20.5x14E (205x14E.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 0.0951 0.0387 0.011 0.710 0.535 8.400 0.080 2.381 28.901 0.08 37544. 0.6052 0.56 0.0287 0.0687 0.0941 0.0394 0.011 0.723 0.530 8.556 0.082 2.356 28.078 0.08 37572. 0.5849 1.12 0.0575 0.1333 0.0930 0.0401 0.012 0.736 0.523 8.711 0.083 2.328 27.252 0.08 37603. 0.5643 1.67 0.0862 0.1939 0.0918 0.0408 0.012 0.749 0.516 8.863 0.085 2.297 26.428 0.08 37637. 0.5436 2.23 0.1149 0.2505 0.0904 0.0415 0.012 0.761 0.509 9.008 0.086 2.262 25.610 0.08 37675. 0.5228 2.79 0.1437 0.3033 0.0888 0.0421 0.012 0.773 0.500 9.144 0.087 2.224 24.802 0.08 37717. 0.5020 3.35 0.1724 0.3523 0.0871 0.0427 0.012 0.783 0.490 9.267 0.088 2.182 24.006 0.08 37762. 0.4812 3.90 0.2012 0.3976 0.0853 0.0431 0.013 0.792 0.480 9.373 0.090 2.135 23.225 0.08 37812. 0.4606 4.46 0.2299 0.4395 0.0832 0.0435 0.013 0.799 0.468 9.458 0.090 2.083 22.461 0.08 37865. 0.4400 5.02 0.2586 0.4780 0.0810 0.0438 0.013 0.805 0.456 9.518 0.091 2.027 21.715 0.08 37923. 0.4196 5.58 0.2874 0.5133 0.0785 0.0440 0.013 0.807 0.442 9.549 0.091 1.965 20.988 0.08 37984. 0.3993 6.14 0.3161 0.5455 0.0758 0.0439 0.013 0.807 0.427 9.546 0.091 1.898 20.278 0.08 38051. 0.3792 6.69 0.3448 0.5748 0.0729 0.0438 0.013 0.803 0.410 9.506 0.091 1.826 19.585 0.08 38121. 0.3592 7.25 0.3736 0.6011 0.0698 0.0434 0.013 0.797 0.393 9.425 0.090 1.748 18.908 0.08 38196. 0.3392 7.81 0.4023 0.6246 0.0665 0.0428 0.012 0.786 0.374 9.299 0.089 1.664 18.243 0.08 38275. 0.3193 8.37 0.4310 0.6452 0.0629 0.0420 0.012 0.771 0.354 9.125 0.087 1.574 17.587 0.08 38359. 0.2994 8.93 0.4598 0.6627 0.0590 0.0410 0.012 0.752 0.332 8.900 0.085 1.478 16.936 0.08 38448. 0.2794 9.48 0.4885 0.6770 0.0550 0.0397 0.012 0.729 0.310 8.624 0.082 1.377 16.283 0.08 38541. 0.2593 10.04 0.5172 0.6877 0.0508 0.0382 0.011 0.702 0.286 8.300 0.079 1.272 15.622 0.08 38638. 0.2391 10.60 0.5460 0.6944 0.0464 0.0365 0.011 0.670 0.261 7.931 0.076 1.162 14.944 0.08 38740. 0.2186 11.16 0.5747 0.6964 0.0419 0.0346 0.010 0.635 0.236 7.518 0.072 1.050 14.237 0.08 38846. 0.1980 11.71 0.6035 0.6927 0.0373 0.0325 0.009 0.597 0.210 7.065 0.067 0.935 13.489 0.08 38956. 0.1770 12.27 0.6322 0.6822 0.0327 0.0303 0.009 0.556 0.184 6.573 0.063 0.817 12.680 0.08 39071. 0.1556 12.83 0.6609 0.6630 0.0279 0.0278 0.008 0.511 0.157 6.046 0.058 0.699 11.786 0.08 39190. 0.1337 13.39 0.6897 0.6322 0.0232 0.0253 0.007 0.464 0.130 5.487 0.052 0.580 10.772 0.08 39314. 0.1113 13.95 0.7184 0.5858 0.0184 0.0225 0.007 0.414 0.103 4.898 0.047 0.460 9.581 0.08 39442. 0.0882 14.50 0.7471 0.5168 0.0136 0.0197 0.006 0.362 0.077 4.283 0.041 0.341 8.128 0.08 39574. 0.0645 15.06 0.7759 0.4136 0.0089 0.0168 0.005 0.308 0.050 3.648 0.035 0.224 6.263 0.08 39710. 0.0402 15.62 0.8046 0.2538 0.0043 0.0138 0.004 0.253 0.024 2.996 0.029 0.109 3.706 0.08 39851. 0.0166 16.18 0.8333 -0.0099 -0.0001 0.0107 0.003 0.197 -0.001 2.334 0.022 -0.003 -0.139 0.08 39996. 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 0.0954 0.0361 0.084 2.651 2.149 62.732 0.300 9.557 15.536 0.16 75086. 0.6518 1.12 0.0288 0.0739 0.0945 0.0368 0.086 2.707 2.126 64.043 0.306 9.459 15.060 0.16 75142. 0.6286 2.24 0.0577 0.1432 0.0934 0.0376 0.088 2.762 2.102 65.355 0.312 9.348 14.586 0.16 75205. 0.6052 3.36 0.0865 0.2078 0.0921 0.0383 0.089 2.816 2.074 66.645 0.318 9.225 14.115 0.16 75274. 0.5818 4.48 0.1153 0.2679 0.0907 0.0391 0.091 2.869 2.043 67.889 0.324 9.087 13.649 0.16 75351. 0.5584 5.60 0.1442 0.3237 0.0892 0.0397 0.093 2.919 2.009 69.059 0.330 8.934 13.192 0.16 75434. 0.5352 6.72 0.1730 0.3753 0.0875 0.0403 0.094 2.964 1.971 70.126 0.335 8.765 12.745 0.16 75525. 0.5121 7.84 0.2018 0.4228 0.0857 0.0409 0.095 3.003 1.928 71.059 0.339 8.578 12.309 0.16 75625. 0.4893 8.95 0.2306 0.4666 0.0836 0.0413 0.096 3.035 1.882 71.823 0.343 8.371 11.885 0.16 75732. 0.4667 10.07 0.2595 0.5067 0.0813 0.0416 0.097 3.059 1.831 72.385 0.346 8.145 11.474 0.16 75848. 0.4444 11.19 0.2883 0.5435 0.0789 0.0418 0.098 3.073 1.775 72.709 0.347 7.897 11.076 0.16 75972. 0.4224 12.31 0.3171 0.5771 0.0762 0.0419 0.098 3.075 1.715 72.761 0.347 7.628 10.690 0.16 76105. 0.4007 13.43 0.3460 0.6076 0.0733 0.0417 0.097 3.064 1.649 72.507 0.346 7.336 10.317 0.16 76247. 0.3793 14.55 0.3748 0.6351 0.0701 0.0414 0.096 3.039 1.579 71.915 0.343 7.021 9.956 0.16 76398. 0.3580 15.67 0.4036 0.6599 0.0667 0.0408 0.095 2.999 1.502 70.953 0.339 6.683 9.605 0.16 76558. 0.3370 16.79 0.4325 0.6818 0.0631 0.0400 0.093 2.941 1.421 69.591 0.332 6.321 9.262 0.16 76727. 0.3160 17.91 0.4613 0.7008 0.0593 0.0390 0.091 2.866 1.334 67.805 0.324 5.935 8.926 0.16 76905. 0.2951 19.03 0.4901 0.7170 0.0552 0.0377 0.088 2.772 1.243 65.595 0.313 5.528 8.594 0.16 77091. 0.2742 20.15 0.5189 0.7299 0.0510 0.0362 0.084 2.662 1.147 62.979 0.301 5.103 8.263 0.16 77287. 0.2533 21.27 0.5478 0.7392 0.0466 0.0345 0.080 2.535 1.048 59.977 0.286 4.663 7.928 0.17 77492. 0.2323 22.39 0.5766 0.7443 0.0420 0.0326 0.076 2.392 0.946 56.608 0.270 4.210 7.584 0.17 77705. 0.2112 23.51 0.6054 0.7445 0.0374 0.0304 0.071 2.235 0.842 52.891 0.253 3.747 7.224 0.17 77928. 0.1898 24.63 0.6343 0.7385 0.0327 0.0281 0.066 2.064 0.737 48.845 0.233 3.277 6.840 0.17 78159. 0.1680 25.75 0.6631 0.7246 0.0280 0.0256 0.060 1.880 0.630 44.492 0.212 2.801 6.420 0.17 78399. 0.1458 26.86 0.6919 0.7000 0.0232 0.0229 0.053 1.684 0.522 39.855 0.190 2.323 5.944 0.17 78647. 0.1229 27.98 0.7208 0.6602 0.0184 0.0201 0.047 1.478 0.415 34.964 0.167 1.845 5.381 0.17 78905. 0.0992 29.10 0.7496 0.5973 0.0137 0.0172 0.040 1.261 0.308 29.849 0.143 1.370 4.681 0.17 79171. 0.0744 30.22 0.7784 0.4962 0.0090 0.0141 0.033 1.038 0.203 24.552 0.117 0.902 3.745 0.17 79445. 0.0483 31.34 0.8073 0.3246 0.0044 0.0110 0.026 0.808 0.100 19.115 0.091 0.443 2.363 0.17 79729. 0.0213 32.46 0.8361 -0.0032 0.0000 0.0078 0.018 0.574 -0.001 13.587 0.065 -0.003 -0.023 0.17 80019. 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 0.0958 0.0351 0.276 5.797 4.853 205.764 0.655 21.587 10.698 0.24 112626. 0.6745 1.68 0.0289 0.0763 0.0948 0.0359 0.282 5.925 4.804 210.309 0.669 21.367 10.360 0.24 112711. 0.6499 3.36 0.0577 0.1477 0.0937 0.0366 0.288 6.054 4.748 214.865 0.684 21.121 10.024 0.24 112805. 0.6252 5.04 0.0866 0.2142 0.0925 0.0374 0.294 6.180 4.687 219.354 0.698 20.846 9.691 0.24 112909. 0.6005 6.72 0.1154 0.2760 0.0912 0.0381 0.300 6.302 4.617 223.693 0.712 20.539 9.363 0.24 113024. 0.5759 8.40 0.1443 0.3331 0.0896 0.0388 0.305 6.418 4.541 227.789 0.725 20.197 9.041 0.24 113150. 0.5514 10.08 0.1732 0.3858 0.0880 0.0395 0.311 6.523 4.455 231.541 0.737 19.817 8.727 0.24 113287. 0.5273 11.77 0.2020 0.4344 0.0861 0.0400 0.315 6.616 4.361 234.837 0.748 19.396 8.422 0.24 113436. 0.5034 13.45 0.2309 0.4790 0.0840 0.0405 0.319 6.693 4.256 237.563 0.756 18.932 8.127 0.24 113597. 0.4799 15.13 0.2597 0.5200 0.0818 0.0408 0.321 6.751 4.142 239.600 0.763 18.423 7.841 0.24 113771. 0.4567 16.81 0.2886 0.5574 0.0793 0.0411 0.323 6.785 4.017 240.826 0.767 17.865 7.565 0.24 113958. 0.4339 18.49 0.3175 0.5916 0.0766 0.0411 0.323 6.793 3.880 241.121 0.768 17.258 7.299 0.25 114159. 0.4115 20.17 0.3463 0.6227 0.0737 0.0410 0.322 6.772 3.732 240.367 0.765 16.600 7.042 0.25 114372. 0.3894 21.85 0.3752 0.6509 0.0705 0.0406 0.320 6.718 3.572 238.451 0.759 15.889 6.795 0.25 114599. 0.3676 23.53 0.4040 0.6762 0.0671 0.0401 0.315 6.628 3.400 235.266 0.749 15.124 6.555 0.25 114839. 0.3460 25.21 0.4329 0.6989 0.0635 0.0393 0.309 6.500 3.216 230.705 0.734 14.306 6.323 0.25 115093. 0.3246 26.89 0.4618 0.7188 0.0596 0.0383 0.301 6.330 3.020 224.677 0.715 13.433 6.097 0.25 115360. 0.3033 28.57 0.4906 0.7359 0.0555 0.0370 0.291 6.119 2.813 217.186 0.691 12.512 5.875 0.25 115641. 0.2820 30.25 0.5195 0.7500 0.0513 0.0355 0.279 5.868 2.597 208.286 0.663 11.550 5.655 0.25 115936. 0.2608 31.93 0.5483 0.7608 0.0468 0.0338 0.266 5.580 2.373 198.041 0.630 10.553 5.434 0.25 116243. 0.2396 33.62 0.5772 0.7677 0.0423 0.0318 0.250 5.255 2.142 186.515 0.594 9.529 5.209 0.25 116564. 0.2182 35.30 0.6061 0.7701 0.0376 0.0296 0.233 4.896 1.907 173.771 0.553 8.481 4.977 0.25 116898. 0.1967 36.98 0.6349 0.7669 0.0329 0.0273 0.214 4.504 1.667 159.876 0.509 7.417 4.731 0.25 117246. 0.1748 38.66 0.6638 0.7563 0.0281 0.0247 0.194 4.082 1.426 144.902 0.461 6.341 4.463 0.25 117606. 0.1525 40.34 0.6926 0.7357 0.0233 0.0220 0.173 3.633 1.183 128.934 0.410 5.260 4.160 0.25 117980. 0.1295 42.02 0.7215 0.7007 0.0186 0.0191 0.150 3.157 0.940 112.068 0.357 4.180 3.804 0.25 118367. 0.1055 43.70 0.7504 0.6430 0.0138 0.0161 0.127 2.660 0.699 94.420 0.301 3.108 3.356 0.25 118767. 0.0803 45.38 0.7792 0.5462 0.0091 0.0130 0.102 2.145 0.461 76.127 0.242 2.050 2.746 0.25 119180. 0.0533 47.06 0.8081 0.3721 0.0045 0.0098 0.077 1.616 0.228 57.348 0.183 1.014 1.804 0.25 119605. 0.0247 48.74 0.8369 0.0049 0.0000 0.0065 0.051 1.077 0.002 38.244 0.122 0.009 0.023 0.25 120041. 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 0.0963 0.0346 0.645 10.170 8.669 481.275 1.149 38.559 8.170 0.33 150163. 0.6885 2.24 0.0289 0.0778 0.0953 0.0354 0.660 10.402 8.582 492.287 1.175 38.174 7.907 0.33 150277. 0.6630 4.49 0.0578 0.1504 0.0942 0.0362 0.675 10.636 8.485 503.340 1.202 37.743 7.646 0.33 150402. 0.6375 6.73 0.0867 0.2180 0.0930 0.0370 0.690 10.866 8.377 514.249 1.228 37.259 7.388 0.33 150541. 0.6120 8.98 0.1156 0.2807 0.0917 0.0377 0.704 11.090 8.255 524.811 1.253 36.718 7.134 0.33 150695. 0.5867 11.22 0.1445 0.3387 0.0902 0.0385 0.717 11.301 8.119 534.803 1.277 36.114 6.886 0.33 150863. 0.5616 13.46 0.1734 0.3921 0.0885 0.0391 0.729 11.495 7.968 543.974 1.299 35.442 6.644 0.33 151046. 0.5368 15.71 0.2023 0.4413 0.0866 0.0397 0.740 11.665 7.801 552.060 1.318 34.697 6.409 0.33 151245. 0.5123 17.95 0.2312 0.4865 0.0846 0.0402 0.749 11.807 7.615 558.780 1.334 33.873 6.182 0.33 151461. 0.4883 20.19 0.2601 0.5278 0.0823 0.0406 0.756 11.914 7.412 563.845 1.346 32.967 5.962 0.33 151694. 0.4646 22.44 0.2890 0.5657 0.0798 0.0408 0.760 11.980 7.188 566.958 1.354 31.974 5.751 0.33 151944. 0.4413 24.68 0.3179 0.6003 0.0771 0.0408 0.761 11.999 6.945 567.828 1.356 30.891 5.548 0.33 152212. 0.4185 26.93 0.3467 0.6318 0.0742 0.0407 0.759 11.963 6.681 566.167 1.352 29.716 5.352 0.33 152498. 0.3959 29.17 0.3756 0.6604 0.0710 0.0404 0.753 11.869 6.395 561.699 1.341 28.445 5.164 0.33 152801. 0.3738 31.41 0.4045 0.6862 0.0676 0.0399 0.743 11.710 6.088 554.168 1.323 27.078 4.983 0.33 153122. 0.3519 33.66 0.4334 0.7093 0.0639 0.0391 0.729 11.480 5.758 543.306 1.297 25.612 4.807 0.33 153462. 0.3302 35.90 0.4623 0.7298 0.0600 0.0380 0.709 11.176 5.407 528.897 1.263 24.050 4.637 0.33 153819. 0.3086 38.14 0.4912 0.7476 0.0559 0.0367 0.685 10.796 5.036 510.938 1.220 22.399 4.470 0.33 154195. 0.2871 40.39 0.5201 0.7625 0.0516 0.0352 0.657 10.345 4.648 489.557 1.169 20.674 4.306 0.33 154588. 0.2657 42.63 0.5490 0.7743 0.0472 0.0334 0.623 9.824 4.246 464.904 1.110 18.887 4.143 0.33 155000. 0.2443 44.88 0.5779 0.7824 0.0426 0.0314 0.586 9.237 3.833 437.129 1.044 17.049 3.977 0.33 155429. 0.2229 47.12 0.6068 0.7863 0.0379 0.0292 0.545 8.587 3.411 406.386 0.970 15.170 3.807 0.33 155876. 0.2012 49.36 0.6357 0.7849 0.0331 0.0268 0.500 7.878 2.981 372.832 0.890 13.261 3.627 0.33 156340. 0.1793 51.61 0.6646 0.7766 0.0283 0.0242 0.451 7.114 2.548 336.646 0.804 11.332 3.433 0.33 156822. 0.1568 53.85 0.6935 0.7588 0.0235 0.0214 0.400 6.298 2.112 298.031 0.711 9.394 3.214 0.33 157322. 0.1337 56.10 0.7224 0.7270 0.0186 0.0185 0.345 5.435 1.677 257.225 0.614 7.457 2.956 0.33 157839. 0.1096 58.34 0.7513 0.6729 0.0138 0.0154 0.288 4.533 1.244 214.512 0.512 5.534 2.631 0.33 158373. 0.0840 60.58 0.7802 0.5789 0.0091 0.0122 0.228 3.597 0.818 170.229 0.406 3.639 2.180 0.34 158925. 0.0564 62.83 0.8091 0.4017 0.0045 0.0090 0.167 2.636 0.401 124.770 0.298 1.784 1.458 0.34 159494. 0.0264 65.07 0.8380 -0.0059 0.0000 0.0056 0.105 1.659 -0.004 78.519 0.187 -0.016 -0.021 0.34 160075. 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 0.0968 0.0344 1.255 15.815 13.625 935.564 1.787 60.603 6.605 0.41 187696. 0.6979 2.80 0.0289 0.0786 0.0959 0.0353 1.284 16.186 13.493 957.507 1.829 60.016 6.392 0.41 187837. 0.6720 5.61 0.0578 0.1519 0.0948 0.0361 1.314 16.559 13.344 979.563 1.871 59.355 6.179 0.41 187995. 0.6460 8.41 0.0867 0.2201 0.0937 0.0369 1.343 16.928 13.177 1001.365 1.912 58.613 5.969 0.41 188169. 0.6202 11.22 0.1156 0.2833 0.0923 0.0377 1.371 17.285 12.990 1022.508 1.953 57.780 5.762 0.41 188360. 0.5944 14.02 0.1444 0.3418 0.0908 0.0384 1.398 17.624 12.781 1042.547 1.991 56.848 5.560 0.41 188570. 0.5690 16.82 0.1733 0.3956 0.0892 0.0391 1.423 17.935 12.547 1060.982 2.026 55.808 5.364 0.41 188800. 0.5438 19.63 0.2022 0.4452 0.0873 0.0397 1.445 18.211 12.287 1077.284 2.057 54.652 5.173 0.41 189049. 0.5190 22.43 0.2311 0.4906 0.0853 0.0402 1.463 18.441 11.999 1090.892 2.083 53.371 4.989 0.41 189319. 0.4946 25.24 0.2600 0.5323 0.0830 0.0406 1.477 18.616 11.682 1101.226 2.103 51.959 4.811 0.41 189611. 0.4707 28.04 0.2889 0.5705 0.0805 0.0408 1.485 18.725 11.333 1107.700 2.116 50.410 4.641 0.41 189924. 0.4472 30.85 0.3178 0.6053 0.0778 0.0409 1.488 18.759 10.952 1109.723 2.119 48.716 4.477 0.41 190259. 0.4240 33.65 0.3467 0.6371 0.0749 0.0408 1.484 18.709 10.539 1106.722 2.114 46.875 4.319 0.41 190616. 0.4013 36.45 0.3756 0.6661 0.0717 0.0404 1.473 18.564 10.091 1098.151 2.097 44.883 4.168 0.41 190996. 0.3789 39.26 0.4045 0.6922 0.0683 0.0399 1.453 18.316 9.608 1083.491 2.069 42.737 4.022 0.41 191398. 0.3569 42.06 0.4333 0.7158 0.0646 0.0391 1.424 17.956 9.091 1062.217 2.029 40.435 3.882 0.41 191822. 0.3350 44.87 0.4622 0.7367 0.0607 0.0381 1.386 17.477 8.538 1033.883 1.975 37.977 3.746 0.41 192269. 0.3133 47.67 0.4911 0.7551 0.0565 0.0368 1.339 16.879 7.954 998.465 1.907 35.379 3.613 0.41 192739. 0.2917 50.47 0.5200 0.7707 0.0522 0.0352 1.282 16.164 7.343 956.204 1.826 32.662 3.483 0.41 193231. 0.2702 53.28 0.5489 0.7834 0.0477 0.0334 1.217 15.339 6.710 907.397 1.733 29.845 3.354 0.41 193746. 0.2487 56.08 0.5778 0.7926 0.0431 0.0314 1.143 14.408 6.058 852.340 1.628 26.946 3.224 0.41 194282. 0.2271 58.89 0.6067 0.7978 0.0383 0.0291 1.061 13.377 5.392 791.331 1.511 23.982 3.090 0.41 194841. 0.2054 61.69 0.6356 0.7980 0.0335 0.0267 0.972 12.251 4.714 724.690 1.384 20.969 2.951 0.41 195421. 0.1834 64.50 0.6645 0.7917 0.0286 0.0240 0.875 11.035 4.030 652.767 1.247 17.924 2.800 0.42 196024. 0.1609 67.30 0.6933 0.7763 0.0237 0.0212 0.772 9.736 3.341 575.969 1.100 14.863 2.631 0.42 196648. 0.1377 70.10 0.7222 0.7477 0.0189 0.0182 0.664 8.364 2.654 494.772 0.945 11.804 2.433 0.42 197294. 0.1134 72.91 0.7511 0.6973 0.0140 0.0151 0.549 6.927 1.971 409.747 0.783 8.767 2.182 0.42 197962. 0.0877 75.71 0.7800 0.6076 0.0092 0.0118 0.431 5.436 1.298 321.571 0.614 5.772 1.830 0.42 198652. 0.0597 78.52 0.8089 0.4320 0.0045 0.0085 0.310 3.906 0.639 231.038 0.441 2.844 1.255 0.42 199363. 0.0287 81.32 0.8378 0.0001 0.0000 0.0051 0.186 2.348 0.000 138.917 0.265 0.000 0.000 0.42 200089. 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 0.0975 0.0345 2.171 22.806 19.760 1618.912 2.577 87.894 5.536 0.49 225223. 0.7044 3.36 0.0289 0.0790 0.0966 0.0353 2.223 23.352 19.576 1657.673 2.638 87.074 5.356 0.49 225392. 0.6783 6.73 0.0578 0.1527 0.0956 0.0362 2.275 23.901 19.368 1696.697 2.700 86.148 5.177 0.49 225581. 0.6522 10.09 0.0867 0.2213 0.0944 0.0370 2.327 24.446 19.133 1735.330 2.762 85.104 5.001 0.49 225790. 0.6261 13.46 0.1156 0.2848 0.0931 0.0378 2.377 24.974 18.869 1772.863 2.822 83.928 4.827 0.49 226020. 0.6002 16.82 0.1444 0.3435 0.0917 0.0385 2.425 25.476 18.572 1808.499 2.878 82.607 4.658 0.49 226272. 0.5745 20.19 0.1733 0.3976 0.0900 0.0392 2.469 25.939 18.239 1841.351 2.931 81.129 4.493 0.49 226548. 0.5492 23.55 0.2022 0.4474 0.0882 0.0399 2.508 26.350 17.869 1870.481 2.977 79.479 4.333 0.49 226848. 0.5242 26.92 0.2311 0.4931 0.0862 0.0404 2.541 26.693 17.457 1894.886 3.016 77.647 4.179 0.49 227173. 0.4997 30.28 0.2600 0.5350 0.0839 0.0408 2.566 26.956 17.001 1913.542 3.045 75.622 4.030 0.49 227523. 0.4756 33.65 0.2889 0.5734 0.0814 0.0410 2.582 27.123 16.500 1925.399 3.064 73.393 3.887 0.49 227899. 0.4519 37.01 0.3178 0.6085 0.0787 0.0411 2.587 27.180 15.952 1929.416 3.071 70.953 3.750 0.49 228302. 0.4287 40.38 0.3467 0.6405 0.0758 0.0410 2.581 27.112 15.354 1924.573 3.063 68.294 3.618 0.49 228731. 0.4058 43.74 0.3755 0.6697 0.0726 0.0407 2.561 26.905 14.706 1909.900 3.040 65.411 3.492 0.49 229187. 0.3833 47.11 0.4044 0.6962 0.0691 0.0402 2.527 26.547 14.007 1884.481 2.999 62.302 3.371 0.49 229670. 0.3611 50.47 0.4333 0.7201 0.0654 0.0394 2.477 26.024 13.256 1847.399 2.940 58.963 3.255 0.49 230181. 0.3392 53.84 0.4622 0.7415 0.0615 0.0383 2.411 25.326 12.454 1797.847 2.861 55.393 3.142 0.49 230718. 0.3174 57.20 0.4911 0.7604 0.0573 0.0370 2.328 24.452 11.604 1735.743 2.763 51.616 3.032 0.49 231282. 0.2957 60.57 0.5200 0.7766 0.0529 0.0354 2.228 23.406 10.715 1661.504 2.644 47.660 2.925 0.49 231873. 0.2741 63.93 0.5489 0.7900 0.0483 0.0336 2.113 22.196 9.792 1575.646 2.508 43.556 2.819 0.50 232491. 0.2525 67.30 0.5778 0.8001 0.0436 0.0315 1.983 20.830 8.842 1478.693 2.353 39.329 2.712 0.50 233136. 0.2308 70.66 0.6066 0.8064 0.0388 0.0292 1.839 19.316 7.870 1371.173 2.182 35.005 2.603 0.50 233806. 0.2090 74.02 0.6355 0.8079 0.0340 0.0267 1.681 17.660 6.881 1253.646 1.995 30.608 2.490 0.50 234503. 0.1869 77.39 0.6644 0.8033 0.0290 0.0240 1.511 15.872 5.882 1126.738 1.793 26.161 2.368 0.50 235227. 0.1644 80.75 0.6933 0.7900 0.0241 0.0211 1.329 13.963 4.876 991.167 1.577 21.690 2.232 0.50 235976. 0.1410 84.12 0.7222 0.7639 0.0191 0.0181 1.137 11.943 3.872 847.782 1.349 17.221 2.071 0.50 236752. 0.1167 87.48 0.7511 0.7166 0.0142 0.0149 0.935 9.827 2.874 697.599 1.110 12.783 1.869 0.50 237553. 0.0907 90.85 0.7800 0.6301 0.0093 0.0115 0.727 7.633 1.890 541.827 0.862 8.407 1.582 0.50 238381. 0.0623 94.21 0.8089 0.4551 0.0046 0.0081 0.512 5.380 0.928 381.892 0.608 4.127 1.102 0.50 239234. 0.0304 97.58 0.8377 -0.0057 0.0000 0.0047 0.294 3.087 -0.006 219.139 0.349 -0.029 -0.013 0.50 240104. 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 0.0984 0.0347 3.470 31.241 27.125 2587.362 3.530 120.651 4.755 0.57 262742. 0.7088 3.92 0.0289 0.0791 0.0975 0.0356 3.554 32.003 26.884 2650.454 3.616 119.582 4.601 0.57 262940. 0.6828 7.85 0.0577 0.1530 0.0965 0.0364 3.640 32.772 26.612 2714.097 3.703 118.369 4.447 0.57 263160. 0.6567 11.77 0.0866 0.2216 0.0954 0.0373 3.724 33.534 26.302 2777.229 3.789 116.993 4.296 0.57 263403. 0.6306 15.69 0.1155 0.2853 0.0941 0.0381 3.807 34.276 25.953 2838.692 3.873 115.437 4.147 0.57 263672. 0.6047 19.62 0.1444 0.3441 0.0927 0.0389 3.885 34.982 25.558 2897.172 3.952 113.681 4.001 0.57 263966. 0.5790 23.54 0.1732 0.3983 0.0911 0.0396 3.958 35.635 25.114 2951.222 4.026 111.706 3.860 0.57 264288. 0.5536 27.46 0.2021 0.4482 0.0893 0.0402 4.022 36.215 24.616 2999.286 4.092 109.493 3.723 0.57 264638. 0.5287 31.39 0.2310 0.4940 0.0872 0.0408 4.076 36.704 24.062 3039.727 4.147 107.026 3.590 0.57 265017. 0.5041 35.31 0.2598 0.5361 0.0850 0.0412 4.118 37.079 23.446 3070.849 4.189 104.288 3.463 0.57 265426. 0.4800 39.23 0.2887 0.5746 0.0826 0.0415 4.145 37.322 22.766 3090.947 4.217 101.265 3.341 0.57 265866. 0.4562 43.16 0.3176 0.6099 0.0798 0.0416 4.155 37.411 22.020 3098.304 4.227 97.945 3.224 0.57 266336. 0.4330 47.08 0.3464 0.6421 0.0769 0.0415 4.145 37.326 21.205 3091.254 4.217 94.318 3.111 0.57 266837. 0.4101 51.00 0.3753 0.6716 0.0737 0.0412 4.115 37.048 20.319 3068.216 4.186 90.378 3.004 0.57 267370. 0.3875 54.93 0.4042 0.6984 0.0702 0.0406 4.060 36.558 19.362 3027.698 4.130 86.120 2.900 0.57 267934. 0.3653 58.85 0.4331 0.7227 0.0665 0.0398 3.980 35.840 18.332 2968.224 4.049 81.539 2.801 0.57 268530. 0.3433 62.77 0.4619 0.7445 0.0625 0.0388 3.873 34.877 17.229 2888.451 3.940 76.634 2.705 0.58 269158. 0.3214 66.70 0.4908 0.7639 0.0582 0.0374 3.739 33.666 16.060 2788.175 3.804 71.434 2.613 0.58 269816. 0.2997 70.62 0.5197 0.7807 0.0538 0.0358 3.578 32.216 14.834 2668.053 3.640 65.982 2.522 0.58 270506. 0.2780 74.54 0.5485 0.7948 0.0492 0.0339 3.391 30.536 13.561 2528.919 3.450 60.319 2.432 0.58 271227. 0.2564 78.47 0.5774 0.8058 0.0444 0.0318 3.180 28.637 12.248 2371.628 3.235 54.481 2.342 0.58 271979. 0.2347 82.39 0.6063 0.8131 0.0395 0.0295 2.946 26.529 10.904 2197.045 2.997 48.503 2.251 0.58 272761. 0.2128 86.31 0.6352 0.8159 0.0346 0.0269 2.690 24.223 9.537 2006.090 2.737 42.419 2.156 0.58 273575. 0.1906 90.23 0.6640 0.8128 0.0296 0.0242 2.414 21.732 8.153 1799.776 2.455 36.263 2.055 0.58 274418. 0.1679 94.16 0.6929 0.8014 0.0245 0.0212 2.118 19.069 6.760 1579.281 2.154 30.070 1.942 0.58 275292. 0.1445 98.08 0.7218 0.7778 0.0195 0.0181 1.805 16.252 5.368 1345.991 1.836 23.876 1.809 0.58 276196. 0.1200 102.00 0.7506 0.7336 0.0144 0.0148 1.477 13.301 3.984 1101.572 1.503 17.722 1.641 0.59 277131. 0.0937 105.93 0.7795 0.6507 0.0095 0.0114 1.137 10.239 2.620 848.013 1.157 11.652 1.401 0.59 278095. 0.0649 109.85 0.8084 0.4775 0.0047 0.0079 0.788 7.096 1.285 587.664 0.802 5.715 0.992 0.59 279090. 0.0322 113.77 0.8373 -0.0080 0.0000 0.0043 0.433 3.897 -0.011 322.723 0.440 -0.051 -0.016 0.59 280103. 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 0.0993 0.0351 5.238 41.267 35.780 3905.862 4.662 159.148 4.155 0.65 300251. 0.7114 4.48 0.0288 0.0790 0.0985 0.0360 5.368 42.288 35.484 4002.555 4.778 157.834 4.021 0.65 300477. 0.6856 8.96 0.0577 0.1527 0.0976 0.0369 5.499 43.322 35.146 4100.418 4.895 156.331 3.888 0.65 300728. 0.6597 13.44 0.0865 0.2213 0.0965 0.0377 5.629 44.351 34.761 4197.822 5.011 154.618 3.756 0.65 301006. 0.6338 17.92 0.1154 0.2848 0.0953 0.0386 5.757 45.356 34.322 4292.951 5.124 152.665 3.626 0.65 301313. 0.6081 22.40 0.1442 0.3436 0.0939 0.0394 5.879 46.316 33.824 4383.748 5.233 150.448 3.500 0.65 301650. 0.5826 26.88 0.1731 0.3978 0.0923 0.0402 5.992 47.205 33.259 4467.936 5.333 147.937 3.376 0.65 302018. 0.5573 31.36 0.2019 0.4477 0.0906 0.0408 6.092 47.999 32.623 4543.078 5.423 145.108 3.257 0.65 302418. 0.5325 35.84 0.2307 0.4936 0.0886 0.0414 6.178 48.670 31.910 4606.619 5.499 141.936 3.142 0.65 302851. 0.5080 40.31 0.2596 0.5357 0.0864 0.0419 6.244 49.191 31.115 4655.915 5.558 138.399 3.031 0.65 303319. 0.4840 44.79 0.2884 0.5744 0.0839 0.0421 6.287 49.533 30.233 4688.316 5.596 134.477 2.925 0.65 303822. 0.4603 49.27 0.3173 0.6098 0.0812 0.0423 6.304 49.669 29.261 4701.166 5.612 130.152 2.823 0.65 304360. 0.4371 53.75 0.3461 0.6423 0.0783 0.0422 6.292 49.571 28.195 4691.886 5.601 125.411 2.726 0.65 304933. 0.4143 58.23 0.3750 0.6720 0.0750 0.0419 6.247 49.213 27.033 4658.028 5.560 120.245 2.632 0.66 305542. 0.3917 62.71 0.4038 0.6991 0.0716 0.0413 6.165 48.572 25.775 4597.310 5.488 114.647 2.543 0.66 306188. 0.3695 67.19 0.4326 0.7238 0.0678 0.0405 6.045 47.623 24.418 4507.488 5.380 108.610 2.457 0.66 306869. 0.3475 71.67 0.4615 0.7460 0.0637 0.0394 5.882 46.344 22.962 4386.476 5.236 102.134 2.374 0.66 307586. 0.3256 76.15 0.4903 0.7659 0.0595 0.0381 5.678 44.732 21.415 4233.822 5.054 95.254 2.294 0.66 308340. 0.3039 80.63 0.5192 0.7833 0.0549 0.0364 5.432 42.795 19.790 4050.483 4.835 88.026 2.216 0.66 309128. 0.2822 85.11 0.5480 0.7981 0.0502 0.0345 5.147 40.547 18.099 3837.756 4.581 80.507 2.139 0.66 309952. 0.2605 89.59 0.5769 0.8100 0.0454 0.0323 4.824 38.003 16.354 3596.970 4.294 72.745 2.062 0.66 310811. 0.2387 94.07 0.6057 0.8183 0.0404 0.0299 4.465 35.177 14.566 3329.463 3.974 64.788 1.984 0.66 311705. 0.2168 98.55 0.6345 0.8223 0.0354 0.0273 4.072 32.083 12.743 3036.650 3.625 56.682 1.903 0.66 312634. 0.1945 103.03 0.6634 0.8207 0.0303 0.0245 3.648 28.739 10.898 2720.104 3.247 48.472 1.817 0.66 313597. 0.1717 107.51 0.6922 0.8113 0.0251 0.0214 3.194 25.163 9.039 2381.635 2.843 40.205 1.721 0.67 314595. 0.1481 111.98 0.7211 0.7900 0.0199 0.0182 2.713 21.378 7.179 2023.386 2.415 31.932 1.609 0.67 315627. 0.1234 116.46 0.7499 0.7489 0.0148 0.0148 2.210 17.411 5.330 1647.938 1.967 23.706 1.467 0.67 316693. 0.0969 120.94 0.7788 0.6697 0.0097 0.0113 1.688 13.296 3.504 1258.431 1.502 15.588 1.263 0.67 317794. 0.0677 125.42 0.8076 0.4991 0.0048 0.0077 1.151 9.072 1.718 858.616 1.025 7.644 0.908 0.67 318929. 0.0341 129.90 0.8364 -0.0093 0.0000 0.0041 0.606 4.776 -0.016 452.044 0.540 -0.072 -0.016 0.67 320084. 0.0000 PROP RPM = 9000 V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM (mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - - 0.00 0.0000 0.0000 0.1004 0.0362 7.685 53.821 45.790 5730.890 6.081 203.673 3.624 0.73 337749. 0.7019 5.03 0.0288 0.0775 0.0997 0.0370 7.864 55.075 45.447 5864.418 6.222 202.149 3.515 0.73 338003. 0.6783 10.06 0.0576 0.1503 0.0988 0.0379 8.046 56.348 45.052 5999.943 6.366 200.393 3.406 0.73 338284. 0.6543 15.10 0.0864 0.2182 0.0978 0.0387 8.228 57.619 44.598 6135.260 6.510 198.372 3.297 0.73 338596. 0.6302 20.13 0.1152 0.2814 0.0967 0.0396 8.405 58.864 44.075 6267.871 6.650 196.047 3.189 0.73 338941. 0.6061 25.16 0.1440 0.3401 0.0954 0.0404 8.576 60.057 43.476 6394.949 6.785 193.381 3.084 0.73 339319. 0.5820 30.19 0.1728 0.3944 0.0939 0.0411 8.734 61.169 42.792 6513.311 6.911 190.337 2.980 0.73 339732. 0.5579 35.22 0.2016 0.4445 0.0922 0.0418 8.877 62.166 42.013 6619.518 7.024 186.876 2.879 0.73 340182. 0.5341 40.26 0.2304 0.4907 0.0902 0.0424 8.998 63.015 41.134 6709.882 7.119 182.965 2.781 0.73 340670. 0.5104 45.29 0.2592 0.5332 0.0881 0.0428 9.093 63.679 40.146 6780.570 7.194 178.571 2.685 0.73 341197. 0.4870 50.32 0.2880 0.5722 0.0856 0.0431 9.156 64.121 39.044 6827.605 7.244 173.667 2.594 0.73 341762. 0.4639 55.35 0.3168 0.6080 0.0830 0.0432 9.182 64.303 37.822 6846.997 7.265 168.230 2.505 0.74 342368. 0.4410 60.38 0.3456 0.6408 0.0800 0.0432 9.166 64.188 36.475 6834.763 7.252 162.241 2.421 0.74 343013. 0.4184 65.42 0.3744 0.6708 0.0768 0.0429 9.102 63.740 35.001 6787.023 7.201 155.685 2.339 0.74 343699. 0.3961 70.45 0.4032 0.6983 0.0733 0.0423 8.985 62.923 33.398 6700.133 7.109 148.556 2.261 0.74 344426. 0.3740 75.48 0.4320 0.7233 0.0695 0.0415 8.811 61.707 31.665 6570.561 6.972 140.845 2.186 0.74 345192. 0.3521 80.51 0.4608 0.7460 0.0654 0.0404 8.576 60.058 29.800 6395.027 6.785 132.549 2.114 0.74 346000. 0.3302 85.54 0.4896 0.7664 0.0610 0.0390 8.278 57.969 27.813 6172.596 6.549 123.710 2.044 0.74 346847. 0.3085 90.58 0.5184 0.7845 0.0564 0.0373 7.918 55.452 25.720 5904.605 6.265 114.402 1.976 0.74 347734. 0.2868 95.61 0.5472 0.8001 0.0516 0.0353 7.500 52.526 23.538 5592.986 5.934 104.697 1.909 0.74 348660. 0.2651 100.64 0.5760 0.8128 0.0467 0.0331 7.027 49.209 21.282 5239.775 5.560 94.661 1.842 0.74 349626. 0.2432 105.67 0.6048 0.8222 0.0416 0.0306 6.500 45.521 18.965 4847.087 5.143 84.357 1.775 0.75 350631. 0.2212 110.71 0.6336 0.8273 0.0364 0.0279 5.924 41.484 16.602 4417.201 4.687 73.845 1.705 0.75 351674. 0.1988 115.74 0.6624 0.8270 0.0312 0.0250 5.301 37.121 14.205 3952.681 4.194 63.183 1.630 0.75 352756. 0.1758 120.77 0.6912 0.8190 0.0259 0.0218 4.635 32.462 11.788 3456.583 3.668 52.435 1.547 0.75 353877. 0.1520 125.80 0.7200 0.7990 0.0205 0.0185 3.933 27.541 9.367 2932.606 3.112 41.664 1.449 0.75 355036. 0.1269 130.83 0.7488 0.7587 0.0153 0.0151 3.199 22.401 6.956 2385.312 2.531 30.942 1.323 0.75 356234. 0.0999 135.87 0.7776 0.6790 0.0100 0.0115 2.441 17.095 4.575 1820.286 1.931 20.348 1.140 0.75 357469. 0.0698 140.90 0.8064 0.5047 0.0049 0.0079 1.669 11.685 2.241 1244.215 1.320 9.969 0.817 0.76 358742. 0.0350 145.93 0.8352 -0.0121 -0.0001 0.0042 0.890 6.232 -0.028 663.570 0.704 -0.123 -0.019 0.76 360038. 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 0.1016 0.0399 11.616 73.215 57.185 8662.162 8.272 254.361 2.994 0.81 375233. 0.6481 5.58 0.0287 0.0714 0.1009 0.0406 11.835 74.591 56.814 8825.055 8.427 252.708 2.920 0.81 375512. 0.6300 11.16 0.0575 0.1391 0.1002 0.0414 12.054 75.974 56.381 8988.668 8.584 250.784 2.845 0.81 375824. 0.6114 16.73 0.0862 0.2032 0.0993 0.0421 12.270 77.336 55.877 9149.750 8.737 248.542 2.770 0.81 376169. 0.5926 22.31 0.1149 0.2636 0.0982 0.0428 12.478 78.646 55.291 9304.763 8.885 245.934 2.695 0.81 376549. 0.5736 27.89 0.1437 0.3205 0.0970 0.0435 12.672 79.871 54.610 9449.706 9.024 242.905 2.621 0.81 376968. 0.5544 33.47 0.1724 0.3739 0.0956 0.0441 12.847 80.975 53.823 9580.310 9.149 239.402 2.548 0.81 377426. 0.5351 39.04 0.2011 0.4239 0.0940 0.0446 12.997 81.920 52.917 9692.074 9.255 235.373 2.476 0.81 377925. 0.5156 44.62 0.2299 0.4707 0.0922 0.0450 13.116 82.666 51.881 9780.418 9.340 230.767 2.406 0.82 378466. 0.4960 50.20 0.2586 0.5143 0.0901 0.0453 13.197 83.176 50.705 9840.728 9.397 225.537 2.337 0.82 379050. 0.4763 55.78 0.2873 0.5550 0.0877 0.0454 13.234 83.410 49.381 9868.368 9.424 219.645 2.270 0.82 379678. 0.4565 61.36 0.3161 0.5928 0.0851 0.0454 13.221 83.328 47.899 9858.733 9.414 213.055 2.204 0.82 380351. 0.4365 66.93 0.3448 0.6277 0.0822 0.0451 13.152 82.893 46.255 9807.267 9.365 205.741 2.139 0.82 381068. 0.4164 72.51 0.3735 0.6600 0.0790 0.0447 13.021 82.067 44.443 9709.451 9.272 197.684 2.076 0.82 381830. 0.3962 78.09 0.4023 0.6896 0.0754 0.0440 12.821 80.811 42.462 9560.855 9.130 188.870 2.014 0.82 382636. 0.3757 83.67 0.4310 0.7167 0.0716 0.0431 12.548 79.087 40.308 9356.977 8.935 179.292 1.954 0.82 383488. 0.3551 89.24 0.4597 0.7412 0.0675 0.0419 12.194 76.857 37.982 9093.039 8.683 168.943 1.895 0.82 384384. 0.3342 94.82 0.4885 0.7633 0.0631 0.0404 11.757 74.100 35.492 8766.952 8.372 157.867 1.836 0.82 385325. 0.3131 100.40 0.5172 0.7827 0.0584 0.0386 11.240 70.843 32.859 8381.583 8.004 146.157 1.778 0.82 386309. 0.2918 105.98 0.5459 0.7991 0.0535 0.0365 10.646 67.100 30.105 7938.703 7.581 133.908 1.720 0.83 387337. 0.2701 111.56 0.5746 0.8123 0.0484 0.0343 9.979 62.896 27.250 7441.286 7.106 121.208 1.661 0.83 388409. 0.2482 117.13 0.6034 0.8216 0.0432 0.0317 9.242 58.253 24.311 6892.061 6.581 108.137 1.600 0.83 389523. 0.2258 122.71 0.6321 0.8260 0.0379 0.0290 8.441 53.199 21.307 6294.112 6.010 94.774 1.535 0.83 390680. 0.2029 128.29 0.6608 0.8238 0.0324 0.0260 7.580 47.777 18.254 5652.558 5.398 81.195 1.465 0.83 391879. 0.1791 133.87 0.6896 0.8119 0.0270 0.0229 6.670 42.038 15.171 4973.632 4.749 67.479 1.383 0.83 393120. 0.1542 139.44 0.7183 0.7850 0.0215 0.0196 5.719 36.048 12.075 4264.939 4.073 53.708 1.284 0.83 394404. 0.1277 145.02 0.7470 0.7330 0.0160 0.0163 4.741 29.882 8.987 3535.388 3.376 39.972 1.153 0.84 395729. 0.0989 150.60 0.7758 0.6352 0.0105 0.0129 3.749 23.626 5.929 2795.278 2.669 26.373 0.962 0.84 397097. 0.0671 156.18 0.8045 0.4422 0.0052 0.0095 2.757 17.379 2.928 2056.154 1.963 13.022 0.646 0.84 398506. 0.0316 161.76 0.8332 0.0018 0.0000 0.0061 1.782 11.233 0.007 1329.005 1.269 0.033 0.002 0.84 399946. 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 0.1021 0.0475 18.411 105.493 69.502 13729.150 11.919 309.143 2.296 0.89 412733. 0.5479 6.16 0.0289 0.0608 0.1015 0.0482 18.695 107.121 69.141 13941.109 12.103 307.537 2.249 0.89 413037. 0.5354 12.33 0.0577 0.1190 0.1009 0.0489 18.975 108.721 68.713 14149.326 12.283 305.635 2.203 0.89 413376. 0.5226 18.49 0.0866 0.1748 0.1002 0.0496 19.241 110.246 68.205 14347.807 12.456 303.377 2.156 0.89 413753. 0.5097 24.65 0.1154 0.2281 0.0993 0.0502 19.485 111.646 67.603 14529.933 12.614 300.696 2.110 0.90 414171. 0.4966 30.81 0.1443 0.2790 0.0982 0.0508 19.698 112.865 66.888 14688.546 12.751 297.518 2.065 0.90 414631. 0.4835 36.98 0.1732 0.3277 0.0970 0.0512 19.869 113.846 66.044 14816.195 12.862 293.766 2.022 0.90 415135. 0.4703 43.14 0.2020 0.3744 0.0955 0.0515 19.989 114.532 65.054 14905.552 12.940 289.362 1.980 0.90 415685. 0.4570 49.30 0.2309 0.4190 0.0938 0.0517 20.048 114.872 63.901 14949.740 12.978 284.232 1.939 0.90 416283. 0.4436 55.46 0.2597 0.4618 0.0919 0.0517 20.038 114.817 62.569 14942.613 12.972 278.306 1.899 0.90 416930. 0.4300 61.63 0.2886 0.5027 0.0896 0.0515 19.953 114.327 61.043 14878.859 12.917 271.521 1.861 0.90 417626. 0.4161 67.79 0.3175 0.5419 0.0871 0.0510 19.785 113.368 59.313 14753.984 12.808 263.825 1.823 0.90 418372. 0.4019 73.95 0.3463 0.5792 0.0842 0.0504 19.531 111.909 57.368 14564.146 12.643 255.174 1.787 0.90 419169. 0.3873 80.11 0.3752 0.6147 0.0811 0.0495 19.185 109.925 55.202 14305.958 12.419 245.537 1.750 0.90 420016. 0.3722 86.28 0.4040 0.6482 0.0775 0.0483 18.743 107.394 52.809 13976.544 12.133 234.895 1.714 0.90 420913. 0.3565 92.44 0.4329 0.6797 0.0737 0.0469 18.202 104.293 50.188 13572.973 11.783 223.236 1.677 0.90 421861. 0.3401 98.60 0.4617 0.7089 0.0695 0.0453 17.556 100.593 47.336 13091.507 11.365 210.549 1.640 0.90 422858. 0.3230 104.76 0.4906 0.7358 0.0650 0.0433 16.806 96.296 44.266 12532.281 10.879 196.897 1.602 0.91 423905. 0.3051 110.93 0.5195 0.7601 0.0602 0.0412 15.959 91.442 41.007 11900.479 10.331 182.400 1.563 0.91 425000. 0.2865 117.09 0.5483 0.7803 0.0552 0.0388 15.039 86.173 37.584 11214.823 9.736 167.174 1.520 0.91 426144. 0.2667 123.25 0.5772 0.7959 0.0500 0.0362 14.050 80.502 34.023 10476.826 9.095 151.336 1.473 0.91 427335. 0.2459 129.42 0.6060 0.8051 0.0446 0.0335 13.008 74.534 30.348 9700.026 8.421 134.987 1.419 0.91 428574. 0.2238 135.58 0.6349 0.8037 0.0390 0.0308 11.955 68.499 26.576 8914.658 7.739 118.212 1.352 0.91 429859. 0.1995 141.74 0.6638 0.7907 0.0334 0.0280 10.869 62.277 22.738 8104.883 7.036 101.138 1.272 0.91 431191. 0.1737 147.90 0.6926 0.7631 0.0277 0.0251 9.747 55.848 18.860 7268.205 6.310 83.889 1.177 0.92 432570. 0.1463 154.07 0.7215 0.7146 0.0220 0.0222 8.608 49.320 14.971 6418.634 5.572 66.593 1.058 0.92 433995. 0.1172 160.23 0.7503 0.6350 0.0163 0.0193 7.471 42.808 11.103 5571.177 4.836 49.386 0.904 0.92 435466. 0.0862 166.39 0.7792 0.5087 0.0107 0.0164 6.358 36.428 7.289 4740.837 4.116 32.422 0.697 0.92 436983. 0.0539 172.55 0.8081 0.3107 0.0052 0.0136 5.286 30.290 3.570 3941.999 3.422 15.877 0.411 0.92 438546. 0.0222 178.72 0.8369 -0.0027 0.0000 0.0110 4.266 24.441 -0.024 3180.820 2.761 -0.109 -0.003 0.93 440153. 0.0000