1.166 23.483 3.921 0.38 170798. 0.2782 46.15 0.5130 0.7635 0.0465 0.0312 0.777 9.801 4.824 579.779 1.107 21.456 3.774 0.38 171205. 0.2560 48.58 0.5400 0.7717 0.0419 0.0294 0.731 9.216 4.356 545.197 1.041 19.373 3.624 0.38 171629. 0.2335 51.01 0.5670 0.7755 0.0373 0.0273 0.680 8.573 3.878 507.134 0.969 17.247 3.468 0.38 172071. 0.2109 53.44 0.5940 0.7738 0.0327 0.0251 0.625 7.873 3.392 465.757 0.890 15.087 3.303 0.38 172530. 0.1879 55.87 0.6210 0.7650 0.0279 0.0227 0.565 7.121 2.901 421.252 0.805 12.904 3.124 0.38 173006. 0.1643 58.30 0.6480 0.7465 0.0232 0.0201 0.501 6.320 2.407 373.837 0.714 10.708 2.921 0.38 173499. 0.1400 60.73 0.6750 0.7137 0.0184 0.0174 0.434 5.473 1.914 323.772 0.618 8.512 2.681 0.39 174009. 0.1145 63.15 0.7020 0.6584 0.0137 0.0146 0.364 4.587 1.423 271.374 0.518 6.329 2.378 0.39 174537. 0.0876 65.58 0.7290 0.5637 0.0090 0.0117 0.291 3.669 0.938 217.025 0.414 4.173 1.961 0.39 175081. 0.0586 68.01 0.7560 0.3884 0.0045 0.0087 0.216 2.725 0.463 161.175 0.308 2.059 1.303 0.39 175642. 0.0274 70.44 0.7830 0.0002 0.0000 0.0056 0.140 1.762 0.000 104.217 0.199 0.001 0.001 0.39 176214. 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 0.0976 0.0339 1.457 15.308 14.585 1086.636 1.729 64.874 6.088 0.45 199587. 0.7180 2.92 0.0270 0.0754 0.0965 0.0346 1.487 15.625 14.422 1109.151 1.765 64.148 5.898 0.45 199732. 0.6917 5.83 0.0540 0.1459 0.0952 0.0353 1.517 15.938 14.241 1131.409 1.801 63.343 5.709 0.45 199891. 0.6653 8.75 0.0810 0.2118 0.0939 0.0359 1.546 16.243 14.040 1153.018 1.835 62.450 5.523 0.45 200066. 0.6391 11.66 0.1080 0.2731 0.0924 0.0366 1.574 16.532 13.818 1173.558 1.868 61.463 5.341 0.45 200258. 0.6131 14.58 0.1350 0.3299 0.0908 0.0372 1.599 16.800 13.573 1192.559 1.898 60.373 5.162 0.45 200467. 0.5873 17.49 0.1621 0.3826 0.0890 0.0377 1.622 17.039 13.303 1209.520 1.925 59.172 4.989 0.45 200693. 0.5619 20.41 0.1891 0.4313 0.0870 0.0381 1.641 17.241 13.007 1223.898 1.948 57.853 4.820 0.45 200938. 0.5368 23.33 0.2161 0.4762 0.0848 0.0385 1.656 17.399 12.682 1235.127 1.966 56.408 4.657 0.45 201202. 0.5122 26.24 0.2431 0.5176 0.0824 0.0387 1.666 17.505 12.327 1242.625 1.978 54.831 4.500 0.45 201486. 0.4879 29.16 0.2701 0.5557 0.0799 0.0388 1.671 17.550 11.941 1245.805 1.983 53.116 4.348 0.45 201789. 0.4640 32.07 0.2971 0.5907 0.0771 0.0388 1.668 17.526 11.524 1244.094 1.980 51.257 4.201 0.45 202113. 0.4404 34.99 0.3241 0.6228 0.0741 0.0385 1.659 17.425 11.073 1236.951 1.969 49.252 4.060 0.45 202457. 0.4172 37.90 0.3511 0.6521 0.0708 0.0381 1.641 17.241 10.589 1223.887 1.948 47.099 3.924 0.46 202822. 0.3943 40.82 0.3781 0.6787 0.0674 0.0375 1.615 16.967 10.071 1204.473 1.917 44.798 3.793 0.46 203207. 0.3717 43.74 0.4051 0.7027 0.0637 0.0367 1.580 16.599 9.521 1178.322 1.875 42.349 3.665 0.46 203613. 0.3492 46.65 0.4321 0.7241 0.0598 0.0357 1.536 16.130 8.937 1145.030 1.822 39.754 3.540 0.46 204041. 0.3269 49.57 0.4591 0.7427 0.0557 0.0344 1.481 15.558 8.323 1104.445 1.758 37.020 3.418 0.46 204488. 0.3045 52.48 0.4862 0.7586 0.0514 0.0329 1.417 14.887 7.682 1056.806 1.682 34.169 3.297 0.46 204957. 0.2822 55.40 0.5132 0.7713 0.0469 0.0312 1.344 14.121 7.019 1002.424 1.595 31.219 3.176 0.46 205446. 0.2598 58.31 0.5402 0.7804 0.0424 0.0293 1.263 13.264 6.337 941.593 1.499 28.189 3.053 0.46 205957. 0.2373 61.23 0.5672 0.7853 0.0377 0.0273 1.173 12.321 5.642 874.599 1.392 25.093 2.926 0.46 206487. 0.2146 64.15 0.5942 0.7850 0.0330 0.0250 1.075 11.294 4.934 801.735 1.276 21.948 2.792 0.46 207038. 0.1915 67.06 0.6212 0.7779 0.0282 0.0225 0.970 10.190 4.219 723.332 1.151 18.768 2.646 0.46 207610. 0.1678 69.98 0.6482 0.7613 0.0234 0.0199 0.858 9.013 3.500 639.775 1.018 15.569 2.482 0.46 208202. 0.1434 72.89 0.6752 0.7309 0.0186 0.0172 0.740 7.769 2.781 551.528 0.878 12.370 2.287 0.46 208815. 0.1178 75.81 0.7022 0.6782 0.0138 0.0143 0.616 6.468 2.066 459.151 0.731 9.189 2.041 0.46 209449. 0.0906 78.72 0.7292 0.5858 0.0091 0.0113 0.487 5.118 1.360 363.326 0.578 6.047 1.697 0.46 210103. 0.0611 81.64 0.7562 0.4091 0.0045 0.0083 0.355 3.731 0.667 264.861 0.422 2.969 1.143 0.47 210776. 0.0288 84.56 0.7833 -0.0069 0.0000 0.0051 0.220 2.316 -0.007 164.417 0.262 -0.030 -0.019 0.47 211461. 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 0.0984 0.0340 2.324 20.924 20.015 1732.917 2.364 89.027 5.239 0.53 232836. 0.7238 3.40 0.0270 0.0757 0.0973 0.0347 2.373 21.366 19.798 1769.533 2.414 88.060 5.075 0.53 233005. 0.6973 6.80 0.0540 0.1465 0.0961 0.0354 2.422 21.804 19.555 1805.777 2.463 86.983 4.912 0.53 233192. 0.6708 10.21 0.0810 0.2126 0.0948 0.0361 2.469 22.229 19.286 1840.998 2.511 85.786 4.752 0.53 233397. 0.6444 13.61 0.1081 0.2741 0.0933 0.0368 2.514 22.634 18.988 1874.512 2.557 84.458 4.594 0.53 233620. 0.6183 17.01 0.1351 0.3312 0.0917 0.0374 2.555 23.009 18.657 1905.560 2.600 82.988 4.441 0.53 233864. 0.5924 20.41 0.1621 0.3841 0.0899 0.0379 2.593 23.344 18.292 1933.314 2.637 81.364 4.291 0.53 234129. 0.5668 23.82 0.1891 0.4329 0.0879 0.0384 2.624 23.629 17.890 1956.894 2.670 79.576 4.147 0.53 234416. 0.5416 27.22 0.2161 0.4781 0.0857 0.0388 2.649 23.852 17.449 1975.376 2.695 77.612 4.006 0.53 234725. 0.5168 30.62 0.2431 0.5197 0.0834 0.0390 2.666 24.002 16.966 1987.813 2.712 75.465 3.871 0.53 235056. 0.4924 34.02 0.2701 0.5580 0.0808 0.0391 2.673 24.068 16.440 1993.247 2.719 73.124 3.741 0.53 235411. 0.4684 37.43 0.2972 0.5932 0.0780 0.0391 2.670 24.038 15.869 1990.744 2.716 70.584 3.616 0.53 235790. 0.4448 40.83 0.3242 0.6255 0.0749 0.0388 2.654 23.901 15.252 1979.424 2.700 67.839 3.495 0.53 236192. 0.4215 44.23 0.3512 0.6551 0.0717 0.0384 2.626 23.648 14.588 1958.485 2.672 64.888 3.378 0.53 236619. 0.3985 47.63 0.3782 0.6820 0.0682 0.0378 2.584 23.271 13.878 1927.232 2.629 61.730 3.266 0.53 237069. 0.3758 51.03 0.4052 0.7064 0.0645 0.0370 2.528 22.761 13.122 1885.039 2.572 58.366 3.157 0.53 237544. 0.3532 54.44 0.4322 0.7282 0.0605 0.0359 2.456 22.112 12.319 1831.255 2.498 54.797 3.051 0.53 238044. 0.3307 57.84 0.4592 0.7474 0.0564 0.0346 2.368 21.319 11.474 1765.612 2.409 51.035 2.947 0.53 238567. 0.3083 61.24 0.4862 0.7638 0.0520 0.0331 2.264 20.388 10.591 1688.483 2.303 47.108 2.845 0.53 239115. 0.2859 64.64 0.5133 0.7772 0.0476 0.0314 2.146 19.324 9.677 1600.372 2.183 43.043 2.743 0.53 239687. 0.2635 68.05 0.5403 0.7872 0.0429 0.0295 2.014 18.133 8.737 1501.757 2.049 38.864 2.639 0.54 240282. 0.2409 71.45 0.5673 0.7931 0.0382 0.0273 1.868 16.821 7.777 1393.098 1.900 34.593 2.532 0.54 240902. 0.2181 74.85 0.5943 0.7940 0.0334 0.0250 1.710 15.394 6.801 1274.879 1.739 30.252 2.420 0.54 241546. 0.1949 78.25 0.6213 0.7883 0.0286 0.0225 1.539 13.857 5.814 1147.635 1.566 25.861 2.298 0.54 242214. 0.1711 81.66 0.6483 0.7735 0.0237 0.0199 1.357 12.219 4.821 1011.997 1.381 21.444 2.161 0.54 242905. 0.1465 85.06 0.6753 0.7452 0.0188 0.0170 1.165 10.489 3.828 868.719 1.185 17.025 1.998 0.54 243621. 0.1207 88.46 0.7024 0.6949 0.0140 0.0141 0.964 8.678 2.839 718.723 0.980 12.630 1.792 0.54 244360. 0.0932 91.86 0.7294 0.6045 0.0092 0.0110 0.755 6.800 1.864 563.128 0.768 8.289 1.501 0.54 245124. 0.0633 95.26 0.7564 0.4262 0.0045 0.0079 0.541 4.869 0.907 403.264 0.550 4.036 1.021 0.54 245910. 0.0300 98.67 0.7834 -0.0199 -0.0001 0.0047 0.322 2.900 -0.024 240.132 0.328 -0.108 -0.046 0.54 246707. 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 0.0993 0.0343 3.499 27.567 26.395 2609.232 3.115 117.406 4.588 0.60 266078. 0.7280 3.88 0.0270 0.0757 0.0983 0.0350 3.574 28.160 26.120 2665.332 3.182 116.181 4.445 0.60 266271. 0.7016 7.76 0.0539 0.1465 0.0971 0.0358 3.649 28.747 25.812 2720.932 3.248 114.812 4.303 0.60 266484. 0.6751 11.65 0.0809 0.2126 0.0958 0.0365 3.721 29.319 25.468 2775.041 3.312 113.284 4.163 0.60 266718. 0.6488 15.53 0.1079 0.2741 0.0944 0.0372 3.791 29.864 25.086 2826.605 3.374 111.582 4.025 0.60 266974. 0.6226 19.41 0.1349 0.3312 0.0928 0.0378 3.855 30.369 24.661 2874.454 3.431 109.692 3.891 0.60 267253. 0.5968 23.29 0.1618 0.3841 0.0910 0.0383 3.912 30.822 24.190 2917.324 3.482 107.596 3.761 0.60 267555. 0.5712 27.18 0.1888 0.4330 0.0890 0.0388 3.961 31.208 23.669 2953.859 3.526 105.281 3.634 0.60 267883. 0.5461 31.06 0.2158 0.4782 0.0869 0.0392 4.000 31.513 23.096 2982.648 3.560 102.732 3.512 0.60 268236. 0.5213 34.94 0.2428 0.5200 0.0845 0.0395 4.026 31.719 22.468 3002.233 3.584 99.936 3.394 0.60 268615. 0.4969 38.82 0.2697 0.5584 0.0819 0.0396 4.038 31.814 21.781 3011.149 3.594 96.883 3.281 0.61 269021. 0.4729 42.71 0.2967 0.5938 0.0791 0.0395 4.034 31.780 21.034 3007.971 3.590 93.561 3.172 0.61 269453. 0.4492 46.59 0.3237 0.6264 0.0761 0.0393 4.011 31.604 20.226 2991.343 3.571 89.965 3.067 0.61 269913. 0.4259 50.47 0.3506 0.6562 0.0728 0.0389 3.969 31.274 19.355 2960.042 3.533 86.091 2.966 0.61 270400. 0.4029 54.35 0.3776 0.6835 0.0693 0.0383 3.906 30.777 18.422 2912.999 3.477 81.939 2.868 0.61 270915. 0.3802 58.24 0.4046 0.7082 0.0656 0.0375 3.821 30.103 17.426 2849.270 3.401 77.512 2.774 0.61 271458. 0.3576 62.12 0.4316 0.7305 0.0616 0.0364 3.712 29.243 16.369 2767.880 3.304 72.809 2.682 0.61 272028. 0.3351 66.00 0.4585 0.7502 0.0574 0.0351 3.578 28.192 15.253 2668.352 3.185 67.845 2.593 0.61 272626. 0.3127 69.88 0.4855 0.7672 0.0530 0.0335 3.421 26.954 14.086 2551.219 3.045 62.656 2.504 0.61 273251. 0.2903 73.77 0.5125 0.7814 0.0484 0.0318 3.242 25.539 12.878 2417.251 2.885 57.280 2.416 0.61 273904. 0.2678 77.65 0.5394 0.7923 0.0438 0.0298 3.040 23.953 11.634 2267.182 2.706 51.749 2.328 0.61 274584. 0.2452 81.53 0.5664 0.7993 0.0390 0.0276 2.818 22.205 10.362 2101.718 2.509 46.091 2.236 0.61 275291. 0.2223 85.41 0.5934 0.8015 0.0341 0.0253 2.577 20.302 9.068 1921.595 2.294 40.336 2.140 0.61 276025. 0.1991 89.29 0.6204 0.7974 0.0292 0.0227 2.317 18.253 7.759 1727.633 2.062 34.512 2.037 0.61 276787. 0.1752 93.18 0.6473 0.7847 0.0242 0.0200 2.039 16.068 6.441 1520.790 1.815 28.649 1.921 0.62 277575. 0.1506 97.06 0.6743 0.7590 0.0193 0.0171 1.746 13.758 5.121 1302.217 1.554 22.780 1.784 0.62 278391. 0.1247 100.94 0.7013 0.7122 0.0143 0.0141 1.439 11.340 3.808 1073.318 1.281 16.940 1.609 0.62 279234. 0.0970 104.82 0.7283 0.6262 0.0094 0.0110 1.121 8.831 2.511 835.803 0.998 11.169 1.363 0.62 280104. 0.0667 108.71 0.7552 0.4527 0.0047 0.0078 0.794 6.252 1.239 591.717 0.706 5.513 0.950 0.62 281001. 0.0327 112.59 0.7822 0.0002 0.0000 0.0045 0.460 3.621 0.000 342.723 0.409 0.001 0.000 0.62 281911. 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 0.1004 0.0348 5.051 35.374 33.783 3766.674 3.997 150.266 4.068 0.68 299309. 0.7302 4.36 0.0270 0.0754 0.0994 0.0355 5.161 36.141 33.448 3848.293 4.083 148.779 3.942 0.68 299527. 0.7041 8.73 0.0539 0.1461 0.0983 0.0363 5.270 36.903 33.073 3929.500 4.169 147.107 3.817 0.68 299766. 0.6780 13.09 0.0809 0.2121 0.0971 0.0370 5.376 37.648 32.651 4008.811 4.253 145.232 3.694 0.68 300030. 0.6519 17.46 0.1078 0.2735 0.0957 0.0377 5.478 38.361 32.179 4084.656 4.334 143.133 3.573 0.68 300318. 0.6260 21.82 0.1348 0.3306 0.0941 0.0384 5.572 39.024 31.652 4155.302 4.409 140.788 3.455 0.68 300632. 0.6003 26.19 0.1617 0.3834 0.0923 0.0389 5.658 39.620 31.065 4218.814 4.476 138.177 3.340 0.68 300973. 0.5749 30.55 0.1887 0.4324 0.0904 0.0395 5.730 40.131 30.414 4273.153 4.534 135.280 3.228 0.68 301342. 0.5498 34.92 0.2156 0.4777 0.0883 0.0398 5.788 40.535 29.694 4316.179 4.580 132.078 3.120 0.68 301740. 0.5251 39.28 0.2426 0.5195 0.0859 0.0401 5.828 40.812 28.901 4345.736 4.611 128.552 3.016 0.68 302167. 0.5008 43.65 0.2695 0.5581 0.0833 0.0402 5.846 40.943 28.032 4359.660 4.626 124.688 2.916 0.68 302625. 0.4769 48.01 0.2965 0.5936 0.0805 0.0402 5.841 40.907 27.085 4355.851 4.622 120.473 2.820 0.68 303112. 0.4533 52.38 0.3234 0.6264 0.0775 0.0400 5.810 40.686 26.056 4332.315 4.597 115.899 2.728 0.68 303631. 0.4300 56.74 0.3504 0.6565 0.0742 0.0396 5.749 40.263 24.946 4287.251 4.549 110.959 2.639 0.68 304180. 0.4071 61.11 0.3774 0.6841 0.0706 0.0390 5.658 39.623 23.753 4219.092 4.477 105.654 2.554 0.68 304760. 0.3843 65.47 0.4043 0.7092 0.0668 0.0381 5.534 38.753 22.479 4126.466 4.378 99.986 2.471 0.68 305371. 0.3618 69.84 0.4313 0.7319 0.0628 0.0370 5.375 37.640 21.124 4007.976 4.253 93.958 2.390 0.68 306014. 0.3393 74.20 0.4582 0.7521 0.0585 0.0357 5.180 36.278 19.691 3862.863 4.099 87.584 2.312 0.69 306687. 0.3168 78.57 0.4852 0.7698 0.0541 0.0341 4.951 34.672 18.191 3691.858 3.917 80.914 2.235 0.69 307391. 0.2944 82.93 0.5121 0.7846 0.0495 0.0323 4.688 32.833 16.635 3496.099 3.709 73.993 2.158 0.69 308126. 0.2718 87.29 0.5391 0.7963 0.0447 0.0303 4.394 30.772 15.033 3276.669 3.477 66.865 2.081 0.69 308891. 0.2492 91.66 0.5660 0.8043 0.0398 0.0280 4.069 28.499 13.392 3034.617 3.220 59.569 2.002 0.69 309687. 0.2262 96.02 0.5930 0.8077 0.0348 0.0256 3.716 26.024 11.722 2771.025 2.940 52.140 1.919 0.69 310513. 0.2029 100.39 0.6199 0.8051 0.0298 0.0230 3.335 23.357 10.031 2487.103 2.639 44.617 1.829 0.69 311369. 0.1789 104.75 0.6469 0.7941 0.0248 0.0202 2.929 20.513 8.327 2184.252 2.318 37.039 1.729 0.69 312256. 0.1541 109.12 0.6739 0.7706 0.0197 0.0172 2.500 17.507 6.620 1864.193 1.978 29.447 1.611 0.69 313174. 0.1280 113.48 0.7008 0.7263 0.0146 0.0141 2.051 14.360 4.921 1529.059 1.622 21.890 1.460 0.69 314121. 0.1000 117.85 0.7278 0.6430 0.0096 0.0109 1.584 11.096 3.242 1181.496 1.254 14.419 1.245 0.70 315099. 0.0692 122.21 0.7547 0.4699 0.0047 0.0076 1.106 7.745 1.595 824.712 0.875 7.093 0.877 0.70 316107. 0.0342 126.58 0.7817 -0.0059 0.0000 0.0043 0.619 4.333 -0.011 461.354 0.490 -0.048 -0.011 0.70 317128. 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 0.1017 0.0361 7.198 45.370 42.237 5367.825 5.126 187.871 3.569 0.75 332529. 0.7163 4.84 0.0269 0.0736 0.1008 0.0368 7.339 46.257 41.849 5472.800 5.226 186.146 3.468 0.75 332770. 0.6929 9.69 0.0538 0.1430 0.0997 0.0375 7.479 47.140 41.410 5577.199 5.326 184.193 3.368 0.75 333035. 0.6693 14.53 0.0807 0.2081 0.0985 0.0382 7.616 48.001 40.914 5679.112 5.423 181.987 3.268 0.75 333328. 0.6455 19.37 0.1077 0.2691 0.0972 0.0389 7.746 48.824 40.355 5776.510 5.516 179.498 3.169 0.75 333648. 0.6216 24.21 0.1346 0.3260 0.0957 0.0395 7.868 49.590 39.726 5867.120 5.603 176.699 3.071 0.75 333997. 0.5978 29.06 0.1615 0.3790 0.0940 0.0400 7.977 50.278 39.020 5948.456 5.680 173.561 2.975 0.75 334376. 0.5740 33.90 0.1884 0.4282 0.0921 0.0405 8.070 50.864 38.232 6017.849 5.747 170.056 2.882 0.76 334787. 0.5502 38.74 0.2153 0.4739 0.0899 0.0409 8.143 51.326 37.356 6072.458 5.799 166.159 2.790 0.76 335229. 0.5267 43.59 0.2422 0.5162 0.0876 0.0411 8.193 51.637 36.386 6109.320 5.834 161.846 2.701 0.76 335705. 0.5032 48.43 0.2692 0.5552 0.0850 0.0412 8.214 51.773 35.319 6125.387 5.849 157.097 2.615 0.76 336213. 0.4800 53.27 0.2961 0.5913 0.0822 0.0412 8.204 51.708 34.149 6117.625 5.842 151.895 2.532 0.76 336756. 0.4569 58.11 0.3230 0.6245 0.0792 0.0409 8.158 51.416 32.875 6083.065 5.809 146.227 2.451 0.76 337333. 0.4340 62.96 0.3499 0.6550 0.0758 0.0405 8.072 50.874 31.495 6018.956 5.748 140.088 2.373 0.76 337944. 0.4113 67.80 0.3768 0.6830 0.0723 0.0399 7.943 50.061 30.008 5922.826 5.656 133.476 2.298 0.76 338589. 0.3888 72.64 0.4037 0.7086 0.0684 0.0390 7.768 48.960 28.416 5792.491 5.531 126.396 2.225 0.76 339269. 0.3663 77.48 0.4307 0.7318 0.0643 0.0379 7.544 47.550 26.720 5625.770 5.372 118.850 2.154 0.76 339983. 0.3439 82.33 0.4576 0.7526 0.0600 0.0365 7.270 45.822 24.923 5421.283 5.177 110.855 2.085 0.76 340731. 0.3215 87.17 0.4845 0.7709 0.0555 0.0349 6.946 43.782 23.038 5179.938 4.946 102.472 2.017 0.76 341514. 0.2990 92.01 0.5114 0.7865 0.0508 0.0330 6.576 41.445 21.079 4903.395 4.682 93.760 1.950 0.76 342330. 0.2765 96.86 0.5383 0.7991 0.0459 0.0309 6.160 38.824 19.059 4593.333 4.386 84.774 1.882 0.76 343180. 0.2537 101.70 0.5652 0.8081 0.0409 0.0286 5.701 35.934 16.988 4251.416 4.060 75.563 1.812 0.77 344063. 0.2307 106.54 0.5921 0.8124 0.0358 0.0261 5.202 32.790 14.878 3879.452 3.705 66.176 1.739 0.77 344980. 0.2072 111.38 0.6191 0.8108 0.0307 0.0234 4.666 29.410 12.738 3479.494 3.323 56.658 1.660 0.77 345931. 0.1830 116.23 0.6460 0.8006 0.0255 0.0206 4.096 25.814 10.580 3054.048 2.916 47.059 1.571 0.77 346915. 0.1578 121.07 0.6729 0.7774 0.0203 0.0175 3.495 22.028 8.416 2606.202 2.489 37.434 1.465 0.77 347932. 0.1312 125.91 0.6998 0.7323 0.0151 0.0144 2.869 18.086 6.259 2139.781 2.043 27.839 1.327 0.77 348983. 0.1025 130.76 0.7267 0.6461 0.0099 0.0112 2.225 14.026 4.124 1659.463 1.585 18.344 1.127 0.77 350068. 0.0707 135.60 0.7536 0.4670 0.0049 0.0079 1.570 9.896 2.028 1170.807 1.118 9.019 0.786 0.78 351185. 0.0345 140.44 0.7806 -0.0073 0.0000 0.0046 0.910 5.734 -0.018 678.427 0.648 -0.079 -0.012 0.78 352317. 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 0.1031 0.0402 10.659 61.074 51.794 7948.369 6.900 230.378 2.956 0.83 365732. 0.6569 5.32 0.0269 0.0674 0.1022 0.0408 10.815 61.966 51.366 8064.481 7.001 228.475 2.889 0.83 365996. 0.6394 10.64 0.0538 0.1317 0.1012 0.0413 10.966 62.834 50.877 8177.384 7.099 226.300 2.822 0.83 366288. 0.6216 15.96 0.0807 0.1928 0.1001 0.0419 11.110 63.656 50.319 8284.435 7.192 223.819 2.755 0.83 366609. 0.6035 21.28 0.1075 0.2508 0.0989 0.0424 11.242 64.414 49.684 8383.014 7.277 220.993 2.688 0.83 366960. 0.5852 26.60 0.1344 0.3058 0.0974 0.0428 11.359 65.084 48.962 8470.185 7.353 217.782 2.622 0.83 367344. 0.5666 31.93 0.1613 0.3578 0.0958 0.0432 11.456 65.642 48.145 8542.877 7.416 214.149 2.556 0.83 367762. 0.5477 37.25 0.1882 0.4068 0.0940 0.0435 11.530 66.065 47.225 8597.918 7.464 210.056 2.491 0.83 368214. 0.5287 42.57 0.2151 0.4530 0.0919 0.0436 11.576 66.327 46.193 8632.031 7.494 205.466 2.427 0.83 368702. 0.5095 47.89 0.2420 0.4963 0.0896 0.0437 11.589 66.403 45.042 8641.920 7.502 200.347 2.364 0.83 369226. 0.4900 53.21 0.2688 0.5369 0.0871 0.0436 11.565 66.268 43.766 8624.261 7.487 194.671 2.302 0.83 369787. 0.4703 58.53 0.2957 0.5749 0.0843 0.0434 11.500 65.895 42.360 8575.710 7.445 188.415 2.240 0.83 370385. 0.4503 63.85 0.3226 0.6102 0.0812 0.0429 11.389 65.259 40.819 8493.008 7.373 181.562 2.180 0.83 371021. 0.4301 69.17 0.3495 0.6430 0.0779 0.0423 11.229 64.338 39.142 8373.124 7.269 174.102 2.120 0.83 371695. 0.4097 74.49 0.3764 0.6732 0.0743 0.0415 11.014 63.109 37.328 8213.188 7.130 166.035 2.061 0.83 372407. 0.3889 79.81 0.4033 0.7009 0.0704 0.0405 10.742 61.552 35.379 8010.567 6.954 157.365 2.003 0.84 373156. 0.3680 85.14 0.4302 0.7261 0.0663 0.0393 10.410 59.645 33.295 7762.437 6.739 148.097 1.945 0.84 373943. 0.3467 90.46 0.4570 0.7487 0.0619 0.0378 10.013 57.372 31.081 7466.513 6.482 138.250 1.888 0.84 374768. 0.3251 95.78 0.4839 0.7686 0.0572 0.0360 9.554 54.742 28.753 7124.309 6.185 127.894 1.831 0.84 375629. 0.3031 101.10 0.5108 0.7852 0.0524 0.0341 9.039 51.794 26.328 6740.652 5.852 117.105 1.772 0.84 376528. 0.2807 106.42 0.5377 0.7979 0.0474 0.0319 8.471 48.538 23.820 6316.901 5.484 105.953 1.710 0.84 377464. 0.2578 111.74 0.5646 0.8062 0.0423 0.0296 7.852 44.992 21.246 5855.338 5.083 94.501 1.646 0.84 378436. 0.2343 117.06 0.5915 0.8089 0.0370 0.0271 7.184 41.164 18.618 5357.187 4.651 82.812 1.576 0.84 379445. 0.2100 122.38 0.6184 0.8042 0.0317 0.0244 6.472 37.086 15.950 4826.474 4.190 70.944 1.499 0.84 380490. 0.1849 127.70 0.6452 0.7885 0.0264 0.0216 5.724 32.799 13.255 4268.584 3.706 58.959 1.408 0.85 381572. 0.1584 133.02 0.6721 0.7563 0.0210 0.0187 4.947 28.348 10.549 3689.345 3.203 46.924 1.297 0.85 382690. 0.1301 138.34 0.6990 0.6974 0.0156 0.0157 4.152 23.788 7.849 3095.810 2.688 34.912 1.150 0.85 383844. 0.0995 143.67 0.7259 0.5920 0.0103 0.0126 3.347 19.179 5.173 2496.051 2.167 23.008 0.940 0.85 385035. 0.0660 148.99 0.7528 0.3966 0.0051 0.0096 2.546 14.591 2.542 1898.899 1.648 11.306 0.607 0.85 386262. 0.0299 154.31 0.7797 -0.0061 -0.0001 0.0066 1.758 10.073 -0.026 1310.889 1.138 -0.116 -0.009 0.85 387509. 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 0.1035 0.0475 16.342 85.834 61.926 12186.192 9.697 275.447 2.305 0.90 398959. 0.5601 5.88 0.0272 0.0583 0.1028 0.0480 16.539 86.870 61.497 12333.323 9.815 273.540 2.262 0.90 399246. 0.5477 11.76 0.0545 0.1144 0.1020 0.0486 16.723 87.835 60.998 12470.328 9.924 271.320 2.219 0.90 399564. 0.5351 17.65 0.0817 0.1684 0.1010 0.0490 16.887 88.694 60.417 12592.269 10.021 268.737 2.176 0.90 399916. 0.5224 23.53 0.1090 0.2202 0.0999 0.0494 17.023 89.411 59.743 12694.061 10.102 265.736 2.135 0.90 400302. 0.5095 29.41 0.1362 0.2700 0.0986 0.0497 17.126 89.950 58.962 12770.544 10.162 262.261 2.094 0.91 400726. 0.4966 35.29 0.1635 0.3179 0.0971 0.0499 17.187 90.275 58.061 12816.694 10.199 258.255 2.055 0.91 401188. 0.4835 41.18 0.1907 0.3640 0.0954 0.0500 17.202 90.353 57.028 12827.811 10.208 253.662 2.016 0.91 401689. 0.4703 47.06 0.2180 0.4083 0.0934 0.0499 17.165 90.155 55.852 12799.729 10.186 248.429 1.979 0.91 402231. 0.4568 52.94 0.2452 0.4509 0.0912 0.0496 17.069 89.654 54.521 12728.617 10.129 242.507 1.943 0.91 402815. 0.4430 58.82 0.2724 0.4918 0.0887 0.0491 16.911 88.824 53.024 12610.765 10.035 235.851 1.907 0.91 403441. 0.4289 64.70 0.2997 0.5310 0.0859 0.0485 16.688 87.654 51.356 12444.550 9.903 228.432 1.872 0.91 404110. 0.4143 70.59 0.3269 0.5683 0.0828 0.0476 16.398 86.126 49.511 12227.689 9.730 220.227 1.837 0.91 404822. 0.3991 76.47 0.3542 0.6038 0.0794 0.0466 16.036 84.228 47.487 11958.174 9.516 211.221 1.801 0.91 405576. 0.3833 82.35 0.3814 0.6373 0.0757 0.0453 15.602 81.947 45.282 11634.287 9.258 201.412 1.765 0.91 406373. 0.3669 88.23 0.4087 0.6687 0.0717 0.0438 15.092 79.271 42.897 11254.446 8.956 190.807 1.729 0.91 407213. 0.3497 94.12 0.4359 0.6979 0.0674 0.0421 14.505 76.188 40.335 10816.701 8.608 179.411 1.691 0.91 408095. 0.3317 100.00 0.4631 0.7245 0.0629 0.0402 13.840 72.691 37.604 10320.174 8.213 167.263 1.653 0.91 409019. 0.3130 105.88 0.4904 0.7485 0.0581 0.0380 13.098 68.797 34.726 9767.452 7.773 154.461 1.613 0.92 409985. 0.2935 111.76 0.5176 0.7685 0.0530 0.0357 12.302 64.615 31.722 9173.721 7.300 141.101 1.568 0.92 410992. 0.2728 117.64 0.5449 0.7822 0.0478 0.0333 11.475 60.272 28.611 8557.086 6.810 127.264 1.517 0.92 412040. 0.2505 123.53 0.5721 0.7871 0.0425 0.0309 10.634 55.851 25.410 7929.462 6.310 113.026 1.453 0.92 413129. 0.2263 129.41 0.5994 0.7798 0.0370 0.0284 9.795 51.449 22.135 7304.482 5.813 98.457 1.374 0.92 414258. 0.1997 135.29 0.6266 0.7606 0.0315 0.0259 8.923 46.866 18.812 6653.786 5.295 83.678 1.282 0.92 415428. 0.1718 141.17 0.6539 0.7249 0.0259 0.0233 8.030 42.175 15.463 5987.746 4.765 68.778 1.171 0.92 416638. 0.1422 147.06 0.6811 0.6658 0.0202 0.0207 7.131 37.455 12.108 5317.666 4.232 53.856 1.033 0.93 417888. 0.1110 152.94 0.7083 0.5734 0.0147 0.0181 6.241 32.780 8.775 4653.861 3.703 39.030 0.855 0.93 419179. 0.0782 158.82 0.7356 0.4329 0.0092 0.0156 5.374 28.226 5.493 4007.380 3.189 24.432 0.622 0.93 420511. 0.0450 164.70 0.7628 0.2218 0.0038 0.0132 4.544 23.866 2.295 3388.295 2.696 10.208 0.307 0.93 421882. 0.0144 170.59 0.7901