19x11 (19x11.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 0.0966 0.0400 0.008 0.502 0.401 5.942 0.057 1.785 30.625 0.08 39484. 0.5991 0.46 0.0255 0.0600 0.0953 0.0405 0.008 0.509 0.396 6.022 0.058 1.760 29.799 0.08 39511. 0.5789 0.92 0.0511 0.1167 0.0938 0.0410 0.008 0.515 0.390 6.099 0.058 1.733 28.974 0.08 39542. 0.5585 1.38 0.0766 0.1702 0.0922 0.0415 0.008 0.522 0.383 6.170 0.059 1.703 28.152 0.08 39575. 0.5380 1.84 0.1022 0.2203 0.0905 0.0420 0.008 0.527 0.376 6.234 0.060 1.671 27.337 0.08 39611. 0.5175 2.30 0.1277 0.2672 0.0886 0.0423 0.008 0.532 0.368 6.290 0.060 1.637 26.529 0.08 39650. 0.4970 2.76 0.1532 0.3110 0.0865 0.0426 0.008 0.536 0.359 6.336 0.061 1.599 25.731 0.08 39692. 0.4764 3.22 0.1788 0.3518 0.0843 0.0429 0.009 0.538 0.350 6.370 0.061 1.558 24.943 0.08 39737. 0.4559 3.68 0.2043 0.3895 0.0820 0.0430 0.009 0.540 0.340 6.389 0.061 1.514 24.165 0.08 39785. 0.4354 4.14 0.2299 0.4243 0.0794 0.0430 0.009 0.540 0.330 6.392 0.061 1.467 23.398 0.08 39837. 0.4149 4.60 0.2554 0.4561 0.0766 0.0429 0.009 0.539 0.318 6.377 0.061 1.416 22.641 0.08 39892. 0.3945 5.06 0.2810 0.4852 0.0737 0.0427 0.009 0.536 0.306 6.342 0.061 1.362 21.893 0.08 39951. 0.3741 5.51 0.3065 0.5114 0.0706 0.0423 0.008 0.531 0.293 6.284 0.060 1.304 21.152 0.08 40013. 0.3536 5.97 0.3320 0.5348 0.0672 0.0418 0.008 0.524 0.279 6.204 0.059 1.242 20.418 0.08 40079. 0.3332 6.43 0.3576 0.5553 0.0638 0.0411 0.008 0.516 0.265 6.101 0.058 1.178 19.686 0.08 40148. 0.3128 6.89 0.3831 0.5728 0.0601 0.0402 0.008 0.505 0.250 5.974 0.057 1.110 18.954 0.08 40220. 0.2925 7.35 0.4087 0.5872 0.0563 0.0392 0.008 0.492 0.234 5.825 0.056 1.041 18.217 0.08 40297. 0.2721 7.81 0.4342 0.5984 0.0524 0.0380 0.008 0.478 0.218 5.652 0.054 0.968 17.471 0.08 40377. 0.2518 8.27 0.4597 0.6059 0.0484 0.0367 0.007 0.461 0.201 5.457 0.052 0.894 16.709 0.08 40460. 0.2314 8.73 0.4853 0.6095 0.0443 0.0353 0.007 0.443 0.184 5.239 0.050 0.818 15.923 0.08 40547. 0.2109 9.19 0.5108 0.6086 0.0401 0.0336 0.007 0.422 0.166 4.998 0.048 0.740 15.104 0.08 40638. 0.1903 9.65 0.5364 0.6024 0.0358 0.0319 0.006 0.400 0.149 4.735 0.045 0.661 14.238 0.08 40733. 0.1695 10.11 0.5619 0.5898 0.0314 0.0299 0.006 0.376 0.131 4.449 0.042 0.581 13.307 0.08 40831. 0.1485 10.57 0.5875 0.5694 0.0270 0.0279 0.006 0.350 0.112 4.141 0.040 0.499 12.288 0.08 40933. 0.1271 11.03 0.6130 0.5388 0.0225 0.0256 0.005 0.322 0.094 3.810 0.036 0.416 11.144 0.08 41038. 0.1053 11.49 0.6385 0.4948 0.0180 0.0233 0.005 0.292 0.075 3.458 0.033 0.333 9.824 0.08 41148. 0.0830 11.95 0.6641 0.4319 0.0135 0.0208 0.004 0.261 0.056 3.085 0.029 0.249 8.246 0.08 41261. 0.0603 12.41 0.6896 0.3414 0.0090 0.0181 0.004 0.228 0.037 2.693 0.026 0.166 6.275 0.08 41377. 0.0374 12.87 0.7152 0.2071 0.0044 0.0154 0.003 0.193 0.018 2.282 0.022 0.082 3.671 0.08 41497. 0.0154 13.33 0.7407 -0.0032 -0.0001 0.0125 0.002 0.157 0.000 1.853 0.018 -0.001 -0.054 0.08 41618. 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 0.0971 0.0362 0.058 1.818 1.612 43.015 0.205 7.172 17.002 0.15 78966. 0.6667 0.93 0.0260 0.0675 0.0957 0.0368 0.059 1.848 1.590 43.717 0.209 7.072 16.497 0.15 79023. 0.6424 1.87 0.0519 0.1310 0.0942 0.0373 0.060 1.876 1.565 44.390 0.212 6.963 15.996 0.15 79084. 0.6181 2.80 0.0779 0.1904 0.0926 0.0379 0.060 1.903 1.539 45.022 0.215 6.844 15.501 0.15 79152. 0.5938 3.74 0.1038 0.2459 0.0909 0.0384 0.061 1.927 1.509 45.599 0.218 6.714 15.014 0.15 79225. 0.5697 4.67 0.1298 0.2975 0.0889 0.0388 0.062 1.949 1.478 46.106 0.220 6.573 14.536 0.15 79305. 0.5457 5.60 0.1557 0.3455 0.0869 0.0391 0.062 1.966 1.443 46.528 0.222 6.419 14.068 0.15 79391. 0.5219 6.54 0.1817 0.3900 0.0846 0.0394 0.063 1.980 1.406 46.849 0.224 6.253 13.609 0.15 79483. 0.4983 7.47 0.2076 0.4310 0.0822 0.0396 0.063 1.988 1.365 47.050 0.225 6.073 13.161 0.15 79583. 0.4749 8.40 0.2336 0.4688 0.0796 0.0396 0.063 1.991 1.322 47.114 0.225 5.879 12.724 0.15 79689. 0.4518 9.34 0.2595 0.5034 0.0767 0.0396 0.063 1.987 1.275 47.023 0.225 5.671 12.297 0.15 79802. 0.4288 10.27 0.2855 0.5350 0.0737 0.0393 0.063 1.976 1.225 46.760 0.223 5.448 11.880 0.15 79922. 0.4060 11.21 0.3114 0.5635 0.0705 0.0390 0.062 1.957 1.171 46.311 0.221 5.210 11.471 0.15 80050. 0.3834 12.14 0.3374 0.5892 0.0671 0.0384 0.061 1.930 1.115 45.666 0.218 4.958 11.071 0.15 80185. 0.3610 13.07 0.3633 0.6119 0.0635 0.0377 0.060 1.894 1.055 44.823 0.214 4.693 10.677 0.15 80327. 0.3387 14.01 0.3893 0.6317 0.0598 0.0368 0.059 1.850 0.993 43.780 0.209 4.417 10.288 0.15 80476. 0.3166 14.94 0.4152 0.6485 0.0559 0.0358 0.057 1.798 0.929 42.540 0.203 4.131 9.901 0.15 80633. 0.2947 15.87 0.4412 0.6622 0.0519 0.0346 0.055 1.737 0.862 41.101 0.196 3.835 9.515 0.15 80798. 0.2728 16.81 0.4671 0.6724 0.0478 0.0332 0.053 1.668 0.794 39.464 0.188 3.531 9.124 0.15 80970. 0.2511 17.74 0.4931 0.6788 0.0436 0.0317 0.050 1.590 0.724 37.628 0.180 3.220 8.727 0.15 81149. 0.2293 18.68 0.5190 0.6808 0.0393 0.0299 0.048 1.504 0.653 35.592 0.170 2.902 8.316 0.15 81336. 0.2074 19.61 0.5450 0.6778 0.0349 0.0281 0.045 1.410 0.580 33.358 0.159 2.579 7.884 0.15 81531. 0.1854 20.54 0.5709 0.6684 0.0305 0.0260 0.041 1.307 0.506 30.926 0.148 2.251 7.421 0.15 81733. 0.1630 21.48 0.5969 0.6509 0.0260 0.0238 0.038 1.196 0.431 28.298 0.135 1.918 6.912 0.15 81942. 0.1402 22.41 0.6228 0.6223 0.0214 0.0214 0.034 1.077 0.356 25.476 0.122 1.582 6.334 0.15 82160. 0.1167 23.35 0.6488 0.5781 0.0168 0.0189 0.030 0.949 0.280 22.466 0.107 1.244 5.649 0.15 82385. 0.0923 24.28 0.6747 0.5098 0.0123 0.0162 0.026 0.815 0.204 19.276 0.092 0.905 4.789 0.15 82617. 0.0667 25.21 0.7007 0.4012 0.0077 0.0134 0.021 0.673 0.127 15.916 0.076 0.567 3.630 0.15 82857. 0.0400 26.15 0.7266 0.2163 0.0031 0.0104 0.017 0.524 0.052 12.401 0.059 0.229 1.887 0.15 83103. 0.0132 27.08 0.7526 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 0.0975 0.0347 0.187 3.925 3.644 139.315 0.443 16.211 11.865 0.23 118446. 0.6995 1.39 0.0257 0.0701 0.0962 0.0353 0.190 3.994 3.595 141.746 0.451 15.990 11.503 0.23 118530. 0.6736 2.78 0.0515 0.1358 0.0947 0.0359 0.193 4.060 3.541 144.089 0.459 15.748 11.145 0.23 118622. 0.6476 4.17 0.0772 0.1972 0.0931 0.0365 0.196 4.122 3.481 146.296 0.466 15.484 10.793 0.23 118722. 0.6219 5.56 0.1030 0.2545 0.0914 0.0370 0.199 4.179 3.416 148.324 0.472 15.196 10.447 0.23 118831. 0.5963 6.95 0.1287 0.3079 0.0895 0.0374 0.201 4.230 3.346 150.122 0.478 14.882 10.109 0.23 118950. 0.5710 8.34 0.1544 0.3574 0.0875 0.0378 0.203 4.272 3.269 151.639 0.483 14.541 9.778 0.23 119077. 0.5460 9.73 0.1802 0.4032 0.0852 0.0381 0.205 4.306 3.186 152.818 0.486 14.171 9.456 0.23 119214. 0.5213 11.12 0.2059 0.4455 0.0828 0.0383 0.206 4.328 3.096 153.603 0.489 13.772 9.143 0.23 119362. 0.4968 12.50 0.2317 0.4845 0.0802 0.0384 0.206 4.337 3.000 153.934 0.490 13.342 8.838 0.23 119519. 0.4727 13.89 0.2574 0.5203 0.0775 0.0383 0.206 4.332 2.895 153.748 0.489 12.879 8.542 0.23 119687. 0.4489 15.28 0.2831 0.5530 0.0745 0.0381 0.205 4.310 2.784 152.989 0.487 12.383 8.254 0.23 119865. 0.4253 16.67 0.3089 0.5828 0.0713 0.0378 0.203 4.271 2.665 151.605 0.483 11.855 7.974 0.23 120054. 0.4020 18.06 0.3346 0.6097 0.0679 0.0373 0.201 4.214 2.539 149.565 0.476 11.294 7.700 0.23 120254. 0.3789 19.45 0.3604 0.6339 0.0644 0.0366 0.197 4.137 2.407 146.854 0.467 10.705 7.433 0.23 120464. 0.3561 20.84 0.3861 0.6552 0.0607 0.0358 0.192 4.042 2.268 143.469 0.457 10.090 7.172 0.23 120686. 0.3336 22.23 0.4118 0.6738 0.0568 0.0347 0.187 3.928 2.125 139.409 0.444 9.452 6.913 0.23 120918. 0.3112 23.62 0.4376 0.6894 0.0529 0.0336 0.181 3.794 1.977 134.675 0.429 8.793 6.657 0.23 121161. 0.2891 25.01 0.4633 0.7019 0.0488 0.0322 0.173 3.642 1.824 129.265 0.411 8.115 6.402 0.23 121416. 0.2670 26.40 0.4891 0.7110 0.0446 0.0307 0.165 3.470 1.668 123.177 0.392 7.421 6.143 0.23 121681. 0.2451 27.79 0.5148 0.7163 0.0404 0.0290 0.156 3.280 1.509 116.410 0.371 6.712 5.880 0.23 121957. 0.2231 29.18 0.5405 0.7171 0.0360 0.0272 0.146 3.070 1.347 108.964 0.347 5.990 5.606 0.23 122245. 0.2009 30.57 0.5663 0.7124 0.0316 0.0251 0.135 2.841 1.182 100.839 0.321 5.257 5.316 0.23 122544. 0.1785 31.96 0.5920 0.7007 0.0272 0.0229 0.123 2.593 1.015 92.042 0.293 4.515 5.002 0.23 122854. 0.1556 33.35 0.6178 0.6796 0.0226 0.0206 0.111 2.327 0.846 82.581 0.263 3.765 4.649 0.23 123175. 0.1321 34.73 0.6435 0.6447 0.0181 0.0181 0.097 2.042 0.677 72.473 0.231 3.009 4.234 0.23 123508. 0.1075 36.12 0.6692 0.5887 0.0135 0.0154 0.083 1.740 0.506 61.742 0.197 2.251 3.718 0.23 123851. 0.0817 37.51 0.6950 0.4965 0.0090 0.0126 0.068 1.421 0.336 50.424 0.161 1.493 3.019 0.23 124205. 0.0540 38.90 0.7207 0.3328 0.0044 0.0096 0.052 1.086 0.166 38.561 0.123 0.738 1.952 0.23 124570. 0.0245 40.29 0.7465 -0.0103 -0.0001 0.0065 0.035 0.736 -0.003 26.121 0.083 -0.015 -0.059 0.23 124928. 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 0.0980 0.0340 0.434 6.839 6.515 323.640 0.773 28.980 9.131 0.30 157922. 0.7198 1.86 0.0259 0.0722 0.0967 0.0347 0.442 6.964 6.427 329.589 0.787 28.588 8.845 0.30 158035. 0.6925 3.73 0.0518 0.1398 0.0953 0.0353 0.450 7.086 6.331 335.325 0.801 28.158 8.563 0.30 158158. 0.6654 5.59 0.0776 0.2030 0.0937 0.0358 0.457 7.200 6.225 340.737 0.813 27.688 8.286 0.30 158293. 0.6384 7.45 0.1035 0.2618 0.0919 0.0364 0.464 7.305 6.109 345.714 0.825 27.173 8.015 0.30 158440. 0.6118 9.31 0.1294 0.3164 0.0900 0.0368 0.470 7.399 5.983 350.135 0.836 26.612 7.750 0.30 158599. 0.5854 11.18 0.1553 0.3671 0.0880 0.0372 0.475 7.478 5.846 353.871 0.845 26.002 7.493 0.30 158770. 0.5595 13.04 0.1812 0.4140 0.0857 0.0375 0.478 7.539 5.697 356.788 0.852 25.340 7.242 0.30 158955. 0.5338 14.90 0.2071 0.4572 0.0833 0.0377 0.481 7.580 5.536 358.744 0.856 24.624 6.999 0.30 159153. 0.5086 16.76 0.2329 0.4971 0.0807 0.0378 0.482 7.598 5.362 359.590 0.858 23.850 6.763 0.30 159365. 0.4837 18.63 0.2588 0.5336 0.0779 0.0378 0.482 7.590 5.175 359.179 0.857 23.019 6.535 0.30 159591. 0.4591 20.49 0.2847 0.5671 0.0749 0.0376 0.479 7.551 4.974 357.369 0.853 22.126 6.314 0.30 159832. 0.4349 22.35 0.3106 0.5976 0.0716 0.0372 0.475 7.481 4.760 354.037 0.845 21.174 6.099 0.30 160086. 0.4109 24.22 0.3365 0.6253 0.0682 0.0367 0.468 7.377 4.534 349.104 0.833 20.165 5.890 0.30 160355. 0.3873 26.08 0.3623 0.6502 0.0646 0.0360 0.459 7.238 4.295 342.536 0.818 19.104 5.687 0.30 160639. 0.3640 27.94 0.3882 0.6723 0.0609 0.0352 0.448 7.064 4.046 334.324 0.798 17.996 5.489 0.30 160937. 0.3409 29.80 0.4141 0.6917 0.0570 0.0341 0.435 6.856 3.787 324.467 0.775 16.846 5.294 0.30 161250. 0.3182 31.67 0.4400 0.7083 0.0530 0.0329 0.420 6.613 3.520 312.962 0.747 15.658 5.102 0.30 161578. 0.2956 33.53 0.4659 0.7218 0.0488 0.0315 0.402 6.335 3.246 299.806 0.716 14.438 4.911 0.30 161920. 0.2732 35.39 0.4918 0.7321 0.0446 0.0300 0.382 6.022 2.965 284.994 0.680 13.187 4.718 0.31 162278. 0.2509 37.25 0.5176 0.7387 0.0403 0.0282 0.360 5.674 2.678 268.521 0.641 11.911 4.523 0.31 162650. 0.2286 39.12 0.5435 0.7411 0.0359 0.0263 0.336 5.291 2.386 250.386 0.598 10.611 4.321 0.31 163038. 0.2061 40.98 0.5694 0.7381 0.0314 0.0242 0.309 4.873 2.089 230.594 0.551 9.291 4.109 0.31 163441. 0.1834 42.84 0.5953 0.7284 0.0269 0.0220 0.280 4.420 1.788 209.157 0.499 7.954 3.878 0.31 163858. 0.1602 44.70 0.6212 0.7092 0.0223 0.0196 0.250 3.932 1.485 186.101 0.444 6.604 3.619 0.31 164291. 0.1362 46.57 0.6470 0.6763 0.0177 0.0170 0.217 3.412 1.179 161.468 0.385 5.245 3.313 0.31 164739. 0.1111 48.43 0.6729 0.6211 0.0131 0.0142 0.181 2.859 0.873 135.321 0.323 3.882 2.925 0.31 165201. 0.0844 50.29 0.6988 0.5257 0.0085 0.0113 0.144 2.277 0.566 107.750 0.257 2.520 2.385 0.31 165679. 0.0554 52.16 0.7247 0.3442 0.0039 0.0083 0.106 1.666 0.262 78.864 0.188 1.164 1.505 0.31 166169. 0.0238 54.02 0.7506 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 0.0987 0.0337 0.840 10.592 10.250 626.570 1.197 45.592 7.420 0.38 197392. 0.7336 2.32 0.0258 0.0731 0.0974 0.0344 0.856 10.792 10.114 638.436 1.219 44.989 7.186 0.38 197533. 0.7057 4.64 0.0516 0.1415 0.0960 0.0350 0.872 10.986 9.965 649.891 1.241 44.325 6.955 0.38 197687. 0.6780 6.96 0.0774 0.2054 0.0944 0.0356 0.886 11.169 9.801 660.714 1.262 43.596 6.728 0.38 197855. 0.6505 9.28 0.1032 0.2648 0.0927 0.0361 0.899 11.338 9.622 670.684 1.281 42.799 6.507 0.38 198038. 0.6234 11.60 0.1290 0.3200 0.0908 0.0366 0.911 11.488 9.426 679.564 1.298 41.929 6.292 0.38 198236. 0.5966 13.92 0.1548 0.3712 0.0887 0.0370 0.921 11.615 9.213 687.103 1.312 40.981 6.082 0.38 198450. 0.5701 16.24 0.1806 0.4186 0.0865 0.0373 0.929 11.715 8.982 693.035 1.324 39.952 5.878 0.38 198681. 0.5441 18.56 0.2064 0.4624 0.0841 0.0375 0.935 11.784 8.731 697.080 1.331 38.838 5.681 0.38 198928. 0.5184 20.89 0.2322 0.5027 0.0815 0.0376 0.937 11.815 8.461 698.951 1.335 37.634 5.490 0.38 199192. 0.4932 23.21 0.2580 0.5398 0.0787 0.0376 0.937 11.805 8.169 698.357 1.334 36.337 5.306 0.38 199473. 0.4683 25.53 0.2837 0.5738 0.0757 0.0374 0.932 11.749 7.856 695.016 1.327 34.946 5.127 0.38 199773. 0.4438 27.85 0.3095 0.6048 0.0725 0.0371 0.924 11.642 7.522 688.686 1.315 33.460 4.954 0.38 200089. 0.4196 30.17 0.3353 0.6331 0.0690 0.0366 0.911 11.482 7.168 679.203 1.297 31.883 4.787 0.38 200424. 0.3958 32.49 0.3611 0.6586 0.0654 0.0359 0.894 11.267 6.795 666.497 1.273 30.224 4.624 0.38 200777. 0.3722 34.81 0.3869 0.6815 0.0617 0.0350 0.872 10.997 6.405 650.545 1.242 28.490 4.466 0.38 201148. 0.3490 37.13 0.4127 0.7017 0.0578 0.0340 0.847 10.673 6.000 631.345 1.206 26.690 4.311 0.38 201538. 0.3261 39.45 0.4385 0.7192 0.0538 0.0328 0.817 10.293 5.582 608.892 1.163 24.831 4.158 0.38 201946. 0.3034 41.77 0.4643 0.7339 0.0496 0.0314 0.782 9.858 5.153 583.180 1.114 22.919 4.007 0.38 202372. 0.2809 44.09 0.4901 0.7455 0.0454 0.0298 0.743 9.368 4.712 554.197 1.058 20.960 3.857 0.38 202816. 0.2585 46.41 0.5159 0.7536 0.0411 0.0281 0.700 8.823 4.262 521.935 0.997 18.959 3.704 0.38 203280. 0.2362 48.73 0.5417 0.7579 0.0366 0.0262 0.652 8.222 3.804 486.391 0.929 16.921 3.547 0.38 203762. 0.2137 51.05 0.5675 0.7573 0.0322 0.0241 0.600 7.566 3.339 447.571 0.855 14.851 3.384 0.38 204262. 0.1909 53.37 0.5933 0.7505 0.0276 0.0218 0.544 6.855 2.867 405.498 0.774 12.754 3.207 0.38 204781. 0.1677 55.69 0.6191 0.7351 0.0230 0.0194 0.483 6.089 2.391 360.222 0.688 10.636 3.011 0.38 205319. 0.1438 58.01 0.6449 0.7072 0.0184 0.0168 0.418 5.271 1.911 311.820 0.596 8.502 2.780 0.38 205875. 0.1187 60.34 0.6707 0.6589 0.0138 0.0140 0.349 4.402 1.430 260.415 0.497 6.361 2.491 0.39 206450. 0.0920 62.66 0.6965 0.5734 0.0091 0.0111 0.276 3.485 0.949 206.176 0.394 4.221 2.087 0.39 207043. 0.0628 64.98 0.7223 0.4066 0.0045 0.0080 0.200 2.524 0.470 149.318 0.285 2.090 1.427 0.39 207653. 0.0302 67.30 0.7481 -0.0144 -0.0001 0.0048 0.120 1.512 -0.010 89.449 0.171 -0.043 -0.049 0.39 208236. 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 0.0995 0.0337 1.450 15.235 14.884 1081.477 1.721 66.202 6.242 0.45 236855. 0.7437 2.79 0.0258 0.0738 0.0983 0.0344 1.479 15.531 14.691 1102.527 1.755 65.344 6.044 0.45 237024. 0.7154 5.57 0.0516 0.1428 0.0968 0.0350 1.506 15.818 14.478 1122.861 1.787 64.397 5.848 0.45 237209. 0.6872 8.36 0.0774 0.2072 0.0953 0.0356 1.532 16.089 14.244 1142.085 1.818 63.356 5.657 0.45 237412. 0.6593 11.14 0.1032 0.2672 0.0936 0.0361 1.555 16.338 13.987 1159.808 1.846 62.215 5.470 0.45 237632. 0.6318 13.93 0.1290 0.3229 0.0917 0.0366 1.577 16.561 13.706 1175.611 1.871 60.966 5.288 0.45 237870. 0.6046 16.71 0.1548 0.3745 0.0896 0.0370 1.595 16.750 13.400 1189.048 1.892 59.603 5.111 0.45 238128. 0.5778 19.50 0.1806 0.4223 0.0874 0.0374 1.609 16.900 13.067 1199.651 1.909 58.120 4.940 0.45 238405. 0.5515 22.28 0.2064 0.4665 0.0850 0.0376 1.619 17.002 12.705 1206.929 1.921 56.512 4.775 0.45 238703. 0.5256 25.07 0.2322 0.5072 0.0824 0.0377 1.623 17.051 12.314 1210.379 1.926 54.772 4.614 0.45 239020. 0.5001 27.86 0.2580 0.5446 0.0795 0.0377 1.622 17.038 11.892 1209.484 1.925 52.897 4.460 0.45 239359. 0.4750 30.64 0.2838 0.5790 0.0765 0.0375 1.614 16.957 11.439 1203.758 1.916 50.882 4.310 0.45 239719. 0.4502 33.43 0.3096 0.6105 0.0733 0.0372 1.600 16.803 10.955 1192.767 1.898 48.728 4.166 0.45 240101. 0.4258 36.21 0.3354 0.6392 0.0698 0.0366 1.577 16.570 10.441 1176.222 1.872 46.441 4.026 0.45 240504. 0.4018 39.00 0.3612 0.6652 0.0662 0.0360 1.548 16.256 9.899 1153.995 1.837 44.032 3.891 0.46 240928. 0.3781 41.78 0.3871 0.6886 0.0624 0.0351 1.510 15.863 9.333 1126.048 1.792 41.513 3.759 0.46 241375. 0.3547 44.57 0.4129 0.7095 0.0585 0.0340 1.465 15.388 8.745 1092.378 1.739 38.897 3.631 0.46 241843. 0.3316 47.36 0.4387 0.7277 0.0544 0.0328 1.412 14.833 8.137 1052.979 1.676 36.194 3.505 0.46 242333. 0.3088 50.14 0.4645 0.7431 0.0502 0.0314 1.352 14.198 7.512 1007.840 1.604 33.413 3.381 0.46 242845. 0.2861 52.93 0.4903 0.7556 0.0460 0.0298 1.283 13.481 6.871 956.942 1.523 30.562 3.257 0.46 243380. 0.2636 55.71 0.5161 0.7649 0.0416 0.0281 1.207 12.682 6.216 900.271 1.433 27.650 3.132 0.46 243937. 0.2412 58.50 0.5419 0.7705 0.0371 0.0261 1.124 11.802 5.549 837.821 1.333 24.684 3.004 0.46 244516. 0.2186 61.28 0.5677 0.7714 0.0326 0.0240 1.032 10.841 4.872 769.604 1.225 21.670 2.871 0.46 245117. 0.1957 64.07 0.5935 0.7665 0.0280 0.0217 0.933 9.800 4.185 695.662 1.107 18.617 2.729 0.46 245741. 0.1724 66.85 0.6193 0.7535 0.0234 0.0192 0.826 8.679 3.492 616.078 0.981 15.532 2.571 0.46 246387. 0.1484 69.64 0.6451 0.7284 0.0187 0.0165 0.712 7.480 2.793 530.990 0.845 12.424 2.386 0.46 247055. 0.1231 72.43 0.6709 0.6837 0.0140 0.0137 0.591 6.207 2.092 440.613 0.701 9.304 2.153 0.46 247746. 0.0962 75.21 0.6967 0.6024 0.0093 0.0108 0.463 4.864 1.391 345.247 0.549 6.185 1.827 0.46 248458. 0.0665 78.00 0.7225 0.4379 0.0046 0.0076 0.329 3.455 0.692 245.272 0.390 3.080 1.281 0.46 249190. 0.0329 80.78 0.7483 -0.0080 0.0000 0.0044 0.188 1.971 -0.007 139.919 0.223 -0.031 -0.023 0.46 249885. 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 0.1005 0.0339 2.314 20.838 20.461 1725.747 2.354 91.011 5.378 0.53 276309. 0.7512 3.25 0.0258 0.0742 0.0993 0.0345 2.360 21.254 20.203 1760.216 2.401 89.862 5.206 0.53 276506. 0.7226 6.51 0.0517 0.1437 0.0979 0.0352 2.405 21.656 19.917 1793.529 2.447 88.591 5.037 0.53 276723. 0.6942 9.76 0.0775 0.2084 0.0963 0.0358 2.447 22.037 19.602 1825.036 2.490 87.188 4.872 0.53 276960. 0.6661 13.01 0.1033 0.2687 0.0946 0.0364 2.486 22.388 19.255 1854.102 2.529 85.645 4.710 0.53 277218. 0.6383 16.26 0.1291 0.3247 0.0927 0.0369 2.521 22.701 18.874 1880.030 2.565 83.951 4.553 0.53 277497. 0.6109 19.52 0.1550 0.3766 0.0907 0.0373 2.551 22.967 18.458 1902.094 2.595 82.099 4.401 0.53 277799. 0.5840 22.77 0.1808 0.4247 0.0885 0.0377 2.574 23.178 18.003 1919.532 2.619 80.080 4.254 0.53 278124. 0.5574 26.02 0.2066 0.4691 0.0860 0.0379 2.590 23.323 17.510 1931.551 2.635 77.884 4.112 0.53 278472. 0.5313 29.28 0.2324 0.5101 0.0834 0.0380 2.598 23.392 16.975 1937.325 2.643 75.505 3.974 0.53 278845. 0.5057 32.53 0.2583 0.5478 0.0806 0.0380 2.596 23.377 16.398 1936.029 2.641 72.936 3.842 0.53 279242. 0.4804 35.78 0.2841 0.5825 0.0775 0.0378 2.584 23.266 15.776 1926.865 2.629 70.173 3.714 0.53 279664. 0.4555 39.03 0.3099 0.6144 0.0743 0.0375 2.560 23.052 15.111 1909.140 2.604 67.215 3.590 0.53 280110. 0.4310 42.29 0.3358 0.6434 0.0708 0.0369 2.524 22.729 14.404 1882.377 2.568 64.070 3.471 0.53 280582. 0.4068 45.54 0.3616 0.6699 0.0671 0.0362 2.476 22.294 13.659 1846.364 2.519 60.755 3.355 0.53 281080. 0.3830 48.79 0.3874 0.6938 0.0633 0.0353 2.415 21.747 12.879 1801.054 2.457 57.286 3.243 0.53 281602. 0.3595 52.05 0.4132 0.7152 0.0593 0.0343 2.342 21.088 12.069 1746.439 2.382 53.681 3.134 0.53 282151. 0.3363 55.30 0.4391 0.7340 0.0552 0.0330 2.256 20.316 11.231 1682.521 2.295 49.954 3.028 0.53 282725. 0.3133 58.55 0.4649 0.7501 0.0509 0.0316 2.158 19.432 10.368 1609.284 2.195 46.119 2.922 0.53 283324. 0.2906 61.80 0.4907 0.7634 0.0466 0.0300 2.047 18.434 9.484 1526.703 2.083 42.186 2.818 0.53 283950. 0.2680 65.06 0.5165 0.7737 0.0422 0.0282 1.924 17.324 8.581 1434.756 1.957 38.167 2.713 0.53 284601. 0.2454 68.31 0.5424 0.7803 0.0376 0.0262 1.788 16.101 7.660 1333.435 1.819 34.071 2.606 0.54 285278. 0.2227 71.56 0.5682 0.7825 0.0330 0.0240 1.640 14.764 6.724 1222.761 1.668 29.910 2.494 0.54 285982. 0.1997 74.82 0.5940 0.7792 0.0284 0.0216 1.479 13.316 5.776 1102.802 1.504 25.692 2.376 0.54 286711. 0.1763 78.07 0.6198 0.7681 0.0237 0.0191 1.306 11.757 4.818 973.692 1.328 21.429 2.244 0.54 287467. 0.1521 81.32 0.6457 0.7454 0.0189 0.0164 1.121 10.090 3.852 835.659 1.140 17.134 2.091 0.54 288248. 0.1267 84.57 0.6715 0.7035 0.0142 0.0135 0.924 8.320 2.883 689.050 0.940 12.822 1.898 0.54 289056. 0.0995 87.83 0.6973 0.6253 0.0094 0.0105 0.717 6.452 1.913 534.357 0.729 8.510 1.624 0.54 289888. 0.0694 91.08 0.7232 0.4612 0.0047 0.0073 0.499 4.494 0.948 372.202 0.508 4.216 1.155 0.54 290744. 0.0347 94.33 0.7490 -0.0209 -0.0001 0.0039 0.269 2.424 -0.022 200.763 0.274 -0.100 -0.051 0.54 291535. 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 0.1017 0.0342 3.490 27.495 27.040 2602.397 3.106 120.273 4.713 0.60 315750. 0.7568 3.75 0.0260 0.0749 0.1005 0.0349 3.562 28.063 26.708 2656.138 3.171 118.798 4.561 0.60 315978. 0.7279 7.49 0.0521 0.1449 0.0991 0.0356 3.632 28.612 26.339 2708.083 3.233 117.157 4.412 0.60 316228. 0.6992 11.24 0.0781 0.2102 0.0976 0.0362 3.697 29.131 25.930 2757.216 3.291 115.337 4.266 0.60 316502. 0.6708 14.99 0.1041 0.2709 0.0959 0.0368 3.758 29.609 25.478 2802.500 3.345 113.325 4.123 0.60 316801. 0.6428 18.73 0.1301 0.3273 0.0940 0.0374 3.812 30.035 24.979 2842.839 3.393 111.108 3.985 0.60 317124. 0.6151 22.48 0.1562 0.3796 0.0919 0.0378 3.858 30.397 24.432 2877.085 3.434 108.672 3.852 0.60 317474. 0.5879 26.23 0.1822 0.4280 0.0897 0.0382 3.894 30.682 23.832 2904.033 3.466 106.007 3.722 0.60 317851. 0.5612 29.97 0.2082 0.4727 0.0872 0.0384 3.919 30.876 23.179 2922.437 3.488 103.100 3.597 0.60 318256. 0.5349 33.72 0.2343 0.5140 0.0845 0.0385 3.931 30.967 22.469 2931.015 3.499 99.941 3.477 0.60 318689. 0.5090 37.47 0.2603 0.5520 0.0816 0.0385 3.927 30.940 21.700 2928.477 3.496 96.522 3.361 0.60 319150. 0.4835 41.21 0.2863 0.5871 0.0785 0.0383 3.907 30.783 20.872 2913.596 3.478 92.837 3.249 0.61 319640. 0.4584 44.96 0.3124 0.6192 0.0752 0.0379 3.869 30.484 19.983 2885.299 3.444 88.886 3.141 0.61 320159. 0.4337 48.71 0.3384 0.6486 0.0716 0.0374 3.812 30.036 19.038 2842.880 3.393 84.681 3.037 0.61 320707. 0.4093 52.45 0.3644 0.6754 0.0679 0.0366 3.736 29.435 18.040 2786.043 3.326 80.244 2.937 0.61 321284. 0.3852 56.20 0.3904 0.6996 0.0639 0.0357 3.641 28.682 16.996 2714.731 3.240 75.598 2.840 0.61 321891. 0.3615 59.95 0.4165 0.7214 0.0599 0.0346 3.525 27.776 15.910 2628.958 3.138 70.768 2.745 0.61 322528. 0.3381 63.69 0.4425 0.7406 0.0556 0.0332 3.391 26.717 14.787 2528.735 3.018 65.773 2.652 0.61 323194. 0.3150 67.44 0.4685 0.7572 0.0513 0.0317 3.237 25.505 13.631 2414.054 2.882 60.631 2.561 0.61 323890. 0.2920 71.19 0.4946 0.7710 0.0468 0.0300 3.064 24.140 12.445 2284.877 2.727 55.358 2.471 0.61 324616. 0.2692 74.93 0.5206 0.7817 0.0423 0.0281 2.871 22.622 11.234 2141.183 2.556 49.967 2.380 0.61 325372. 0.2463 78.68 0.5466 0.7889 0.0376 0.0261 2.659 20.951 9.999 1982.962 2.367 44.474 2.287 0.61 326158. 0.2233 82.43 0.5726 0.7916 0.0329 0.0238 2.428 19.126 8.744 1810.261 2.161 38.891 2.191 0.61 326974. 0.2001 86.17 0.5987 0.7887 0.0281 0.0213 2.177 17.150 7.471 1623.200 1.938 33.233 2.088 0.61 327821. 0.1762 89.92 0.6247 0.7778 0.0233 0.0187 1.907 15.024 6.186 1422.008 1.697 27.515 1.973 0.61 328697. 0.1516 93.67 0.6507 0.7547 0.0184 0.0159 1.619 12.753 4.891 1207.067 1.441 21.755 1.838 0.62 329603. 0.1255 97.41 0.6768 0.7106 0.0135 0.0129 1.313 10.343 3.591 978.962 1.169 15.974 1.664 0.62 330540. 0.0974 101.16 0.7028 0.6243 0.0086 0.0097 0.990 7.803 2.292 738.510 0.882 10.195 1.408 0.62 331505. 0.0658 104.91 0.7288 0.4283 0.0038 0.0064 0.653 5.142 0.999 486.686 0.581 4.445 0.931 0.62 332495. 0.0288 108.65 0.7549 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 0.1031 0.0348 5.057 35.412 34.691 3770.723 4.001 154.304 4.173 0.68 355177. 0.7590 4.21 0.0260 0.0745 0.1019 0.0355 5.161 36.145 34.288 3848.719 4.084 152.512 4.041 0.68 355432. 0.7307 8.41 0.0520 0.1442 0.1006 0.0362 5.263 36.855 33.836 3924.338 4.164 150.504 3.911 0.68 355714. 0.7025 12.62 0.0779 0.2093 0.0991 0.0369 5.359 37.529 33.333 3996.081 4.240 148.263 3.783 0.68 356022. 0.6746 16.83 0.1039 0.2699 0.0974 0.0375 5.448 38.152 32.772 4062.455 4.310 145.772 3.659 0.68 356357. 0.6469 21.03 0.1299 0.3262 0.0956 0.0381 5.527 38.709 32.152 4121.809 4.373 143.012 3.538 0.68 356722. 0.6196 25.24 0.1559 0.3785 0.0935 0.0385 5.595 39.185 31.467 4172.438 4.427 139.966 3.421 0.68 357116. 0.5926 29.45 0.1818 0.4269 0.0913 0.0389 5.649 39.562 30.715 4212.542 4.470 136.618 3.307 0.68 357541. 0.5660 33.65 0.2078 0.4717 0.0889 0.0391 5.686 39.822 29.891 4240.235 4.499 132.954 3.197 0.68 357996. 0.5398 37.86 0.2338 0.5131 0.0862 0.0393 5.704 39.947 28.993 4253.604 4.513 128.960 3.092 0.68 358484. 0.5141 42.06 0.2598 0.5513 0.0833 0.0392 5.700 39.920 28.018 4250.737 4.510 124.625 2.990 0.68 359003. 0.4887 46.27 0.2857 0.5865 0.0802 0.0390 5.672 39.724 26.965 4229.813 4.488 119.940 2.892 0.68 359555. 0.4637 50.48 0.3117 0.6189 0.0768 0.0387 5.618 39.343 25.833 4189.268 4.445 114.907 2.797 0.68 360139. 0.4390 54.68 0.3377 0.6487 0.0732 0.0381 5.536 38.768 24.627 4128.044 4.380 109.540 2.706 0.68 360756. 0.4147 58.89 0.3637 0.6759 0.0694 0.0374 5.425 37.995 23.351 4045.702 4.293 103.866 2.618 0.68 361406. 0.3907 63.10 0.3896 0.7006 0.0654 0.0364 5.287 37.023 22.014 3942.183 4.183 97.917 2.533 0.68 362089. 0.3670 67.30 0.4156 0.7229 0.0613 0.0352 5.119 35.852 20.621 3817.536 4.051 91.724 2.450 0.68 362804. 0.3436 71.51 0.4416 0.7428 0.0570 0.0339 4.924 34.483 19.180 3671.816 3.896 85.314 2.369 0.68 363553. 0.3204 75.72 0.4676 0.7601 0.0526 0.0324 4.700 32.917 17.696 3505.029 3.719 78.710 2.290 0.69 364336. 0.2975 79.92 0.4936 0.7748 0.0481 0.0306 4.448 31.153 16.172 3317.150 3.520 71.932 2.211 0.69 365151. 0.2746 84.13 0.5195 0.7865 0.0434 0.0287 4.168 29.190 14.613 3108.147 3.298 65.000 2.133 0.69 366000. 0.2518 88.34 0.5455 0.7949 0.0387 0.0266 3.859 27.029 13.024 2878.015 3.054 57.930 2.053 0.69 366883. 0.2288 92.54 0.5715 0.7991 0.0339 0.0243 3.523 24.670 11.408 2626.826 2.787 50.741 1.970 0.69 367799. 0.2055 96.75 0.5975 0.7981 0.0290 0.0217 3.158 22.114 9.768 2354.746 2.498 43.450 1.882 0.69 368749. 0.1816 100.95 0.6234 0.7896 0.0241 0.0190 2.765 19.366 8.111 2062.095 2.188 36.077 1.784 0.69 369732. 0.1569 105.16 0.6494 0.7698 0.0191 0.0162 2.346 16.430 6.440 1749.426 1.856 28.646 1.670 0.69 370749. 0.1309 109.37 0.6754 0.7305 0.0142 0.0131 1.901 13.313 4.762 1417.599 1.504 21.181 1.524 0.69 371799. 0.1027 113.57 0.7014 0.6521 0.0092 0.0099 1.432 10.029 3.083 1067.859 1.133 13.714 1.310 0.69 372882. 0.0710 117.78 0.7273 0.4711 0.0042 0.0065 0.941 6.591 1.412 701.784 0.745 6.279 0.912 0.70 373992. 0.0335 121.99 0.7533 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 0.1047 0.0365 7.279 45.875 43.486 5427.605 5.183 193.425 3.634 0.75 394584. 0.7401 4.65 0.0258 0.0720 0.1036 0.0372 7.411 46.713 43.021 5526.649 5.278 191.356 3.531 0.75 394866. 0.7152 9.30 0.0517 0.1398 0.1023 0.0378 7.539 47.517 42.494 5621.863 5.368 189.015 3.428 0.75 395177. 0.6902 13.95 0.0775 0.2035 0.1009 0.0384 7.659 48.274 41.902 5711.355 5.454 186.378 3.328 0.75 395518. 0.6652 18.60 0.1034 0.2633 0.0993 0.0390 7.769 48.966 41.237 5793.232 5.532 183.422 3.229 0.75 395889. 0.6403 23.25 0.1292 0.3192 0.0975 0.0395 7.866 49.577 40.495 5865.493 5.601 180.122 3.131 0.75 396293. 0.6154 27.90 0.1551 0.3714 0.0955 0.0399 7.947 50.088 39.671 5926.028 5.659 176.456 3.036 0.75 396729. 0.5906 32.55 0.1809 0.4201 0.0933 0.0402 8.009 50.482 38.760 5972.584 5.703 172.402 2.943 0.75 397200. 0.5659 37.21 0.2068 0.4653 0.0909 0.0404 8.050 50.737 37.757 6002.810 5.732 167.942 2.853 0.76 397705. 0.5414 41.86 0.2326 0.5073 0.0883 0.0405 8.065 50.834 36.658 6014.210 5.743 163.057 2.765 0.76 398245. 0.5169 46.51 0.2585 0.5462 0.0854 0.0404 8.052 50.749 35.461 6004.230 5.734 157.732 2.679 0.76 398821. 0.4926 51.16 0.2843 0.5821 0.0823 0.0402 8.006 50.463 34.163 5970.375 5.701 151.957 2.595 0.76 399432. 0.4685 55.81 0.3102 0.6152 0.0789 0.0398 7.926 49.956 32.764 5910.388 5.644 145.733 2.514 0.76 400079. 0.4445 60.46 0.3360 0.6456 0.0753 0.0392 7.808 49.214 31.267 5822.594 5.560 139.076 2.436 0.76 400762. 0.4206 65.11 0.3619 0.6734 0.0715 0.0384 7.652 48.230 29.681 5706.129 5.449 132.020 2.359 0.76 401482. 0.3969 69.76 0.3877 0.6988 0.0675 0.0374 7.457 47.000 28.014 5560.688 5.310 124.606 2.285 0.76 402237. 0.3735 74.41 0.4136 0.7218 0.0633 0.0362 7.223 45.525 26.276 5386.148 5.143 116.873 2.213 0.76 403029. 0.3503 79.06 0.4394 0.7424 0.0589 0.0349 6.950 43.803 24.473 5182.398 4.949 108.858 2.142 0.76 403857. 0.3272 83.71 0.4653 0.7606 0.0545 0.0333 6.637 41.833 22.615 4949.312 4.726 100.590 2.072 0.76 404721. 0.3044 88.36 0.4911 0.7762 0.0499 0.0315 6.285 39.614 20.705 4686.785 4.476 92.097 2.004 0.76 405622. 0.2816 93.01 0.5170 0.7891 0.0451 0.0296 5.893 37.146 18.750 4394.776 4.197 83.401 1.935 0.76 406560. 0.2588 97.66 0.5428 0.7988 0.0403 0.0274 5.462 34.429 16.755 4073.354 3.890 74.525 1.866 0.76 407534. 0.2358 102.31 0.5687 0.8046 0.0355 0.0251 4.992 31.465 14.723 3722.710 3.555 65.490 1.794 0.77 408545. 0.2126 106.97 0.5945 0.8055 0.0305 0.0225 4.483 28.258 12.661 3343.285 3.193 56.318 1.718 0.77 409593. 0.1888 111.62 0.6204 0.7994 0.0255 0.0198 3.937 24.815 10.574 2935.853 2.804 47.034 1.634 0.77 410677. 0.1641 116.27 0.6462 0.7825 0.0204 0.0168 3.355 21.144 8.468 2501.637 2.389 37.664 1.535 0.77 411798. 0.1380 120.92 0.6720 0.7474 0.0153 0.0137 2.739 17.263 6.349 2042.439 1.950 28.241 1.410 0.77 412956. 0.1097 125.57 0.6979 0.6762 0.0102 0.0105 2.093 13.192 4.227 1560.736 1.490 18.800 1.228 0.77 414149. 0.0780 130.22 0.7237 0.5155 0.0051 0.0071 1.421 8.957 2.110 1059.673 1.012 9.384 0.903 0.77 415374. 0.0405 134.87 0.7496 -0.0135 -0.0001 0.0036 0.715 4.508 -0.027 533.366 0.509 -0.120 -0.023 0.77 416481. 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 0.1064 0.0413 10.949 62.738 53.463 8164.961 7.088 237.804 2.970 0.83 433970. 0.6706 5.12 0.0259 0.0652 0.1054 0.0418 11.097 63.582 52.953 8274.705 7.183 235.536 2.903 0.83 434279. 0.6523 10.24 0.0517 0.1273 0.1042 0.0423 11.231 64.353 52.368 8375.107 7.271 232.933 2.836 0.83 434619. 0.6338 15.36 0.0776 0.1866 0.1029 0.0428 11.350 65.032 51.700 8463.444 7.347 229.961 2.771 0.83 434994. 0.6152 20.48 0.1035 0.2430 0.1014 0.0432 11.449 65.599 50.940 8537.268 7.411 226.583 2.706 0.83 435403. 0.5965 25.60 0.1294 0.2966 0.0997 0.0435 11.525 66.037 50.082 8594.252 7.461 222.764 2.643 0.83 435848. 0.5777 30.72 0.1552 0.3476 0.0977 0.0436 11.576 66.328 49.117 8632.179 7.494 218.474 2.581 0.83 436331. 0.5586 35.84 0.1811 0.3959 0.0956 0.0437 11.598 66.457 48.040 8648.890 7.508 213.683 2.519 0.83 436851. 0.5393 40.96 0.2070 0.4415 0.0932 0.0437 11.589 66.405 46.845 8642.173 7.502 208.367 2.459 0.83 437411. 0.5197 46.08 0.2328 0.4845 0.0906 0.0435 11.546 66.155 45.526 8609.667 7.474 202.501 2.398 0.83 438009. 0.4998 51.20 0.2587 0.5250 0.0877 0.0432 11.464 65.688 44.080 8548.862 7.421 196.067 2.339 0.83 438647. 0.4795 56.32 0.2846 0.5628 0.0846 0.0428 11.341 64.983 42.502 8457.101 7.342 189.051 2.279 0.83 439325. 0.4589 61.44 0.3104 0.5982 0.0812 0.0421 11.173 64.022 40.794 8331.979 7.233 181.451 2.221 0.83 440042. 0.4380 66.56 0.3363 0.6310 0.0775 0.0413 10.959 62.791 38.958 8171.763 7.094 173.286 2.162 0.83 440799. 0.4168 71.68 0.3622 0.6613 0.0736 0.0403 10.696 61.285 37.006 7975.785 6.924 164.601 2.104 0.83 441596. 0.3954 76.80 0.3881 0.6892 0.0695 0.0392 10.385 59.504 34.948 7744.029 6.723 155.448 2.047 0.84 442433. 0.3737 81.92 0.4139 0.7146 0.0653 0.0378 10.026 57.449 32.797 7476.540 6.491 145.879 1.990 0.84 443310. 0.3519 87.04 0.4398 0.7374 0.0608 0.0363 9.619 55.118 30.562 7173.181 6.227 135.941 1.932 0.84 444226. 0.3299 92.16 0.4657 0.7577 0.0562 0.0346 9.164 52.509 28.254 6833.616 5.932 125.674 1.875 0.84 445183. 0.3078 97.28 0.4915 0.7751 0.0515 0.0327 8.661 49.628 25.880 6458.775 5.607 115.112 1.817 0.84 446179. 0.2855 102.40 0.5174 0.7893 0.0467 0.0306 8.112 46.478 23.446 6048.801 5.251 104.286 1.758 0.84 447216. 0.2629 107.52 0.5433 0.7997 0.0417 0.0283 7.514 43.054 20.958 5603.119 4.864 93.223 1.697 0.84 448292. 0.2399 112.64 0.5692 0.8050 0.0367 0.0259 6.874 39.389 18.424 5126.237 4.450 81.949 1.630 0.84 449409. 0.2161 117.76 0.5950 0.8042 0.0315 0.0233 6.188 35.457 15.848 4614.502 4.006 70.492 1.558 0.84 450566. 0.1915 122.89 0.6209 0.7946 0.0263 0.0206 5.459 31.278 13.238 4070.673 3.534 58.882 1.475 0.85 451763. 0.1657 128.01 0.6468 0.7713 0.0211 0.0177 4.691 26.879 10.601 3498.068 3.037 47.152 1.375 0.85 453000. 0.1382 133.13 0.6726 0.7250 0.0158 0.0147 3.890 22.291 7.946 2900.978 2.518 35.342 1.242 0.85 454277. 0.1081 138.25 0.6985 0.6356 0.0105 0.0116 3.064 17.556 5.283 2284.726 1.983 23.499 1.049 0.85 455592. 0.0744 143.37 0.7244 0.4520 0.0052 0.0084 2.220 12.720 2.625 1655.408 1.437 11.676 0.719 0.85 456943. 0.0360 148.49 0.7502 -0.0161 -0.0001 0.0051 1.349 7.728 -0.055 1005.749 0.873 -0.244 -0.025 0.85 458186. 0.0000