20x13E (20x13E.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 0.0954 0.0384 0.010 0.623 0.486 7.376 0.070 2.163 29.899 0.08 36651. 0.6117 0.52 0.0276 0.0665 0.0942 0.0391 0.010 0.634 0.481 7.500 0.072 2.138 29.061 0.08 36677. 0.5910 1.04 0.0552 0.1292 0.0930 0.0397 0.010 0.644 0.474 7.622 0.073 2.110 28.223 0.08 36707. 0.5702 1.57 0.0827 0.1881 0.0916 0.0403 0.010 0.654 0.467 7.739 0.074 2.079 27.389 0.08 36739. 0.5493 2.09 0.1103 0.2433 0.0901 0.0409 0.011 0.663 0.460 7.849 0.075 2.045 26.562 0.08 36775. 0.5283 2.61 0.1379 0.2947 0.0885 0.0414 0.011 0.672 0.451 7.949 0.076 2.007 25.745 0.08 36814. 0.5074 3.13 0.1655 0.3426 0.0867 0.0419 0.011 0.679 0.442 8.038 0.077 1.966 24.941 0.08 36856. 0.4865 3.66 0.1930 0.3871 0.0847 0.0422 0.011 0.686 0.432 8.110 0.077 1.921 24.152 0.08 36901. 0.4656 4.18 0.2206 0.4282 0.0825 0.0425 0.011 0.690 0.421 8.165 0.078 1.872 23.378 0.08 36951. 0.4449 4.70 0.2482 0.4662 0.0802 0.0427 0.011 0.693 0.409 8.197 0.078 1.818 22.621 0.08 37003. 0.4243 5.22 0.2758 0.5010 0.0776 0.0427 0.011 0.694 0.396 8.205 0.078 1.761 21.881 0.08 37060. 0.4039 5.75 0.3033 0.5329 0.0749 0.0426 0.011 0.692 0.382 8.185 0.078 1.698 21.156 0.08 37120. 0.3835 6.27 0.3309 0.5618 0.0719 0.0424 0.011 0.688 0.367 8.135 0.078 1.631 20.447 0.08 37185. 0.3633 6.79 0.3585 0.5879 0.0687 0.0419 0.011 0.680 0.351 8.051 0.077 1.559 19.750 0.08 37253. 0.3431 7.31 0.3861 0.6110 0.0654 0.0413 0.011 0.670 0.333 7.930 0.076 1.482 19.062 0.08 37325. 0.3229 7.83 0.4136 0.6312 0.0618 0.0405 0.010 0.657 0.315 7.771 0.074 1.401 18.380 0.08 37401. 0.3026 8.36 0.4412 0.6484 0.0579 0.0394 0.010 0.640 0.295 7.571 0.072 1.314 17.698 0.08 37481. 0.2822 8.88 0.4688 0.6622 0.0539 0.0382 0.010 0.620 0.275 7.332 0.070 1.223 17.012 0.08 37566. 0.2617 9.40 0.4964 0.6723 0.0498 0.0367 0.009 0.596 0.254 7.056 0.067 1.129 16.313 0.08 37654. 0.2411 9.92 0.5240 0.6783 0.0455 0.0351 0.009 0.570 0.232 6.745 0.064 1.031 15.591 0.08 37746. 0.2203 10.45 0.5515 0.6794 0.0411 0.0333 0.009 0.541 0.209 6.400 0.061 0.931 14.836 0.08 37841. 0.1992 10.97 0.5791 0.6748 0.0366 0.0314 0.008 0.509 0.186 6.024 0.058 0.829 14.034 0.08 37941. 0.1778 11.49 0.6067 0.6632 0.0320 0.0293 0.008 0.475 0.163 5.617 0.054 0.725 13.166 0.08 38045. 0.1560 12.01 0.6343 0.6428 0.0273 0.0270 0.007 0.438 0.139 5.181 0.049 0.620 12.206 0.08 38153. 0.1337 12.53 0.6618 0.6109 0.0227 0.0246 0.006 0.399 0.116 4.720 0.045 0.515 11.117 0.08 38264. 0.1109 13.06 0.6894 0.5635 0.0180 0.0221 0.006 0.358 0.092 4.235 0.040 0.409 9.844 0.08 38380. 0.0876 13.58 0.7170 0.4942 0.0134 0.0194 0.005 0.315 0.068 3.728 0.036 0.304 8.302 0.08 38499. 0.0636 14.10 0.7446 0.3923 0.0088 0.0167 0.004 0.271 0.045 3.205 0.031 0.199 6.346 0.08 38622. 0.0394 14.62 0.7721 0.2382 0.0043 0.0139 0.004 0.225 0.022 2.667 0.025 0.097 3.716 0.08 38749. 0.0161 15.15 0.7997 -0.0079 -0.0001 0.0110 0.003 0.179 -0.001 2.121 0.020 -0.002 -0.119 0.08 38880. 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 0.0957 0.0358 0.074 2.325 1.952 55.012 0.263 8.683 16.095 0.16 73300. 0.6598 1.05 0.0277 0.0717 0.0946 0.0365 0.075 2.369 1.930 56.063 0.268 8.582 15.610 0.16 73354. 0.6362 2.10 0.0553 0.1390 0.0934 0.0372 0.077 2.413 1.904 57.100 0.273 8.471 15.128 0.16 73413. 0.6125 3.14 0.0830 0.2020 0.0920 0.0378 0.078 2.455 1.877 58.103 0.277 8.348 14.651 0.16 73478. 0.5888 4.19 0.1107 0.2607 0.0905 0.0384 0.079 2.496 1.846 59.052 0.282 8.212 14.180 0.16 73550. 0.5653 5.24 0.1384 0.3152 0.0889 0.0390 0.080 2.533 1.812 59.928 0.286 8.062 13.718 0.16 73628. 0.5418 6.29 0.1660 0.3658 0.0870 0.0395 0.081 2.565 1.775 60.704 0.290 7.897 13.266 0.16 73712. 0.5186 7.34 0.1937 0.4125 0.0851 0.0399 0.082 2.593 1.735 61.358 0.293 7.717 12.825 0.16 73804. 0.4956 8.39 0.2214 0.4557 0.0829 0.0403 0.083 2.614 1.691 61.863 0.295 7.520 12.395 0.16 73903. 0.4728 9.43 0.2491 0.4954 0.0805 0.0405 0.083 2.628 1.642 62.192 0.297 7.306 11.978 0.16 74010. 0.4504 10.48 0.2767 0.5319 0.0780 0.0406 0.084 2.634 1.590 62.320 0.298 7.073 11.573 0.16 74124. 0.4282 11.53 0.3044 0.5652 0.0752 0.0405 0.083 2.629 1.534 62.220 0.297 6.822 11.181 0.16 74245. 0.4062 12.58 0.3321 0.5955 0.0722 0.0403 0.083 2.615 1.473 61.866 0.295 6.552 10.799 0.16 74375. 0.3845 13.63 0.3598 0.6230 0.0690 0.0399 0.082 2.588 1.408 61.235 0.292 6.262 10.428 0.16 74512. 0.3630 14.68 0.3874 0.6476 0.0656 0.0393 0.081 2.548 1.338 60.304 0.288 5.953 10.066 0.16 74657. 0.3416 15.72 0.4151 0.6694 0.0620 0.0384 0.079 2.495 1.264 59.047 0.282 5.623 9.710 0.16 74811. 0.3203 16.77 0.4428 0.6882 0.0581 0.0374 0.077 2.428 1.186 57.455 0.274 5.274 9.360 0.16 74972. 0.2990 17.82 0.4705 0.7040 0.0541 0.0362 0.074 2.347 1.103 55.535 0.265 4.908 9.012 0.16 75141. 0.2777 18.87 0.4981 0.7165 0.0499 0.0347 0.071 2.253 1.018 53.301 0.254 4.528 8.662 0.16 75318. 0.2564 19.92 0.5258 0.7253 0.0456 0.0330 0.068 2.145 0.930 50.766 0.242 4.135 8.306 0.16 75503. 0.2350 20.97 0.5535 0.7297 0.0411 0.0312 0.064 2.026 0.839 47.942 0.229 3.733 7.939 0.16 75696. 0.2134 22.01 0.5812 0.7290 0.0366 0.0292 0.060 1.895 0.747 44.843 0.214 3.322 7.554 0.16 75897. 0.1915 23.06 0.6088 0.7219 0.0320 0.0270 0.056 1.753 0.653 41.483 0.198 2.905 7.141 0.16 76106. 0.1693 24.11 0.6365 0.7068 0.0274 0.0247 0.051 1.601 0.558 37.876 0.181 2.484 6.687 0.16 76323. 0.1466 25.16 0.6642 0.6807 0.0227 0.0222 0.046 1.439 0.463 34.041 0.163 2.060 6.172 0.16 76547. 0.1232 26.21 0.6918 0.6393 0.0180 0.0195 0.040 1.268 0.368 29.998 0.143 1.637 5.565 0.16 76780. 0.0990 27.25 0.7195 0.5750 0.0134 0.0168 0.035 1.089 0.273 25.774 0.123 1.216 4.812 0.16 77020. 0.0738 28.30 0.7472 0.4735 0.0088 0.0139 0.029 0.904 0.180 21.397 0.102 0.801 3.816 0.16 77268. 0.0475 29.35 0.7749 0.3054 0.0043 0.0110 0.023 0.714 0.088 16.903 0.081 0.393 2.373 0.16 77524. 0.0207 30.40 0.8025 -0.0036 0.0000 0.0080 0.017 0.521 -0.001 12.326 0.059 -0.003 -0.027 0.16 77786. 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 0.0961 0.0348 0.242 5.080 4.410 180.312 0.574 19.614 11.092 0.24 109947. 0.6833 1.57 0.0277 0.0742 0.0950 0.0355 0.247 5.183 4.359 183.968 0.586 19.389 10.747 0.24 110028. 0.6583 3.15 0.0554 0.1436 0.0938 0.0362 0.252 5.285 4.303 187.579 0.597 19.140 10.405 0.24 110117. 0.6332 4.72 0.0831 0.2085 0.0924 0.0369 0.256 5.384 4.241 191.083 0.608 18.864 10.067 0.24 110215. 0.6082 6.30 0.1109 0.2688 0.0909 0.0375 0.261 5.477 4.172 194.410 0.619 18.559 9.735 0.24 110323. 0.5834 7.87 0.1386 0.3248 0.0893 0.0381 0.265 5.564 4.097 197.486 0.629 18.223 9.409 0.24 110440. 0.5587 9.45 0.1663 0.3766 0.0875 0.0386 0.269 5.641 4.014 200.231 0.637 17.853 9.092 0.24 110568. 0.5344 11.02 0.1940 0.4244 0.0855 0.0391 0.272 5.707 3.922 202.558 0.645 17.447 8.783 0.24 110706. 0.5103 12.60 0.2217 0.4685 0.0833 0.0394 0.274 5.758 3.823 204.379 0.651 17.004 8.484 0.24 110855. 0.4866 14.17 0.2494 0.5090 0.0809 0.0397 0.276 5.793 3.714 205.601 0.654 16.521 8.194 0.24 111015. 0.4633 15.75 0.2771 0.5462 0.0784 0.0398 0.276 5.808 3.596 206.132 0.656 15.996 7.913 0.24 111186. 0.4403 17.32 0.3048 0.5803 0.0756 0.0397 0.276 5.801 3.469 205.882 0.655 15.429 7.642 0.24 111369. 0.4176 18.89 0.3326 0.6113 0.0726 0.0395 0.275 5.769 3.332 204.761 0.652 14.819 7.380 0.24 111564. 0.3952 20.47 0.3603 0.6395 0.0694 0.0391 0.272 5.711 3.184 202.687 0.645 14.164 7.126 0.24 111771. 0.3731 22.04 0.3880 0.6648 0.0660 0.0385 0.268 5.623 3.027 199.577 0.635 13.464 6.879 0.24 111989. 0.3511 23.62 0.4157 0.6874 0.0623 0.0377 0.262 5.504 2.859 195.345 0.622 12.718 6.639 0.24 112220. 0.3293 25.19 0.4434 0.7072 0.0584 0.0366 0.255 5.352 2.682 189.955 0.605 11.928 6.403 0.24 112463. 0.3076 26.77 0.4711 0.7241 0.0544 0.0354 0.246 5.168 2.495 183.429 0.584 11.100 6.171 0.24 112717. 0.2860 28.34 0.4988 0.7379 0.0502 0.0339 0.236 4.953 2.302 175.809 0.560 10.239 5.939 0.24 112984. 0.2643 29.92 0.5265 0.7482 0.0458 0.0322 0.224 4.709 2.102 167.138 0.532 9.350 5.705 0.24 113262. 0.2427 31.49 0.5543 0.7545 0.0413 0.0304 0.211 4.436 1.897 157.459 0.501 8.439 5.465 0.24 113553. 0.2209 33.07 0.5820 0.7561 0.0368 0.0283 0.197 4.136 1.688 146.815 0.467 7.510 5.216 0.24 113855. 0.1988 34.64 0.6097 0.7518 0.0322 0.0261 0.181 3.811 1.476 135.253 0.431 6.566 4.950 0.24 114169. 0.1765 36.22 0.6374 0.7399 0.0275 0.0237 0.165 3.461 1.262 122.826 0.391 5.613 4.660 0.24 114495. 0.1536 37.79 0.6651 0.7177 0.0228 0.0211 0.147 3.088 1.047 109.596 0.349 4.656 4.332 0.24 114833. 0.1300 39.36 0.6928 0.6807 0.0181 0.0184 0.128 2.695 0.832 95.638 0.304 3.700 3.945 0.24 115182. 0.1055 40.94 0.7205 0.6209 0.0135 0.0156 0.109 2.283 0.618 81.041 0.258 2.749 3.459 0.24 115543. 0.0798 42.51 0.7482 0.5223 0.0089 0.0127 0.088 1.857 0.407 65.908 0.210 1.811 2.802 0.24 115917. 0.0525 44.09 0.7760 0.3492 0.0044 0.0097 0.068 1.419 0.201 50.365 0.160 0.892 1.807 0.25 116301. 0.0237 45.66 0.8037 -0.0011 0.0000 0.0067 0.046 0.973 0.000 34.528 0.110 -0.002 -0.006 0.25 116694. 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 0.0966 0.0343 0.565 8.907 7.878 421.538 1.006 35.039 8.476 0.32 146591. 0.6980 2.10 0.0277 0.0756 0.0955 0.0350 0.577 9.095 7.789 430.403 1.028 34.645 8.208 0.32 146699. 0.6721 4.20 0.0555 0.1463 0.0943 0.0357 0.589 9.280 7.690 439.173 1.048 34.206 7.942 0.32 146818. 0.6462 6.30 0.0832 0.2122 0.0929 0.0364 0.600 9.460 7.581 447.694 1.069 33.720 7.680 0.32 146949. 0.6204 8.40 0.1109 0.2735 0.0914 0.0371 0.611 9.631 7.460 455.801 1.088 33.181 7.423 0.32 147093. 0.5948 10.50 0.1386 0.3302 0.0898 0.0377 0.621 9.790 7.326 463.313 1.106 32.586 7.172 0.32 147250. 0.5695 12.60 0.1664 0.3828 0.0880 0.0382 0.630 9.932 7.179 470.036 1.122 31.930 6.927 0.32 147420. 0.5445 14.70 0.1941 0.4312 0.0860 0.0387 0.638 10.053 7.017 475.762 1.136 31.210 6.689 0.32 147604. 0.5199 16.81 0.2218 0.4759 0.0838 0.0391 0.644 10.148 6.839 480.274 1.147 30.422 6.459 0.32 147803. 0.4956 18.91 0.2496 0.5169 0.0815 0.0393 0.648 10.214 6.646 483.351 1.154 29.562 6.237 0.32 148017. 0.4717 21.01 0.2773 0.5546 0.0789 0.0394 0.650 10.243 6.436 484.768 1.157 28.628 6.022 0.32 148246. 0.4482 23.11 0.3050 0.5891 0.0761 0.0394 0.649 10.234 6.209 484.304 1.156 27.618 5.815 0.32 148491. 0.4251 25.21 0.3327 0.6206 0.0731 0.0392 0.646 10.180 5.964 481.745 1.150 26.528 5.615 0.32 148751. 0.4023 27.31 0.3605 0.6492 0.0699 0.0388 0.640 10.077 5.701 476.888 1.138 25.359 5.422 0.32 149027. 0.3798 29.41 0.3882 0.6750 0.0664 0.0382 0.630 9.921 5.420 469.532 1.121 24.107 5.236 0.32 149319. 0.3576 31.51 0.4159 0.6982 0.0628 0.0374 0.616 9.709 5.120 459.470 1.097 22.773 5.054 0.32 149627. 0.3355 33.61 0.4437 0.7186 0.0589 0.0363 0.599 9.437 4.802 446.604 1.066 21.360 4.877 0.32 149952. 0.3136 35.71 0.4714 0.7363 0.0548 0.0351 0.578 9.107 4.469 430.987 1.029 19.878 4.703 0.32 150292. 0.2917 37.81 0.4991 0.7510 0.0505 0.0336 0.553 8.721 4.123 412.715 0.985 18.337 4.531 0.32 150648. 0.2699 39.91 0.5269 0.7625 0.0461 0.0319 0.526 8.281 3.765 391.887 0.936 16.746 4.357 0.32 151020. 0.2481 42.01 0.5546 0.7701 0.0417 0.0300 0.494 7.789 3.398 368.603 0.880 15.114 4.181 0.32 151407. 0.2261 44.11 0.5823 0.7733 0.0371 0.0279 0.460 7.247 3.024 342.968 0.819 13.449 3.999 0.32 151811. 0.2040 46.22 0.6100 0.7710 0.0324 0.0256 0.423 6.658 2.644 315.095 0.752 11.759 3.806 0.32 152230. 0.1815 48.32 0.6378 0.7616 0.0277 0.0232 0.382 6.025 2.260 285.111 0.681 10.053 3.595 0.32 152665. 0.1586 50.42 0.6655 0.7423 0.0230 0.0206 0.340 5.350 1.875 253.168 0.604 8.338 3.359 0.32 153116. 0.1349 52.52 0.6932 0.7088 0.0183 0.0179 0.294 4.637 1.489 219.447 0.524 6.625 3.079 0.32 153583. 0.1102 54.62 0.7210 0.6528 0.0136 0.0150 0.247 3.891 1.107 184.164 0.440 4.924 2.726 0.33 154065. 0.0841 56.72 0.7487 0.5575 0.0089 0.0120 0.198 3.118 0.729 147.578 0.352 3.245 2.242 0.33 154563. 0.0562 58.82 0.7764 0.3826 0.0044 0.0090 0.148 2.324 0.360 109.994 0.263 1.600 1.484 0.33 155077. 0.0261 60.92 0.8041 0.0002 0.0000 0.0058 0.096 1.515 0.000 71.687 0.171 0.000 0.001 0.33 155601. 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 0.0971 0.0341 1.098 13.847 12.384 819.133 1.564 55.083 6.857 0.40 183231. 0.7079 2.63 0.0277 0.0765 0.0961 0.0349 1.122 14.146 12.247 836.827 1.598 54.476 6.638 0.40 183366. 0.6816 5.25 0.0555 0.1479 0.0949 0.0356 1.146 14.442 12.095 854.354 1.632 53.800 6.421 0.40 183515. 0.6552 7.88 0.0832 0.2145 0.0936 0.0363 1.169 14.731 11.926 871.404 1.664 53.048 6.208 0.40 183679. 0.6289 10.51 0.1110 0.2763 0.0921 0.0370 1.190 15.005 11.739 887.648 1.695 52.213 5.998 0.40 183859. 0.6029 13.14 0.1387 0.3336 0.0905 0.0376 1.211 15.260 11.531 902.727 1.724 51.289 5.794 0.40 184055. 0.5772 15.76 0.1665 0.3866 0.0887 0.0382 1.229 15.489 11.301 916.250 1.750 50.269 5.595 0.40 184268. 0.5518 18.39 0.1942 0.4355 0.0867 0.0387 1.244 15.684 11.049 927.802 1.772 49.147 5.402 0.40 184499. 0.5268 21.02 0.2219 0.4805 0.0845 0.0390 1.256 15.839 10.773 936.951 1.789 47.916 5.215 0.40 184749. 0.5022 23.64 0.2497 0.5219 0.0821 0.0393 1.265 15.945 10.470 943.253 1.801 46.572 5.035 0.40 185017. 0.4780 26.27 0.2774 0.5599 0.0796 0.0394 1.269 15.996 10.142 946.259 1.807 45.110 4.861 0.40 185304. 0.4542 28.90 0.3052 0.5947 0.0768 0.0394 1.268 15.984 9.785 945.525 1.806 43.525 4.694 0.40 185610. 0.4308 31.53 0.3329 0.6265 0.0737 0.0392 1.261 15.901 9.401 940.627 1.796 41.815 4.533 0.40 185936. 0.4078 34.15 0.3607 0.6555 0.0705 0.0388 1.249 15.741 8.988 931.157 1.778 39.977 4.378 0.40 186282. 0.3851 36.78 0.3884 0.6818 0.0670 0.0382 1.229 15.497 8.545 916.716 1.751 38.010 4.228 0.40 186648. 0.3626 39.41 0.4161 0.7054 0.0633 0.0374 1.203 15.161 8.073 896.890 1.713 35.910 4.083 0.40 187034. 0.3403 42.04 0.4439 0.7263 0.0594 0.0363 1.169 14.732 7.573 871.472 1.664 33.685 3.941 0.40 187440. 0.3182 44.66 0.4716 0.7446 0.0553 0.0350 1.127 14.209 7.048 840.557 1.605 31.349 3.803 0.40 187866. 0.2962 47.29 0.4994 0.7601 0.0510 0.0335 1.079 13.597 6.502 804.332 1.536 28.919 3.666 0.40 188312. 0.2743 49.92 0.5271 0.7724 0.0466 0.0318 1.023 12.898 5.937 762.992 1.457 26.410 3.530 0.40 188777. 0.2523 52.54 0.5549 0.7811 0.0420 0.0299 0.961 12.116 5.358 716.735 1.369 23.834 3.391 0.40 189263. 0.2303 55.17 0.5826 0.7856 0.0374 0.0277 0.893 11.254 4.768 665.768 1.272 21.207 3.248 0.40 189768. 0.2081 57.80 0.6103 0.7849 0.0327 0.0254 0.818 10.317 4.168 610.313 1.166 18.539 3.097 0.40 190293. 0.1855 60.43 0.6381 0.7773 0.0279 0.0229 0.738 9.308 3.562 550.628 1.052 15.844 2.934 0.40 190838. 0.1625 63.05 0.6658 0.7603 0.0232 0.0203 0.653 8.233 2.954 487.015 0.930 13.137 2.751 0.41 191402. 0.1387 65.68 0.6936 0.7296 0.0184 0.0175 0.563 7.097 2.345 419.838 0.802 10.432 2.534 0.41 191986. 0.1138 68.31 0.7213 0.6767 0.0137 0.0146 0.469 5.909 1.741 349.532 0.668 7.745 2.260 0.41 192590. 0.0875 70.93 0.7491 0.5840 0.0090 0.0115 0.371 4.676 1.145 276.622 0.528 5.095 1.878 0.41 193213. 0.0590 73.56 0.7768 0.4075 0.0044 0.0084 0.271 3.410 0.562 201.724 0.385 2.499 1.263 0.41 193855. 0.0278 76.19 0.8046 -0.0070 0.0000 0.0052 0.168 2.119 -0.006 125.367 0.239 -0.026 -0.021 0.41 194510. 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 0.0979 0.0342 1.900 19.962 17.965 1417.010 2.255 79.909 5.750 0.48 219864. 0.7151 3.15 0.0277 0.0769 0.0968 0.0349 1.942 20.402 17.773 1448.265 2.305 79.055 5.566 0.48 220026. 0.6885 6.30 0.0554 0.1487 0.0957 0.0357 1.984 20.839 17.558 1479.265 2.354 78.099 5.384 0.48 220205. 0.6618 9.45 0.0832 0.2156 0.0943 0.0364 2.024 21.264 17.319 1509.458 2.402 77.034 5.204 0.48 220402. 0.6354 12.60 0.1109 0.2778 0.0929 0.0371 2.063 21.670 17.052 1538.271 2.448 75.848 5.028 0.48 220618. 0.6091 15.75 0.1386 0.3353 0.0913 0.0377 2.099 22.047 16.756 1565.061 2.491 74.532 4.856 0.48 220854. 0.5832 18.90 0.1663 0.3886 0.0895 0.0383 2.131 22.386 16.429 1589.138 2.529 73.075 4.689 0.48 221110. 0.5576 22.05 0.1941 0.4377 0.0875 0.0388 2.159 22.677 16.068 1609.769 2.562 71.469 4.527 0.48 221387. 0.5324 25.20 0.2218 0.4829 0.0854 0.0392 2.181 22.908 15.671 1626.188 2.588 69.703 4.371 0.48 221687. 0.5076 28.35 0.2495 0.5246 0.0830 0.0395 2.196 23.069 15.236 1637.608 2.606 67.771 4.220 0.48 222008. 0.4833 31.50 0.2772 0.5628 0.0804 0.0396 2.204 23.148 14.763 1643.240 2.615 65.666 4.075 0.48 222353. 0.4593 34.65 0.3050 0.5979 0.0776 0.0396 2.202 23.135 14.249 1642.301 2.614 63.380 3.935 0.48 222721. 0.4358 37.80 0.3327 0.6300 0.0746 0.0394 2.191 23.019 13.694 1634.035 2.601 60.909 3.801 0.48 223113. 0.4127 40.96 0.3604 0.6593 0.0713 0.0390 2.169 22.789 13.096 1617.728 2.575 58.251 3.672 0.48 223528. 0.3898 44.11 0.3881 0.6859 0.0679 0.0384 2.136 22.436 12.456 1592.680 2.535 55.403 3.547 0.48 223967. 0.3673 47.26 0.4159 0.7099 0.0641 0.0376 2.090 21.950 11.771 1558.159 2.480 52.360 3.427 0.48 224431. 0.3449 50.41 0.4436 0.7313 0.0602 0.0365 2.030 21.325 11.046 1513.771 2.409 49.130 3.310 0.48 224918. 0.3227 53.56 0.4713 0.7502 0.0560 0.0352 1.957 20.562 10.283 1459.664 2.323 45.738 3.195 0.48 225429. 0.3006 56.71 0.4990 0.7663 0.0517 0.0337 1.872 19.668 9.489 1396.158 2.222 42.205 3.083 0.48 225964. 0.2786 59.86 0.5267 0.7795 0.0472 0.0319 1.775 18.646 8.668 1323.598 2.107 38.555 2.970 0.48 226523. 0.2566 63.01 0.5545 0.7892 0.0426 0.0300 1.666 17.501 7.825 1242.331 1.977 34.806 2.857 0.48 227105. 0.2345 66.16 0.5822 0.7948 0.0379 0.0278 1.546 16.238 6.965 1152.717 1.835 30.979 2.740 0.48 227711. 0.2122 69.31 0.6099 0.7955 0.0332 0.0254 1.415 14.864 6.091 1055.152 1.679 27.092 2.618 0.48 228340. 0.1896 72.46 0.6376 0.7898 0.0284 0.0229 1.274 13.384 5.208 950.087 1.512 23.165 2.486 0.49 228994. 0.1665 75.61 0.6654 0.7751 0.0235 0.0202 1.124 11.806 4.321 838.057 1.334 19.218 2.338 0.49 229670. 0.1426 78.76 0.6931 0.7471 0.0187 0.0174 0.965 10.138 3.433 719.702 1.145 15.272 2.164 0.49 230370. 0.1176 81.91 0.7208 0.6977 0.0139 0.0144 0.799 8.393 2.552 595.795 0.948 11.352 1.943 0.49 231094. 0.0911 85.06 0.7485 0.6091 0.0092 0.0113 0.627 6.582 1.683 467.266 0.744 7.484 1.633 0.49 231841. 0.0622 88.21 0.7763 0.4349 0.0045 0.0081 0.450 4.722 0.831 335.213 0.534 3.697 1.125 0.49 232611. 0.0301 91.36 0.8040 0.0023 0.0000 0.0048 0.269 2.826 0.003 200.584 0.319 0.011 0.006 0.49 233395. 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 0.0987 0.0344 3.036 27.338 24.670 2264.120 3.089 109.732 4.942 0.56 256490. 0.7202 3.67 0.0277 0.0771 0.0977 0.0351 3.105 27.953 24.416 2315.037 3.158 108.603 4.784 0.56 256679. 0.6935 7.35 0.0554 0.1491 0.0966 0.0359 3.172 28.564 24.131 2365.609 3.227 107.335 4.627 0.56 256888. 0.6668 11.02 0.0831 0.2161 0.0953 0.0367 3.238 29.160 23.812 2414.944 3.294 105.916 4.472 0.56 257118. 0.6403 14.70 0.1109 0.2784 0.0939 0.0374 3.302 29.729 23.456 2462.098 3.359 104.331 4.321 0.56 257370. 0.6140 18.37 0.1386 0.3361 0.0923 0.0380 3.361 30.259 23.059 2506.014 3.419 102.565 4.173 0.56 257646. 0.5880 22.05 0.1663 0.3895 0.0905 0.0386 3.414 30.737 22.618 2545.563 3.473 100.603 4.030 0.56 257945. 0.5623 25.72 0.1940 0.4388 0.0886 0.0392 3.459 31.147 22.130 2579.541 3.519 98.433 3.891 0.56 258269. 0.5370 29.40 0.2217 0.4842 0.0864 0.0396 3.496 31.475 21.592 2606.691 3.556 96.041 3.757 0.56 258619. 0.5122 33.07 0.2494 0.5260 0.0841 0.0399 3.521 31.705 21.002 2625.733 3.582 93.417 3.628 0.56 258995. 0.4878 36.75 0.2772 0.5644 0.0815 0.0400 3.534 31.821 20.357 2635.372 3.595 90.549 3.504 0.56 259398. 0.4638 40.42 0.3049 0.5997 0.0787 0.0400 3.533 31.809 19.656 2634.333 3.594 87.429 3.384 0.56 259828. 0.4402 44.09 0.3326 0.6320 0.0756 0.0398 3.515 31.652 18.896 2621.384 3.576 84.051 3.270 0.56 260286. 0.4170 47.77 0.3603 0.6616 0.0724 0.0394 3.480 31.338 18.078 2595.363 3.541 80.410 3.159 0.56 260771. 0.3941 51.44 0.3880 0.6885 0.0688 0.0388 3.426 30.852 17.199 2555.140 3.486 76.502 3.053 0.56 261285. 0.3715 55.12 0.4157 0.7129 0.0651 0.0379 3.352 30.181 16.260 2499.533 3.410 72.322 2.950 0.56 261826. 0.3490 58.79 0.4435 0.7348 0.0611 0.0369 3.256 29.315 15.261 2427.857 3.312 67.881 2.851 0.56 262395. 0.3268 62.47 0.4712 0.7542 0.0569 0.0355 3.138 28.258 14.211 2340.315 3.193 63.209 2.754 0.56 262992. 0.3046 66.14 0.4989 0.7710 0.0525 0.0340 3.000 27.016 13.116 2237.425 3.052 58.339 2.659 0.56 263617. 0.2825 69.82 0.5266 0.7848 0.0480 0.0322 2.843 25.595 11.983 2119.753 2.892 53.303 2.564 0.56 264269. 0.2604 73.49 0.5543 0.7954 0.0433 0.0302 2.666 24.003 10.820 1987.864 2.712 48.127 2.469 0.56 264949. 0.2382 77.16 0.5820 0.8021 0.0385 0.0280 2.471 22.246 9.631 1842.345 2.513 42.839 2.371 0.56 265656. 0.2159 80.84 0.6098 0.8041 0.0337 0.0256 2.258 20.332 8.423 1683.842 2.297 37.465 2.269 0.57 266391. 0.1932 84.51 0.6375 0.7998 0.0288 0.0230 2.029 18.270 7.202 1513.094 2.064 32.033 2.159 0.57 267153. 0.1700 88.19 0.6652 0.7870 0.0239 0.0202 1.785 16.071 5.974 1330.969 1.816 26.570 2.036 0.57 267943. 0.1460 91.86 0.6929 0.7614 0.0190 0.0173 1.527 13.747 4.746 1138.519 1.553 21.108 1.891 0.57 268759. 0.1208 95.54 0.7206 0.7147 0.0141 0.0142 1.257 11.314 3.525 937.009 1.278 15.680 1.706 0.57 269604. 0.0940 99.21 0.7483 0.6289 0.0093 0.0111 0.976 8.790 2.321 727.969 0.993 10.323 1.446 0.57 270475. 0.0646 102.89 0.7761 0.4550 0.0046 0.0078 0.688 6.197 1.141 513.206 0.700 5.077 1.009 0.57 271373. 0.0316 106.56 0.8038 -0.0048 0.0000 0.0045 0.395 3.553 -0.007 294.226 0.401 -0.029 -0.010 0.57 272285. 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 0.0998 0.0348 4.582 36.099 32.559 3416.778 4.078 144.823 4.322 0.63 293106. 0.7236 4.20 0.0277 0.0770 0.0988 0.0355 4.687 36.926 32.241 3495.053 4.172 143.408 4.184 0.63 293322. 0.6970 8.39 0.0554 0.1489 0.0977 0.0363 4.791 37.749 31.882 3572.958 4.265 141.811 4.047 0.63 293561. 0.6705 12.59 0.0831 0.2159 0.0965 0.0371 4.894 38.554 31.478 3649.100 4.356 140.014 3.913 0.63 293824. 0.6440 16.78 0.1108 0.2782 0.0951 0.0379 4.991 39.324 31.025 3722.023 4.443 137.997 3.781 0.64 294112. 0.6178 20.98 0.1385 0.3359 0.0935 0.0385 5.083 40.043 30.517 3790.089 4.524 135.738 3.652 0.64 294427. 0.5919 25.18 0.1662 0.3893 0.0918 0.0392 5.165 40.693 29.950 3851.533 4.597 133.218 3.527 0.64 294769. 0.5663 29.37 0.1939 0.4386 0.0898 0.0397 5.236 41.252 29.321 3904.491 4.661 130.418 3.406 0.64 295141. 0.5411 33.57 0.2216 0.4841 0.0877 0.0401 5.293 41.701 28.624 3947.013 4.711 127.319 3.289 0.64 295541. 0.5163 37.77 0.2493 0.5260 0.0854 0.0405 5.333 42.019 27.857 3977.114 4.747 123.906 3.177 0.64 295972. 0.4919 41.96 0.2770 0.5646 0.0828 0.0406 5.354 42.185 27.015 3992.797 4.766 120.165 3.069 0.64 296433. 0.4680 46.16 0.3046 0.6000 0.0800 0.0406 5.353 42.178 26.098 3992.098 4.765 116.083 2.965 0.64 296925. 0.4444 50.35 0.3323 0.6326 0.0769 0.0404 5.328 41.977 25.102 3973.130 4.743 111.652 2.866 0.64 297449. 0.4212 54.55 0.3600 0.6624 0.0736 0.0400 5.276 41.565 24.026 3934.104 4.696 106.866 2.770 0.64 298005. 0.3983 58.75 0.3877 0.6897 0.0701 0.0394 5.194 40.923 22.869 3873.308 4.623 101.720 2.678 0.64 298592. 0.3757 62.94 0.4154 0.7145 0.0663 0.0385 5.081 40.031 21.629 3788.947 4.523 96.206 2.589 0.64 299211. 0.3533 67.14 0.4431 0.7368 0.0622 0.0374 4.935 38.879 20.310 3679.889 4.393 90.337 2.503 0.64 299862. 0.3310 71.34 0.4708 0.7567 0.0580 0.0361 4.756 37.469 18.919 3546.383 4.233 84.152 2.420 0.64 300545. 0.3088 75.53 0.4985 0.7741 0.0535 0.0345 4.545 35.808 17.468 3389.226 4.046 77.697 2.338 0.64 301259. 0.2866 79.73 0.5262 0.7886 0.0489 0.0326 4.304 33.907 15.965 3209.286 3.831 71.012 2.256 0.64 302005. 0.2645 83.92 0.5539 0.8001 0.0442 0.0306 4.033 31.775 14.419 3007.444 3.590 64.135 2.175 0.64 302782. 0.2423 88.12 0.5816 0.8078 0.0393 0.0283 3.734 29.420 12.838 2784.610 3.324 57.103 2.091 0.65 303590. 0.2198 92.32 0.6093 0.8110 0.0344 0.0259 3.409 26.855 11.230 2541.780 3.034 49.952 2.004 0.65 304430. 0.1970 96.51 0.6370 0.8083 0.0294 0.0232 3.058 24.090 9.604 2280.086 2.722 42.717 1.910 0.65 305300. 0.1737 100.71 0.6647 0.7974 0.0244 0.0204 2.683 21.140 7.967 2000.870 2.388 35.437 1.806 0.65 306202. 0.1496 104.91 0.6924 0.7740 0.0194 0.0173 2.287 18.022 6.330 1705.747 2.036 28.154 1.683 0.65 307135. 0.1242 109.10 0.7201 0.7303 0.0144 0.0142 1.873 14.756 4.701 1396.672 1.667 20.912 1.527 0.65 308099. 0.0971 113.30 0.7478 0.6477 0.0095 0.0109 1.443 11.368 3.094 1076.013 1.284 13.761 1.304 0.65 309093. 0.0673 117.49 0.7755 0.4754 0.0047 0.0076 1.001 7.888 1.519 746.581 0.891 6.757 0.923 0.65 310118. 0.0334 121.69 0.8032 -0.0082 0.0000 0.0042 0.551 4.339 -0.014 410.695 0.490 -0.062 -0.015 0.66 311159. 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 0.1010 0.0355 6.669 46.704 41.704 4973.071 5.277 185.501 3.804 0.71 329710. 0.7207 4.71 0.0277 0.0762 0.1001 0.0363 6.817 47.742 41.325 5083.616 5.394 183.815 3.687 0.71 329953. 0.6954 9.43 0.0553 0.1476 0.0990 0.0371 6.965 48.780 40.895 5194.104 5.511 181.900 3.571 0.71 330221. 0.6700 14.14 0.0830 0.2143 0.0978 0.0379 7.111 49.799 40.407 5302.612 5.626 179.729 3.456 0.71 330516. 0.6446 18.86 0.1106 0.2764 0.0965 0.0386 7.251 50.780 39.855 5407.037 5.737 177.274 3.343 0.71 330841. 0.6192 23.57 0.1383 0.3341 0.0950 0.0393 7.382 51.700 39.233 5505.048 5.841 174.507 3.232 0.71 331195. 0.5940 28.29 0.1660 0.3875 0.0933 0.0400 7.502 52.536 38.534 5594.082 5.936 171.399 3.124 0.71 331580. 0.5690 33.00 0.1936 0.4369 0.0914 0.0405 7.605 53.262 37.752 5671.350 6.017 167.923 3.019 0.72 331998. 0.5443 37.72 0.2213 0.4824 0.0893 0.0410 7.689 53.850 36.883 5733.944 6.084 164.055 2.918 0.72 332449. 0.5198 42.43 0.2489 0.5245 0.0870 0.0413 7.750 54.271 35.920 5778.859 6.132 159.774 2.819 0.72 332934. 0.4957 47.15 0.2766 0.5632 0.0844 0.0415 7.782 54.498 34.860 5803.025 6.157 155.059 2.725 0.72 333454. 0.4720 51.86 0.3043 0.5988 0.0816 0.0415 7.782 54.502 33.699 5803.404 6.158 149.895 2.634 0.72 334008. 0.4486 56.58 0.3319 0.6316 0.0785 0.0413 7.747 54.255 32.435 5777.053 6.130 144.269 2.547 0.72 334598. 0.4255 61.29 0.3596 0.6617 0.0752 0.0409 7.672 53.730 31.064 5721.236 6.070 138.174 2.463 0.72 335224. 0.4027 66.01 0.3872 0.6893 0.0716 0.0402 7.555 52.906 29.587 5633.425 5.977 131.604 2.382 0.72 335885. 0.3802 70.72 0.4149 0.7145 0.0678 0.0394 7.390 51.756 28.001 5511.037 5.847 124.549 2.305 0.72 336582. 0.3578 75.44 0.4426 0.7373 0.0637 0.0382 7.177 50.265 26.309 5352.261 5.679 117.022 2.230 0.72 337315. 0.3355 80.15 0.4702 0.7578 0.0594 0.0368 6.916 48.435 24.522 5157.350 5.472 109.072 2.157 0.72 338084. 0.3133 84.87 0.4979 0.7758 0.0548 0.0352 6.608 46.276 22.653 4927.462 5.228 100.759 2.085 0.72 338887. 0.2912 89.58 0.5255 0.7911 0.0502 0.0333 6.254 43.801 20.714 4663.906 4.949 92.137 2.014 0.72 339726. 0.2690 94.30 0.5532 0.8035 0.0453 0.0312 5.858 41.022 18.717 4367.995 4.635 83.255 1.944 0.72 340600. 0.2467 99.01 0.5809 0.8123 0.0404 0.0289 5.419 37.951 16.673 4041.095 4.288 74.161 1.871 0.73 341509. 0.2242 103.73 0.6085 0.8168 0.0353 0.0263 4.941 34.605 14.591 3684.726 3.910 64.903 1.796 0.73 342453. 0.2013 108.44 0.6362 0.8155 0.0302 0.0236 4.426 30.998 12.484 3300.667 3.502 55.527 1.715 0.73 343431. 0.1778 113.16 0.6638 0.8063 0.0251 0.0207 3.877 27.151 10.360 2891.042 3.067 46.083 1.625 0.73 344444. 0.1535 117.87 0.6915 0.7850 0.0199 0.0176 3.297 23.088 8.234 2458.477 2.609 36.626 1.519 0.73 345492. 0.1279 122.59 0.7192 0.7434 0.0148 0.0143 2.690 18.841 6.118 2006.232 2.129 27.214 1.383 0.73 346574. 0.1004 127.30 0.7468 0.6627 0.0098 0.0110 2.063 14.447 4.027 1538.345 1.632 17.913 1.187 0.73 347691. 0.0699 132.02 0.7745 0.4898 0.0048 0.0076 1.421 9.952 1.977 1059.687 1.124 8.795 0.846 0.74 348842. 0.0349 136.73 0.8022 -0.0093 0.0000 0.0041 0.770 5.395 -0.020 574.443 0.610 -0.087 -0.016 0.74 350009. 0.0000 PROP RPM = 10000 V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM (mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - - 0.00 0.0000 0.0000 0.1023 0.0382 9.835 61.987 52.163 7333.817 7.003 232.023 3.226 0.79 366299. 0.6836 5.23 0.0276 0.0720 0.1015 0.0389 10.016 63.128 51.737 7468.777 7.132 230.124 3.142 0.79 366567. 0.6630 10.46 0.0552 0.1401 0.1005 0.0396 10.195 64.258 51.247 7602.425 7.260 227.946 3.057 0.79 366864. 0.6421 15.68 0.0828 0.2044 0.0994 0.0403 10.369 65.354 50.686 7732.166 7.384 225.453 2.973 0.79 367191. 0.6210 20.91 0.1104 0.2649 0.0982 0.0409 10.534 66.395 50.046 7855.268 7.501 222.607 2.890 0.79 367551. 0.5998 26.14 0.1380 0.3217 0.0967 0.0415 10.686 67.353 49.318 7968.700 7.610 219.367 2.807 0.79 367944. 0.5784 31.37 0.1656 0.3748 0.0951 0.0420 10.821 68.203 48.493 8069.221 7.706 215.696 2.726 0.79 368371. 0.5569 36.59 0.1932 0.4245 0.0933 0.0425 10.934 68.914 47.562 8153.358 7.786 211.554 2.646 0.79 368835. 0.5353 41.82 0.2208 0.4707 0.0912 0.0428 11.020 69.457 46.517 8217.535 7.847 206.908 2.568 0.80 369336. 0.5138 47.05 0.2484 0.5138 0.0889 0.0430 11.074 69.799 45.352 8258.004 7.886 201.725 2.491 0.80 369875. 0.4921 52.28 0.2760 0.5537 0.0864 0.0431 11.092 69.909 44.060 8271.010 7.898 195.979 2.416 0.80 370453. 0.4705 57.50 0.3036 0.5907 0.0836 0.0430 11.067 69.755 42.636 8252.813 7.881 189.647 2.343 0.80 371070. 0.4489 62.73 0.3312 0.6249 0.0806 0.0427 10.996 69.306 41.077 8199.690 7.830 182.711 2.272 0.80 371726. 0.4273 67.96 0.3588 0.6563 0.0772 0.0422 10.873 68.531 39.380 8108.003 7.743 175.162 2.203 0.80 372421. 0.4056 73.19 0.3864 0.6852 0.0736 0.0415 10.694 67.399 37.543 7974.149 7.615 166.993 2.135 0.80 373156. 0.3839 78.41 0.4140 0.7115 0.0697 0.0406 10.452 65.879 35.565 7794.271 7.443 158.192 2.070 0.80 373931. 0.3621 83.64 0.4416 0.7353 0.0656 0.0394 10.145 63.943 33.447 7565.170 7.224 148.770 2.005 0.80 374745. 0.3402 88.87 0.4692 0.7567 0.0612 0.0379 9.772 61.589 31.202 7286.676 6.958 138.788 1.942 0.80 375598. 0.3183 94.10 0.4968 0.7755 0.0566 0.0362 9.334 58.830 28.849 6960.241 6.647 128.320 1.880 0.80 376491. 0.2962 99.32 0.5244 0.7916 0.0518 0.0343 8.834 55.679 26.402 6587.455 6.291 117.438 1.818 0.80 377422. 0.2740 104.55 0.5520 0.8045 0.0468 0.0321 8.274 52.150 23.877 6169.923 5.892 106.205 1.755 0.81 378392. 0.2516 109.78 0.5796 0.8138 0.0417 0.0297 7.657 48.262 21.287 5709.939 5.453 94.684 1.691 0.81 379400. 0.2289 115.01 0.6072 0.8183 0.0366 0.0271 6.987 44.040 18.645 5210.417 4.976 82.935 1.623 0.81 380447. 0.2056 120.23 0.6348 0.8165 0.0313 0.0243 6.269 39.513 15.966 4674.799 4.464 71.017 1.549 0.81 381531. 0.1816 125.46 0.6624 0.8055 0.0260 0.0214 5.508 34.717 13.263 4107.486 3.922 58.992 1.465 0.81 382654. 0.1565 130.69 0.6900 0.7803 0.0207 0.0183 4.712 29.699 10.551 3513.726 3.355 46.929 1.362 0.81 383815. 0.1298 135.92 0.7176 0.7313 0.0154 0.0151 3.889 24.511 7.847 2899.953 2.769 34.904 1.227 0.81 385014. 0.1009 141.14 0.7452 0.6382 0.0101 0.0118 3.049 19.217 5.170 2273.609 2.171 22.997 1.031 0.82 386251. 0.0688 146.37 0.7728 0.4500 0.0050 0.0086 2.204 13.889 2.541 1643.245 1.569 11.302 0.701 0.82 387525. 0.0328 151.60 0.8004 -0.0073 0.0000 0.0053 1.363 8.588 -0.025 1016.038 0.970 -0.110 -0.011 0.82 388821. 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 0.1034 0.0449 15.375 88.095 63.801 11464.945 9.953 283.785 2.524 0.87 402879. 0.5915 5.75 0.0276 0.0624 0.1027 0.0455 15.580 89.272 63.354 11618.145 10.086 281.797 2.473 0.87 403172. 0.5776 11.51 0.0552 0.1222 0.1018 0.0460 15.776 90.395 62.834 11764.287 10.213 279.487 2.423 0.87 403497. 0.5634 17.26 0.0829 0.1795 0.1009 0.0466 15.957 91.431 62.231 11899.058 10.330 276.805 2.372 0.87 403855. 0.5490 23.02 0.1105 0.2343 0.0997 0.0470 16.116 92.345 61.532 12018.014 10.433 273.696 2.322 0.87 404250. 0.5344 28.77 0.1381 0.2867 0.0984 0.0474 16.249 93.102 60.725 12116.560 10.519 270.106 2.273 0.87 404681. 0.5197 34.53 0.1657 0.3368 0.0969 0.0477 16.347 93.667 59.797 12190.116 10.582 265.979 2.225 0.87 405152. 0.5048 40.28 0.1933 0.3845 0.0952 0.0479 16.406 94.007 58.737 12234.314 10.621 261.260 2.178 0.87 405664. 0.4896 46.03 0.2210 0.4301 0.0932 0.0479 16.421 94.089 57.532 12245.022 10.630 255.902 2.131 0.87 406216. 0.4742 51.79 0.2486 0.4734 0.0910 0.0478 16.385 93.884 56.173 12218.388 10.607 249.857 2.085 0.88 406811. 0.4585 57.54 0.2762 0.5146 0.0886 0.0475 16.295 93.365 54.651 12150.838 10.548 243.088 2.040 0.88 407450. 0.4425 63.30 0.3038 0.5537 0.0858 0.0471 16.144 92.504 52.959 12038.713 10.451 235.560 1.995 0.88 408131. 0.4260 69.05 0.3314 0.5905 0.0828 0.0465 15.930 91.275 51.090 11878.752 10.312 227.247 1.951 0.88 408857. 0.4091 74.81 0.3591 0.6252 0.0795 0.0457 15.647 89.656 49.041 11668.078 10.129 218.134 1.906 0.88 409626. 0.3917 80.56 0.3867 0.6576 0.0759 0.0446 15.292 87.622 46.810 11403.357 9.899 208.211 1.862 0.88 410439. 0.3737 86.31 0.4143 0.6876 0.0720 0.0434 14.860 85.144 44.394 11080.889 9.620 197.465 1.817 0.88 411296. 0.3552 92.07 0.4419 0.7153 0.0677 0.0419 14.345 82.197 41.795 10697.420 9.287 185.906 1.772 0.88 412197. 0.3361 97.82 0.4695 0.7404 0.0633 0.0401 13.750 78.784 39.030 10253.156 8.901 173.607 1.727 0.88 413141. 0.3165 103.58 0.4972 0.7627 0.0585 0.0382 13.081 74.950 36.120 9754.251 8.468 160.663 1.680 0.88 414127. 0.2962 109.33 0.5248 0.7811 0.0536 0.0360 12.349 70.755 33.085 9208.287 7.994 147.164 1.630 0.88 415157. 0.2750 115.09 0.5524 0.7951 0.0485 0.0337 11.557 66.221 29.945 8618.224 7.482 133.193 1.576 0.89 416228. 0.2530 120.84 0.5800 0.8030 0.0433 0.0313 10.719 61.420 26.714 7993.418 6.939 118.824 1.516 0.89 417342. 0.2299 126.59 0.6076 0.8025 0.0379 0.0287 9.847 56.423 23.410 7343.043 6.375 104.130 1.446 0.89 418497. 0.2053 132.35 0.6353 0.7928 0.0325 0.0260 8.928 51.154 20.055 6657.324 5.779 89.206 1.366 0.89 419694. 0.1795 138.10 0.6629 0.7699 0.0270 0.0233 7.972 45.678 16.668 5944.609 5.161 74.137 1.272 0.89 420932. 0.1523 143.86 0.6905 0.7276 0.0215 0.0204 6.994 40.077 13.267 5215.678 4.528 59.012 1.154 0.89 422212. 0.1233 149.61 0.7181 0.6557 0.0160 0.0175 6.010 34.434 9.877 4481.315 3.890 43.933 1.000 0.90 423534. 0.0922 155.36 0.7458 0.5369 0.0106 0.0147 5.033 28.840 6.523 3753.371 3.258 29.016 0.788 0.90 424897. 0.0591 161.12 0.7734 0.3406 0.0052 0.0119 4.083 23.393 3.237 3044.428 2.643 14.399 0.482 0.90 426300. 0.0255 166.87 0.8010 0.0056 0.0001 0.0092 3.165 18.138 0.040 2360.469 2.049 0.177 0.008 0.90 427737. 0.0000 PROP RPM = 12000 V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM (mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - - 0.00 0.0000 0.0000 0.1018 0.0519 23.100 121.328 74.719 17225.434 13.708 332.352 1.967 0.95 439562. 0.4990 6.43 0.0283 0.0545 0.1012 0.0526 23.414 122.978 74.306 17459.686 13.894 330.511 1.930 0.95 439882. 0.4882 12.87 0.0566 0.1068 0.1005 0.0533 23.722 124.596 73.818 17689.385 14.077 328.345 1.893 0.95 440237. 0.4771 19.30 0.0849 0.1570 0.0998 0.0540 24.014 126.131 73.244 17907.293 14.250 325.790 1.855 0.95 440630. 0.4658 25.74 0.1132 0.2051 0.0988 0.0546 24.279 127.524 72.566 18105.150 14.408 322.775 1.818 0.95 441065. 0.4543 32.17 0.1416 0.2513 0.0977 0.0551 24.505 128.710 71.767 18273.432 14.542 319.222 1.781 0.95 441542. 0.4427 38.61 0.1699 0.2955 0.0965 0.0555 24.677 129.612 70.829 18401.621 14.644 315.045 1.746 0.95 442065. 0.4311 45.04 0.1982 0.3380 0.0950 0.0557 24.780 130.154 69.730 18478.572 14.705 310.158 1.712 0.95 442635. 0.4193 51.48 0.2265 0.3789 0.0932 0.0557 24.800 130.256 68.451 18493.035 14.716 304.471 1.679 0.95 443254. 0.4075 57.91 0.2548 0.4184 0.0912 0.0556 24.721 129.844 66.974 18434.527 14.670 297.899 1.648 0.96 443922. 0.3956 64.35 0.2831 0.4566 0.0889 0.0551 24.533 128.855 65.280 18294.047 14.558 290.365 1.619 0.96 444641. 0.3837 70.78 0.3114 0.4936 0.0863 0.0544 24.225 127.240 63.355 18064.824 14.376 281.802 1.591 0.96 445412. 0.3715 77.22 0.3397 0.5295 0.0833 0.0535 23.793 124.970 61.187 17742.467 14.119 272.159 1.564 0.96 446234. 0.3590 83.65 0.3681 0.5642 0.0800 0.0522 23.233 122.027 58.768 17324.742 13.787 261.401 1.539 0.96 447108. 0.3460 90.08 0.3964 0.5977 0.0764 0.0507 22.542 118.400 56.092 16809.695 13.377 249.496 1.514 0.96 448034. 0.3326 96.52 0.4247 0.6298 0.0724 0.0488 21.722 114.092 53.155 16198.079 12.890 236.433 1.488 0.96 449011. 0.3184 102.95 0.4530 0.6602 0.0681 0.0467 20.776 109.122 49.966 15492.526 12.329 222.247 1.463 0.96 450039. 0.3034 109.39 0.4813 0.6888 0.0634 0.0443 19.714 103.545 46.551 14700.659 11.698 207.059 1.436 0.96 451117. 0.2875 115.82 0.5096 0.7150 0.0585 0.0417 18.548 97.422 42.942 13831.415 11.007 191.007 1.408 0.96 452244. 0.2707 122.26 0.5379 0.7367 0.0533 0.0389 17.331 91.028 39.164 12923.612 10.284 174.202 1.375 0.97 453420. 0.2524 128.69 0.5662 0.7524 0.0480 0.0361 16.076 84.435 35.245 11987.564 9.539 156.768 1.334 0.97 454645. 0.2323 135.13 0.5946 0.7593 0.0425 0.0333 14.809 77.784 31.209 11043.363 8.788 138.817 1.282 0.97 455917. 0.2101 141.56 0.6229 0.7430 0.0368 0.0309 13.747 72.204 27.057 10251.056 8.158 120.348 1.197 0.97 457236. 0.1827 148.00 0.6512 0.7100 0.0311 0.0285 12.700 66.706 22.848 9470.498 7.536 101.629 1.094 0.97 458603. 0.1535 154.43 0.6795 0.6579 0.0254 0.0262 11.657 61.225 18.624 8692.390 6.917 82.842 0.972 0.97 460018. 0.1230 160.87 0.7078 0.5819 0.0196 0.0239 10.635 55.859 14.427 7930.568 6.311 64.171 0.825 0.98 461479. 0.0919 167.30 0.7361 0.4762 0.0140 0.0217 9.653 50.701 10.304 7198.215 5.728 45.832 0.649 0.98 462988. 0.0611 173.74 0.7644 0.3347 0.0086 0.0196 8.725 45.826 6.304 6506.167 5.177 28.040 0.439 0.98 464546. 0.0324 180.17 0.7927 0.1507 0.0034 0.0177 7.857 41.268 2.464 5858.929 4.662 10.961 0.191 0.98 466164. 0.0088 186.60 0.8211