20x10.5PN (20x105PN.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 0.0885 0.0348 0.009 0.565 0.451 6.688 0.064 2.006 30.590 0.08 41723. 0.6027 0.45 0.0238 0.0587 0.0871 0.0352 0.009 0.572 0.444 6.767 0.065 1.976 29.771 0.08 41749. 0.5821 0.90 0.0475 0.1142 0.0856 0.0356 0.009 0.578 0.437 6.841 0.065 1.942 28.953 0.08 41778. 0.5613 1.35 0.0713 0.1665 0.0841 0.0360 0.009 0.584 0.429 6.910 0.066 1.907 28.139 0.08 41809. 0.5405 1.80 0.0950 0.2156 0.0824 0.0363 0.009 0.589 0.420 6.970 0.067 1.868 27.330 0.08 41843. 0.5196 2.25 0.1188 0.2616 0.0805 0.0366 0.009 0.593 0.411 7.020 0.067 1.826 26.528 0.08 41880. 0.4987 2.70 0.1425 0.3045 0.0786 0.0368 0.009 0.597 0.401 7.059 0.067 1.782 25.734 0.08 41919. 0.4778 3.15 0.1663 0.3444 0.0764 0.0369 0.010 0.599 0.390 7.085 0.068 1.733 24.949 0.08 41961. 0.4569 3.60 0.1900 0.3814 0.0742 0.0369 0.010 0.600 0.378 7.094 0.068 1.682 24.173 0.08 42006. 0.4361 4.05 0.2138 0.4154 0.0717 0.0369 0.010 0.599 0.366 7.086 0.068 1.627 23.405 0.08 42054. 0.4152 4.50 0.2375 0.4466 0.0691 0.0368 0.009 0.597 0.352 7.059 0.067 1.568 22.646 0.08 42105. 0.3944 4.95 0.2613 0.4750 0.0664 0.0365 0.009 0.592 0.338 7.010 0.067 1.505 21.893 0.08 42159. 0.3736 5.40 0.2850 0.5005 0.0634 0.0361 0.009 0.586 0.323 6.939 0.066 1.439 21.146 0.08 42216. 0.3529 5.85 0.3088 0.5231 0.0604 0.0356 0.009 0.579 0.308 6.844 0.065 1.369 20.403 0.08 42276. 0.3321 6.30 0.3325 0.5429 0.0572 0.0350 0.009 0.569 0.292 6.727 0.064 1.297 19.661 0.08 42340. 0.3115 6.75 0.3563 0.5596 0.0539 0.0343 0.009 0.557 0.275 6.587 0.063 1.222 18.916 0.08 42406. 0.2909 7.20 0.3801 0.5732 0.0505 0.0335 0.009 0.543 0.257 6.424 0.061 1.144 18.165 0.08 42476. 0.2703 7.65 0.4038 0.5834 0.0469 0.0325 0.008 0.527 0.239 6.237 0.060 1.064 17.401 0.08 42550. 0.2497 8.10 0.4276 0.5900 0.0433 0.0314 0.008 0.509 0.221 6.026 0.058 0.982 16.621 0.08 42626. 0.2291 8.55 0.4513 0.5926 0.0396 0.0302 0.008 0.490 0.202 5.792 0.055 0.898 15.814 0.08 42706. 0.2085 9.00 0.4751 0.5906 0.0358 0.0288 0.007 0.468 0.183 5.534 0.053 0.813 14.973 0.08 42789. 0.1878 9.45 0.4988 0.5833 0.0320 0.0273 0.007 0.444 0.163 5.252 0.050 0.725 14.083 0.08 42876. 0.1668 9.90 0.5226 0.5696 0.0281 0.0258 0.007 0.418 0.143 4.945 0.047 0.637 13.127 0.08 42966. 0.1457 10.35 0.5463 0.5480 0.0241 0.0240 0.006 0.390 0.123 4.615 0.044 0.547 12.082 0.08 43059. 0.1243 10.80 0.5701 0.5165 0.0201 0.0222 0.006 0.360 0.103 4.261 0.041 0.456 10.913 0.08 43156. 0.1025 11.25 0.5938 0.4719 0.0161 0.0202 0.005 0.328 0.082 3.884 0.037 0.365 9.571 0.08 43256. 0.0804 11.70 0.6176 0.4092 0.0120 0.0182 0.005 0.295 0.061 3.485 0.033 0.273 7.980 0.08 43359. 0.0580 12.15 0.6413 0.3204 0.0080 0.0160 0.004 0.259 0.041 3.065 0.029 0.181 6.016 0.08 43466. 0.0356 12.60 0.6651 0.1915 0.0039 0.0137 0.004 0.222 0.020 2.625 0.025 0.089 3.468 0.08 43576. 0.0144 13.05 0.6888 -0.0049 -0.0001 0.0113 0.003 0.183 0.000 2.166 0.021 -0.002 -0.085 0.08 43687. 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 0.0889 0.0314 0.065 2.040 1.813 48.270 0.230 8.064 17.036 0.16 83444. 0.6730 0.90 0.0239 0.0656 0.0875 0.0319 0.066 2.069 1.786 48.964 0.234 7.942 16.541 0.16 83497. 0.6485 1.81 0.0477 0.1272 0.0861 0.0323 0.067 2.097 1.756 49.622 0.237 7.810 16.050 0.16 83556. 0.6239 2.71 0.0716 0.1851 0.0845 0.0327 0.067 2.123 1.724 50.229 0.240 7.667 15.565 0.16 83618. 0.5995 3.62 0.0955 0.2392 0.0828 0.0331 0.068 2.146 1.689 50.773 0.242 7.512 15.087 0.16 83687. 0.5752 4.52 0.1193 0.2897 0.0810 0.0334 0.069 2.165 1.651 51.239 0.245 7.345 14.617 0.16 83760. 0.5511 5.42 0.1432 0.3367 0.0790 0.0336 0.069 2.181 1.611 51.612 0.246 7.165 14.156 0.16 83839. 0.5271 6.33 0.1671 0.3802 0.0768 0.0338 0.070 2.192 1.567 51.873 0.248 6.972 13.704 0.16 83924. 0.5034 7.23 0.1910 0.4205 0.0746 0.0339 0.070 2.198 1.521 52.007 0.248 6.764 13.262 0.16 84014. 0.4798 8.14 0.2148 0.4577 0.0721 0.0338 0.070 2.197 1.471 51.996 0.248 6.542 12.829 0.16 84111. 0.4564 9.04 0.2387 0.4917 0.0695 0.0337 0.069 2.190 1.417 51.822 0.247 6.304 12.405 0.16 84214. 0.4333 9.95 0.2626 0.5227 0.0667 0.0335 0.069 2.175 1.361 51.472 0.246 6.052 11.989 0.16 84323. 0.4103 10.85 0.2864 0.5509 0.0638 0.0332 0.068 2.153 1.301 50.937 0.243 5.785 11.582 0.16 84438. 0.3875 11.75 0.3103 0.5761 0.0607 0.0327 0.067 2.122 1.238 50.211 0.240 5.506 11.181 0.16 84560. 0.3649 12.66 0.3342 0.5985 0.0575 0.0321 0.066 2.083 1.172 49.293 0.235 5.214 10.786 0.16 84688. 0.3426 13.56 0.3580 0.6180 0.0541 0.0314 0.065 2.036 1.104 48.179 0.230 4.911 10.394 0.16 84822. 0.3204 14.47 0.3819 0.6344 0.0507 0.0305 0.063 1.981 1.034 46.867 0.224 4.598 10.004 0.16 84964. 0.2984 15.37 0.4058 0.6477 0.0471 0.0295 0.061 1.917 0.961 45.356 0.217 4.276 9.613 0.16 85111. 0.2765 16.27 0.4297 0.6576 0.0435 0.0284 0.059 1.844 0.887 43.643 0.208 3.945 9.217 0.16 85266. 0.2547 17.18 0.4535 0.6638 0.0398 0.0272 0.056 1.763 0.811 41.726 0.199 3.607 8.814 0.16 85427. 0.2329 18.08 0.4774 0.6658 0.0360 0.0258 0.053 1.674 0.733 39.605 0.189 3.262 8.398 0.16 85595. 0.2110 18.99 0.5013 0.6628 0.0321 0.0243 0.050 1.575 0.654 37.276 0.178 2.911 7.962 0.16 85770. 0.1890 19.89 0.5251 0.6538 0.0282 0.0226 0.047 1.468 0.574 34.741 0.166 2.554 7.497 0.16 85951. 0.1667 20.80 0.5490 0.6372 0.0242 0.0208 0.043 1.352 0.493 32.001 0.153 2.193 6.989 0.16 86140. 0.1440 21.70 0.5729 0.6105 0.0202 0.0189 0.039 1.228 0.411 29.058 0.139 1.829 6.418 0.16 86335. 0.1207 22.60 0.5967 0.5700 0.0161 0.0169 0.035 1.095 0.329 25.917 0.124 1.462 5.752 0.16 86537. 0.0967 23.51 0.6206 0.5089 0.0121 0.0147 0.030 0.954 0.246 22.585 0.108 1.094 4.938 0.16 86746. 0.0718 24.41 0.6445 0.4152 0.0080 0.0124 0.026 0.806 0.163 19.074 0.091 0.726 3.880 0.16 86961. 0.0460 25.32 0.6683 0.2643 0.0040 0.0100 0.021 0.651 0.081 15.395 0.074 0.360 2.381 0.16 87183. 0.0199 26.22 0.6922 -0.0058 -0.0001 0.0075 0.015 0.488 -0.001 11.539 0.055 -0.006 -0.051 0.16 87402. 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 0.0894 0.0301 0.209 4.401 4.101 156.215 0.497 18.240 11.906 0.24 125163. 0.7073 1.36 0.0239 0.0688 0.0880 0.0306 0.213 4.470 4.039 158.656 0.505 17.966 11.547 0.24 125243. 0.6808 2.72 0.0478 0.1334 0.0866 0.0310 0.216 4.535 3.972 160.974 0.512 17.668 11.192 0.24 125330. 0.6544 4.08 0.0718 0.1939 0.0850 0.0315 0.219 4.596 3.900 163.123 0.519 17.346 10.843 0.24 125425. 0.6282 5.44 0.0957 0.2503 0.0833 0.0318 0.221 4.650 3.821 165.056 0.525 16.997 10.501 0.24 125528. 0.6022 6.80 0.1196 0.3029 0.0814 0.0322 0.224 4.697 3.737 166.723 0.531 16.620 10.165 0.24 125638. 0.5765 8.16 0.1435 0.3518 0.0794 0.0324 0.225 4.735 3.645 168.070 0.535 16.214 9.838 0.24 125758. 0.5511 9.52 0.1675 0.3970 0.0773 0.0326 0.227 4.763 3.547 169.039 0.538 15.777 9.518 0.24 125885. 0.5259 10.87 0.1914 0.4389 0.0750 0.0327 0.227 4.777 3.442 169.570 0.540 15.308 9.206 0.24 126022. 0.5010 12.23 0.2153 0.4774 0.0725 0.0327 0.227 4.778 3.329 169.601 0.540 14.805 8.902 0.24 126167. 0.4765 13.59 0.2392 0.5128 0.0699 0.0326 0.227 4.763 3.208 169.073 0.538 14.268 8.606 0.24 126322. 0.4522 14.95 0.2632 0.5452 0.0671 0.0324 0.225 4.732 3.079 167.939 0.535 13.697 8.317 0.24 126487. 0.4282 16.31 0.2871 0.5746 0.0641 0.0320 0.223 4.682 2.944 166.166 0.529 13.094 8.035 0.24 126660. 0.4045 17.67 0.3110 0.6012 0.0610 0.0316 0.220 4.613 2.801 163.736 0.521 12.460 7.760 0.24 126844. 0.3810 19.03 0.3349 0.6249 0.0578 0.0310 0.215 4.526 2.653 160.635 0.511 11.799 7.490 0.24 127037. 0.3579 20.39 0.3589 0.6458 0.0544 0.0303 0.210 4.419 2.498 156.857 0.499 11.113 7.224 0.24 127240. 0.3350 21.75 0.3828 0.6638 0.0510 0.0294 0.204 4.294 2.339 152.393 0.485 10.404 6.961 0.24 127452. 0.3124 23.11 0.4067 0.6788 0.0474 0.0284 0.197 4.148 2.175 147.233 0.469 9.674 6.700 0.24 127675. 0.2899 24.47 0.4306 0.6905 0.0437 0.0273 0.190 3.983 2.006 141.371 0.450 8.925 6.437 0.24 127908. 0.2675 25.83 0.4546 0.6988 0.0400 0.0260 0.181 3.798 1.834 134.800 0.429 8.159 6.172 0.24 128151. 0.2452 27.19 0.4785 0.7032 0.0361 0.0246 0.171 3.593 1.659 127.512 0.406 7.377 5.900 0.24 128404. 0.2229 28.55 0.5024 0.7029 0.0322 0.0230 0.160 3.367 1.480 119.504 0.380 6.582 5.616 0.24 128667. 0.2004 29.91 0.5263 0.6970 0.0283 0.0214 0.149 3.121 1.298 110.775 0.353 5.775 5.316 0.24 128941. 0.1777 31.27 0.5503 0.6839 0.0243 0.0195 0.136 2.855 1.115 101.329 0.323 4.958 4.989 0.24 129224. 0.1545 32.62 0.5742 0.6611 0.0202 0.0176 0.122 2.569 0.929 91.176 0.290 4.133 4.622 0.24 129519. 0.1307 33.98 0.5981 0.6246 0.0162 0.0155 0.108 2.263 0.742 80.332 0.256 3.303 4.192 0.24 129823. 0.1060 35.34 0.6220 0.5670 0.0121 0.0133 0.092 1.939 0.555 68.825 0.219 2.470 3.659 0.24 130138. 0.0800 36.70 0.6460 0.4739 0.0080 0.0109 0.076 1.597 0.368 56.692 0.180 1.638 2.946 0.24 130463. 0.0524 38.06 0.6699 0.3133 0.0040 0.0085 0.059 1.239 0.182 43.980 0.140 0.810 1.878 0.24 130796. 0.0235 39.42 0.6938 -0.0104 -0.0001 0.0059 0.041 0.862 -0.004 30.602 0.097 -0.018 -0.060 0.24 131119. 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 0.0899 0.0295 0.487 7.671 7.338 363.016 0.867 32.639 9.168 0.32 166877. 0.7286 1.82 0.0240 0.0707 0.0886 0.0300 0.495 7.797 7.229 368.978 0.881 32.153 8.886 0.32 166984. 0.7009 3.63 0.0479 0.1371 0.0871 0.0305 0.502 7.916 7.110 374.646 0.894 31.625 8.608 0.32 167101. 0.6734 5.45 0.0719 0.1991 0.0856 0.0309 0.509 8.028 6.981 379.907 0.907 31.051 8.335 0.32 167228. 0.6461 7.26 0.0959 0.2569 0.0839 0.0313 0.516 8.128 6.841 384.649 0.918 30.430 8.067 0.32 167365. 0.6190 9.08 0.1199 0.3107 0.0820 0.0316 0.521 8.215 6.690 388.751 0.928 29.759 7.806 0.32 167514. 0.5924 10.90 0.1438 0.3607 0.0800 0.0319 0.526 8.285 6.528 392.081 0.936 29.034 7.551 0.32 167673. 0.5660 12.71 0.1678 0.4070 0.0779 0.0321 0.529 8.336 6.352 394.499 0.942 28.254 7.303 0.32 167844. 0.5400 14.53 0.1918 0.4498 0.0755 0.0322 0.531 8.365 6.164 395.860 0.945 27.416 7.062 0.32 168027. 0.5144 16.34 0.2158 0.4893 0.0731 0.0322 0.531 8.368 5.961 396.014 0.945 26.516 6.828 0.32 168223. 0.4891 18.16 0.2397 0.5255 0.0704 0.0321 0.529 8.343 5.745 394.819 0.943 25.555 6.600 0.32 168430. 0.4641 19.98 0.2637 0.5587 0.0676 0.0319 0.526 8.287 5.515 392.157 0.936 24.532 6.379 0.32 168650. 0.4395 21.79 0.2877 0.5889 0.0646 0.0316 0.520 8.198 5.272 387.950 0.926 23.451 6.164 0.32 168883. 0.4152 23.61 0.3116 0.6163 0.0615 0.0311 0.512 8.075 5.017 382.150 0.912 22.316 5.955 0.32 169128. 0.3913 25.43 0.3356 0.6409 0.0582 0.0305 0.503 7.918 4.751 374.727 0.895 21.130 5.750 0.32 169387. 0.3677 27.24 0.3596 0.6627 0.0548 0.0298 0.490 7.727 4.474 365.660 0.873 19.900 5.549 0.32 169659. 0.3444 29.06 0.3836 0.6818 0.0513 0.0289 0.476 7.500 4.188 354.927 0.847 18.628 5.352 0.32 169944. 0.3213 30.87 0.4075 0.6979 0.0477 0.0279 0.459 7.237 3.894 342.508 0.818 17.319 5.156 0.32 170242. 0.2985 32.69 0.4315 0.7109 0.0440 0.0267 0.440 6.939 3.592 328.383 0.784 15.976 4.961 0.32 170554. 0.2758 34.51 0.4555 0.7207 0.0402 0.0254 0.419 6.604 3.283 312.534 0.746 14.602 4.764 0.32 170879. 0.2532 36.32 0.4795 0.7267 0.0364 0.0240 0.396 6.232 2.968 294.945 0.704 13.200 4.564 0.32 171218. 0.2306 38.14 0.5034 0.7283 0.0324 0.0224 0.370 5.824 2.647 275.606 0.658 11.773 4.356 0.32 171570. 0.2079 39.95 0.5274 0.7246 0.0285 0.0207 0.341 5.378 2.321 254.517 0.608 10.326 4.137 0.32 171936. 0.1849 41.77 0.5514 0.7141 0.0244 0.0189 0.311 4.896 1.992 231.685 0.553 8.860 3.900 0.32 172316. 0.1615 43.59 0.5753 0.6943 0.0203 0.0169 0.278 4.377 1.659 207.134 0.494 7.380 3.633 0.32 172710. 0.1373 45.40 0.5993 0.6610 0.0162 0.0147 0.243 3.823 1.324 180.908 0.432 5.891 3.321 0.32 173118. 0.1121 47.22 0.6233 0.6065 0.0121 0.0125 0.205 3.235 0.989 153.072 0.365 4.398 2.930 0.32 173539. 0.0855 49.03 0.6473 0.5149 0.0080 0.0101 0.166 2.614 0.653 123.721 0.295 2.906 2.395 0.32 173974. 0.0568 50.85 0.6712 0.3479 0.0039 0.0076 0.125 1.964 0.320 92.968 0.222 1.423 1.560 0.32 174420. 0.0259 52.67 0.6952 -0.0269 -0.0002 0.0049 0.081 1.277 -0.016 60.416 0.144 -0.069 -0.117 0.33 174837. 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 0.0907 0.0293 0.944 11.894 11.560 703.601 1.344 51.420 7.452 0.40 208584. 0.7434 2.27 0.0240 0.0719 0.0894 0.0298 0.960 12.096 11.390 715.549 1.367 50.665 7.220 0.40 208719. 0.7149 4.54 0.0480 0.1392 0.0879 0.0303 0.975 12.288 11.205 726.914 1.388 49.842 6.992 0.40 208865. 0.6867 6.81 0.0719 0.2021 0.0863 0.0307 0.989 12.467 11.004 737.472 1.408 48.948 6.768 0.40 209025. 0.6587 9.08 0.0959 0.2608 0.0846 0.0311 1.002 12.628 10.786 747.000 1.427 47.978 6.549 0.40 209197. 0.6311 11.35 0.1199 0.3153 0.0828 0.0315 1.013 12.767 10.550 755.254 1.442 46.928 6.336 0.40 209383. 0.6038 13.62 0.1439 0.3660 0.0808 0.0317 1.022 12.881 10.295 761.976 1.455 45.794 6.128 0.40 209583. 0.5769 15.89 0.1678 0.4129 0.0786 0.0319 1.028 12.964 10.021 766.889 1.465 44.572 5.927 0.40 209797. 0.5504 18.16 0.1918 0.4563 0.0763 0.0321 1.032 13.011 9.725 769.701 1.470 43.257 5.731 0.40 210027. 0.5243 20.43 0.2158 0.4964 0.0738 0.0321 1.033 13.018 9.408 770.118 1.471 41.845 5.541 0.40 210271. 0.4986 22.71 0.2398 0.5332 0.0711 0.0320 1.030 12.980 9.068 767.858 1.467 40.336 5.357 0.40 210531. 0.4732 24.98 0.2637 0.5670 0.0683 0.0318 1.023 12.893 8.707 762.684 1.457 38.728 5.178 0.40 210807. 0.4483 27.25 0.2877 0.5978 0.0653 0.0314 1.012 12.753 8.325 754.436 1.441 37.028 5.005 0.40 211098. 0.4236 29.52 0.3117 0.6258 0.0622 0.0310 0.996 12.560 7.923 743.018 1.419 35.241 4.836 0.40 211406. 0.3994 31.79 0.3357 0.6511 0.0589 0.0303 0.977 12.313 7.503 728.372 1.391 33.374 4.672 0.40 211730. 0.3755 34.06 0.3596 0.6737 0.0554 0.0296 0.953 12.010 7.068 710.453 1.357 31.436 4.512 0.40 212070. 0.3519 36.33 0.3836 0.6935 0.0519 0.0287 0.924 11.651 6.617 689.219 1.316 29.433 4.355 0.40 212427. 0.3286 38.60 0.4076 0.7106 0.0483 0.0277 0.891 11.235 6.153 664.631 1.269 27.370 4.199 0.40 212800. 0.3056 40.87 0.4316 0.7247 0.0445 0.0265 0.854 10.762 5.677 636.647 1.216 25.252 4.045 0.40 213191. 0.2827 43.14 0.4556 0.7356 0.0407 0.0252 0.812 10.231 5.190 605.231 1.156 23.086 3.890 0.40 213598. 0.2600 45.41 0.4795 0.7430 0.0368 0.0238 0.765 9.642 4.693 570.354 1.089 20.876 3.732 0.40 214022. 0.2372 47.68 0.5035 0.7463 0.0329 0.0222 0.713 8.993 4.188 531.993 1.016 18.627 3.570 0.40 214463. 0.2144 49.95 0.5275 0.7446 0.0288 0.0204 0.657 8.286 3.674 490.148 0.936 16.343 3.400 0.40 214921. 0.1912 52.22 0.5515 0.7364 0.0247 0.0185 0.597 7.520 3.155 444.834 0.850 14.032 3.217 0.40 215397. 0.1676 54.49 0.5754 0.7194 0.0206 0.0165 0.531 6.696 2.630 396.098 0.756 11.697 3.011 0.40 215889. 0.1433 56.76 0.5994 0.6895 0.0165 0.0143 0.461 5.816 2.102 344.025 0.657 9.348 2.771 0.40 216399. 0.1178 59.03 0.6234 0.6390 0.0123 0.0120 0.387 4.881 1.572 288.747 0.551 6.991 2.469 0.40 216926. 0.0908 61.30 0.6474 0.5515 0.0082 0.0096 0.309 3.896 1.043 230.452 0.440 4.638 2.052 0.40 217469. 0.0615 63.57 0.6713 0.3853 0.0040 0.0071 0.227 2.863 0.516 169.366 0.323 2.296 1.383 0.41 218028. 0.0291 65.84 0.6953 -0.0166 -0.0001 0.0044 0.140 1.770 -0.013 104.682 0.200 -0.059 -0.057 0.41 218547. 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 0.0916 0.0293 1.632 17.141 16.816 1216.766 1.937 74.799 6.269 0.48 250283. 0.7542 2.72 0.0240 0.0725 0.0903 0.0298 1.660 17.439 16.574 1237.975 1.970 73.720 6.072 0.48 250445. 0.7253 5.45 0.0479 0.1404 0.0888 0.0303 1.687 17.724 16.309 1258.153 2.002 72.542 5.879 0.48 250621. 0.6966 8.17 0.0719 0.2039 0.0873 0.0308 1.712 17.988 16.020 1276.903 2.032 71.258 5.691 0.48 250813. 0.6682 10.90 0.0959 0.2630 0.0856 0.0312 1.735 18.226 15.707 1293.831 2.059 69.864 5.506 0.48 251020. 0.6402 13.62 0.1198 0.3180 0.0837 0.0315 1.755 18.433 15.367 1308.512 2.083 68.353 5.327 0.48 251244. 0.6126 16.34 0.1438 0.3691 0.0817 0.0318 1.771 18.602 15.000 1320.488 2.102 66.718 5.152 0.48 251485. 0.5854 19.07 0.1678 0.4165 0.0796 0.0320 1.783 18.726 14.603 1329.274 2.116 64.953 4.983 0.48 251743. 0.5586 21.79 0.1918 0.4603 0.0772 0.0322 1.789 18.797 14.175 1334.361 2.124 63.052 4.818 0.48 252019. 0.5322 24.51 0.2157 0.5007 0.0747 0.0322 1.791 18.809 13.716 1335.229 2.125 61.010 4.659 0.48 252313. 0.5063 27.24 0.2397 0.5380 0.0720 0.0321 1.785 18.755 13.225 1331.383 2.119 58.823 4.505 0.48 252626. 0.4807 29.96 0.2637 0.5722 0.0692 0.0319 1.773 18.629 12.701 1322.406 2.105 56.493 4.356 0.48 252958. 0.4555 32.69 0.2876 0.6035 0.0662 0.0315 1.754 18.426 12.146 1308.008 2.082 54.026 4.212 0.48 253308. 0.4306 35.41 0.3116 0.6321 0.0630 0.0311 1.727 18.144 11.563 1288.024 2.050 51.431 4.072 0.48 253678. 0.4062 38.13 0.3356 0.6579 0.0597 0.0304 1.693 17.783 10.953 1262.347 2.009 48.719 3.936 0.48 254067. 0.3821 40.86 0.3595 0.6811 0.0562 0.0297 1.651 17.340 10.320 1230.904 1.959 45.902 3.803 0.48 254476. 0.3584 43.58 0.3835 0.7017 0.0527 0.0288 1.601 16.815 9.665 1193.623 1.900 42.988 3.672 0.48 254905. 0.3350 46.30 0.4075 0.7195 0.0490 0.0277 1.543 16.206 8.990 1150.435 1.831 39.986 3.544 0.48 255354. 0.3118 49.03 0.4315 0.7345 0.0452 0.0266 1.477 15.514 8.297 1101.270 1.753 36.905 3.417 0.48 255822. 0.2888 51.75 0.4554 0.7465 0.0413 0.0252 1.403 14.736 7.588 1046.066 1.665 33.752 3.290 0.48 256311. 0.2659 54.48 0.4794 0.7551 0.0374 0.0237 1.321 13.873 6.865 984.769 1.567 30.534 3.162 0.48 256820. 0.2430 57.20 0.5034 0.7598 0.0334 0.0221 1.230 12.923 6.128 917.344 1.460 27.258 3.030 0.48 257350. 0.2201 59.92 0.5273 0.7598 0.0293 0.0203 1.132 11.886 5.380 843.785 1.343 23.931 2.892 0.48 257900. 0.1968 62.65 0.5513 0.7536 0.0252 0.0184 1.025 10.764 4.623 764.120 1.216 20.563 2.744 0.48 258470. 0.1731 65.37 0.5753 0.7392 0.0210 0.0164 0.910 9.557 3.858 678.431 1.080 17.161 2.579 0.48 259062. 0.1486 68.10 0.5992 0.7125 0.0168 0.0141 0.787 8.267 3.088 586.865 0.934 13.736 2.387 0.48 259673. 0.1230 70.82 0.6232 0.6659 0.0126 0.0118 0.657 6.898 2.316 489.653 0.779 10.299 2.145 0.49 260305. 0.0958 73.54 0.6472 0.5831 0.0084 0.0093 0.519 5.453 1.544 387.125 0.616 6.866 1.809 0.49 260957. 0.0659 76.27 0.6711 0.4207 0.0042 0.0067 0.375 3.940 0.776 279.682 0.445 3.451 1.258 0.49 261627. 0.0325 78.99 0.6951 0.0043 0.0000 0.0040 0.223 2.340 0.005 166.109 0.264 0.020 0.013 0.49 262257. 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 0.0927 0.0296 2.611 23.509 23.171 1947.015 2.656 103.066 5.398 0.56 291970. 0.7623 3.18 0.0240 0.0730 0.0914 0.0301 2.658 23.930 22.844 1981.829 2.704 101.611 5.228 0.56 292160. 0.7331 6.37 0.0480 0.1413 0.0900 0.0306 2.702 24.330 22.486 2014.941 2.749 100.017 5.062 0.56 292367. 0.7042 9.55 0.0720 0.2051 0.0884 0.0311 2.743 24.701 22.095 2045.710 2.791 98.276 4.899 0.56 292592. 0.6756 12.73 0.0960 0.2646 0.0867 0.0315 2.781 25.036 21.668 2073.478 2.829 96.380 4.740 0.56 292836. 0.6473 15.91 0.1200 0.3199 0.0849 0.0318 2.813 25.327 21.205 2097.551 2.861 94.320 4.585 0.56 293098. 0.6195 19.10 0.1441 0.3713 0.0829 0.0321 2.839 25.564 20.703 2117.182 2.888 92.086 4.435 0.56 293381. 0.5921 22.28 0.1681 0.4190 0.0807 0.0324 2.859 25.738 20.160 2131.585 2.908 89.671 4.290 0.56 293684. 0.5651 25.46 0.1921 0.4631 0.0783 0.0325 2.870 25.839 19.574 2139.930 2.919 87.064 4.149 0.56 294008. 0.5385 28.65 0.2161 0.5039 0.0758 0.0325 2.872 25.856 18.943 2141.376 2.921 84.259 4.012 0.56 294354. 0.5123 31.83 0.2401 0.5415 0.0731 0.0324 2.863 25.781 18.267 2135.113 2.913 81.252 3.881 0.56 294721. 0.4866 35.01 0.2641 0.5761 0.0702 0.0322 2.844 25.604 17.546 2120.461 2.893 78.044 3.753 0.56 295110. 0.4612 38.20 0.2881 0.6078 0.0672 0.0318 2.812 25.320 16.781 2096.951 2.861 74.642 3.630 0.56 295521. 0.4362 41.38 0.3121 0.6368 0.0639 0.0313 2.768 24.926 15.976 2064.312 2.816 71.062 3.510 0.56 295955. 0.4116 44.56 0.3361 0.6631 0.0606 0.0307 2.712 24.420 15.135 2022.382 2.759 67.319 3.394 0.56 296412. 0.3874 47.74 0.3601 0.6868 0.0571 0.0299 2.643 23.800 14.260 1971.045 2.689 63.427 3.281 0.56 296892. 0.3635 50.93 0.3841 0.7079 0.0534 0.0290 2.562 23.065 13.354 1910.198 2.606 59.399 3.171 0.56 297394. 0.3400 54.11 0.4081 0.7264 0.0497 0.0279 2.467 22.214 12.421 1839.729 2.510 55.249 3.062 0.56 297920. 0.3166 57.29 0.4322 0.7422 0.0459 0.0267 2.360 21.246 11.463 1759.529 2.400 50.987 2.955 0.56 298470. 0.2935 60.48 0.4562 0.7550 0.0420 0.0253 2.239 20.159 10.482 1669.502 2.278 46.624 2.848 0.56 299043. 0.2705 63.66 0.4802 0.7646 0.0379 0.0238 2.105 18.952 9.481 1569.564 2.141 42.170 2.740 0.56 299639. 0.2475 66.84 0.5042 0.7704 0.0339 0.0222 1.957 17.625 8.461 1459.660 1.991 37.635 2.629 0.56 300260. 0.2244 70.02 0.5282 0.7717 0.0297 0.0203 1.797 16.177 7.425 1339.779 1.828 33.029 2.514 0.56 300904. 0.2010 73.21 0.5522 0.7671 0.0255 0.0184 1.623 14.610 6.377 1209.974 1.651 28.363 2.390 0.56 301572. 0.1771 76.39 0.5762 0.7545 0.0213 0.0163 1.435 12.924 5.317 1070.374 1.460 23.650 2.253 0.56 302264. 0.1524 79.57 0.6002 0.7299 0.0170 0.0140 1.235 11.123 4.250 921.226 1.257 18.904 2.092 0.57 302980. 0.1266 82.76 0.6242 0.6858 0.0127 0.0116 1.023 9.212 3.179 762.909 1.041 14.142 1.890 0.57 303720. 0.0989 85.94 0.6482 0.6049 0.0084 0.0090 0.799 7.196 2.110 595.968 0.813 9.383 1.605 0.57 304484. 0.0684 89.12 0.6722 0.4399 0.0042 0.0064 0.565 5.084 1.045 421.062 0.574 4.649 1.126 0.57 305268. 0.0338 92.31 0.6962 -0.0255 -0.0001 0.0036 0.315 2.833 -0.033 234.618 0.320 -0.145 -0.063 0.57 305961. 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 0.0941 0.0300 3.952 31.139 30.711 2947.315 3.518 136.602 4.726 0.63 333643. 0.7684 3.64 0.0240 0.0731 0.0928 0.0305 4.025 31.710 30.291 3001.327 3.583 134.733 4.578 0.63 333861. 0.7391 7.28 0.0481 0.1415 0.0914 0.0311 4.094 32.253 29.828 3052.726 3.644 132.676 4.432 0.63 334099. 0.7101 10.92 0.0721 0.2054 0.0899 0.0315 4.158 32.758 29.321 3100.484 3.701 130.420 4.289 0.63 334357. 0.6814 14.57 0.0961 0.2650 0.0882 0.0320 4.216 33.213 28.767 3143.575 3.752 127.955 4.151 0.63 334637. 0.6531 18.21 0.1202 0.3205 0.0863 0.0324 4.266 33.607 28.162 3180.920 3.797 125.266 4.016 0.64 334939. 0.6252 21.85 0.1442 0.3721 0.0843 0.0327 4.307 33.929 27.505 3211.372 3.833 122.344 3.885 0.64 335264. 0.5977 25.49 0.1682 0.4200 0.0821 0.0329 4.336 34.165 26.793 3233.710 3.860 119.174 3.758 0.64 335613. 0.5707 29.13 0.1923 0.4643 0.0797 0.0330 4.354 34.302 26.022 3246.668 3.875 115.747 3.635 0.64 335986. 0.5441 32.77 0.2163 0.5053 0.0772 0.0330 4.357 34.326 25.191 3248.964 3.878 112.051 3.517 0.64 336383. 0.5179 36.41 0.2403 0.5431 0.0745 0.0329 4.344 34.225 24.299 3239.365 3.867 108.082 3.402 0.64 336805. 0.4920 40.06 0.2644 0.5780 0.0715 0.0327 4.314 33.987 23.345 3216.811 3.840 103.839 3.292 0.64 337253. 0.4666 43.70 0.2884 0.6101 0.0684 0.0324 4.265 33.604 22.333 3180.590 3.797 99.336 3.185 0.64 337726. 0.4416 47.34 0.3124 0.6395 0.0652 0.0318 4.198 33.072 21.266 3130.288 3.737 94.589 3.081 0.64 338224. 0.4169 50.98 0.3365 0.6662 0.0617 0.0312 4.111 32.390 20.149 3065.676 3.659 89.621 2.981 0.64 338749. 0.3926 54.62 0.3605 0.6905 0.0582 0.0304 4.005 31.554 18.986 2986.596 3.565 84.451 2.883 0.64 339300. 0.3686 58.26 0.3845 0.7122 0.0545 0.0294 3.879 30.564 17.783 2892.906 3.453 79.099 2.788 0.64 339877. 0.3449 61.90 0.4086 0.7313 0.0507 0.0283 3.734 29.419 16.542 2784.451 3.324 73.580 2.695 0.64 340481. 0.3215 65.55 0.4326 0.7478 0.0468 0.0271 3.569 28.115 15.267 2661.079 3.176 67.910 2.602 0.64 341111. 0.2983 69.19 0.4566 0.7614 0.0428 0.0257 3.383 26.653 13.962 2522.644 3.011 62.102 2.510 0.64 341769. 0.2752 72.83 0.4807 0.7720 0.0387 0.0241 3.177 25.029 12.628 2369.027 2.828 56.171 2.418 0.64 342453. 0.2521 76.47 0.5047 0.7789 0.0345 0.0224 2.950 23.245 11.270 2200.150 2.626 50.129 2.323 0.64 343165. 0.2288 80.11 0.5287 0.7815 0.0303 0.0205 2.703 21.300 9.890 2015.999 2.406 43.990 2.225 0.64 343903. 0.2053 83.75 0.5528 0.7784 0.0260 0.0185 2.436 19.193 8.491 1816.653 2.168 37.770 2.120 0.64 344669. 0.1813 87.40 0.5768 0.7677 0.0217 0.0163 2.149 16.929 7.078 1602.316 1.913 31.485 2.004 0.65 345463. 0.1564 91.04 0.6008 0.7454 0.0173 0.0140 1.842 14.510 5.655 1373.360 1.639 25.153 1.868 0.65 346283. 0.1303 94.68 0.6249 0.7039 0.0130 0.0115 1.516 11.943 4.226 1130.376 1.349 18.798 1.696 0.65 347131. 0.1023 98.32 0.6489 0.6258 0.0086 0.0089 1.172 9.236 2.798 874.207 1.044 12.447 1.452 0.65 348006. 0.0713 101.96 0.6729 0.4609 0.0042 0.0062 0.812 6.401 1.377 605.870 0.723 6.126 1.031 0.65 348903. 0.0355 105.60 0.6970 -0.0536 -0.0002 0.0032 0.424 3.339 -0.081 315.990 0.377 -0.359 -0.116 0.65 349608. 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 0.0957 0.0308 5.791 40.553 39.542 4318.101 4.582 175.885 4.154 0.71 375297. 0.7663 4.11 0.0241 0.0726 0.0945 0.0314 5.892 41.262 39.025 4393.594 4.662 173.582 4.029 0.71 375544. 0.7384 8.22 0.0482 0.1407 0.0931 0.0319 5.988 41.936 38.451 4465.421 4.738 171.031 3.906 0.71 375813. 0.7105 12.33 0.0723 0.2045 0.0916 0.0324 6.078 42.563 37.819 4532.159 4.809 168.217 3.785 0.71 376106. 0.6829 16.43 0.0964 0.2642 0.0899 0.0328 6.158 43.128 37.123 4592.343 4.873 165.122 3.666 0.71 376424. 0.6554 20.54 0.1205 0.3198 0.0880 0.0332 6.228 43.618 36.360 4644.425 4.928 161.730 3.551 0.71 376767. 0.6282 24.65 0.1446 0.3716 0.0860 0.0335 6.285 44.015 35.527 4686.732 4.973 158.026 3.438 0.71 377136. 0.6012 28.76 0.1687 0.4197 0.0838 0.0337 6.326 44.304 34.621 4717.483 5.005 153.993 3.329 0.72 377532. 0.5746 32.87 0.1928 0.4643 0.0814 0.0338 6.349 44.466 33.637 4734.781 5.024 149.616 3.222 0.72 377956. 0.5483 36.98 0.2169 0.5056 0.0789 0.0338 6.352 44.484 32.573 4736.687 5.026 144.883 3.119 0.72 378407. 0.5223 41.08 0.2410 0.5438 0.0761 0.0337 6.331 44.340 31.427 4721.302 5.009 139.786 3.019 0.72 378887. 0.4966 45.19 0.2651 0.5790 0.0731 0.0335 6.285 44.017 30.199 4686.983 4.973 134.325 2.922 0.72 379395. 0.4712 49.30 0.2892 0.6114 0.0700 0.0331 6.212 43.506 28.893 4632.574 4.915 128.516 2.829 0.72 379933. 0.4461 53.41 0.3133 0.6412 0.0666 0.0326 6.112 42.800 27.514 4557.381 4.836 122.384 2.738 0.72 380499. 0.4214 57.52 0.3374 0.6684 0.0631 0.0319 5.982 41.895 26.070 4461.021 4.733 115.957 2.651 0.72 381095. 0.3970 61.63 0.3615 0.6931 0.0595 0.0310 5.824 40.789 24.565 4343.242 4.608 109.263 2.565 0.72 381720. 0.3730 65.74 0.3856 0.7153 0.0557 0.0300 5.637 39.480 23.005 4203.848 4.460 102.326 2.482 0.72 382375. 0.3493 69.84 0.4098 0.7350 0.0518 0.0289 5.421 37.966 21.396 4042.661 4.289 95.169 2.401 0.72 383060. 0.3258 73.95 0.4339 0.7522 0.0478 0.0276 5.176 36.246 19.742 3859.471 4.095 87.811 2.320 0.72 383775. 0.3024 78.06 0.4580 0.7666 0.0437 0.0261 4.900 34.317 18.047 3654.081 3.877 80.271 2.240 0.72 384520. 0.2792 82.17 0.4821 0.7780 0.0395 0.0245 4.595 32.178 16.314 3426.317 3.635 72.567 2.160 0.72 385296. 0.2559 86.28 0.5062 0.7859 0.0352 0.0227 4.259 29.828 14.549 3176.082 3.370 64.715 2.078 0.72 386102. 0.2325 90.39 0.5303 0.7896 0.0309 0.0207 3.893 27.267 12.755 2903.373 3.081 56.733 1.993 0.72 386939. 0.2088 94.49 0.5544 0.7878 0.0265 0.0186 3.498 24.496 10.936 2608.336 2.768 48.643 1.902 0.73 387806. 0.1845 98.60 0.5785 0.7784 0.0220 0.0164 3.073 21.519 9.097 2291.326 2.431 40.464 1.801 0.73 388705. 0.1593 102.71 0.6026 0.7576 0.0175 0.0140 2.619 18.341 7.244 1952.988 2.072 32.222 1.682 0.73 389634. 0.1329 106.82 0.6267 0.7173 0.0130 0.0114 2.138 14.973 5.384 1594.371 1.692 23.948 1.532 0.73 390593. 0.1043 110.93 0.6508 0.6387 0.0085 0.0087 1.632 11.429 3.524 1217.000 1.291 15.676 1.313 0.73 391583. 0.0723 115.04 0.6749 0.4651 0.0041 0.0059 1.103 7.727 1.673 822.755 0.873 7.442 0.922 0.73 392598. 0.0350 119.15 0.6990 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 0.0976 0.0336 8.646 54.497 49.777 6447.615 6.157 221.407 3.502 0.79 416926. 0.7248 4.55 0.0240 0.0681 0.0964 0.0340 8.760 55.212 49.173 6532.243 6.238 218.721 3.414 0.79 417199. 0.7024 9.10 0.0481 0.1328 0.0951 0.0344 8.864 55.870 48.497 6610.116 6.312 215.717 3.328 0.79 417498. 0.6799 13.65 0.0721 0.1941 0.0936 0.0348 8.957 56.457 47.746 6679.488 6.378 212.373 3.242 0.79 417824. 0.6573 18.21 0.0961 0.2520 0.0920 0.0351 9.037 56.957 46.912 6738.674 6.435 208.665 3.158 0.79 418177. 0.6345 22.76 0.1202 0.3067 0.0902 0.0353 9.100 57.356 45.992 6785.937 6.480 204.572 3.074 0.79 418559. 0.6116 27.31 0.1442 0.3582 0.0882 0.0355 9.145 57.639 44.980 6819.431 6.512 200.071 2.992 0.79 418970. 0.5887 31.86 0.1682 0.4065 0.0860 0.0356 9.169 57.790 43.872 6837.181 6.529 195.143 2.910 0.79 419411. 0.5656 36.41 0.1922 0.4518 0.0837 0.0356 9.169 57.788 42.664 6837.030 6.529 189.768 2.830 0.79 419883. 0.5424 40.96 0.2163 0.4941 0.0811 0.0355 9.141 57.617 41.351 6816.725 6.509 183.929 2.751 0.80 420386. 0.5191 45.51 0.2403 0.5335 0.0783 0.0353 9.084 57.255 39.932 6773.974 6.469 177.616 2.674 0.80 420920. 0.4957 50.06 0.2643 0.5701 0.0753 0.0349 8.994 56.687 38.406 6706.725 6.404 170.829 2.597 0.80 421486. 0.4722 54.62 0.2884 0.6039 0.0721 0.0344 8.869 55.899 36.778 6613.486 6.315 163.587 2.522 0.80 422084. 0.4488 59.17 0.3124 0.6351 0.0687 0.0338 8.708 54.883 35.054 6493.365 6.201 155.920 2.449 0.80 422714. 0.4253 63.72 0.3364 0.6637 0.0652 0.0330 8.510 53.636 33.243 6345.787 6.060 147.866 2.376 0.80 423376. 0.4019 68.27 0.3605 0.6898 0.0615 0.0321 8.275 52.153 31.354 6170.299 5.892 139.460 2.305 0.80 424071. 0.3786 72.82 0.3845 0.7133 0.0576 0.0311 8.001 50.430 29.392 5966.415 5.698 130.736 2.234 0.80 424799. 0.3554 77.37 0.4085 0.7343 0.0537 0.0299 7.689 48.462 27.366 5733.597 5.475 121.723 2.165 0.80 425559. 0.3322 81.92 0.4326 0.7527 0.0496 0.0285 7.337 46.244 25.280 5471.243 5.225 112.447 2.096 0.80 426353. 0.3091 86.47 0.4566 0.7683 0.0454 0.0270 6.945 43.776 23.141 5179.160 4.946 102.932 2.027 0.80 427179. 0.2860 91.03 0.4806 0.7809 0.0411 0.0253 6.513 41.051 20.953 4856.836 4.638 93.200 1.957 0.80 428039. 0.2628 95.58 0.5046 0.7899 0.0367 0.0235 6.040 38.070 18.721 4504.075 4.301 83.273 1.885 0.80 428933. 0.2393 100.13 0.5287 0.7948 0.0323 0.0215 5.526 34.831 16.451 4120.943 3.935 73.172 1.811 0.80 429860. 0.2155 104.68 0.5527 0.7941 0.0277 0.0193 4.973 31.342 14.146 3708.088 3.541 62.923 1.730 0.81 430821. 0.1909 109.23 0.5767 0.7855 0.0232 0.0170 4.381 27.612 11.815 3266.804 3.120 52.552 1.640 0.81 431815. 0.1654 113.78 0.6008 0.7649 0.0186 0.0146 3.753 23.658 9.462 2798.984 2.673 42.088 1.533 0.81 432844. 0.1384 118.33 0.6248 0.7238 0.0139 0.0120 3.094 19.501 7.097 2307.241 2.203 31.568 1.395 0.81 433905. 0.1090 122.88 0.6488 0.6438 0.0093 0.0093 2.407 15.172 4.729 1794.979 1.714 21.036 1.195 0.81 435000. 0.0762 127.44 0.6729 0.4740 0.0046 0.0066 1.698 10.702 2.368 1266.177 1.209 10.535 0.848 0.81 436123. 0.0383 131.99 0.6969 -0.0094 0.0000 0.0037 0.952 6.003 -0.025 710.259 0.678 -0.113 -0.016 0.81 437119. 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 0.0993 0.0401 13.740 78.727 61.274 10245.703 8.894 272.549 2.713 0.87 458542. 0.6230 5.02 0.0241 0.0586 0.0983 0.0404 13.853 79.374 60.619 10329.923 8.968 269.635 2.662 0.87 458840. 0.6080 10.04 0.0482 0.1149 0.0970 0.0407 13.945 79.902 59.877 10398.686 9.027 266.331 2.612 0.87 459168. 0.5929 15.06 0.0723 0.1692 0.0957 0.0409 14.012 80.286 59.037 10448.719 9.071 262.599 2.563 0.87 459525. 0.5777 20.07 0.0964 0.2213 0.0942 0.0410 14.050 80.505 58.094 10477.193 9.095 258.401 2.515 0.87 459914. 0.5624 25.09 0.1204 0.2715 0.0924 0.0410 14.056 80.539 57.037 10481.641 9.099 253.701 2.468 0.87 460336. 0.5469 30.11 0.1445 0.3198 0.0905 0.0409 14.027 80.373 55.860 10460.024 9.081 248.466 2.422 0.87 460791. 0.5311 35.13 0.1686 0.3661 0.0884 0.0407 13.960 79.991 54.556 10410.324 9.037 242.665 2.377 0.87 461280. 0.5151 40.15 0.1927 0.4105 0.0861 0.0404 13.854 79.384 53.119 10331.259 8.969 236.272 2.332 0.87 461804. 0.4987 45.17 0.2168 0.4529 0.0835 0.0400 13.707 78.539 51.544 10221.347 8.873 229.267 2.287 0.87 462362. 0.4818 50.19 0.2409 0.4933 0.0808 0.0394 13.516 77.445 49.828 10078.940 8.750 221.633 2.242 0.88 462956. 0.4644 55.20 0.2650 0.5317 0.0778 0.0387 13.280 76.091 47.970 9902.688 8.597 213.369 2.197 0.88 463586. 0.4465 60.22 0.2891 0.5681 0.0745 0.0379 12.997 74.472 45.975 9691.991 8.414 204.499 2.152 0.88 464251. 0.4280 65.24 0.3132 0.6022 0.0711 0.0370 12.669 72.590 43.854 9447.027 8.201 195.063 2.106 0.88 464952. 0.4091 70.26 0.3372 0.6342 0.0675 0.0359 12.295 70.448 41.617 9168.249 7.959 185.112 2.059 0.88 465688. 0.3897 75.28 0.3613 0.6638 0.0637 0.0347 11.876 68.049 39.275 8856.051 7.688 174.693 2.011 0.88 466461. 0.3698 80.30 0.3854 0.6911 0.0597 0.0333 11.413 65.393 36.837 8510.490 7.388 163.852 1.963 0.88 467270. 0.3496 85.32 0.4095 0.7159 0.0556 0.0318 10.904 62.480 34.314 8131.320 7.059 152.626 1.914 0.88 468114. 0.3289 90.33 0.4336 0.7380 0.0514 0.0302 10.350 59.304 31.712 7717.973 6.700 141.054 1.864 0.88 468996. 0.3079 95.35 0.4577 0.7574 0.0471 0.0284 9.749 55.859 29.039 7269.680 6.311 129.166 1.812 0.88 469913. 0.2864 100.37 0.4818 0.7731 0.0426 0.0266 9.106 52.175 26.302 6790.186 5.895 116.991 1.757 0.88 470867. 0.2644 105.39 0.5059 0.7845 0.0381 0.0246 8.421 48.251 23.507 6279.577 5.451 104.557 1.698 0.88 471858. 0.2415 110.41 0.5300 0.7875 0.0335 0.0225 7.723 44.250 20.656 5758.782 4.999 91.879 1.627 0.88 472886. 0.2169 115.43 0.5541 0.7811 0.0288 0.0204 6.998 40.095 17.759 5218.122 4.530 78.994 1.544 0.89 473950. 0.1909 120.45 0.5781 0.7635 0.0240 0.0182 6.237 35.735 14.825 4650.710 4.037 65.942 1.446 0.89 475052. 0.1633 125.46 0.6022 0.7287 0.0192 0.0159 5.446 31.205 11.862 4061.063 3.525 52.764 1.325 0.89 476190. 0.1339 130.48 0.6263 0.6671 0.0144 0.0135 4.633 26.547 8.883 3454.965 2.999 39.510 1.166 0.89 477365. 0.1020 135.50 0.6504 0.5598 0.0096 0.0111 3.807 21.815 5.899 2839.080 2.465 26.237 0.942 0.89 478576. 0.0671 140.52 0.6745 0.3681 0.0047 0.0087 2.978 17.062 2.925 2220.454 1.928 13.012 0.598 0.89 479818. 0.0300 145.54 0.6986 -0.0146 -0.0001 0.0062 2.120 12.149 -0.080 1581.128 1.373 -0.354 -0.023 0.89 480959. 0.0000