21x13.5EPN (21x135EPN.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 0.0955 0.0379 0.012 0.785 0.592 9.287 0.089 2.632 28.897 0.08 41273. 0.6211 0.54 0.0273 0.0670 0.0943 0.0385 0.013 0.798 0.584 9.440 0.090 2.600 28.083 0.08 41303. 0.5999 1.09 0.0547 0.1300 0.0930 0.0391 0.013 0.811 0.577 9.590 0.092 2.565 27.270 0.08 41336. 0.5786 1.63 0.0820 0.1893 0.0916 0.0397 0.013 0.823 0.568 9.733 0.093 2.526 26.461 0.08 41373. 0.5571 2.18 0.1094 0.2447 0.0901 0.0403 0.013 0.834 0.558 9.868 0.094 2.483 25.660 0.08 41413. 0.5357 2.72 0.1367 0.2964 0.0884 0.0408 0.013 0.844 0.548 9.990 0.095 2.436 24.869 0.08 41456. 0.5143 3.26 0.1641 0.3446 0.0865 0.0412 0.014 0.853 0.536 10.096 0.096 2.385 24.090 0.08 41503. 0.4929 3.81 0.1914 0.3893 0.0845 0.0416 0.014 0.861 0.524 10.183 0.097 2.329 23.326 0.08 41554. 0.4717 4.35 0.2188 0.4306 0.0823 0.0418 0.014 0.866 0.510 10.247 0.098 2.269 22.577 0.08 41609. 0.4505 4.89 0.2461 0.4687 0.0799 0.0420 0.014 0.869 0.495 10.283 0.098 2.203 21.845 0.08 41668. 0.4295 5.44 0.2735 0.5037 0.0773 0.0420 0.014 0.870 0.479 10.289 0.098 2.132 21.128 0.08 41731. 0.4087 5.98 0.3008 0.5357 0.0746 0.0419 0.014 0.867 0.462 10.260 0.098 2.055 20.427 0.08 41798. 0.3880 6.53 0.3282 0.5648 0.0716 0.0416 0.014 0.862 0.444 10.193 0.097 1.973 19.740 0.08 41870. 0.3674 7.07 0.3555 0.5909 0.0684 0.0412 0.014 0.852 0.424 10.085 0.096 1.886 19.066 0.08 41946. 0.3469 7.61 0.3829 0.6142 0.0650 0.0405 0.013 0.839 0.403 9.932 0.095 1.792 18.401 0.08 42026. 0.3264 8.16 0.4102 0.6345 0.0614 0.0397 0.013 0.822 0.381 9.730 0.093 1.693 17.742 0.08 42110. 0.3058 8.70 0.4375 0.6517 0.0576 0.0387 0.013 0.801 0.357 9.478 0.091 1.588 17.084 0.08 42199. 0.2852 9.24 0.4649 0.6656 0.0536 0.0374 0.012 0.776 0.332 9.177 0.088 1.478 16.422 0.08 42293. 0.2645 9.79 0.4922 0.6758 0.0495 0.0360 0.012 0.746 0.307 8.829 0.084 1.363 15.748 0.08 42391. 0.2436 10.33 0.5196 0.6820 0.0452 0.0344 0.011 0.713 0.280 8.436 0.081 1.245 15.055 0.08 42493. 0.2226 10.88 0.5469 0.6833 0.0408 0.0326 0.011 0.676 0.253 8.000 0.076 1.124 14.331 0.08 42599. 0.2013 11.42 0.5743 0.6790 0.0363 0.0307 0.010 0.636 0.225 7.524 0.072 1.001 13.562 0.08 42710. 0.1797 11.96 0.6016 0.6678 0.0317 0.0286 0.009 0.592 0.197 7.009 0.067 0.875 12.732 0.08 42825. 0.1578 12.51 0.6290 0.6478 0.0271 0.0264 0.009 0.546 0.168 6.459 0.062 0.748 11.814 0.08 42945. 0.1354 13.05 0.6563 0.6165 0.0225 0.0240 0.008 0.497 0.140 5.875 0.056 0.621 10.774 0.09 43069. 0.1125 13.60 0.6837 0.5697 0.0179 0.0215 0.007 0.445 0.111 5.260 0.050 0.493 9.558 0.09 43197. 0.0889 14.14 0.7110 0.5009 0.0133 0.0189 0.006 0.390 0.082 4.620 0.044 0.366 8.082 0.09 43329. 0.0648 14.68 0.7384 0.3992 0.0087 0.0161 0.005 0.334 0.054 3.957 0.038 0.241 6.202 0.09 43466. 0.0403 15.23 0.7657 0.2441 0.0043 0.0134 0.004 0.277 0.026 3.277 0.031 0.118 3.657 0.09 43607. 0.0166 15.77 0.7930 -0.0068 -0.0001 0.0105 0.003 0.218 -0.001 2.585 0.025 -0.002 -0.098 0.09 43752. 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 0.0958 0.0354 0.093 2.935 2.376 69.459 0.332 10.567 15.513 0.17 82545. 0.6681 1.09 0.0274 0.0720 0.0947 0.0361 0.095 2.990 2.347 70.757 0.338 10.440 15.046 0.17 82605. 0.6441 2.18 0.0549 0.1395 0.0934 0.0367 0.097 3.044 2.316 72.033 0.344 10.300 14.581 0.17 82672. 0.6200 3.27 0.0823 0.2026 0.0920 0.0374 0.098 3.096 2.281 73.263 0.350 10.145 14.121 0.17 82745. 0.5959 4.36 0.1097 0.2615 0.0905 0.0380 0.100 3.145 2.243 74.423 0.355 9.975 13.667 0.17 82825. 0.5719 5.46 0.1372 0.3162 0.0888 0.0385 0.101 3.190 2.201 75.486 0.360 9.788 13.222 0.17 82912. 0.5480 6.55 0.1646 0.3670 0.0869 0.0390 0.102 3.230 2.155 76.423 0.365 9.583 12.787 0.17 83007. 0.5244 7.64 0.1920 0.4139 0.0849 0.0394 0.104 3.263 2.104 77.204 0.369 9.360 12.362 0.17 83109. 0.5011 8.73 0.2195 0.4573 0.0827 0.0397 0.104 3.288 2.050 77.798 0.371 9.116 11.949 0.17 83219. 0.4780 9.82 0.2469 0.4971 0.0803 0.0399 0.105 3.304 1.990 78.172 0.373 8.852 11.547 0.17 83338. 0.4552 10.91 0.2743 0.5337 0.0777 0.0399 0.105 3.309 1.926 78.294 0.374 8.567 11.157 0.17 83465. 0.4326 12.00 0.3018 0.5672 0.0749 0.0399 0.105 3.302 1.857 78.132 0.373 8.259 10.779 0.17 83600. 0.4104 13.09 0.3292 0.5976 0.0719 0.0396 0.104 3.282 1.783 77.656 0.371 7.929 10.411 0.17 83744. 0.3884 14.18 0.3566 0.6252 0.0687 0.0392 0.103 3.247 1.703 76.837 0.367 7.576 10.054 0.17 83897. 0.3666 15.28 0.3841 0.6499 0.0653 0.0386 0.101 3.197 1.619 75.646 0.361 7.199 9.705 0.17 84058. 0.3450 16.37 0.4115 0.6718 0.0617 0.0378 0.099 3.130 1.529 74.053 0.354 6.799 9.362 0.17 84229. 0.3234 17.46 0.4389 0.6907 0.0578 0.0367 0.097 3.045 1.433 72.042 0.344 6.376 9.025 0.17 84408. 0.3019 18.55 0.4664 0.7067 0.0538 0.0355 0.093 2.942 1.334 69.618 0.332 5.933 8.690 0.17 84596. 0.2804 19.64 0.4938 0.7193 0.0496 0.0341 0.090 2.823 1.230 66.797 0.319 5.472 8.354 0.17 84792. 0.2589 20.73 0.5212 0.7282 0.0453 0.0324 0.085 2.688 1.123 63.595 0.304 4.997 8.013 0.17 84998. 0.2373 21.82 0.5487 0.7329 0.0409 0.0306 0.081 2.537 1.014 60.029 0.287 4.510 7.661 0.17 85212. 0.2155 22.91 0.5761 0.7325 0.0364 0.0286 0.075 2.372 0.902 56.115 0.268 4.013 7.292 0.17 85435. 0.1935 24.00 0.6035 0.7259 0.0318 0.0265 0.070 2.192 0.789 51.871 0.248 3.509 6.898 0.17 85667. 0.1712 25.10 0.6310 0.7113 0.0272 0.0241 0.063 2.000 0.674 47.315 0.226 3.000 6.465 0.17 85907. 0.1484 26.19 0.6584 0.6859 0.0226 0.0217 0.057 1.795 0.559 42.471 0.203 2.489 5.975 0.17 86157. 0.1249 27.28 0.6858 0.6454 0.0179 0.0191 0.050 1.579 0.445 37.364 0.178 1.978 5.397 0.17 86415. 0.1005 28.37 0.7133 0.5820 0.0133 0.0163 0.043 1.354 0.330 32.028 0.153 1.470 4.680 0.17 86681. 0.0752 29.46 0.7407 0.4815 0.0088 0.0135 0.036 1.120 0.218 26.500 0.127 0.969 3.728 0.17 86957. 0.0486 30.55 0.7681 0.3134 0.0043 0.0106 0.028 0.880 0.107 20.823 0.099 0.478 2.340 0.17 87241. 0.0214 31.64 0.7956 0.0000 0.0000 0.0077 0.020 0.636 0.000 15.042 0.072 0.000 0.000 0.17 87531. 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 0.0962 0.0345 0.306 6.427 5.368 228.107 0.726 23.879 10.675 0.25 123814. 0.6911 1.64 0.0275 0.0743 0.0951 0.0352 0.312 6.554 5.305 232.626 0.740 23.595 10.343 0.25 123905. 0.6656 3.28 0.0550 0.1440 0.0938 0.0358 0.318 6.679 5.234 237.075 0.755 23.282 10.014 0.25 124005. 0.6401 4.92 0.0825 0.2089 0.0924 0.0365 0.324 6.801 5.156 241.374 0.768 22.935 9.689 0.25 124115. 0.6147 6.56 0.1099 0.2694 0.0909 0.0371 0.329 6.915 5.070 245.439 0.781 22.553 9.370 0.25 124235. 0.5895 8.20 0.1374 0.3255 0.0892 0.0377 0.334 7.020 4.976 249.177 0.793 22.133 9.058 0.25 124366. 0.5645 9.84 0.1649 0.3775 0.0874 0.0382 0.339 7.114 4.872 252.489 0.804 21.673 8.753 0.25 124509. 0.5398 11.48 0.1924 0.4255 0.0853 0.0386 0.342 7.192 4.759 255.269 0.813 21.169 8.456 0.25 124663. 0.5155 13.12 0.2199 0.4697 0.0831 0.0389 0.345 7.252 4.636 257.408 0.819 20.620 8.169 0.25 124829. 0.4914 14.76 0.2474 0.5104 0.0807 0.0391 0.347 7.291 4.502 258.796 0.824 20.024 7.890 0.25 125008. 0.4678 16.40 0.2748 0.5478 0.0781 0.0392 0.348 7.306 4.357 259.320 0.825 19.379 7.620 0.25 125199. 0.4444 18.04 0.3023 0.5819 0.0753 0.0391 0.347 7.293 4.201 258.869 0.824 18.684 7.360 0.25 125402. 0.4215 19.68 0.3298 0.6131 0.0723 0.0389 0.345 7.250 4.033 257.335 0.819 17.937 7.108 0.25 125619. 0.3988 21.32 0.3573 0.6414 0.0691 0.0385 0.341 7.174 3.853 254.617 0.810 17.137 6.863 0.25 125849. 0.3764 22.96 0.3848 0.6668 0.0656 0.0379 0.336 7.061 3.661 250.617 0.798 16.285 6.626 0.25 126092. 0.3543 24.59 0.4123 0.6895 0.0620 0.0371 0.329 6.909 3.457 245.231 0.781 15.379 6.395 0.25 126349. 0.3322 26.23 0.4397 0.7094 0.0581 0.0360 0.320 6.717 3.242 238.394 0.759 14.420 6.168 0.25 126618. 0.3103 27.87 0.4672 0.7264 0.0541 0.0348 0.309 6.484 3.016 230.126 0.733 13.415 5.945 0.25 126901. 0.2885 29.51 0.4947 0.7403 0.0499 0.0333 0.296 6.212 2.781 220.477 0.702 12.371 5.722 0.25 127198. 0.2666 31.15 0.5222 0.7508 0.0455 0.0317 0.281 5.903 2.539 209.502 0.667 11.295 5.497 0.25 127507. 0.2448 32.79 0.5497 0.7574 0.0411 0.0298 0.265 5.557 2.291 197.253 0.628 10.190 5.268 0.25 127829. 0.2228 34.43 0.5772 0.7592 0.0365 0.0278 0.246 5.178 2.038 183.786 0.585 9.065 5.029 0.25 128165. 0.2006 36.07 0.6046 0.7553 0.0319 0.0256 0.227 4.766 1.781 169.159 0.538 7.923 4.776 0.25 128514. 0.1781 37.71 0.6321 0.7438 0.0273 0.0232 0.206 4.323 1.522 153.441 0.488 6.770 4.499 0.25 128876. 0.1551 39.35 0.6596 0.7222 0.0226 0.0207 0.183 3.852 1.262 136.710 0.435 5.613 4.186 0.26 129251. 0.1314 40.99 0.6871 0.6859 0.0180 0.0180 0.160 3.354 1.002 119.060 0.379 4.457 3.817 0.26 129640. 0.1067 42.63 0.7146 0.6268 0.0133 0.0152 0.135 2.834 0.744 100.605 0.320 3.309 3.354 0.26 130041. 0.0808 44.27 0.7421 0.5286 0.0088 0.0123 0.109 2.296 0.489 81.477 0.259 2.176 2.724 0.26 130456. 0.0532 45.91 0.7695 0.3544 0.0043 0.0093 0.083 1.742 0.240 61.835 0.197 1.068 1.761 0.26 130883. 0.0241 47.55 0.7970 -0.0055 0.0000 0.0063 0.056 1.178 -0.002 41.821 0.133 -0.011 -0.026 0.26 131319. 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 0.0968 0.0341 0.716 11.289 9.597 534.240 1.275 42.686 8.147 0.33 165079. 0.7052 2.19 0.0275 0.0757 0.0956 0.0348 0.731 11.520 9.484 545.204 1.302 42.187 7.890 0.33 165200. 0.6790 4.37 0.0550 0.1464 0.0944 0.0354 0.746 11.749 9.360 556.016 1.327 41.634 7.636 0.33 165334. 0.6527 6.56 0.0825 0.2124 0.0930 0.0361 0.760 11.970 9.223 566.479 1.352 41.023 7.384 0.33 165480. 0.6266 8.75 0.1100 0.2738 0.0915 0.0367 0.773 12.179 9.071 576.388 1.376 40.348 7.138 0.33 165641. 0.6007 10.94 0.1375 0.3307 0.0898 0.0373 0.785 12.372 8.904 585.521 1.398 39.604 6.897 0.33 165816. 0.5751 13.12 0.1650 0.3833 0.0879 0.0378 0.796 12.544 8.720 593.635 1.417 38.788 6.663 0.33 166007. 0.5497 15.31 0.1925 0.4319 0.0859 0.0383 0.805 12.688 8.519 600.477 1.434 37.894 6.435 0.33 166213. 0.5248 17.50 0.2200 0.4767 0.0837 0.0386 0.812 12.801 8.300 605.783 1.446 36.918 6.214 0.33 166435. 0.5002 19.69 0.2475 0.5179 0.0813 0.0388 0.817 12.874 8.061 609.282 1.455 35.857 6.001 0.33 166673. 0.4761 21.87 0.2750 0.5557 0.0787 0.0389 0.819 12.904 7.803 610.702 1.458 34.708 5.795 0.33 166928. 0.4523 24.06 0.3025 0.5903 0.0759 0.0389 0.818 12.885 7.524 609.774 1.456 33.467 5.597 0.33 167201. 0.4290 26.25 0.3300 0.6219 0.0729 0.0387 0.813 12.810 7.224 606.236 1.447 32.134 5.405 0.34 167491. 0.4059 28.43 0.3575 0.6507 0.0696 0.0382 0.804 12.675 6.903 599.843 1.432 30.705 5.220 0.34 167798. 0.3832 30.62 0.3850 0.6767 0.0662 0.0376 0.792 12.475 6.561 590.355 1.409 29.182 5.041 0.34 168123. 0.3607 32.81 0.4124 0.6999 0.0625 0.0368 0.774 12.203 6.196 577.521 1.379 27.560 4.866 0.34 168465. 0.3385 35.00 0.4399 0.7205 0.0586 0.0358 0.753 11.858 5.810 561.180 1.340 25.844 4.696 0.34 168825. 0.3163 37.18 0.4674 0.7383 0.0545 0.0345 0.726 11.439 5.406 541.369 1.292 24.045 4.529 0.34 169203. 0.2942 39.37 0.4949 0.7531 0.0503 0.0330 0.695 10.950 4.985 518.205 1.237 22.175 4.364 0.34 169599. 0.2722 41.56 0.5224 0.7648 0.0459 0.0314 0.660 10.392 4.552 491.816 1.174 20.246 4.198 0.34 170012. 0.2502 43.74 0.5499 0.7727 0.0414 0.0295 0.620 9.769 4.107 462.327 1.104 18.267 4.029 0.34 170442. 0.2281 45.93 0.5774 0.7762 0.0368 0.0274 0.576 9.083 3.653 429.869 1.026 16.249 3.855 0.34 170891. 0.2058 48.12 0.6049 0.7742 0.0322 0.0252 0.529 8.338 3.193 394.586 0.942 14.202 3.670 0.34 171356. 0.1832 50.31 0.6324 0.7653 0.0275 0.0227 0.478 7.536 2.728 356.640 0.851 12.136 3.470 0.34 171840. 0.1601 52.49 0.6599 0.7466 0.0228 0.0202 0.424 6.682 2.262 316.222 0.755 10.061 3.244 0.34 172341. 0.1363 54.68 0.6874 0.7138 0.0181 0.0174 0.367 5.781 1.796 273.562 0.653 7.989 2.978 0.34 172859. 0.1115 56.87 0.7149 0.6587 0.0134 0.0146 0.307 4.838 1.333 228.936 0.547 5.931 2.642 0.34 173395. 0.0852 59.06 0.7424 0.5640 0.0088 0.0116 0.245 3.860 0.877 182.673 0.436 3.903 2.179 0.34 173948. 0.0570 61.24 0.7699 0.3883 0.0043 0.0086 0.181 2.856 0.431 135.161 0.323 1.917 1.446 0.34 174518. 0.0265 63.43 0.7974 -0.0049 0.0000 0.0055 0.116 1.833 -0.003 86.734 0.207 -0.015 -0.018 0.34 175099. 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 0.0974 0.0340 1.395 17.583 15.099 1040.154 1.987 67.159 6.584 0.42 206337. 0.7148 2.75 0.0277 0.0770 0.0963 0.0347 1.424 17.956 14.925 1062.222 2.029 66.386 6.373 0.42 206490. 0.6879 5.51 0.0554 0.1489 0.0951 0.0354 1.454 18.324 14.732 1084.002 2.070 65.526 6.164 0.42 206659. 0.6610 8.26 0.0831 0.2159 0.0937 0.0361 1.482 18.681 14.517 1105.095 2.111 64.572 5.958 0.42 206845. 0.6343 11.02 0.1108 0.2781 0.0922 0.0367 1.509 19.019 14.280 1125.080 2.149 63.516 5.757 0.42 207048. 0.6078 13.77 0.1385 0.3357 0.0905 0.0373 1.533 19.330 14.017 1143.501 2.184 62.350 5.560 0.42 207269. 0.5816 16.53 0.1662 0.3890 0.0886 0.0379 1.555 19.607 13.729 1159.864 2.215 61.065 5.369 0.42 207510. 0.5558 19.28 0.1939 0.4381 0.0866 0.0383 1.574 19.840 13.412 1173.645 2.241 59.655 5.183 0.42 207771. 0.5304 22.04 0.2216 0.4834 0.0843 0.0387 1.588 20.020 13.065 1184.305 2.262 58.113 5.004 0.42 208052. 0.5054 24.79 0.2493 0.5250 0.0819 0.0389 1.598 20.138 12.687 1191.292 2.275 56.433 4.831 0.42 208355. 0.4808 27.55 0.2770 0.5632 0.0792 0.0390 1.601 20.185 12.277 1194.048 2.280 54.610 4.664 0.42 208678. 0.4566 30.30 0.3047 0.5982 0.0764 0.0389 1.599 20.151 11.834 1192.027 2.277 52.639 4.503 0.42 209024. 0.4328 33.05 0.3324 0.6301 0.0733 0.0387 1.589 20.027 11.357 1184.696 2.263 50.517 4.348 0.42 209391. 0.4094 35.81 0.3601 0.6592 0.0700 0.0382 1.571 19.805 10.846 1171.554 2.238 48.242 4.199 0.42 209781. 0.3864 38.56 0.3878 0.6855 0.0665 0.0376 1.545 19.476 10.299 1152.115 2.200 45.811 4.055 0.42 210192. 0.3636 41.32 0.4155 0.7091 0.0627 0.0368 1.510 19.032 9.718 1125.868 2.150 43.224 3.915 0.42 210627. 0.3410 44.07 0.4432 0.7301 0.0587 0.0357 1.465 18.468 9.102 1092.512 2.087 40.484 3.779 0.42 211083. 0.3185 46.83 0.4710 0.7483 0.0546 0.0343 1.411 17.786 8.456 1052.145 2.009 37.612 3.645 0.42 211563. 0.2962 49.58 0.4987 0.7637 0.0502 0.0328 1.348 16.989 7.785 1005.003 1.919 34.627 3.513 0.42 212064. 0.2739 52.34 0.5264 0.7758 0.0458 0.0311 1.276 16.082 7.092 951.342 1.817 31.547 3.381 0.42 212588. 0.2516 55.09 0.5541 0.7843 0.0412 0.0291 1.195 15.069 6.383 891.417 1.702 28.390 3.248 0.42 213134. 0.2292 57.85 0.5818 0.7885 0.0365 0.0269 1.107 13.955 5.659 825.496 1.577 25.171 3.109 0.42 213702. 0.2067 60.60 0.6095 0.7872 0.0318 0.0246 1.011 12.744 4.925 753.876 1.440 21.907 2.963 0.42 214293. 0.1837 63.35 0.6372 0.7788 0.0270 0.0221 0.908 11.443 4.185 676.894 1.293 18.614 2.804 0.42 214906. 0.1603 66.11 0.6649 0.7605 0.0222 0.0194 0.798 10.057 3.442 594.957 1.136 15.310 2.624 0.43 215540. 0.1360 68.86 0.6926 0.7272 0.0174 0.0166 0.682 8.597 2.701 508.548 0.971 12.014 2.409 0.43 216197. 0.1106 71.62 0.7203 0.6694 0.0127 0.0137 0.561 7.070 1.966 418.257 0.799 8.745 2.132 0.43 216877. 0.0835 74.37 0.7480 0.5657 0.0080 0.0106 0.436 5.490 1.242 324.785 0.620 5.526 1.735 0.43 217578. 0.0540 77.13 0.7757 0.3586 0.0035 0.0075 0.307 3.870 0.535 228.950 0.437 2.381 1.061 0.43 218300. 0.0217 79.88 0.8034 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 0.0983 0.0341 2.418 25.404 21.927 1803.365 2.870 97.533 5.515 0.50 247588. 0.7216 3.28 0.0275 0.0767 0.0972 0.0348 2.470 25.950 21.685 1842.141 2.932 96.453 5.339 0.50 247770. 0.6947 6.56 0.0550 0.1485 0.0960 0.0355 2.522 26.490 21.414 1880.462 2.993 95.249 5.165 0.50 247971. 0.6678 9.84 0.0824 0.2153 0.0946 0.0362 2.572 27.014 21.113 1917.642 3.052 93.910 4.994 0.50 248192. 0.6411 13.11 0.1099 0.2775 0.0931 0.0369 2.619 27.511 20.779 1952.953 3.108 92.424 4.826 0.50 248434. 0.6146 16.39 0.1374 0.3350 0.0915 0.0375 2.663 27.971 20.409 1985.601 3.160 90.779 4.662 0.50 248697. 0.5885 19.67 0.1649 0.3883 0.0896 0.0381 2.702 28.382 20.001 2014.730 3.207 88.964 4.503 0.50 248983. 0.5627 22.95 0.1923 0.4375 0.0876 0.0385 2.735 28.730 19.552 2039.435 3.246 86.968 4.348 0.50 249293. 0.5372 26.23 0.2198 0.4829 0.0854 0.0389 2.761 29.002 19.061 2058.782 3.277 84.782 4.199 0.50 249627. 0.5123 29.51 0.2473 0.5246 0.0830 0.0391 2.778 29.186 18.524 2071.814 3.297 82.395 4.055 0.50 249986. 0.4877 32.79 0.2748 0.5630 0.0804 0.0392 2.786 29.267 17.941 2077.570 3.307 79.801 3.917 0.50 250370. 0.4635 36.07 0.3023 0.5982 0.0776 0.0392 2.783 29.232 17.309 2075.097 3.303 76.992 3.783 0.50 250780. 0.4398 39.34 0.3297 0.6304 0.0745 0.0390 2.767 29.068 16.629 2063.478 3.284 73.965 3.655 0.50 251216. 0.4165 42.62 0.3572 0.6599 0.0713 0.0386 2.738 28.764 15.898 2041.839 3.250 70.714 3.532 0.50 251678. 0.3934 45.90 0.3847 0.6867 0.0678 0.0380 2.695 28.306 15.117 2009.349 3.198 67.240 3.412 0.50 252166. 0.3707 49.18 0.4122 0.7108 0.0640 0.0371 2.635 27.683 14.284 1965.134 3.128 63.536 3.297 0.50 252681. 0.3482 52.46 0.4397 0.7324 0.0601 0.0361 2.559 26.886 13.402 1908.568 3.038 59.610 3.185 0.50 253222. 0.3258 55.74 0.4671 0.7515 0.0559 0.0348 2.467 25.916 12.474 1839.728 2.928 55.485 3.075 0.51 253789. 0.3035 59.02 0.4946 0.7678 0.0516 0.0332 2.359 24.779 11.509 1759.005 2.800 51.191 2.968 0.51 254383. 0.2813 62.29 0.5221 0.7811 0.0471 0.0315 2.235 23.481 10.512 1666.834 2.653 46.755 2.860 0.51 255004. 0.2591 65.57 0.5496 0.7911 0.0425 0.0295 2.097 22.027 9.488 1563.659 2.489 42.201 2.752 0.51 255650. 0.2369 68.85 0.5770 0.7972 0.0378 0.0274 1.944 20.425 8.443 1449.934 2.308 37.553 2.641 0.51 256323. 0.2144 72.13 0.6045 0.7984 0.0331 0.0251 1.778 18.682 7.382 1326.161 2.111 32.834 2.525 0.51 257022. 0.1917 75.41 0.6320 0.7932 0.0283 0.0225 1.600 16.805 6.310 1192.911 1.899 28.068 2.399 0.51 257746. 0.1684 78.69 0.6595 0.7792 0.0235 0.0199 1.409 14.804 5.234 1050.863 1.673 23.279 2.259 0.51 258497. 0.1444 81.97 0.6870 0.7522 0.0186 0.0170 1.208 12.690 4.158 900.830 1.434 18.493 2.093 0.51 259274. 0.1193 85.25 0.7144 0.7040 0.0138 0.0141 0.997 10.478 3.089 743.796 1.184 13.741 1.884 0.51 260078. 0.0925 88.52 0.7419 0.6167 0.0091 0.0110 0.779 8.184 2.035 580.945 0.925 9.054 1.589 0.51 260907. 0.0633 91.80 0.7694 0.4430 0.0045 0.0078 0.555 5.827 1.004 413.670 0.658 4.465 1.101 0.51 261761. 0.0308 95.08 0.7969 0.0003 0.0000 0.0046 0.326 3.425 0.000 243.131 0.387 0.001 0.001 0.52 262630. 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 0.0993 0.0344 3.874 34.885 30.152 2889.103 3.941 134.116 4.734 0.58 288828. 0.7263 3.82 0.0275 0.0768 0.0982 0.0351 3.959 35.650 29.831 2952.454 4.028 132.690 4.583 0.58 289040. 0.6994 7.65 0.0549 0.1486 0.0970 0.0359 4.043 36.407 29.473 3015.156 4.113 131.094 4.434 0.58 289275. 0.6725 11.47 0.0824 0.2156 0.0957 0.0366 4.125 37.142 29.072 3076.072 4.196 129.311 4.287 0.58 289533. 0.6458 15.29 0.1099 0.2778 0.0943 0.0373 4.203 37.842 28.625 3134.018 4.275 127.325 4.143 0.58 289816. 0.6193 19.12 0.1373 0.3354 0.0926 0.0379 4.275 38.490 28.129 3187.674 4.349 125.118 4.002 0.58 290124. 0.5931 22.94 0.1648 0.3888 0.0908 0.0385 4.339 39.069 27.579 3235.643 4.414 122.673 3.866 0.58 290459. 0.5673 26.76 0.1923 0.4381 0.0888 0.0390 4.394 39.562 26.973 3276.428 4.470 119.976 3.734 0.58 290821. 0.5419 30.59 0.2197 0.4836 0.0866 0.0394 4.437 39.949 26.307 3308.500 4.513 117.011 3.606 0.58 291211. 0.5168 34.41 0.2472 0.5255 0.0842 0.0396 4.466 40.212 25.577 3330.286 4.543 113.766 3.483 0.58 291631. 0.4922 38.24 0.2747 0.5641 0.0816 0.0397 4.479 40.332 24.782 3340.216 4.557 110.230 3.365 0.59 292080. 0.4681 42.06 0.3021 0.5995 0.0788 0.0397 4.475 40.290 23.919 3336.734 4.552 106.393 3.251 0.59 292559. 0.4443 45.88 0.3296 0.6320 0.0757 0.0395 4.450 40.068 22.987 3318.344 4.527 102.248 3.142 0.59 293068. 0.4209 49.71 0.3571 0.6618 0.0724 0.0391 4.403 39.649 21.985 3283.623 4.479 97.791 3.037 0.59 293608. 0.3979 53.53 0.3845 0.6889 0.0689 0.0384 4.333 39.016 20.912 3231.225 4.408 93.018 2.935 0.59 294179. 0.3751 57.35 0.4120 0.7134 0.0651 0.0376 4.237 38.153 19.767 3159.753 4.310 87.925 2.838 0.59 294780. 0.3525 61.18 0.4395 0.7355 0.0611 0.0365 4.114 37.047 18.552 3068.138 4.186 82.517 2.743 0.59 295412. 0.3301 65.00 0.4669 0.7551 0.0569 0.0352 3.965 35.698 17.273 2956.452 4.033 76.829 2.650 0.59 296075. 0.3077 68.82 0.4944 0.7721 0.0525 0.0336 3.789 34.115 15.940 2825.327 3.854 70.900 2.559 0.59 296769. 0.2855 72.65 0.5219 0.7862 0.0479 0.0318 3.588 32.305 14.561 2675.477 3.650 64.769 2.469 0.59 297493. 0.2632 76.47 0.5493 0.7971 0.0433 0.0298 3.363 30.279 13.145 2507.624 3.421 58.470 2.378 0.59 298248. 0.2409 80.29 0.5768 0.8042 0.0385 0.0276 3.115 28.044 11.699 2322.516 3.168 52.036 2.285 0.59 299033. 0.2183 84.12 0.6043 0.8067 0.0337 0.0252 2.844 25.610 10.229 2120.974 2.893 45.500 2.188 0.59 299848. 0.1955 87.94 0.6317 0.8031 0.0288 0.0226 2.553 22.989 8.744 1903.931 2.597 38.894 2.083 0.59 300694. 0.1721 91.76 0.6592 0.7911 0.0239 0.0199 2.243 20.195 7.251 1672.494 2.282 32.253 1.966 0.60 301570. 0.1480 95.59 0.6867 0.7665 0.0190 0.0170 1.915 17.243 5.759 1427.999 1.948 25.614 1.829 0.60 302477. 0.1226 99.41 0.7141 0.7211 0.0141 0.0139 1.572 14.152 4.276 1172.061 1.599 19.019 1.655 0.60 303413. 0.0956 103.23 0.7416 0.6369 0.0093 0.0108 1.216 10.947 2.813 906.626 1.237 12.512 1.407 0.60 304380. 0.0659 107.06 0.7691 0.4636 0.0045 0.0075 0.850 7.655 1.381 633.999 0.865 6.141 0.988 0.60 305376. 0.0324 110.88 0.7965 -0.0081 0.0000 0.0042 0.477 4.299 -0.013 356.007 0.486 -0.058 -0.017 0.60 306387. 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 0.1005 0.0349 5.868 46.233 39.861 4375.956 5.223 177.304 4.132 0.67 330054. 0.7289 4.37 0.0274 0.0766 0.0995 0.0356 5.999 47.262 39.461 4473.320 5.340 175.522 4.001 0.67 330297. 0.7023 8.73 0.0549 0.1482 0.0983 0.0364 6.128 48.283 39.010 4569.964 5.455 173.516 3.872 0.67 330566. 0.6757 13.10 0.0823 0.2150 0.0971 0.0372 6.255 49.278 38.503 4664.130 5.567 171.263 3.744 0.67 330861. 0.6492 17.46 0.1098 0.2771 0.0956 0.0379 6.375 50.227 37.936 4753.952 5.675 168.738 3.619 0.67 331184. 0.6229 21.83 0.1372 0.3347 0.0940 0.0386 6.487 51.108 37.302 4837.343 5.774 165.918 3.498 0.67 331536. 0.5969 26.19 0.1646 0.3880 0.0923 0.0391 6.587 51.898 36.596 4912.087 5.863 162.779 3.379 0.67 331919. 0.5712 30.56 0.1921 0.4373 0.0903 0.0397 6.673 52.571 35.814 4975.851 5.939 159.300 3.265 0.67 332334. 0.5459 34.92 0.2195 0.4828 0.0881 0.0401 6.740 53.104 34.950 5026.240 6.000 155.458 3.154 0.67 332781. 0.5210 39.29 0.2469 0.5248 0.0857 0.0403 6.787 53.469 34.001 5060.818 6.041 151.237 3.047 0.67 333261. 0.4965 43.65 0.2744 0.5635 0.0831 0.0405 6.809 53.642 32.963 5077.146 6.060 146.621 2.945 0.67 333775. 0.4724 48.02 0.3018 0.5992 0.0803 0.0404 6.803 53.596 31.834 5072.826 6.055 141.597 2.846 0.67 334324. 0.4487 52.38 0.3293 0.6319 0.0772 0.0402 6.766 53.308 30.610 5045.557 6.023 136.155 2.752 0.67 334907. 0.4254 56.75 0.3567 0.6619 0.0738 0.0398 6.696 52.754 29.292 4993.161 5.960 130.289 2.661 0.67 335525. 0.4024 61.11 0.3841 0.6894 0.0703 0.0392 6.589 51.914 27.876 4913.586 5.865 123.994 2.573 0.67 336178. 0.3796 65.48 0.4116 0.7144 0.0665 0.0383 6.443 50.763 26.364 4804.721 5.735 117.265 2.489 0.67 336866. 0.3570 69.84 0.4390 0.7370 0.0624 0.0372 6.256 49.286 24.754 4664.862 5.568 110.108 2.407 0.67 337589. 0.3346 74.21 0.4664 0.7571 0.0581 0.0358 6.027 47.481 23.059 4494.007 5.364 102.565 2.327 0.67 338347. 0.3123 78.57 0.4939 0.7747 0.0537 0.0342 5.757 45.358 21.288 4293.109 5.125 94.691 2.249 0.67 339140. 0.2900 82.94 0.5213 0.7896 0.0490 0.0324 5.449 42.930 19.455 4063.283 4.850 86.537 2.172 0.68 339968. 0.2677 87.30 0.5488 0.8014 0.0443 0.0303 5.103 40.208 17.570 3805.655 4.543 78.151 2.094 0.68 340830. 0.2453 91.67 0.5762 0.8097 0.0394 0.0281 4.722 37.204 15.642 3521.383 4.203 69.576 2.015 0.68 341727. 0.2226 96.03 0.6036 0.8134 0.0345 0.0256 4.307 33.933 13.682 3211.736 3.834 60.856 1.932 0.68 342658. 0.1997 100.40 0.6311 0.8114 0.0295 0.0229 3.860 30.409 11.699 2878.156 3.436 52.036 1.844 0.68 343624. 0.1762 104.76 0.6585 0.8014 0.0245 0.0201 3.383 26.649 9.704 2522.349 3.011 43.163 1.745 0.68 344624. 0.1519 109.13 0.6859 0.7793 0.0194 0.0171 2.878 22.677 7.708 2146.369 2.562 34.286 1.629 0.68 345658. 0.1264 113.49 0.7134 0.7370 0.0144 0.0140 2.350 18.518 5.724 1752.741 2.092 25.462 1.481 0.68 346727. 0.0990 117.86 0.7408 0.6564 0.0095 0.0107 1.803 14.206 3.766 1344.569 1.605 16.750 1.270 0.68 347830. 0.0689 122.22 0.7683 0.4852 0.0047 0.0074 1.241 9.779 1.848 925.601 1.105 8.219 0.905 0.69 348967. 0.0344 126.59 0.7957 -0.0099 0.0000 0.0040 0.669 5.271 -0.020 498.872 0.595 -0.087 -0.018 0.69 350119. 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 0.1019 0.0363 8.686 60.826 51.155 6476.792 6.872 227.538 3.582 0.75 371264. 0.7159 4.90 0.0274 0.0748 0.1010 0.0370 8.861 62.057 50.682 6607.886 7.011 225.433 3.479 0.75 371537. 0.6920 9.80 0.0548 0.1451 0.0999 0.0377 9.036 63.280 50.144 6738.130 7.149 223.043 3.375 0.75 371838. 0.6679 14.71 0.0822 0.2110 0.0987 0.0384 9.206 64.473 49.536 6865.156 7.284 220.336 3.273 0.75 372169. 0.6436 19.61 0.1096 0.2726 0.0973 0.0391 9.369 65.612 48.849 6986.434 7.413 217.279 3.171 0.75 372533. 0.6193 24.51 0.1369 0.3300 0.0958 0.0397 9.520 66.671 48.075 7099.161 7.532 213.838 3.072 0.75 372929. 0.5951 29.41 0.1643 0.3834 0.0940 0.0403 9.656 67.621 47.207 7200.298 7.640 209.978 2.974 0.75 373360. 0.5709 34.31 0.1917 0.4330 0.0921 0.0408 9.772 68.431 46.239 7286.612 7.731 205.670 2.878 0.75 373827. 0.5469 39.22 0.2191 0.4788 0.0900 0.0412 9.863 69.071 45.163 7354.676 7.804 200.884 2.785 0.75 374331. 0.5230 44.12 0.2465 0.5212 0.0876 0.0414 9.925 69.505 43.974 7400.926 7.853 195.595 2.695 0.75 374872. 0.4993 49.02 0.2739 0.5604 0.0850 0.0415 9.953 69.700 42.667 7421.735 7.875 189.782 2.608 0.75 375451. 0.4759 53.92 0.3013 0.5964 0.0821 0.0415 9.942 69.623 41.238 7413.450 7.866 183.425 2.523 0.75 376068. 0.4527 58.82 0.3287 0.6296 0.0790 0.0413 9.887 69.238 39.683 7372.504 7.822 176.512 2.441 0.75 376725. 0.4297 63.73 0.3561 0.6601 0.0757 0.0408 9.783 68.514 38.002 7295.446 7.741 169.034 2.363 0.75 377421. 0.4070 68.63 0.3834 0.6880 0.0721 0.0402 9.627 67.421 36.193 7178.997 7.617 160.988 2.287 0.76 378156. 0.3844 73.53 0.4108 0.7135 0.0682 0.0393 9.414 65.926 34.255 7019.849 7.448 152.365 2.213 0.76 378930. 0.3619 78.43 0.4382 0.7366 0.0641 0.0381 9.139 64.003 32.188 6815.119 7.231 143.170 2.142 0.76 379744. 0.3396 83.33 0.4656 0.7574 0.0598 0.0367 8.803 61.650 30.004 6564.501 6.965 133.456 2.073 0.76 380597. 0.3173 88.24 0.4930 0.7757 0.0552 0.0351 8.407 58.878 27.719 6269.365 6.652 123.294 2.005 0.76 381489. 0.2950 93.14 0.5204 0.7915 0.0505 0.0332 7.954 55.704 25.349 5931.403 6.293 112.751 1.938 0.76 382420. 0.2727 98.04 0.5478 0.8043 0.0456 0.0311 7.446 52.145 22.907 5552.413 5.891 101.890 1.871 0.76 383389. 0.2502 102.94 0.5752 0.8136 0.0406 0.0287 6.885 48.218 20.407 5134.328 5.448 90.769 1.803 0.76 384397. 0.2275 107.84 0.6026 0.8185 0.0356 0.0262 6.275 43.945 17.861 4679.305 4.965 79.445 1.731 0.76 385443. 0.2044 112.75 0.6300 0.8177 0.0304 0.0235 5.619 39.349 15.282 4189.900 4.446 67.975 1.654 0.76 386528. 0.1807 117.65 0.6573 0.8087 0.0253 0.0205 4.921 34.459 12.685 3669.233 3.893 56.422 1.568 0.77 387651. 0.1560 122.55 0.6847 0.7872 0.0201 0.0175 4.186 29.312 10.083 3121.171 3.312 44.849 1.465 0.77 388812. 0.1300 127.45 0.7121 0.7446 0.0149 0.0143 3.420 23.953 7.493 2550.491 2.706 33.329 1.333 0.77 390011. 0.1019 132.36 0.7395 0.6613 0.0098 0.0110 2.632 18.435 4.933 1963.002 2.083 21.941 1.140 0.77 391249. 0.0707 137.26 0.7669 0.4840 0.0048 0.0076 1.831 12.825 2.422 1365.564 1.449 10.772 0.804 0.77 392524. 0.0350 142.16 0.7943 -0.0095 -0.0001 0.0043 1.024 7.174 -0.026 763.892 0.811 -0.114 -0.015 0.77 393817. 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 0.1034 0.0409 13.432 84.658 64.086 10016.083 9.565 285.055 2.902 0.83 412451. 0.6491 5.48 0.0275 0.0681 0.1025 0.0415 13.631 85.912 63.556 10164.388 9.706 282.699 2.836 0.83 412755. 0.6318 10.96 0.0551 0.1330 0.1016 0.0421 13.823 87.126 62.948 10308.042 9.843 279.993 2.770 0.83 413091. 0.6140 16.43 0.0826 0.1948 0.1004 0.0426 14.005 88.272 62.251 10443.564 9.973 276.892 2.704 0.83 413462. 0.5960 21.91 0.1102 0.2534 0.0992 0.0431 14.171 89.318 61.453 10567.343 10.091 273.345 2.638 0.83 413869. 0.5778 27.39 0.1377 0.3089 0.0977 0.0436 14.316 90.232 60.545 10675.497 10.194 269.302 2.572 0.83 414314. 0.5593 32.87 0.1653 0.3613 0.0960 0.0439 14.435 90.982 59.514 10764.233 10.279 264.716 2.508 0.83 414798. 0.5405 38.34 0.1928 0.4108 0.0941 0.0442 14.523 91.534 58.350 10829.609 10.342 259.541 2.444 0.83 415323. 0.5216 43.82 0.2204 0.4574 0.0920 0.0443 14.574 91.856 57.045 10867.688 10.378 253.736 2.381 0.84 415890. 0.5024 49.30 0.2479 0.5011 0.0897 0.0444 14.583 91.914 55.590 10874.498 10.384 247.263 2.319 0.84 416499. 0.4830 54.78 0.2755 0.5421 0.0871 0.0443 14.545 91.673 53.977 10846.003 10.357 240.091 2.257 0.84 417152. 0.4634 60.26 0.3030 0.5803 0.0842 0.0440 14.454 91.099 52.202 10778.104 10.292 232.194 2.197 0.84 417848. 0.4435 65.73 0.3305 0.6159 0.0811 0.0435 14.304 90.157 50.259 10666.644 10.186 223.552 2.137 0.84 418589. 0.4233 71.21 0.3581 0.6488 0.0777 0.0429 14.091 88.812 48.145 10507.508 10.034 214.150 2.078 0.84 419373. 0.4029 76.69 0.3856 0.6792 0.0740 0.0420 13.808 87.031 45.860 10296.738 9.833 203.985 2.020 0.84 420202. 0.3822 82.17 0.4132 0.7070 0.0700 0.0409 13.451 84.777 43.401 10030.133 9.578 193.049 1.963 0.84 421076. 0.3613 87.64 0.4407 0.7322 0.0658 0.0396 13.013 82.018 40.771 9703.668 9.266 181.348 1.906 0.84 421993. 0.3400 93.12 0.4683 0.7549 0.0613 0.0380 12.494 78.745 37.984 9316.504 8.897 168.951 1.849 0.84 422954. 0.3184 98.60 0.4958 0.7747 0.0566 0.0362 11.899 74.997 35.061 8872.985 8.473 155.952 1.792 0.84 423959. 0.2965 104.08 0.5234 0.7911 0.0517 0.0342 11.234 70.806 32.023 8377.150 8.000 142.437 1.734 0.84 425007. 0.2741 109.56 0.5509 0.8036 0.0466 0.0320 10.501 66.186 28.887 7830.577 7.478 128.489 1.673 0.85 426099. 0.2513 115.03 0.5785 0.8113 0.0414 0.0295 9.705 61.172 25.671 7237.372 6.911 114.186 1.609 0.85 427233. 0.2278 120.51 0.6060 0.8132 0.0361 0.0269 8.849 55.773 22.394 6598.548 6.301 99.606 1.539 0.85 428410. 0.2035 125.99 0.6335 0.8069 0.0308 0.0242 7.940 50.043 19.070 5920.728 5.654 84.826 1.461 0.85 429630. 0.1783 131.47 0.6611 0.7887 0.0254 0.0213 6.987 44.041 15.720 5210.533 4.976 69.924 1.368 0.85 430892. 0.1516 136.94 0.6886 0.7520 0.0199 0.0183 6.003 37.838 12.363 4476.701 4.275 54.989 1.253 0.85 432197. 0.1231 142.42 0.7162 0.6850 0.0146 0.0152 5.001 31.518 9.020 3728.916 3.561 40.120 1.097 0.85 433544. 0.0921 147.90 0.7437 0.5645 0.0092 0.0122 3.994 25.171 5.716 2977.970 2.844 25.425 0.871 0.86 434934. 0.0582 153.38 0.7713 0.3380 0.0040 0.0091 2.998 18.896 2.478 2235.616 2.135 11.022 0.503 0.86 436366. 0.0221 158.86 0.7988 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 0.1036 0.0492 21.509 123.246 77.686 16039.554 13.924 345.547 2.197 0.92 453680. 0.5410 6.02 0.0275 0.0569 0.1029 0.0498 21.770 124.741 77.174 16234.130 14.093 343.272 2.156 0.92 454006. 0.5293 12.04 0.0550 0.1116 0.1021 0.0503 22.014 126.138 76.576 16416.021 14.251 340.610 2.116 0.92 454369. 0.5173 18.05 0.0825 0.1643 0.1012 0.0508 22.232 127.386 75.877 16578.422 14.392 337.499 2.076 0.92 454769. 0.5053 24.07 0.1100 0.2150 0.1001 0.0512 22.414 128.430 75.061 16714.260 14.510 333.870 2.037 0.92 455210. 0.4931 30.09 0.1376 0.2637 0.0988 0.0516 22.551 129.214 74.112 16816.312 14.599 329.648 1.999 0.92 455694. 0.4808 36.11 0.1651 0.3106 0.0974 0.0517 22.633 129.685 73.013 16877.537 14.652 324.762 1.962 0.92 456221. 0.4685 42.13 0.1926 0.3558 0.0957 0.0518 22.652 129.792 71.750 16891.451 14.664 319.142 1.927 0.92 456794. 0.4560 48.15 0.2201 0.3994 0.0938 0.0517 22.599 129.492 70.307 16852.426 14.630 312.723 1.892 0.92 457414. 0.4433 54.16 0.2476 0.4414 0.0916 0.0514 22.470 128.750 68.671 16755.904 14.546 305.448 1.859 0.92 458082. 0.4304 60.18 0.2751 0.4818 0.0891 0.0509 22.259 127.538 66.832 16598.199 14.409 297.267 1.826 0.92 458799. 0.4172 66.20 0.3026 0.5207 0.0864 0.0502 21.961 125.834 64.780 16376.427 14.217 288.140 1.794 0.92 459564. 0.4035 72.22 0.3301 0.5580 0.0834 0.0493 21.574 123.615 62.507 16087.601 13.966 278.033 1.762 0.92 460379. 0.3893 78.24 0.3577 0.5935 0.0800 0.0482 21.093 120.860 60.010 15729.145 13.655 266.923 1.730 0.92 461243. 0.3746 84.26 0.3852 0.6273 0.0764 0.0469 20.517 117.562 57.285 15299.864 13.282 254.804 1.698 0.92 462156. 0.3591 90.27 0.4127 0.6591 0.0724 0.0454 19.844 113.702 54.332 14797.471 12.846 241.670 1.665 0.92 463119. 0.3430 96.29 0.4402 0.6888 0.0682 0.0436 19.069 109.261 51.152 14219.514 12.344 227.523 1.632 0.93 464130. 0.3261 102.31 0.4677 0.7162 0.0637 0.0416 18.194 104.248 47.762 13567.111 11.778 212.446 1.597 0.93 465189. 0.3083 108.33 0.4952 0.7411 0.0589 0.0394 17.224 98.692 44.191 12844.030 11.150 196.560 1.561 0.93 466297. 0.2899 114.35 0.5227 0.7620 0.0540 0.0370 16.189 92.761 40.461 12072.214 10.480 179.969 1.520 0.93 467452. 0.2702 120.36 0.5502 0.7771 0.0488 0.0346 15.114 86.601 36.595 11270.565 9.784 162.773 1.473 0.93 468653. 0.2489 126.38 0.5778 0.7841 0.0435 0.0320 14.018 80.321 32.615 10453.182 9.075 145.072 1.415 0.93 469902. 0.2258 132.40 0.6053 0.7764 0.0381 0.0297 12.976 74.352 28.536 9676.411 8.400 126.927 1.338 0.93 471197. 0.1996 138.42 0.6328 0.7570 0.0325 0.0272 11.895 68.155 24.396 8869.838 7.700 108.513 1.248 0.93 472539. 0.1722 144.44 0.6603 0.7214 0.0270 0.0247 10.796 61.860 20.221 8050.677 6.989 89.941 1.139 0.94 473927. 0.1431 150.46 0.6878 0.6638 0.0214 0.0222 9.695 55.552 16.040 7229.722 6.276 71.348 1.006 0.94 475361. 0.1126 156.47 0.7153 0.5761 0.0159 0.0197 8.613 49.352 11.891 6422.783 5.576 52.893 0.840 0.94 476841. 0.0809 162.49 0.7428 0.4473 0.0104 0.0173 7.567 43.355 7.811 5642.389 4.898 34.741 0.628 0.94 478368. 0.0490 168.51 0.7703 0.2626 0.0051 0.0150 6.571 37.652 3.840 4900.095 4.254 17.081 0.355 0.94 479942. 0.0195 174.53 0.7978 0.0002 0.0000 0.0128 5.621 32.206 0.003 4191.363 3.639 0.013 0.000 0.95 481570. 0.0000