20x15(WCAR-T6) (20x15(WCAR-T6).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 0.1035 0.0454 0.012 0.737 0.528 8.722 0.083 2.347 27.434 0.08 38073. 0.5846 0.59 0.0309 0.0684 0.1028 0.0464 0.012 0.754 0.524 8.916 0.085 2.332 26.665 0.08 38104. 0.5664 1.17 0.0618 0.1328 0.1020 0.0475 0.012 0.770 0.520 9.113 0.087 2.314 25.891 0.08 38139. 0.5479 1.76 0.0927 0.1933 0.1011 0.0485 0.012 0.787 0.515 9.308 0.089 2.293 25.120 0.08 38178. 0.5291 2.34 0.1236 0.2500 0.1000 0.0494 0.013 0.802 0.510 9.494 0.091 2.268 24.358 0.08 38221. 0.5103 2.93 0.1545 0.3028 0.0987 0.0503 0.013 0.817 0.503 9.666 0.092 2.238 23.610 0.08 38269. 0.4913 3.51 0.1854 0.3522 0.0971 0.0511 0.013 0.829 0.495 9.813 0.094 2.202 22.882 0.08 38322. 0.4723 4.10 0.2163 0.3982 0.0952 0.0517 0.013 0.839 0.485 9.928 0.095 2.159 22.177 0.08 38380. 0.4533 4.68 0.2472 0.4412 0.0930 0.0521 0.013 0.845 0.474 10.000 0.095 2.108 21.499 0.08 38443. 0.4342 5.27 0.2781 0.4814 0.0904 0.0522 0.013 0.847 0.461 10.025 0.096 2.050 20.849 0.08 38511. 0.4152 5.85 0.3090 0.5189 0.0874 0.0521 0.013 0.845 0.446 9.998 0.095 1.983 20.228 0.08 38585. 0.3963 6.44 0.3399 0.5540 0.0842 0.0517 0.013 0.838 0.429 9.919 0.095 1.910 19.631 0.08 38664. 0.3774 7.02 0.3708 0.5866 0.0807 0.0510 0.013 0.827 0.411 9.789 0.093 1.829 19.055 0.08 38748. 0.3585 7.61 0.4017 0.6168 0.0768 0.0500 0.013 0.812 0.392 9.610 0.092 1.743 18.495 0.08 38837. 0.3397 8.19 0.4326 0.6445 0.0728 0.0489 0.013 0.793 0.371 9.383 0.090 1.651 17.946 0.08 38932. 0.3208 8.78 0.4635 0.6697 0.0686 0.0475 0.012 0.770 0.350 9.112 0.087 1.555 17.403 0.08 39032. 0.3019 9.36 0.4944 0.6921 0.0641 0.0458 0.012 0.744 0.327 8.798 0.084 1.455 16.860 0.08 39137. 0.2829 9.95 0.5253 0.7114 0.0595 0.0440 0.011 0.714 0.304 8.443 0.081 1.351 16.313 0.08 39248. 0.2637 10.53 0.5562 0.7275 0.0548 0.0419 0.011 0.680 0.280 8.048 0.077 1.243 15.754 0.08 39364. 0.2444 11.12 0.5871 0.7397 0.0500 0.0397 0.010 0.644 0.255 7.616 0.073 1.133 15.176 0.08 39485. 0.2247 11.70 0.6180 0.7475 0.0450 0.0372 0.010 0.604 0.230 7.146 0.068 1.021 14.568 0.08 39611. 0.2048 12.29 0.6489 0.7498 0.0400 0.0346 0.009 0.561 0.204 6.641 0.063 0.906 13.918 0.08 39743. 0.1843 12.87 0.6797 0.7454 0.0348 0.0318 0.008 0.516 0.178 6.100 0.058 0.790 13.207 0.08 39879. 0.1633 13.46 0.7106 0.7322 0.0297 0.0288 0.007 0.467 0.151 5.527 0.053 0.673 12.409 0.08 40021. 0.1416 14.04 0.7415 0.7071 0.0244 0.0256 0.007 0.416 0.125 4.923 0.047 0.554 11.484 0.08 40168. 0.1189 14.63 0.7724 0.6647 0.0192 0.0223 0.006 0.363 0.098 4.290 0.041 0.436 10.364 0.08 40320. 0.0952 15.21 0.8033 0.5956 0.0140 0.0189 0.005 0.307 0.071 3.631 0.035 0.318 8.929 0.08 40476. 0.0700 15.80 0.8342 0.4805 0.0088 0.0154 0.004 0.249 0.045 2.949 0.028 0.201 6.937 0.08 40637. 0.0432 16.39 0.8651 0.2740 0.0037 0.0117 0.003 0.190 0.019 2.243 0.021 0.084 3.814 0.08 40798. 0.0154 16.97 0.8960 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 0.1038 0.0419 0.086 2.722 2.117 64.415 0.308 9.418 14.908 0.16 76145. 0.6364 1.16 0.0306 0.0735 0.1032 0.0430 0.089 2.792 2.104 66.055 0.315 9.360 14.449 0.16 76207. 0.6149 2.32 0.0613 0.1424 0.1024 0.0441 0.091 2.862 2.089 67.730 0.323 9.292 13.989 0.16 76276. 0.5932 3.48 0.0919 0.2066 0.1015 0.0452 0.093 2.933 2.071 69.405 0.331 9.211 13.533 0.16 76353. 0.5714 4.64 0.1226 0.2663 0.1005 0.0462 0.095 3.002 2.049 71.036 0.339 9.115 13.084 0.16 76438. 0.5495 5.80 0.1532 0.3217 0.0992 0.0472 0.097 3.067 2.023 72.569 0.346 8.998 12.644 0.16 76533. 0.5276 6.96 0.1838 0.3730 0.0976 0.0481 0.099 3.125 1.992 73.936 0.353 8.859 12.218 0.16 76638. 0.5059 8.12 0.2145 0.4205 0.0958 0.0489 0.101 3.172 1.954 75.065 0.358 8.691 11.807 0.16 76752. 0.4842 9.28 0.2451 0.4645 0.0936 0.0494 0.102 3.207 1.909 75.887 0.362 8.493 11.413 0.16 76876. 0.4627 10.45 0.2758 0.5054 0.0911 0.0497 0.102 3.227 1.858 76.349 0.365 8.264 11.037 0.16 77011. 0.4414 11.61 0.3064 0.5433 0.0882 0.0497 0.102 3.230 1.799 76.418 0.365 8.003 10.679 0.16 77156. 0.4202 12.77 0.3370 0.5786 0.0850 0.0495 0.102 3.215 1.734 76.080 0.363 7.713 10.337 0.16 77312. 0.3994 13.93 0.3677 0.6112 0.0815 0.0490 0.101 3.184 1.663 75.335 0.360 7.396 10.011 0.16 77478. 0.3787 15.09 0.3983 0.6413 0.0778 0.0483 0.099 3.135 1.586 74.190 0.354 7.055 9.696 0.16 77654. 0.3583 16.25 0.4289 0.6690 0.0738 0.0473 0.097 3.071 1.505 72.659 0.347 6.692 9.392 0.16 77841. 0.3380 17.41 0.4596 0.6942 0.0696 0.0461 0.095 2.990 1.419 70.753 0.338 6.311 9.096 0.16 78038. 0.3179 18.57 0.4902 0.7168 0.0652 0.0446 0.092 2.894 1.329 68.487 0.327 5.914 8.805 0.16 78245. 0.2978 19.73 0.5209 0.7366 0.0606 0.0429 0.088 2.784 1.237 65.870 0.315 5.501 8.517 0.16 78463. 0.2779 20.89 0.5515 0.7536 0.0560 0.0410 0.084 2.659 1.141 62.911 0.300 5.077 8.229 0.16 78691. 0.2579 22.05 0.5821 0.7673 0.0512 0.0388 0.080 2.520 1.043 59.620 0.285 4.641 7.937 0.16 78930. 0.2379 23.21 0.6128 0.7773 0.0462 0.0365 0.075 2.367 0.943 56.002 0.267 4.195 7.639 0.16 79179. 0.2176 24.37 0.6434 0.7829 0.0412 0.0339 0.070 2.200 0.841 52.066 0.249 3.742 7.328 0.16 79438. 0.1972 25.53 0.6741 0.7832 0.0362 0.0311 0.064 2.021 0.738 47.819 0.228 3.281 6.997 0.16 79707. 0.1763 26.69 0.7047 0.7765 0.0310 0.0282 0.058 1.829 0.633 43.272 0.207 2.816 6.636 0.16 79986. 0.1549 27.85 0.7353 0.7605 0.0259 0.0250 0.052 1.625 0.528 38.442 0.184 2.348 6.228 0.16 80276. 0.1327 29.01 0.7660 0.7308 0.0207 0.0217 0.045 1.409 0.422 33.349 0.159 1.879 5.745 0.16 80575. 0.1096 30.17 0.7966 0.6796 0.0156 0.0182 0.038 1.184 0.317 28.015 0.134 1.411 5.138 0.16 80884. 0.0849 31.34 0.8273 0.5906 0.0104 0.0146 0.030 0.949 0.213 22.461 0.107 0.947 4.299 0.16 81201. 0.0582 32.50 0.8579 0.4227 0.0054 0.0109 0.022 0.705 0.109 16.692 0.080 0.486 2.967 0.16 81522. 0.0288 33.66 0.8885 0.0206 0.0002 0.0069 0.014 0.445 0.003 10.523 0.050 0.014 0.140 0.16 81787. 0.0002 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 0.1041 0.0405 0.282 5.917 4.778 210.028 0.669 21.253 10.318 0.24 114215. 0.6617 1.75 0.0308 0.0765 0.1035 0.0416 0.289 6.079 4.750 215.767 0.687 21.127 9.985 0.24 114307. 0.6384 3.50 0.0615 0.1479 0.1028 0.0428 0.297 6.245 4.716 221.653 0.706 20.978 9.651 0.24 114411. 0.6149 5.24 0.0923 0.2143 0.1019 0.0439 0.305 6.412 4.676 227.570 0.724 20.800 9.320 0.24 114528. 0.5913 6.99 0.1231 0.2758 0.1009 0.0450 0.313 6.575 4.628 233.370 0.743 20.587 8.996 0.24 114657. 0.5678 8.74 0.1538 0.3326 0.0996 0.0461 0.320 6.730 4.570 238.864 0.760 20.329 8.679 0.24 114800. 0.5443 10.49 0.1846 0.3850 0.0981 0.0470 0.327 6.870 4.500 243.825 0.776 20.018 8.372 0.24 114958. 0.5211 12.24 0.2154 0.4333 0.0962 0.0478 0.333 6.987 4.416 248.000 0.789 19.643 8.077 0.24 115130. 0.4980 13.99 0.2461 0.4779 0.0940 0.0484 0.337 7.076 4.316 251.147 0.799 19.197 7.795 0.24 115318. 0.4751 15.73 0.2769 0.5191 0.0915 0.0488 0.339 7.130 4.199 253.079 0.806 18.679 7.526 0.24 115521. 0.4525 17.48 0.3077 0.5573 0.0886 0.0489 0.340 7.147 4.067 253.674 0.807 18.089 7.271 0.24 115741. 0.4302 19.23 0.3385 0.5926 0.0854 0.0488 0.339 7.125 3.919 252.875 0.805 17.431 7.029 0.24 115976. 0.4082 20.98 0.3692 0.6252 0.0819 0.0483 0.336 7.062 3.757 250.672 0.798 16.712 6.798 0.24 116227. 0.3866 22.73 0.4000 0.6553 0.0781 0.0477 0.331 6.961 3.583 247.084 0.786 15.937 6.577 0.24 116493. 0.3653 24.47 0.4308 0.6829 0.0740 0.0467 0.325 6.822 3.398 242.145 0.771 15.114 6.365 0.24 116776. 0.3442 26.22 0.4615 0.7080 0.0698 0.0455 0.316 6.646 3.203 235.895 0.751 14.247 6.159 0.24 117074. 0.3234 27.97 0.4923 0.7306 0.0654 0.0440 0.306 6.434 3.000 228.372 0.727 13.342 5.958 0.24 117388. 0.3027 29.72 0.5231 0.7505 0.0608 0.0424 0.294 6.187 2.789 219.607 0.699 12.405 5.760 0.24 117717. 0.2822 31.47 0.5538 0.7676 0.0560 0.0404 0.281 5.906 2.572 209.631 0.667 11.439 5.564 0.24 118062. 0.2618 33.22 0.5846 0.7817 0.0512 0.0383 0.266 5.592 2.349 198.466 0.632 10.448 5.368 0.24 118423. 0.2414 34.96 0.6154 0.7923 0.0462 0.0359 0.250 5.244 2.121 186.134 0.592 9.435 5.169 0.24 118799. 0.2209 36.71 0.6461 0.7989 0.0412 0.0333 0.232 4.865 1.890 172.660 0.550 8.405 4.964 0.24 119191. 0.2002 38.46 0.6769 0.8004 0.0361 0.0305 0.212 4.454 1.654 158.073 0.503 7.359 4.747 0.24 119598. 0.1791 40.21 0.7077 0.7956 0.0309 0.0275 0.191 4.012 1.417 142.412 0.453 6.303 4.513 0.24 120021. 0.1576 41.96 0.7384 0.7818 0.0257 0.0243 0.169 3.542 1.178 125.732 0.400 5.241 4.251 0.24 120458. 0.1354 43.71 0.7692 0.7551 0.0205 0.0209 0.145 3.046 0.939 108.107 0.344 4.178 3.941 0.25 120910. 0.1121 45.45 0.8000 0.7073 0.0153 0.0173 0.120 2.525 0.701 89.617 0.285 3.119 3.549 0.25 121377. 0.0872 47.20 0.8307 0.6204 0.0101 0.0136 0.094 1.982 0.465 70.333 0.224 2.068 2.998 0.25 121855. 0.0600 48.95 0.8615 0.4456 0.0050 0.0097 0.067 1.416 0.230 50.263 0.160 1.023 2.076 0.25 122339. 0.0292 50.70 0.8923 -0.0576 -0.0004 0.0054 0.038 0.793 -0.016 28.135 0.090 -0.071 -0.259 0.25 122624. 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 0.1045 0.0398 0.656 10.338 8.523 489.237 1.168 37.910 7.902 0.32 152282. 0.6768 2.35 0.0310 0.0785 0.1039 0.0410 0.675 10.634 8.475 503.264 1.201 37.695 7.638 0.32 152406. 0.6523 4.69 0.0619 0.1517 0.1032 0.0421 0.694 10.939 8.417 517.702 1.236 37.440 7.375 0.32 152545. 0.6277 7.04 0.0929 0.2195 0.1023 0.0433 0.714 11.247 8.348 532.274 1.271 37.134 7.114 0.32 152701. 0.6030 9.38 0.1239 0.2821 0.1013 0.0445 0.733 11.551 8.265 546.625 1.305 36.764 6.858 0.32 152875. 0.5785 11.73 0.1548 0.3398 0.1001 0.0456 0.751 11.839 8.164 560.297 1.338 36.314 6.609 0.32 153067. 0.5540 14.07 0.1858 0.3929 0.0986 0.0466 0.768 12.102 8.041 572.732 1.367 35.766 6.368 0.32 153279. 0.5298 16.42 0.2168 0.4418 0.0967 0.0475 0.782 12.326 7.892 583.307 1.393 35.103 6.137 0.32 153512. 0.5058 18.77 0.2477 0.4867 0.0946 0.0481 0.793 12.497 7.714 591.421 1.412 34.311 5.916 0.32 153765. 0.4820 21.11 0.2787 0.5281 0.0920 0.0485 0.800 12.607 7.506 596.600 1.424 33.385 5.706 0.32 154039. 0.4587 23.46 0.3096 0.5664 0.0891 0.0487 0.803 12.647 7.268 598.536 1.429 32.328 5.508 0.32 154335. 0.4356 25.80 0.3406 0.6018 0.0858 0.0486 0.801 12.616 7.002 597.072 1.425 31.147 5.319 0.32 154652. 0.4130 28.15 0.3716 0.6344 0.0823 0.0482 0.794 12.513 6.711 592.171 1.414 29.852 5.141 0.32 154990. 0.3907 30.50 0.4025 0.6644 0.0784 0.0475 0.783 12.338 6.398 583.872 1.394 28.457 4.970 0.32 155350. 0.3688 32.84 0.4335 0.6920 0.0743 0.0466 0.767 12.092 6.064 572.251 1.366 26.971 4.806 0.32 155732. 0.3472 35.19 0.4645 0.7170 0.0700 0.0454 0.747 11.778 5.712 557.397 1.331 25.407 4.648 0.32 156134. 0.3259 37.53 0.4954 0.7395 0.0655 0.0439 0.723 11.398 5.345 539.396 1.288 23.775 4.495 0.32 156557. 0.3049 39.88 0.5264 0.7595 0.0609 0.0422 0.695 10.953 4.965 518.325 1.237 22.083 4.344 0.32 157002. 0.2840 42.22 0.5574 0.7767 0.0560 0.0402 0.663 10.444 4.572 494.251 1.180 20.338 4.196 0.32 157468. 0.2632 44.57 0.5883 0.7910 0.0511 0.0380 0.627 9.873 4.170 467.229 1.115 18.549 4.048 0.32 157955. 0.2425 46.92 0.6193 0.8019 0.0461 0.0356 0.586 9.241 3.759 437.312 1.044 16.721 3.899 0.32 158463. 0.2218 49.26 0.6503 0.8089 0.0410 0.0329 0.543 8.549 3.341 404.558 0.966 14.861 3.746 0.32 158991. 0.2009 51.61 0.6812 0.8111 0.0358 0.0300 0.495 7.798 2.917 369.041 0.881 12.975 3.585 0.32 159540. 0.1796 53.95 0.7122 0.8070 0.0305 0.0269 0.444 6.991 2.489 330.862 0.790 11.070 3.412 0.33 160110. 0.1579 56.30 0.7432 0.7942 0.0252 0.0236 0.389 6.131 2.059 290.165 0.693 9.157 3.218 0.33 160701. 0.1355 58.65 0.7741 0.7684 0.0200 0.0201 0.331 5.222 1.628 247.132 0.590 7.243 2.989 0.33 161311. 0.1119 60.99 0.8051 0.7206 0.0147 0.0164 0.271 4.268 1.200 201.965 0.482 5.338 2.695 0.33 161940. 0.0866 63.34 0.8360 0.6303 0.0095 0.0126 0.208 3.272 0.775 154.829 0.370 3.447 2.270 0.33 162585. 0.0586 65.68 0.8670 0.4353 0.0043 0.0086 0.142 2.233 0.352 105.686 0.252 1.567 1.512 0.33 163231. 0.0263 68.03 0.8980 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 0.1049 0.0395 1.271 16.024 13.370 947.921 1.810 59.468 6.397 0.40 190344. 0.6863 2.92 0.0308 0.0791 0.1043 0.0407 1.309 16.495 13.299 975.788 1.864 59.155 6.182 0.40 190498. 0.6614 5.84 0.0616 0.1527 0.1037 0.0419 1.347 16.982 13.215 1004.575 1.919 58.781 5.967 0.40 190671. 0.6364 8.76 0.0925 0.2209 0.1029 0.0431 1.386 17.475 13.114 1033.759 1.974 58.331 5.754 0.40 190864. 0.6113 11.68 0.1233 0.2838 0.1019 0.0443 1.425 17.964 12.991 1062.660 2.030 57.784 5.545 0.40 191080. 0.5863 14.59 0.1541 0.3417 0.1007 0.0454 1.462 18.433 12.841 1090.402 2.083 57.115 5.341 0.40 191319. 0.5615 17.51 0.1849 0.3950 0.0993 0.0465 1.496 18.864 12.656 1115.894 2.131 56.296 5.144 0.40 191582. 0.5369 20.43 0.2158 0.4439 0.0975 0.0474 1.526 19.236 12.432 1137.906 2.173 55.297 4.955 0.40 191870. 0.5126 23.35 0.2466 0.4888 0.0954 0.0481 1.549 19.529 12.162 1155.227 2.206 54.097 4.775 0.40 192184. 0.4886 26.27 0.2774 0.5302 0.0929 0.0486 1.565 19.725 11.845 1166.866 2.229 52.685 4.604 0.40 192525. 0.4649 29.19 0.3082 0.5685 0.0901 0.0488 1.572 19.815 11.480 1172.157 2.239 51.064 4.442 0.40 192892. 0.4416 32.11 0.3391 0.6037 0.0869 0.0488 1.570 19.791 11.071 1170.740 2.236 49.244 4.289 0.40 193286. 0.4187 35.03 0.3699 0.6363 0.0833 0.0484 1.559 19.651 10.621 1162.497 2.220 47.242 4.144 0.40 193706. 0.3962 37.95 0.4007 0.6664 0.0795 0.0478 1.539 19.398 10.134 1147.480 2.192 45.076 4.006 0.40 194153. 0.3741 40.86 0.4315 0.6939 0.0754 0.0469 1.510 19.032 9.615 1125.827 2.150 42.766 3.874 0.40 194626. 0.3524 43.78 0.4624 0.7191 0.0711 0.0457 1.472 18.556 9.067 1097.708 2.096 40.329 3.746 0.40 195126. 0.3310 46.70 0.4932 0.7418 0.0666 0.0443 1.426 17.974 8.494 1063.293 2.031 37.781 3.623 0.40 195651. 0.3098 49.62 0.5240 0.7621 0.0620 0.0426 1.372 17.289 7.899 1022.737 1.953 35.137 3.503 0.40 196203. 0.2889 52.54 0.5548 0.7798 0.0572 0.0407 1.309 16.502 7.286 976.173 1.864 32.409 3.385 0.40 196782. 0.2681 55.46 0.5857 0.7947 0.0522 0.0385 1.239 15.615 6.656 923.716 1.764 29.608 3.269 0.40 197386. 0.2474 58.38 0.6165 0.8065 0.0472 0.0361 1.161 14.630 6.013 865.472 1.653 26.745 3.151 0.40 198016. 0.2267 61.30 0.6473 0.8146 0.0420 0.0334 1.075 13.550 5.357 801.554 1.531 23.829 3.032 0.40 198672. 0.2059 64.22 0.6781 0.8184 0.0368 0.0305 0.982 12.376 4.692 732.102 1.398 20.872 2.907 0.41 199353. 0.1848 67.13 0.7089 0.8166 0.0315 0.0274 0.881 11.112 4.021 657.312 1.255 17.884 2.774 0.41 200060. 0.1632 70.05 0.7398 0.8070 0.0262 0.0241 0.774 9.762 3.345 577.452 1.103 14.880 2.628 0.41 200792. 0.1410 72.97 0.7706 0.7858 0.0209 0.0205 0.661 8.332 2.669 492.878 0.941 11.873 2.456 0.41 201549. 0.1177 75.89 0.8014 0.7456 0.0157 0.0168 0.542 6.829 1.996 403.988 0.772 8.878 2.241 0.41 202329. 0.0929 78.81 0.8322 0.6686 0.0104 0.0130 0.417 5.259 1.327 311.124 0.594 5.904 1.935 0.41 203130. 0.0654 81.73 0.8631 0.5029 0.0052 0.0089 0.287 3.623 0.663 214.328 0.409 2.950 1.404 0.41 203938. 0.0335 84.65 0.8939 -0.0632 -0.0003 0.0044 0.143 1.798 -0.040 106.343 0.203 -0.178 -0.170 0.41 204302. 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 0.1054 0.0394 2.193 23.038 19.340 1635.423 2.603 86.022 5.364 0.48 228400. 0.6920 3.56 0.0314 0.0809 0.1048 0.0406 2.260 23.743 19.245 1685.467 2.683 85.600 5.179 0.48 228588. 0.6665 7.13 0.0627 0.1560 0.1042 0.0419 2.330 24.475 19.130 1737.395 2.765 85.092 4.994 0.48 228799. 0.6409 10.69 0.0941 0.2255 0.1035 0.0432 2.401 25.220 18.991 1790.267 2.849 84.474 4.812 0.48 229036. 0.6152 14.25 0.1254 0.2894 0.1025 0.0444 2.471 25.960 18.820 1842.849 2.933 83.713 4.632 0.48 229300. 0.5896 17.82 0.1568 0.3481 0.1014 0.0457 2.539 26.674 18.609 1893.509 3.014 82.771 4.457 0.48 229594. 0.5641 21.38 0.1881 0.4019 0.0999 0.0468 2.602 27.332 18.346 1940.206 3.088 81.602 4.289 0.48 229918. 0.5389 24.94 0.2195 0.4513 0.0982 0.0478 2.656 27.901 18.022 1980.615 3.152 80.161 4.127 0.48 230273. 0.5140 28.50 0.2508 0.4965 0.0960 0.0485 2.699 28.349 17.628 2012.434 3.203 78.411 3.973 0.48 230661. 0.4894 32.07 0.2822 0.5381 0.0935 0.0490 2.727 28.650 17.162 2033.794 3.237 76.338 3.827 0.48 231081. 0.4652 35.63 0.3135 0.5764 0.0906 0.0493 2.740 28.786 16.624 2043.428 3.252 73.944 3.690 0.48 231535. 0.4414 39.19 0.3449 0.6117 0.0873 0.0492 2.737 28.747 16.018 2040.656 3.248 71.246 3.560 0.48 232022. 0.4180 42.76 0.3763 0.6443 0.0836 0.0488 2.716 28.530 15.348 2025.266 3.223 68.270 3.437 0.48 232542. 0.3951 46.32 0.4076 0.6743 0.0797 0.0482 2.679 28.137 14.623 1997.367 3.179 65.045 3.321 0.48 233096. 0.3726 49.88 0.4390 0.7018 0.0754 0.0472 2.625 27.572 13.849 1957.234 3.115 61.600 3.209 0.48 233682. 0.3504 53.45 0.4703 0.7269 0.0710 0.0459 2.555 26.839 13.032 1905.201 3.032 57.965 3.102 0.48 234301. 0.3286 57.01 0.5017 0.7495 0.0663 0.0444 2.470 25.943 12.177 1841.592 2.931 54.164 2.999 0.48 234952. 0.3070 60.57 0.5330 0.7697 0.0615 0.0426 2.369 24.888 11.290 1766.698 2.812 50.218 2.899 0.48 235636. 0.2857 64.13 0.5644 0.7872 0.0565 0.0405 2.254 23.677 10.375 1680.776 2.675 46.148 2.800 0.48 236352. 0.2646 67.70 0.5957 0.8019 0.0514 0.0382 2.124 22.315 9.436 1584.044 2.521 41.971 2.702 0.48 237101. 0.2435 71.26 0.6271 0.8133 0.0462 0.0356 1.980 20.803 8.476 1476.712 2.350 37.702 2.603 0.49 237881. 0.2224 74.82 0.6584 0.8210 0.0409 0.0328 1.822 19.144 7.499 1359.009 2.163 33.357 2.503 0.49 238693. 0.2011 78.39 0.6898 0.8240 0.0355 0.0297 1.651 17.344 6.509 1231.232 1.960 28.954 2.398 0.49 239538. 0.1795 81.95 0.7212 0.8209 0.0300 0.0264 1.467 15.408 5.510 1093.790 1.741 24.510 2.285 0.49 240413. 0.1574 85.51 0.7525 0.8091 0.0246 0.0228 1.270 13.344 4.507 947.248 1.508 20.049 2.158 0.49 241320. 0.1344 89.08 0.7839 0.7836 0.0191 0.0191 1.063 11.161 3.505 792.316 1.261 15.591 2.007 0.49 242256. 0.1102 92.64 0.8152 0.7338 0.0137 0.0152 0.844 8.871 2.508 629.723 1.002 11.158 1.807 0.49 243221. 0.0840 96.20 0.8466 0.6318 0.0083 0.0111 0.617 6.480 1.519 459.965 0.732 6.757 1.498 0.49 244207. 0.0542 99.76 0.8779 0.3739 0.0029 0.0068 0.378 3.975 0.532 282.140 0.449 2.366 0.855 0.49 245169. 0.0183 103.33 0.9093 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 0.1059 0.0396 3.495 31.466 26.457 2605.979 3.555 117.679 4.605 0.56 266450. 0.6949 4.10 0.0310 0.0800 0.1054 0.0408 3.602 32.433 26.342 2686.078 3.664 117.171 4.448 0.56 266665. 0.6698 8.21 0.0619 0.1544 0.1049 0.0420 3.714 33.442 26.205 2769.582 3.778 116.560 4.292 0.56 266907. 0.6445 12.31 0.0929 0.2233 0.1042 0.0433 3.829 34.474 26.037 2855.108 3.895 115.811 4.136 0.56 267179. 0.6192 16.42 0.1238 0.2867 0.1034 0.0446 3.944 35.509 25.828 2940.824 4.012 114.884 3.984 0.56 267481. 0.5940 20.52 0.1548 0.3450 0.1023 0.0459 4.056 36.517 25.568 3024.261 4.126 113.725 3.835 0.56 267816. 0.5688 24.63 0.1858 0.3984 0.1010 0.0471 4.160 37.459 25.241 3102.271 4.232 112.273 3.690 0.56 268186. 0.5440 28.73 0.2167 0.4474 0.0994 0.0481 4.253 38.291 24.834 3171.172 4.326 110.463 3.552 0.56 268592. 0.5193 32.84 0.2477 0.4923 0.0974 0.0490 4.328 38.967 24.335 3227.197 4.402 108.242 3.420 0.56 269035. 0.4950 36.94 0.2786 0.5336 0.0950 0.0496 4.381 39.449 23.736 3267.118 4.457 105.579 3.295 0.56 269515. 0.4710 41.04 0.3096 0.5717 0.0922 0.0499 4.410 39.709 23.038 3288.613 4.486 102.472 3.177 0.56 270034. 0.4474 45.15 0.3405 0.6069 0.0890 0.0500 4.412 39.729 22.244 3290.316 4.489 98.939 3.066 0.56 270591. 0.4243 49.25 0.3715 0.6394 0.0855 0.0497 4.387 39.504 21.360 3271.682 4.463 95.011 2.961 0.56 271186. 0.4015 53.36 0.4025 0.6694 0.0816 0.0491 4.335 39.034 20.397 3232.756 4.410 90.727 2.862 0.56 271818. 0.3792 57.46 0.4334 0.6971 0.0775 0.0482 4.256 38.324 19.364 3173.946 4.330 86.129 2.767 0.56 272488. 0.3572 61.57 0.4644 0.7224 0.0731 0.0470 4.152 37.381 18.268 3095.810 4.223 81.256 2.676 0.56 273196. 0.3356 65.67 0.4953 0.7454 0.0685 0.0455 4.022 36.211 17.119 2998.912 4.091 76.144 2.589 0.56 273940. 0.3143 69.77 0.5263 0.7661 0.0637 0.0438 3.867 34.820 15.923 2883.773 3.934 70.824 2.504 0.56 274722. 0.2932 73.88 0.5573 0.7843 0.0588 0.0418 3.689 33.215 14.686 2750.835 3.753 65.324 2.422 0.56 275540. 0.2723 77.98 0.5882 0.7999 0.0537 0.0395 3.487 31.400 13.415 2600.501 3.548 59.669 2.340 0.56 276395. 0.2514 82.09 0.6192 0.8126 0.0485 0.0369 3.263 29.379 12.114 2433.129 3.319 53.881 2.258 0.57 277286. 0.2306 86.19 0.6501 0.8220 0.0432 0.0341 3.016 27.157 10.787 2249.087 3.068 47.982 2.175 0.57 278214. 0.2096 90.30 0.6811 0.8274 0.0378 0.0311 2.748 24.739 9.441 2048.822 2.795 41.994 2.090 0.57 279177. 0.1884 94.40 0.7121 0.8275 0.0323 0.0278 2.458 22.132 8.080 1832.926 2.500 35.941 2.000 0.57 280176. 0.1668 98.51 0.7430 0.8205 0.0269 0.0243 2.149 19.346 6.711 1602.213 2.186 29.852 1.900 0.57 281211. 0.1444 102.61 0.7740 0.8026 0.0214 0.0206 1.821 16.394 5.341 1357.743 1.852 23.757 1.784 0.57 282280. 0.1210 106.71 0.8049 0.7665 0.0159 0.0167 1.476 13.290 3.976 1100.687 1.502 17.684 1.638 0.57 283382. 0.0958 110.82 0.8359 0.6937 0.0105 0.0126 1.116 10.046 2.619 832.014 1.135 11.651 1.428 0.57 284513. 0.0678 114.92 0.8668 0.5265 0.0051 0.0084 0.740 6.662 1.271 551.727 0.753 5.654 1.045 0.58 285649. 0.0346 119.03 0.8978 -0.1556 -0.0006 0.0036 0.318 2.862 -0.156 237.017 0.323 -0.693 -0.298 0.58 285302. 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 0.1065 0.0399 5.260 41.445 34.745 3922.737 4.682 154.547 4.017 0.63 304493. 0.6948 4.71 0.0311 0.0801 0.1061 0.0411 5.424 42.734 34.616 4044.743 4.828 153.973 3.882 0.63 304738. 0.6701 9.42 0.0621 0.1546 0.1056 0.0424 5.596 44.086 34.460 4172.755 4.981 153.277 3.746 0.63 305015. 0.6451 14.12 0.0932 0.2235 0.1050 0.0438 5.773 45.482 34.266 4304.841 5.139 152.416 3.610 0.63 305325. 0.6200 18.83 0.1243 0.2870 0.1043 0.0451 5.952 46.892 34.023 4438.342 5.298 151.335 3.477 0.64 305671. 0.5950 23.54 0.1554 0.3453 0.1033 0.0465 6.128 48.278 33.715 4569.528 5.454 149.963 3.347 0.64 306055. 0.5701 28.25 0.1864 0.3987 0.1021 0.0477 6.294 49.589 33.321 4693.567 5.603 148.212 3.220 0.64 306479. 0.5453 32.95 0.2175 0.4476 0.1006 0.0489 6.443 50.762 32.822 4804.622 5.735 145.992 3.098 0.64 306945. 0.5208 37.66 0.2486 0.4924 0.0987 0.0498 6.566 51.734 32.199 4896.568 5.845 143.223 2.983 0.64 307453. 0.4965 42.37 0.2796 0.5336 0.0964 0.0505 6.657 52.446 31.442 4963.992 5.925 139.855 2.873 0.64 308006. 0.4726 47.08 0.3107 0.5716 0.0936 0.0509 6.709 52.857 30.548 5002.849 5.972 135.877 2.770 0.64 308602. 0.4491 51.78 0.3418 0.6066 0.0905 0.0510 6.719 52.939 29.520 5010.639 5.981 131.306 2.672 0.64 309243. 0.4260 56.49 0.3728 0.6391 0.0869 0.0507 6.687 52.681 28.369 4986.260 5.952 126.184 2.581 0.64 309929. 0.4032 61.20 0.4039 0.6691 0.0831 0.0501 6.611 52.083 27.105 4929.674 5.884 120.561 2.494 0.64 310658. 0.3809 65.91 0.4350 0.6968 0.0789 0.0492 6.493 51.152 25.741 4841.524 5.779 114.496 2.411 0.64 311430. 0.3590 70.61 0.4661 0.7222 0.0744 0.0480 6.333 49.897 24.291 4722.771 5.637 108.045 2.333 0.64 312246. 0.3373 75.32 0.4971 0.7454 0.0698 0.0465 6.134 48.330 22.765 4574.429 5.460 101.259 2.257 0.64 313104. 0.3160 80.03 0.5282 0.7663 0.0649 0.0447 5.897 46.460 21.174 4397.421 5.249 94.184 2.184 0.64 314005. 0.2948 84.74 0.5593 0.7848 0.0598 0.0426 5.622 44.295 19.527 4192.529 5.004 86.858 2.113 0.64 314948. 0.2739 89.45 0.5903 0.8008 0.0546 0.0403 5.311 41.843 17.832 3960.440 4.727 79.316 2.042 0.65 315934. 0.2530 94.15 0.6214 0.8140 0.0493 0.0377 4.964 39.111 16.095 3701.800 4.419 71.590 1.972 0.65 316961. 0.2321 98.86 0.6525 0.8239 0.0439 0.0348 4.583 36.104 14.323 3417.244 4.079 63.710 1.901 0.65 318029. 0.2111 103.57 0.6835 0.8300 0.0384 0.0316 4.167 32.832 12.524 3107.511 3.709 55.706 1.828 0.65 319139. 0.1898 108.28 0.7146 0.8309 0.0328 0.0282 3.719 29.304 10.704 2773.566 3.311 47.613 1.751 0.65 320290. 0.1680 112.98 0.7457 0.8249 0.0272 0.0246 3.241 25.533 8.873 2416.716 2.885 39.468 1.665 0.65 321482. 0.1455 117.69 0.7768 0.8081 0.0216 0.0207 2.734 21.539 7.040 2038.632 2.433 31.314 1.566 0.65 322713. 0.1219 122.40 0.8078 0.7731 0.0160 0.0167 2.201 17.339 5.213 1641.140 1.959 23.187 1.441 0.66 323981. 0.0965 127.11 0.8389 0.7005 0.0104 0.0125 1.644 12.950 3.397 1225.697 1.463 15.111 1.257 0.66 325281. 0.0680 131.81 0.8700 0.5264 0.0049 0.0081 1.062 8.369 1.591 792.097 0.945 7.076 0.911 0.66 326583. 0.0337 136.52 0.9010 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 0.1071 0.0412 7.736 54.173 44.213 5768.381 6.120 196.661 3.477 0.71 342527. 0.6782 5.27 0.0309 0.0778 0.1067 0.0424 7.963 55.765 44.080 5937.897 6.300 196.067 3.367 0.71 342800. 0.6559 10.55 0.0619 0.1506 0.1063 0.0437 8.202 57.443 43.918 6116.575 6.490 195.345 3.257 0.71 343108. 0.6332 15.82 0.0928 0.2182 0.1058 0.0450 8.451 59.185 43.715 6302.006 6.687 194.445 3.146 0.71 343453. 0.6103 21.10 0.1238 0.2808 0.1052 0.0464 8.704 60.957 43.457 6490.748 6.887 193.299 3.037 0.71 343838. 0.5873 26.37 0.1547 0.3386 0.1044 0.0477 8.955 62.714 43.124 6677.853 7.085 191.818 2.929 0.71 344266. 0.5643 31.64 0.1856 0.3917 0.1034 0.0490 9.195 64.393 42.691 6856.615 7.275 189.890 2.824 0.72 344738. 0.5413 36.92 0.2166 0.4406 0.1020 0.0501 9.412 65.916 42.129 7018.768 7.447 187.389 2.722 0.72 345256. 0.5184 42.19 0.2475 0.4855 0.1003 0.0511 9.595 67.199 41.412 7155.360 7.592 184.200 2.625 0.72 345823. 0.4956 47.46 0.2785 0.5269 0.0981 0.0518 9.733 68.164 40.522 7258.117 7.701 180.242 2.532 0.72 346440. 0.4729 52.74 0.3094 0.5651 0.0955 0.0523 9.817 68.750 39.452 7320.564 7.767 175.481 2.444 0.72 347106. 0.4504 58.01 0.3403 0.6005 0.0925 0.0524 9.841 68.918 38.202 7338.423 7.786 169.924 2.361 0.72 347822. 0.4282 63.29 0.3713 0.6332 0.0891 0.0522 9.802 68.647 36.783 7309.573 7.756 163.613 2.282 0.72 348589. 0.4061 68.56 0.4022 0.6636 0.0853 0.0517 9.700 67.934 35.210 7233.603 7.675 156.612 2.208 0.72 349405. 0.3843 73.83 0.4332 0.6916 0.0811 0.0508 9.536 66.784 33.498 7111.225 7.545 148.997 2.137 0.72 350270. 0.3628 79.11 0.4641 0.7173 0.0767 0.0496 9.312 65.211 31.665 6943.715 7.368 140.845 2.068 0.72 351183. 0.3415 84.38 0.4950 0.7409 0.0720 0.0481 9.028 63.227 29.727 6732.465 7.143 132.228 2.003 0.72 352145. 0.3204 89.65 0.5260 0.7622 0.0671 0.0463 8.688 60.845 27.700 6478.790 6.874 123.210 1.939 0.72 353154. 0.2994 94.93 0.5569 0.7813 0.0620 0.0442 8.293 58.074 25.595 6183.804 6.561 113.847 1.877 0.73 354210. 0.2787 100.20 0.5878 0.7980 0.0567 0.0418 7.843 54.925 23.423 5848.485 6.205 104.187 1.817 0.73 355313. 0.2579 105.48 0.6188 0.8120 0.0513 0.0391 7.341 51.407 21.194 5473.864 5.808 94.271 1.756 0.73 356462. 0.2372 110.75 0.6497 0.8231 0.0458 0.0362 6.787 47.530 18.917 5060.995 5.370 84.141 1.695 0.73 357658. 0.2163 116.02 0.6807 0.8306 0.0402 0.0329 6.184 43.304 16.600 4611.038 4.892 73.837 1.633 0.73 358900. 0.1952 121.30 0.7116 0.8334 0.0345 0.0295 5.532 38.743 14.255 4125.414 4.377 63.404 1.567 0.73 360187. 0.1736 126.57 0.7425 0.8299 0.0288 0.0258 4.836 33.865 11.891 3605.993 3.826 52.890 1.496 0.73 361519. 0.1513 131.84 0.7735 0.8170 0.0231 0.0218 4.097 28.692 9.521 3055.178 3.242 42.349 1.413 0.74 362895. 0.1280 137.12 0.8044 0.7881 0.0173 0.0177 3.320 23.250 7.156 2475.665 2.627 31.830 1.311 0.74 364314. 0.1029 142.39 0.8354 0.7274 0.0116 0.0134 2.507 17.560 4.804 1869.818 1.984 21.366 1.165 0.74 365769. 0.0749 147.67 0.8663 0.5840 0.0060 0.0088 1.661 11.629 2.463 1238.288 1.314 10.956 0.902 0.74 367236. 0.0415 152.94 0.8972 -0.0031 0.0000 0.0038 0.723 5.060 -0.005 538.829 0.572 -0.024 -0.005 0.74 367965. 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 0.1075 0.0457 11.774 74.210 54.809 8779.859 8.384 243.792 2.831 0.79 380550. 0.6150 5.88 0.0311 0.0710 0.1072 0.0469 12.073 76.094 54.680 9002.786 8.597 243.214 2.755 0.79 380853. 0.5976 11.77 0.0621 0.1381 0.1069 0.0481 12.389 78.083 54.522 9238.139 8.822 242.514 2.677 0.79 381195. 0.5799 17.65 0.0932 0.2010 0.1065 0.0494 12.717 80.150 54.325 9482.695 9.055 241.637 2.598 0.79 381578. 0.5619 23.53 0.1242 0.2600 0.1060 0.0507 13.051 82.255 54.070 9731.763 9.293 240.504 2.520 0.79 382006. 0.5437 29.41 0.1553 0.3149 0.1054 0.0520 13.381 84.340 53.734 9978.415 9.529 239.009 2.442 0.79 382480. 0.5253 35.30 0.1864 0.3662 0.1045 0.0532 13.696 86.323 53.285 10213.027 9.753 237.011 2.366 0.79 383005. 0.5068 41.18 0.2174 0.4139 0.1033 0.0543 13.978 88.100 52.685 10423.270 9.953 234.344 2.293 0.80 383582. 0.4882 47.06 0.2485 0.4584 0.1018 0.0552 14.209 89.554 51.898 10595.320 10.118 230.842 2.222 0.80 384213. 0.4696 52.94 0.2795 0.5000 0.0998 0.0558 14.371 90.575 50.894 10716.130 10.233 226.376 2.154 0.80 384900. 0.4509 58.83 0.3106 0.5390 0.0974 0.0561 14.450 91.076 49.656 10775.403 10.290 220.872 2.090 0.80 385644. 0.4321 64.71 0.3417 0.5758 0.0945 0.0561 14.438 91.002 48.182 10766.661 10.281 214.312 2.030 0.80 386446. 0.4134 70.59 0.3727 0.6104 0.0912 0.0557 14.332 90.332 46.477 10687.366 10.206 206.729 1.972 0.80 387304. 0.3945 76.47 0.4038 0.6429 0.0874 0.0549 14.132 89.072 44.558 10538.268 10.063 198.195 1.918 0.80 388219. 0.3756 82.36 0.4348 0.6734 0.0832 0.0538 13.842 87.245 42.447 10322.138 9.857 188.806 1.865 0.80 389190. 0.3565 88.24 0.4659 0.7018 0.0788 0.0523 13.468 84.884 40.167 10042.805 9.590 178.665 1.814 0.80 390215. 0.3373 94.12 0.4970 0.7279 0.0740 0.0505 13.013 82.021 37.741 9704.081 9.267 167.873 1.764 0.80 391294. 0.3179 100.00 0.5280 0.7517 0.0690 0.0485 12.484 78.683 35.189 9309.076 8.890 156.522 1.715 0.80 392427. 0.2984 105.89 0.5591 0.7730 0.0638 0.0461 11.882 74.887 32.529 8860.045 8.461 144.691 1.665 0.81 393613. 0.2786 111.77 0.5901 0.7918 0.0584 0.0435 11.209 70.647 29.777 8358.396 7.982 132.449 1.616 0.81 394852. 0.2587 117.65 0.6212 0.8077 0.0528 0.0406 10.466 65.968 26.946 7804.842 7.453 119.854 1.566 0.81 396142. 0.2385 123.53 0.6523 0.8204 0.0472 0.0375 9.655 60.856 24.047 7200.003 6.875 106.960 1.515 0.81 397483. 0.2179 129.42 0.6833 0.8294 0.0414 0.0341 8.777 55.318 21.094 6544.820 6.250 93.824 1.462 0.81 398876. 0.1970 135.30 0.7144 0.8335 0.0355 0.0304 7.834 49.375 18.099 5841.693 5.578 80.505 1.405 0.81 400320. 0.1754 141.18 0.7454 0.8307 0.0296 0.0265 6.833 43.066 15.078 5095.175 4.866 67.066 1.342 0.82 401814. 0.1529 147.06 0.7765 0.8177 0.0236 0.0224 5.776 36.407 12.045 4307.392 4.113 53.577 1.268 0.82 403356. 0.1291 152.95 0.8076 0.7873 0.0177 0.0181 4.670 29.437 9.016 3482.714 3.326 40.102 1.174 0.82 404946. 0.1034 158.83 0.8386 0.7212 0.0118 0.0137 3.522 22.199 5.997 2626.435 2.508 26.677 1.036 0.82 406575. 0.0744 164.71 0.8697 0.5622 0.0059 0.0091 2.335 14.716 2.989 1741.099 1.663 13.294 0.779 0.82 408215. 0.0395 170.59 0.9007 -0.1024 -0.0004 0.0038 0.983 6.194 -0.221 732.809 0.700 -0.984 -0.137 0.83 408187. 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 0.1073 0.0552 18.919 108.404 66.202 14107.965 12.247 294.466 2.128 0.87 418595. 0.5081 6.49 0.0311 0.0591 0.1071 0.0564 19.331 110.766 66.091 14415.448 12.514 293.972 2.079 0.87 418924. 0.4960 12.97 0.0623 0.1154 0.1069 0.0577 19.766 113.255 65.956 14739.325 12.795 293.374 2.030 0.87 419295. 0.4836 19.46 0.0934 0.1688 0.1066 0.0590 20.216 115.834 65.786 15074.962 13.087 292.618 1.979 0.87 419711. 0.4710 25.94 0.1245 0.2194 0.1063 0.0603 20.673 118.452 65.563 15415.740 13.383 291.623 1.929 0.87 420177. 0.4582 32.43 0.1557 0.2672 0.1058 0.0616 21.124 121.036 65.259 15751.933 13.675 290.272 1.879 0.87 420694. 0.4454 38.92 0.1868 0.3122 0.1051 0.0629 21.550 123.476 64.840 16069.564 13.950 288.407 1.830 0.87 421267. 0.4323 45.40 0.2179 0.3548 0.1042 0.0640 21.926 125.631 64.259 16350.053 14.194 285.826 1.783 0.87 421897. 0.4192 51.89 0.2491 0.3952 0.1029 0.0648 22.222 127.331 63.470 16571.211 14.386 282.313 1.737 0.88 422587. 0.4060 58.37 0.2802 0.4336 0.1012 0.0654 22.409 128.399 62.428 16710.174 14.506 277.678 1.694 0.88 423340. 0.3928 64.86 0.3113 0.4706 0.0990 0.0655 22.458 128.682 61.102 16747.070 14.538 271.780 1.655 0.88 424157. 0.3795 71.35 0.3425 0.5062 0.0964 0.0652 22.352 128.075 59.475 16668.064 14.470 264.543 1.618 0.88 425038. 0.3662 77.83 0.3736 0.5408 0.0933 0.0644 22.083 126.534 57.545 16467.541 14.296 255.958 1.585 0.88 425984. 0.3527 84.32 0.4047 0.5744 0.0897 0.0632 21.655 124.078 55.325 16147.930 14.018 246.085 1.554 0.88 426995. 0.3391 90.81 0.4359 0.6070 0.0856 0.0615 21.077 120.766 52.838 15716.817 13.644 235.024 1.525 0.88 428069. 0.3252 97.29 0.4670 0.6384 0.0812 0.0594 20.364 116.685 50.113 15185.703 13.183 222.904 1.497 0.88 429205. 0.3109 103.78 0.4981 0.6684 0.0765 0.0570 19.534 111.926 47.181 14566.403 12.645 209.859 1.469 0.88 430402. 0.2961 110.26 0.5293 0.6966 0.0714 0.0543 18.599 106.572 44.069 13869.591 12.040 196.019 1.441 0.88 431659. 0.2807 116.75 0.5604 0.7229 0.0661 0.0513 17.572 100.687 40.804 13103.698 11.376 181.496 1.412 0.89 432975. 0.2647 123.24 0.5915 0.7468 0.0606 0.0480 16.460 94.316 37.408 12274.556 10.656 166.390 1.382 0.89 434349. 0.2480 129.72 0.6227 0.7680 0.0549 0.0445 15.269 87.487 33.900 11385.862 9.884 150.785 1.350 0.89 435780. 0.2307 136.21 0.6538 0.7860 0.0491 0.0408 14.000 80.218 30.297 10439.789 9.063 134.759 1.316 0.89 437267. 0.2126 142.69 0.6849 0.8002 0.0431 0.0369 12.656 72.518 26.616 9437.714 8.193 118.386 1.279 0.89 438811. 0.1936 149.18 0.7161 0.8095 0.0371 0.0328 11.240 64.406 22.874 8381.929 7.277 101.744 1.238 0.90 440411. 0.1737 155.67 0.7472 0.8101 0.0309 0.0285 9.780 56.041 19.087 7293.292 6.331 84.898 1.187 0.90 442066. 0.1521 162.15 0.7783 0.7923 0.0247 0.0243 8.330 47.732 15.264 6211.978 5.393 67.896 1.115 0.90 443774. 0.1278 168.64 0.8095 0.7473 0.0185 0.0201 6.877 39.404 11.429 5128.208 4.452 50.834 1.011 0.90 445534. 0.1003 175.12 0.8406 0.6571 0.0123 0.0158 5.399 30.937 7.597 4026.281 3.495 33.792 0.856 0.90 447338. 0.0692 181.61 0.8717 0.4669 0.0061 0.0114 3.909 22.396 3.768 2914.650 2.530 16.762 0.586 0.91 449155. 0.0334 188.10 0.9029 -0.0733 -0.0005 0.0063 2.162 12.390 -0.316 1612.503 1.400 -1.405 -0.089 0.91 449583. 0.0000