20x18(F1-GT) (20x18(F1-GT).dat) v2022-0915 Simulation Date: 10/10/2023 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 0.1075 0.0483 0.012 0.784 0.548 9.276 0.089 2.439 26.811 0.08 38467. 0.5825 0.64 0.0337 0.0728 0.1069 0.0495 0.013 0.803 0.545 9.501 0.091 2.425 26.025 0.08 38502. 0.5637 1.28 0.0674 0.1412 0.1062 0.0507 0.013 0.823 0.541 9.734 0.093 2.408 25.230 0.08 38541. 0.5447 1.92 0.1011 0.2051 0.1053 0.0519 0.013 0.843 0.537 9.971 0.095 2.389 24.434 0.08 38585. 0.5254 2.55 0.1348 0.2647 0.1043 0.0532 0.014 0.863 0.532 10.206 0.097 2.366 23.643 0.08 38634. 0.5059 3.19 0.1685 0.3199 0.1031 0.0543 0.014 0.882 0.526 10.433 0.100 2.339 22.863 0.08 38689. 0.4864 3.83 0.2022 0.3711 0.1017 0.0554 0.014 0.900 0.519 10.644 0.102 2.307 22.100 0.08 38750. 0.4669 4.47 0.2359 0.4184 0.1000 0.0564 0.015 0.915 0.510 10.829 0.103 2.268 21.358 0.08 38817. 0.4475 5.11 0.2697 0.4621 0.0980 0.0572 0.015 0.928 0.500 10.978 0.105 2.222 20.641 0.08 38890. 0.4280 5.75 0.3034 0.5025 0.0956 0.0577 0.015 0.937 0.487 11.081 0.106 2.168 19.951 0.08 38969. 0.4086 6.38 0.3371 0.5398 0.0928 0.0580 0.015 0.941 0.473 11.128 0.106 2.105 19.288 0.08 39055. 0.3893 7.02 0.3708 0.5742 0.0896 0.0579 0.015 0.939 0.457 11.115 0.106 2.033 18.652 0.08 39147. 0.3700 7.66 0.4045 0.6059 0.0861 0.0575 0.015 0.933 0.439 11.038 0.105 1.953 18.041 0.08 39246. 0.3507 8.30 0.4382 0.6349 0.0822 0.0567 0.015 0.921 0.419 10.897 0.104 1.865 17.452 0.08 39352. 0.3315 8.94 0.4719 0.6614 0.0781 0.0557 0.014 0.904 0.398 10.694 0.102 1.770 16.881 0.08 39463. 0.3124 9.58 0.5056 0.6853 0.0736 0.0543 0.014 0.882 0.375 10.430 0.100 1.670 16.324 0.08 39582. 0.2934 10.21 0.5393 0.7065 0.0690 0.0526 0.014 0.854 0.352 10.107 0.097 1.564 15.778 0.08 39706. 0.2745 10.85 0.5730 0.7250 0.0641 0.0506 0.013 0.822 0.327 9.725 0.093 1.453 15.238 0.08 39837. 0.2555 11.49 0.6067 0.7404 0.0590 0.0484 0.012 0.785 0.301 9.288 0.089 1.339 14.698 0.08 39974. 0.2366 12.13 0.6404 0.7526 0.0538 0.0458 0.012 0.743 0.274 8.795 0.084 1.221 14.153 0.08 40118. 0.2175 12.77 0.6741 0.7608 0.0485 0.0429 0.011 0.697 0.247 8.247 0.079 1.099 13.593 0.08 40267. 0.1983 13.41 0.7078 0.7645 0.0430 0.0398 0.010 0.646 0.219 7.647 0.073 0.975 13.008 0.08 40423. 0.1787 14.04 0.7415 0.7623 0.0374 0.0364 0.009 0.591 0.191 6.994 0.067 0.849 12.381 0.08 40585. 0.1587 14.68 0.7752 0.7523 0.0318 0.0328 0.008 0.532 0.162 6.289 0.060 0.721 11.688 0.08 40753. 0.1380 15.32 0.8090 0.7313 0.0261 0.0288 0.007 0.468 0.133 5.535 0.053 0.591 10.888 0.08 40927. 0.1164 15.96 0.8427 0.6934 0.0203 0.0246 0.006 0.400 0.103 4.731 0.045 0.460 9.911 0.08 41107. 0.0935 16.60 0.8764 0.6270 0.0145 0.0202 0.005 0.328 0.074 3.881 0.037 0.328 8.616 0.08 41292. 0.0686 17.24 0.9101 0.5049 0.0086 0.0155 0.004 0.252 0.044 2.986 0.029 0.196 6.681 0.08 41482. 0.0411 17.87 0.9438 0.2446 0.0028 0.0106 0.003 0.173 0.014 2.041 0.019 0.062 3.121 0.08 41669. 0.0109 18.51 0.9775 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 0.1078 0.0455 0.094 2.952 2.200 69.859 0.334 9.784 14.282 0.16 76933. 0.6214 1.26 0.0334 0.0767 0.1073 0.0467 0.096 3.031 2.188 71.711 0.342 9.730 13.836 0.16 77001. 0.6004 2.53 0.0667 0.1484 0.1066 0.0479 0.099 3.112 2.173 73.636 0.352 9.667 13.387 0.16 77078. 0.5790 3.79 0.1001 0.2151 0.1057 0.0492 0.101 3.195 2.157 75.602 0.361 9.593 12.939 0.16 77165. 0.5575 5.06 0.1335 0.2770 0.1048 0.0505 0.104 3.278 2.137 77.571 0.370 9.506 12.496 0.16 77263. 0.5359 6.32 0.1668 0.3341 0.1036 0.0517 0.107 3.359 2.114 79.493 0.380 9.401 12.060 0.16 77371. 0.5144 7.58 0.2002 0.3868 0.1023 0.0529 0.109 3.436 2.086 81.306 0.388 9.276 11.634 0.16 77491. 0.4929 8.85 0.2336 0.4352 0.1006 0.0540 0.111 3.505 2.052 82.936 0.396 9.127 11.222 0.16 77622. 0.4716 10.11 0.2669 0.4798 0.0986 0.0549 0.113 3.563 2.012 84.303 0.403 8.949 10.824 0.16 77766. 0.4504 11.38 0.3003 0.5208 0.0963 0.0555 0.114 3.606 1.964 85.323 0.407 8.738 10.443 0.16 77922. 0.4294 12.64 0.3337 0.5584 0.0936 0.0559 0.115 3.631 1.909 85.925 0.410 8.492 10.078 0.16 78091. 0.4086 13.90 0.3670 0.5931 0.0905 0.0560 0.115 3.637 1.846 86.056 0.411 8.212 9.730 0.16 78273. 0.3879 15.17 0.4004 0.6249 0.0871 0.0558 0.115 3.621 1.776 85.692 0.409 7.898 9.398 0.16 78467. 0.3674 16.43 0.4338 0.6540 0.0833 0.0552 0.114 3.585 1.698 84.823 0.405 7.553 9.080 0.16 78674. 0.3471 17.69 0.4671 0.6807 0.0792 0.0543 0.112 3.527 1.614 83.454 0.398 7.181 8.775 0.16 78894. 0.3271 18.96 0.5005 0.7048 0.0748 0.0531 0.109 3.448 1.525 81.591 0.390 6.785 8.480 0.16 79126. 0.3073 20.22 0.5339 0.7264 0.0702 0.0516 0.106 3.349 1.432 79.244 0.378 6.368 8.194 0.16 79371. 0.2876 21.49 0.5672 0.7455 0.0654 0.0497 0.102 3.230 1.334 76.424 0.365 5.932 7.914 0.16 79628. 0.2681 22.75 0.6006 0.7619 0.0604 0.0476 0.098 3.091 1.232 73.139 0.349 5.479 7.639 0.16 79897. 0.2488 24.01 0.6340 0.7754 0.0553 0.0452 0.093 2.933 1.127 69.398 0.331 5.013 7.366 0.16 80179. 0.2294 25.28 0.6673 0.7857 0.0500 0.0424 0.087 2.756 1.019 65.208 0.311 4.534 7.090 0.16 80473. 0.2100 26.54 0.7007 0.7922 0.0446 0.0394 0.081 2.560 0.909 60.575 0.289 4.044 6.808 0.16 80779. 0.1905 27.81 0.7341 0.7940 0.0391 0.0361 0.074 2.346 0.797 55.505 0.265 3.545 6.513 0.16 81097. 0.1706 29.07 0.7674 0.7896 0.0335 0.0326 0.067 2.113 0.683 50.006 0.239 3.039 6.196 0.16 81428. 0.1502 30.33 0.8008 0.7767 0.0278 0.0287 0.059 1.863 0.568 44.087 0.211 2.525 5.841 0.16 81769. 0.1291 31.60 0.8342 0.7508 0.0221 0.0246 0.051 1.596 0.451 37.760 0.180 2.007 5.420 0.16 82123. 0.1068 32.86 0.8675 0.7032 0.0164 0.0202 0.042 1.312 0.334 31.038 0.148 1.486 4.881 0.16 82487. 0.0828 34.13 0.9009 0.6136 0.0106 0.0156 0.032 1.012 0.216 23.937 0.114 0.963 4.102 0.17 82860. 0.0560 35.39 0.9343 0.4216 0.0048 0.0107 0.022 0.695 0.099 16.452 0.079 0.438 2.717 0.17 83235. 0.0250 36.65 0.9676 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 0.1081 0.0443 0.308 6.471 4.963 229.678 0.731 22.074 9.800 0.24 115397. 0.6405 1.89 0.0333 0.0788 0.1076 0.0455 0.317 6.651 4.936 236.061 0.751 21.957 9.485 0.24 115499. 0.6183 3.79 0.0667 0.1523 0.1069 0.0468 0.325 6.838 4.906 242.715 0.773 21.821 9.168 0.24 115614. 0.5957 5.68 0.1000 0.2206 0.1061 0.0481 0.335 7.030 4.870 249.536 0.794 21.660 8.851 0.24 115745. 0.5730 7.58 0.1334 0.2837 0.1052 0.0495 0.344 7.224 4.827 256.393 0.816 21.469 8.539 0.24 115891. 0.5503 9.47 0.1667 0.3419 0.1041 0.0507 0.353 7.413 4.775 263.119 0.838 21.240 8.232 0.24 116053. 0.5277 11.37 0.2001 0.3954 0.1027 0.0520 0.361 7.593 4.713 269.505 0.858 20.965 7.932 0.24 116232. 0.5052 13.26 0.2334 0.4444 0.1011 0.0531 0.369 7.756 4.639 275.303 0.876 20.634 7.643 0.24 116429. 0.4830 15.16 0.2668 0.4894 0.0992 0.0541 0.376 7.895 4.550 280.235 0.892 20.239 7.364 0.24 116645. 0.4609 17.05 0.3001 0.5307 0.0969 0.0548 0.381 8.002 4.445 284.016 0.904 19.769 7.098 0.24 116879. 0.4390 18.95 0.3335 0.5685 0.0942 0.0552 0.384 8.069 4.321 286.391 0.912 19.221 6.844 0.24 117132. 0.4174 20.84 0.3668 0.6032 0.0911 0.0554 0.385 8.091 4.180 287.179 0.914 18.592 6.602 0.24 117405. 0.3960 22.74 0.4002 0.6351 0.0876 0.0552 0.384 8.066 4.021 286.279 0.911 17.887 6.371 0.24 117696. 0.3748 24.63 0.4335 0.6643 0.0838 0.0547 0.380 7.992 3.847 283.658 0.903 17.112 6.151 0.24 118006. 0.3540 26.53 0.4669 0.6910 0.0797 0.0539 0.375 7.870 3.659 279.319 0.889 16.274 5.941 0.24 118336. 0.3334 28.42 0.5002 0.7152 0.0754 0.0527 0.366 7.699 3.458 273.282 0.870 15.381 5.739 0.24 118684. 0.3131 30.32 0.5336 0.7369 0.0707 0.0512 0.356 7.482 3.246 265.578 0.845 14.440 5.544 0.24 119051. 0.2931 32.21 0.5669 0.7562 0.0659 0.0494 0.344 7.219 3.025 256.237 0.816 13.456 5.355 0.24 119436. 0.2733 34.11 0.6003 0.7730 0.0609 0.0473 0.329 6.911 2.796 245.288 0.781 12.436 5.170 0.24 119840. 0.2536 36.00 0.6336 0.7871 0.0558 0.0449 0.312 6.558 2.559 232.757 0.741 11.383 4.987 0.24 120263. 0.2340 37.90 0.6670 0.7981 0.0505 0.0422 0.293 6.161 2.316 218.666 0.696 10.301 4.804 0.24 120704. 0.2145 39.79 0.7003 0.8057 0.0451 0.0392 0.272 5.720 2.067 203.036 0.646 9.196 4.618 0.24 121163. 0.1948 41.69 0.7337 0.8089 0.0395 0.0359 0.249 5.237 1.814 185.890 0.592 8.069 4.426 0.24 121640. 0.1749 43.58 0.7670 0.8066 0.0339 0.0323 0.224 4.712 1.557 167.250 0.532 6.924 4.222 0.24 122135. 0.1545 45.48 0.8004 0.7965 0.0282 0.0284 0.197 4.146 1.296 147.148 0.468 5.765 3.995 0.25 122647. 0.1334 47.37 0.8337 0.7747 0.0225 0.0242 0.168 3.539 1.033 125.622 0.400 4.596 3.730 0.25 123176. 0.1112 49.27 0.8671 0.7329 0.0167 0.0198 0.138 2.894 0.769 102.723 0.327 3.419 3.394 0.25 123722. 0.0873 51.16 0.9004 0.6520 0.0110 0.0151 0.105 2.212 0.503 78.504 0.250 2.238 2.907 0.25 124282. 0.0605 53.06 0.9338 0.4724 0.0052 0.0102 0.071 1.492 0.237 52.949 0.169 1.055 2.031 0.25 124845. 0.0290 54.95 0.9671 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 0.1085 0.0437 0.721 11.358 8.850 537.531 1.283 39.366 7.468 0.32 153857. 0.6518 2.52 0.0333 0.0799 0.1079 0.0450 0.741 11.683 8.806 552.917 1.320 39.169 7.224 0.32 153993. 0.6289 5.05 0.0666 0.1544 0.1073 0.0463 0.763 12.023 8.754 568.999 1.358 38.938 6.978 0.32 154147. 0.6057 7.57 0.1000 0.2235 0.1066 0.0476 0.785 12.373 8.693 585.534 1.398 38.665 6.734 0.32 154320. 0.5825 10.10 0.1333 0.2874 0.1057 0.0490 0.808 12.725 8.619 602.215 1.438 38.339 6.492 0.32 154514. 0.5592 12.62 0.1666 0.3461 0.1046 0.0503 0.830 13.072 8.531 618.646 1.477 37.946 6.255 0.32 154730. 0.5360 15.15 0.1999 0.3999 0.1033 0.0516 0.851 13.404 8.424 634.332 1.514 37.472 6.024 0.32 154968. 0.5129 17.67 0.2332 0.4493 0.1017 0.0528 0.870 13.707 8.296 648.677 1.549 36.899 5.800 0.32 155231. 0.4901 20.19 0.2666 0.4945 0.0998 0.0538 0.886 13.968 8.141 661.011 1.578 36.209 5.586 0.32 155518. 0.4676 22.72 0.2999 0.5359 0.0975 0.0546 0.899 14.171 7.956 670.638 1.601 35.388 5.381 0.32 155830. 0.4453 25.24 0.3332 0.5738 0.0949 0.0551 0.908 14.304 7.739 676.934 1.616 34.423 5.185 0.32 156167. 0.4232 27.77 0.3665 0.6086 0.0918 0.0553 0.911 14.357 7.489 679.440 1.622 33.313 5.000 0.32 156530. 0.4014 30.29 0.3998 0.6405 0.0884 0.0552 0.909 14.324 7.209 677.901 1.618 32.065 4.823 0.32 156918. 0.3799 32.81 0.4331 0.6697 0.0846 0.0547 0.901 14.204 6.900 672.218 1.605 30.690 4.655 0.32 157332. 0.3588 35.34 0.4665 0.6964 0.0805 0.0539 0.888 13.997 6.565 662.391 1.581 29.201 4.495 0.32 157771. 0.3379 37.86 0.4998 0.7207 0.0761 0.0528 0.870 13.702 6.208 648.463 1.548 27.612 4.342 0.32 158235. 0.3174 40.39 0.5331 0.7426 0.0715 0.0513 0.846 13.323 5.830 630.501 1.505 25.934 4.194 0.32 158723. 0.2971 42.91 0.5664 0.7622 0.0666 0.0495 0.816 12.860 5.436 608.576 1.453 24.179 4.051 0.32 159237. 0.2771 45.44 0.5997 0.7792 0.0616 0.0474 0.781 12.314 5.026 582.756 1.391 22.357 3.912 0.32 159775. 0.2573 47.96 0.6331 0.7937 0.0564 0.0450 0.742 11.687 4.604 553.102 1.320 20.477 3.775 0.32 160338. 0.2376 50.48 0.6664 0.8054 0.0511 0.0423 0.697 10.981 4.169 519.668 1.241 18.545 3.639 0.32 160925. 0.2180 53.01 0.6997 0.8137 0.0457 0.0393 0.647 10.196 3.725 482.504 1.152 16.569 3.502 0.33 161537. 0.1983 55.53 0.7330 0.8181 0.0401 0.0359 0.592 9.333 3.272 441.660 1.054 14.555 3.361 0.33 162172. 0.1783 58.06 0.7663 0.8173 0.0345 0.0323 0.533 8.393 2.812 397.195 0.948 12.509 3.211 0.33 162831. 0.1580 60.58 0.7997 0.8094 0.0288 0.0284 0.468 7.378 2.346 349.180 0.834 10.436 3.048 0.33 163513. 0.1370 63.10 0.8330 0.7906 0.0230 0.0242 0.399 6.291 1.876 297.710 0.711 8.344 2.858 0.33 164218. 0.1148 65.63 0.8663 0.7535 0.0172 0.0198 0.326 5.133 1.403 242.905 0.580 6.239 2.619 0.33 164945. 0.0910 68.15 0.8996 0.6800 0.0114 0.0150 0.248 3.907 0.928 184.893 0.441 4.127 2.276 0.33 165690. 0.0643 70.68 0.9329 0.5135 0.0055 0.0101 0.166 2.613 0.452 123.659 0.295 2.010 1.657 0.33 166441. 0.0327 73.20 0.9663 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 0.1089 0.0435 1.401 17.660 13.879 1044.677 1.995 61.736 6.026 0.40 192312. 0.6586 3.18 0.0336 0.0813 0.1084 0.0448 1.442 18.181 13.814 1075.503 2.054 61.446 5.826 0.40 192483. 0.6353 6.36 0.0672 0.1569 0.1078 0.0462 1.486 18.727 13.738 1107.825 2.116 61.105 5.624 0.40 192677. 0.6116 9.55 0.1008 0.2270 0.1071 0.0475 1.530 19.291 13.646 1141.166 2.179 60.698 5.424 0.40 192896. 0.5878 12.73 0.1344 0.2916 0.1062 0.0489 1.576 19.861 13.536 1174.914 2.244 60.207 5.225 0.40 193141. 0.5640 15.91 0.1680 0.3509 0.1051 0.0503 1.620 20.425 13.402 1208.261 2.308 59.612 5.031 0.40 193414. 0.5403 19.09 0.2016 0.4052 0.1039 0.0517 1.663 20.965 13.239 1240.197 2.369 58.887 4.842 0.40 193716. 0.5169 22.27 0.2352 0.4549 0.1023 0.0529 1.702 21.460 13.040 1269.498 2.425 58.004 4.659 0.40 194049. 0.4936 25.46 0.2688 0.5004 0.1004 0.0539 1.736 21.887 12.799 1294.771 2.473 56.932 4.484 0.40 194413. 0.4706 28.64 0.3024 0.5419 0.0981 0.0548 1.763 22.222 12.510 1314.578 2.511 55.645 4.316 0.40 194809. 0.4479 31.82 0.3360 0.5799 0.0955 0.0553 1.780 22.443 12.168 1327.625 2.536 54.125 4.157 0.40 195237. 0.4254 35.00 0.3696 0.6147 0.0924 0.0555 1.788 22.533 11.774 1332.968 2.546 52.369 4.006 0.40 195697. 0.4033 38.18 0.4032 0.6467 0.0889 0.0554 1.784 22.484 11.328 1330.088 2.540 50.389 3.863 0.40 196190. 0.3815 41.36 0.4368 0.6759 0.0850 0.0549 1.769 22.293 10.837 1318.787 2.519 48.203 3.727 0.40 196716. 0.3600 44.55 0.4704 0.7026 0.0808 0.0541 1.742 21.960 10.304 1299.063 2.481 45.834 3.598 0.40 197273. 0.3388 47.73 0.5040 0.7269 0.0764 0.0530 1.704 21.486 9.735 1271.012 2.427 43.302 3.474 0.40 197862. 0.3180 50.91 0.5376 0.7488 0.0717 0.0514 1.656 20.873 9.134 1234.769 2.358 40.628 3.355 0.40 198483. 0.2975 54.09 0.5712 0.7684 0.0667 0.0496 1.596 20.124 8.505 1190.479 2.274 37.830 3.240 0.40 199136. 0.2772 57.27 0.6048 0.7856 0.0616 0.0474 1.526 19.242 7.852 1138.280 2.174 34.924 3.129 0.40 199820. 0.2572 60.46 0.6384 0.8001 0.0563 0.0449 1.446 18.228 7.177 1078.298 2.059 31.924 3.019 0.40 200534. 0.2373 63.64 0.6720 0.8119 0.0509 0.0421 1.355 17.084 6.484 1010.645 1.930 28.842 2.910 0.41 201280. 0.2174 66.82 0.7056 0.8204 0.0453 0.0390 1.254 15.813 5.776 935.424 1.787 25.690 2.801 0.41 202057. 0.1975 70.00 0.7392 0.8249 0.0396 0.0355 1.144 14.415 5.053 852.741 1.629 22.477 2.688 0.41 202863. 0.1773 73.18 0.7728 0.8241 0.0339 0.0318 1.023 12.893 4.320 762.719 1.457 19.213 2.569 0.41 203700. 0.1566 76.37 0.8064 0.8160 0.0281 0.0277 0.892 11.250 3.576 665.512 1.271 15.908 2.438 0.41 204566. 0.1352 79.55 0.8400 0.7965 0.0222 0.0234 0.753 9.489 2.827 561.324 1.072 12.573 2.284 0.41 205461. 0.1127 82.73 0.8736 0.7569 0.0163 0.0188 0.604 7.614 2.072 450.409 0.860 9.218 2.087 0.41 206382. 0.0881 85.91 0.9072 0.6751 0.0103 0.0139 0.447 5.630 1.316 333.018 0.636 5.854 1.792 0.41 207326. 0.0603 89.09 0.9408 0.4721 0.0044 0.0087 0.280 3.531 0.557 208.869 0.399 2.476 1.209 0.41 208266. 0.0265 92.28 0.9744 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 0.1093 0.0435 2.422 25.445 20.071 1806.261 2.875 89.276 5.040 0.48 230762. 0.6625 3.82 0.0336 0.0815 0.1089 0.0449 2.495 26.208 19.985 1860.413 2.961 88.895 4.872 0.48 230966. 0.6391 7.63 0.0672 0.1574 0.1083 0.0462 2.571 27.010 19.884 1917.390 3.052 88.445 4.704 0.48 231199. 0.6154 11.45 0.1008 0.2277 0.1077 0.0477 2.650 27.842 19.763 1976.400 3.146 87.904 4.535 0.48 231461. 0.5915 15.27 0.1344 0.2924 0.1069 0.0491 2.731 28.687 19.615 2036.390 3.241 87.248 4.369 0.48 231754. 0.5677 19.08 0.1679 0.3519 0.1059 0.0505 2.811 29.526 19.435 2095.966 3.336 86.445 4.206 0.48 232081. 0.5439 22.90 0.2015 0.4063 0.1047 0.0519 2.888 30.334 19.212 2153.353 3.427 85.456 4.047 0.48 232443. 0.5204 26.72 0.2351 0.4560 0.1032 0.0532 2.959 31.081 18.939 2206.376 3.512 84.240 3.893 0.48 232842. 0.4971 30.54 0.2687 0.5015 0.1013 0.0543 3.021 31.732 18.604 2252.549 3.585 82.750 3.746 0.48 233279. 0.4740 34.35 0.3023 0.5430 0.0991 0.0552 3.070 32.249 18.198 2289.266 3.643 80.944 3.606 0.48 233754. 0.4512 38.17 0.3359 0.5810 0.0965 0.0558 3.103 32.600 17.715 2314.159 3.683 78.795 3.472 0.48 234268. 0.4287 41.99 0.3695 0.6158 0.0934 0.0561 3.119 32.759 17.153 2325.475 3.701 76.297 3.346 0.48 234820. 0.4065 45.80 0.4031 0.6478 0.0900 0.0560 3.114 32.713 16.516 2322.226 3.696 73.463 3.226 0.48 235413. 0.3846 49.62 0.4367 0.6770 0.0861 0.0555 3.090 32.457 15.810 2304.022 3.667 70.323 3.112 0.48 236043. 0.3631 53.44 0.4702 0.7038 0.0819 0.0547 3.045 31.990 15.042 2270.843 3.614 66.907 3.004 0.48 236713. 0.3419 57.25 0.5038 0.7283 0.0775 0.0536 2.981 31.314 14.219 2222.860 3.538 63.248 2.901 0.48 237420. 0.3210 61.07 0.5374 0.7504 0.0727 0.0521 2.897 30.433 13.349 2160.326 3.438 59.376 2.803 0.48 238166. 0.3004 64.89 0.5710 0.7702 0.0678 0.0502 2.794 29.350 12.437 2083.500 3.316 55.319 2.707 0.48 238950. 0.2801 68.71 0.6046 0.7876 0.0626 0.0480 2.672 28.070 11.488 1992.639 3.171 51.100 2.615 0.48 239771. 0.2600 72.52 0.6382 0.8026 0.0572 0.0455 2.532 26.596 10.508 1887.973 3.005 46.740 2.524 0.49 240629. 0.2401 76.34 0.6718 0.8149 0.0518 0.0427 2.373 24.930 9.500 1769.714 2.817 42.258 2.435 0.49 241524. 0.2202 80.16 0.7054 0.8240 0.0461 0.0395 2.197 23.075 8.469 1638.051 2.607 37.670 2.345 0.49 242456. 0.2002 83.97 0.7390 0.8294 0.0404 0.0360 2.002 21.035 7.417 1493.178 2.376 32.990 2.253 0.49 243424. 0.1800 87.79 0.7726 0.8298 0.0346 0.0322 1.791 18.811 6.348 1335.314 2.125 28.234 2.156 0.49 244428. 0.1594 91.61 0.8061 0.8233 0.0287 0.0281 1.562 16.408 5.264 1164.734 1.854 23.416 2.050 0.49 245468. 0.1380 95.42 0.8397 0.8060 0.0227 0.0237 1.317 13.831 4.171 981.794 1.563 18.551 1.927 0.49 246541. 0.1154 99.24 0.8733 0.7699 0.0167 0.0190 1.055 11.086 3.070 786.941 1.252 13.656 1.770 0.49 247647. 0.0910 103.06 0.9069 0.6940 0.0107 0.0140 0.779 8.179 1.966 580.629 0.924 8.746 1.536 0.50 248779. 0.0632 106.87 0.9405 0.5030 0.0047 0.0087 0.486 5.106 0.858 362.447 0.577 3.816 1.074 0.50 249909. 0.0292 110.69 0.9741 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 0.1099 0.0438 3.866 34.811 27.448 2883.003 3.933 122.090 4.318 0.56 269204. 0.6638 4.43 0.0334 0.0811 0.1094 0.0451 3.983 35.862 27.346 2969.998 4.052 121.633 4.176 0.56 269441. 0.6407 8.86 0.0668 0.1566 0.1090 0.0465 4.106 36.971 27.224 3061.903 4.177 121.091 4.033 0.56 269710. 0.6173 13.29 0.1002 0.2266 0.1084 0.0479 4.234 38.126 27.077 3157.542 4.307 120.437 3.889 0.56 270012. 0.5938 17.72 0.1337 0.2911 0.1077 0.0494 4.365 39.307 26.897 3255.321 4.441 119.636 3.748 0.56 270351. 0.5702 22.15 0.1671 0.3504 0.1068 0.0509 4.497 40.487 26.674 3353.065 4.574 118.645 3.608 0.56 270729. 0.5467 26.58 0.2005 0.4046 0.1056 0.0523 4.624 41.633 26.396 3447.963 4.704 117.410 3.472 0.56 271148. 0.5234 31.01 0.2339 0.4542 0.1043 0.0537 4.743 42.702 26.050 3536.519 4.824 115.872 3.341 0.56 271609. 0.5003 35.44 0.2673 0.4995 0.1025 0.0549 4.847 43.646 25.621 3614.673 4.931 113.964 3.215 0.56 272114. 0.4774 39.87 0.3007 0.5409 0.1004 0.0558 4.932 44.412 25.096 3678.107 5.018 111.625 3.095 0.56 272663. 0.4548 44.30 0.3342 0.5788 0.0979 0.0565 4.992 44.952 24.463 3722.813 5.079 108.811 2.980 0.56 273258. 0.4325 48.73 0.3676 0.6136 0.0949 0.0569 5.023 45.228 23.720 3745.733 5.110 105.508 2.872 0.56 273898. 0.4104 53.16 0.4010 0.6456 0.0915 0.0569 5.022 45.220 22.871 3745.073 5.109 101.732 2.770 0.56 274584. 0.3886 57.59 0.4344 0.6749 0.0878 0.0565 4.989 44.919 21.924 3720.083 5.075 97.520 2.673 0.56 275314. 0.3672 62.02 0.4678 0.7018 0.0836 0.0557 4.922 44.322 20.889 3670.683 5.007 92.915 2.581 0.56 276089. 0.3461 66.45 0.5012 0.7264 0.0792 0.0546 4.824 43.434 19.776 3597.145 4.907 87.963 2.494 0.56 276909. 0.3253 70.88 0.5346 0.7488 0.0744 0.0531 4.693 42.260 18.594 3499.902 4.775 82.706 2.410 0.56 277772. 0.3048 75.31 0.5681 0.7689 0.0695 0.0513 4.532 40.805 17.352 3379.413 4.610 77.184 2.329 0.56 278679. 0.2846 79.74 0.6015 0.7868 0.0643 0.0491 4.340 39.075 16.059 3236.110 4.415 71.430 2.251 0.57 279630. 0.2646 84.17 0.6349 0.8024 0.0589 0.0466 4.117 37.074 14.720 3070.398 4.189 65.473 2.174 0.57 280623. 0.2448 88.60 0.6683 0.8154 0.0534 0.0438 3.866 34.807 13.341 2882.643 3.932 59.342 2.099 0.57 281659. 0.2249 93.03 0.7017 0.8255 0.0477 0.0406 3.585 32.278 11.928 2673.180 3.647 53.057 2.024 0.57 282738. 0.2051 97.46 0.7351 0.8320 0.0420 0.0371 3.275 29.490 10.486 2442.332 3.332 46.641 1.947 0.57 283858. 0.1850 101.89 0.7686 0.8341 0.0361 0.0333 2.937 26.449 9.018 2190.454 2.988 40.113 1.867 0.57 285019. 0.1645 106.32 0.8020 0.8300 0.0301 0.0291 2.572 23.159 7.530 1917.977 2.616 33.494 1.781 0.57 286222. 0.1434 110.75 0.8354 0.8164 0.0241 0.0247 2.180 19.627 6.026 1625.454 2.217 26.804 1.682 0.57 287463. 0.1211 115.18 0.8688 0.7866 0.0181 0.0199 1.762 15.861 4.511 1313.590 1.792 20.066 1.558 0.58 288743. 0.0971 119.61 0.9022 0.7234 0.0120 0.0149 1.318 11.871 2.990 983.146 1.341 13.301 1.380 0.58 290054. 0.0700 124.04 0.9356 0.5697 0.0059 0.0096 0.850 7.656 1.465 634.020 0.865 6.514 1.048 0.58 291374. 0.0372 128.47 0.9691 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 0.1104 0.0444 5.858 46.152 36.031 4368.221 5.214 160.267 3.741 0.63 307639. 0.6589 5.06 0.0334 0.0804 0.1101 0.0457 6.031 47.518 35.917 4497.550 5.369 159.760 3.622 0.63 307908. 0.6369 10.13 0.0668 0.1554 0.1096 0.0471 6.216 48.969 35.782 4634.930 5.533 159.156 3.502 0.63 308214. 0.6145 15.19 0.1002 0.2251 0.1091 0.0486 6.408 50.489 35.617 4778.794 5.704 158.423 3.380 0.63 308558. 0.5919 20.25 0.1337 0.2894 0.1085 0.0501 6.607 52.055 35.412 4926.945 5.881 157.513 3.260 0.64 308945. 0.5692 25.32 0.1671 0.3486 0.1077 0.0516 6.807 53.633 35.155 5076.299 6.059 156.370 3.141 0.64 309375. 0.5464 30.38 0.2005 0.4028 0.1067 0.0531 7.004 55.179 34.829 5222.698 6.234 154.921 3.025 0.64 309853. 0.5237 35.44 0.2339 0.4524 0.1055 0.0545 7.189 56.639 34.416 5360.834 6.399 153.081 2.912 0.64 310379. 0.5012 40.50 0.2673 0.4977 0.1039 0.0558 7.355 57.944 33.893 5484.383 6.546 150.756 2.803 0.64 310955. 0.4788 45.57 0.3007 0.5391 0.1019 0.0568 7.492 59.023 33.241 5586.464 6.668 147.857 2.699 0.64 311583. 0.4565 50.63 0.3342 0.5771 0.0994 0.0576 7.591 59.805 32.445 5660.527 6.757 144.315 2.600 0.64 312264. 0.4345 55.69 0.3676 0.6118 0.0965 0.0580 7.646 60.237 31.498 5701.406 6.806 140.105 2.506 0.64 312996. 0.4126 60.76 0.4010 0.6438 0.0932 0.0580 7.652 60.285 30.406 5705.915 6.811 135.244 2.417 0.64 313781. 0.3910 65.82 0.4344 0.6732 0.0894 0.0577 7.607 59.932 29.177 5672.573 6.771 129.778 2.333 0.64 314617. 0.3697 70.88 0.4678 0.7002 0.0853 0.0570 7.511 59.178 27.825 5601.142 6.686 123.766 2.253 0.64 315505. 0.3487 75.95 0.5012 0.7250 0.0808 0.0559 7.365 58.025 26.365 5492.078 6.556 117.272 2.177 0.64 316444. 0.3280 81.01 0.5347 0.7475 0.0760 0.0544 7.169 56.483 24.810 5346.117 6.381 110.355 2.105 0.64 317433. 0.3076 86.07 0.5681 0.7680 0.0710 0.0525 6.925 54.560 23.172 5164.058 6.164 103.069 2.035 0.64 318471. 0.2874 91.14 0.6015 0.7862 0.0658 0.0503 6.634 52.263 21.462 4946.637 5.905 95.461 1.968 0.65 319560. 0.2675 96.20 0.6349 0.8022 0.0603 0.0477 6.295 49.599 19.688 4694.505 5.604 87.572 1.902 0.65 320697. 0.2476 101.26 0.6683 0.8157 0.0547 0.0448 5.912 46.575 17.859 4408.279 5.262 79.437 1.838 0.65 321883. 0.2278 106.33 0.7017 0.8265 0.0490 0.0416 5.483 43.196 15.983 4088.522 4.880 71.091 1.773 0.65 323118. 0.2080 111.39 0.7352 0.8339 0.0431 0.0380 5.010 39.470 14.065 3735.786 4.459 62.560 1.708 0.65 324400. 0.1879 116.45 0.7686 0.8370 0.0371 0.0341 4.493 35.401 12.112 3350.638 4.000 53.873 1.640 0.65 325729. 0.1674 121.51 0.8020 0.8343 0.0310 0.0298 3.934 30.996 10.129 2933.752 3.502 45.056 1.566 0.66 327104. 0.1462 126.58 0.8354 0.8226 0.0249 0.0253 3.334 26.265 8.124 2485.983 2.967 36.138 1.482 0.66 328525. 0.1240 131.64 0.8688 0.7955 0.0187 0.0204 2.693 21.220 6.104 2008.418 2.397 27.148 1.378 0.66 329988. 0.0999 136.70 0.9022 0.7370 0.0125 0.0153 2.015 15.872 4.073 1502.240 1.793 18.118 1.230 0.66 331488. 0.0728 141.77 0.9357 0.5931 0.0062 0.0098 1.297 10.221 2.035 967.429 1.155 9.053 0.954 0.66 332999. 0.0399 146.83 0.9691 -0.1392 -0.0005 0.0036 0.474 3.734 -0.168 353.374 0.422 -0.749 -0.216 0.66 332629. 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 0.1109 0.0472 8.852 61.995 45.804 6601.219 7.004 203.736 3.147 0.71 346065. 0.6249 5.71 0.0335 0.0765 0.1106 0.0484 9.090 63.657 45.687 6778.265 7.192 203.217 3.057 0.71 346367. 0.6063 11.42 0.0670 0.1485 0.1103 0.0498 9.342 65.426 45.549 6966.632 7.392 202.601 2.965 0.71 346710. 0.5872 17.13 0.1005 0.2158 0.1099 0.0512 9.607 67.281 45.379 7164.175 7.601 201.847 2.873 0.71 347097. 0.5678 22.84 0.1340 0.2785 0.1094 0.0526 9.880 69.194 45.166 7367.840 7.818 200.899 2.780 0.71 347531. 0.5482 28.55 0.1675 0.3366 0.1087 0.0541 10.156 71.123 44.893 7573.264 8.035 199.685 2.689 0.72 348015. 0.5285 34.27 0.2010 0.3903 0.1078 0.0555 10.426 73.014 44.539 7774.527 8.249 198.109 2.598 0.72 348553. 0.5088 39.98 0.2345 0.4399 0.1067 0.0569 10.680 74.793 44.077 7963.960 8.450 196.056 2.510 0.72 349145. 0.4890 45.69 0.2680 0.4857 0.1053 0.0581 10.906 76.373 43.478 8132.288 8.629 193.392 2.425 0.72 349795. 0.4691 51.40 0.3015 0.5279 0.1034 0.0591 11.089 77.660 42.713 8269.316 8.774 189.986 2.343 0.72 350504. 0.4492 57.11 0.3350 0.5668 0.1011 0.0598 11.218 78.563 41.756 8365.446 8.876 185.733 2.264 0.72 351273. 0.4292 62.82 0.3685 0.6028 0.0983 0.0601 11.282 79.012 40.599 8413.268 8.927 180.582 2.189 0.72 352102. 0.4091 68.53 0.4020 0.6360 0.0950 0.0601 11.276 78.967 39.242 8408.412 8.922 174.548 2.117 0.72 352990. 0.3890 74.24 0.4356 0.6666 0.0913 0.0596 11.196 78.410 37.699 8349.167 8.859 167.687 2.048 0.72 353937. 0.3689 79.95 0.4691 0.6947 0.0871 0.0588 11.044 77.342 35.989 8235.428 8.738 160.077 1.982 0.72 354943. 0.3488 85.66 0.5026 0.7205 0.0826 0.0576 10.819 75.769 34.128 8067.923 8.560 151.803 1.919 0.72 356007. 0.3288 91.37 0.5361 0.7441 0.0778 0.0561 10.524 73.700 32.137 7847.652 8.327 142.946 1.857 0.72 357127. 0.3089 97.09 0.5696 0.7653 0.0727 0.0541 10.159 71.145 30.032 7575.581 8.038 133.582 1.798 0.73 358305. 0.2891 102.80 0.6031 0.7843 0.0674 0.0518 9.726 68.111 27.827 7252.530 7.695 123.776 1.740 0.73 359538. 0.2693 108.51 0.6366 0.8009 0.0618 0.0491 9.225 64.604 25.536 6879.083 7.299 113.586 1.684 0.73 360826. 0.2496 114.22 0.6701 0.8151 0.0561 0.0461 8.657 60.628 23.170 6455.703 6.850 103.059 1.628 0.73 362170. 0.2299 119.93 0.7036 0.8266 0.0502 0.0427 8.023 56.188 20.737 5982.931 6.348 92.239 1.572 0.73 363568. 0.2100 125.64 0.7371 0.8347 0.0442 0.0390 7.324 51.290 18.248 5461.428 5.795 81.166 1.515 0.73 365019. 0.1899 131.35 0.7706 0.8387 0.0380 0.0349 6.560 45.942 15.710 4891.984 5.191 69.877 1.457 0.74 366524. 0.1694 137.06 0.8041 0.8370 0.0318 0.0305 5.734 40.154 13.131 4275.573 4.537 58.408 1.393 0.74 368081. 0.1481 142.77 0.8376 0.8266 0.0255 0.0258 4.846 33.935 10.521 3613.447 3.834 46.797 1.321 0.74 369688. 0.1257 148.48 0.8711 0.8010 0.0191 0.0208 3.899 27.303 7.888 2907.210 3.085 35.084 1.231 0.74 371343. 0.1014 154.19 0.9046 0.7443 0.0127 0.0154 2.895 20.272 5.240 2158.610 2.290 23.307 1.101 0.74 373040. 0.0739 159.91 0.9381 0.5999 0.0062 0.0098 1.834 12.843 2.580 1367.507 1.451 11.476 0.856 0.75 374746. 0.0403 165.62 0.9716