20x12WE (20x12WE.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 0.0984 0.0390 0.010 0.633 0.502 7.487 0.071 2.231 30.384 0.08 39956. 0.6313 0.49 0.0258 0.0633 0.0970 0.0395 0.010 0.641 0.495 7.588 0.072 2.200 29.560 0.08 39985. 0.6099 0.98 0.0516 0.1231 0.0955 0.0400 0.010 0.649 0.487 7.683 0.073 2.165 28.739 0.08 40016. 0.5883 1.47 0.0774 0.1794 0.0938 0.0405 0.010 0.657 0.478 7.772 0.074 2.128 27.925 0.08 40050. 0.5667 1.95 0.1031 0.2322 0.0921 0.0409 0.011 0.664 0.469 7.851 0.075 2.088 27.119 0.08 40087. 0.5451 2.44 0.1289 0.2818 0.0901 0.0412 0.011 0.669 0.460 7.919 0.076 2.044 26.324 0.08 40127. 0.5236 2.93 0.1547 0.3281 0.0880 0.0415 0.011 0.674 0.449 7.973 0.076 1.997 25.541 0.08 40170. 0.5021 3.42 0.1805 0.3712 0.0858 0.0417 0.011 0.677 0.437 8.011 0.076 1.946 24.771 0.08 40216. 0.4807 3.91 0.2063 0.4113 0.0834 0.0418 0.011 0.679 0.425 8.031 0.077 1.891 24.014 0.08 40265. 0.4594 4.40 0.2321 0.4484 0.0808 0.0418 0.011 0.679 0.412 8.030 0.077 1.832 23.270 0.08 40318. 0.4382 4.88 0.2578 0.4825 0.0780 0.0417 0.011 0.677 0.398 8.006 0.076 1.770 22.539 0.08 40374. 0.4171 5.37 0.2836 0.5138 0.0751 0.0414 0.011 0.672 0.383 7.956 0.076 1.702 21.820 0.08 40434. 0.3960 5.86 0.3094 0.5423 0.0719 0.0410 0.011 0.666 0.367 7.879 0.075 1.631 21.110 0.08 40497. 0.3750 6.35 0.3352 0.5680 0.0686 0.0405 0.010 0.657 0.350 7.772 0.074 1.555 20.407 0.08 40564. 0.3540 6.84 0.3610 0.5907 0.0650 0.0398 0.010 0.645 0.332 7.633 0.073 1.475 19.709 0.08 40634. 0.3330 7.33 0.3868 0.6105 0.0613 0.0389 0.010 0.631 0.313 7.461 0.071 1.391 19.010 0.08 40708. 0.3119 7.81 0.4126 0.6271 0.0574 0.0378 0.010 0.613 0.293 7.256 0.069 1.303 18.307 0.08 40786. 0.2907 8.30 0.4383 0.6403 0.0534 0.0366 0.009 0.593 0.272 7.021 0.067 1.211 17.593 0.08 40867. 0.2693 8.79 0.4641 0.6497 0.0492 0.0352 0.009 0.571 0.251 6.754 0.065 1.117 16.860 0.08 40952. 0.2479 9.28 0.4899 0.6549 0.0450 0.0336 0.009 0.546 0.229 6.459 0.062 1.020 16.100 0.08 41041. 0.2262 9.77 0.5157 0.6551 0.0406 0.0320 0.008 0.519 0.207 6.135 0.059 0.921 15.301 0.08 41134. 0.2042 10.26 0.5415 0.6496 0.0361 0.0301 0.008 0.489 0.184 5.784 0.055 0.820 14.449 0.08 41230. 0.1820 10.74 0.5673 0.6370 0.0316 0.0282 0.007 0.457 0.161 5.407 0.052 0.717 13.525 0.08 41329. 0.1593 11.23 0.5930 0.6157 0.0271 0.0261 0.007 0.423 0.138 5.004 0.048 0.614 12.504 0.08 41433. 0.1363 11.72 0.6188 0.5831 0.0225 0.0238 0.006 0.387 0.115 4.579 0.044 0.510 11.348 0.08 41540. 0.1127 12.21 0.6446 0.5355 0.0179 0.0215 0.006 0.349 0.091 4.131 0.039 0.405 10.004 0.08 41651. 0.0886 12.70 0.6704 0.4670 0.0133 0.0191 0.005 0.310 0.068 3.665 0.035 0.302 8.389 0.08 41765. 0.0641 13.19 0.6962 0.3680 0.0088 0.0166 0.004 0.269 0.045 3.182 0.030 0.199 6.366 0.08 41883. 0.0395 13.67 0.7220 0.2217 0.0043 0.0140 0.004 0.227 0.022 2.685 0.026 0.097 3.698 0.08 42005. 0.0161 14.16 0.7478 -0.0051 -0.0001 0.0113 0.003 0.184 0.000 2.178 0.021 -0.002 -0.083 0.08 42130. 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 0.0987 0.0364 0.075 2.365 2.014 55.956 0.267 8.958 16.325 0.16 79911. 0.6797 0.98 0.0259 0.0681 0.0974 0.0370 0.076 2.401 1.986 56.820 0.271 8.833 15.852 0.16 79969. 0.6554 1.96 0.0518 0.1322 0.0959 0.0375 0.077 2.436 1.955 57.646 0.275 8.697 15.384 0.16 80031. 0.6311 2.94 0.0776 0.1924 0.0942 0.0380 0.078 2.469 1.922 58.415 0.279 8.548 14.921 0.16 80100. 0.6069 3.92 0.1035 0.2487 0.0924 0.0385 0.079 2.498 1.885 59.113 0.282 8.386 14.466 0.16 80174. 0.5828 4.90 0.1294 0.3013 0.0905 0.0389 0.080 2.524 1.846 59.719 0.285 8.211 14.020 0.16 80254. 0.5589 5.88 0.1553 0.3503 0.0884 0.0392 0.081 2.545 1.803 60.216 0.288 8.021 13.583 0.16 80340. 0.5352 6.86 0.1812 0.3958 0.0862 0.0394 0.081 2.560 1.757 60.582 0.289 7.816 13.157 0.16 80433. 0.5117 7.84 0.2071 0.4381 0.0837 0.0396 0.082 2.569 1.708 60.799 0.290 7.596 12.740 0.16 80532. 0.4885 8.82 0.2329 0.4771 0.0811 0.0396 0.082 2.571 1.655 60.846 0.291 7.360 12.334 0.16 80638. 0.4655 9.80 0.2588 0.5131 0.0783 0.0395 0.081 2.565 1.598 60.703 0.290 7.107 11.938 0.16 80752. 0.4427 10.78 0.2847 0.5461 0.0754 0.0393 0.081 2.550 1.537 60.350 0.288 6.837 11.552 0.16 80872. 0.4202 11.76 0.3106 0.5763 0.0722 0.0389 0.080 2.526 1.472 59.769 0.285 6.549 11.174 0.16 80999. 0.3978 12.74 0.3365 0.6036 0.0688 0.0384 0.079 2.491 1.404 58.940 0.281 6.244 10.803 0.16 81134. 0.3755 13.73 0.3623 0.6281 0.0653 0.0377 0.078 2.444 1.331 57.841 0.276 5.921 10.439 0.16 81275. 0.3534 14.71 0.3882 0.6498 0.0615 0.0368 0.076 2.386 1.255 56.466 0.270 5.581 10.079 0.16 81425. 0.3312 15.69 0.4141 0.6685 0.0576 0.0357 0.074 2.317 1.175 54.818 0.262 5.226 9.721 0.16 81581. 0.3091 16.67 0.4400 0.6840 0.0535 0.0344 0.071 2.236 1.092 52.906 0.253 4.857 9.362 0.16 81745. 0.2870 17.65 0.4659 0.6961 0.0493 0.0330 0.068 2.144 1.007 50.736 0.242 4.477 8.998 0.16 81916. 0.2648 18.63 0.4918 0.7043 0.0450 0.0315 0.065 2.042 0.919 48.314 0.231 4.087 8.625 0.16 82095. 0.2425 19.61 0.5176 0.7081 0.0406 0.0297 0.061 1.929 0.829 45.648 0.218 3.688 8.238 0.16 82281. 0.2201 20.59 0.5435 0.7066 0.0362 0.0278 0.057 1.806 0.738 42.746 0.204 3.282 7.828 0.16 82475. 0.1973 21.57 0.5694 0.6986 0.0316 0.0258 0.053 1.674 0.645 39.617 0.189 2.870 7.388 0.16 82675. 0.1741 22.55 0.5953 0.6823 0.0271 0.0236 0.049 1.533 0.552 36.271 0.173 2.455 6.902 0.16 82884. 0.1504 23.53 0.6212 0.6550 0.0225 0.0213 0.044 1.383 0.458 32.723 0.156 2.038 6.350 0.16 83099. 0.1261 24.51 0.6471 0.6125 0.0179 0.0189 0.039 1.225 0.364 28.987 0.138 1.620 5.701 0.16 83323. 0.1009 25.49 0.6729 0.5475 0.0133 0.0163 0.034 1.060 0.271 25.084 0.120 1.205 4.899 0.16 83553. 0.0748 26.47 0.6988 0.4468 0.0088 0.0137 0.028 0.889 0.179 21.037 0.100 0.794 3.851 0.16 83791. 0.0477 27.45 0.7247 0.2840 0.0043 0.0110 0.023 0.713 0.088 16.873 0.081 0.390 2.360 0.16 84037. 0.0205 28.43 0.7506 -0.0046 -0.0001 0.0082 0.017 0.533 -0.001 12.616 0.060 -0.005 -0.037 0.16 84287. 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 0.0992 0.0354 0.246 5.174 4.551 183.635 0.585 20.243 11.241 0.24 119863. 0.7035 1.47 0.0259 0.0704 0.0978 0.0360 0.250 5.259 4.488 186.657 0.594 19.962 10.905 0.24 119950. 0.6778 2.95 0.0518 0.1365 0.0963 0.0366 0.254 5.340 4.419 189.548 0.603 19.655 10.574 0.24 120044. 0.6521 4.42 0.0778 0.1985 0.0947 0.0371 0.258 5.417 4.344 192.253 0.612 19.321 10.248 0.24 120147. 0.6266 5.89 0.1037 0.2564 0.0929 0.0376 0.261 5.486 4.262 194.713 0.620 18.957 9.928 0.24 120259. 0.6013 7.36 0.1296 0.3104 0.0909 0.0380 0.264 5.546 4.173 196.865 0.627 18.562 9.615 0.24 120379. 0.5763 8.84 0.1555 0.3606 0.0888 0.0383 0.266 5.597 4.077 198.642 0.632 18.135 9.310 0.24 120509. 0.5515 10.31 0.1814 0.4073 0.0866 0.0386 0.268 5.634 3.973 199.977 0.637 17.674 9.012 0.24 120648. 0.5270 11.78 0.2074 0.4505 0.0841 0.0387 0.269 5.657 3.862 200.800 0.639 17.176 8.723 0.24 120798. 0.5029 13.25 0.2333 0.4905 0.0815 0.0388 0.270 5.664 3.742 201.039 0.640 16.643 8.441 0.24 120958. 0.4790 14.73 0.2592 0.5274 0.0787 0.0387 0.269 5.652 3.613 200.625 0.639 16.071 8.168 0.24 121128. 0.4555 16.20 0.2851 0.5613 0.0757 0.0385 0.268 5.621 3.476 199.492 0.635 15.460 7.903 0.24 121309. 0.4323 17.67 0.3110 0.5923 0.0726 0.0381 0.265 5.566 3.330 197.572 0.629 14.811 7.644 0.24 121500. 0.4092 19.15 0.3370 0.6204 0.0692 0.0376 0.261 5.488 3.175 194.795 0.620 14.121 7.392 0.24 121703. 0.3864 20.62 0.3629 0.6459 0.0656 0.0369 0.256 5.384 3.010 191.089 0.608 13.390 7.145 0.24 121916. 0.3637 22.09 0.3888 0.6685 0.0618 0.0360 0.250 5.252 2.837 186.426 0.593 12.620 6.903 0.24 122141. 0.3411 23.56 0.4147 0.6883 0.0579 0.0349 0.242 5.094 2.656 180.820 0.576 11.816 6.663 0.24 122377. 0.3186 25.04 0.4406 0.7052 0.0538 0.0336 0.234 4.911 2.469 174.293 0.555 10.981 6.425 0.24 122623. 0.2962 26.51 0.4666 0.7187 0.0496 0.0322 0.224 4.701 2.275 166.865 0.531 10.120 6.185 0.24 122881. 0.2737 27.98 0.4925 0.7287 0.0453 0.0306 0.213 4.467 2.077 158.560 0.505 9.237 5.940 0.24 123150. 0.2511 29.45 0.5184 0.7345 0.0408 0.0288 0.200 4.209 1.874 149.401 0.476 8.334 5.688 0.24 123430. 0.2284 30.93 0.5443 0.7354 0.0363 0.0269 0.187 3.928 1.667 139.414 0.444 7.415 5.424 0.24 123721. 0.2055 32.40 0.5702 0.7302 0.0318 0.0248 0.172 3.624 1.458 128.630 0.409 6.485 5.141 0.24 124023. 0.1821 33.87 0.5962 0.7172 0.0272 0.0226 0.157 3.299 1.247 117.088 0.373 5.546 4.830 0.24 124336. 0.1582 35.35 0.6221 0.6937 0.0225 0.0202 0.141 2.954 1.035 104.833 0.334 4.603 4.477 0.24 124661. 0.1336 36.82 0.6480 0.6553 0.0179 0.0177 0.123 2.590 0.823 91.922 0.293 3.659 4.060 0.24 124996. 0.1080 38.29 0.6739 0.5940 0.0133 0.0151 0.105 2.209 0.612 78.422 0.250 2.721 3.539 0.24 125343. 0.0812 39.76 0.6998 0.4950 0.0088 0.0124 0.086 1.815 0.403 64.419 0.205 1.794 2.840 0.24 125702. 0.0529 41.24 0.7258 0.3254 0.0043 0.0096 0.067 1.409 0.198 50.009 0.159 0.883 1.800 0.24 126071. 0.0235 42.71 0.7517 -0.0046 0.0000 0.0068 0.047 0.994 -0.002 35.265 0.112 -0.008 -0.024 0.24 126445. 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 0.0997 0.0350 0.576 9.081 8.135 429.761 1.026 36.182 8.585 0.32 159811. 0.7184 1.96 0.0259 0.0717 0.0983 0.0356 0.586 9.236 8.023 437.107 1.044 35.686 8.325 0.32 159927. 0.6918 3.93 0.0519 0.1390 0.0968 0.0361 0.596 9.385 7.901 444.148 1.060 35.142 8.068 0.32 160053. 0.6653 5.89 0.0778 0.2020 0.0952 0.0367 0.604 9.525 7.767 450.744 1.076 34.549 7.816 0.32 160191. 0.6391 7.86 0.1037 0.2608 0.0934 0.0372 0.613 9.652 7.622 456.756 1.090 33.904 7.569 0.32 160340. 0.6131 9.82 0.1297 0.3156 0.0915 0.0376 0.620 9.763 7.465 462.031 1.103 33.202 7.328 0.32 160501. 0.5874 11.79 0.1556 0.3666 0.0894 0.0380 0.625 9.855 7.294 466.409 1.113 32.442 7.093 0.32 160674. 0.5620 13.75 0.1816 0.4139 0.0871 0.0382 0.630 9.926 7.109 469.724 1.121 31.620 6.864 0.32 160861. 0.5370 15.72 0.2075 0.4578 0.0847 0.0384 0.633 9.970 6.910 471.808 1.126 30.734 6.643 0.32 161061. 0.5123 17.68 0.2334 0.4983 0.0821 0.0384 0.634 9.984 6.696 472.488 1.128 29.782 6.428 0.32 161274. 0.4879 19.65 0.2594 0.5357 0.0793 0.0384 0.632 9.965 6.466 471.597 1.126 28.762 6.219 0.32 161502. 0.4640 21.61 0.2853 0.5701 0.0763 0.0382 0.629 9.910 6.221 468.971 1.120 27.672 6.017 0.32 161743. 0.4403 23.58 0.3112 0.6017 0.0731 0.0378 0.623 9.814 5.960 464.449 1.109 26.511 5.821 0.32 162000. 0.4169 25.54 0.3372 0.6304 0.0697 0.0373 0.614 9.675 5.683 457.860 1.093 25.278 5.630 0.32 162270. 0.3937 27.51 0.3631 0.6565 0.0661 0.0365 0.602 9.488 5.389 449.029 1.072 23.970 5.443 0.32 162555. 0.3707 29.47 0.3891 0.6798 0.0623 0.0356 0.587 9.253 5.079 437.884 1.045 22.593 5.261 0.32 162855. 0.3479 31.44 0.4150 0.7004 0.0583 0.0345 0.569 8.969 4.756 424.454 1.013 21.153 5.082 0.32 163170. 0.3251 33.40 0.4409 0.7181 0.0542 0.0333 0.548 8.638 4.420 408.787 0.976 19.659 4.904 0.32 163500. 0.3025 35.37 0.4669 0.7328 0.0499 0.0318 0.524 8.261 4.073 390.934 0.933 18.118 4.726 0.32 163844. 0.2798 37.33 0.4928 0.7440 0.0456 0.0302 0.497 7.838 3.718 370.948 0.886 16.536 4.546 0.32 164203. 0.2571 39.30 0.5187 0.7512 0.0411 0.0284 0.468 7.372 3.354 348.883 0.833 14.919 4.361 0.32 164577. 0.2343 41.26 0.5447 0.7539 0.0366 0.0264 0.436 6.863 2.984 324.802 0.775 13.274 4.167 0.32 164966. 0.2112 43.23 0.5706 0.7507 0.0320 0.0243 0.401 6.313 2.610 298.782 0.713 11.607 3.961 0.32 165369. 0.1877 45.19 0.5965 0.7402 0.0274 0.0220 0.363 5.725 2.231 270.912 0.647 9.926 3.736 0.32 165788. 0.1637 47.16 0.6225 0.7196 0.0227 0.0196 0.324 5.099 1.852 241.304 0.576 8.236 3.481 0.32 166221. 0.1390 49.12 0.6484 0.6844 0.0180 0.0171 0.282 4.439 1.472 210.097 0.502 6.548 3.178 0.32 166669. 0.1131 51.09 0.6744 0.6266 0.0134 0.0144 0.238 3.750 1.095 177.459 0.424 4.869 2.798 0.32 167132. 0.0859 53.05 0.7003 0.5300 0.0088 0.0117 0.193 3.034 0.721 143.594 0.343 3.209 2.279 0.33 167610. 0.0568 55.02 0.7262 0.3570 0.0044 0.0088 0.146 2.298 0.355 108.743 0.260 1.579 1.480 0.33 168103. 0.0259 56.98 0.7522 -0.0056 0.0000 0.0059 0.098 1.544 -0.004 73.064 0.174 -0.016 -0.023 0.33 168602. 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 0.1004 0.0348 1.121 14.132 12.797 836.012 1.597 56.922 6.943 0.40 199754. 0.7287 2.46 0.0259 0.0725 0.0990 0.0354 1.141 14.380 12.624 850.686 1.625 56.151 6.731 0.40 199899. 0.7016 4.91 0.0519 0.1404 0.0975 0.0360 1.160 14.618 12.434 864.763 1.652 55.307 6.522 0.40 200057. 0.6747 7.37 0.0778 0.2040 0.0959 0.0366 1.177 14.842 12.227 877.968 1.677 54.385 6.317 0.40 200229. 0.6480 9.82 0.1037 0.2633 0.0941 0.0371 1.194 15.045 12.001 890.019 1.700 53.379 6.116 0.40 200415. 0.6216 12.28 0.1297 0.3186 0.0922 0.0375 1.208 15.224 11.755 900.615 1.720 52.285 5.920 0.40 200617. 0.5955 14.73 0.1556 0.3701 0.0901 0.0379 1.220 15.374 11.488 909.436 1.737 51.098 5.729 0.40 200834. 0.5697 17.19 0.1815 0.4178 0.0879 0.0382 1.229 15.487 11.199 916.154 1.750 49.813 5.544 0.40 201068. 0.5443 19.64 0.2074 0.4620 0.0854 0.0383 1.234 15.559 10.887 920.429 1.758 48.426 5.365 0.40 201318. 0.5193 22.10 0.2334 0.5030 0.0828 0.0384 1.236 15.585 10.552 921.922 1.761 46.934 5.191 0.40 201585. 0.4947 24.56 0.2593 0.5408 0.0800 0.0383 1.234 15.557 10.192 920.298 1.758 45.334 5.023 0.40 201870. 0.4705 27.01 0.2852 0.5756 0.0769 0.0381 1.227 15.471 9.808 915.229 1.748 43.624 4.860 0.40 202173. 0.4466 29.47 0.3112 0.6075 0.0737 0.0378 1.215 15.322 9.398 906.397 1.731 41.801 4.703 0.40 202493. 0.4230 31.92 0.3371 0.6367 0.0703 0.0372 1.198 15.104 8.962 893.464 1.706 39.863 4.550 0.40 202832. 0.3996 34.38 0.3630 0.6632 0.0667 0.0365 1.175 14.810 8.500 876.081 1.673 37.808 4.401 0.40 203189. 0.3764 36.83 0.3890 0.6871 0.0629 0.0356 1.145 14.438 8.013 854.092 1.631 35.641 4.255 0.40 203564. 0.3534 39.29 0.4149 0.7084 0.0589 0.0345 1.110 13.989 7.503 827.546 1.580 33.376 4.113 0.40 203958. 0.3305 41.74 0.4408 0.7268 0.0547 0.0332 1.068 13.465 6.975 796.537 1.521 31.023 3.972 0.40 204370. 0.3077 44.20 0.4668 0.7423 0.0504 0.0317 1.021 12.867 6.429 761.165 1.454 28.595 3.831 0.40 204801. 0.2850 46.66 0.4927 0.7545 0.0460 0.0301 0.968 12.197 5.868 721.531 1.378 26.102 3.689 0.40 205250. 0.2622 49.11 0.5186 0.7630 0.0415 0.0282 0.909 11.457 5.295 677.744 1.294 23.553 3.544 0.40 205717. 0.2392 51.57 0.5445 0.7670 0.0370 0.0262 0.845 10.649 4.712 629.929 1.203 20.960 3.393 0.40 206203. 0.2161 54.02 0.5705 0.7656 0.0323 0.0241 0.775 9.775 4.121 578.233 1.104 18.332 3.233 0.40 206708. 0.1925 56.48 0.5964 0.7572 0.0277 0.0218 0.701 8.838 3.525 522.839 0.999 15.680 3.058 0.40 207231. 0.1684 58.93 0.6223 0.7391 0.0230 0.0193 0.622 7.843 2.926 463.969 0.886 13.016 2.861 0.40 207773. 0.1436 61.39 0.6483 0.7069 0.0183 0.0167 0.539 6.794 2.327 401.898 0.768 10.352 2.627 0.41 208333. 0.1176 63.84 0.6742 0.6525 0.0136 0.0140 0.452 5.696 1.732 336.964 0.644 7.703 2.331 0.41 208912. 0.0900 66.30 0.7001 0.5591 0.0090 0.0112 0.362 4.557 1.143 269.578 0.515 5.085 1.923 0.41 209509. 0.0603 68.76 0.7261 0.3858 0.0044 0.0083 0.269 3.385 0.565 200.223 0.382 2.513 1.280 0.41 210125. 0.0282 71.21 0.7520 -0.0006 0.0000 0.0054 0.173 2.184 -0.001 129.205 0.247 -0.002 -0.002 0.41 210748. 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 0.1012 0.0349 1.942 20.397 18.583 1447.957 2.304 82.657 5.821 0.48 239689. 0.7362 2.95 0.0259 0.0729 0.0999 0.0355 1.977 20.763 18.336 1473.929 2.346 81.559 5.643 0.48 239863. 0.7089 5.89 0.0519 0.1412 0.0984 0.0361 2.010 21.115 18.065 1498.859 2.386 80.353 5.467 0.48 240053. 0.6817 8.84 0.0778 0.2052 0.0968 0.0367 2.041 21.444 17.768 1522.264 2.423 79.032 5.294 0.48 240260. 0.6547 11.79 0.1037 0.2649 0.0950 0.0372 2.070 21.745 17.444 1543.643 2.457 77.589 5.125 0.48 240484. 0.6280 14.73 0.1297 0.3205 0.0931 0.0377 2.095 22.011 17.090 1562.465 2.487 76.017 4.961 0.48 240727. 0.6017 17.68 0.1556 0.3722 0.0910 0.0380 2.116 22.232 16.706 1578.163 2.512 74.308 4.801 0.48 240988. 0.5757 20.63 0.1815 0.4202 0.0887 0.0383 2.132 22.401 16.289 1590.156 2.531 72.456 4.646 0.48 241269. 0.5502 23.58 0.2075 0.4647 0.0863 0.0385 2.143 22.509 15.839 1597.845 2.543 70.454 4.496 0.48 241570. 0.5250 26.52 0.2334 0.5059 0.0836 0.0386 2.146 22.548 15.355 1600.630 2.547 68.297 4.351 0.48 241892. 0.5002 29.47 0.2593 0.5440 0.0808 0.0385 2.143 22.510 14.834 1597.918 2.543 65.982 4.211 0.48 242235. 0.4758 32.42 0.2853 0.5791 0.0778 0.0383 2.131 22.386 14.277 1589.134 2.529 63.504 4.075 0.48 242599. 0.4517 35.36 0.3112 0.6114 0.0745 0.0379 2.110 22.169 13.683 1573.715 2.505 60.861 3.944 0.48 242984. 0.4280 38.31 0.3371 0.6409 0.0711 0.0374 2.080 21.850 13.051 1551.074 2.469 58.049 3.816 0.48 243392. 0.4045 41.26 0.3631 0.6679 0.0674 0.0367 2.039 21.421 12.380 1520.592 2.420 55.064 3.693 0.48 243821. 0.3812 44.20 0.3890 0.6922 0.0636 0.0357 1.987 20.877 11.672 1481.975 2.359 51.915 3.572 0.48 244272. 0.3580 47.15 0.4149 0.7140 0.0595 0.0346 1.925 20.219 10.931 1435.298 2.284 48.620 3.454 0.48 244746. 0.3351 50.10 0.4409 0.7331 0.0554 0.0333 1.852 19.450 10.161 1380.728 2.197 45.196 3.338 0.48 245241. 0.3122 53.04 0.4668 0.7493 0.0510 0.0318 1.768 18.573 9.366 1318.439 2.098 41.661 3.222 0.48 245758. 0.2893 55.99 0.4927 0.7624 0.0466 0.0301 1.674 17.589 8.550 1248.609 1.987 38.029 3.106 0.48 246298. 0.2664 58.94 0.5187 0.7718 0.0420 0.0282 1.571 16.502 7.715 1171.430 1.864 34.316 2.987 0.48 246860. 0.2434 61.89 0.5446 0.7771 0.0374 0.0262 1.458 15.314 6.865 1087.123 1.730 30.535 2.864 0.48 247443. 0.2202 64.83 0.5705 0.7771 0.0327 0.0240 1.336 14.030 6.003 995.951 1.585 26.703 2.734 0.48 248049. 0.1965 67.78 0.5965 0.7703 0.0280 0.0217 1.205 12.653 5.134 898.233 1.430 22.836 2.592 0.48 248678. 0.1723 70.73 0.6224 0.7543 0.0232 0.0192 1.065 11.190 4.260 794.364 1.264 18.950 2.433 0.49 249328. 0.1473 73.67 0.6483 0.7245 0.0185 0.0165 0.918 9.647 3.387 684.832 1.090 15.064 2.243 0.49 250001. 0.1211 76.62 0.6743 0.6727 0.0137 0.0137 0.765 8.033 2.518 570.241 0.908 11.200 2.003 0.49 250696. 0.0932 79.57 0.7002 0.5816 0.0090 0.0109 0.605 6.358 1.659 451.321 0.718 7.379 1.667 0.49 251413. 0.0630 82.51 0.7261 0.4068 0.0044 0.0079 0.441 4.634 0.815 328.936 0.524 3.627 1.124 0.49 252152. 0.0298 85.46 0.7521 -0.0083 -0.0001 0.0049 0.273 2.868 -0.010 203.559 0.324 -0.044 -0.022 0.49 252897. 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 0.1023 0.0352 3.107 27.976 25.551 2316.916 3.161 113.653 5.002 0.56 279613. 0.7418 3.46 0.0261 0.0736 0.1009 0.0358 3.164 28.491 25.217 2359.564 3.219 112.167 4.847 0.56 279818. 0.7142 6.92 0.0522 0.1425 0.0995 0.0364 3.219 28.985 24.850 2400.526 3.275 110.531 4.695 0.56 280042. 0.6867 10.39 0.0783 0.2070 0.0978 0.0370 3.271 29.450 24.445 2438.976 3.327 108.733 4.546 0.56 280287. 0.6594 13.85 0.1044 0.2671 0.0961 0.0376 3.318 29.874 24.003 2474.082 3.375 106.763 4.400 0.56 280551. 0.6325 17.31 0.1306 0.3231 0.0941 0.0380 3.359 30.246 23.518 2504.951 3.417 104.610 4.258 0.56 280838. 0.6059 20.77 0.1567 0.3752 0.0920 0.0384 3.394 30.557 22.991 2530.641 3.452 102.264 4.121 0.56 281147. 0.5797 24.23 0.1828 0.4236 0.0897 0.0387 3.420 30.792 22.418 2550.179 3.479 99.714 3.987 0.56 281479. 0.5539 27.69 0.2089 0.4684 0.0872 0.0389 3.436 30.942 21.797 2562.569 3.496 96.952 3.858 0.56 281836. 0.5284 31.16 0.2350 0.5099 0.0846 0.0390 3.442 30.993 21.127 2566.815 3.502 93.972 3.733 0.56 282216. 0.5034 34.62 0.2611 0.5483 0.0817 0.0389 3.436 30.934 20.406 2561.931 3.495 90.765 3.613 0.56 282621. 0.4788 38.08 0.2872 0.5837 0.0786 0.0387 3.416 30.754 19.633 2546.969 3.475 87.329 3.496 0.56 283052. 0.4545 41.54 0.3133 0.6163 0.0753 0.0383 3.381 30.440 18.808 2521.000 3.439 83.658 3.384 0.56 283508. 0.4305 45.00 0.3395 0.6461 0.0718 0.0377 3.330 29.982 17.929 2483.056 3.387 79.747 3.275 0.56 283990. 0.4068 48.47 0.3656 0.6734 0.0680 0.0369 3.262 29.367 16.995 2432.124 3.318 75.592 3.169 0.56 284498. 0.3833 51.93 0.3917 0.6981 0.0641 0.0359 3.175 28.590 16.009 2367.753 3.230 71.206 3.067 0.56 285032. 0.3600 55.39 0.4178 0.7203 0.0599 0.0348 3.071 27.652 14.976 2290.087 3.124 66.614 2.966 0.56 285592. 0.3368 58.85 0.4439 0.7397 0.0556 0.0334 2.949 26.557 13.903 2199.406 3.000 61.841 2.867 0.56 286178. 0.3136 62.31 0.4700 0.7564 0.0512 0.0318 2.811 25.308 12.795 2096.004 2.859 56.912 2.769 0.56 286790. 0.2906 65.77 0.4961 0.7699 0.0467 0.0301 2.655 23.910 11.656 1980.181 2.701 51.847 2.670 0.56 287428. 0.2674 69.24 0.5222 0.7798 0.0420 0.0281 2.484 22.365 10.492 1852.267 2.527 46.668 2.569 0.56 288092. 0.2441 72.70 0.5484 0.7855 0.0372 0.0260 2.297 20.679 9.307 1712.635 2.336 41.396 2.465 0.56 288782. 0.2206 76.16 0.5745 0.7860 0.0324 0.0237 2.094 18.857 8.105 1561.734 2.130 36.053 2.354 0.56 289499. 0.1966 79.62 0.6006 0.7795 0.0276 0.0213 1.878 16.906 6.893 1400.116 1.910 30.661 2.233 0.57 290241. 0.1720 83.08 0.6267 0.7633 0.0227 0.0187 1.647 14.833 5.676 1228.462 1.676 25.246 2.096 0.57 291010. 0.1465 86.55 0.6528 0.7325 0.0178 0.0159 1.405 12.650 4.459 1047.616 1.429 19.835 1.931 0.57 291805. 0.1196 90.01 0.6789 0.6775 0.0130 0.0130 1.151 10.368 3.250 858.622 1.171 14.458 1.717 0.57 292626. 0.0908 93.47 0.7050 0.5768 0.0082 0.0101 0.889 8.002 2.057 662.748 0.904 9.148 1.408 0.57 293474. 0.0592 96.93 0.7311 0.3700 0.0035 0.0070 0.619 5.572 0.886 461.479 0.630 3.941 0.871 0.57 294346. 0.0240 100.39 0.7573 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 0.1035 0.0356 4.697 37.007 33.779 3502.704 4.181 150.251 4.374 0.63 319525. 0.7459 3.94 0.0260 0.0733 0.1022 0.0363 4.785 37.699 33.354 3568.185 4.259 148.357 4.240 0.63 319759. 0.7184 7.88 0.0520 0.1419 0.1008 0.0369 4.869 38.364 32.883 3631.137 4.334 146.263 4.107 0.63 320015. 0.6910 11.82 0.0780 0.2062 0.0992 0.0375 4.949 38.989 32.364 3690.312 4.405 143.956 3.978 0.63 320293. 0.6639 15.77 0.1040 0.2662 0.0974 0.0381 5.021 39.561 31.794 3744.426 4.470 141.419 3.851 0.64 320596. 0.6371 19.71 0.1301 0.3221 0.0955 0.0386 5.085 40.065 31.169 3792.106 4.526 138.639 3.728 0.64 320923. 0.6106 23.65 0.1561 0.3741 0.0934 0.0390 5.139 40.485 30.486 3831.916 4.574 135.600 3.608 0.64 321275. 0.5845 27.59 0.1821 0.4224 0.0911 0.0393 5.180 40.807 29.742 3862.369 4.610 132.290 3.493 0.64 321654. 0.5588 31.53 0.2081 0.4673 0.0887 0.0395 5.206 41.014 28.934 3881.949 4.634 128.698 3.381 0.64 322061. 0.5335 35.47 0.2341 0.5089 0.0860 0.0396 5.215 41.090 28.060 3889.133 4.642 124.811 3.273 0.64 322495. 0.5086 39.41 0.2601 0.5474 0.0831 0.0395 5.206 41.019 27.119 3882.440 4.634 120.624 3.168 0.64 322957. 0.4840 43.35 0.2861 0.5830 0.0800 0.0393 5.177 40.787 26.108 3860.422 4.608 116.127 3.067 0.64 323448. 0.4598 47.30 0.3121 0.6158 0.0767 0.0389 5.125 40.377 25.026 3821.679 4.562 111.318 2.970 0.64 323967. 0.4359 51.24 0.3382 0.6460 0.0732 0.0383 5.049 39.776 23.873 3764.779 4.494 106.188 2.876 0.64 324516. 0.4123 55.18 0.3642 0.6737 0.0694 0.0375 4.946 38.967 22.647 3688.185 4.402 100.732 2.785 0.64 325095. 0.3888 59.12 0.3902 0.6989 0.0654 0.0365 4.816 37.941 21.349 3591.087 4.287 94.962 2.697 0.64 325703. 0.3655 63.06 0.4162 0.7216 0.0613 0.0353 4.658 36.700 19.989 3473.652 4.146 88.912 2.610 0.64 326340. 0.3424 67.00 0.4422 0.7417 0.0569 0.0339 4.474 35.249 18.574 3336.310 3.982 82.617 2.525 0.64 327007. 0.3193 70.94 0.4682 0.7591 0.0524 0.0323 4.264 33.593 17.110 3179.522 3.795 76.107 2.441 0.64 327703. 0.2962 74.88 0.4942 0.7736 0.0478 0.0306 4.028 31.736 15.605 3003.751 3.585 69.412 2.356 0.64 328429. 0.2731 78.83 0.5202 0.7847 0.0431 0.0286 3.768 29.683 14.065 2809.502 3.354 62.560 2.271 0.64 329184. 0.2498 82.77 0.5463 0.7917 0.0383 0.0264 3.483 27.442 12.495 2597.340 3.100 55.579 2.182 0.64 329969. 0.2263 86.71 0.5723 0.7939 0.0334 0.0241 3.175 25.018 10.903 2367.944 2.827 48.498 2.088 0.65 330783. 0.2023 90.65 0.5983 0.7895 0.0285 0.0216 2.846 22.421 9.296 2122.137 2.533 41.347 1.987 0.65 331626. 0.1777 94.59 0.6243 0.7762 0.0235 0.0189 2.496 19.661 7.679 1860.943 2.221 34.158 1.872 0.65 332500. 0.1522 98.53 0.6503 0.7492 0.0186 0.0161 2.126 16.753 6.063 1585.630 1.893 26.969 1.734 0.65 333402. 0.1253 102.47 0.6763 0.6995 0.0137 0.0132 1.740 13.711 4.455 1297.762 1.549 19.818 1.557 0.65 334335. 0.0964 106.41 0.7023 0.6070 0.0088 0.0102 1.340 10.557 2.866 999.256 1.193 12.750 1.301 0.65 335297. 0.0646 110.36 0.7283 0.4142 0.0040 0.0070 0.928 7.315 1.307 692.372 0.826 5.814 0.856 0.65 336288. 0.0287 114.30 0.7544 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 0.1050 0.0364 6.831 47.841 43.367 5094.149 5.405 192.894 3.861 0.71 359421. 0.7460 4.41 0.0259 0.0724 0.1037 0.0371 6.956 48.714 42.847 5187.057 5.504 190.584 3.747 0.71 359683. 0.7195 8.81 0.0517 0.1404 0.1023 0.0377 7.076 49.556 42.270 5276.798 5.599 188.019 3.633 0.71 359969. 0.6930 13.22 0.0776 0.2041 0.1008 0.0383 7.190 50.353 41.632 5361.589 5.689 185.179 3.522 0.71 360281. 0.6667 17.63 0.1034 0.2637 0.0991 0.0389 7.295 51.085 40.927 5439.559 5.772 182.043 3.413 0.71 360620. 0.6405 22.03 0.1293 0.3193 0.0972 0.0394 7.387 51.734 40.151 5508.712 5.845 178.592 3.306 0.71 360986. 0.6146 26.44 0.1551 0.3711 0.0952 0.0398 7.465 52.281 39.300 5566.903 5.907 174.806 3.202 0.71 361381. 0.5889 30.85 0.1810 0.4194 0.0929 0.0401 7.526 52.704 38.370 5611.916 5.954 170.668 3.101 0.72 361805. 0.5636 35.25 0.2068 0.4642 0.0904 0.0403 7.565 52.981 37.357 5641.460 5.986 166.162 3.003 0.72 362260. 0.5386 39.66 0.2327 0.5058 0.0878 0.0404 7.581 53.092 36.258 5653.227 5.998 161.275 2.909 0.72 362746. 0.5139 44.07 0.2585 0.5444 0.0849 0.0403 7.570 53.014 35.071 5644.962 5.989 155.995 2.818 0.72 363263. 0.4896 48.47 0.2844 0.5801 0.0818 0.0401 7.529 52.728 33.793 5614.489 5.957 150.313 2.730 0.72 363812. 0.4656 52.88 0.3102 0.6132 0.0785 0.0397 7.456 52.214 32.424 5559.801 5.899 144.224 2.645 0.72 364394. 0.4419 57.29 0.3361 0.6437 0.0750 0.0391 7.347 51.454 30.962 5478.868 5.813 137.720 2.563 0.72 365007. 0.4184 61.69 0.3619 0.6718 0.0712 0.0384 7.201 50.427 29.404 5369.501 5.697 130.791 2.484 0.72 365654. 0.3952 66.10 0.3878 0.6974 0.0672 0.0374 7.014 49.120 27.754 5230.284 5.550 123.448 2.407 0.72 366333. 0.3720 70.51 0.4136 0.7207 0.0630 0.0362 6.787 47.533 26.019 5061.347 5.370 115.733 2.332 0.72 367045. 0.3489 74.91 0.4395 0.7416 0.0586 0.0347 6.522 45.673 24.211 4863.311 5.160 107.691 2.258 0.72 367790. 0.3260 79.32 0.4653 0.7598 0.0541 0.0331 6.218 43.547 22.339 4636.859 4.920 99.362 2.185 0.72 368567. 0.3030 83.73 0.4912 0.7753 0.0494 0.0313 5.877 41.160 20.410 4382.702 4.650 90.785 2.112 0.72 369376. 0.2800 88.13 0.5170 0.7876 0.0446 0.0293 5.500 38.519 18.434 4101.568 4.352 81.994 2.039 0.72 370218. 0.2568 92.54 0.5429 0.7962 0.0398 0.0271 5.088 35.634 16.418 3794.296 4.026 73.028 1.963 0.72 371093. 0.2333 96.95 0.5687 0.8002 0.0348 0.0247 4.643 32.512 14.371 3461.916 3.673 63.921 1.883 0.73 372000. 0.2094 101.35 0.5946 0.7982 0.0298 0.0222 4.165 29.167 12.301 3105.694 3.295 54.713 1.796 0.73 372940. 0.1848 105.76 0.6205 0.7878 0.0247 0.0195 3.657 25.612 10.217 2727.223 2.894 45.445 1.699 0.73 373913. 0.1593 110.17 0.6463 0.7649 0.0197 0.0166 3.123 21.868 8.130 2328.516 2.471 36.164 1.584 0.73 374918. 0.1325 114.57 0.6722 0.7210 0.0147 0.0137 2.564 17.957 6.052 1912.112 2.029 26.918 1.436 0.73 375956. 0.1036 118.98 0.6980 0.6380 0.0097 0.0106 1.986 13.910 3.994 1481.169 1.572 17.766 1.223 0.73 377027. 0.0717 123.39 0.7239 0.4653 0.0048 0.0074 1.394 9.762 1.971 1039.486 1.103 8.768 0.860 0.73 378129. 0.0354 127.79 0.7497 -0.0045 0.0000 0.0042 0.790 5.535 -0.011 589.348 0.625 -0.047 -0.008 0.73 379239. 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 0.1067 0.0388 9.994 62.990 54.417 7452.430 7.117 242.047 3.312 0.79 399294. 0.7168 4.89 0.0258 0.0692 0.1055 0.0394 10.138 63.901 53.808 7560.233 7.219 239.338 3.228 0.79 399585. 0.6947 9.77 0.0516 0.1347 0.1042 0.0399 10.276 64.770 53.127 7662.999 7.318 236.308 3.145 0.79 399903. 0.6724 14.66 0.0774 0.1967 0.1027 0.0404 10.404 65.577 52.367 7758.490 7.409 232.931 3.061 0.79 400250. 0.6500 19.54 0.1032 0.2553 0.1010 0.0409 10.520 66.303 51.524 7844.419 7.491 229.177 2.979 0.79 400627. 0.6274 24.43 0.1290 0.3104 0.0992 0.0412 10.619 66.927 50.589 7918.312 7.561 225.020 2.898 0.79 401034. 0.6047 29.32 0.1548 0.3621 0.0972 0.0415 10.698 67.428 49.558 7977.561 7.618 220.432 2.818 0.79 401474. 0.5819 34.20 0.1806 0.4107 0.0950 0.0418 10.754 67.782 48.424 8019.390 7.658 215.389 2.739 0.79 401947. 0.5591 39.09 0.2064 0.4561 0.0925 0.0419 10.783 67.965 47.183 8041.013 7.679 209.869 2.661 0.80 402453. 0.5363 43.98 0.2322 0.4985 0.0899 0.0419 10.781 67.952 45.830 8039.554 7.677 203.853 2.586 0.80 402994. 0.5135 48.86 0.2580 0.5380 0.0870 0.0417 10.744 67.720 44.363 8012.133 7.651 197.327 2.511 0.80 403570. 0.4908 53.75 0.2838 0.5747 0.0839 0.0414 10.669 67.245 42.779 7955.873 7.597 190.280 2.439 0.80 404181. 0.4680 58.63 0.3096 0.6087 0.0806 0.0410 10.551 66.501 41.075 7867.895 7.513 182.702 2.368 0.80 404829. 0.4452 63.52 0.3354 0.6401 0.0770 0.0403 10.387 65.465 39.251 7745.246 7.396 174.587 2.299 0.80 405512. 0.4225 68.41 0.3612 0.6690 0.0732 0.0395 10.171 64.107 37.303 7584.600 7.243 165.922 2.231 0.80 406231. 0.3997 73.29 0.3870 0.6955 0.0691 0.0385 9.901 62.406 35.233 7383.387 7.051 156.716 2.164 0.80 406986. 0.3769 78.18 0.4128 0.7195 0.0648 0.0372 9.577 60.362 33.053 7141.513 6.820 147.021 2.099 0.80 407778. 0.3541 83.07 0.4386 0.7410 0.0604 0.0357 9.199 57.980 30.776 6859.708 6.551 136.892 2.035 0.80 408606. 0.3312 87.95 0.4644 0.7600 0.0557 0.0341 8.769 55.267 28.414 6538.785 6.244 126.384 1.971 0.80 409469. 0.3082 92.84 0.4902 0.7760 0.0509 0.0322 8.287 52.231 25.977 6179.589 5.901 115.545 1.907 0.80 410368. 0.2851 97.72 0.5160 0.7888 0.0460 0.0301 7.756 48.883 23.476 5783.402 5.523 104.423 1.841 0.80 411303. 0.2617 102.61 0.5418 0.7976 0.0410 0.0279 7.177 45.237 20.922 5352.099 5.111 93.061 1.773 0.81 412274. 0.2379 107.50 0.5676 0.8014 0.0359 0.0255 6.555 41.312 18.324 4887.754 4.667 81.507 1.700 0.81 413281. 0.2136 112.38 0.5934 0.7983 0.0308 0.0229 5.891 37.132 15.695 4393.150 4.195 69.810 1.620 0.81 414323. 0.1883 117.27 0.6192 0.7856 0.0256 0.0202 5.192 32.724 13.044 3871.666 3.697 58.021 1.528 0.81 415401. 0.1619 122.16 0.6450 0.7582 0.0204 0.0173 4.462 28.124 10.386 3327.379 3.177 46.197 1.416 0.81 416515. 0.1339 127.04 0.6708 0.7065 0.0152 0.0144 3.708 23.373 7.734 2765.286 2.641 34.401 1.269 0.81 417665. 0.1035 131.93 0.6966 0.6111 0.0100 0.0114 2.939 18.521 5.104 2191.264 2.093 22.705 1.057 0.81 418851. 0.0700 136.81 0.7224 0.4245 0.0049 0.0084 2.162 13.625 2.515 1612.050 1.539 11.189 0.708 0.81 420072. 0.0329 141.70 0.7482 -0.0065 0.0000 0.0054 1.383 8.720 -0.024 1031.629 0.985 -0.106 -0.010 0.82 421305. 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 0.1084 0.0453 15.533 89.000 66.878 11582.682 10.055 297.473 2.619 0.87 439148. 0.6283 5.38 0.0258 0.0607 0.1073 0.0457 15.663 89.749 66.202 11680.207 10.140 294.468 2.571 0.87 439468. 0.6137 10.77 0.0517 0.1191 0.1061 0.0460 15.777 90.400 65.438 11764.943 10.213 291.068 2.523 0.87 439818. 0.5987 16.15 0.0775 0.1752 0.1047 0.0463 15.869 90.930 64.576 11833.849 10.273 287.235 2.475 0.87 440200. 0.5835 21.53 0.1034 0.2292 0.1031 0.0465 15.937 91.315 63.608 11884.007 10.317 282.929 2.428 0.87 440615. 0.5680 26.92 0.1292 0.2809 0.1013 0.0466 15.975 91.534 62.525 11912.542 10.341 278.112 2.381 0.87 441066. 0.5523 32.30 0.1550 0.3305 0.0994 0.0466 15.980 91.566 61.319 11916.658 10.345 272.746 2.334 0.87 441552. 0.5362 37.68 0.1809 0.3779 0.0972 0.0465 15.950 91.389 59.981 11893.657 10.325 266.797 2.287 0.87 442075. 0.5197 43.07 0.2067 0.4231 0.0948 0.0463 15.879 90.984 58.507 11840.876 10.279 260.237 2.241 0.87 442637. 0.5029 48.45 0.2326 0.4662 0.0922 0.0460 15.765 90.329 56.888 11755.683 10.205 253.038 2.195 0.88 443236. 0.4857 53.83 0.2584 0.5071 0.0893 0.0455 15.603 89.405 55.121 11635.437 10.101 245.179 2.149 0.88 443875. 0.4680 59.22 0.2842 0.5458 0.0862 0.0449 15.391 88.191 53.202 11477.416 9.964 236.643 2.102 0.88 444554. 0.4499 64.60 0.3101 0.5823 0.0829 0.0441 15.125 86.663 51.128 11278.605 9.791 227.416 2.056 0.88 445272. 0.4313 69.98 0.3359 0.6165 0.0793 0.0432 14.800 84.802 48.896 11036.354 9.581 217.489 2.010 0.88 446029. 0.4122 75.37 0.3618 0.6485 0.0754 0.0421 14.412 82.581 46.504 10747.310 9.330 206.849 1.963 0.88 446827. 0.3927 80.75 0.3876 0.6780 0.0712 0.0407 13.958 79.979 43.953 10408.682 9.036 195.505 1.915 0.88 447665. 0.3725 86.13 0.4134 0.7052 0.0669 0.0392 13.438 76.995 41.259 10020.411 8.699 183.520 1.868 0.88 448543. 0.3519 91.52 0.4393 0.7295 0.0623 0.0375 12.858 73.673 38.437 9588.057 8.324 170.967 1.818 0.88 449460. 0.3307 96.90 0.4651 0.7503 0.0575 0.0357 12.226 70.052 35.502 9116.808 7.914 157.911 1.766 0.88 450417. 0.3087 102.28 0.4910 0.7671 0.0526 0.0337 11.543 66.142 32.467 8607.958 7.473 144.415 1.711 0.88 451413. 0.2860 107.67 0.5168 0.7787 0.0476 0.0316 10.820 62.000 29.347 8068.806 7.005 130.537 1.650 0.88 452448. 0.2622 113.05 0.5426 0.7833 0.0424 0.0294 10.065 57.671 26.154 7505.535 6.516 116.332 1.581 0.89 453522. 0.2371 118.43 0.5685 0.7807 0.0371 0.0270 9.265 53.088 22.903 6909.008 5.998 101.872 1.504 0.89 454635. 0.2111 123.82 0.5943 0.7682 0.0318 0.0246 8.427 48.287 19.609 6284.195 5.455 87.220 1.415 0.89 455787. 0.1839 129.20 0.6202 0.7421 0.0264 0.0221 7.561 43.325 16.287 5638.427 4.895 72.447 1.310 0.89 456978. 0.1551 134.58 0.6460 0.6962 0.0210 0.0195 6.678 38.265 12.956 4979.907 4.323 57.628 1.180 0.89 458209. 0.1246 139.97 0.6718 0.6211 0.0156 0.0169 5.789 33.170 9.633 4316.786 3.747 42.849 1.012 0.89 459479. 0.0922 145.35 0.6977 0.5010 0.0103 0.0143 4.906 28.111 6.342 3658.394 3.176 28.210 0.786 0.89 460788. 0.0581 150.73 0.7235 0.3089 0.0050 0.0118 4.042 23.159 3.107 3014.034 2.617 13.818 0.467 0.90 462135. 0.0242 156.12 0.7494 -0.0080 -0.0001 0.0093 3.197 18.320 -0.062 2384.227 2.070 -0.275 -0.012 0.90 463505. 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 0.1075 0.0533 23.739 124.685 78.928 17702.100 14.087 351.074 2.022 0.95 479101. 0.5271 5.94 0.0261 0.0518 0.1066 0.0538 23.954 125.816 78.285 17862.559 14.215 348.211 1.988 0.95 479442. 0.5160 11.89 0.0523 0.1018 0.1056 0.0543 24.144 126.811 77.545 18003.951 14.327 344.919 1.954 0.95 479819. 0.5047 17.83 0.0784 0.1501 0.1045 0.0546 24.298 127.623 76.695 18119.197 14.419 341.141 1.920 0.95 480230. 0.4933 23.77 0.1046 0.1967 0.1031 0.0549 24.408 128.199 75.722 18200.875 14.484 336.812 1.887 0.95 480681. 0.4817 29.71 0.1307 0.2417 0.1016 0.0550 24.462 128.483 74.611 18241.320 14.516 331.869 1.855 0.95 481170. 0.4701 35.66 0.1569 0.2852 0.0999 0.0549 24.451 128.425 73.347 18233.076 14.509 326.247 1.825 0.95 481701. 0.4584 41.60 0.1830 0.3274 0.0979 0.0548 24.366 127.977 71.916 18169.361 14.459 319.884 1.795 0.95 482275. 0.4467 47.54 0.2092 0.3683 0.0958 0.0544 24.198 127.097 70.307 18044.539 14.359 312.724 1.767 0.95 482892. 0.4347 53.49 0.2353 0.4081 0.0933 0.0538 23.943 125.758 68.507 17854.357 14.208 304.720 1.740 0.95 483554. 0.4226 59.43 0.2615 0.4467 0.0906 0.0530 23.597 123.938 66.509 17595.945 14.002 295.832 1.714 0.96 484262. 0.4102 65.37 0.2876 0.4841 0.0876 0.0520 23.156 121.625 64.305 17267.635 13.741 286.031 1.689 0.96 485014. 0.3974 71.32 0.3138 0.5203 0.0843 0.0508 22.621 118.814 61.892 16868.498 13.424 275.295 1.664 0.96 485813. 0.3841 77.26 0.3399 0.5552 0.0807 0.0494 21.990 115.500 59.265 16397.998 13.049 263.609 1.639 0.96 486657. 0.3702 83.20 0.3661 0.5887 0.0768 0.0478 21.262 111.677 56.419 15855.294 12.617 250.954 1.614 0.96 487547. 0.3557 89.14 0.3922 0.6206 0.0727 0.0459 20.438 107.346 53.359 15240.354 12.128 237.341 1.588 0.96 488482. 0.3403 95.09 0.4184 0.6507 0.0682 0.0439 19.523 102.542 50.105 14558.354 11.585 222.865 1.561 0.96 489463. 0.3242 101.03 0.4445 0.6788 0.0636 0.0416 18.526 97.306 46.680 13815.003 10.994 207.631 1.533 0.96 490488. 0.3072 106.97 0.4707 0.7033 0.0587 0.0393 17.481 91.819 43.103 13035.873 10.374 191.720 1.500 0.96 491557. 0.2889 112.92 0.4968 0.7229 0.0537 0.0369 16.407 86.175 39.392 12234.619 9.736 175.217 1.460 0.96 492669. 0.2689 118.86 0.5230 0.7361 0.0484 0.0344 15.314 80.434 35.568 11419.596 9.087 158.208 1.413 0.97 493826. 0.2472 124.80 0.5491 0.7343 0.0431 0.0322 14.338 75.308 31.635 10691.812 8.508 140.712 1.342 0.97 495025. 0.2214 130.75 0.5753 0.7164 0.0376 0.0302 13.440 70.594 27.619 10022.564 7.976 122.848 1.250 0.97 496268. 0.1927 136.69 0.6014 0.6850 0.0321 0.0282 12.535 65.837 23.558 9347.155 7.438 104.786 1.143 0.97 497554. 0.1628 142.63 0.6276 0.6371 0.0265 0.0261 11.630 61.087 19.481 8672.826 6.902 86.652 1.019 0.97 498884. 0.1319 148.57 0.6537 0.5687 0.0210 0.0241 10.741 56.418 15.420 8009.836 6.374 68.588 0.873 0.97 500256. 0.1006 154.52 0.6799 0.4759 0.0155 0.0222 9.880 51.896 11.411 7367.851 5.863 50.757 0.702 0.97 501673. 0.0696 160.46 0.7060 0.3540 0.0102 0.0204 9.057 47.573 7.494 6754.073 5.375 33.334 0.503 0.98 503135. 0.0404 166.40 0.7322 0.1985 0.0050 0.0186 8.277 43.474 3.702 6172.160 4.912 16.466 0.272 0.98 504647. 0.0154 172.35 0.7583 -0.0001 0.0000 0.0169 7.500 39.394 -0.002 5592.947 4.451 -0.008 0.000 0.98 506259. 0.0000