20.5x12WE (205x12WE.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 0.1042 0.0415 0.012 0.762 0.587 9.012 0.086 2.609 29.525 0.08 46791. 0.6473 0.49 0.0253 0.0619 0.1026 0.0420 0.012 0.770 0.578 9.115 0.087 2.569 28.742 0.08 46826. 0.6252 0.98 0.0506 0.1205 0.1009 0.0424 0.012 0.779 0.568 9.211 0.088 2.526 27.963 0.08 46863. 0.6031 1.47 0.0759 0.1757 0.0990 0.0428 0.012 0.786 0.557 9.296 0.089 2.479 27.190 0.08 46904. 0.5810 1.97 0.1013 0.2277 0.0970 0.0431 0.013 0.792 0.546 9.370 0.089 2.428 26.427 0.08 46948. 0.5589 2.46 0.1266 0.2766 0.0948 0.0434 0.013 0.797 0.534 9.429 0.090 2.374 25.674 0.08 46995. 0.5369 2.95 0.1519 0.3223 0.0925 0.0436 0.013 0.801 0.521 9.471 0.090 2.316 24.932 0.08 47045. 0.5149 3.44 0.1772 0.3650 0.0900 0.0437 0.013 0.802 0.507 9.494 0.091 2.253 24.201 0.08 47099. 0.4930 3.93 0.2025 0.4047 0.0873 0.0437 0.013 0.803 0.492 9.496 0.091 2.187 23.482 0.08 47157. 0.4713 4.42 0.2278 0.4416 0.0845 0.0436 0.013 0.801 0.476 9.473 0.090 2.116 22.775 0.08 47218. 0.4496 4.91 0.2531 0.4756 0.0815 0.0434 0.013 0.797 0.459 9.424 0.090 2.040 22.077 0.08 47283. 0.4280 5.41 0.2785 0.5069 0.0783 0.0430 0.013 0.790 0.441 9.346 0.089 1.960 21.389 0.08 47352. 0.4064 5.90 0.3038 0.5354 0.0749 0.0425 0.012 0.781 0.422 9.237 0.088 1.876 20.709 0.08 47424. 0.3849 6.39 0.3291 0.5611 0.0714 0.0419 0.012 0.769 0.402 9.093 0.087 1.786 20.033 0.08 47501. 0.3634 6.88 0.3544 0.5839 0.0676 0.0410 0.012 0.753 0.380 8.913 0.085 1.692 19.359 0.08 47582. 0.3418 7.37 0.3797 0.6038 0.0637 0.0400 0.012 0.735 0.358 8.698 0.083 1.594 18.684 0.08 47666. 0.3201 7.86 0.4050 0.6206 0.0596 0.0389 0.011 0.714 0.335 8.448 0.081 1.491 18.002 0.08 47755. 0.2984 8.35 0.4304 0.6339 0.0554 0.0376 0.011 0.690 0.312 8.165 0.078 1.386 17.308 0.08 47848. 0.2765 8.85 0.4557 0.6435 0.0510 0.0361 0.011 0.663 0.287 7.848 0.075 1.277 16.594 0.08 47944. 0.2545 9.34 0.4810 0.6489 0.0466 0.0345 0.010 0.634 0.262 7.499 0.072 1.166 15.852 0.08 48045. 0.2323 9.83 0.5063 0.6494 0.0420 0.0328 0.010 0.602 0.237 7.118 0.068 1.052 15.072 0.08 48150. 0.2098 10.32 0.5316 0.6442 0.0374 0.0309 0.009 0.567 0.211 6.707 0.064 0.937 14.239 0.08 48259. 0.1870 10.81 0.5569 0.6320 0.0327 0.0288 0.008 0.530 0.184 6.266 0.060 0.819 13.335 0.08 48372. 0.1638 11.30 0.5822 0.6112 0.0280 0.0267 0.008 0.490 0.158 5.797 0.055 0.701 12.334 0.08 48489. 0.1402 11.79 0.6076 0.5792 0.0233 0.0244 0.007 0.448 0.131 5.302 0.051 0.582 11.201 0.08 48610. 0.1160 12.29 0.6329 0.5322 0.0185 0.0220 0.006 0.404 0.104 4.782 0.046 0.463 9.881 0.08 48735. 0.0913 12.78 0.6582 0.4645 0.0138 0.0195 0.006 0.358 0.078 4.239 0.040 0.345 8.293 0.08 48865. 0.0661 13.27 0.6835 0.3664 0.0091 0.0169 0.005 0.311 0.051 3.677 0.035 0.227 6.299 0.08 48998. 0.0407 13.76 0.7088 0.2207 0.0044 0.0143 0.004 0.262 0.025 3.098 0.030 0.111 3.658 0.08 49136. 0.0166 14.25 0.7341 -0.0067 -0.0001 0.0115 0.003 0.212 -0.001 2.506 0.024 -0.003 -0.108 0.08 49276. 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 0.1046 0.0389 0.091 2.861 2.356 67.689 0.323 10.479 15.787 0.16 93580. 0.6936 0.99 0.0254 0.0663 0.1030 0.0395 0.092 2.898 2.320 68.580 0.327 10.319 15.343 0.16 93650. 0.6689 1.97 0.0508 0.1289 0.1013 0.0399 0.093 2.933 2.281 69.411 0.331 10.144 14.903 0.16 93725. 0.6442 2.96 0.0762 0.1877 0.0994 0.0404 0.094 2.965 2.238 70.163 0.335 9.956 14.470 0.16 93807. 0.6197 3.95 0.1016 0.2429 0.0974 0.0407 0.095 2.993 2.193 70.819 0.338 9.754 14.045 0.16 93895. 0.5953 4.93 0.1270 0.2946 0.0952 0.0411 0.096 3.016 2.144 71.358 0.341 9.536 13.627 0.16 93989. 0.5711 5.92 0.1524 0.3429 0.0929 0.0413 0.096 3.033 2.091 71.761 0.343 9.302 13.218 0.16 94091. 0.5471 6.90 0.1778 0.3880 0.0904 0.0414 0.097 3.043 2.035 72.008 0.344 9.051 12.818 0.16 94199. 0.5233 7.89 0.2032 0.4299 0.0877 0.0415 0.097 3.046 1.975 72.077 0.344 8.783 12.426 0.16 94315. 0.4998 8.88 0.2287 0.4687 0.0849 0.0414 0.096 3.041 1.911 71.948 0.344 8.498 12.044 0.16 94438. 0.4765 9.86 0.2541 0.5047 0.0818 0.0412 0.096 3.026 1.842 71.601 0.342 8.194 11.670 0.16 94569. 0.4534 10.85 0.2795 0.5377 0.0786 0.0409 0.095 3.001 1.770 71.015 0.339 7.873 11.304 0.16 94708. 0.4305 11.84 0.3049 0.5680 0.0752 0.0404 0.094 2.965 1.693 70.167 0.335 7.532 10.946 0.16 94854. 0.4077 12.82 0.3303 0.5955 0.0716 0.0397 0.093 2.918 1.612 69.035 0.330 7.171 10.593 0.16 95009. 0.3850 13.81 0.3557 0.6202 0.0678 0.0389 0.091 2.857 1.527 67.604 0.323 6.792 10.245 0.16 95171. 0.3623 14.80 0.3811 0.6421 0.0639 0.0379 0.088 2.784 1.438 65.875 0.315 6.395 9.900 0.16 95342. 0.3398 15.78 0.4065 0.6611 0.0598 0.0367 0.086 2.699 1.345 63.854 0.305 5.984 9.555 0.16 95520. 0.3172 16.77 0.4319 0.6770 0.0555 0.0354 0.083 2.601 1.250 61.546 0.294 5.558 9.209 0.16 95707. 0.2946 17.76 0.4573 0.6894 0.0511 0.0339 0.079 2.492 1.151 58.956 0.281 5.121 8.857 0.16 95901. 0.2720 18.74 0.4827 0.6980 0.0467 0.0323 0.075 2.370 1.050 56.089 0.268 4.673 8.495 0.16 96104. 0.2492 19.73 0.5081 0.7021 0.0421 0.0305 0.071 2.238 0.948 52.953 0.253 4.216 8.118 0.16 96315. 0.2262 20.71 0.5335 0.7010 0.0375 0.0285 0.066 2.094 0.843 49.553 0.237 3.751 7.719 0.16 96534. 0.2029 21.70 0.5589 0.6934 0.0328 0.0264 0.062 1.940 0.738 45.899 0.219 3.281 7.289 0.17 96762. 0.1792 22.69 0.5843 0.6777 0.0280 0.0242 0.056 1.775 0.631 42.002 0.201 2.807 6.814 0.17 96997. 0.1549 23.67 0.6097 0.6511 0.0233 0.0218 0.051 1.601 0.524 37.875 0.181 2.330 6.273 0.17 97241. 0.1300 24.66 0.6351 0.6093 0.0185 0.0193 0.045 1.417 0.417 33.534 0.160 1.853 5.636 0.17 97493. 0.1041 25.65 0.6606 0.5450 0.0138 0.0167 0.039 1.226 0.310 29.000 0.138 1.379 4.848 0.17 97754. 0.0772 26.63 0.6860 0.4452 0.0091 0.0140 0.033 1.027 0.204 24.298 0.116 0.909 3.813 0.17 98022. 0.0493 27.62 0.7114 0.2828 0.0045 0.0112 0.026 0.822 0.100 19.456 0.093 0.446 2.336 0.17 98299. 0.0212 28.61 0.7368 -0.0074 -0.0001 0.0083 0.019 0.613 -0.002 14.494 0.069 -0.008 -0.059 0.17 98580. 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 0.1051 0.0380 0.299 6.276 5.325 222.767 0.709 23.687 10.843 0.24 140366. 0.7162 1.48 0.0254 0.0684 0.1035 0.0385 0.303 6.364 5.244 225.886 0.719 23.326 10.530 0.24 140471. 0.6902 2.96 0.0509 0.1328 0.1018 0.0390 0.307 6.446 5.156 228.802 0.728 22.934 10.221 0.24 140584. 0.6643 4.44 0.0763 0.1932 0.0999 0.0395 0.310 6.521 5.061 231.452 0.737 22.511 9.918 0.24 140707. 0.6386 5.93 0.1017 0.2499 0.0979 0.0399 0.313 6.586 4.958 233.773 0.744 22.055 9.620 0.24 140839. 0.6131 7.41 0.1272 0.3029 0.0957 0.0402 0.316 6.641 4.848 235.699 0.750 21.563 9.329 0.24 140981. 0.5879 8.89 0.1526 0.3524 0.0934 0.0404 0.318 6.682 4.729 237.159 0.755 21.036 9.045 0.24 141134. 0.5630 10.37 0.1780 0.3985 0.0909 0.0406 0.319 6.708 4.602 238.084 0.758 20.470 8.767 0.24 141297. 0.5383 11.85 0.2035 0.4414 0.0882 0.0406 0.320 6.717 4.466 238.401 0.759 19.866 8.497 0.24 141471. 0.5140 13.33 0.2289 0.4812 0.0853 0.0406 0.319 6.707 4.321 238.039 0.758 19.221 8.234 0.24 141657. 0.4899 14.81 0.2543 0.5181 0.0823 0.0404 0.318 6.675 4.167 236.926 0.754 18.535 7.977 0.24 141854. 0.4661 16.29 0.2798 0.5520 0.0790 0.0401 0.315 6.621 4.003 234.990 0.748 17.808 7.727 0.24 142062. 0.4426 17.78 0.3052 0.5831 0.0756 0.0396 0.311 6.541 3.830 232.157 0.739 17.037 7.483 0.25 142282. 0.4192 19.26 0.3307 0.6116 0.0720 0.0389 0.306 6.433 3.647 228.341 0.727 16.222 7.244 0.25 142515. 0.3960 20.74 0.3561 0.6373 0.0682 0.0381 0.300 6.297 3.454 223.495 0.711 15.363 7.010 0.25 142759. 0.3729 22.22 0.3815 0.6603 0.0642 0.0371 0.292 6.131 3.252 217.618 0.693 14.466 6.779 0.25 143015. 0.3499 23.70 0.4070 0.6805 0.0601 0.0359 0.283 5.937 3.043 210.727 0.671 13.534 6.549 0.25 143284. 0.3270 25.18 0.4324 0.6977 0.0558 0.0346 0.272 5.715 2.826 202.838 0.646 12.571 6.320 0.25 143564. 0.3041 26.66 0.4578 0.7117 0.0514 0.0331 0.260 5.465 2.604 193.968 0.617 11.581 6.088 0.25 143857. 0.2812 28.14 0.4833 0.7221 0.0469 0.0314 0.247 5.188 2.376 184.134 0.586 10.568 5.852 0.25 144162. 0.2582 29.63 0.5087 0.7283 0.0423 0.0296 0.232 4.884 2.143 173.357 0.552 9.534 5.608 0.25 144479. 0.2350 31.11 0.5341 0.7297 0.0377 0.0276 0.217 4.555 1.907 161.660 0.515 8.483 5.351 0.25 144809. 0.2115 32.59 0.5596 0.7251 0.0329 0.0254 0.200 4.200 1.668 149.074 0.475 7.419 5.075 0.25 145151. 0.1876 34.07 0.5850 0.7127 0.0282 0.0231 0.182 3.821 1.427 135.637 0.432 6.347 4.772 0.25 145505. 0.1631 35.55 0.6104 0.6899 0.0234 0.0207 0.163 3.420 1.185 121.394 0.386 5.270 4.426 0.25 145872. 0.1379 37.03 0.6359 0.6522 0.0186 0.0181 0.143 2.998 0.942 106.404 0.339 4.192 4.017 0.25 146251. 0.1116 38.51 0.6613 0.5920 0.0138 0.0155 0.122 2.556 0.701 90.738 0.289 3.120 3.506 0.25 146642. 0.0840 40.00 0.6867 0.4940 0.0091 0.0127 0.100 2.099 0.463 74.485 0.237 2.058 2.818 0.25 147046. 0.0549 41.48 0.7122 0.3254 0.0045 0.0098 0.077 1.627 0.228 57.744 0.184 1.013 1.790 0.25 147462. 0.0245 42.96 0.7376 -0.0054 -0.0001 0.0069 0.054 1.143 -0.003 40.575 0.129 -0.012 -0.029 0.25 147883. 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 0.1058 0.0376 0.701 11.040 9.523 522.481 1.247 42.359 8.267 0.33 187146. 0.7302 1.98 0.0254 0.0695 0.1042 0.0381 0.711 11.201 9.379 530.068 1.265 41.718 8.026 0.33 187286. 0.7035 3.95 0.0509 0.1349 0.1024 0.0386 0.720 11.351 9.223 537.171 1.282 41.023 7.787 0.33 187437. 0.6769 5.93 0.0763 0.1963 0.1005 0.0391 0.729 11.487 9.054 543.637 1.298 40.271 7.554 0.33 187601. 0.6506 7.90 0.1018 0.2538 0.0985 0.0395 0.737 11.607 8.871 549.315 1.311 39.459 7.325 0.33 187778. 0.6245 9.88 0.1272 0.3076 0.0963 0.0398 0.743 11.707 8.675 554.044 1.323 38.585 7.102 0.33 187968. 0.5987 11.86 0.1527 0.3578 0.0940 0.0401 0.748 11.784 8.463 557.656 1.331 37.645 6.884 0.33 188172. 0.5732 13.83 0.1781 0.4046 0.0915 0.0403 0.751 11.833 8.237 559.980 1.337 36.636 6.671 0.33 188391. 0.5480 15.81 0.2036 0.4481 0.0888 0.0403 0.752 11.851 7.994 560.840 1.339 35.558 6.465 0.33 188624. 0.5232 17.78 0.2290 0.4884 0.0859 0.0403 0.751 11.834 7.735 560.063 1.337 34.407 6.264 0.33 188872. 0.4987 19.76 0.2545 0.5258 0.0828 0.0401 0.748 11.780 7.460 557.477 1.331 33.182 6.070 0.33 189135. 0.4745 21.74 0.2799 0.5603 0.0796 0.0398 0.741 11.683 7.168 552.910 1.320 31.882 5.880 0.33 189413. 0.4506 23.71 0.3054 0.5920 0.0762 0.0393 0.732 11.541 6.858 546.178 1.304 30.504 5.695 0.33 189708. 0.4269 25.69 0.3308 0.6211 0.0725 0.0386 0.720 11.349 6.530 537.079 1.282 29.046 5.515 0.33 190018. 0.4034 27.67 0.3563 0.6475 0.0687 0.0378 0.705 11.104 6.185 525.488 1.255 27.511 5.338 0.33 190345. 0.3800 29.64 0.3817 0.6712 0.0647 0.0368 0.686 10.806 5.824 511.405 1.221 25.905 5.165 0.33 190687. 0.3568 31.62 0.4072 0.6922 0.0605 0.0356 0.664 10.457 5.449 494.863 1.181 24.236 4.994 0.33 191046. 0.3337 33.59 0.4326 0.7104 0.0562 0.0342 0.638 10.056 5.061 475.901 1.136 22.512 4.824 0.33 191421. 0.3106 35.57 0.4581 0.7255 0.0518 0.0327 0.610 9.605 4.663 454.556 1.085 20.739 4.652 0.33 191812. 0.2875 37.55 0.4835 0.7372 0.0472 0.0310 0.578 9.105 4.254 430.871 1.029 18.924 4.479 0.33 192219. 0.2644 39.52 0.5090 0.7449 0.0426 0.0291 0.543 8.556 3.838 404.893 0.967 17.072 4.299 0.33 192643. 0.2411 41.50 0.5344 0.7481 0.0379 0.0271 0.505 7.959 3.415 376.680 0.899 15.190 4.112 0.33 193083. 0.2175 43.47 0.5599 0.7455 0.0332 0.0249 0.464 7.318 2.987 346.304 0.827 13.285 3.912 0.33 193539. 0.1935 45.45 0.5853 0.7356 0.0284 0.0226 0.421 6.632 2.555 313.854 0.749 11.363 3.692 0.33 194012. 0.1689 47.43 0.6108 0.7157 0.0236 0.0201 0.375 5.905 2.121 279.447 0.667 9.434 3.442 0.33 194501. 0.1435 49.40 0.6362 0.6814 0.0187 0.0175 0.326 5.139 1.687 243.222 0.581 7.504 3.146 0.33 195008. 0.1170 51.38 0.6617 0.6246 0.0139 0.0148 0.275 4.339 1.255 205.355 0.490 5.584 2.773 0.33 195530. 0.0889 53.35 0.6871 0.5291 0.0092 0.0119 0.223 3.509 0.828 166.059 0.396 3.683 2.262 0.33 196069. 0.0589 55.33 0.7125 0.3572 0.0045 0.0090 0.168 2.654 0.408 125.585 0.300 1.813 1.473 0.33 196625. 0.0269 57.31 0.7380 -0.0066 -0.0001 0.0060 0.113 1.776 -0.005 84.045 0.201 -0.022 -0.026 0.33 197184. 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 0.1065 0.0375 1.366 17.216 14.992 1018.431 1.945 66.683 6.677 0.41 233917. 0.7399 2.47 0.0254 0.0702 0.1050 0.0381 1.386 17.472 14.767 1033.586 1.974 65.686 6.480 0.41 234093. 0.7128 4.94 0.0509 0.1361 0.1032 0.0386 1.405 17.712 14.524 1047.785 2.001 64.602 6.287 0.41 234283. 0.6858 7.41 0.0763 0.1980 0.1013 0.0391 1.422 17.931 14.260 1060.727 2.026 63.429 6.098 0.41 234488. 0.6591 9.88 0.1018 0.2560 0.0993 0.0395 1.438 18.123 13.975 1072.108 2.048 62.161 5.912 0.41 234710. 0.6326 12.35 0.1272 0.3102 0.0971 0.0398 1.450 18.284 13.668 1081.604 2.066 60.794 5.732 0.41 234948. 0.6065 14.82 0.1526 0.3608 0.0948 0.0401 1.460 18.407 13.337 1088.887 2.080 59.322 5.555 0.41 235204. 0.5807 17.29 0.1781 0.4080 0.0923 0.0403 1.467 18.487 12.982 1093.610 2.089 57.743 5.384 0.41 235477. 0.5553 19.75 0.2035 0.4519 0.0896 0.0403 1.469 18.518 12.602 1095.431 2.092 56.052 5.218 0.41 235769. 0.5302 22.22 0.2290 0.4926 0.0867 0.0403 1.467 18.494 12.196 1094.000 2.089 54.247 5.056 0.41 236079. 0.5054 24.69 0.2544 0.5304 0.0836 0.0401 1.460 18.409 11.763 1088.978 2.080 52.324 4.900 0.41 236409. 0.4810 27.16 0.2798 0.5653 0.0803 0.0398 1.448 18.257 11.304 1080.023 2.063 50.281 4.747 0.41 236758. 0.4569 29.63 0.3053 0.5975 0.0769 0.0393 1.431 18.033 10.817 1066.776 2.037 48.116 4.599 0.41 237126. 0.4330 32.10 0.3307 0.6270 0.0732 0.0386 1.407 17.730 10.302 1048.832 2.003 45.824 4.455 0.41 237515. 0.4093 34.57 0.3562 0.6539 0.0694 0.0378 1.376 17.343 9.759 1025.932 1.959 43.408 4.314 0.41 237923. 0.3858 37.04 0.3816 0.6782 0.0653 0.0368 1.338 16.872 9.191 998.066 1.906 40.880 4.177 0.41 238352. 0.3624 39.51 0.4070 0.6999 0.0611 0.0355 1.294 16.318 8.600 965.298 1.844 38.252 4.041 0.41 238801. 0.3392 41.98 0.4325 0.7188 0.0568 0.0342 1.244 15.682 7.989 927.704 1.772 35.536 3.906 0.41 239270. 0.3160 44.45 0.4579 0.7348 0.0523 0.0326 1.187 14.967 7.361 885.357 1.691 32.742 3.771 0.41 239759. 0.2929 46.92 0.4834 0.7475 0.0477 0.0309 1.124 14.172 6.718 838.339 1.601 29.880 3.634 0.41 240268. 0.2696 49.39 0.5088 0.7566 0.0431 0.0290 1.055 13.300 6.061 786.746 1.503 26.960 3.494 0.41 240798. 0.2462 51.86 0.5342 0.7612 0.0383 0.0269 0.980 12.352 5.394 730.689 1.396 23.993 3.348 0.41 241348. 0.2226 54.32 0.5597 0.7604 0.0335 0.0247 0.899 11.331 4.718 670.314 1.280 20.988 3.193 0.41 241919. 0.1985 56.79 0.5851 0.7526 0.0287 0.0223 0.812 10.241 4.037 605.799 1.157 17.957 3.023 0.41 242510. 0.1738 59.26 0.6106 0.7352 0.0238 0.0198 0.721 9.084 3.353 537.370 1.026 14.913 2.830 0.41 243121. 0.1483 61.73 0.6360 0.7039 0.0190 0.0171 0.624 7.866 2.668 465.311 0.889 11.868 2.601 0.41 243754. 0.1216 64.20 0.6614 0.6504 0.0141 0.0144 0.523 6.592 1.987 389.972 0.745 8.838 2.311 0.42 244407. 0.0932 66.67 0.6869 0.5581 0.0093 0.0115 0.418 5.271 1.313 311.781 0.595 5.838 1.910 0.42 245080. 0.0626 69.14 0.7123 0.3860 0.0046 0.0085 0.310 3.909 0.649 231.241 0.442 2.888 1.273 0.42 245774. 0.0294 71.61 0.7378 -0.0019 0.0000 0.0055 0.199 2.511 -0.002 148.558 0.284 -0.009 -0.006 0.42 246472. 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 0.1075 0.0377 2.370 24.900 21.789 1767.590 2.813 96.918 5.591 0.49 280678. 0.7470 2.96 0.0254 0.0705 0.1060 0.0382 2.406 25.278 21.468 1794.402 2.856 95.489 5.426 0.49 280889. 0.7196 5.93 0.0509 0.1368 0.1042 0.0388 2.440 25.632 21.118 1819.536 2.896 93.935 5.264 0.49 281118. 0.6924 8.89 0.0763 0.1990 0.1024 0.0393 2.471 25.955 20.739 1842.453 2.932 92.249 5.106 0.49 281365. 0.6655 11.85 0.1018 0.2572 0.1003 0.0397 2.498 26.239 20.329 1862.615 2.964 90.423 4.950 0.49 281632. 0.6389 14.81 0.1272 0.3117 0.0981 0.0401 2.520 26.476 19.886 1879.458 2.991 88.452 4.799 0.49 281919. 0.6125 17.78 0.1526 0.3625 0.0958 0.0403 2.538 26.658 19.408 1892.390 3.012 86.329 4.652 0.49 282227. 0.5866 20.74 0.1781 0.4100 0.0933 0.0405 2.549 26.777 18.895 1900.808 3.025 84.047 4.509 0.49 282556. 0.5610 23.70 0.2035 0.4541 0.0905 0.0406 2.553 26.823 18.345 1904.102 3.030 81.601 4.370 0.49 282907. 0.5357 26.67 0.2289 0.4951 0.0876 0.0405 2.550 26.789 17.758 1901.661 3.027 78.986 4.235 0.49 283281. 0.5109 29.63 0.2544 0.5332 0.0845 0.0403 2.538 26.665 17.131 1892.882 3.013 76.199 4.105 0.49 283677. 0.4863 32.59 0.2798 0.5684 0.0813 0.0400 2.517 26.444 16.465 1877.171 2.988 73.236 3.978 0.49 284097. 0.4621 35.55 0.3053 0.6009 0.0778 0.0395 2.486 26.116 15.758 1853.896 2.951 70.093 3.855 0.49 284540. 0.4381 38.52 0.3307 0.6308 0.0741 0.0388 2.444 25.672 15.010 1822.355 2.900 66.764 3.736 0.49 285008. 0.4143 41.48 0.3561 0.6582 0.0702 0.0380 2.390 25.104 14.221 1782.069 2.836 63.253 3.619 0.49 285499. 0.3907 44.44 0.3816 0.6830 0.0661 0.0369 2.324 24.413 13.394 1733.003 2.758 59.576 3.506 0.49 286014. 0.3672 47.41 0.4070 0.7053 0.0619 0.0357 2.247 23.600 12.534 1675.271 2.666 55.752 3.394 0.49 286554. 0.3439 50.37 0.4324 0.7249 0.0575 0.0343 2.158 22.666 11.645 1609.003 2.561 51.797 3.283 0.49 287117. 0.3206 53.33 0.4579 0.7416 0.0530 0.0327 2.058 21.614 10.730 1534.337 2.442 47.726 3.172 0.49 287705. 0.2974 56.30 0.4833 0.7552 0.0483 0.0309 1.946 20.446 9.792 1451.414 2.310 43.556 3.060 0.49 288317. 0.2741 59.26 0.5088 0.7653 0.0436 0.0290 1.824 19.164 8.835 1360.402 2.165 39.299 2.946 0.49 288953. 0.2506 62.22 0.5342 0.7711 0.0388 0.0269 1.692 17.771 7.862 1261.505 2.008 34.972 2.827 0.49 289614. 0.2269 65.18 0.5596 0.7718 0.0339 0.0246 1.549 16.270 6.877 1154.971 1.838 30.589 2.701 0.50 290299. 0.2027 68.15 0.5851 0.7657 0.0290 0.0222 1.396 14.666 5.883 1041.120 1.657 26.168 2.563 0.50 291009. 0.1779 71.11 0.6105 0.7504 0.0241 0.0196 1.234 12.965 4.884 920.354 1.465 21.725 2.407 0.50 291743. 0.1523 74.07 0.6359 0.7215 0.0192 0.0169 1.064 11.173 3.885 793.173 1.262 17.282 2.222 0.50 292502. 0.1253 77.04 0.6614 0.6708 0.0143 0.0141 0.885 9.300 2.891 660.201 1.051 12.859 1.986 0.50 293286. 0.0967 80.00 0.6868 0.5808 0.0094 0.0111 0.700 7.356 1.907 522.200 0.831 8.481 1.656 0.50 294095. 0.0655 82.96 0.7123 0.4073 0.0046 0.0081 0.510 5.354 0.938 380.065 0.605 4.174 1.120 0.50 294927. 0.0310 85.92 0.7377 -0.0094 -0.0001 0.0050 0.314 3.297 -0.013 234.059 0.373 -0.057 -0.025 0.50 295761. 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 0.1088 0.0380 3.802 34.231 29.994 2834.971 3.867 133.415 4.799 0.57 327425. 0.7523 3.48 0.0256 0.0710 0.1072 0.0386 3.861 34.762 29.558 2878.952 3.927 131.473 4.657 0.57 327673. 0.7247 6.95 0.0512 0.1377 0.1055 0.0392 3.916 35.260 29.082 2920.172 3.984 129.355 4.517 0.57 327943. 0.6972 10.43 0.0768 0.2003 0.1036 0.0397 3.966 35.713 28.564 2957.720 4.035 127.051 4.380 0.57 328234. 0.6701 13.91 0.1023 0.2589 0.1015 0.0401 4.011 36.112 28.002 2990.717 4.080 124.552 4.247 0.57 328549. 0.6432 17.38 0.1279 0.3137 0.0993 0.0405 4.047 36.444 27.393 3018.211 4.117 121.846 4.117 0.57 328888. 0.6167 20.86 0.1535 0.3649 0.0969 0.0408 4.076 36.698 26.737 3039.224 4.146 118.925 3.990 0.57 329251. 0.5905 24.34 0.1791 0.4126 0.0944 0.0410 4.094 36.861 26.030 3052.752 4.165 115.780 3.867 0.57 329640. 0.5648 27.81 0.2047 0.4571 0.0916 0.0410 4.101 36.922 25.270 3057.791 4.171 112.402 3.748 0.57 330055. 0.5393 31.29 0.2303 0.4984 0.0887 0.0410 4.095 36.868 24.457 3053.326 4.165 108.787 3.633 0.57 330496. 0.5143 34.77 0.2558 0.5367 0.0855 0.0408 4.075 36.687 23.590 3038.368 4.145 104.927 3.521 0.57 330965. 0.4896 38.24 0.2814 0.5723 0.0822 0.0404 4.039 36.368 22.666 3011.933 4.109 100.819 3.413 0.57 331461. 0.4651 41.72 0.3070 0.6051 0.0786 0.0399 3.987 35.898 21.685 2972.998 4.056 96.456 3.308 0.57 331985. 0.4410 45.20 0.3326 0.6353 0.0749 0.0392 3.916 35.263 20.645 2920.409 3.984 91.831 3.206 0.57 332537. 0.4170 48.67 0.3582 0.6630 0.0709 0.0383 3.826 34.454 19.548 2853.387 3.893 86.948 3.107 0.57 333117. 0.3932 52.15 0.3838 0.6883 0.0667 0.0372 3.717 33.470 18.398 2771.893 3.781 81.832 3.010 0.57 333726. 0.3696 55.63 0.4094 0.7110 0.0624 0.0359 3.589 32.313 17.201 2676.126 3.651 76.509 2.915 0.57 334363. 0.3461 59.10 0.4349 0.7310 0.0579 0.0344 3.441 30.987 15.963 2566.307 3.501 71.001 2.821 0.57 335028. 0.3226 62.58 0.4605 0.7483 0.0533 0.0328 3.276 29.494 14.688 2442.671 3.332 65.332 2.727 0.58 335722. 0.2992 66.06 0.4861 0.7624 0.0485 0.0309 3.092 27.838 13.382 2305.461 3.145 59.521 2.633 0.58 336445. 0.2757 69.53 0.5117 0.7730 0.0437 0.0289 2.890 26.020 12.048 2154.963 2.940 53.591 2.536 0.58 337196. 0.2519 73.01 0.5373 0.7795 0.0388 0.0267 2.671 24.047 10.693 1991.522 2.717 47.561 2.435 0.58 337975. 0.2279 76.49 0.5629 0.7807 0.0338 0.0244 2.435 21.922 9.320 1815.572 2.477 41.454 2.328 0.58 338784. 0.2034 79.96 0.5885 0.7752 0.0288 0.0218 2.183 19.653 7.935 1627.653 2.220 35.294 2.211 0.58 339621. 0.1783 83.44 0.6140 0.7601 0.0237 0.0192 1.916 17.248 6.544 1428.456 1.949 29.107 2.078 0.58 340487. 0.1521 86.92 0.6396 0.7307 0.0187 0.0164 1.634 14.717 5.153 1218.841 1.663 22.920 1.918 0.58 341383. 0.1246 90.40 0.6652 0.6776 0.0137 0.0134 1.341 12.073 3.769 999.879 1.364 16.766 1.710 0.58 342307. 0.0950 93.87 0.6908 0.5799 0.0087 0.0104 1.036 9.332 2.401 772.880 1.054 10.679 1.409 0.58 343260. 0.0625 97.35 0.7164 0.3790 0.0038 0.0072 0.723 6.513 1.056 539.369 0.736 4.698 0.888 0.58 344241. 0.0261 100.83 0.7420 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 0.1103 0.0386 5.764 45.411 39.713 4298.142 5.131 176.645 4.191 0.65 374152. 0.7559 3.94 0.0254 0.0703 0.1087 0.0392 5.854 46.121 39.155 4365.314 5.211 174.161 4.068 0.65 374435. 0.7286 7.88 0.0507 0.1363 0.1070 0.0398 5.938 46.787 38.544 4428.324 5.286 171.445 3.948 0.65 374741. 0.7015 11.82 0.0761 0.1984 0.1052 0.0403 6.016 47.394 37.879 4485.814 5.355 168.485 3.830 0.65 375073. 0.6747 15.76 0.1015 0.2566 0.1031 0.0408 6.083 47.929 37.155 4536.439 5.415 165.266 3.715 0.65 375430. 0.6481 19.69 0.1268 0.3111 0.1010 0.0412 6.140 48.376 36.370 4578.771 5.466 161.776 3.603 0.65 375815. 0.6219 23.63 0.1522 0.3620 0.0986 0.0415 6.184 48.720 35.522 4611.345 5.504 158.000 3.494 0.65 376227. 0.5960 27.57 0.1775 0.4096 0.0961 0.0416 6.212 48.945 34.606 4632.651 5.530 153.928 3.388 0.65 376668. 0.5705 31.51 0.2029 0.4539 0.0933 0.0417 6.224 49.035 33.622 4641.173 5.540 149.548 3.286 0.65 377138. 0.5453 35.45 0.2283 0.4952 0.0904 0.0417 6.216 48.975 32.566 4635.410 5.533 144.854 3.187 0.65 377639. 0.5205 39.39 0.2536 0.5337 0.0873 0.0415 6.187 48.747 31.438 4613.873 5.507 139.836 3.091 0.65 378169. 0.4960 43.33 0.2790 0.5694 0.0839 0.0411 6.135 48.338 30.236 4575.124 5.461 134.489 2.998 0.65 378731. 0.4718 47.27 0.3044 0.6025 0.0804 0.0406 6.058 47.730 28.958 4517.656 5.393 128.807 2.907 0.65 379324. 0.4478 51.21 0.3297 0.6330 0.0766 0.0399 5.954 46.908 27.603 4439.798 5.300 122.777 2.820 0.65 379948. 0.4241 55.15 0.3551 0.6612 0.0727 0.0390 5.820 45.856 26.170 4340.207 5.181 116.403 2.735 0.65 380604. 0.4004 59.08 0.3804 0.6869 0.0685 0.0379 5.657 44.572 24.666 4218.680 5.036 109.713 2.652 0.66 381292. 0.3770 63.02 0.4058 0.7102 0.0641 0.0366 5.465 43.059 23.098 4075.508 4.865 102.741 2.571 0.66 382012. 0.3536 66.96 0.4312 0.7311 0.0596 0.0352 5.245 41.321 21.474 3911.042 4.668 95.519 2.490 0.66 382763. 0.3303 70.90 0.4565 0.7493 0.0550 0.0335 4.996 39.363 19.801 3725.644 4.447 88.075 2.411 0.66 383546. 0.3070 74.84 0.4819 0.7646 0.0502 0.0316 4.720 37.187 18.084 3519.693 4.201 80.438 2.330 0.66 384362. 0.2837 78.78 0.5073 0.7767 0.0453 0.0296 4.417 34.798 16.330 3293.606 3.931 72.635 2.249 0.66 385209. 0.2601 82.72 0.5326 0.7849 0.0404 0.0274 4.087 32.202 14.544 3047.900 3.638 64.693 2.164 0.66 386088. 0.2363 86.66 0.5580 0.7884 0.0354 0.0250 3.732 29.405 12.734 2783.197 3.322 56.641 2.075 0.66 386999. 0.2120 90.60 0.5834 0.7858 0.0303 0.0225 3.353 26.416 10.906 2500.284 2.984 48.509 1.978 0.66 387942. 0.1870 94.54 0.6087 0.7747 0.0252 0.0198 2.950 23.245 9.067 2200.144 2.626 40.331 1.869 0.66 388918. 0.1611 98.47 0.6341 0.7511 0.0201 0.0169 2.527 19.905 7.226 1884.022 2.249 32.143 1.740 0.66 389926. 0.1339 102.41 0.6594 0.7069 0.0150 0.0140 2.083 16.413 5.393 1553.460 1.854 23.986 1.574 0.66 390967. 0.1047 106.35 0.6848 0.6248 0.0099 0.0109 1.623 12.788 3.576 1210.364 1.445 15.905 1.340 0.67 392040. 0.0725 110.29 0.7102 0.4573 0.0050 0.0077 1.149 9.055 1.787 857.030 1.023 7.949 0.946 0.67 393144. 0.0362 114.23 0.7355 0.0141 0.0001 0.0044 0.663 5.225 0.031 494.500 0.590 0.137 0.028 0.67 394254. 0.0001 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 0.1121 0.0397 8.424 58.993 51.086 6281.637 6.665 227.231 3.689 0.73 420855. 0.7546 4.43 0.0253 0.0696 0.1105 0.0403 8.550 59.877 50.394 6375.701 6.765 224.151 3.585 0.73 421174. 0.7284 8.86 0.0507 0.1352 0.1089 0.0408 8.669 60.708 49.633 6464.211 6.859 220.768 3.483 0.73 421520. 0.7023 13.28 0.0760 0.1970 0.1070 0.0413 8.777 61.469 48.801 6545.223 6.945 217.066 3.382 0.73 421894. 0.6762 17.71 0.1014 0.2549 0.1051 0.0418 8.873 62.140 47.892 6616.753 7.021 213.025 3.283 0.73 422298. 0.6503 22.14 0.1267 0.3093 0.1029 0.0422 8.954 62.703 46.903 6676.700 7.084 208.626 3.186 0.73 422733. 0.6246 26.57 0.1521 0.3602 0.1005 0.0424 9.015 63.137 45.830 6722.838 7.133 203.852 3.092 0.73 423199. 0.5991 31.00 0.1774 0.4077 0.0980 0.0426 9.056 63.419 44.669 6752.866 7.165 198.688 3.000 0.73 423698. 0.5740 35.43 0.2028 0.4521 0.0952 0.0427 9.071 63.527 43.417 6764.433 7.177 193.119 2.911 0.73 424229. 0.5491 39.85 0.2281 0.4935 0.0923 0.0427 9.059 63.441 42.072 6755.209 7.167 187.134 2.825 0.73 424795. 0.5244 44.28 0.2534 0.5321 0.0891 0.0424 9.016 63.137 40.630 6722.889 7.133 180.724 2.741 0.73 425395. 0.5001 48.71 0.2788 0.5681 0.0857 0.0421 8.938 62.596 39.092 6665.252 7.072 173.880 2.660 0.73 426029. 0.4761 53.14 0.3041 0.6014 0.0822 0.0415 8.824 61.796 37.454 6580.128 6.982 166.594 2.582 0.74 426699. 0.4522 57.57 0.3295 0.6323 0.0783 0.0408 8.670 60.716 35.714 6465.113 6.860 158.854 2.506 0.74 427404. 0.4286 61.99 0.3548 0.6608 0.0743 0.0399 8.473 59.336 33.871 6318.145 6.704 150.658 2.432 0.74 428144. 0.4050 66.42 0.3802 0.6871 0.0700 0.0388 8.232 57.652 31.934 6138.820 6.513 142.042 2.359 0.74 428920. 0.3816 70.85 0.4055 0.7109 0.0656 0.0374 7.949 55.668 29.912 5927.577 6.289 133.050 2.289 0.74 429732. 0.3583 75.28 0.4309 0.7324 0.0610 0.0359 7.624 53.390 27.816 5684.975 6.032 123.725 2.219 0.74 430580. 0.3350 79.71 0.4562 0.7513 0.0563 0.0342 7.257 50.822 25.653 5411.563 5.742 114.104 2.150 0.74 431463. 0.3117 84.14 0.4816 0.7675 0.0514 0.0323 6.850 47.971 23.432 5107.934 5.420 104.225 2.081 0.74 432382. 0.2883 88.56 0.5069 0.7804 0.0464 0.0301 6.403 44.842 21.161 4774.770 5.066 94.122 2.010 0.74 433336. 0.2647 92.99 0.5322 0.7897 0.0413 0.0279 5.918 41.444 18.847 4412.930 4.682 83.832 1.937 0.74 434326. 0.2407 97.42 0.5576 0.7944 0.0362 0.0254 5.396 37.786 16.500 4023.514 4.269 73.391 1.860 0.74 435351. 0.2163 101.85 0.5829 0.7930 0.0310 0.0228 4.838 33.883 14.128 3607.915 3.828 62.839 1.776 0.74 436413. 0.1911 106.28 0.6083 0.7831 0.0258 0.0200 4.248 29.751 11.740 3167.933 3.361 52.220 1.681 0.75 437511. 0.1648 110.70 0.6336 0.7605 0.0205 0.0171 3.629 25.412 9.348 2705.841 2.871 41.580 1.567 0.75 438644. 0.1371 115.13 0.6590 0.7166 0.0153 0.0140 2.983 20.891 6.963 2224.510 2.360 30.972 1.420 0.75 439814. 0.1072 119.56 0.6843 0.6329 0.0101 0.0109 2.317 16.223 4.599 1727.474 1.833 20.455 1.207 0.75 441020. 0.0741 123.99 0.7097 0.4590 0.0050 0.0077 1.635 11.447 2.269 1218.922 1.293 10.094 0.844 0.75 442262. 0.0364 128.42 0.7350 -0.0080 0.0000 0.0044 0.939 6.578 -0.022 700.445 0.743 -0.097 -0.014 0.75 443503. 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 0.1142 0.0429 12.485 78.690 64.265 9309.988 8.890 285.853 3.131 0.81 467524. 0.7184 4.91 0.0253 0.0658 0.1127 0.0433 12.615 79.511 63.443 9407.115 8.983 282.194 3.059 0.81 467878. 0.6974 9.82 0.0506 0.1286 0.1111 0.0437 12.734 80.260 62.534 9495.655 9.068 278.150 2.987 0.81 468264. 0.6761 14.73 0.0759 0.1882 0.1093 0.0441 12.838 80.916 61.532 9573.298 9.142 273.696 2.915 0.81 468681. 0.6546 19.64 0.1012 0.2448 0.1074 0.0444 12.924 81.459 60.433 9637.579 9.203 268.805 2.844 0.81 469131. 0.6328 24.55 0.1264 0.2985 0.1052 0.0446 12.989 81.869 59.230 9686.118 9.250 263.453 2.774 0.81 469616. 0.6110 29.45 0.1517 0.3491 0.1029 0.0447 13.030 82.125 57.917 9716.411 9.278 257.616 2.704 0.81 470136. 0.5889 34.36 0.1770 0.3969 0.1004 0.0448 13.042 82.205 56.492 9725.770 9.287 251.274 2.635 0.81 470692. 0.5668 39.27 0.2023 0.4419 0.0976 0.0447 13.023 82.083 54.948 9711.384 9.274 244.408 2.566 0.81 471285. 0.5445 44.18 0.2276 0.4841 0.0947 0.0445 12.968 81.736 53.283 9670.366 9.235 237.002 2.499 0.82 471915. 0.5221 49.09 0.2529 0.5236 0.0915 0.0442 12.874 81.140 51.493 9599.777 9.167 229.042 2.433 0.82 472584. 0.4997 54.00 0.2782 0.5606 0.0881 0.0437 12.735 80.268 49.577 9496.688 9.069 220.519 2.368 0.82 473291. 0.4772 58.91 0.3035 0.5950 0.0845 0.0431 12.549 79.097 47.532 9358.063 8.936 211.423 2.304 0.82 474038. 0.4546 63.82 0.3287 0.6269 0.0806 0.0423 12.311 77.596 45.355 9180.466 8.767 201.739 2.241 0.82 474823. 0.4319 68.73 0.3540 0.6565 0.0765 0.0412 12.016 75.736 43.044 8960.495 8.557 191.461 2.179 0.82 475648. 0.4092 73.64 0.3793 0.6837 0.0722 0.0400 11.663 73.509 40.609 8696.936 8.305 180.630 2.118 0.82 476512. 0.3863 78.55 0.4046 0.7085 0.0676 0.0386 11.252 70.919 38.063 8390.521 8.012 169.303 2.058 0.82 477415. 0.3633 83.46 0.4299 0.7307 0.0629 0.0370 10.786 67.983 35.417 8043.164 7.681 157.534 1.997 0.82 478358. 0.3402 88.36 0.4552 0.7502 0.0581 0.0352 10.266 64.704 32.683 7655.251 7.310 145.373 1.936 0.82 479340. 0.3169 93.27 0.4805 0.7666 0.0531 0.0333 9.692 61.087 29.872 7227.320 6.902 132.869 1.875 0.82 480360. 0.2933 98.18 0.5058 0.7795 0.0480 0.0311 9.067 57.146 26.993 6760.992 6.456 120.065 1.811 0.82 481420. 0.2693 103.09 0.5311 0.7880 0.0427 0.0288 8.392 52.894 24.057 6258.011 5.976 107.007 1.744 0.82 482519. 0.2448 108.00 0.5563 0.7911 0.0374 0.0263 7.672 48.357 21.075 5721.259 5.463 93.741 1.671 0.83 483657. 0.2195 112.91 0.5816 0.7866 0.0321 0.0237 6.911 43.562 18.057 5153.896 4.922 80.318 1.589 0.83 484834. 0.1933 117.82 0.6069 0.7715 0.0267 0.0210 6.115 38.542 15.016 4559.920 4.354 66.789 1.494 0.83 486051. 0.1657 122.73 0.6322 0.7402 0.0213 0.0182 5.289 33.337 11.964 3944.134 3.766 53.215 1.376 0.83 487308. 0.1362 127.64 0.6575 0.6833 0.0158 0.0152 4.442 27.996 8.917 3312.249 3.163 39.663 1.221 0.83 488604. 0.1044 132.55 0.6828 0.5815 0.0105 0.0123 3.581 22.573 5.892 2670.683 2.550 26.209 1.001 0.83 489939. 0.0695 137.46 0.7081 0.3921 0.0052 0.0093 2.718 17.129 2.908 2026.612 1.935 12.933 0.651 0.83 491314. 0.0318 142.37 0.7334 -0.0061 -0.0001 0.0064 1.854 11.688 -0.030 1382.855 1.321 -0.132 -0.010 0.84 492696. 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 0.1160 0.0507 19.680 112.763 78.999 14675.319 12.740 351.386 2.442 0.89 514173. 0.6212 5.48 0.0257 0.0578 0.1146 0.0510 19.763 113.238 78.065 14737.095 12.794 347.232 2.403 0.89 514568. 0.6076 10.97 0.0514 0.1137 0.1131 0.0511 19.819 113.559 77.019 14778.965 12.830 342.582 2.364 0.89 514998. 0.5938 16.45 0.0771 0.1677 0.1114 0.0512 19.844 113.706 75.855 14798.028 12.846 337.401 2.325 0.89 515466. 0.5796 21.94 0.1027 0.2199 0.1095 0.0512 19.836 113.656 74.562 14791.557 12.841 331.650 2.286 0.89 515972. 0.5651 27.42 0.1284 0.2702 0.1074 0.0510 19.789 113.390 73.132 14756.944 12.811 325.293 2.248 0.90 516518. 0.5502 32.91 0.1541 0.3187 0.1051 0.0508 19.702 112.889 71.559 14691.690 12.754 318.296 2.209 0.90 517105. 0.5349 38.39 0.1798 0.3653 0.1025 0.0505 19.570 112.132 69.835 14593.223 12.669 310.627 2.171 0.90 517734. 0.5192 43.88 0.2055 0.4100 0.0998 0.0500 19.390 111.100 67.954 14458.935 12.552 302.260 2.132 0.90 518405. 0.5030 49.36 0.2312 0.4528 0.0968 0.0494 19.158 109.772 65.911 14286.116 12.402 293.171 2.093 0.90 519120. 0.4863 54.85 0.2568 0.4937 0.0935 0.0487 18.871 108.128 63.701 14072.074 12.216 283.340 2.053 0.90 519879. 0.4690 60.33 0.2825 0.5325 0.0900 0.0478 18.525 106.147 61.321 13814.278 11.992 272.754 2.013 0.90 520681. 0.4513 65.82 0.3082 0.5693 0.0863 0.0467 18.117 103.809 58.769 13510.054 11.728 261.403 1.973 0.90 521529. 0.4329 71.30 0.3339 0.6039 0.0823 0.0455 17.642 101.088 56.040 13155.904 11.421 249.267 1.932 0.90 522421. 0.4140 76.78 0.3596 0.6364 0.0780 0.0441 17.096 97.956 53.135 12748.350 11.067 236.342 1.890 0.90 523358. 0.3944 82.27 0.3853 0.6666 0.0735 0.0425 16.477 94.409 50.065 12286.725 10.666 222.688 1.848 0.90 524339. 0.3743 87.75 0.4109 0.6944 0.0688 0.0407 15.786 90.453 46.848 11771.865 10.219 208.380 1.805 0.90 525365. 0.3536 93.24 0.4366 0.7191 0.0639 0.0388 15.039 86.170 43.499 11214.437 9.735 193.485 1.759 0.90 526435. 0.3321 98.72 0.4623 0.7395 0.0588 0.0368 14.252 81.659 40.032 10627.409 9.226 178.064 1.709 0.90 527549. 0.3094 104.21 0.4880 0.7541 0.0535 0.0346 13.436 76.985 36.461 10019.093 8.698 162.177 1.651 0.91 528707. 0.2853 109.69 0.5137 0.7610 0.0482 0.0325 12.606 72.229 32.797 9400.162 8.160 145.879 1.582 0.91 529909. 0.2594 115.18 0.5394 0.7605 0.0427 0.0303 11.735 67.241 29.059 8750.989 7.597 129.253 1.506 0.91 531155. 0.2324 120.66 0.5651 0.7508 0.0371 0.0279 10.826 62.029 25.262 8072.689 7.008 112.368 1.419 0.91 532445. 0.2042 126.15 0.5907 0.7286 0.0315 0.0255 9.891 56.672 21.424 7375.421 6.403 95.295 1.318 0.91 533779. 0.1746 131.63 0.6164 0.6896 0.0258 0.0231 8.939 51.217 17.562 6665.487 5.786 78.116 1.195 0.91 535157. 0.1433 137.12 0.6421 0.6273 0.0201 0.0206 7.983 45.739 13.696 5952.551 5.168 60.921 1.044 0.91 536580. 0.1105 142.60 0.6678 0.5325 0.0145 0.0181 7.035 40.307 9.851 5245.717 4.554 43.815 0.852 0.91 538047. 0.0765 148.09 0.6935 0.3913 0.0089 0.0157 6.108 34.995 6.052 4554.403 3.954 26.917 0.603 0.92 539558. 0.0424 153.57 0.7192 0.1831 0.0034 0.0134 5.212 29.865 2.330 3886.717 3.374 10.365 0.272 0.92 541113. 0.0119 159.05 0.7448