22x8 (22x8.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 0.0633 0.0223 0.009 0.583 0.473 6.892 0.066 2.103 31.108 0.09 37892. 0.5704 0.39 0.0188 0.0521 0.0620 0.0224 0.009 0.586 0.463 6.934 0.066 2.060 30.298 0.09 37908. 0.5500 0.78 0.0376 0.1014 0.0607 0.0225 0.009 0.589 0.453 6.970 0.067 2.015 29.487 0.09 37926. 0.5294 1.18 0.0565 0.1479 0.0593 0.0226 0.009 0.591 0.442 6.998 0.067 1.968 28.680 0.09 37946. 0.5088 1.57 0.0753 0.1917 0.0578 0.0227 0.009 0.593 0.431 7.017 0.067 1.918 27.875 0.09 37966. 0.4882 1.96 0.0941 0.2327 0.0562 0.0227 0.009 0.594 0.419 7.028 0.067 1.866 27.073 0.09 37988. 0.4677 2.35 0.1129 0.2710 0.0545 0.0227 0.009 0.594 0.407 7.029 0.067 1.811 26.274 0.09 38011. 0.4471 2.74 0.1317 0.3066 0.0528 0.0227 0.009 0.593 0.394 7.018 0.067 1.754 25.478 0.09 38036. 0.4267 3.14 0.1506 0.3395 0.0510 0.0226 0.009 0.591 0.381 6.997 0.067 1.694 24.684 0.09 38062. 0.4063 3.53 0.1694 0.3696 0.0491 0.0225 0.009 0.589 0.367 6.963 0.066 1.631 23.892 0.09 38090. 0.3859 3.92 0.1882 0.3971 0.0472 0.0224 0.009 0.585 0.352 6.916 0.066 1.567 23.100 0.09 38119. 0.3657 4.31 0.2070 0.4218 0.0452 0.0222 0.009 0.579 0.337 6.855 0.065 1.500 22.308 0.09 38150. 0.3455 4.71 0.2259 0.4438 0.0431 0.0219 0.009 0.573 0.322 6.780 0.065 1.430 21.514 0.09 38182. 0.3254 5.10 0.2447 0.4629 0.0409 0.0216 0.009 0.565 0.306 6.689 0.064 1.359 20.715 0.09 38216. 0.3054 5.49 0.2635 0.4792 0.0387 0.0213 0.009 0.556 0.289 6.582 0.063 1.285 19.910 0.09 38252. 0.2854 5.88 0.2823 0.4924 0.0364 0.0209 0.009 0.546 0.272 6.459 0.062 1.210 19.095 0.09 38289. 0.2656 6.27 0.3011 0.5024 0.0341 0.0204 0.008 0.534 0.254 6.319 0.060 1.132 18.267 0.09 38329. 0.2458 6.67 0.3200 0.5091 0.0317 0.0199 0.008 0.521 0.237 6.160 0.059 1.052 17.420 0.09 38370. 0.2260 7.06 0.3388 0.5121 0.0292 0.0193 0.008 0.506 0.218 5.983 0.057 0.971 16.549 0.09 38413. 0.2062 7.45 0.3576 0.5111 0.0267 0.0187 0.008 0.489 0.200 5.788 0.055 0.888 15.647 0.09 38457. 0.1865 7.84 0.3764 0.5055 0.0242 0.0180 0.007 0.471 0.181 5.573 0.053 0.804 14.704 0.09 38504. 0.1667 8.23 0.3952 0.4949 0.0216 0.0173 0.007 0.451 0.161 5.338 0.051 0.718 13.709 0.09 38552. 0.1469 8.63 0.4141 0.4783 0.0190 0.0164 0.007 0.430 0.142 5.084 0.049 0.630 12.646 0.09 38603. 0.1270 9.02 0.4329 0.4545 0.0163 0.0156 0.006 0.406 0.122 4.809 0.046 0.542 11.495 0.09 38655. 0.1070 9.41 0.4517 0.4220 0.0136 0.0146 0.006 0.382 0.102 4.515 0.043 0.453 10.228 0.09 38709. 0.0870 9.80 0.4705 0.3785 0.0109 0.0136 0.006 0.355 0.082 4.200 0.040 0.363 8.807 0.09 38765. 0.0671 10.19 0.4894 0.3208 0.0082 0.0125 0.005 0.327 0.061 3.866 0.037 0.272 7.178 0.09 38823. 0.0473 10.59 0.5082 0.2440 0.0055 0.0114 0.005 0.297 0.041 3.512 0.034 0.181 5.258 0.09 38883. 0.0283 10.98 0.5270 0.1405 0.0027 0.0101 0.004 0.265 0.020 3.139 0.030 0.090 2.919 0.09 38945. 0.0111 11.37 0.5458 -0.0043 -0.0001 0.0089 0.004 0.232 -0.001 2.742 0.026 -0.002 -0.086 0.09 39005. 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 0.0637 0.0197 0.065 2.060 1.902 48.750 0.233 8.460 17.695 0.17 75782. 0.6509 0.79 0.0189 0.0595 0.0624 0.0199 0.066 2.077 1.864 49.142 0.235 8.289 17.201 0.17 75816. 0.6263 1.58 0.0379 0.1156 0.0610 0.0200 0.066 2.091 1.823 49.481 0.236 8.109 16.711 0.17 75852. 0.6018 2.37 0.0568 0.1684 0.0596 0.0201 0.067 2.103 1.780 49.758 0.238 7.918 16.227 0.17 75891. 0.5774 3.16 0.0757 0.2179 0.0581 0.0202 0.067 2.112 1.735 49.967 0.239 7.717 15.749 0.17 75932. 0.5533 3.95 0.0947 0.2642 0.0565 0.0202 0.067 2.117 1.688 50.099 0.239 7.506 15.278 0.17 75977. 0.5293 4.73 0.1136 0.3074 0.0548 0.0203 0.067 2.119 1.638 50.149 0.239 7.285 14.812 0.17 76023. 0.5056 5.52 0.1326 0.3475 0.0531 0.0203 0.067 2.118 1.586 50.109 0.239 7.053 14.353 0.17 76073. 0.4821 6.31 0.1515 0.3846 0.0513 0.0202 0.067 2.112 1.531 49.971 0.239 6.812 13.900 0.17 76126. 0.4588 7.10 0.1704 0.4188 0.0494 0.0201 0.067 2.102 1.475 49.728 0.237 6.560 13.452 0.17 76182. 0.4357 7.89 0.1894 0.4500 0.0474 0.0200 0.066 2.087 1.416 49.375 0.236 6.299 13.009 0.17 76241. 0.4129 8.68 0.2083 0.4783 0.0454 0.0198 0.066 2.067 1.355 48.903 0.233 6.028 12.570 0.17 76303. 0.3903 9.47 0.2272 0.5037 0.0433 0.0195 0.065 2.042 1.292 48.307 0.231 5.748 12.134 0.17 76368. 0.3679 10.26 0.2462 0.5262 0.0411 0.0192 0.064 2.011 1.227 47.581 0.227 5.460 11.701 0.18 76437. 0.3457 11.05 0.2651 0.5457 0.0389 0.0189 0.063 1.974 1.161 46.717 0.223 5.162 11.268 0.18 76510. 0.3238 11.84 0.2841 0.5622 0.0366 0.0185 0.061 1.932 1.092 45.709 0.218 4.857 10.834 0.18 76586. 0.3019 12.62 0.3030 0.5755 0.0342 0.0180 0.060 1.883 1.021 44.554 0.213 4.543 10.398 0.18 76665. 0.2803 13.41 0.3219 0.5854 0.0318 0.0175 0.058 1.828 0.949 43.244 0.206 4.222 9.956 0.18 76748. 0.2587 14.20 0.3409 0.5918 0.0293 0.0169 0.056 1.766 0.875 41.776 0.199 3.894 9.505 0.18 76835. 0.2372 14.99 0.3598 0.5942 0.0268 0.0162 0.054 1.697 0.800 40.145 0.192 3.559 9.041 0.18 76925. 0.2157 15.78 0.3787 0.5921 0.0242 0.0155 0.051 1.621 0.724 38.347 0.183 3.218 8.558 0.18 77019. 0.1942 16.57 0.3977 0.5848 0.0216 0.0147 0.049 1.537 0.646 36.380 0.174 2.872 8.050 0.18 77117. 0.1725 17.36 0.4166 0.5712 0.0190 0.0138 0.046 1.447 0.567 34.241 0.163 2.520 7.506 0.18 77219. 0.1507 18.15 0.4355 0.5500 0.0163 0.0129 0.043 1.349 0.487 31.928 0.152 2.164 6.913 0.18 77325. 0.1286 18.94 0.4545 0.5189 0.0136 0.0119 0.039 1.244 0.406 29.442 0.141 1.805 6.251 0.18 77435. 0.1062 19.73 0.4734 0.4748 0.0109 0.0108 0.036 1.132 0.324 26.783 0.128 1.442 5.490 0.18 77548. 0.0834 20.51 0.4924 0.4125 0.0081 0.0097 0.032 1.012 0.242 23.953 0.114 1.077 4.586 0.18 77665. 0.0602 21.30 0.5113 0.3233 0.0054 0.0085 0.028 0.886 0.160 20.957 0.100 0.711 3.461 0.18 77786. 0.0369 22.09 0.5302 0.1914 0.0026 0.0072 0.024 0.752 0.078 17.795 0.085 0.345 1.976 0.18 77911. 0.0147 22.88 0.5492 -0.0228 -0.0002 0.0058 0.019 0.607 -0.007 14.366 0.069 -0.032 -0.228 0.18 78023. 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 0.0641 0.0187 0.210 4.407 4.310 156.410 0.498 19.169 12.497 0.26 113670. 0.6919 1.18 0.0189 0.0629 0.0629 0.0189 0.212 4.446 4.223 157.811 0.502 18.785 12.138 0.26 113721. 0.6653 2.36 0.0378 0.1222 0.0615 0.0190 0.213 4.481 4.132 159.031 0.506 18.378 11.784 0.26 113775. 0.6389 3.55 0.0568 0.1778 0.0601 0.0192 0.215 4.509 4.035 160.040 0.509 17.948 11.436 0.26 113834. 0.6127 4.73 0.0757 0.2300 0.0585 0.0193 0.216 4.531 3.933 160.814 0.512 17.495 11.093 0.26 113896. 0.5868 5.91 0.0946 0.2788 0.0569 0.0193 0.216 4.545 3.826 161.328 0.514 17.019 10.757 0.26 113962. 0.5612 7.09 0.1135 0.3243 0.0553 0.0193 0.217 4.552 3.714 161.556 0.514 16.519 10.427 0.26 114033. 0.5359 8.28 0.1324 0.3665 0.0535 0.0193 0.217 4.549 3.596 161.473 0.514 15.997 10.102 0.26 114107. 0.5110 9.46 0.1513 0.4057 0.0517 0.0193 0.216 4.538 3.474 161.055 0.513 15.451 9.783 0.26 114187. 0.4863 10.64 0.1703 0.4417 0.0498 0.0192 0.215 4.516 3.346 160.278 0.510 14.884 9.469 0.26 114270. 0.4620 11.82 0.1892 0.4748 0.0478 0.0191 0.213 4.483 3.214 159.116 0.506 14.294 9.161 0.26 114359. 0.4380 13.01 0.2081 0.5050 0.0458 0.0189 0.211 4.439 3.076 157.548 0.501 13.683 8.857 0.26 114452. 0.4143 14.19 0.2270 0.5322 0.0437 0.0186 0.209 4.382 2.934 155.549 0.495 13.052 8.556 0.26 114550. 0.3909 15.37 0.2459 0.5565 0.0415 0.0183 0.205 4.313 2.788 153.097 0.487 12.400 8.259 0.26 114654. 0.3678 16.55 0.2648 0.5779 0.0392 0.0180 0.201 4.231 2.637 150.172 0.478 11.729 7.964 0.26 114762. 0.3449 17.73 0.2838 0.5964 0.0369 0.0176 0.197 4.135 2.482 146.751 0.467 11.039 7.670 0.26 114876. 0.3223 18.92 0.3027 0.6117 0.0346 0.0171 0.192 4.024 2.323 142.816 0.455 10.331 7.376 0.26 114995. 0.2998 20.10 0.3216 0.6239 0.0321 0.0166 0.186 3.898 2.160 138.349 0.440 9.606 7.080 0.26 115119. 0.2775 21.28 0.3405 0.6326 0.0297 0.0160 0.179 3.756 1.993 133.331 0.424 8.865 6.780 0.26 115249. 0.2553 22.46 0.3594 0.6375 0.0271 0.0153 0.171 3.599 1.823 127.749 0.407 8.110 6.473 0.26 115384. 0.2331 23.65 0.3783 0.6381 0.0246 0.0146 0.163 3.426 1.650 121.589 0.387 7.340 6.156 0.26 115526. 0.2109 24.83 0.3973 0.6338 0.0219 0.0138 0.154 3.236 1.474 114.841 0.366 6.558 5.823 0.26 115672. 0.1886 26.01 0.4162 0.6235 0.0193 0.0129 0.144 3.029 1.296 107.496 0.342 5.764 5.468 0.26 115825. 0.1660 27.19 0.4351 0.6057 0.0166 0.0119 0.133 2.805 1.115 99.549 0.317 4.960 5.081 0.26 115983. 0.1431 28.38 0.4540 0.5782 0.0139 0.0109 0.122 2.564 0.933 91.000 0.290 4.148 4.648 0.26 116147. 0.1197 29.56 0.4729 0.5375 0.0111 0.0098 0.110 2.306 0.748 81.852 0.261 3.329 4.148 0.26 116317. 0.0957 30.74 0.4919 0.4775 0.0084 0.0086 0.097 2.032 0.563 72.112 0.230 2.506 3.543 0.26 116493. 0.0709 31.92 0.5108 0.3878 0.0056 0.0074 0.083 1.741 0.378 61.791 0.197 1.679 2.771 0.27 116674. 0.0454 33.11 0.5297 0.2477 0.0029 0.0061 0.068 1.434 0.191 50.896 0.162 0.852 1.706 0.27 116861. 0.0199 34.29 0.5486 0.0024 0.0000 0.0047 0.053 1.103 0.001 39.157 0.125 0.006 0.016 0.27 117034. 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 0.0647 0.0183 0.486 7.652 7.733 362.146 0.865 34.396 9.685 0.35 151553. 0.7183 1.58 0.0190 0.0652 0.0634 0.0185 0.490 7.725 7.578 365.599 0.873 33.709 9.402 0.35 151622. 0.6903 3.16 0.0379 0.1265 0.0621 0.0186 0.494 7.789 7.414 368.608 0.880 32.979 9.123 0.35 151695. 0.6626 4.74 0.0569 0.1840 0.0606 0.0187 0.498 7.842 7.241 371.104 0.886 32.208 8.850 0.35 151774. 0.6352 6.32 0.0759 0.2380 0.0591 0.0188 0.500 7.882 7.058 373.027 0.891 31.395 8.582 0.35 151857. 0.6081 7.91 0.0949 0.2884 0.0575 0.0189 0.502 7.910 6.866 374.315 0.894 30.540 8.320 0.35 151946. 0.5814 9.49 0.1138 0.3353 0.0558 0.0189 0.503 7.922 6.664 374.906 0.895 29.643 8.063 0.35 152041. 0.5551 11.07 0.1328 0.3790 0.0540 0.0189 0.503 7.918 6.453 374.739 0.895 28.704 7.811 0.35 152141. 0.5292 12.65 0.1518 0.4195 0.0522 0.0189 0.501 7.898 6.233 373.754 0.892 27.724 7.564 0.35 152248. 0.5037 14.23 0.1708 0.4568 0.0503 0.0188 0.499 7.858 6.004 371.891 0.888 26.704 7.322 0.35 152360. 0.4785 15.81 0.1897 0.4911 0.0483 0.0186 0.495 7.799 5.765 369.093 0.881 25.644 7.085 0.35 152479. 0.4537 17.39 0.2087 0.5224 0.0462 0.0185 0.490 7.719 5.518 365.300 0.872 24.545 6.852 0.35 152604. 0.4293 18.97 0.2277 0.5509 0.0441 0.0182 0.483 7.617 5.263 360.458 0.861 23.409 6.622 0.35 152736. 0.4052 20.56 0.2467 0.5764 0.0419 0.0179 0.475 7.491 4.999 354.512 0.846 22.236 6.396 0.35 152875. 0.3814 22.14 0.2656 0.5990 0.0396 0.0176 0.466 7.341 4.728 347.409 0.829 21.028 6.172 0.35 153020. 0.3579 23.72 0.2846 0.6187 0.0372 0.0171 0.455 7.165 4.448 339.098 0.810 19.787 5.950 0.35 153173. 0.3347 25.30 0.3036 0.6354 0.0348 0.0166 0.442 6.963 4.162 329.533 0.787 18.513 5.729 0.35 153332. 0.3117 26.88 0.3226 0.6489 0.0324 0.0161 0.427 6.734 3.869 318.667 0.761 17.209 5.507 0.35 153499. 0.2889 28.46 0.3415 0.6591 0.0299 0.0155 0.411 6.476 3.569 306.460 0.732 15.876 5.282 0.35 153674. 0.2662 30.04 0.3605 0.6656 0.0273 0.0148 0.393 6.189 3.263 292.875 0.699 14.515 5.054 0.35 153856. 0.2435 31.62 0.3795 0.6680 0.0247 0.0140 0.373 5.872 2.952 277.881 0.663 13.130 4.818 0.35 154045. 0.2208 33.21 0.3985 0.6656 0.0221 0.0132 0.351 5.525 2.635 261.450 0.624 11.722 4.572 0.35 154242. 0.1980 34.79 0.4174 0.6573 0.0194 0.0123 0.327 5.147 2.314 243.564 0.581 10.294 4.310 0.35 154447. 0.1749 36.37 0.4364 0.6416 0.0167 0.0113 0.301 4.738 1.989 224.212 0.535 8.848 4.024 0.35 154659. 0.1514 37.95 0.4554 0.6161 0.0139 0.0103 0.273 4.298 1.661 203.391 0.486 7.386 3.703 0.35 154879. 0.1273 39.53 0.4744 0.5769 0.0111 0.0092 0.243 3.827 1.329 181.109 0.432 5.913 3.329 0.35 155107. 0.1024 41.11 0.4933 0.5174 0.0083 0.0080 0.211 3.326 0.996 157.388 0.376 4.431 2.871 0.35 155343. 0.0764 42.69 0.5123 0.4250 0.0055 0.0067 0.177 2.795 0.662 132.254 0.316 2.945 2.270 0.35 155586. 0.0493 44.27 0.5313 0.2726 0.0027 0.0053 0.142 2.234 0.327 105.717 0.252 1.456 1.404 0.35 155835. 0.0214 45.86 0.5503 -0.0292 -0.0002 0.0039 0.102 1.611 -0.024 76.245 0.182 -0.108 -0.145 0.35 156029. 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 0.0655 0.0182 0.941 11.861 12.229 701.652 1.340 54.395 7.905 0.44 189431. 0.7373 1.98 0.0190 0.0665 0.0642 0.0183 0.950 11.978 11.986 708.586 1.353 53.313 7.672 0.44 189518. 0.7084 3.96 0.0380 0.1291 0.0628 0.0185 0.958 12.080 11.728 714.628 1.365 52.165 7.443 0.44 189610. 0.6799 5.93 0.0570 0.1878 0.0614 0.0186 0.965 12.165 11.455 719.643 1.374 50.950 7.219 0.44 189709. 0.6517 7.91 0.0760 0.2428 0.0598 0.0187 0.970 12.230 11.166 723.504 1.382 49.668 7.000 0.44 189814. 0.6239 9.89 0.0949 0.2942 0.0582 0.0188 0.974 12.274 10.863 726.090 1.387 48.319 6.786 0.44 189926. 0.5965 11.87 0.1139 0.3422 0.0565 0.0188 0.975 12.294 10.545 727.279 1.389 46.904 6.576 0.44 190044. 0.5696 13.85 0.1329 0.3868 0.0547 0.0188 0.975 12.289 10.212 726.948 1.388 45.422 6.372 0.44 190171. 0.5430 15.82 0.1519 0.4281 0.0529 0.0188 0.972 12.255 9.864 724.979 1.385 43.875 6.171 0.44 190304. 0.5169 17.80 0.1709 0.4663 0.0509 0.0187 0.967 12.192 9.502 721.252 1.377 42.263 5.975 0.44 190445. 0.4912 19.78 0.1899 0.5015 0.0489 0.0185 0.960 12.098 9.125 715.654 1.367 40.588 5.783 0.44 190595. 0.4659 21.76 0.2089 0.5337 0.0468 0.0183 0.950 11.970 8.735 708.068 1.352 38.852 5.595 0.44 190752. 0.4410 23.74 0.2279 0.5630 0.0446 0.0181 0.937 11.806 8.331 698.385 1.334 37.056 5.411 0.44 190917. 0.4165 25.71 0.2469 0.5894 0.0424 0.0178 0.921 11.605 7.914 686.495 1.311 35.202 5.229 0.44 191091. 0.3923 27.69 0.2658 0.6130 0.0401 0.0174 0.902 11.365 7.485 672.294 1.284 33.292 5.050 0.44 191274. 0.3685 29.67 0.2848 0.6338 0.0377 0.0170 0.879 11.084 7.043 655.683 1.252 31.329 4.872 0.44 191465. 0.3449 31.65 0.3038 0.6515 0.0353 0.0165 0.854 10.761 6.591 636.566 1.216 29.315 4.696 0.44 191665. 0.3215 33.63 0.3228 0.6663 0.0328 0.0159 0.825 10.394 6.127 614.854 1.174 27.252 4.520 0.44 191875. 0.2984 35.60 0.3418 0.6778 0.0303 0.0153 0.792 9.981 5.653 590.464 1.128 25.143 4.342 0.44 192093. 0.2753 37.58 0.3608 0.6857 0.0277 0.0146 0.755 9.523 5.169 563.326 1.076 22.991 4.162 0.44 192321. 0.2524 39.56 0.3798 0.6897 0.0251 0.0138 0.715 9.016 4.676 533.373 1.019 20.800 3.977 0.44 192558. 0.2294 41.54 0.3988 0.6890 0.0224 0.0129 0.671 8.462 4.175 500.553 0.956 18.572 3.783 0.44 192805. 0.2062 43.52 0.4178 0.6826 0.0196 0.0120 0.623 7.858 3.667 464.830 0.888 16.311 3.578 0.44 193062. 0.1828 45.49 0.4367 0.6692 0.0169 0.0110 0.572 7.204 3.152 426.179 0.814 14.022 3.355 0.44 193328. 0.1589 47.47 0.4557 0.6461 0.0141 0.0099 0.516 6.501 2.632 384.597 0.735 11.709 3.104 0.44 193603. 0.1343 49.45 0.4747 0.6095 0.0113 0.0088 0.456 5.749 2.108 340.101 0.650 9.377 2.811 0.44 193889. 0.1089 51.43 0.4937 0.5522 0.0085 0.0076 0.393 4.948 1.581 292.730 0.559 7.031 2.449 0.44 194184. 0.0821 53.41 0.5127 0.4604 0.0056 0.0063 0.325 4.100 1.052 242.543 0.463 4.677 1.967 0.44 194488. 0.0538 55.38 0.5317 0.3031 0.0028 0.0049 0.254 3.204 0.522 189.555 0.362 2.320 1.248 0.44 194800. 0.0240 57.36 0.5507 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 0.0665 0.0182 1.631 17.135 17.880 1216.329 1.936 79.528 6.667 0.52 227301. 0.7519 2.37 0.0190 0.0673 0.0652 0.0184 1.648 17.308 17.527 1228.612 1.955 77.961 6.471 0.52 227406. 0.7225 4.74 0.0379 0.1305 0.0638 0.0186 1.662 17.458 17.153 1239.301 1.972 76.294 6.278 0.52 227517. 0.6934 7.12 0.0569 0.1899 0.0623 0.0187 1.674 17.583 16.756 1248.155 1.987 74.530 6.089 0.52 227636. 0.6648 9.49 0.0759 0.2456 0.0608 0.0188 1.683 17.679 16.337 1254.955 1.997 72.668 5.905 0.52 227763. 0.6365 11.86 0.0949 0.2976 0.0591 0.0189 1.689 17.742 15.896 1259.482 2.005 70.707 5.725 0.52 227898. 0.6087 14.23 0.1138 0.3462 0.0574 0.0189 1.692 17.771 15.433 1261.526 2.008 68.647 5.549 0.52 228041. 0.5814 16.60 0.1328 0.3914 0.0556 0.0189 1.691 17.762 14.948 1260.871 2.007 66.490 5.377 0.52 228193. 0.5545 18.97 0.1518 0.4334 0.0537 0.0188 1.686 17.712 14.442 1257.312 2.001 64.237 5.210 0.52 228354. 0.5280 21.35 0.1708 0.4722 0.0518 0.0187 1.677 17.618 13.914 1250.643 1.990 61.889 5.046 0.52 228524. 0.5020 23.72 0.1897 0.5080 0.0497 0.0186 1.664 17.477 13.365 1240.661 1.975 59.448 4.886 0.52 228704. 0.4764 26.09 0.2087 0.5409 0.0476 0.0184 1.646 17.287 12.796 1227.168 1.953 56.917 4.730 0.52 228893. 0.4512 28.46 0.2277 0.5710 0.0454 0.0181 1.623 17.045 12.207 1209.970 1.926 54.298 4.576 0.52 229092. 0.4264 30.83 0.2467 0.5982 0.0432 0.0178 1.594 16.748 11.600 1188.880 1.892 51.595 4.425 0.53 229301. 0.4020 33.20 0.2656 0.6226 0.0408 0.0174 1.561 16.393 10.973 1163.716 1.852 48.809 4.277 0.53 229521. 0.3779 35.58 0.2846 0.6442 0.0384 0.0170 1.521 15.979 10.329 1134.304 1.805 45.945 4.130 0.53 229751. 0.3540 37.95 0.3036 0.6629 0.0360 0.0165 1.476 15.502 9.668 1100.477 1.751 43.005 3.985 0.53 229991. 0.3305 40.32 0.3226 0.6787 0.0335 0.0159 1.424 14.962 8.992 1062.081 1.690 39.994 3.840 0.53 230243. 0.3071 42.69 0.3415 0.6914 0.0309 0.0153 1.366 14.354 8.299 1018.971 1.622 36.916 3.694 0.53 230505. 0.2839 45.06 0.3605 0.7007 0.0283 0.0145 1.302 13.679 7.593 971.020 1.545 33.774 3.547 0.53 230778. 0.2607 47.43 0.3795 0.7061 0.0256 0.0137 1.231 12.934 6.874 918.114 1.461 30.574 3.396 0.53 231063. 0.2374 49.81 0.3984 0.7072 0.0229 0.0129 1.153 12.117 6.142 860.163 1.369 27.320 3.239 0.53 231359. 0.2141 52.18 0.4174 0.7028 0.0201 0.0119 1.069 11.229 5.399 797.096 1.269 24.017 3.072 0.53 231667. 0.1904 54.55 0.4364 0.6916 0.0173 0.0109 0.977 10.268 4.647 728.873 1.160 20.672 2.892 0.53 231986. 0.1663 56.92 0.4554 0.6712 0.0145 0.0098 0.879 9.234 3.887 655.487 1.043 17.290 2.690 0.53 232317. 0.1414 59.29 0.4743 0.6377 0.0116 0.0086 0.774 8.128 3.121 576.965 0.918 13.881 2.453 0.53 232659. 0.1156 61.66 0.4933 0.5839 0.0087 0.0074 0.662 6.950 2.349 493.379 0.785 10.450 2.160 0.53 233013. 0.0883 64.04 0.5123 0.4956 0.0059 0.0061 0.543 5.703 1.576 404.827 0.644 7.008 1.765 0.53 233377. 0.0591 66.41 0.5313 0.3395 0.0030 0.0047 0.418 4.386 0.800 311.351 0.496 3.560 1.166 0.53 233752. 0.0278 68.78 0.5502 -0.0047 0.0000 0.0031 0.280 2.938 -0.007 208.572 0.332 -0.032 -0.016 0.53 234062. 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 0.0678 0.0184 2.624 23.627 24.801 1956.726 2.669 110.314 5.749 0.61 265161. 0.7636 2.78 0.0190 0.0679 0.0665 0.0186 2.651 23.870 24.316 1976.849 2.697 108.156 5.579 0.61 265284. 0.7337 5.55 0.0381 0.1318 0.0651 0.0188 2.674 24.081 23.799 1994.306 2.721 105.858 5.413 0.61 265415. 0.7043 8.33 0.0571 0.1917 0.0636 0.0189 2.694 24.254 23.251 2008.695 2.740 103.422 5.250 0.61 265556. 0.6752 11.10 0.0761 0.2479 0.0620 0.0190 2.708 24.387 22.672 2019.654 2.755 100.846 5.092 0.61 265705. 0.6466 13.88 0.0952 0.3004 0.0603 0.0191 2.718 24.473 22.062 2026.828 2.765 98.131 4.937 0.61 265865. 0.6185 16.66 0.1142 0.3495 0.0586 0.0191 2.722 24.510 21.420 2029.871 2.769 95.276 4.786 0.61 266034. 0.5908 19.43 0.1333 0.3952 0.0567 0.0191 2.720 24.493 20.747 2028.439 2.767 92.284 4.639 0.61 266213. 0.5636 22.21 0.1523 0.4377 0.0548 0.0191 2.712 24.417 20.044 2022.193 2.759 89.156 4.496 0.61 266403. 0.5368 24.99 0.1713 0.4771 0.0528 0.0190 2.697 24.280 19.311 2010.802 2.743 85.895 4.356 0.61 266604. 0.5105 27.76 0.1904 0.5135 0.0507 0.0188 2.674 24.076 18.548 1993.940 2.720 82.503 4.219 0.61 266816. 0.4847 30.54 0.2094 0.5470 0.0485 0.0186 2.644 23.803 17.757 1971.289 2.689 78.984 4.086 0.61 267039. 0.4592 33.31 0.2284 0.5776 0.0463 0.0183 2.605 23.455 16.938 1942.537 2.650 75.341 3.955 0.61 267273. 0.4341 36.09 0.2475 0.6055 0.0440 0.0180 2.558 23.031 16.092 1907.384 2.602 71.579 3.827 0.61 267520. 0.4094 38.87 0.2665 0.6306 0.0416 0.0176 2.502 22.526 15.221 1865.534 2.545 67.702 3.701 0.61 267778. 0.3851 41.64 0.2856 0.6529 0.0392 0.0171 2.436 21.936 14.324 1816.708 2.478 63.714 3.576 0.61 268049. 0.3610 44.42 0.3046 0.6724 0.0366 0.0166 2.361 21.259 13.404 1760.638 2.402 59.620 3.453 0.61 268332. 0.3372 47.20 0.3236 0.6891 0.0341 0.0160 2.276 20.492 12.461 1697.078 2.315 55.426 3.330 0.61 268628. 0.3135 49.97 0.3427 0.7027 0.0314 0.0153 2.180 19.631 11.497 1625.791 2.218 51.136 3.207 0.61 268936. 0.2900 52.75 0.3617 0.7129 0.0287 0.0146 2.074 18.674 10.512 1546.571 2.110 46.758 3.083 0.61 269258. 0.2666 55.52 0.3807 0.7195 0.0260 0.0138 1.957 17.620 9.509 1459.237 1.991 42.297 2.956 0.62 269593. 0.2431 58.30 0.3998 0.7217 0.0232 0.0129 1.829 16.465 8.489 1363.642 1.860 37.761 2.824 0.62 269941. 0.2194 61.08 0.4188 0.7187 0.0204 0.0119 1.689 15.210 7.454 1259.673 1.718 33.155 2.684 0.62 270303. 0.1954 63.85 0.4379 0.7089 0.0175 0.0108 1.539 13.853 6.405 1147.267 1.565 28.490 2.532 0.62 270678. 0.1709 66.63 0.4569 0.6899 0.0146 0.0097 1.376 12.394 5.345 1026.416 1.400 23.774 2.362 0.62 271066. 0.1456 69.41 0.4759 0.6577 0.0117 0.0085 1.203 10.833 4.276 897.169 1.224 19.018 2.162 0.62 271468. 0.1192 72.18 0.4950 0.6046 0.0087 0.0072 1.019 9.172 3.200 759.648 1.036 14.233 1.911 0.62 271884. 0.0912 74.96 0.5140 0.5147 0.0058 0.0058 0.823 7.414 2.120 614.020 0.838 9.431 1.566 0.62 272312. 0.0608 77.73 0.5330 0.3488 0.0028 0.0043 0.617 5.558 1.039 460.316 0.628 4.620 1.023 0.62 272751. 0.0278 80.51 0.5521 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 0.0694 0.0189 4.011 31.602 33.161 2991.146 3.570 147.499 5.028 0.70 303005. 0.7723 3.18 0.0191 0.0681 0.0681 0.0191 4.052 31.924 32.521 3021.543 3.607 144.651 4.882 0.70 303147. 0.7425 6.36 0.0382 0.1321 0.0666 0.0192 4.087 32.202 31.837 3047.887 3.638 141.612 4.738 0.70 303299. 0.7130 9.54 0.0573 0.1923 0.0651 0.0194 4.116 32.431 31.111 3069.529 3.664 138.383 4.597 0.70 303462. 0.6839 12.72 0.0763 0.2487 0.0635 0.0195 4.138 32.603 30.342 3085.873 3.683 134.963 4.460 0.70 303635. 0.6552 15.90 0.0954 0.3016 0.0618 0.0196 4.152 32.714 29.530 3096.343 3.696 131.351 4.326 0.70 303820. 0.6270 19.08 0.1145 0.3510 0.0600 0.0196 4.158 32.756 28.676 3100.379 3.701 127.550 4.195 0.70 304016. 0.5992 22.26 0.1336 0.3970 0.0581 0.0196 4.154 32.725 27.779 3097.422 3.697 123.560 4.068 0.70 304223. 0.5718 25.44 0.1527 0.4399 0.0562 0.0195 4.140 32.614 26.840 3086.939 3.685 119.384 3.944 0.70 304443. 0.5449 28.63 0.1718 0.4797 0.0541 0.0194 4.115 32.419 25.860 3068.418 3.663 115.027 3.823 0.70 304674. 0.5185 31.81 0.1908 0.5166 0.0520 0.0192 4.079 32.133 24.841 3041.366 3.630 110.491 3.705 0.70 304919. 0.4924 34.99 0.2099 0.5505 0.0498 0.0190 4.030 31.752 23.782 3005.302 3.587 105.783 3.589 0.70 305177. 0.4668 38.17 0.2290 0.5817 0.0475 0.0187 3.969 31.271 22.686 2959.760 3.533 100.906 3.476 0.70 305447. 0.4416 41.35 0.2481 0.6101 0.0451 0.0183 3.895 30.685 21.553 2904.279 3.467 95.866 3.366 0.70 305732. 0.4168 44.53 0.2672 0.6359 0.0427 0.0179 3.806 29.989 20.385 2838.428 3.388 90.671 3.257 0.70 306030. 0.3922 47.71 0.2863 0.6589 0.0401 0.0174 3.704 29.179 19.183 2761.778 3.297 85.324 3.150 0.70 306342. 0.3680 50.89 0.3053 0.6792 0.0376 0.0169 3.586 28.251 17.948 2673.932 3.192 79.834 3.045 0.70 306668. 0.3440 54.07 0.3244 0.6967 0.0349 0.0163 3.452 27.201 16.683 2574.515 3.073 74.208 2.939 0.70 307009. 0.3202 57.25 0.3435 0.7112 0.0322 0.0156 3.303 26.024 15.389 2463.174 2.940 68.452 2.834 0.70 307364. 0.2965 60.43 0.3626 0.7226 0.0294 0.0148 3.137 24.719 14.068 2339.597 2.793 62.575 2.727 0.70 307735. 0.2728 63.61 0.3817 0.7303 0.0266 0.0139 2.955 23.281 12.721 2203.507 2.630 56.585 2.619 0.70 308120. 0.2491 66.79 0.4008 0.7338 0.0238 0.0130 2.755 21.708 11.352 2054.683 2.453 50.492 2.506 0.70 308520. 0.2252 69.97 0.4198 0.7321 0.0208 0.0120 2.538 20.000 9.961 1892.952 2.260 44.305 2.387 0.70 308936. 0.2009 73.15 0.4389 0.7239 0.0179 0.0109 2.304 18.154 8.551 1718.223 2.051 38.035 2.257 0.70 309367. 0.1761 76.33 0.4580 0.7067 0.0149 0.0097 2.052 16.170 7.126 1530.484 1.827 31.696 2.112 0.71 309814. 0.1504 79.52 0.4771 0.6763 0.0119 0.0084 1.783 14.050 5.688 1329.817 1.587 25.301 1.940 0.71 310276. 0.1234 82.70 0.4962 0.6247 0.0089 0.0071 1.497 11.795 4.241 1116.415 1.333 18.866 1.723 0.71 310753. 0.0947 85.88 0.5153 0.5348 0.0058 0.0056 1.194 9.409 2.789 890.556 1.063 12.407 1.421 0.71 311245. 0.0633 89.06 0.5343 0.3621 0.0028 0.0041 0.875 6.892 1.334 652.287 0.779 5.933 0.928 0.71 311749. 0.0286 92.24 0.5534 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 0.0714 0.0203 6.131 42.934 43.194 4571.669 4.851 192.129 4.285 0.79 340827. 0.7512 3.56 0.0190 0.0653 0.0701 0.0204 6.166 43.182 42.386 4598.015 4.879 188.531 4.181 0.79 340988. 0.7260 7.13 0.0380 0.1274 0.0687 0.0205 6.194 43.378 41.519 4618.889 4.901 184.678 4.077 0.79 341161. 0.7007 10.69 0.0570 0.1862 0.0671 0.0206 6.214 43.515 40.596 4633.540 4.916 180.571 3.974 0.79 341345. 0.6753 14.25 0.0760 0.2419 0.0655 0.0206 6.224 43.588 39.615 4641.283 4.925 176.209 3.871 0.79 341542. 0.6499 17.81 0.0950 0.2944 0.0638 0.0206 6.224 43.589 38.577 4641.421 4.925 171.591 3.770 0.79 341750. 0.6245 21.38 0.1140 0.3439 0.0620 0.0206 6.213 43.513 37.482 4633.269 4.916 166.720 3.669 0.79 341972. 0.5991 24.94 0.1330 0.3903 0.0601 0.0205 6.190 43.352 36.330 4616.123 4.898 161.598 3.570 0.79 342206. 0.5739 28.50 0.1520 0.4338 0.0581 0.0204 6.154 43.100 35.123 4589.266 4.869 156.229 3.471 0.79 342455. 0.5487 32.07 0.1710 0.4743 0.0560 0.0202 6.104 42.749 33.862 4551.966 4.830 150.619 3.374 0.79 342716. 0.5237 35.63 0.1900 0.5120 0.0538 0.0200 6.039 42.294 32.548 4503.481 4.778 144.774 3.278 0.79 342992. 0.4988 39.19 0.2090 0.5469 0.0516 0.0197 5.958 41.726 31.182 4443.044 4.714 138.699 3.183 0.79 343283. 0.4741 42.75 0.2280 0.5791 0.0492 0.0194 5.860 41.039 29.767 4369.880 4.637 132.401 3.090 0.79 343588. 0.4496 46.32 0.2470 0.6086 0.0468 0.0190 5.744 40.225 28.302 4283.211 4.545 125.889 2.997 0.79 343908. 0.4253 49.88 0.2660 0.6354 0.0443 0.0186 5.609 39.277 26.792 4182.276 4.438 119.170 2.906 0.79 344243. 0.4011 53.44 0.2850 0.6595 0.0417 0.0180 5.453 38.188 25.236 4066.323 4.315 112.251 2.815 0.79 344594. 0.3772 57.01 0.3040 0.6810 0.0391 0.0175 5.276 36.952 23.638 3934.644 4.175 105.143 2.725 0.79 344960. 0.3533 60.57 0.3230 0.6997 0.0364 0.0168 5.078 35.561 21.999 3786.577 4.018 97.853 2.635 0.79 345343. 0.3296 64.13 0.3420 0.7156 0.0336 0.0161 4.857 34.011 20.322 3621.507 3.843 90.392 2.545 0.79 345742. 0.3060 67.69 0.3610 0.7284 0.0308 0.0153 4.612 32.296 18.608 3438.935 3.649 82.769 2.454 0.79 346157. 0.2824 71.26 0.3800 0.7376 0.0279 0.0144 4.343 30.416 16.861 3238.719 3.436 74.996 2.361 0.79 346588. 0.2586 74.82 0.3990 0.7429 0.0249 0.0134 4.050 28.365 15.082 3020.346 3.205 67.084 2.265 0.79 347037. 0.2346 78.38 0.4180 0.7432 0.0220 0.0123 3.733 26.144 13.275 2783.779 2.954 59.045 2.163 0.79 347502. 0.2102 81.95 0.4370 0.7372 0.0189 0.0112 3.392 23.752 11.442 2529.174 2.684 50.894 2.052 0.79 347985. 0.1851 85.51 0.4560 0.7223 0.0159 0.0100 3.026 21.195 9.588 2256.855 2.395 42.646 1.927 0.79 348484. 0.1591 89.07 0.4750 0.6946 0.0128 0.0087 2.638 18.477 7.715 1967.439 2.088 34.318 1.779 0.79 349001. 0.1318 92.63 0.4940 0.6462 0.0096 0.0074 2.229 15.607 5.830 1661.802 1.763 25.930 1.591 0.80 349534. 0.1025 96.20 0.5131 0.5613 0.0065 0.0059 1.798 12.594 3.935 1341.014 1.423 17.503 1.331 0.80 350084. 0.0704 99.76 0.5321 0.4012 0.0034 0.0045 1.349 9.447 2.035 1005.972 1.067 9.050 0.917 0.80 350648. 0.0349 103.32 0.5511 0.0175 0.0001 0.0028 0.857 6.003 0.055 639.238 0.678 0.243 0.039 0.80 351121. 0.0002 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 0.0738 0.0249 10.334 65.136 55.057 7706.353 7.359 244.894 3.240 0.87 378626. 0.6413 4.04 0.0194 0.0565 0.0724 0.0248 10.300 64.920 54.060 7680.835 7.335 240.459 3.192 0.87 378810. 0.6260 8.07 0.0387 0.1112 0.0710 0.0247 10.251 64.610 52.983 7644.152 7.300 235.670 3.144 0.87 379008. 0.6103 12.11 0.0581 0.1642 0.0694 0.0246 10.186 64.202 51.827 7595.892 7.254 230.526 3.095 0.87 379219. 0.5942 16.14 0.0775 0.2155 0.0678 0.0244 10.106 63.694 50.590 7535.696 7.196 225.023 3.045 0.87 379445. 0.5776 20.18 0.0968 0.2649 0.0660 0.0241 10.008 63.081 49.272 7463.244 7.127 219.162 2.994 0.87 379685. 0.5606 24.21 0.1162 0.3124 0.0641 0.0239 9.894 62.363 47.874 7378.246 7.046 212.945 2.943 0.87 379940. 0.5431 28.25 0.1356 0.3580 0.0622 0.0235 9.763 61.535 46.398 7280.341 6.952 206.376 2.891 0.87 380211. 0.5251 32.28 0.1550 0.4015 0.0601 0.0232 9.614 60.595 44.843 7169.157 6.846 199.463 2.837 0.87 380498. 0.5067 36.32 0.1743 0.4430 0.0579 0.0228 9.447 59.540 43.213 7044.279 6.727 192.211 2.782 0.87 380800. 0.4878 40.35 0.1937 0.4823 0.0556 0.0223 9.260 58.365 41.509 6905.264 6.594 184.632 2.727 0.87 381119. 0.4685 44.39 0.2131 0.5194 0.0532 0.0218 9.054 57.066 39.733 6751.571 6.447 176.734 2.669 0.87 381455. 0.4488 48.42 0.2324 0.5542 0.0508 0.0213 8.827 55.638 37.889 6582.589 6.286 168.530 2.611 0.88 381808. 0.4286 52.46 0.2518 0.5866 0.0482 0.0207 8.579 54.074 35.978 6397.565 6.109 160.030 2.551 0.88 382178. 0.4081 56.49 0.2712 0.6165 0.0455 0.0200 8.309 52.367 34.003 6195.654 5.916 151.247 2.489 0.88 382565. 0.3872 60.53 0.2905 0.6438 0.0428 0.0193 8.014 50.510 31.968 5975.930 5.707 142.192 2.426 0.88 382971. 0.3659 64.56 0.3099 0.6685 0.0400 0.0186 7.694 48.494 29.874 5737.387 5.479 132.879 2.362 0.88 383394. 0.3443 68.60 0.3293 0.6903 0.0371 0.0177 7.347 46.310 27.725 5478.984 5.232 123.322 2.295 0.88 383836. 0.3223 72.64 0.3486 0.7090 0.0342 0.0168 6.973 43.949 25.524 5199.635 4.965 113.532 2.227 0.88 384297. 0.3000 76.67 0.3680 0.7244 0.0312 0.0158 6.569 41.401 23.275 4898.272 4.678 103.525 2.155 0.88 384776. 0.2773 80.71 0.3874 0.7355 0.0281 0.0148 6.139 38.690 20.979 4577.537 4.371 93.314 2.079 0.88 385275. 0.2539 84.74 0.4068 0.7365 0.0250 0.0138 5.718 36.040 18.637 4263.974 4.072 82.898 1.982 0.88 385792. 0.2283 88.78 0.4261 0.7298 0.0218 0.0127 5.273 33.236 16.257 3932.241 3.755 72.310 1.875 0.88 386329. 0.2016 92.81 0.4455 0.7131 0.0185 0.0116 4.804 30.280 13.843 3582.510 3.421 61.572 1.753 0.88 386886. 0.1739 96.85 0.4649 0.6824 0.0153 0.0104 4.314 27.190 11.399 3216.943 3.072 50.705 1.607 0.88 387461. 0.1447 100.88 0.4842 0.6316 0.0120 0.0092 3.805 23.982 8.933 2837.314 2.709 39.736 1.428 0.88 388057. 0.1138 104.92 0.5036 0.5500 0.0086 0.0079 3.281 20.680 6.451 2446.721 2.336 28.692 1.196 0.88 388672. 0.0810 108.95 0.5230 0.4187 0.0053 0.0066 2.746 17.309 3.957 2047.835 1.956 17.602 0.877 0.88 389304. 0.0465 112.99 0.5423 0.1988 0.0019 0.0053 2.199 13.860 1.451 1639.858 1.566 6.455 0.401 0.89 389946. 0.0129 117.02 0.5617 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 0.0739 0.0313 17.300 99.124 66.710 12900.256 11.199 296.726 2.346 0.96 416486. 0.5109 4.48 0.0195 0.0454 0.0727 0.0313 17.279 99.006 65.683 12884.936 11.186 292.157 2.312 0.96 416684. 0.4998 8.95 0.0391 0.0894 0.0715 0.0312 17.232 98.739 64.561 12850.206 11.155 287.167 2.279 0.96 416898. 0.4883 13.43 0.0586 0.1322 0.0701 0.0311 17.156 98.304 63.341 12793.519 11.106 281.740 2.246 0.96 417127. 0.4767 17.90 0.0781 0.1737 0.0687 0.0309 17.047 97.680 62.018 12712.305 11.036 275.857 2.213 0.96 417373. 0.4648 22.38 0.0976 0.2139 0.0671 0.0306 16.902 96.847 60.590 12603.984 10.942 269.504 2.180 0.96 417635. 0.4527 26.85 0.1172 0.2529 0.0654 0.0303 16.717 95.788 59.053 12466.090 10.822 262.667 2.149 0.96 417915. 0.4404 31.33 0.1367 0.2908 0.0635 0.0299 16.490 94.483 57.405 12296.253 10.675 255.336 2.117 0.96 418213. 0.4279 35.80 0.1562 0.3276 0.0616 0.0294 16.216 92.917 55.644 12092.556 10.498 247.505 2.087 0.96 418529. 0.4152 40.28 0.1758 0.3633 0.0595 0.0288 15.896 91.082 53.770 11853.696 10.290 239.171 2.057 0.96 418864. 0.4024 44.75 0.1953 0.3980 0.0573 0.0281 15.528 88.973 51.785 11579.150 10.052 230.338 2.028 0.96 419218. 0.3893 49.23 0.2148 0.4316 0.0550 0.0274 15.112 86.591 49.688 11269.268 9.783 221.013 2.000 0.96 419591. 0.3760 53.70 0.2343 0.4641 0.0526 0.0265 14.651 83.947 47.484 10925.082 9.484 211.210 1.971 0.96 419985. 0.3623 58.18 0.2539 0.4955 0.0500 0.0256 14.145 81.049 45.177 10548.003 9.157 200.945 1.943 0.96 420398. 0.3482 62.65 0.2734 0.5255 0.0473 0.0246 13.597 77.911 42.770 10139.609 8.802 190.239 1.913 0.96 420832. 0.3337 67.13 0.2929 0.5540 0.0446 0.0236 13.010 74.546 40.268 9701.615 8.422 179.113 1.883 0.96 421286. 0.3186 71.60 0.3124 0.5808 0.0417 0.0224 12.385 70.965 37.678 9235.637 8.018 167.592 1.850 0.96 421761. 0.3029 76.08 0.3320 0.6057 0.0388 0.0212 11.725 67.181 35.005 8743.071 7.590 155.701 1.816 0.97 422257. 0.2866 80.55 0.3515 0.6281 0.0357 0.0200 11.030 63.200 32.254 8224.992 7.140 143.467 1.779 0.97 422773. 0.2694 85.03 0.3710 0.6478 0.0326 0.0187 10.302 59.027 29.433 7681.967 6.669 130.918 1.738 0.97 423311. 0.2515 89.50 0.3906 0.6637 0.0294 0.0173 9.546 54.699 26.546 7118.690 6.180 118.078 1.691 0.97 423870. 0.2324 93.98 0.4101 0.6709 0.0261 0.0160 8.814 50.503 23.596 6572.548 5.706 104.954 1.628 0.97 424450. 0.2110 98.45 0.4296 0.6567 0.0228 0.0149 8.226 47.136 20.577 6134.354 5.325 91.527 1.521 0.97 425052. 0.1841 102.93 0.4491 0.6210 0.0194 0.0140 7.736 44.324 17.503 5768.438 5.008 77.854 1.376 0.97 425675. 0.1536 107.40 0.4687 0.5691 0.0159 0.0131 7.244 41.505 14.394 5401.602 4.689 64.024 1.209 0.97 426320. 0.1223 111.88 0.4882 0.4969 0.0125 0.0122 6.760 38.737 11.260 5041.298 4.376 50.084 1.013 0.97 426987. 0.0907 116.35 0.5077 0.4004 0.0090 0.0114 6.289 36.036 8.115 4689.819 4.071 36.097 0.785 0.97 427675. 0.0596 120.83 0.5273 0.2748 0.0055 0.0106 5.830 33.407 4.972 4347.676 3.774 22.117 0.519 0.97 428384. 0.0309 125.30 0.5468 0.1137 0.0020 0.0097 5.374 30.791 1.828 4007.238 3.479 8.131 0.207 0.97 429111. 0.0075 129.78 0.5663