18x12WE (18x12WE.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 0.1050 0.0446 0.007 0.427 0.351 5.056 0.048 1.563 31.515 0.07 32617. 0.6089 0.48 0.0280 0.0643 0.1038 0.0453 0.007 0.434 0.347 5.135 0.049 1.545 30.673 0.07 32642. 0.5892 0.96 0.0561 0.1250 0.1025 0.0460 0.007 0.441 0.343 5.213 0.050 1.525 29.828 0.07 32670. 0.5693 1.43 0.0841 0.1822 0.1010 0.0466 0.007 0.447 0.338 5.287 0.050 1.503 28.985 0.07 32701. 0.5492 1.91 0.1122 0.2359 0.0994 0.0472 0.007 0.453 0.332 5.357 0.051 1.479 28.148 0.07 32735. 0.5291 2.39 0.1402 0.2862 0.0976 0.0478 0.007 0.458 0.327 5.421 0.052 1.452 27.318 0.07 32772. 0.5089 2.87 0.1682 0.3332 0.0956 0.0483 0.007 0.463 0.320 5.477 0.052 1.423 26.500 0.07 32812. 0.4886 3.35 0.1963 0.3769 0.0935 0.0487 0.007 0.467 0.313 5.522 0.053 1.391 25.695 0.07 32855. 0.4685 3.82 0.2243 0.4175 0.0912 0.0490 0.007 0.470 0.305 5.555 0.053 1.357 24.904 0.07 32902. 0.4483 4.30 0.2524 0.4550 0.0886 0.0492 0.007 0.471 0.296 5.574 0.053 1.319 24.128 0.07 32952. 0.4283 4.78 0.2804 0.4897 0.0859 0.0492 0.007 0.471 0.287 5.576 0.053 1.278 23.368 0.07 33006. 0.4083 5.26 0.3084 0.5214 0.0829 0.0490 0.007 0.470 0.277 5.559 0.053 1.233 22.623 0.07 33063. 0.3883 5.74 0.3365 0.5505 0.0797 0.0487 0.007 0.467 0.267 5.522 0.053 1.186 21.891 0.07 33123. 0.3684 6.21 0.3645 0.5767 0.0762 0.0482 0.007 0.462 0.255 5.464 0.052 1.134 21.171 0.07 33188. 0.3485 6.69 0.3926 0.6001 0.0725 0.0475 0.007 0.455 0.243 5.381 0.051 1.080 20.458 0.07 33256. 0.3285 7.17 0.4206 0.6207 0.0686 0.0465 0.007 0.446 0.230 5.274 0.050 1.021 19.749 0.07 33327. 0.3085 7.65 0.4487 0.6382 0.0645 0.0453 0.007 0.434 0.216 5.140 0.049 0.960 19.037 0.07 33403. 0.2882 8.13 0.4767 0.6525 0.0601 0.0439 0.007 0.421 0.201 4.980 0.048 0.895 18.317 0.07 33482. 0.2678 8.60 0.5047 0.6631 0.0556 0.0423 0.006 0.405 0.186 4.795 0.046 0.827 17.580 0.07 33564. 0.2470 9.08 0.5328 0.6695 0.0508 0.0404 0.006 0.388 0.170 4.586 0.044 0.756 16.816 0.07 33651. 0.2260 9.56 0.5608 0.6711 0.0460 0.0384 0.006 0.368 0.154 4.355 0.042 0.684 16.014 0.07 33740. 0.2047 10.04 0.5889 0.6670 0.0410 0.0362 0.006 0.347 0.137 4.102 0.039 0.610 15.157 0.07 33834. 0.1829 10.52 0.6169 0.6558 0.0359 0.0338 0.005 0.324 0.120 3.830 0.037 0.534 14.225 0.07 33931. 0.1607 10.99 0.6449 0.6357 0.0308 0.0312 0.005 0.299 0.103 3.540 0.034 0.458 13.191 0.07 34032. 0.1380 11.47 0.6730 0.6043 0.0256 0.0285 0.004 0.273 0.086 3.232 0.031 0.381 12.016 0.07 34136. 0.1146 11.95 0.7010 0.5574 0.0204 0.0257 0.004 0.246 0.068 2.909 0.028 0.304 10.641 0.07 34244. 0.0906 12.43 0.7291 0.4891 0.0152 0.0227 0.003 0.217 0.051 2.572 0.025 0.226 8.977 0.07 34355. 0.0660 12.91 0.7571 0.3890 0.0101 0.0196 0.003 0.188 0.034 2.224 0.021 0.150 6.876 0.07 34470. 0.0412 13.38 0.7851 0.2392 0.0050 0.0165 0.003 0.158 0.017 1.866 0.018 0.075 4.077 0.07 34588. 0.0172 13.86 0.8132 0.0038 0.0001 0.0132 0.002 0.127 0.000 1.502 0.014 0.001 0.063 0.07 34710. 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 0.1054 0.0416 0.051 1.593 1.410 37.693 0.180 6.272 16.968 0.14 65232. 0.6568 0.96 0.0282 0.0694 0.1042 0.0423 0.051 1.621 1.394 38.367 0.183 6.201 16.480 0.14 65284. 0.6343 1.92 0.0564 0.1347 0.1028 0.0430 0.052 1.650 1.376 39.032 0.186 6.121 15.992 0.14 65341. 0.6116 2.88 0.0846 0.1960 0.1014 0.0437 0.053 1.677 1.357 39.675 0.189 6.034 15.508 0.14 65403. 0.5888 3.84 0.1128 0.2533 0.0998 0.0444 0.054 1.702 1.335 40.282 0.192 5.938 15.030 0.14 65471. 0.5661 4.80 0.1409 0.3067 0.0980 0.0450 0.055 1.726 1.311 40.841 0.195 5.831 14.560 0.14 65545. 0.5434 5.77 0.1691 0.3564 0.0960 0.0456 0.055 1.747 1.285 41.334 0.197 5.715 14.098 0.14 65626. 0.5209 6.73 0.1973 0.4024 0.0939 0.0460 0.056 1.764 1.256 41.745 0.199 5.587 13.647 0.14 65713. 0.4986 7.69 0.2255 0.4451 0.0915 0.0464 0.056 1.777 1.225 42.056 0.201 5.447 13.207 0.14 65807. 0.4764 8.65 0.2537 0.4845 0.0890 0.0466 0.057 1.786 1.190 42.251 0.202 5.295 12.779 0.14 65908. 0.4545 9.61 0.2819 0.5208 0.0862 0.0466 0.057 1.788 1.153 42.310 0.202 5.129 12.362 0.14 66016. 0.4327 10.57 0.3101 0.5541 0.0832 0.0465 0.057 1.784 1.113 42.216 0.202 4.950 11.957 0.14 66132. 0.4112 11.53 0.3383 0.5845 0.0799 0.0462 0.056 1.773 1.070 41.953 0.200 4.757 11.563 0.14 66254. 0.3898 12.49 0.3664 0.6122 0.0764 0.0458 0.056 1.754 1.023 41.507 0.198 4.550 11.178 0.14 66384. 0.3685 13.45 0.3946 0.6371 0.0727 0.0450 0.055 1.727 0.973 40.864 0.195 4.329 10.802 0.14 66521. 0.3474 14.41 0.4228 0.6592 0.0688 0.0441 0.054 1.691 0.920 40.013 0.191 4.094 10.432 0.14 66666. 0.3262 15.38 0.4510 0.6785 0.0646 0.0429 0.052 1.646 0.864 38.943 0.186 3.844 10.066 0.14 66818. 0.3050 16.34 0.4792 0.6947 0.0602 0.0415 0.050 1.591 0.805 37.649 0.180 3.581 9.700 0.14 66978. 0.2837 17.30 0.5074 0.7075 0.0556 0.0398 0.048 1.527 0.743 36.140 0.173 3.307 9.331 0.14 67144. 0.2623 18.26 0.5356 0.7167 0.0508 0.0380 0.046 1.455 0.680 34.429 0.164 3.023 8.954 0.14 67318. 0.2406 19.22 0.5638 0.7214 0.0459 0.0359 0.044 1.375 0.614 32.527 0.155 2.731 8.562 0.15 67500. 0.2187 20.18 0.5919 0.7210 0.0409 0.0336 0.041 1.287 0.547 30.443 0.145 2.433 8.150 0.15 67689. 0.1965 21.14 0.6201 0.7141 0.0358 0.0311 0.038 1.191 0.479 28.188 0.135 2.130 7.705 0.15 67885. 0.1738 22.10 0.6483 0.6989 0.0306 0.0284 0.035 1.089 0.410 25.770 0.123 1.823 7.213 0.15 68088. 0.1505 23.06 0.6765 0.6727 0.0254 0.0256 0.031 0.981 0.340 23.203 0.111 1.514 6.654 0.15 68298. 0.1265 24.02 0.7047 0.6310 0.0202 0.0226 0.027 0.866 0.271 20.499 0.098 1.204 5.991 0.15 68516. 0.1016 24.98 0.7329 0.5663 0.0151 0.0195 0.024 0.747 0.201 17.674 0.084 0.896 5.170 0.15 68741. 0.0756 25.95 0.7611 0.4648 0.0099 0.0163 0.020 0.623 0.133 14.748 0.070 0.591 4.086 0.15 68973. 0.0486 26.91 0.7893 0.2981 0.0049 0.0129 0.016 0.496 0.065 11.742 0.056 0.291 2.528 0.15 69212. 0.0211 27.87 0.8174 -0.0023 0.0000 0.0096 0.012 0.367 0.000 8.680 0.041 -0.002 -0.019 0.15 69457. 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 0.1057 0.0403 0.166 3.477 3.183 123.424 0.393 14.159 11.698 0.21 97846. 0.6804 1.44 0.0282 0.0719 0.1045 0.0411 0.169 3.543 3.147 125.770 0.400 13.999 11.350 0.21 97924. 0.6564 2.89 0.0565 0.1393 0.1032 0.0418 0.172 3.609 3.108 128.088 0.408 13.822 11.004 0.21 98009. 0.6323 4.33 0.0847 0.2025 0.1017 0.0426 0.175 3.672 3.063 130.335 0.415 13.626 10.661 0.21 98103. 0.6083 5.78 0.1130 0.2614 0.1001 0.0433 0.178 3.732 3.015 132.466 0.422 13.410 10.323 0.21 98205. 0.5843 7.22 0.1412 0.3163 0.0984 0.0439 0.180 3.787 2.961 134.431 0.428 13.171 9.991 0.21 98317. 0.5605 8.66 0.1694 0.3672 0.0964 0.0445 0.183 3.837 2.902 136.176 0.433 12.909 9.667 0.21 98439. 0.5368 10.11 0.1977 0.4144 0.0942 0.0450 0.185 3.878 2.838 137.644 0.438 12.621 9.350 0.21 98570. 0.5134 11.55 0.2259 0.4580 0.0919 0.0453 0.186 3.910 2.767 138.773 0.442 12.306 9.043 0.21 98712. 0.4903 13.00 0.2542 0.4982 0.0893 0.0456 0.187 3.930 2.689 139.501 0.444 11.963 8.744 0.21 98864. 0.4675 14.44 0.2824 0.5353 0.0865 0.0457 0.187 3.938 2.605 139.767 0.445 11.589 8.455 0.22 99026. 0.4449 15.89 0.3106 0.5693 0.0835 0.0456 0.187 3.931 2.515 139.509 0.444 11.185 8.175 0.22 99200. 0.4226 17.33 0.3389 0.6005 0.0803 0.0453 0.186 3.907 2.416 138.671 0.441 10.748 7.904 0.22 99384. 0.4005 18.77 0.3671 0.6288 0.0768 0.0448 0.184 3.865 2.311 137.199 0.437 10.280 7.641 0.22 99580. 0.3786 20.22 0.3954 0.6545 0.0730 0.0441 0.181 3.805 2.199 135.051 0.430 9.780 7.384 0.22 99787. 0.3569 21.66 0.4236 0.6774 0.0690 0.0432 0.177 3.724 2.079 132.187 0.421 9.247 7.134 0.22 100004. 0.3353 23.11 0.4518 0.6976 0.0648 0.0420 0.172 3.622 1.952 128.561 0.409 8.683 6.887 0.22 100233. 0.3137 24.55 0.4801 0.7149 0.0604 0.0406 0.167 3.498 1.818 124.159 0.395 8.088 6.642 0.22 100473. 0.2920 25.99 0.5083 0.7290 0.0558 0.0389 0.160 3.353 1.679 119.013 0.379 7.467 6.398 0.22 100725. 0.2702 27.44 0.5366 0.7397 0.0510 0.0370 0.152 3.188 1.534 113.162 0.360 6.824 6.150 0.22 100987. 0.2483 28.88 0.5648 0.7463 0.0460 0.0348 0.143 3.005 1.386 106.641 0.339 6.164 5.894 0.22 101260. 0.2262 30.33 0.5930 0.7481 0.0410 0.0325 0.133 2.803 1.234 99.483 0.317 5.490 5.627 0.22 101544. 0.2038 31.77 0.6213 0.7439 0.0359 0.0300 0.123 2.584 1.080 91.722 0.292 4.804 5.341 0.22 101839. 0.1810 33.21 0.6495 0.7320 0.0307 0.0272 0.112 2.349 0.924 83.392 0.265 4.111 5.027 0.22 102145. 0.1575 34.66 0.6778 0.7095 0.0255 0.0243 0.100 2.100 0.767 74.534 0.237 3.413 4.670 0.22 102462. 0.1333 36.10 0.7060 0.6720 0.0203 0.0213 0.087 1.837 0.610 65.194 0.208 2.715 4.246 0.22 102789. 0.1081 37.55 0.7342 0.6114 0.0151 0.0181 0.074 1.562 0.454 55.430 0.176 2.019 3.715 0.22 103128. 0.0816 38.99 0.7625 0.5122 0.0099 0.0148 0.061 1.277 0.299 45.308 0.144 1.331 2.996 0.22 103477. 0.0534 40.43 0.7907 0.3396 0.0049 0.0114 0.047 0.984 0.147 34.909 0.111 0.656 1.916 0.22 103837. 0.0240 41.88 0.8190 -0.0021 0.0000 0.0079 0.033 0.685 -0.001 24.309 0.077 -0.003 -0.011 0.22 104205. 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 0.1061 0.0397 0.386 6.088 5.682 288.098 0.688 25.272 8.945 0.29 130458. 0.6951 1.93 0.0283 0.0733 0.1050 0.0405 0.394 6.208 5.618 293.786 0.701 24.991 8.674 0.29 130561. 0.6702 3.85 0.0565 0.1420 0.1037 0.0413 0.402 6.327 5.548 299.412 0.715 24.678 8.405 0.29 130675. 0.6453 5.78 0.0848 0.2063 0.1022 0.0420 0.409 6.442 5.470 304.874 0.728 24.332 8.138 0.29 130801. 0.6205 7.71 0.1131 0.2662 0.1006 0.0427 0.416 6.552 5.384 310.063 0.740 23.949 7.876 0.29 130938. 0.5958 9.64 0.1413 0.3219 0.0988 0.0434 0.422 6.653 5.289 314.860 0.752 23.526 7.619 0.29 131087. 0.5712 11.56 0.1696 0.3736 0.0969 0.0440 0.428 6.743 5.185 319.133 0.762 23.061 7.369 0.29 131249. 0.5469 13.49 0.1979 0.4214 0.0947 0.0445 0.433 6.820 5.070 322.744 0.770 22.549 7.125 0.29 131425. 0.5229 15.42 0.2261 0.4656 0.0924 0.0449 0.437 6.879 4.944 325.546 0.777 21.989 6.888 0.29 131614. 0.4992 17.35 0.2544 0.5064 0.0898 0.0451 0.439 6.918 4.806 327.387 0.782 21.378 6.658 0.29 131817. 0.4758 19.27 0.2827 0.5439 0.0870 0.0452 0.440 6.933 4.656 328.118 0.783 20.712 6.437 0.29 132035. 0.4528 21.20 0.3110 0.5784 0.0840 0.0451 0.439 6.922 4.494 327.590 0.782 19.991 6.223 0.29 132267. 0.4300 23.13 0.3392 0.6100 0.0807 0.0449 0.437 6.881 4.319 325.664 0.777 19.212 6.016 0.29 132513. 0.4076 25.06 0.3675 0.6388 0.0772 0.0444 0.432 6.809 4.131 322.215 0.769 18.376 5.815 0.29 132775. 0.3853 26.98 0.3958 0.6650 0.0734 0.0437 0.425 6.701 3.930 317.133 0.757 17.482 5.621 0.29 133051. 0.3633 28.91 0.4240 0.6884 0.0694 0.0428 0.416 6.557 3.716 310.321 0.741 16.530 5.432 0.29 133342. 0.3413 30.84 0.4523 0.7093 0.0652 0.0416 0.405 6.375 3.489 301.673 0.720 15.520 5.246 0.29 133648. 0.3195 32.77 0.4806 0.7273 0.0607 0.0401 0.390 6.152 3.250 291.146 0.695 14.456 5.063 0.29 133969. 0.2975 34.69 0.5088 0.7423 0.0561 0.0384 0.374 5.892 3.000 278.815 0.666 13.345 4.881 0.29 134305. 0.2756 36.62 0.5371 0.7541 0.0512 0.0365 0.355 5.595 2.742 264.772 0.632 12.196 4.697 0.29 134655. 0.2535 38.55 0.5654 0.7620 0.0463 0.0343 0.334 5.264 2.476 249.101 0.595 11.015 4.509 0.29 135020. 0.2313 40.48 0.5936 0.7654 0.0412 0.0320 0.311 4.900 2.205 231.879 0.554 9.809 4.314 0.29 135400. 0.2088 42.40 0.6219 0.7632 0.0360 0.0294 0.286 4.505 1.930 213.184 0.509 8.583 4.105 0.29 135794. 0.1859 44.33 0.6502 0.7536 0.0308 0.0266 0.259 4.080 1.651 193.103 0.461 7.343 3.877 0.29 136202. 0.1624 46.26 0.6784 0.7339 0.0256 0.0237 0.230 3.629 1.370 171.733 0.410 6.095 3.619 0.29 136626. 0.1381 48.18 0.7067 0.6997 0.0204 0.0206 0.200 3.152 1.090 149.188 0.356 4.846 3.312 0.29 137064. 0.1127 50.11 0.7350 0.6427 0.0151 0.0173 0.168 2.654 0.810 125.607 0.300 3.603 2.925 0.29 137516. 0.0858 52.04 0.7632 0.5461 0.0100 0.0139 0.136 2.137 0.534 101.156 0.241 2.375 2.394 0.29 137983. 0.0570 53.97 0.7915 0.3709 0.0049 0.0105 0.102 1.607 0.263 76.031 0.182 1.169 1.568 0.29 138463. 0.0262 55.89 0.8198 -0.0034 0.0000 0.0069 0.068 1.065 -0.002 50.413 0.120 -0.007 -0.014 0.30 138954. 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 0.1067 0.0394 0.749 9.444 8.921 558.654 1.067 39.680 7.243 0.36 163066. 0.7052 2.41 0.0283 0.0742 0.1055 0.0402 0.764 9.635 8.823 569.982 1.089 39.245 7.021 0.36 163195. 0.6798 4.82 0.0565 0.1437 0.1042 0.0410 0.779 9.825 8.714 581.198 1.110 38.762 6.801 0.36 163338. 0.6544 7.23 0.0848 0.2086 0.1028 0.0418 0.794 10.009 8.594 592.101 1.131 38.226 6.583 0.36 163495. 0.6291 9.64 0.1131 0.2691 0.1012 0.0425 0.808 10.185 8.460 602.475 1.151 37.632 6.369 0.36 163666. 0.6039 12.05 0.1414 0.3254 0.0994 0.0432 0.821 10.347 8.313 612.081 1.169 36.975 6.160 0.36 163853. 0.5789 14.46 0.1696 0.3775 0.0974 0.0438 0.832 10.492 8.150 620.660 1.185 36.250 5.956 0.36 164056. 0.5542 16.87 0.1979 0.4257 0.0953 0.0443 0.842 10.615 7.971 627.934 1.199 35.453 5.757 0.36 164276. 0.5299 19.28 0.2262 0.4703 0.0930 0.0447 0.850 10.711 7.774 633.612 1.210 34.579 5.565 0.36 164513. 0.5058 21.69 0.2545 0.5114 0.0904 0.0450 0.855 10.775 7.559 637.395 1.217 33.623 5.379 0.36 164767. 0.4821 24.10 0.2827 0.5493 0.0876 0.0451 0.857 10.802 7.325 638.981 1.220 32.582 5.200 0.36 165039. 0.4587 26.51 0.3110 0.5841 0.0845 0.0450 0.856 10.786 7.071 638.076 1.219 31.453 5.027 0.36 165330. 0.4357 28.92 0.3393 0.6160 0.0813 0.0448 0.851 10.724 6.797 634.402 1.212 30.233 4.860 0.36 165639. 0.4130 31.33 0.3676 0.6452 0.0777 0.0443 0.842 10.611 6.502 627.707 1.199 28.921 4.698 0.36 165966. 0.3905 33.74 0.3958 0.6717 0.0740 0.0436 0.828 10.443 6.186 617.774 1.180 27.517 4.542 0.36 166312. 0.3683 36.14 0.4241 0.6957 0.0700 0.0426 0.811 10.217 5.850 604.407 1.154 26.023 4.390 0.36 166676. 0.3462 38.55 0.4524 0.7170 0.0657 0.0414 0.788 9.930 5.494 587.395 1.122 24.436 4.242 0.36 167059. 0.3241 40.96 0.4806 0.7356 0.0612 0.0400 0.760 9.579 5.118 566.646 1.082 22.763 4.096 0.36 167460. 0.3021 43.37 0.5089 0.7514 0.0565 0.0383 0.727 9.167 4.725 542.302 1.036 21.016 3.952 0.36 167880. 0.2800 45.78 0.5372 0.7640 0.0516 0.0363 0.690 8.698 4.318 514.544 0.983 19.208 3.807 0.36 168319. 0.2579 48.19 0.5655 0.7730 0.0466 0.0341 0.648 8.174 3.901 483.534 0.923 17.350 3.659 0.36 168775. 0.2356 50.60 0.5937 0.7777 0.0415 0.0317 0.603 7.597 3.474 449.426 0.858 15.451 3.506 0.36 169250. 0.2130 53.01 0.6220 0.7770 0.0363 0.0291 0.553 6.971 3.040 412.374 0.788 13.521 3.343 0.36 169743. 0.1900 55.42 0.6503 0.7694 0.0311 0.0263 0.500 6.298 2.601 372.547 0.712 11.569 3.167 0.36 170255. 0.1665 57.83 0.6786 0.7522 0.0258 0.0233 0.443 5.581 2.159 330.140 0.631 9.605 2.967 0.37 170784. 0.1421 60.24 0.7068 0.7209 0.0205 0.0201 0.383 4.824 1.717 285.382 0.545 7.639 2.730 0.37 171332. 0.1166 62.65 0.7351 0.6672 0.0153 0.0168 0.320 4.033 1.278 238.551 0.456 5.683 2.429 0.37 171897. 0.0895 65.06 0.7634 0.5740 0.0101 0.0134 0.255 3.212 0.843 189.980 0.363 3.749 2.012 0.37 172481. 0.0602 67.47 0.7917 0.3987 0.0050 0.0099 0.188 2.368 0.416 140.062 0.267 1.851 1.348 0.37 173082. 0.0284 69.88 0.8199 0.0006 0.0000 0.0063 0.120 1.507 0.000 89.156 0.170 0.002 0.002 0.37 173695. 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 0.1073 0.0394 1.292 13.577 12.921 963.776 1.534 57.473 6.081 0.43 195669. 0.7125 2.89 0.0283 0.0747 0.1061 0.0402 1.319 13.858 12.783 983.747 1.566 56.857 5.894 0.43 195824. 0.6869 5.79 0.0566 0.1448 0.1049 0.0410 1.346 14.137 12.628 1003.540 1.597 56.170 5.708 0.43 195996. 0.6612 8.68 0.0849 0.2102 0.1034 0.0418 1.372 14.408 12.457 1022.805 1.628 55.407 5.524 0.43 196184. 0.6355 11.57 0.1131 0.2711 0.1018 0.0425 1.396 14.667 12.266 1041.157 1.657 54.559 5.344 0.43 196390. 0.6101 14.46 0.1414 0.3276 0.1001 0.0432 1.419 14.907 12.055 1058.173 1.684 53.620 5.167 0.43 196615. 0.5848 17.36 0.1697 0.3801 0.0982 0.0438 1.439 15.121 11.821 1073.398 1.708 52.582 4.995 0.43 196859. 0.5599 20.25 0.1980 0.4286 0.0960 0.0444 1.457 15.303 11.564 1086.340 1.729 51.438 4.828 0.43 197124. 0.5352 23.14 0.2263 0.4734 0.0937 0.0448 1.470 15.446 11.282 1096.488 1.745 50.180 4.667 0.43 197408. 0.5110 26.03 0.2546 0.5148 0.0911 0.0450 1.480 15.542 10.972 1103.312 1.756 48.804 4.511 0.43 197714. 0.4870 28.93 0.2828 0.5529 0.0883 0.0452 1.484 15.584 10.634 1106.279 1.761 47.302 4.360 0.43 198042. 0.4635 31.82 0.3111 0.5880 0.0853 0.0451 1.482 15.564 10.268 1104.870 1.758 45.671 4.215 0.43 198391. 0.4403 34.71 0.3394 0.6202 0.0820 0.0449 1.473 15.476 9.871 1098.593 1.748 43.906 4.075 0.43 198762. 0.4174 37.60 0.3677 0.6497 0.0784 0.0444 1.458 15.313 9.444 1087.003 1.730 42.008 3.941 0.43 199156. 0.3948 40.50 0.3960 0.6765 0.0746 0.0437 1.435 15.069 8.987 1069.716 1.703 39.974 3.811 0.43 199572. 0.3724 43.39 0.4243 0.7008 0.0706 0.0427 1.403 14.741 8.500 1046.387 1.665 37.807 3.684 0.43 200010. 0.3501 46.28 0.4525 0.7226 0.0663 0.0415 1.363 14.322 7.982 1016.644 1.618 35.505 3.561 0.43 200470. 0.3280 49.18 0.4808 0.7417 0.0617 0.0400 1.315 13.810 7.436 980.318 1.560 33.076 3.441 0.43 200953. 0.3058 52.07 0.5091 0.7581 0.0570 0.0383 1.257 13.209 6.866 937.648 1.492 30.539 3.321 0.43 201458. 0.2837 54.96 0.5374 0.7714 0.0521 0.0363 1.192 12.523 6.275 888.947 1.415 27.912 3.202 0.43 201984. 0.2614 57.85 0.5657 0.7813 0.0471 0.0341 1.119 11.756 5.668 834.502 1.328 25.210 3.081 0.44 202533. 0.2391 60.75 0.5940 0.7871 0.0419 0.0316 1.039 10.912 5.047 774.579 1.233 22.450 2.955 0.44 203104. 0.2164 63.64 0.6222 0.7877 0.0367 0.0290 0.951 9.994 4.416 709.454 1.129 19.643 2.823 0.44 203696. 0.1934 66.53 0.6505 0.7816 0.0314 0.0261 0.857 9.008 3.778 639.422 1.018 16.804 2.680 0.44 204310. 0.1698 69.42 0.6788 0.7663 0.0260 0.0231 0.757 7.957 3.135 564.828 0.899 13.946 2.518 0.44 204946. 0.1453 72.32 0.7071 0.7373 0.0207 0.0198 0.652 6.847 2.492 486.078 0.774 11.086 2.326 0.44 205604. 0.1197 75.21 0.7354 0.6863 0.0154 0.0165 0.541 5.686 1.853 403.665 0.642 8.240 2.082 0.44 206283. 0.0924 78.10 0.7637 0.5955 0.0101 0.0130 0.427 4.482 1.220 318.181 0.506 5.427 1.739 0.44 206984. 0.0626 80.99 0.7919 0.4193 0.0050 0.0094 0.309 3.245 0.600 230.329 0.367 2.667 1.181 0.44 207706. 0.0298 83.89 0.8202 -0.0063 0.0000 0.0057 0.189 1.982 -0.005 140.722 0.224 -0.023 -0.017 0.44 208442. 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 0.1080 0.0395 2.058 18.530 17.709 1534.644 2.094 78.770 5.234 0.50 228266. 0.7180 3.37 0.0283 0.0750 0.1069 0.0403 2.101 18.921 17.524 1567.045 2.138 77.949 5.072 0.50 228448. 0.6922 6.75 0.0566 0.1453 0.1056 0.0411 2.145 19.310 17.318 1599.198 2.182 77.031 4.912 0.50 228648. 0.6663 10.12 0.0848 0.2110 0.1042 0.0419 2.187 19.688 17.088 1630.521 2.224 76.008 4.753 0.50 228868. 0.6405 13.50 0.1131 0.2721 0.1027 0.0427 2.227 20.049 16.832 1660.399 2.265 74.869 4.598 0.50 229109. 0.6149 16.87 0.1414 0.3289 0.1009 0.0434 2.264 20.384 16.547 1688.144 2.303 73.603 4.446 0.50 229372. 0.5896 20.25 0.1697 0.3815 0.0990 0.0440 2.297 20.684 16.232 1713.012 2.337 72.201 4.298 0.50 229657. 0.5645 23.62 0.1980 0.4302 0.0969 0.0446 2.326 20.940 15.884 1734.204 2.366 70.651 4.154 0.50 229966. 0.5397 27.00 0.2263 0.4752 0.0946 0.0450 2.348 21.141 15.500 1750.890 2.389 68.944 4.015 0.50 230299. 0.5153 30.37 0.2545 0.5168 0.0920 0.0453 2.363 21.278 15.079 1762.206 2.404 67.072 3.881 0.50 230656. 0.4913 33.75 0.2828 0.5551 0.0892 0.0454 2.370 21.339 14.619 1767.289 2.411 65.026 3.752 0.50 231039. 0.4676 37.12 0.3111 0.5903 0.0861 0.0454 2.367 21.315 14.119 1765.294 2.408 62.800 3.628 0.50 231447. 0.4443 40.50 0.3394 0.6228 0.0828 0.0451 2.354 21.196 13.577 1755.422 2.395 60.390 3.508 0.50 231881. 0.4214 43.87 0.3677 0.6525 0.0793 0.0447 2.329 20.973 12.993 1736.952 2.370 57.791 3.393 0.50 232341. 0.3987 47.24 0.3960 0.6797 0.0754 0.0439 2.292 20.639 12.366 1709.253 2.332 55.006 3.282 0.50 232826. 0.3762 50.62 0.4242 0.7043 0.0714 0.0430 2.242 20.186 11.698 1671.772 2.281 52.034 3.174 0.50 233338. 0.3539 53.99 0.4525 0.7265 0.0670 0.0418 2.178 19.608 10.988 1623.913 2.215 48.875 3.069 0.50 233876. 0.3316 57.37 0.4808 0.7461 0.0625 0.0402 2.099 18.901 10.238 1565.379 2.135 45.539 2.966 0.51 234440. 0.3094 60.74 0.5091 0.7630 0.0577 0.0385 2.007 18.070 9.454 1496.543 2.042 42.051 2.865 0.51 235029. 0.2872 64.12 0.5374 0.7770 0.0527 0.0365 1.901 17.121 8.642 1417.910 1.934 38.438 2.764 0.51 235645. 0.2649 67.49 0.5656 0.7877 0.0476 0.0342 1.783 16.059 7.806 1329.941 1.814 34.721 2.662 0.51 236285. 0.2425 70.87 0.5939 0.7944 0.0424 0.0317 1.654 14.889 6.952 1233.072 1.682 30.920 2.557 0.51 236952. 0.2198 74.24 0.6222 0.7962 0.0371 0.0290 1.512 13.617 6.082 1127.744 1.538 27.055 2.446 0.51 237643. 0.1967 77.62 0.6505 0.7916 0.0317 0.0261 1.360 12.249 5.203 1014.442 1.384 23.144 2.326 0.51 238360. 0.1730 80.99 0.6788 0.7781 0.0263 0.0230 1.199 10.791 4.318 893.723 1.219 19.206 2.191 0.51 239102. 0.1484 84.36 0.7071 0.7513 0.0209 0.0197 1.028 9.252 3.432 766.249 1.045 15.264 2.031 0.51 239870. 0.1227 87.74 0.7353 0.7029 0.0156 0.0163 0.849 7.641 2.550 632.823 0.863 11.341 1.827 0.51 240663. 0.0951 91.11 0.7636 0.6148 0.0102 0.0127 0.663 5.970 1.678 494.412 0.674 7.462 1.539 0.51 241480. 0.0650 94.49 0.7919 0.4387 0.0050 0.0091 0.472 4.252 0.822 352.167 0.480 3.657 1.059 0.52 242323. 0.0313 97.86 0.8202 -0.0111 -0.0001 0.0053 0.278 2.500 -0.012 207.058 0.282 -0.053 -0.026 0.52 243179. 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 0.1089 0.0397 3.092 24.362 23.318 2305.884 2.752 103.717 4.587 0.57 260857. 0.7220 3.85 0.0283 0.0751 0.1078 0.0406 3.159 24.886 23.083 2355.399 2.812 102.675 4.445 0.57 261064. 0.6962 7.71 0.0565 0.1454 0.1066 0.0414 3.225 25.405 22.821 2404.604 2.870 101.506 4.305 0.57 261293. 0.6703 11.56 0.0848 0.2111 0.1052 0.0422 3.289 25.913 22.527 2452.605 2.928 100.199 4.166 0.57 261544. 0.6446 15.41 0.1130 0.2723 0.1037 0.0430 3.350 26.397 22.198 2498.460 2.982 98.738 4.030 0.57 261819. 0.6189 19.26 0.1413 0.3291 0.1020 0.0438 3.408 26.848 21.832 2541.115 3.033 97.110 3.897 0.57 262120. 0.5936 23.12 0.1695 0.3818 0.1001 0.0444 3.459 27.252 21.425 2579.427 3.079 95.299 3.767 0.57 262446. 0.5685 26.97 0.1978 0.4306 0.0980 0.0450 3.503 27.598 20.974 2612.175 3.118 93.292 3.642 0.57 262799. 0.5437 30.82 0.2260 0.4757 0.0956 0.0454 3.538 27.872 20.476 2638.079 3.149 91.077 3.520 0.57 263179. 0.5193 34.68 0.2543 0.5174 0.0931 0.0457 3.562 28.060 19.928 2655.827 3.170 88.640 3.403 0.57 263588. 0.4953 38.53 0.2825 0.5558 0.0903 0.0459 3.573 28.147 19.328 2664.095 3.180 85.971 3.291 0.57 264026. 0.4716 42.38 0.3108 0.5913 0.0872 0.0458 3.569 28.121 18.674 2661.598 3.177 83.061 3.182 0.57 264493. 0.4483 46.23 0.3390 0.6239 0.0839 0.0456 3.550 27.967 17.964 2647.105 3.160 79.903 3.078 0.57 264989. 0.4253 50.09 0.3673 0.6539 0.0803 0.0451 3.513 27.676 17.198 2619.514 3.127 76.495 2.978 0.58 265515. 0.4025 53.94 0.3956 0.6813 0.0765 0.0444 3.457 27.236 16.375 2577.864 3.077 72.836 2.881 0.58 266070. 0.3801 57.79 0.4238 0.7063 0.0724 0.0434 3.381 26.638 15.496 2521.315 3.010 68.927 2.788 0.58 266655. 0.3577 61.65 0.4521 0.7288 0.0680 0.0422 3.284 25.874 14.561 2448.978 2.923 64.768 2.697 0.58 267270. 0.3355 65.50 0.4803 0.7489 0.0634 0.0407 3.165 24.938 13.573 2360.350 2.817 60.371 2.608 0.58 267914. 0.3132 69.35 0.5086 0.7664 0.0586 0.0389 3.025 23.835 12.538 2255.966 2.693 55.768 2.521 0.58 268587. 0.2910 73.20 0.5368 0.7811 0.0535 0.0368 2.865 22.574 11.465 2136.593 2.550 50.996 2.434 0.58 269290. 0.2686 77.06 0.5651 0.7926 0.0484 0.0345 2.686 21.162 10.360 2002.941 2.391 46.083 2.346 0.58 270022. 0.2462 80.91 0.5933 0.8002 0.0431 0.0320 2.489 19.606 9.230 1855.675 2.215 41.056 2.256 0.58 270783. 0.2234 84.76 0.6216 0.8032 0.0377 0.0292 2.274 17.913 8.080 1695.473 2.024 35.940 2.162 0.58 271572. 0.2003 88.62 0.6498 0.8001 0.0323 0.0262 2.042 16.092 6.916 1523.066 1.818 30.761 2.059 0.58 272391. 0.1766 92.47 0.6781 0.7884 0.0268 0.0231 1.796 14.150 5.743 1339.306 1.599 25.545 1.945 0.58 273238. 0.1519 96.32 0.7064 0.7640 0.0213 0.0197 1.536 12.099 4.568 1145.205 1.367 20.320 1.809 0.59 274114. 0.1261 100.17 0.7346 0.7187 0.0159 0.0162 1.263 9.952 3.399 941.983 1.124 15.118 1.637 0.59 275019. 0.0984 104.03 0.7629 0.6344 0.0105 0.0126 0.980 7.725 2.242 731.122 0.873 9.973 1.391 0.59 275952. 0.0679 107.88 0.7911 0.4617 0.0052 0.0089 0.690 5.435 1.107 514.391 0.614 4.925 0.976 0.59 276913. 0.0335 111.73 0.8194 0.0003 0.0000 0.0051 0.393 3.099 0.000 293.312 0.350 0.002 0.001 0.59 277891. 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 0.1099 0.0401 4.448 31.151 29.787 3317.031 3.519 132.495 4.073 0.64 293438. 0.7247 4.33 0.0282 0.0750 0.1089 0.0410 4.545 31.832 29.502 3389.516 3.596 131.226 3.948 0.64 293671. 0.6990 8.66 0.0565 0.1452 0.1077 0.0419 4.642 32.510 29.181 3461.681 3.673 129.796 3.823 0.64 293928. 0.6733 13.00 0.0847 0.2108 0.1064 0.0427 4.737 33.172 28.819 3532.211 3.748 128.189 3.701 0.64 294211. 0.6476 17.33 0.1130 0.2720 0.1049 0.0435 4.827 33.806 28.414 3599.703 3.819 126.384 3.580 0.64 294521. 0.6221 21.66 0.1412 0.3288 0.1032 0.0443 4.912 34.397 27.959 3662.606 3.886 124.363 3.462 0.64 294859. 0.5968 25.99 0.1694 0.3815 0.1013 0.0450 4.988 34.929 27.452 3719.230 3.946 122.105 3.348 0.64 295226. 0.5718 30.32 0.1977 0.4303 0.0992 0.0456 5.053 35.385 26.887 3767.770 3.998 119.594 3.237 0.64 295624. 0.5471 34.66 0.2259 0.4755 0.0969 0.0460 5.104 35.747 26.261 3806.350 4.039 116.810 3.129 0.64 296053. 0.5228 38.99 0.2542 0.5172 0.0944 0.0464 5.140 35.997 25.571 3833.032 4.067 113.738 3.026 0.64 296514. 0.4988 43.32 0.2824 0.5557 0.0916 0.0465 5.157 36.118 24.812 3845.878 4.081 110.364 2.926 0.65 297007. 0.4752 47.65 0.3106 0.5913 0.0885 0.0465 5.154 36.091 23.983 3842.993 4.078 106.675 2.831 0.65 297533. 0.4519 51.99 0.3389 0.6241 0.0852 0.0462 5.126 35.899 23.081 3822.585 4.056 102.664 2.739 0.65 298092. 0.4289 56.32 0.3671 0.6544 0.0816 0.0458 5.073 35.528 22.105 3783.036 4.014 98.324 2.650 0.65 298685. 0.4062 60.65 0.3953 0.6821 0.0777 0.0450 4.993 34.964 21.056 3722.937 3.950 93.657 2.565 0.65 299310. 0.3837 64.98 0.4236 0.7074 0.0736 0.0440 4.883 34.195 19.933 3641.068 3.863 88.663 2.483 0.65 299970. 0.3614 69.31 0.4518 0.7303 0.0691 0.0428 4.742 33.209 18.737 3536.167 3.752 83.343 2.403 0.65 300662. 0.3391 73.65 0.4801 0.7508 0.0645 0.0412 4.569 32.001 17.471 3407.443 3.615 77.710 2.326 0.65 301387. 0.3169 77.98 0.5083 0.7689 0.0596 0.0394 4.366 30.575 16.144 3255.628 3.454 71.807 2.249 0.65 302146. 0.2946 82.31 0.5365 0.7842 0.0545 0.0373 4.133 28.943 14.766 3081.848 3.270 65.679 2.173 0.65 302937. 0.2722 86.64 0.5648 0.7964 0.0493 0.0349 3.872 27.114 13.346 2887.154 3.063 59.365 2.097 0.65 303761. 0.2497 90.97 0.5930 0.8050 0.0439 0.0323 3.584 25.099 11.893 2672.520 2.836 52.899 2.018 0.65 304617. 0.2269 95.31 0.6213 0.8091 0.0384 0.0295 3.271 22.905 10.412 2438.940 2.588 46.315 1.936 0.66 305505. 0.2037 99.64 0.6495 0.8072 0.0329 0.0265 2.933 20.544 8.913 2187.494 2.321 39.644 1.848 0.66 306426. 0.1799 103.97 0.6777 0.7972 0.0273 0.0232 2.574 18.026 7.402 1919.424 2.037 32.922 1.749 0.66 307379. 0.1551 108.30 0.7060 0.7748 0.0217 0.0198 2.194 15.366 5.887 1636.209 1.736 26.186 1.632 0.66 308364. 0.1291 112.64 0.7342 0.7320 0.0162 0.0162 1.796 12.581 4.378 1339.643 1.421 19.475 1.482 0.66 309381. 0.1011 116.97 0.7625 0.6505 0.0107 0.0125 1.384 9.691 2.886 1031.906 1.095 12.837 1.269 0.66 310430. 0.0702 121.30 0.7907 0.4789 0.0052 0.0087 0.960 6.721 1.421 715.625 0.759 6.321 0.901 0.66 311511. 0.0350 125.63 0.8189 -0.0050 0.0000 0.0048 0.527 3.691 -0.008 393.056 0.417 -0.035 -0.009 0.66 312608. 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 0.1111 0.0409 6.223 39.224 37.165 4640.678 4.432 165.309 3.632 0.71 326008. 0.7219 4.81 0.0282 0.0743 0.1101 0.0418 6.355 40.056 36.831 4739.123 4.526 163.826 3.525 0.71 326267. 0.6974 9.62 0.0564 0.1441 0.1090 0.0427 6.487 40.888 36.453 4837.547 4.620 162.144 3.418 0.71 326552. 0.6727 14.43 0.0846 0.2094 0.1077 0.0435 6.617 41.705 36.025 4934.165 4.712 160.241 3.312 0.71 326866. 0.6479 19.23 0.1128 0.2704 0.1062 0.0443 6.741 42.490 35.542 5027.084 4.801 158.090 3.207 0.71 327211. 0.6232 24.04 0.1411 0.3272 0.1046 0.0451 6.858 43.226 34.997 5114.134 4.884 155.666 3.104 0.71 327586. 0.5986 28.85 0.1693 0.3799 0.1028 0.0458 6.964 43.892 34.385 5192.948 4.959 152.943 3.003 0.72 327995. 0.5741 33.66 0.1975 0.4287 0.1007 0.0464 7.055 44.467 33.700 5260.978 5.024 149.896 2.905 0.72 328437. 0.5498 38.47 0.2257 0.4740 0.0985 0.0469 7.128 44.928 32.936 5315.516 5.076 146.501 2.810 0.72 328914. 0.5258 43.28 0.2539 0.5158 0.0959 0.0472 7.180 45.251 32.090 5353.757 5.112 142.738 2.719 0.72 329427. 0.5020 48.09 0.2821 0.5545 0.0931 0.0474 7.205 45.413 31.157 5372.851 5.131 138.588 2.630 0.72 329976. 0.4786 52.90 0.3103 0.5902 0.0901 0.0474 7.201 45.388 30.134 5369.974 5.128 134.034 2.545 0.72 330561. 0.4554 57.70 0.3385 0.6232 0.0867 0.0471 7.164 45.156 29.017 5342.441 5.102 129.067 2.464 0.72 331183. 0.4326 62.51 0.3667 0.6536 0.0831 0.0466 7.091 44.694 27.806 5287.856 5.050 123.679 2.385 0.72 331842. 0.4100 67.32 0.3950 0.6816 0.0792 0.0459 6.979 43.987 26.499 5204.212 4.970 117.870 2.310 0.72 332538. 0.3876 72.13 0.4232 0.7073 0.0750 0.0449 6.826 43.020 25.099 5089.806 4.860 111.642 2.237 0.72 333272. 0.3653 76.94 0.4514 0.7306 0.0706 0.0436 6.629 41.779 23.605 4942.907 4.720 104.997 2.166 0.72 334042. 0.3431 81.75 0.4796 0.7516 0.0658 0.0420 6.386 40.252 22.021 4762.311 4.548 97.948 2.097 0.72 334848. 0.3208 86.56 0.5078 0.7702 0.0609 0.0401 6.100 38.449 20.357 4548.964 4.344 90.549 2.030 0.72 335692. 0.2985 91.36 0.5360 0.7862 0.0557 0.0380 5.772 36.382 18.628 4304.469 4.110 82.856 1.963 0.72 336571. 0.2762 96.17 0.5642 0.7992 0.0503 0.0355 5.405 34.065 16.844 4030.333 3.849 74.921 1.896 0.73 337486. 0.2536 100.98 0.5924 0.8087 0.0449 0.0329 4.999 31.510 15.015 3727.956 3.560 66.786 1.827 0.73 338437. 0.2308 105.79 0.6206 0.8139 0.0393 0.0300 4.558 28.727 13.151 3398.788 3.246 58.494 1.755 0.73 339424. 0.2075 110.60 0.6488 0.8134 0.0337 0.0268 4.083 25.732 11.261 3044.445 2.907 50.087 1.678 0.73 340447. 0.1835 115.41 0.6771 0.8049 0.0280 0.0235 3.576 22.541 9.354 2666.836 2.547 41.608 1.591 0.73 341504. 0.1586 120.22 0.7053 0.7843 0.0222 0.0200 3.042 19.172 7.442 2268.283 2.166 33.103 1.488 0.73 342598. 0.1323 125.02 0.7335 0.7433 0.0165 0.0163 2.483 15.651 5.536 1851.667 1.768 24.625 1.356 0.73 343726. 0.1040 129.83 0.7617 0.6631 0.0109 0.0125 1.905 12.007 3.649 1420.561 1.357 16.231 1.165 0.73 344890. 0.0725 134.64 0.7899 0.4908 0.0054 0.0086 1.313 8.277 1.795 979.304 0.935 7.985 0.831 0.74 346089. 0.0363 139.45 0.8181 -0.0075 0.0000 0.0047 0.713 4.494 -0.014 531.723 0.508 -0.064 -0.012 0.74 347306. 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 0.1124 0.0434 8.778 50.299 45.484 6546.083 5.683 202.314 3.152 0.79 358565. 0.6929 5.28 0.0282 0.0711 0.1114 0.0442 8.937 51.210 45.112 6664.672 5.786 200.656 3.070 0.79 358848. 0.6722 10.56 0.0563 0.1383 0.1104 0.0449 9.095 52.115 44.686 6782.448 5.888 198.762 2.988 0.79 359161. 0.6512 15.84 0.0845 0.2018 0.1092 0.0457 9.249 52.997 44.200 6897.125 5.988 196.600 2.907 0.79 359506. 0.6299 21.12 0.1126 0.2616 0.1078 0.0464 9.396 53.835 43.646 7006.256 6.082 194.136 2.826 0.79 359884. 0.6085 26.40 0.1408 0.3177 0.1063 0.0471 9.531 54.610 43.016 7107.110 6.170 191.336 2.745 0.79 360296. 0.5869 31.68 0.1690 0.3703 0.1045 0.0477 9.651 55.299 42.303 7196.718 6.248 188.164 2.666 0.79 360745. 0.5653 36.96 0.1971 0.4194 0.1025 0.0482 9.752 55.876 41.499 7271.896 6.313 184.586 2.588 0.79 361232. 0.5435 42.24 0.2253 0.4652 0.1003 0.0486 9.829 56.318 40.596 7329.378 6.363 180.572 2.512 0.79 361757. 0.5218 47.52 0.2534 0.5079 0.0978 0.0488 9.878 56.597 39.589 7365.763 6.394 176.093 2.438 0.79 362321. 0.5000 52.80 0.2816 0.5475 0.0950 0.0489 9.893 56.688 38.472 7377.570 6.405 171.124 2.365 0.79 362925. 0.4782 58.08 0.3098 0.5842 0.0920 0.0488 9.872 56.563 37.240 7361.309 6.390 165.644 2.295 0.79 363569. 0.4565 63.36 0.3379 0.6182 0.0887 0.0485 9.808 56.196 35.890 7313.580 6.349 159.638 2.226 0.79 364254. 0.4347 68.64 0.3661 0.6496 0.0850 0.0479 9.697 55.563 34.420 7231.173 6.278 153.098 2.159 0.79 364980. 0.4129 73.92 0.3942 0.6785 0.0811 0.0471 9.536 54.641 32.829 7111.184 6.173 146.021 2.094 0.79 365746. 0.3911 79.20 0.4224 0.7050 0.0769 0.0461 9.321 53.410 31.118 6950.994 6.034 138.413 2.031 0.79 366553. 0.3692 84.48 0.4506 0.7291 0.0724 0.0447 9.049 51.850 29.289 6747.926 5.858 130.276 1.969 0.79 367400. 0.3473 89.76 0.4787 0.7508 0.0675 0.0431 8.716 49.943 27.343 6499.767 5.643 121.622 1.908 0.79 368287. 0.3252 95.04 0.5069 0.7701 0.0625 0.0411 8.325 47.698 25.296 6207.587 5.389 112.517 1.848 0.80 369214. 0.3030 100.32 0.5350 0.7867 0.0572 0.0389 7.876 45.130 23.164 5873.367 5.099 103.032 1.789 0.80 370181. 0.2806 105.60 0.5632 0.8003 0.0518 0.0364 7.374 42.254 20.960 5499.099 4.774 93.231 1.729 0.80 371187. 0.2580 110.88 0.5913 0.8104 0.0462 0.0337 6.822 39.089 18.698 5087.112 4.416 83.168 1.667 0.80 372232. 0.2350 116.16 0.6195 0.8158 0.0405 0.0307 6.222 35.653 16.389 4639.939 4.028 72.896 1.602 0.80 373316. 0.2114 121.44 0.6477 0.8151 0.0347 0.0276 5.580 31.970 14.044 4160.635 3.612 62.467 1.531 0.80 374439. 0.1870 126.72 0.6758 0.8054 0.0288 0.0242 4.898 28.067 11.676 3652.763 3.171 51.933 1.450 0.80 375600. 0.1615 132.00 0.7040 0.7819 0.0230 0.0207 4.185 23.978 9.297 3120.625 2.709 41.352 1.351 0.80 376800. 0.1343 137.28 0.7321 0.7353 0.0171 0.0170 3.446 19.744 6.921 2569.512 2.231 30.786 1.222 0.81 378038. 0.1048 142.56 0.7603 0.6453 0.0113 0.0133 2.690 15.412 4.566 2005.710 1.741 20.308 1.032 0.81 379315. 0.0719 147.84 0.7885 0.4599 0.0056 0.0095 1.926 11.037 2.247 1436.421 1.247 9.996 0.710 0.81 380630. 0.0347 153.12 0.8166 -0.0067 0.0000 0.0058 1.164 6.669 -0.019 867.914 0.753 -0.084 -0.010 0.81 381967. 0.0000 PROP RPM = 12000 V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM (mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - - 0.00 0.0000 0.0000 0.1136 0.0493 12.956 68.048 54.706 9661.065 7.688 243.334 2.568 0.86 391109. 0.6193 5.76 0.0282 0.0636 0.1127 0.0500 13.130 68.965 54.311 9791.300 7.792 241.575 2.516 0.86 391416. 0.6044 11.53 0.0564 0.1245 0.1118 0.0506 13.299 69.849 53.854 9916.735 7.891 239.542 2.463 0.86 391756. 0.5892 17.29 0.0845 0.1827 0.1107 0.0512 13.456 70.675 53.326 10034.022 7.985 237.195 2.411 0.86 392132. 0.5738 23.05 0.1127 0.2383 0.1094 0.0517 13.597 71.418 52.718 10139.470 8.069 234.488 2.358 0.86 392544. 0.5582 28.82 0.1409 0.2914 0.1080 0.0522 13.718 72.052 52.018 10229.590 8.140 231.374 2.306 0.86 392994. 0.5423 34.58 0.1691 0.3419 0.1063 0.0526 13.813 72.553 51.216 10300.690 8.197 227.808 2.255 0.86 393485. 0.5261 40.34 0.1972 0.3899 0.1044 0.0528 13.878 72.894 50.302 10349.005 8.235 223.744 2.205 0.86 394017. 0.5097 46.11 0.2254 0.4355 0.1023 0.0529 13.907 73.046 49.267 10370.712 8.253 219.138 2.155 0.86 394591. 0.4930 51.87 0.2536 0.4788 0.0998 0.0529 13.896 72.986 48.101 10362.113 8.246 213.953 2.105 0.86 395209. 0.4760 57.63 0.2818 0.5197 0.0971 0.0527 13.839 72.686 46.796 10319.471 8.212 208.151 2.057 0.86 395871. 0.4587 63.40 0.3099 0.5583 0.0941 0.0523 13.731 72.120 45.347 10239.223 8.148 201.703 2.009 0.86 396577. 0.4410 69.16 0.3381 0.5946 0.0908 0.0516 13.568 71.267 43.748 10118.005 8.052 194.589 1.961 0.86 397328. 0.4228 74.92 0.3663 0.6286 0.0872 0.0508 13.347 70.103 41.996 9952.771 7.920 186.796 1.914 0.86 398124. 0.4043 80.69 0.3945 0.6603 0.0832 0.0497 13.063 68.610 40.090 9740.782 7.751 178.322 1.867 0.86 398964. 0.3853 86.45 0.4226 0.6897 0.0790 0.0484 12.712 66.769 38.033 9479.542 7.544 169.172 1.820 0.86 399849. 0.3658 92.21 0.4508 0.7166 0.0744 0.0468 12.292 64.562 35.825 9166.133 7.294 159.351 1.773 0.87 400778. 0.3459 97.97 0.4790 0.7411 0.0695 0.0449 11.798 61.970 33.470 8798.124 7.001 148.874 1.725 0.87 401751. 0.3254 103.74 0.5072 0.7630 0.0643 0.0428 11.234 59.004 30.985 8376.988 6.666 137.821 1.678 0.87 402767. 0.3044 109.50 0.5353 0.7813 0.0589 0.0404 10.610 55.727 28.389 7911.858 6.296 126.275 1.627 0.87 403826. 0.2827 115.26 0.5635 0.7953 0.0533 0.0378 9.933 52.171 25.700 7406.980 5.894 114.315 1.574 0.87 404928. 0.2601 121.03 0.5917 0.8037 0.0476 0.0350 9.209 48.371 22.934 6867.495 5.465 102.009 1.515 0.87 406072. 0.2365 126.79 0.6199 0.8055 0.0417 0.0321 8.439 44.324 20.105 6292.859 5.008 89.427 1.449 0.87 407258. 0.2118 132.55 0.6480 0.7989 0.0358 0.0290 7.623 40.039 17.230 5684.479 4.524 76.638 1.375 0.87 408487. 0.1860 138.32 0.6762 0.7801 0.0297 0.0258 6.772 35.568 14.323 5049.685 4.018 63.707 1.286 0.88 409757. 0.1587 144.08 0.7044 0.7429 0.0237 0.0224 5.896 30.967 11.400 4396.513 3.499 50.709 1.176 0.88 411068. 0.1295 149.84 0.7326 0.6768 0.0176 0.0191 5.007 26.299 8.481 3733.743 2.971 37.725 1.030 0.88 412422. 0.0978 155.61 0.7607 0.5628 0.0116 0.0157 4.119 21.633 5.586 3071.352 2.444 24.848 0.825 0.88 413817. 0.0636 161.37 0.7889 0.3634 0.0057 0.0124 3.245 17.046 2.741 2420.062 1.926 12.190 0.514 0.88 415253. 0.0277 167.13 0.8171 -0.0070 -0.0001 0.0091 2.395 12.580 -0.038 1785.979 1.421 -0.167 -0.010 0.89 416718. 0.0000 PROP RPM = 13000 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 0.1129 0.0568 18.979 92.016 63.851 14152.506 10.396 284.010 2.046 0.93 423724. 0.5330 6.29 0.0284 0.0553 0.1123 0.0576 19.232 93.241 63.484 14341.013 10.534 282.377 2.008 0.93 424051. 0.5215 12.57 0.0567 0.1086 0.1115 0.0583 19.474 94.416 63.053 14521.750 10.667 280.458 1.969 0.93 424414. 0.5098 18.86 0.0851 0.1597 0.1106 0.0590 19.698 95.503 62.545 14688.811 10.790 278.200 1.931 0.93 424816. 0.4979 25.15 0.1135 0.2088 0.1096 0.0596 19.894 96.455 61.948 14835.315 10.897 275.543 1.894 0.93 425258. 0.4859 31.44 0.1419 0.2560 0.1083 0.0600 20.053 97.226 61.246 14953.808 10.984 272.422 1.858 0.93 425742. 0.4739 37.72 0.1702 0.3014 0.1069 0.0604 20.164 97.764 60.425 15036.633 11.045 268.769 1.823 0.93 426272. 0.4619 44.01 0.1986 0.3452 0.1052 0.0605 20.218 98.023 59.468 15076.401 11.075 264.514 1.789 0.93 426848. 0.4497 50.30 0.2270 0.3874 0.1032 0.0605 20.204 97.957 58.362 15066.354 11.067 259.594 1.757 0.93 427472. 0.4375 56.58 0.2554 0.4282 0.1010 0.0602 20.116 97.530 57.092 15000.703 11.019 253.946 1.726 0.93 428145. 0.4252 62.87 0.2837 0.4677 0.0984 0.0597 19.948 96.712 55.647 14874.880 10.927 247.518 1.697 0.93 428868. 0.4126 69.16 0.3121 0.5058 0.0955 0.0590 19.694 95.482 54.017 14685.579 10.787 240.266 1.668 0.93 429641. 0.3997 75.44 0.3405 0.5426 0.0923 0.0579 19.352 93.824 52.194 14430.634 10.600 232.157 1.640 0.93 430464. 0.3863 81.73 0.3688 0.5779 0.0887 0.0566 18.920 91.732 50.174 14108.819 10.364 223.172 1.613 0.93 431337. 0.3724 88.02 0.3972 0.6118 0.0848 0.0551 18.398 89.202 47.955 13719.706 10.078 213.306 1.585 0.94 432260. 0.3579 94.31 0.4256 0.6439 0.0806 0.0532 17.786 86.234 45.541 13263.255 9.743 202.566 1.557 0.94 433233. 0.3426 100.59 0.4540 0.6741 0.0759 0.0511 17.083 82.825 42.931 12738.854 9.357 190.959 1.529 0.94 434254. 0.3265 106.88 0.4823 0.7022 0.0710 0.0488 16.288 78.968 40.132 12145.723 8.922 178.507 1.499 0.94 435324. 0.3095 113.17 0.5107 0.7280 0.0657 0.0461 15.404 74.684 37.164 11486.802 8.438 165.306 1.467 0.94 436442. 0.2916 119.45 0.5391 0.7508 0.0602 0.0432 14.447 70.046 34.055 10773.447 7.914 151.475 1.434 0.94 437607. 0.2727 125.74 0.5674 0.7677 0.0545 0.0403 13.463 65.271 30.823 10039.038 7.374 137.099 1.393 0.94 438819. 0.2520 132.03 0.5958 0.7764 0.0486 0.0373 12.465 60.436 27.489 9295.406 6.828 122.273 1.341 0.94 440077. 0.2293 138.32 0.6242 0.7690 0.0426 0.0345 11.542 55.958 24.063 8606.564 6.322 107.034 1.268 0.95 441380. 0.2028 144.60 0.6526 0.7483 0.0364 0.0317 10.604 51.412 20.580 7907.392 5.808 91.539 1.180 0.95 442730. 0.1746 150.89 0.6809 0.7114 0.0302 0.0289 9.651 46.791 17.063 7196.759 5.286 75.897 1.075 0.95 444125. 0.1448 157.18 0.7093 0.6522 0.0239 0.0260 8.700 42.180 13.539 6487.574 4.766 60.222 0.947 0.95 445565. 0.1135 163.46 0.7377 0.5633 0.0178 0.0233 7.767 37.658 10.038 5792.002 4.255 44.648 0.786 0.95 447051. 0.0812 169.75 0.7661 0.4347 0.0117 0.0206 6.866 33.291 6.594 5120.268 3.761 29.330 0.584 0.96 448582. 0.0489 176.04 0.7944 0.2535 0.0057 0.0180 6.010 29.137 3.246 4481.425 3.292 14.437 0.328 0.96 450161. 0.0193 182.32 0.8228 0.0006 0.0000 0.0155 5.187 25.150 0.006 3868.133 2.841 0.027 0.001 0.96 451802. 0.0000