20x10W (20x10W.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 0.0942 0.0376 0.010 0.610 0.481 7.213 0.069 2.138 30.217 0.08 47529. 0.6145 0.44 0.0231 0.0563 0.0926 0.0379 0.010 0.615 0.472 7.276 0.069 2.100 29.425 0.08 47560. 0.5931 0.87 0.0461 0.1096 0.0908 0.0382 0.010 0.620 0.463 7.332 0.070 2.059 28.638 0.08 47594. 0.5716 1.31 0.0692 0.1599 0.0889 0.0384 0.010 0.624 0.453 7.378 0.070 2.016 27.856 0.08 47630. 0.5501 1.75 0.0922 0.2073 0.0868 0.0386 0.010 0.627 0.443 7.414 0.071 1.969 27.082 0.08 47669. 0.5287 2.18 0.1153 0.2518 0.0846 0.0387 0.010 0.629 0.432 7.439 0.071 1.920 26.315 0.08 47710. 0.5072 2.62 0.1383 0.2935 0.0823 0.0388 0.010 0.630 0.420 7.450 0.071 1.867 25.556 0.08 47754. 0.4858 3.06 0.1614 0.3323 0.0799 0.0388 0.010 0.629 0.407 7.446 0.071 1.811 24.805 0.08 47801. 0.4644 3.49 0.1844 0.3684 0.0773 0.0387 0.010 0.628 0.394 7.426 0.071 1.752 24.061 0.08 47850. 0.4431 3.93 0.2075 0.4018 0.0745 0.0385 0.010 0.625 0.380 7.389 0.071 1.690 23.323 0.08 47903. 0.4218 4.37 0.2305 0.4324 0.0716 0.0382 0.010 0.620 0.365 7.334 0.070 1.625 22.592 0.08 47959. 0.4006 4.80 0.2536 0.4603 0.0686 0.0378 0.010 0.614 0.350 7.260 0.069 1.557 21.865 0.08 48017. 0.3795 5.24 0.2766 0.4855 0.0655 0.0373 0.010 0.606 0.334 7.167 0.068 1.486 21.140 0.08 48079. 0.3585 5.68 0.2997 0.5080 0.0623 0.0367 0.009 0.596 0.317 7.053 0.067 1.412 20.416 0.08 48144. 0.3375 6.11 0.3227 0.5276 0.0589 0.0360 0.009 0.585 0.300 6.919 0.066 1.336 19.690 0.08 48212. 0.3166 6.55 0.3458 0.5443 0.0555 0.0352 0.009 0.572 0.283 6.765 0.065 1.258 18.959 0.08 48283. 0.2958 6.99 0.3688 0.5579 0.0519 0.0343 0.009 0.557 0.265 6.589 0.063 1.177 18.218 0.08 48358. 0.2749 7.42 0.3919 0.5682 0.0483 0.0333 0.009 0.540 0.246 6.391 0.061 1.094 17.463 0.08 48436. 0.2541 7.86 0.4149 0.5749 0.0445 0.0321 0.008 0.522 0.227 6.171 0.059 1.010 16.687 0.08 48517. 0.2333 8.30 0.4380 0.5776 0.0407 0.0309 0.008 0.501 0.208 5.929 0.057 0.924 15.884 0.08 48602. 0.2124 8.73 0.4610 0.5759 0.0368 0.0295 0.008 0.479 0.188 5.664 0.054 0.836 15.044 0.08 48690. 0.1913 9.17 0.4841 0.5688 0.0329 0.0280 0.007 0.454 0.168 5.376 0.051 0.746 14.153 0.08 48781. 0.1701 9.60 0.5071 0.5556 0.0289 0.0264 0.007 0.428 0.147 5.065 0.048 0.655 13.194 0.08 48876. 0.1486 10.04 0.5302 0.5346 0.0248 0.0246 0.006 0.400 0.127 4.730 0.045 0.563 12.144 0.08 48974. 0.1268 10.48 0.5532 0.5038 0.0207 0.0228 0.006 0.370 0.106 4.373 0.042 0.470 10.968 0.08 49076. 0.1046 10.91 0.5763 0.4603 0.0166 0.0208 0.005 0.337 0.085 3.993 0.038 0.377 9.619 0.08 49181. 0.0821 11.35 0.5993 0.3991 0.0124 0.0187 0.005 0.303 0.063 3.590 0.034 0.282 8.020 0.08 49290. 0.0593 11.79 0.6224 0.3126 0.0083 0.0165 0.004 0.268 0.042 3.166 0.030 0.188 6.050 0.08 49402. 0.0365 12.22 0.6454 0.1875 0.0041 0.0142 0.004 0.230 0.021 2.722 0.026 0.093 3.499 0.08 49517. 0.0149 12.66 0.6685 -0.0031 -0.0001 0.0117 0.003 0.191 0.000 2.255 0.022 -0.001 -0.056 0.08 49629. 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 0.0947 0.0341 0.070 2.216 1.932 52.435 0.250 8.593 16.711 0.16 95057. 0.6814 0.88 0.0231 0.0624 0.0930 0.0345 0.071 2.240 1.898 52.995 0.253 8.441 16.243 0.16 95119. 0.6565 1.75 0.0463 0.1213 0.0913 0.0348 0.072 2.261 1.861 53.495 0.255 8.278 15.780 0.16 95187. 0.6316 2.63 0.0694 0.1767 0.0893 0.0351 0.072 2.279 1.822 53.924 0.257 8.104 15.325 0.16 95259. 0.6069 3.51 0.0926 0.2287 0.0873 0.0353 0.073 2.293 1.780 54.269 0.259 7.918 14.878 0.16 95337. 0.5824 4.38 0.1157 0.2775 0.0851 0.0355 0.073 2.304 1.735 54.519 0.260 7.719 14.438 0.16 95420. 0.5580 5.26 0.1389 0.3230 0.0828 0.0356 0.073 2.310 1.688 54.660 0.261 7.508 14.007 0.16 95509. 0.5339 6.14 0.1620 0.3655 0.0803 0.0356 0.073 2.311 1.638 54.681 0.261 7.284 13.583 0.16 95603. 0.5100 7.01 0.1852 0.4049 0.0777 0.0355 0.073 2.306 1.584 54.569 0.261 7.047 13.168 0.16 95703. 0.4863 7.89 0.2083 0.4414 0.0749 0.0354 0.073 2.295 1.528 54.314 0.259 6.797 12.760 0.16 95809. 0.4628 8.77 0.2315 0.4751 0.0720 0.0351 0.072 2.278 1.469 53.908 0.257 6.534 12.359 0.16 95921. 0.4395 9.64 0.2546 0.5059 0.0690 0.0347 0.072 2.254 1.407 53.345 0.255 6.259 11.965 0.16 96039. 0.4164 10.52 0.2778 0.5340 0.0658 0.0343 0.071 2.224 1.343 52.619 0.251 5.974 11.577 0.16 96163. 0.3936 11.40 0.3009 0.5593 0.0626 0.0337 0.069 2.186 1.276 51.725 0.247 5.677 11.193 0.16 96294. 0.3710 12.27 0.3241 0.5818 0.0592 0.0330 0.068 2.141 1.208 50.660 0.242 5.371 10.812 0.16 96431. 0.3486 13.15 0.3472 0.6015 0.0557 0.0322 0.066 2.088 1.137 49.419 0.236 5.056 10.432 0.16 96575. 0.3263 14.03 0.3703 0.6182 0.0522 0.0312 0.064 2.028 1.064 47.997 0.229 4.731 10.052 0.16 96725. 0.3042 14.91 0.3935 0.6318 0.0485 0.0302 0.062 1.960 0.989 46.390 0.221 4.399 9.669 0.16 96882. 0.2821 15.78 0.4166 0.6421 0.0447 0.0290 0.060 1.885 0.912 44.595 0.213 4.059 9.280 0.16 97046. 0.2601 16.66 0.4398 0.6487 0.0409 0.0277 0.057 1.801 0.834 42.609 0.203 3.711 8.882 0.16 97216. 0.2380 17.54 0.4629 0.6510 0.0370 0.0263 0.054 1.709 0.755 40.428 0.193 3.358 8.469 0.16 97394. 0.2159 18.41 0.4861 0.6485 0.0330 0.0248 0.051 1.608 0.674 38.051 0.182 2.998 8.034 0.16 97578. 0.1935 19.29 0.5092 0.6400 0.0290 0.0231 0.048 1.499 0.592 35.476 0.169 2.633 7.568 0.16 97769. 0.1708 20.17 0.5324 0.6240 0.0250 0.0213 0.044 1.382 0.509 32.702 0.156 2.264 7.058 0.16 97967. 0.1477 21.04 0.5555 0.5981 0.0208 0.0194 0.040 1.257 0.425 29.732 0.142 1.890 6.483 0.16 98172. 0.1240 21.92 0.5787 0.5585 0.0167 0.0173 0.036 1.123 0.340 26.568 0.127 1.514 5.812 0.16 98384. 0.0995 22.80 0.6018 0.4988 0.0125 0.0151 0.031 0.981 0.255 23.215 0.111 1.136 4.991 0.16 98603. 0.0740 23.67 0.6250 0.4074 0.0084 0.0128 0.026 0.832 0.170 19.679 0.094 0.758 3.926 0.16 98829. 0.0475 24.55 0.6481 0.2607 0.0042 0.0104 0.021 0.675 0.085 15.969 0.076 0.379 2.423 0.16 99060. 0.0208 25.43 0.6713 -0.0009 0.0000 0.0078 0.016 0.509 0.000 12.052 0.058 -0.001 -0.008 0.16 99276. 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 0.0952 0.0329 0.228 4.799 4.370 170.321 0.542 19.439 11.638 0.24 142580. 0.7138 1.32 0.0232 0.0653 0.0936 0.0332 0.231 4.854 4.294 172.300 0.548 19.098 11.303 0.24 142674. 0.6871 2.64 0.0464 0.1268 0.0918 0.0336 0.233 4.904 4.211 174.076 0.554 18.731 10.972 0.24 142776. 0.6606 3.95 0.0696 0.1846 0.0898 0.0339 0.235 4.948 4.123 175.609 0.559 18.338 10.648 0.24 142885. 0.6343 5.27 0.0928 0.2388 0.0878 0.0341 0.237 4.983 4.028 176.856 0.563 17.917 10.331 0.24 143003. 0.6083 6.59 0.1160 0.2895 0.0856 0.0343 0.238 5.009 3.927 177.775 0.566 17.469 10.020 0.24 143128. 0.5826 7.91 0.1392 0.3369 0.0832 0.0344 0.239 5.024 3.820 178.324 0.568 16.991 9.716 0.24 143261. 0.5571 9.23 0.1624 0.3810 0.0808 0.0344 0.239 5.028 3.706 178.458 0.568 16.484 9.419 0.24 143403. 0.5320 10.55 0.1856 0.4220 0.0781 0.0344 0.239 5.019 3.585 178.135 0.567 15.947 9.129 0.24 143554. 0.5071 11.86 0.2088 0.4600 0.0754 0.0342 0.238 4.996 3.458 177.319 0.564 15.381 8.845 0.24 143714. 0.4826 13.18 0.2320 0.4951 0.0724 0.0339 0.236 4.958 3.324 175.982 0.560 14.787 8.568 0.24 143883. 0.4583 14.50 0.2552 0.5274 0.0694 0.0336 0.233 4.905 3.185 174.100 0.554 14.165 8.297 0.24 144061. 0.4344 15.82 0.2784 0.5569 0.0662 0.0331 0.230 4.836 3.039 171.657 0.546 13.518 8.030 0.24 144248. 0.4107 17.14 0.3016 0.5836 0.0629 0.0325 0.226 4.751 2.888 168.633 0.537 12.847 7.769 0.24 144445. 0.3873 18.45 0.3248 0.6076 0.0595 0.0318 0.221 4.649 2.732 165.012 0.525 12.153 7.510 0.24 144652. 0.3642 19.77 0.3480 0.6288 0.0560 0.0310 0.216 4.530 2.572 160.779 0.512 11.438 7.255 0.24 144869. 0.3413 21.09 0.3712 0.6472 0.0524 0.0301 0.209 4.393 2.406 155.919 0.496 10.704 7.000 0.24 145095. 0.3186 22.41 0.3944 0.6627 0.0487 0.0290 0.202 4.238 2.237 150.417 0.479 9.950 6.745 0.24 145332. 0.2960 23.73 0.4176 0.6749 0.0450 0.0278 0.193 4.064 2.064 144.261 0.459 9.179 6.489 0.24 145578. 0.2735 25.05 0.4408 0.6837 0.0411 0.0265 0.184 3.872 1.887 137.437 0.437 8.393 6.227 0.24 145835. 0.2510 26.36 0.4640 0.6886 0.0372 0.0251 0.174 3.661 1.707 129.937 0.414 7.591 5.958 0.24 146102. 0.2283 27.68 0.4872 0.6888 0.0332 0.0235 0.163 3.430 1.524 121.752 0.388 6.777 5.676 0.24 146380. 0.2055 29.00 0.5104 0.6834 0.0292 0.0218 0.151 3.180 1.338 112.879 0.359 5.950 5.375 0.24 146668. 0.1824 30.32 0.5336 0.6708 0.0251 0.0199 0.139 2.911 1.150 103.317 0.329 5.114 5.047 0.24 146966. 0.1588 31.64 0.5568 0.6487 0.0209 0.0180 0.125 2.622 0.960 93.068 0.296 4.269 4.677 0.24 147275. 0.1344 32.95 0.5800 0.6129 0.0167 0.0158 0.110 2.314 0.768 82.145 0.261 3.418 4.242 0.24 147595. 0.1091 34.27 0.6032 0.5563 0.0126 0.0136 0.095 1.988 0.576 70.564 0.225 2.562 3.703 0.24 147925. 0.0825 35.59 0.6264 0.4651 0.0084 0.0113 0.078 1.644 0.383 58.349 0.186 1.706 2.981 0.24 148264. 0.0542 36.91 0.6496 0.3081 0.0042 0.0088 0.061 1.283 0.191 45.528 0.145 0.850 1.904 0.24 148612. 0.0244 38.23 0.6728 -0.0077 -0.0001 0.0062 0.043 0.899 -0.003 31.913 0.102 -0.014 -0.046 0.24 148922. 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 0.0959 0.0323 0.532 8.385 7.824 396.816 0.947 34.799 8.943 0.32 190097. 0.7338 1.76 0.0232 0.0670 0.0942 0.0327 0.539 8.487 7.687 401.654 0.959 34.191 8.680 0.32 190224. 0.7061 3.52 0.0465 0.1300 0.0924 0.0330 0.544 8.579 7.540 406.007 0.969 33.537 8.423 0.32 190360. 0.6786 5.28 0.0697 0.1892 0.0905 0.0333 0.550 8.659 7.382 409.771 0.978 32.836 8.171 0.32 190506. 0.6514 7.04 0.0929 0.2446 0.0884 0.0336 0.554 8.724 7.213 412.847 0.986 32.086 7.925 0.32 190663. 0.6245 8.80 0.1162 0.2965 0.0862 0.0338 0.557 8.772 7.033 415.133 0.991 31.285 7.685 0.32 190831. 0.5979 10.56 0.1394 0.3449 0.0839 0.0339 0.559 8.801 6.842 416.525 0.994 30.432 7.450 0.32 191010. 0.5717 12.32 0.1626 0.3901 0.0814 0.0339 0.559 8.810 6.638 416.917 0.995 29.525 7.221 0.32 191200. 0.5458 14.08 0.1859 0.4320 0.0787 0.0339 0.558 8.795 6.422 416.207 0.994 28.565 6.999 0.32 191402. 0.5203 15.84 0.2091 0.4709 0.0759 0.0337 0.556 8.754 6.194 414.304 0.989 27.552 6.781 0.32 191616. 0.4952 17.60 0.2323 0.5069 0.0730 0.0335 0.551 8.688 5.955 411.139 0.982 26.488 6.570 0.32 191842. 0.4703 19.36 0.2556 0.5401 0.0699 0.0331 0.545 8.593 5.705 406.659 0.971 25.375 6.363 0.32 192080. 0.4459 21.12 0.2788 0.5705 0.0667 0.0326 0.538 8.469 5.444 400.816 0.957 24.216 6.161 0.32 192332. 0.4217 22.88 0.3020 0.5981 0.0634 0.0320 0.528 8.316 5.174 393.569 0.940 23.013 5.963 0.32 192595. 0.3979 24.64 0.3253 0.6231 0.0600 0.0313 0.516 8.133 4.894 384.878 0.919 21.770 5.768 0.32 192872. 0.3744 26.40 0.3485 0.6454 0.0565 0.0305 0.502 7.918 4.606 374.704 0.895 20.489 5.576 0.32 193162. 0.3511 28.16 0.3717 0.6649 0.0528 0.0295 0.487 7.671 4.310 363.010 0.867 19.172 5.386 0.32 193465. 0.3280 29.92 0.3950 0.6816 0.0491 0.0285 0.469 7.391 4.007 349.762 0.835 17.822 5.196 0.32 193782. 0.3051 31.68 0.4182 0.6952 0.0453 0.0273 0.449 7.077 3.696 334.926 0.800 16.440 5.005 0.32 194112. 0.2823 33.44 0.4414 0.7056 0.0414 0.0259 0.427 6.730 3.379 318.475 0.760 15.030 4.812 0.32 194455. 0.2595 35.20 0.4647 0.7122 0.0375 0.0244 0.403 6.347 3.056 300.384 0.717 13.593 4.615 0.32 194813. 0.2367 36.96 0.4879 0.7144 0.0334 0.0228 0.376 5.930 2.728 280.634 0.670 12.133 4.409 0.32 195184. 0.2136 38.72 0.5111 0.7113 0.0294 0.0211 0.348 5.477 2.395 259.215 0.619 10.652 4.190 0.32 195569. 0.1902 40.48 0.5344 0.7014 0.0252 0.0192 0.317 4.989 2.057 236.125 0.564 9.152 3.952 0.32 195968. 0.1663 42.24 0.5576 0.6823 0.0210 0.0172 0.283 4.466 1.717 211.375 0.505 7.637 3.684 0.32 196382. 0.1416 44.00 0.5809 0.6498 0.0168 0.0151 0.248 3.909 1.374 184.990 0.442 6.111 3.368 0.32 196809. 0.1158 45.76 0.6041 0.5965 0.0126 0.0128 0.211 3.318 1.029 157.011 0.375 4.578 2.973 0.32 197250. 0.0885 47.52 0.6273 0.5070 0.0084 0.0104 0.171 2.694 0.684 127.499 0.304 3.042 2.433 0.32 197704. 0.0590 49.28 0.6506 0.3445 0.0042 0.0079 0.129 2.040 0.339 96.520 0.230 1.509 1.595 0.32 198168. 0.0273 51.04 0.6738 -0.0182 -0.0001 0.0052 0.085 1.339 -0.011 63.387 0.151 -0.051 -0.081 0.32 198554. 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 0.0967 0.0321 1.034 13.029 12.332 770.763 1.472 54.853 7.257 0.40 237606. 0.7477 2.20 0.0232 0.0680 0.0951 0.0325 1.047 13.193 12.118 780.458 1.491 53.902 7.043 0.40 237765. 0.7193 4.40 0.0465 0.1319 0.0933 0.0329 1.058 13.341 11.888 789.187 1.507 52.879 6.833 0.40 237936. 0.6911 6.60 0.0697 0.1919 0.0913 0.0332 1.068 13.469 11.641 796.744 1.522 51.780 6.627 0.40 238120. 0.6634 8.81 0.0930 0.2481 0.0892 0.0335 1.077 13.573 11.377 802.931 1.533 50.603 6.427 0.40 238316. 0.6359 11.01 0.1162 0.3007 0.0870 0.0336 1.083 13.651 11.094 807.546 1.542 49.346 6.231 0.40 238527. 0.6089 13.21 0.1395 0.3498 0.0847 0.0338 1.087 13.699 10.793 810.381 1.548 48.007 6.041 0.40 238751. 0.5822 15.41 0.1627 0.3956 0.0822 0.0338 1.088 13.713 10.473 811.227 1.549 46.583 5.855 0.40 238990. 0.5559 17.61 0.1860 0.4381 0.0795 0.0337 1.086 13.691 10.133 809.878 1.547 45.073 5.675 0.40 239243. 0.5300 19.81 0.2092 0.4777 0.0767 0.0336 1.081 13.628 9.775 806.154 1.540 43.479 5.500 0.40 239512. 0.5045 22.01 0.2325 0.5143 0.0737 0.0333 1.073 13.522 9.398 799.918 1.528 41.804 5.329 0.40 239795. 0.4793 24.21 0.2557 0.5481 0.0706 0.0330 1.061 13.372 9.004 791.060 1.511 40.051 5.163 0.40 240095. 0.4545 26.42 0.2789 0.5791 0.0674 0.0325 1.045 13.177 8.594 779.490 1.489 38.225 5.001 0.40 240409. 0.4301 28.62 0.3022 0.6075 0.0641 0.0319 1.026 12.934 8.168 765.125 1.461 36.331 4.842 0.40 240740. 0.4060 30.82 0.3254 0.6332 0.0606 0.0312 1.003 12.643 7.727 747.883 1.428 34.371 4.686 0.40 241087. 0.3822 33.02 0.3487 0.6562 0.0571 0.0303 0.976 12.301 7.273 727.691 1.390 32.352 4.533 0.40 241450. 0.3587 35.22 0.3719 0.6766 0.0534 0.0293 0.945 11.909 6.806 704.476 1.345 30.275 4.382 0.40 241830. 0.3354 37.42 0.3952 0.6943 0.0496 0.0283 0.909 11.464 6.328 678.168 1.295 28.145 4.232 0.40 242227. 0.3123 39.62 0.4184 0.7090 0.0458 0.0270 0.870 10.966 5.838 648.703 1.239 25.966 4.082 0.40 242640. 0.2893 41.82 0.4417 0.7206 0.0419 0.0257 0.826 10.414 5.338 616.025 1.177 23.742 3.930 0.40 243071. 0.2664 44.03 0.4649 0.7286 0.0379 0.0242 0.778 9.806 4.828 580.084 1.108 21.476 3.775 0.40 243518. 0.2434 46.23 0.4882 0.7325 0.0338 0.0225 0.725 9.143 4.310 540.846 1.033 19.172 3.615 0.40 243983. 0.2202 48.43 0.5114 0.7314 0.0297 0.0208 0.668 8.423 3.785 498.288 0.952 16.834 3.445 0.40 244466. 0.1966 50.63 0.5347 0.7238 0.0255 0.0188 0.607 7.648 3.252 452.406 0.864 14.467 3.261 0.40 244965. 0.1725 52.83 0.5579 0.7073 0.0213 0.0168 0.541 6.816 2.715 403.222 0.770 12.076 3.054 0.40 245483. 0.1476 55.03 0.5811 0.6780 0.0171 0.0146 0.470 5.930 2.173 350.785 0.670 9.667 2.810 0.40 246017. 0.1216 57.23 0.6044 0.6282 0.0128 0.0123 0.396 4.990 1.629 295.180 0.564 7.247 2.504 0.40 246569. 0.0938 59.44 0.6276 0.5418 0.0085 0.0099 0.317 3.998 1.084 236.529 0.452 4.824 2.080 0.40 247137. 0.0635 61.64 0.6509 0.3785 0.0042 0.0073 0.235 2.958 0.540 174.960 0.334 2.403 1.401 0.41 247718. 0.0302 63.84 0.6741 -0.0179 -0.0001 0.0045 0.146 1.840 -0.015 108.864 0.208 -0.068 -0.064 0.41 248180. 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 0.0978 0.0322 1.791 18.815 17.952 1335.617 2.126 79.851 6.096 0.48 285103. 0.7578 2.67 0.0235 0.0691 0.0961 0.0326 1.814 19.059 17.642 1352.945 2.153 78.470 5.914 0.48 285296. 0.7288 5.33 0.0469 0.1340 0.0943 0.0330 1.835 19.279 17.307 1368.530 2.178 76.979 5.736 0.48 285505. 0.7001 8.00 0.0704 0.1949 0.0923 0.0333 1.853 19.468 16.946 1381.995 2.200 75.377 5.562 0.48 285728. 0.6717 10.66 0.0938 0.2520 0.0902 0.0336 1.868 19.623 16.560 1392.982 2.217 73.658 5.392 0.48 285968. 0.6437 13.33 0.1173 0.3053 0.0880 0.0338 1.879 19.738 16.146 1401.124 2.230 71.818 5.227 0.48 286225. 0.6162 15.99 0.1407 0.3552 0.0856 0.0339 1.886 19.807 15.705 1406.049 2.238 69.856 5.066 0.48 286498. 0.5890 18.66 0.1642 0.4016 0.0830 0.0339 1.887 19.826 15.235 1407.377 2.240 67.766 4.910 0.48 286790. 0.5623 21.32 0.1876 0.4448 0.0803 0.0339 1.884 19.789 14.737 1404.740 2.236 65.549 4.758 0.48 287099. 0.5359 23.99 0.2111 0.4849 0.0774 0.0337 1.875 19.691 14.210 1397.815 2.225 63.206 4.611 0.48 287426. 0.5099 26.65 0.2345 0.5220 0.0744 0.0334 1.859 19.530 13.656 1386.354 2.206 60.741 4.468 0.48 287773. 0.4844 29.32 0.2580 0.5563 0.0712 0.0330 1.837 19.302 13.076 1370.169 2.181 58.161 4.328 0.48 288138. 0.4592 31.98 0.2814 0.5879 0.0679 0.0325 1.809 19.005 12.471 1349.096 2.147 55.472 4.193 0.48 288522. 0.4344 34.65 0.3049 0.6167 0.0645 0.0319 1.774 18.637 11.844 1322.991 2.106 52.681 4.060 0.48 288926. 0.4100 37.31 0.3283 0.6430 0.0610 0.0311 1.732 18.196 11.195 1291.715 2.056 49.794 3.931 0.48 289349. 0.3859 39.98 0.3518 0.6666 0.0573 0.0303 1.683 17.681 10.525 1255.135 1.998 46.817 3.804 0.48 289793. 0.3620 42.64 0.3753 0.6876 0.0536 0.0292 1.627 17.089 9.837 1213.121 1.931 43.756 3.678 0.48 290256. 0.3384 45.31 0.3987 0.7058 0.0497 0.0281 1.563 16.419 9.131 1165.552 1.855 40.616 3.553 0.48 290740. 0.3150 47.97 0.4222 0.7211 0.0458 0.0268 1.492 15.669 8.409 1112.317 1.770 37.404 3.429 0.48 291245. 0.2917 50.64 0.4456 0.7334 0.0418 0.0254 1.413 14.838 7.672 1053.314 1.676 34.124 3.304 0.48 291770. 0.2685 53.30 0.4691 0.7421 0.0377 0.0238 1.326 13.925 6.921 988.461 1.573 30.783 3.176 0.48 292317. 0.2451 55.97 0.4925 0.7466 0.0335 0.0221 1.231 12.928 6.157 917.697 1.461 27.386 3.043 0.48 292884. 0.2215 58.63 0.5160 0.7461 0.0293 0.0203 1.128 11.847 5.382 840.985 1.338 23.939 2.903 0.48 293473. 0.1976 61.30 0.5394 0.7390 0.0250 0.0183 1.017 10.683 4.598 758.331 1.207 20.451 2.750 0.48 294082. 0.1730 63.96 0.5629 0.7227 0.0207 0.0161 0.898 9.435 3.806 669.779 1.066 16.927 2.577 0.48 294714. 0.1475 66.63 0.5863 0.6925 0.0164 0.0139 0.772 8.106 3.008 575.431 0.916 13.379 2.371 0.48 295366. 0.1206 69.29 0.6098 0.6395 0.0120 0.0115 0.638 6.698 2.207 475.454 0.757 9.815 2.105 0.48 296039. 0.0917 71.96 0.6332 0.5431 0.0077 0.0089 0.496 5.213 1.405 370.082 0.589 6.248 1.722 0.49 296731. 0.0599 74.62 0.6567 0.3455 0.0033 0.0063 0.348 3.656 0.604 259.511 0.413 2.688 1.056 0.49 297436. 0.0241 77.29 0.6801 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 0.0991 0.0325 2.872 25.861 24.760 2141.752 2.922 110.134 5.244 0.56 332585. 0.7655 3.08 0.0233 0.0688 0.0974 0.0329 2.910 26.200 24.342 2169.822 2.960 108.274 5.088 0.56 332810. 0.7365 6.17 0.0465 0.1334 0.0956 0.0333 2.944 26.505 23.890 2195.090 2.995 106.264 4.936 0.56 333052. 0.7079 9.25 0.0698 0.1941 0.0937 0.0337 2.973 26.769 23.404 2216.958 3.024 104.100 4.788 0.56 333311. 0.6796 12.33 0.0930 0.2510 0.0916 0.0339 2.997 26.985 22.881 2234.850 3.049 101.776 4.644 0.56 333590. 0.6517 15.41 0.1163 0.3043 0.0893 0.0341 3.015 27.146 22.322 2248.190 3.067 99.287 4.503 0.56 333887. 0.6242 18.50 0.1395 0.3541 0.0870 0.0343 3.026 27.245 21.724 2256.387 3.078 96.629 4.367 0.56 334205. 0.5971 21.58 0.1628 0.4006 0.0844 0.0343 3.029 27.275 21.088 2258.848 3.081 93.798 4.234 0.56 334542. 0.5705 24.66 0.1860 0.4439 0.0817 0.0342 3.024 27.228 20.412 2254.986 3.076 90.792 4.106 0.56 334900. 0.5442 27.74 0.2093 0.4842 0.0788 0.0341 3.010 27.099 19.697 2244.286 3.062 87.612 3.981 0.56 335279. 0.5183 30.83 0.2325 0.5216 0.0758 0.0338 2.986 26.882 18.944 2226.347 3.037 84.264 3.859 0.56 335679. 0.4928 33.91 0.2558 0.5562 0.0727 0.0334 2.951 26.575 18.156 2200.857 3.002 80.757 3.742 0.56 336101. 0.4677 36.99 0.2790 0.5882 0.0694 0.0329 2.907 26.173 17.333 2167.580 2.957 77.099 3.627 0.56 336545. 0.4430 40.07 0.3023 0.6176 0.0660 0.0323 2.851 25.674 16.479 2126.282 2.901 73.300 3.515 0.56 337012. 0.4187 43.16 0.3255 0.6444 0.0624 0.0315 2.785 25.076 15.596 2076.762 2.833 69.369 3.406 0.56 337500. 0.3946 46.24 0.3488 0.6687 0.0588 0.0307 2.707 24.376 14.684 2018.809 2.754 65.313 3.299 0.56 338012. 0.3709 49.32 0.3720 0.6905 0.0550 0.0296 2.618 23.572 13.746 1952.225 2.663 61.141 3.194 0.56 338547. 0.3474 52.40 0.3953 0.7097 0.0512 0.0285 2.517 22.662 12.783 1876.823 2.560 56.860 3.089 0.56 339104. 0.3241 55.49 0.4185 0.7262 0.0472 0.0272 2.404 21.643 11.798 1792.427 2.445 52.478 2.986 0.56 339686. 0.3009 58.57 0.4418 0.7398 0.0432 0.0258 2.278 20.513 10.792 1698.879 2.318 48.003 2.881 0.56 340291. 0.2777 61.65 0.4650 0.7502 0.0391 0.0242 2.140 19.272 9.766 1596.045 2.177 43.441 2.775 0.56 340920. 0.2545 64.73 0.4883 0.7567 0.0349 0.0225 1.990 17.917 8.723 1483.821 2.024 38.801 2.666 0.56 341573. 0.2311 67.82 0.5115 0.7588 0.0307 0.0207 1.827 16.447 7.664 1362.148 1.858 34.091 2.552 0.56 342250. 0.2073 70.90 0.5348 0.7549 0.0264 0.0187 1.651 14.864 6.592 1231.018 1.679 29.321 2.429 0.56 342951. 0.1830 73.98 0.5580 0.7431 0.0220 0.0166 1.462 13.167 5.508 1090.484 1.488 24.500 2.291 0.56 343677. 0.1577 77.07 0.5813 0.7193 0.0177 0.0143 1.261 11.358 4.416 940.690 1.283 19.641 2.129 0.56 344426. 0.1313 80.15 0.6045 0.6762 0.0133 0.0119 1.049 9.441 3.318 781.875 1.067 14.757 1.925 0.57 345200. 0.1028 83.23 0.6278 0.5973 0.0089 0.0093 0.824 7.419 2.218 614.388 0.838 9.864 1.637 0.57 345996. 0.0715 86.31 0.6510 0.4377 0.0045 0.0067 0.588 5.296 1.119 438.610 0.598 4.976 1.157 0.57 346810. 0.0359 89.40 0.6743 -0.0040 0.0000 0.0038 0.335 3.015 -0.006 249.662 0.341 -0.025 -0.010 0.57 347440. 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 0.1007 0.0331 4.358 34.338 32.861 3250.034 3.879 146.165 4.586 0.63 380047. 0.7713 3.53 0.0233 0.0689 0.0990 0.0335 4.417 34.796 32.315 3293.440 3.931 143.738 4.450 0.63 380305. 0.7422 7.06 0.0466 0.1336 0.0972 0.0339 4.469 35.209 31.724 3332.475 3.978 141.110 4.318 0.63 380584. 0.7135 10.59 0.0699 0.1944 0.0953 0.0342 4.514 35.565 31.087 3366.210 4.018 138.274 4.189 0.63 380884. 0.6852 14.12 0.0932 0.2515 0.0932 0.0345 4.551 35.856 30.401 3393.757 4.051 135.222 4.063 0.63 381204. 0.6572 17.65 0.1165 0.3049 0.0909 0.0347 4.579 36.072 29.664 3414.211 4.075 131.946 3.941 0.64 381548. 0.6297 21.18 0.1398 0.3548 0.0885 0.0349 4.595 36.204 28.876 3426.670 4.090 128.441 3.822 0.64 381913. 0.6026 24.70 0.1631 0.4015 0.0859 0.0349 4.600 36.241 28.035 3430.230 4.095 124.701 3.707 0.64 382302. 0.5759 28.23 0.1863 0.4450 0.0832 0.0348 4.592 36.176 27.141 3423.991 4.087 120.725 3.595 0.64 382715. 0.5495 31.76 0.2096 0.4856 0.0803 0.0347 4.569 35.998 26.194 3407.159 4.067 116.513 3.487 0.64 383152. 0.5236 35.29 0.2329 0.5233 0.0772 0.0344 4.531 35.701 25.196 3379.115 4.034 112.073 3.382 0.64 383613. 0.4981 38.82 0.2562 0.5582 0.0740 0.0340 4.478 35.282 24.149 3339.406 3.986 107.417 3.280 0.64 384099. 0.4729 42.35 0.2795 0.5906 0.0707 0.0334 4.409 34.735 23.057 3287.661 3.924 102.557 3.181 0.64 384611. 0.4481 45.88 0.3028 0.6204 0.0672 0.0328 4.323 34.058 21.921 3223.563 3.848 97.506 3.084 0.64 385147. 0.4237 49.41 0.3261 0.6477 0.0636 0.0320 4.220 33.247 20.746 3146.805 3.756 92.276 2.990 0.64 385710. 0.3996 52.94 0.3494 0.6726 0.0599 0.0311 4.100 32.299 19.532 3057.094 3.649 86.879 2.898 0.64 386298. 0.3757 56.47 0.3727 0.6949 0.0560 0.0300 3.962 31.211 18.283 2954.135 3.526 81.324 2.807 0.64 386913. 0.3522 60.00 0.3960 0.7148 0.0521 0.0289 3.805 29.981 17.002 2837.652 3.387 75.623 2.718 0.64 387555. 0.3287 63.53 0.4193 0.7320 0.0481 0.0275 3.631 28.604 15.689 2707.387 3.232 69.785 2.628 0.64 388223. 0.3054 67.06 0.4426 0.7464 0.0440 0.0261 3.437 27.080 14.348 2563.098 3.059 63.820 2.539 0.64 388918. 0.2822 70.59 0.4659 0.7577 0.0398 0.0245 3.225 25.405 12.981 2404.592 2.870 57.738 2.449 0.64 389641. 0.2588 74.11 0.4892 0.7653 0.0355 0.0227 2.993 23.579 11.590 2231.716 2.664 51.551 2.355 0.64 390391. 0.2353 77.64 0.5124 0.7686 0.0312 0.0208 2.742 21.599 10.177 2044.379 2.440 45.269 2.258 0.64 391168. 0.2113 81.17 0.5357 0.7662 0.0268 0.0187 2.471 19.467 8.746 1842.569 2.199 38.904 2.153 0.64 391973. 0.1868 84.70 0.5590 0.7560 0.0224 0.0165 2.181 17.183 7.300 1626.377 1.941 32.470 2.036 0.64 392806. 0.1614 88.23 0.5823 0.7341 0.0179 0.0142 1.872 14.749 5.842 1396.024 1.666 25.983 1.898 0.65 393667. 0.1346 91.76 0.6056 0.6931 0.0134 0.0117 1.545 12.170 4.375 1151.886 1.375 19.462 1.723 0.65 394554. 0.1057 95.29 0.6289 0.6156 0.0089 0.0091 1.200 9.451 2.906 894.508 1.068 12.927 1.474 0.65 395468. 0.0737 98.82 0.6522 0.4526 0.0044 0.0064 0.837 6.598 1.438 624.469 0.745 6.398 1.045 0.65 396400. 0.0368 102.35 0.6755 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 0.1026 0.0340 6.376 44.653 42.393 4754.657 5.045 188.562 4.044 0.71 427482. 0.7725 4.00 0.0235 0.0689 0.1010 0.0344 6.458 45.228 41.702 4815.956 5.110 185.489 3.927 0.71 427777. 0.7441 8.01 0.0470 0.1339 0.0992 0.0348 6.532 45.746 40.950 4871.097 5.168 182.146 3.813 0.71 428095. 0.7159 12.01 0.0705 0.1949 0.0972 0.0351 6.596 46.193 40.136 4918.689 5.219 178.525 3.701 0.71 428438. 0.6879 16.02 0.0940 0.2522 0.0950 0.0354 6.648 46.556 39.256 4957.354 5.260 174.613 3.592 0.71 428806. 0.6602 20.02 0.1175 0.3059 0.0928 0.0356 6.686 46.823 38.309 4985.690 5.290 170.401 3.485 0.71 429199. 0.6329 24.02 0.1409 0.3561 0.0903 0.0357 6.708 46.978 37.293 5002.278 5.308 165.880 3.381 0.71 429619. 0.6058 28.03 0.1644 0.4031 0.0877 0.0358 6.713 47.010 36.206 5005.705 5.311 161.045 3.281 0.71 430065. 0.5791 32.03 0.1879 0.4469 0.0849 0.0357 6.698 46.906 35.047 4994.561 5.299 155.891 3.183 0.72 430538. 0.5528 36.04 0.2114 0.4878 0.0819 0.0355 6.662 46.652 33.818 4967.577 5.271 150.421 3.088 0.72 431039. 0.5268 40.04 0.2349 0.5258 0.0787 0.0352 6.603 46.241 32.519 4923.788 5.224 144.645 2.996 0.72 431569. 0.5012 44.04 0.2584 0.5611 0.0754 0.0347 6.521 45.665 31.156 4862.480 5.159 138.580 2.906 0.72 432126. 0.4759 48.05 0.2819 0.5939 0.0720 0.0342 6.414 44.920 29.731 4783.084 5.075 132.242 2.819 0.72 432712. 0.4510 52.05 0.3054 0.6241 0.0684 0.0335 6.283 44.000 28.249 4685.155 4.971 125.650 2.735 0.72 433328. 0.4264 56.06 0.3289 0.6518 0.0647 0.0326 6.126 42.902 26.713 4568.265 4.847 118.819 2.652 0.72 433973. 0.4022 60.06 0.3524 0.6771 0.0608 0.0317 5.943 41.623 25.127 4432.019 4.703 111.766 2.572 0.72 434647. 0.3782 64.06 0.3758 0.6999 0.0569 0.0305 5.734 40.158 23.495 4276.003 4.537 104.504 2.492 0.72 435352. 0.3544 68.07 0.3993 0.7203 0.0528 0.0293 5.498 38.503 21.818 4099.833 4.350 97.048 2.414 0.72 436087. 0.3308 72.07 0.4228 0.7381 0.0487 0.0279 5.234 36.656 20.101 3903.124 4.141 89.411 2.336 0.72 436852. 0.3073 76.08 0.4463 0.7530 0.0444 0.0263 4.942 34.612 18.347 3685.535 3.910 81.605 2.258 0.72 437648. 0.2837 80.08 0.4698 0.7649 0.0401 0.0246 4.622 32.370 16.557 3446.796 3.657 73.645 2.179 0.72 438475. 0.2601 84.08 0.4933 0.7731 0.0357 0.0228 4.273 29.927 14.735 3186.698 3.381 65.543 2.097 0.72 439334. 0.2362 88.09 0.5168 0.7769 0.0312 0.0208 3.896 27.283 12.886 2905.130 3.082 57.316 2.012 0.72 440223. 0.2119 92.09 0.5403 0.7749 0.0267 0.0186 3.489 24.437 11.012 2602.102 2.761 48.980 1.919 0.72 441144. 0.1869 96.10 0.5638 0.7648 0.0221 0.0163 3.055 21.392 9.117 2277.835 2.417 40.553 1.815 0.73 442097. 0.1608 100.10 0.5873 0.7422 0.0174 0.0138 2.592 18.152 7.207 1932.835 2.051 32.057 1.691 0.73 443081. 0.1332 104.10 0.6107 0.6980 0.0128 0.0112 2.103 14.725 5.287 1567.950 1.664 23.516 1.529 0.73 444095. 0.1032 108.11 0.6342 0.6104 0.0081 0.0085 1.588 11.123 3.363 1184.380 1.257 14.959 1.288 0.73 445138. 0.0693 112.11 0.6577 0.4100 0.0035 0.0056 1.050 7.356 1.441 783.273 0.831 6.408 0.834 0.73 446197. 0.0294 116.12 0.6812 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 0.1050 0.0366 9.412 59.322 53.526 7018.530 6.702 238.083 3.459 0.79 474879. 0.7425 4.45 0.0235 0.0658 0.1033 0.0369 9.492 59.827 52.689 7078.218 6.759 234.362 3.376 0.79 475208. 0.7190 8.89 0.0470 0.1284 0.1015 0.0371 9.560 60.257 51.774 7129.150 6.808 230.291 3.294 0.79 475565. 0.6954 13.34 0.0704 0.1878 0.0996 0.0373 9.615 60.601 50.777 7169.766 6.847 225.858 3.212 0.79 475949. 0.6716 17.78 0.0939 0.2441 0.0975 0.0375 9.653 60.843 49.696 7198.480 6.874 221.048 3.131 0.79 476361. 0.6476 22.23 0.1174 0.2974 0.0952 0.0376 9.674 60.972 48.527 7213.699 6.889 215.847 3.051 0.79 476801. 0.6236 26.68 0.1409 0.3476 0.0927 0.0376 9.674 60.972 47.267 7213.677 6.889 210.245 2.972 0.79 477271. 0.5995 31.12 0.1643 0.3948 0.0901 0.0375 9.651 60.828 45.916 7196.667 6.872 204.234 2.894 0.79 477771. 0.5753 35.57 0.1878 0.4392 0.0872 0.0373 9.603 60.525 44.471 7160.859 6.838 197.807 2.817 0.79 478302. 0.5511 40.01 0.2113 0.4808 0.0842 0.0370 9.527 60.050 42.933 7104.583 6.784 190.967 2.741 0.80 478863. 0.5269 44.46 0.2348 0.5197 0.0810 0.0366 9.423 59.390 41.305 7026.507 6.710 183.725 2.666 0.80 479455. 0.5027 48.91 0.2582 0.5559 0.0776 0.0361 9.287 58.537 39.592 6925.640 6.613 176.105 2.593 0.80 480080. 0.4787 53.35 0.2817 0.5896 0.0741 0.0354 9.120 57.485 37.798 6801.151 6.495 168.127 2.521 0.80 480735. 0.4547 57.80 0.3052 0.6208 0.0705 0.0346 8.921 56.227 35.930 6652.278 6.352 159.817 2.450 0.80 481424. 0.4308 62.24 0.3287 0.6494 0.0667 0.0337 8.687 54.756 33.992 6478.249 6.186 151.196 2.380 0.80 482144. 0.4071 66.69 0.3521 0.6757 0.0627 0.0327 8.419 53.066 31.989 6278.283 5.995 142.286 2.311 0.80 482898. 0.3835 71.14 0.3756 0.6995 0.0587 0.0315 8.115 51.150 29.924 6051.590 5.779 133.104 2.243 0.80 483684. 0.3600 75.58 0.3991 0.7208 0.0545 0.0302 7.774 49.001 27.803 5797.349 5.536 123.669 2.175 0.80 484504. 0.3365 80.03 0.4226 0.7395 0.0503 0.0287 7.396 46.613 25.629 5514.857 5.266 113.999 2.108 0.80 485357. 0.3131 84.47 0.4460 0.7555 0.0459 0.0271 6.979 43.986 23.406 5204.063 4.970 104.110 2.040 0.80 486244. 0.2896 88.92 0.4695 0.7682 0.0415 0.0253 6.524 41.118 21.137 4864.757 4.646 94.017 1.971 0.80 487166. 0.2658 93.37 0.4930 0.7773 0.0369 0.0234 6.030 38.006 18.826 4496.561 4.294 83.739 1.899 0.80 488121. 0.2417 97.81 0.5165 0.7817 0.0323 0.0214 5.498 34.655 16.478 4100.088 3.915 73.293 1.823 0.80 489112. 0.2171 102.26 0.5399 0.7797 0.0276 0.0191 4.930 31.071 14.096 3676.074 3.510 62.700 1.739 0.80 490136. 0.1916 106.71 0.5634 0.7687 0.0229 0.0168 4.326 27.265 11.687 3225.816 3.080 51.983 1.643 0.81 491195. 0.1648 111.15 0.5869 0.7435 0.0182 0.0143 3.689 23.253 9.255 2751.078 2.627 41.166 1.526 0.81 492289. 0.1362 115.60 0.6104 0.6942 0.0134 0.0117 3.023 19.053 6.808 2254.139 2.153 30.281 1.370 0.81 493416. 0.1049 120.04 0.6338 0.5979 0.0085 0.0091 2.330 14.689 4.353 1737.837 1.660 19.362 1.136 0.81 494575. 0.0695 124.49 0.6573 0.3897 0.0037 0.0063 1.616 10.184 1.897 1204.942 1.151 8.438 0.714 0.81 495752. 0.0289 128.94 0.6808 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 0.1074 0.0433 14.857 85.126 66.259 11078.593 9.618 294.719 2.713 0.87 522241. 0.6478 4.86 0.0233 0.0568 0.1059 0.0434 14.880 85.259 65.309 11095.833 9.632 290.494 2.670 0.87 522601. 0.6330 9.71 0.0466 0.1118 0.1042 0.0434 14.879 85.254 64.258 11095.243 9.632 285.821 2.627 0.87 522991. 0.6178 14.57 0.0699 0.1651 0.1023 0.0433 14.852 85.101 63.103 11075.333 9.615 280.681 2.584 0.87 523411. 0.6023 19.43 0.0932 0.2165 0.1002 0.0432 14.798 84.790 61.837 11034.772 9.579 275.052 2.542 0.87 523863. 0.5864 24.28 0.1166 0.2660 0.0980 0.0429 14.715 84.313 60.458 10972.748 9.526 268.919 2.499 0.87 524347. 0.5701 29.14 0.1399 0.3138 0.0956 0.0426 14.601 83.664 58.963 10888.246 9.452 262.269 2.456 0.87 524864. 0.5533 33.99 0.1632 0.3596 0.0930 0.0422 14.457 82.834 57.350 10780.280 9.359 255.093 2.413 0.87 525413. 0.5361 38.85 0.1865 0.4035 0.0901 0.0417 14.279 81.816 55.617 10647.738 9.243 247.384 2.369 0.87 525997. 0.5184 43.71 0.2098 0.4454 0.0871 0.0410 14.067 80.600 53.764 10489.517 9.106 239.143 2.325 0.87 526614. 0.5001 48.56 0.2331 0.4854 0.0840 0.0403 13.819 79.180 51.795 10304.754 8.946 230.384 2.280 0.88 527265. 0.4814 53.42 0.2564 0.5232 0.0806 0.0395 13.535 77.553 49.715 10092.922 8.762 221.132 2.234 0.88 527950. 0.4622 58.28 0.2797 0.5590 0.0770 0.0386 13.214 75.714 47.531 9853.601 8.554 211.419 2.188 0.88 528671. 0.4425 63.13 0.3030 0.5926 0.0733 0.0375 12.855 73.659 45.250 9586.208 8.322 201.272 2.141 0.88 529426. 0.4225 67.99 0.3263 0.6240 0.0695 0.0363 12.458 71.383 42.877 9289.965 8.065 190.719 2.093 0.88 530216. 0.4022 72.84 0.3497 0.6531 0.0655 0.0351 12.021 68.878 40.420 8963.999 7.782 179.786 2.045 0.88 531042. 0.3815 77.70 0.3730 0.6800 0.0614 0.0337 11.543 66.139 37.882 8607.539 7.472 168.500 1.996 0.88 531903. 0.3605 82.56 0.3963 0.7044 0.0572 0.0322 11.023 63.159 35.271 8219.709 7.136 156.886 1.946 0.88 532800. 0.3391 87.41 0.4196 0.7263 0.0528 0.0305 10.459 59.930 32.591 7799.510 6.771 144.967 1.895 0.88 533733. 0.3174 92.27 0.4429 0.7455 0.0484 0.0287 9.851 56.444 29.848 7345.854 6.377 132.766 1.843 0.88 534703. 0.2954 97.13 0.4662 0.7598 0.0438 0.0269 9.219 52.821 27.044 6874.269 5.968 120.292 1.784 0.88 535709. 0.2722 101.98 0.4895 0.7663 0.0392 0.0250 8.582 49.172 24.181 6399.405 5.555 107.558 1.714 0.88 536752. 0.2473 106.84 0.5128 0.7664 0.0345 0.0231 7.906 45.303 21.269 5895.831 5.118 94.604 1.636 0.88 537832. 0.2214 111.69 0.5361 0.7577 0.0297 0.0210 7.198 41.242 18.312 5367.320 4.659 81.453 1.547 0.89 538948. 0.1943 116.55 0.5594 0.7371 0.0248 0.0188 6.458 37.004 15.317 4815.829 4.181 68.131 1.443 0.89 540102. 0.1656 121.41 0.5828 0.6989 0.0199 0.0166 5.694 32.623 12.291 4245.668 3.686 54.671 1.313 0.89 541293. 0.1351 126.26 0.6061 0.6337 0.0150 0.0143 4.911 28.137 9.243 3661.838 3.179 41.112 1.145 0.89 542520. 0.1021 131.12 0.6294 0.5252 0.0100 0.0120 4.116 23.583 6.183 3069.182 2.664 27.500 0.914 0.89 543781. 0.0667 135.98 0.6527 0.3413 0.0051 0.0097 3.316 19.001 3.122 2472.851 2.147 13.885 0.573 0.89 545070. 0.0297 140.83 0.6760 0.0007 0.0000 0.0072 2.481 14.216 0.005 1850.167 1.606 0.022 0.001 0.89 546155. 0.0000