21x12WE (21x12WE.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 0.0957 0.0368 0.012 0.762 0.593 9.021 0.086 2.637 29.809 0.08 44141. 0.6413 0.49 0.0248 0.0627 0.0942 0.0373 0.012 0.772 0.584 9.131 0.087 2.597 29.004 0.08 44172. 0.6193 0.99 0.0496 0.1219 0.0926 0.0377 0.012 0.780 0.574 9.234 0.088 2.554 28.203 0.08 44205. 0.5971 1.48 0.0744 0.1777 0.0909 0.0381 0.013 0.788 0.564 9.327 0.089 2.507 27.410 0.08 44240. 0.5750 1.97 0.0992 0.2302 0.0891 0.0384 0.013 0.795 0.552 9.409 0.090 2.457 26.625 0.08 44279. 0.5529 2.47 0.1240 0.2794 0.0871 0.0387 0.013 0.801 0.540 9.477 0.090 2.402 25.850 0.08 44321. 0.5308 2.96 0.1488 0.3253 0.0850 0.0389 0.013 0.805 0.527 9.528 0.091 2.344 25.086 0.08 44365. 0.5088 3.45 0.1735 0.3682 0.0828 0.0390 0.013 0.808 0.513 9.560 0.091 2.282 24.335 0.08 44413. 0.4870 3.94 0.1983 0.4080 0.0803 0.0391 0.013 0.809 0.498 9.571 0.091 2.215 23.596 0.08 44465. 0.4652 4.44 0.2231 0.4448 0.0777 0.0390 0.013 0.808 0.482 9.557 0.091 2.143 22.868 0.08 44519. 0.4435 4.93 0.2479 0.4788 0.0750 0.0388 0.013 0.804 0.465 9.516 0.091 2.067 22.152 0.08 44577. 0.4220 5.42 0.2727 0.5099 0.0721 0.0385 0.013 0.798 0.447 9.446 0.090 1.987 21.446 0.08 44639. 0.4005 5.92 0.2975 0.5381 0.0690 0.0381 0.013 0.790 0.427 9.344 0.089 1.901 20.748 0.08 44704. 0.3790 6.41 0.3223 0.5635 0.0657 0.0376 0.012 0.778 0.407 9.207 0.088 1.811 20.055 0.08 44773. 0.3575 6.90 0.3471 0.5860 0.0622 0.0369 0.012 0.764 0.386 9.034 0.086 1.716 19.366 0.08 44845. 0.3361 7.40 0.3719 0.6054 0.0586 0.0360 0.012 0.746 0.363 8.824 0.084 1.616 18.675 0.08 44921. 0.3145 7.89 0.3967 0.6217 0.0549 0.0350 0.012 0.725 0.340 8.578 0.082 1.512 17.978 0.08 45001. 0.2929 8.38 0.4215 0.6345 0.0510 0.0339 0.011 0.701 0.316 8.298 0.079 1.405 17.269 0.08 45084. 0.2712 8.87 0.4463 0.6435 0.0470 0.0326 0.011 0.675 0.291 7.983 0.076 1.295 16.541 0.08 45172. 0.2494 9.37 0.4710 0.6483 0.0429 0.0312 0.010 0.645 0.266 7.634 0.073 1.182 15.785 0.08 45262. 0.2274 9.86 0.4958 0.6481 0.0387 0.0296 0.010 0.613 0.240 7.254 0.069 1.066 14.992 0.08 45357. 0.2051 10.35 0.5206 0.6421 0.0344 0.0279 0.009 0.578 0.213 6.841 0.065 0.949 14.146 0.08 45455. 0.1826 10.85 0.5454 0.6291 0.0301 0.0261 0.009 0.541 0.187 6.398 0.061 0.830 13.229 0.08 45557. 0.1597 11.34 0.5702 0.6073 0.0258 0.0242 0.008 0.501 0.160 5.927 0.057 0.710 12.217 0.08 45663. 0.1364 11.83 0.5950 0.5744 0.0214 0.0221 0.007 0.459 0.133 5.427 0.052 0.589 11.074 0.08 45773. 0.1126 12.33 0.6198 0.5267 0.0170 0.0200 0.007 0.414 0.105 4.903 0.047 0.469 9.747 0.08 45886. 0.0884 12.82 0.6446 0.4584 0.0126 0.0178 0.006 0.368 0.078 4.356 0.042 0.348 8.157 0.09 46004. 0.0638 13.31 0.6694 0.3601 0.0083 0.0155 0.005 0.320 0.052 3.788 0.036 0.229 6.171 0.09 46125. 0.0391 13.80 0.6942 0.2155 0.0041 0.0131 0.004 0.271 0.025 3.205 0.031 0.112 3.562 0.09 46250. 0.0158 14.30 0.7190 -0.0074 -0.0001 0.0106 0.003 0.220 -0.001 2.608 0.025 -0.003 -0.118 0.09 46377. 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 0.0960 0.0344 0.091 2.853 2.381 67.507 0.322 10.591 15.999 0.17 88281. 0.6898 1.00 0.0252 0.0683 0.0946 0.0349 0.092 2.894 2.345 68.471 0.327 10.430 15.533 0.17 88343. 0.6646 2.01 0.0504 0.1325 0.0930 0.0354 0.093 2.932 2.305 69.377 0.331 10.254 15.072 0.17 88410. 0.6394 3.01 0.0756 0.1928 0.0913 0.0358 0.094 2.967 2.263 70.205 0.335 10.064 14.617 0.17 88483. 0.6143 4.01 0.1009 0.2492 0.0894 0.0362 0.095 2.998 2.216 70.937 0.339 9.858 14.171 0.17 88562. 0.5895 5.01 0.1261 0.3019 0.0874 0.0365 0.096 3.024 2.166 71.552 0.342 9.636 13.733 0.17 88647. 0.5648 6.02 0.1513 0.3509 0.0852 0.0367 0.097 3.044 2.113 72.026 0.344 9.398 13.305 0.17 88739. 0.5404 7.02 0.1765 0.3965 0.0829 0.0369 0.097 3.057 2.055 72.339 0.345 9.141 12.886 0.17 88837. 0.5162 8.02 0.2017 0.4388 0.0804 0.0370 0.097 3.063 1.993 72.467 0.346 8.867 12.477 0.17 88942. 0.4922 9.03 0.2269 0.4779 0.0778 0.0369 0.097 3.059 1.928 72.388 0.346 8.574 12.078 0.17 89055. 0.4685 10.03 0.2521 0.5138 0.0749 0.0368 0.097 3.046 1.857 72.079 0.344 8.262 11.688 0.17 89174. 0.4451 11.03 0.2773 0.5468 0.0719 0.0365 0.096 3.022 1.783 71.518 0.341 7.930 11.306 0.17 89301. 0.4218 12.03 0.3026 0.5768 0.0687 0.0361 0.095 2.987 1.704 70.682 0.337 7.578 10.933 0.17 89435. 0.3987 13.04 0.3278 0.6038 0.0653 0.0355 0.093 2.939 1.620 69.544 0.332 7.206 10.566 0.17 89576. 0.3757 14.04 0.3530 0.6280 0.0618 0.0347 0.091 2.878 1.532 68.092 0.325 6.814 10.204 0.17 89725. 0.3529 15.04 0.3782 0.6492 0.0581 0.0338 0.089 2.803 1.440 66.326 0.317 6.403 9.845 0.17 89882. 0.3300 16.04 0.4034 0.6673 0.0542 0.0328 0.086 2.715 1.344 64.250 0.307 5.977 9.487 0.17 90046. 0.3073 17.05 0.4286 0.6820 0.0502 0.0316 0.083 2.615 1.245 61.871 0.295 5.537 9.126 0.17 90218. 0.2845 18.05 0.4538 0.6931 0.0461 0.0302 0.079 2.502 1.143 59.194 0.283 5.084 8.759 0.17 90398. 0.2616 19.05 0.4791 0.7000 0.0419 0.0287 0.075 2.376 1.039 56.224 0.268 4.621 8.380 0.17 90585. 0.2387 20.06 0.5043 0.7021 0.0376 0.0270 0.071 2.239 0.933 52.970 0.253 4.148 7.986 0.17 90780. 0.2155 21.06 0.5295 0.6985 0.0333 0.0252 0.066 2.089 0.825 49.438 0.236 3.668 7.566 0.17 90983. 0.1920 22.06 0.5547 0.6878 0.0289 0.0233 0.061 1.929 0.716 45.641 0.218 3.183 7.111 0.17 91193. 0.1681 23.06 0.5799 0.6679 0.0244 0.0212 0.056 1.758 0.606 41.589 0.199 2.694 6.605 0.17 91411. 0.1436 24.07 0.6051 0.6356 0.0200 0.0190 0.050 1.576 0.495 37.299 0.178 2.203 6.024 0.17 91638. 0.1185 25.07 0.6303 0.5857 0.0155 0.0167 0.044 1.386 0.385 32.792 0.157 1.714 5.329 0.17 91872. 0.0924 26.07 0.6555 0.5093 0.0111 0.0143 0.038 1.187 0.276 28.090 0.134 1.227 4.456 0.17 92114. 0.0654 27.08 0.6808 0.3896 0.0068 0.0118 0.031 0.981 0.168 23.223 0.111 0.747 3.282 0.17 92363. 0.0376 28.08 0.7060 0.1904 0.0025 0.0093 0.024 0.770 0.062 18.224 0.087 0.276 1.547 0.17 92620. 0.0108 29.08 0.7312 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 0.0965 0.0335 0.297 6.249 5.383 221.815 0.706 23.945 11.008 0.25 132417. 0.7136 1.49 0.0249 0.0696 0.0951 0.0340 0.302 6.343 5.303 225.144 0.717 23.587 10.683 0.25 132509. 0.6874 2.97 0.0498 0.1350 0.0935 0.0345 0.306 6.432 5.215 228.286 0.727 23.198 10.362 0.25 132609. 0.6612 4.46 0.0747 0.1963 0.0918 0.0349 0.310 6.513 5.121 231.175 0.736 22.777 10.047 0.25 132717. 0.6352 5.94 0.0996 0.2537 0.0900 0.0353 0.313 6.586 5.018 233.747 0.744 22.322 9.738 0.25 132834. 0.6095 7.43 0.1245 0.3073 0.0880 0.0357 0.316 6.647 4.908 235.933 0.751 21.831 9.435 0.25 132960. 0.5841 8.91 0.1494 0.3572 0.0859 0.0359 0.319 6.696 4.789 237.660 0.756 21.303 9.140 0.25 133095. 0.5589 10.40 0.1743 0.4036 0.0836 0.0361 0.320 6.729 4.662 238.853 0.760 20.736 8.852 0.25 133240. 0.5341 11.89 0.1992 0.4467 0.0811 0.0362 0.321 6.746 4.525 239.438 0.762 20.128 8.572 0.25 133395. 0.5095 13.37 0.2241 0.4866 0.0785 0.0362 0.321 6.743 4.379 239.338 0.762 19.480 8.300 0.25 133560. 0.4853 14.86 0.2491 0.5233 0.0757 0.0360 0.320 6.719 4.224 238.477 0.759 18.789 8.034 0.25 133736. 0.4614 16.34 0.2740 0.5571 0.0728 0.0358 0.318 6.671 4.059 236.784 0.754 18.055 7.776 0.25 133923. 0.4377 17.83 0.2989 0.5881 0.0696 0.0354 0.314 6.598 3.884 234.178 0.745 17.278 7.523 0.25 134120. 0.4143 19.32 0.3238 0.6162 0.0663 0.0348 0.309 6.496 3.699 230.576 0.734 16.454 7.277 0.25 134328. 0.3911 20.80 0.3487 0.6415 0.0628 0.0341 0.303 6.365 3.504 225.918 0.719 15.586 7.035 0.25 134547. 0.3680 22.29 0.3736 0.6641 0.0592 0.0333 0.295 6.204 3.300 220.199 0.701 14.678 6.797 0.25 134777. 0.3450 23.77 0.3985 0.6838 0.0554 0.0323 0.286 6.013 3.087 213.432 0.679 13.733 6.561 0.25 135019. 0.3221 25.26 0.4234 0.7005 0.0514 0.0311 0.276 5.794 2.868 205.632 0.655 12.756 6.326 0.25 135271. 0.2993 26.74 0.4483 0.7139 0.0474 0.0297 0.264 5.545 2.642 196.817 0.626 11.751 6.088 0.25 135535. 0.2765 28.23 0.4732 0.7236 0.0432 0.0283 0.251 5.269 2.410 187.003 0.595 10.722 5.847 0.25 135810. 0.2536 29.72 0.4981 0.7291 0.0390 0.0266 0.236 4.965 2.174 176.213 0.561 9.671 5.597 0.25 136097. 0.2306 31.20 0.5230 0.7297 0.0347 0.0249 0.221 4.634 1.934 164.472 0.524 8.604 5.334 0.25 136394. 0.2073 32.69 0.5479 0.7242 0.0303 0.0229 0.204 4.277 1.691 151.812 0.483 7.523 5.053 0.25 136703. 0.1836 34.17 0.5728 0.7109 0.0259 0.0209 0.185 3.896 1.446 138.272 0.440 6.434 4.745 0.25 137024. 0.1594 35.66 0.5977 0.6870 0.0215 0.0187 0.166 3.491 1.201 123.902 0.394 5.340 4.395 0.25 137356. 0.1345 37.15 0.6226 0.6483 0.0171 0.0164 0.146 3.064 0.955 108.765 0.346 4.247 3.981 0.25 137699. 0.1087 38.63 0.6475 0.5870 0.0127 0.0140 0.125 2.618 0.710 92.937 0.296 3.159 3.466 0.26 138054. 0.0816 40.12 0.6724 0.4884 0.0084 0.0116 0.103 2.156 0.468 76.511 0.244 2.083 2.777 0.26 138420. 0.0531 41.60 0.6973 0.3203 0.0041 0.0090 0.080 1.679 0.231 59.596 0.190 1.026 1.756 0.26 138797. 0.0236 43.09 0.7222 -0.0043 0.0000 0.0064 0.057 1.190 -0.002 42.253 0.134 -0.009 -0.023 0.26 139179. 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 0.0971 0.0331 0.697 10.985 9.630 519.848 1.241 42.834 8.402 0.33 176548. 0.7285 1.98 0.0249 0.0708 0.0957 0.0337 0.708 11.156 9.487 527.950 1.260 42.199 8.151 0.33 176671. 0.7015 3.96 0.0498 0.1374 0.0941 0.0341 0.718 11.318 9.332 535.608 1.279 41.509 7.903 0.33 176804. 0.6745 5.95 0.0748 0.1997 0.0924 0.0346 0.728 11.467 9.164 542.662 1.296 40.760 7.659 0.33 176949. 0.6478 7.93 0.0997 0.2580 0.0906 0.0350 0.736 11.600 8.982 548.955 1.311 39.951 7.421 0.33 177105. 0.6214 9.91 0.1246 0.3124 0.0886 0.0353 0.743 11.713 8.785 554.320 1.323 39.077 7.189 0.33 177274. 0.5953 11.89 0.1495 0.3630 0.0865 0.0356 0.749 11.803 8.574 558.583 1.334 38.136 6.962 0.33 177455. 0.5696 13.88 0.1744 0.4101 0.0842 0.0358 0.753 11.866 8.347 561.561 1.341 37.125 6.741 0.33 177649. 0.5442 15.86 0.1994 0.4538 0.0817 0.0359 0.755 11.898 8.103 563.073 1.344 36.042 6.527 0.33 177856. 0.5191 17.84 0.2243 0.4942 0.0791 0.0359 0.755 11.895 7.843 562.934 1.344 34.884 6.319 0.33 178077. 0.4945 19.82 0.2492 0.5316 0.0763 0.0358 0.752 11.853 7.565 560.962 1.339 33.650 6.117 0.33 178312. 0.4701 21.81 0.2741 0.5660 0.0733 0.0355 0.747 11.769 7.270 556.978 1.330 32.338 5.920 0.33 178561. 0.4460 23.79 0.2990 0.5975 0.0702 0.0351 0.739 11.639 6.958 550.795 1.315 30.947 5.729 0.33 178825. 0.4223 25.77 0.3240 0.6262 0.0668 0.0346 0.727 11.457 6.626 542.206 1.294 29.474 5.543 0.33 179103. 0.3987 27.75 0.3489 0.6523 0.0633 0.0339 0.712 11.222 6.277 531.064 1.268 27.920 5.361 0.34 179396. 0.3753 29.73 0.3738 0.6756 0.0596 0.0330 0.694 10.932 5.911 517.352 1.235 26.294 5.183 0.34 179704. 0.3521 31.72 0.3987 0.6961 0.0558 0.0319 0.672 10.588 5.531 501.097 1.196 24.602 5.006 0.34 180026. 0.3290 33.70 0.4236 0.7137 0.0518 0.0308 0.647 10.192 5.137 482.336 1.151 22.852 4.831 0.34 180364. 0.3060 35.68 0.4486 0.7282 0.0477 0.0294 0.618 9.743 4.733 461.106 1.101 21.051 4.655 0.34 180716. 0.2830 37.66 0.4735 0.7392 0.0435 0.0279 0.587 9.244 4.318 437.449 1.044 19.206 4.477 0.34 181084. 0.2599 39.65 0.4984 0.7463 0.0393 0.0262 0.552 8.693 3.895 411.416 0.982 17.323 4.294 0.34 181466. 0.2368 41.63 0.5233 0.7486 0.0349 0.0244 0.514 8.094 3.464 383.066 0.915 15.410 4.102 0.34 181864. 0.2133 43.61 0.5482 0.7452 0.0305 0.0225 0.473 7.448 3.029 352.478 0.841 13.473 3.898 0.34 182276. 0.1895 45.59 0.5732 0.7344 0.0261 0.0204 0.429 6.756 2.590 319.748 0.763 11.520 3.674 0.34 182704. 0.1652 47.58 0.5981 0.7134 0.0217 0.0182 0.382 6.022 2.149 284.997 0.680 9.560 3.420 0.34 183147. 0.1401 49.56 0.6230 0.6779 0.0172 0.0158 0.333 5.248 1.709 248.377 0.593 7.600 3.120 0.34 183606. 0.1140 51.54 0.6479 0.6199 0.0128 0.0134 0.282 4.439 1.271 210.076 0.502 5.652 2.743 0.34 184079. 0.0864 53.52 0.6729 0.5233 0.0084 0.0109 0.228 3.599 0.837 170.322 0.407 3.725 2.230 0.34 184568. 0.0570 55.50 0.6978 0.3513 0.0042 0.0082 0.174 2.734 0.412 129.380 0.309 1.832 1.444 0.34 185072. 0.0259 57.49 0.7227 -0.0070 -0.0001 0.0056 0.117 1.846 -0.005 87.376 0.209 -0.024 -0.028 0.34 185580. 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 0.0979 0.0331 1.358 17.125 15.166 1013.022 1.935 67.458 6.790 0.42 220672. 0.7389 2.48 0.0249 0.0715 0.0964 0.0336 1.380 17.398 14.944 1029.222 1.966 66.471 6.586 0.42 220826. 0.7113 4.95 0.0498 0.1387 0.0949 0.0341 1.401 17.657 14.702 1044.545 1.995 65.396 6.384 0.42 220993. 0.6840 7.43 0.0747 0.2015 0.0932 0.0346 1.420 17.896 14.440 1058.673 2.022 64.230 6.187 0.42 221174. 0.6569 9.91 0.0996 0.2603 0.0914 0.0350 1.437 18.110 14.156 1071.295 2.046 62.967 5.994 0.42 221370. 0.6301 12.39 0.1246 0.3152 0.0894 0.0353 1.451 18.292 13.849 1082.076 2.067 61.601 5.805 0.42 221581. 0.6036 14.86 0.1495 0.3663 0.0872 0.0356 1.463 18.437 13.518 1090.668 2.083 60.129 5.622 0.42 221808. 0.5775 17.34 0.1744 0.4138 0.0849 0.0358 1.471 18.539 13.162 1096.711 2.095 58.546 5.444 0.42 222051. 0.5518 19.82 0.1993 0.4579 0.0825 0.0359 1.475 18.592 12.780 1099.840 2.101 56.847 5.271 0.42 222311. 0.5265 22.29 0.2242 0.4987 0.0798 0.0359 1.475 18.590 12.372 1099.689 2.100 55.031 5.103 0.42 222587. 0.5015 24.77 0.2491 0.5365 0.0770 0.0358 1.470 18.526 11.936 1095.898 2.093 53.093 4.940 0.42 222881. 0.4769 27.25 0.2740 0.5713 0.0740 0.0355 1.459 18.394 11.473 1088.106 2.078 51.032 4.782 0.42 223193. 0.4526 29.72 0.2989 0.6032 0.0709 0.0351 1.443 18.188 10.981 1075.948 2.055 48.845 4.629 0.42 223523. 0.4286 32.20 0.3239 0.6325 0.0675 0.0346 1.420 17.902 10.460 1059.013 2.023 46.528 4.480 0.42 223872. 0.4049 34.68 0.3488 0.6590 0.0640 0.0339 1.391 17.530 9.911 1036.998 1.981 44.083 4.335 0.42 224238. 0.3813 37.16 0.3737 0.6829 0.0602 0.0330 1.354 17.071 9.335 1009.857 1.929 41.521 4.193 0.42 224623. 0.3579 39.63 0.3986 0.7042 0.0564 0.0319 1.311 16.527 8.735 977.642 1.867 38.855 4.053 0.42 225027. 0.3347 42.11 0.4235 0.7226 0.0524 0.0307 1.261 15.897 8.115 940.423 1.796 36.097 3.914 0.42 225449. 0.3115 44.59 0.4484 0.7380 0.0483 0.0293 1.205 15.185 7.477 898.273 1.716 33.257 3.775 0.42 225890. 0.2884 47.06 0.4733 0.7500 0.0440 0.0278 1.142 14.390 6.823 851.276 1.626 30.347 3.635 0.42 226349. 0.2653 49.54 0.4982 0.7583 0.0397 0.0261 1.072 13.516 6.155 799.529 1.527 27.377 3.492 0.42 226827. 0.2420 52.02 0.5231 0.7622 0.0353 0.0243 0.997 12.563 5.476 743.154 1.419 24.358 3.342 0.42 227324. 0.2185 54.49 0.5481 0.7605 0.0309 0.0223 0.915 11.534 4.789 682.302 1.303 21.301 3.183 0.42 227840. 0.1947 56.97 0.5730 0.7518 0.0264 0.0201 0.828 10.433 4.096 617.165 1.179 18.218 3.010 0.42 228375. 0.1702 59.45 0.5979 0.7334 0.0219 0.0179 0.735 9.263 3.400 547.987 1.047 15.122 2.814 0.42 228929. 0.1450 61.93 0.6228 0.7009 0.0175 0.0155 0.637 8.031 2.704 475.070 0.907 12.028 2.582 0.42 229502. 0.1186 64.40 0.6477 0.6462 0.0130 0.0130 0.535 6.741 2.012 398.791 0.762 8.951 2.289 0.43 230094. 0.0907 66.88 0.6726 0.5527 0.0086 0.0104 0.429 5.403 1.328 319.607 0.610 5.908 1.885 0.43 230704. 0.0607 69.36 0.6975 0.3801 0.0042 0.0078 0.319 4.024 0.656 238.056 0.455 2.918 1.250 0.43 231334. 0.0283 71.83 0.7224 -0.0027 0.0000 0.0050 0.207 2.609 -0.003 154.363 0.295 -0.013 -0.008 0.43 231967. 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 0.0988 0.0332 2.358 24.771 22.054 1758.387 2.799 98.096 5.689 0.50 264786. 0.7465 2.97 0.0249 0.0719 0.0974 0.0338 2.397 25.175 21.737 1787.087 2.844 96.685 5.517 0.50 264972. 0.7187 5.94 0.0498 0.1394 0.0959 0.0343 2.433 25.557 21.391 1814.244 2.887 95.145 5.348 0.50 265173. 0.6911 8.92 0.0747 0.2026 0.0942 0.0347 2.467 25.910 21.014 1839.303 2.927 93.471 5.182 0.50 265391. 0.6637 11.89 0.0996 0.2616 0.0924 0.0352 2.497 26.226 20.606 1861.697 2.963 91.654 5.020 0.50 265627. 0.6367 14.86 0.1245 0.3168 0.0904 0.0355 2.522 26.496 20.164 1880.848 2.993 89.687 4.862 0.50 265881. 0.6101 17.83 0.1495 0.3681 0.0882 0.0358 2.543 26.711 19.686 1896.129 3.018 87.564 4.709 0.50 266154. 0.5838 20.80 0.1744 0.4159 0.0859 0.0360 2.557 26.863 19.172 1906.906 3.035 85.276 4.560 0.50 266446. 0.5579 23.78 0.1993 0.4603 0.0835 0.0361 2.565 26.942 18.620 1912.538 3.044 82.820 4.416 0.50 266759. 0.5324 26.75 0.2242 0.5014 0.0808 0.0361 2.565 26.940 18.028 1912.377 3.044 80.190 4.276 0.50 267092. 0.5073 29.72 0.2491 0.5395 0.0780 0.0360 2.556 26.847 17.397 1905.783 3.033 77.381 4.140 0.50 267446. 0.4825 32.69 0.2740 0.5746 0.0750 0.0357 2.537 26.655 16.725 1892.130 3.011 74.391 4.009 0.50 267821. 0.4581 35.66 0.2989 0.6069 0.0718 0.0353 2.509 26.354 16.011 1870.774 2.977 71.216 3.882 0.50 268218. 0.4340 38.64 0.3238 0.6366 0.0684 0.0348 2.469 25.934 15.254 1840.997 2.930 67.850 3.758 0.50 268637. 0.4101 41.61 0.3487 0.6636 0.0648 0.0340 2.417 25.388 14.455 1802.251 2.868 64.294 3.638 0.50 269077. 0.3864 44.58 0.3736 0.6880 0.0610 0.0331 2.353 24.715 13.616 1754.433 2.792 60.566 3.520 0.50 269540. 0.3630 47.55 0.3985 0.7098 0.0571 0.0321 2.277 23.915 12.744 1697.632 2.702 56.683 3.405 0.50 270026. 0.3396 50.53 0.4234 0.7289 0.0531 0.0308 2.189 22.990 11.840 1631.971 2.597 52.664 3.291 0.50 270533. 0.3164 53.50 0.4484 0.7451 0.0489 0.0294 2.089 21.942 10.909 1557.583 2.479 48.525 3.177 0.50 271063. 0.2932 56.47 0.4733 0.7580 0.0446 0.0279 1.977 20.773 9.955 1474.615 2.347 44.280 3.062 0.51 271614. 0.2699 59.44 0.4982 0.7674 0.0403 0.0261 1.855 19.486 8.981 1383.239 2.201 39.947 2.945 0.51 272189. 0.2466 62.41 0.5231 0.7725 0.0358 0.0242 1.721 18.083 7.990 1283.671 2.043 35.541 2.823 0.51 272786. 0.2230 65.39 0.5480 0.7723 0.0313 0.0222 1.577 16.569 6.987 1176.178 1.872 31.078 2.694 0.51 273405. 0.1990 68.36 0.5729 0.7654 0.0268 0.0200 1.423 14.948 5.975 1061.101 1.689 26.576 2.554 0.51 274047. 0.1744 71.33 0.5978 0.7491 0.0222 0.0177 1.259 13.226 4.958 938.870 1.494 22.055 2.395 0.51 274712. 0.1490 74.30 0.6227 0.7190 0.0177 0.0153 1.086 11.411 3.942 810.024 1.289 17.535 2.207 0.51 275399. 0.1225 77.27 0.6476 0.6671 0.0131 0.0128 0.906 9.512 2.931 675.233 1.075 13.039 1.969 0.51 276110. 0.0942 80.25 0.6725 0.5758 0.0087 0.0101 0.718 7.541 1.932 535.314 0.852 8.593 1.637 0.51 276843. 0.0636 83.22 0.6974 0.4017 0.0043 0.0074 0.525 5.511 0.950 391.225 0.623 4.224 1.101 0.51 277598. 0.0300 86.19 0.7224 -0.0097 -0.0001 0.0046 0.326 3.427 -0.014 243.260 0.387 -0.061 -0.026 0.51 278354. 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 0.1000 0.0336 3.784 34.068 30.379 2821.485 3.849 135.128 4.884 0.58 308888. 0.7521 3.49 0.0250 0.0724 0.0986 0.0341 3.847 34.638 29.950 2868.634 3.913 133.215 4.735 0.58 309106. 0.7241 6.97 0.0501 0.1403 0.0971 0.0347 3.907 35.176 29.479 2913.240 3.974 131.123 4.590 0.58 309343. 0.6963 10.46 0.0751 0.2038 0.0954 0.0351 3.962 35.673 28.966 2954.383 4.030 128.841 4.447 0.58 309600. 0.6687 13.94 0.1001 0.2633 0.0935 0.0356 4.011 36.117 28.408 2991.128 4.080 126.359 4.308 0.58 309878. 0.6415 17.43 0.1252 0.3187 0.0915 0.0360 4.053 36.495 27.802 3022.490 4.123 123.664 4.172 0.58 310178. 0.6147 20.91 0.1502 0.3704 0.0894 0.0363 4.087 36.797 27.146 3047.439 4.157 120.747 4.040 0.58 310500. 0.5882 24.40 0.1753 0.4185 0.0871 0.0365 4.110 37.008 26.439 3064.932 4.181 117.600 3.913 0.58 310845. 0.5621 27.88 0.2003 0.4631 0.0846 0.0366 4.122 37.116 25.677 3073.889 4.193 114.212 3.789 0.58 311214. 0.5364 31.37 0.2253 0.5045 0.0819 0.0366 4.121 37.108 24.860 3073.242 4.192 110.578 3.669 0.58 311607. 0.5112 34.85 0.2504 0.5429 0.0790 0.0364 4.106 36.972 23.987 3061.947 4.177 106.692 3.553 0.58 312024. 0.4862 38.34 0.2754 0.5783 0.0759 0.0362 4.075 36.694 23.055 3038.966 4.146 102.549 3.441 0.59 312467. 0.4617 41.82 0.3004 0.6110 0.0727 0.0357 4.027 36.263 22.065 3003.249 4.097 98.144 3.332 0.59 312936. 0.4374 45.31 0.3255 0.6410 0.0692 0.0351 3.961 35.664 21.014 2953.621 4.029 93.469 3.227 0.59 313430. 0.4133 48.79 0.3505 0.6684 0.0655 0.0344 3.874 34.886 19.902 2889.182 3.941 88.526 3.124 0.59 313950. 0.3895 52.28 0.3756 0.6932 0.0617 0.0334 3.768 33.927 18.736 2809.782 3.833 83.339 3.025 0.59 314497. 0.3658 55.76 0.4006 0.7154 0.0577 0.0323 3.642 32.790 17.521 2715.574 3.705 77.935 2.927 0.59 315069. 0.3423 59.25 0.4256 0.7350 0.0536 0.0310 3.496 31.476 16.263 2606.767 3.556 72.338 2.830 0.59 315668. 0.3189 62.73 0.4507 0.7517 0.0493 0.0295 3.331 29.988 14.966 2483.589 3.388 66.571 2.733 0.59 316292. 0.2955 66.22 0.4757 0.7653 0.0449 0.0279 3.146 28.331 13.637 2346.295 3.201 60.656 2.636 0.59 316943. 0.2720 69.71 0.5007 0.7753 0.0404 0.0261 2.944 26.506 12.279 2195.177 2.995 54.617 2.537 0.59 317620. 0.2484 73.19 0.5258 0.7811 0.0359 0.0242 2.723 24.519 10.898 2030.601 2.770 48.474 2.434 0.59 318324. 0.2245 76.68 0.5508 0.7816 0.0313 0.0220 2.485 22.375 9.499 1853.025 2.528 42.253 2.325 0.59 319054. 0.2002 80.16 0.5759 0.7753 0.0266 0.0198 2.230 20.080 8.089 1663.032 2.269 35.978 2.206 0.59 319811. 0.1753 83.65 0.6009 0.7594 0.0220 0.0174 1.960 17.645 6.672 1461.357 1.994 29.676 2.071 0.59 320594. 0.1495 87.13 0.6259 0.7291 0.0173 0.0149 1.675 15.080 5.256 1248.922 1.704 23.379 1.909 0.59 321404. 0.1223 90.62 0.6510 0.6753 0.0127 0.0122 1.377 12.399 3.849 1026.875 1.401 17.118 1.700 0.60 322241. 0.0932 94.10 0.6760 0.5773 0.0081 0.0095 1.068 9.619 2.458 796.619 1.087 10.932 1.399 0.60 323104. 0.0613 97.59 0.7010 0.3787 0.0036 0.0067 0.751 6.759 1.093 559.784 0.764 4.860 0.885 0.60 323993. 0.0259 101.07 0.7261 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 0.1015 0.0341 5.741 45.234 40.257 4281.358 5.110 179.061 4.265 0.67 352973. 0.7561 3.95 0.0248 0.0717 0.1001 0.0347 5.838 45.997 39.708 4353.609 5.197 176.622 4.137 0.67 353221. 0.7284 7.90 0.0497 0.1390 0.0986 0.0352 5.930 46.720 39.107 4422.063 5.278 173.946 4.011 0.67 353490. 0.7009 11.86 0.0745 0.2021 0.0969 0.0357 6.015 47.388 38.448 4485.288 5.354 171.019 3.888 0.67 353783. 0.6736 15.81 0.0994 0.2611 0.0951 0.0362 6.091 47.986 37.731 4541.863 5.421 167.826 3.768 0.67 354099. 0.6467 19.76 0.1242 0.3163 0.0932 0.0366 6.156 48.498 36.950 4590.306 5.479 164.352 3.651 0.67 354439. 0.6201 23.71 0.1491 0.3678 0.0910 0.0369 6.208 48.907 36.102 4629.046 5.526 160.582 3.537 0.67 354805. 0.5939 27.67 0.1739 0.4157 0.0887 0.0371 6.244 49.197 35.186 4656.499 5.558 156.506 3.427 0.67 355197. 0.5680 31.62 0.1987 0.4603 0.0862 0.0372 6.264 49.351 34.198 4671.047 5.576 152.111 3.321 0.67 355616. 0.5426 35.57 0.2236 0.5017 0.0835 0.0372 6.264 49.352 33.136 4671.092 5.576 147.387 3.218 0.67 356062. 0.5175 39.52 0.2484 0.5402 0.0807 0.0371 6.243 49.182 31.998 4655.054 5.557 142.328 3.118 0.67 356536. 0.4928 43.48 0.2733 0.5758 0.0776 0.0368 6.197 48.826 30.784 4621.388 5.516 136.927 3.021 0.67 357038. 0.4684 47.43 0.2981 0.6088 0.0743 0.0364 6.127 48.268 29.491 4568.547 5.453 131.177 2.928 0.67 357569. 0.4443 51.38 0.3230 0.6391 0.0709 0.0358 6.028 47.489 28.118 4494.829 5.365 125.069 2.837 0.67 358129. 0.4204 55.33 0.3478 0.6669 0.0672 0.0351 5.899 46.474 26.664 4398.733 5.251 118.603 2.749 0.67 358718. 0.3967 59.28 0.3726 0.6923 0.0634 0.0341 5.739 45.218 25.136 4279.884 5.109 111.804 2.664 0.67 359336. 0.3732 63.24 0.3975 0.7153 0.0593 0.0330 5.550 43.724 23.541 4138.495 4.940 104.709 2.580 0.67 359983. 0.3498 67.19 0.4223 0.7356 0.0552 0.0317 5.330 41.996 21.886 3974.898 4.745 97.350 2.497 0.67 360660. 0.3265 71.14 0.4472 0.7533 0.0509 0.0302 5.082 40.037 20.180 3789.444 4.523 89.759 2.415 0.67 361366. 0.3032 75.09 0.4720 0.7680 0.0465 0.0286 4.804 37.850 18.427 3582.523 4.276 81.965 2.333 0.67 362102. 0.2798 79.05 0.4969 0.7795 0.0419 0.0267 4.499 35.442 16.636 3354.580 4.004 73.996 2.249 0.67 362867. 0.2563 83.00 0.5217 0.7870 0.0373 0.0248 4.165 32.817 14.812 3106.151 3.708 65.883 2.163 0.68 363661. 0.2326 86.95 0.5465 0.7897 0.0327 0.0226 3.806 29.983 12.962 2837.906 3.388 57.657 2.072 0.68 364485. 0.2084 90.90 0.5714 0.7862 0.0280 0.0203 3.421 26.949 11.095 2550.696 3.045 49.350 1.973 0.68 365339. 0.1836 94.86 0.5962 0.7742 0.0232 0.0179 3.011 23.725 9.217 2245.585 2.680 40.997 1.862 0.68 366223. 0.1579 98.81 0.6211 0.7494 0.0185 0.0153 2.580 20.327 7.338 1923.923 2.297 32.639 1.730 0.68 367136. 0.1309 102.76 0.6459 0.7037 0.0138 0.0127 2.129 16.771 5.467 1587.407 1.895 24.318 1.562 0.68 368079. 0.1021 106.71 0.6708 0.6197 0.0091 0.0099 1.660 13.081 3.616 1238.154 1.478 16.083 1.325 0.68 369053. 0.0704 110.66 0.6956 0.4496 0.0045 0.0070 1.178 9.284 1.795 878.706 1.049 7.986 0.927 0.68 370055. 0.0347 114.62 0.7204 0.0043 0.0000 0.0041 0.684 5.389 0.010 510.109 0.609 0.043 0.008 0.68 371060. 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 0.1033 0.0353 8.454 59.208 51.834 6304.510 6.689 230.557 3.729 0.75 397035. 0.7502 4.44 0.0248 0.0706 0.1019 0.0358 8.584 60.117 51.159 6401.301 6.792 227.555 3.625 0.75 397315. 0.7244 8.88 0.0496 0.1371 0.1004 0.0363 8.708 60.980 50.415 6493.190 6.889 224.244 3.522 0.75 397619. 0.6987 13.32 0.0744 0.1997 0.0988 0.0368 8.822 61.778 49.597 6578.194 6.980 220.606 3.420 0.75 397949. 0.6729 17.76 0.0992 0.2585 0.0970 0.0372 8.924 62.493 48.700 6654.325 7.060 216.618 3.319 0.75 398306. 0.6473 22.20 0.1241 0.3135 0.0951 0.0376 9.011 63.105 47.720 6719.449 7.130 212.259 3.221 0.75 398690. 0.6217 26.64 0.1489 0.3650 0.0929 0.0379 9.080 63.592 46.653 6771.296 7.185 207.512 3.125 0.75 399103. 0.5964 31.08 0.1737 0.4131 0.0906 0.0381 9.129 63.932 45.494 6807.498 7.223 202.358 3.031 0.75 399546. 0.5713 35.53 0.1985 0.4579 0.0881 0.0382 9.153 64.102 44.240 6825.647 7.242 196.782 2.940 0.75 400019. 0.5464 39.97 0.2233 0.4995 0.0854 0.0382 9.150 64.080 42.889 6823.283 7.240 190.771 2.851 0.75 400523. 0.5217 44.41 0.2481 0.5382 0.0825 0.0380 9.116 63.842 41.438 6797.963 7.213 184.316 2.765 0.75 401058. 0.4973 48.85 0.2729 0.5742 0.0794 0.0378 9.048 63.366 39.885 6747.271 7.159 177.408 2.681 0.75 401625. 0.4731 53.29 0.2977 0.6074 0.0761 0.0373 8.943 62.629 38.229 6668.774 7.076 170.041 2.600 0.75 402224. 0.4492 57.73 0.3225 0.6381 0.0726 0.0367 8.797 61.606 36.466 6559.841 6.960 162.201 2.521 0.75 402855. 0.4254 62.17 0.3474 0.6664 0.0689 0.0359 8.607 60.274 34.597 6418.042 6.810 153.886 2.445 0.75 403520. 0.4018 66.61 0.3722 0.6923 0.0650 0.0349 8.371 58.627 32.628 6242.620 6.624 145.128 2.371 0.75 404217. 0.3784 71.05 0.3970 0.7158 0.0609 0.0338 8.092 56.666 30.569 6033.880 6.402 135.973 2.298 0.76 404947. 0.3550 75.49 0.4218 0.7368 0.0566 0.0324 7.768 54.398 28.432 5792.357 6.146 126.464 2.226 0.76 405709. 0.3317 79.93 0.4466 0.7553 0.0522 0.0309 7.401 51.828 26.224 5518.637 5.855 116.644 2.155 0.76 406504. 0.3084 84.37 0.4714 0.7709 0.0477 0.0292 6.991 48.961 23.954 5213.410 5.532 106.549 2.084 0.76 407332. 0.2850 88.81 0.4962 0.7832 0.0431 0.0273 6.541 45.806 21.632 4877.470 5.175 96.219 2.012 0.76 408193. 0.2614 93.25 0.5210 0.7918 0.0384 0.0253 6.050 42.372 19.265 4511.805 4.787 85.692 1.937 0.76 409087. 0.2375 97.69 0.5458 0.7956 0.0336 0.0230 5.522 38.671 16.863 4117.666 4.369 75.007 1.858 0.76 410014. 0.2131 102.14 0.5707 0.7931 0.0288 0.0207 4.957 34.717 14.435 3696.665 3.922 64.208 1.771 0.76 410974. 0.1880 106.58 0.5955 0.7817 0.0239 0.0182 4.359 30.530 11.992 3250.870 3.449 53.341 1.673 0.76 411967. 0.1619 111.02 0.6203 0.7571 0.0190 0.0156 3.732 26.135 9.545 2782.906 2.953 42.455 1.556 0.76 412993. 0.1343 115.46 0.6451 0.7105 0.0142 0.0129 3.079 21.563 7.106 2296.052 2.436 31.608 1.404 0.77 414052. 0.1046 119.90 0.6699 0.6232 0.0093 0.0100 2.406 16.851 4.690 1794.317 1.904 20.863 1.186 0.77 415145. 0.0717 124.34 0.6947 0.4459 0.0046 0.0072 1.720 12.043 2.313 1282.393 1.361 10.287 0.818 0.77 416271. 0.0348 128.78 0.7195 -0.0077 0.0000 0.0043 1.022 7.158 -0.023 762.194 0.809 -0.102 -0.014 0.77 417397. 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 0.1053 0.0393 12.905 81.341 65.256 9623.585 9.190 290.257 3.076 0.83 441067. 0.6942 4.93 0.0248 0.0650 0.1040 0.0396 13.028 82.112 64.463 9714.799 9.277 286.730 3.010 0.83 441378. 0.6752 9.85 0.0495 0.1271 0.1026 0.0400 13.138 82.806 63.581 9796.892 9.355 282.809 2.944 0.83 441717. 0.6558 14.78 0.0743 0.1864 0.1010 0.0403 13.233 83.403 62.605 9867.607 9.423 278.469 2.878 0.83 442084. 0.6362 19.71 0.0991 0.2429 0.0993 0.0405 13.309 83.885 61.528 9924.634 9.477 273.679 2.812 0.83 442482. 0.6163 24.63 0.1239 0.2966 0.0974 0.0407 13.364 84.232 60.344 9965.585 9.516 268.411 2.746 0.83 442911. 0.5961 29.56 0.1486 0.3475 0.0953 0.0408 13.394 84.421 59.046 9987.961 9.538 262.638 2.681 0.83 443372. 0.5757 34.48 0.1734 0.3956 0.0930 0.0408 13.396 84.431 57.630 9989.172 9.539 256.337 2.617 0.83 443866. 0.5550 39.41 0.1982 0.4410 0.0905 0.0407 13.365 84.239 56.089 9966.502 9.517 249.485 2.553 0.83 444394. 0.5342 44.34 0.2230 0.4838 0.0878 0.0405 13.299 83.822 54.421 9917.165 9.470 242.065 2.489 0.84 444956. 0.5130 49.26 0.2477 0.5239 0.0849 0.0401 13.193 83.156 52.622 9838.352 9.395 234.062 2.426 0.84 445554. 0.4917 54.19 0.2725 0.5615 0.0818 0.0397 13.045 82.218 50.689 9727.307 9.289 225.465 2.364 0.84 446186. 0.4702 59.12 0.2973 0.5965 0.0784 0.0391 12.848 80.982 48.621 9581.126 9.149 216.266 2.302 0.84 446855. 0.4484 64.04 0.3220 0.6290 0.0749 0.0383 12.601 79.422 46.415 9396.547 8.973 206.452 2.240 0.84 447560. 0.4265 68.97 0.3468 0.6591 0.0711 0.0374 12.297 77.508 44.068 9170.118 8.757 196.015 2.180 0.84 448300. 0.4043 73.90 0.3716 0.6866 0.0671 0.0363 11.935 75.227 41.590 8900.251 8.499 184.991 2.119 0.84 449077. 0.3819 78.82 0.3964 0.7116 0.0629 0.0350 11.516 72.585 38.993 8587.680 8.201 173.439 2.059 0.84 449890. 0.3593 83.75 0.4211 0.7338 0.0586 0.0336 11.045 69.613 36.289 8235.990 7.865 161.413 1.998 0.84 450739. 0.3364 88.68 0.4459 0.7528 0.0540 0.0320 10.519 66.300 33.491 7844.083 7.491 148.969 1.937 0.84 451624. 0.3131 93.60 0.4707 0.7684 0.0494 0.0303 9.943 62.667 30.611 7414.197 7.080 136.156 1.873 0.84 452545. 0.2895 98.53 0.4955 0.7800 0.0446 0.0283 9.316 58.718 27.659 6947.015 6.634 123.026 1.806 0.84 453503. 0.2654 103.45 0.5202 0.7869 0.0398 0.0263 8.640 54.457 24.646 6442.914 6.153 109.627 1.735 0.84 454496. 0.2407 108.38 0.5450 0.7877 0.0348 0.0241 7.919 49.914 21.585 5905.404 5.639 96.011 1.658 0.85 455526. 0.2152 113.31 0.5698 0.7803 0.0298 0.0218 7.158 45.118 18.487 5337.978 5.097 82.231 1.571 0.85 456591. 0.1887 118.23 0.5945 0.7612 0.0248 0.0194 6.364 40.111 15.366 4745.559 4.532 68.347 1.469 0.85 457694. 0.1609 123.16 0.6193 0.7249 0.0197 0.0169 5.543 34.938 12.235 4133.618 3.947 54.423 1.343 0.85 458832. 0.1312 128.09 0.6441 0.6615 0.0147 0.0143 4.705 29.655 9.112 3508.491 3.350 40.530 1.178 0.85 460007. 0.0994 133.01 0.6689 0.5528 0.0097 0.0117 3.859 24.321 6.014 2877.432 2.748 26.751 0.948 0.85 461219. 0.0650 137.94 0.6936 0.3614 0.0048 0.0092 3.015 19.003 2.963 2248.316 2.147 13.177 0.598 0.85 462466. 0.0287 142.87 0.7184 -0.0061 -0.0001 0.0066 2.177 13.722 -0.035 1623.423 1.550 -0.155 -0.010 0.85 463723. 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 0.1064 0.0476 20.829 119.350 79.818 15532.555 13.484 355.032 2.331 0.92 485113. 0.5818 5.50 0.0251 0.0553 0.1053 0.0479 20.938 119.973 78.964 15613.690 13.555 351.230 2.294 0.92 485456. 0.5695 11.00 0.0503 0.1089 0.1040 0.0480 21.015 120.414 77.997 15671.011 13.604 346.931 2.257 0.92 485831. 0.5571 16.50 0.0754 0.1608 0.1026 0.0481 21.055 120.641 76.909 15700.520 13.630 342.090 2.222 0.92 486239. 0.5444 22.01 0.1006 0.2110 0.1009 0.0481 21.052 120.627 75.689 15698.711 13.628 336.663 2.187 0.92 486682. 0.5316 27.51 0.1257 0.2596 0.0991 0.0480 21.004 120.347 74.327 15662.374 13.597 330.604 2.152 0.92 487162. 0.5185 33.01 0.1509 0.3066 0.0971 0.0478 20.905 119.781 72.814 15588.697 13.533 323.875 2.119 0.92 487680. 0.5051 38.51 0.1760 0.3520 0.0949 0.0474 20.752 118.909 71.141 15475.132 13.434 316.437 2.085 0.92 488236. 0.4914 44.01 0.2012 0.3959 0.0924 0.0470 20.544 117.712 69.303 15319.377 13.299 308.258 2.052 0.92 488831. 0.4773 49.51 0.2263 0.4382 0.0897 0.0464 20.275 116.174 67.291 15119.270 13.125 299.310 2.019 0.92 489466. 0.4627 55.01 0.2515 0.4788 0.0868 0.0456 19.945 114.281 65.102 14872.933 12.911 289.572 1.985 0.92 490142. 0.4476 60.51 0.2766 0.5178 0.0836 0.0447 19.550 112.021 62.731 14578.764 12.656 279.028 1.952 0.92 490858. 0.4319 66.02 0.3018 0.5549 0.0802 0.0436 19.090 109.381 60.177 14235.117 12.358 267.668 1.917 0.92 491616. 0.4156 71.52 0.3269 0.5902 0.0766 0.0424 18.559 106.339 57.435 13839.281 12.014 255.470 1.882 0.92 492415. 0.3986 77.02 0.3521 0.6234 0.0727 0.0410 17.955 102.881 54.504 13389.193 11.623 242.433 1.846 0.92 493255. 0.3809 82.52 0.3772 0.6545 0.0685 0.0395 17.279 99.006 51.397 12884.880 11.186 228.613 1.809 0.92 494136. 0.3624 88.02 0.4024 0.6833 0.0642 0.0378 16.532 94.726 48.132 12327.901 10.702 214.092 1.771 0.92 495059. 0.3433 93.52 0.4275 0.7093 0.0596 0.0359 15.725 90.102 44.726 11726.154 10.180 198.940 1.730 0.92 496022. 0.3233 99.02 0.4527 0.7305 0.0549 0.0340 14.890 85.317 41.191 11103.378 9.639 183.217 1.683 0.93 497026. 0.3017 104.52 0.4778 0.7468 0.0501 0.0320 14.013 80.295 37.546 10449.857 9.072 167.005 1.630 0.93 498070. 0.2790 110.03 0.5030 0.7541 0.0451 0.0301 13.151 75.353 33.801 9806.662 8.513 150.345 1.563 0.93 499155. 0.2540 115.53 0.5281 0.7504 0.0400 0.0281 12.304 70.499 29.971 9174.940 7.965 133.311 1.482 0.93 500280. 0.2266 121.03 0.5533 0.7368 0.0348 0.0261 11.423 65.454 26.081 8518.330 7.395 116.008 1.389 0.93 501446. 0.1982 126.53 0.5784 0.7102 0.0295 0.0241 10.522 60.291 22.149 7846.394 6.812 98.518 1.280 0.93 502653. 0.1684 132.03 0.6036 0.6666 0.0243 0.0220 9.610 55.065 18.196 7166.386 6.221 80.936 1.152 0.93 503900. 0.1373 137.53 0.6287 0.6004 0.0190 0.0199 8.701 49.858 14.246 6488.646 5.633 63.366 0.996 0.93 505189. 0.1050 143.03 0.6539 0.5044 0.0138 0.0179 7.808 44.741 10.326 5822.682 5.055 45.929 0.804 0.94 506518. 0.0722 148.54 0.6790 0.3689 0.0086 0.0159 6.942 39.779 6.467 5176.944 4.494 28.764 0.567 0.94 507889. 0.0403 154.04 0.7042 0.1817 0.0036 0.0140 6.113 35.026 2.704 4558.441 3.957 12.025 0.269 0.94 509301. 0.0124 159.54 0.7293