16x8 (16x8.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 0.0946 0.0408 0.003 0.217 0.197 2.570 0.025 0.878 34.852 0.06 30478. 0.5680 0.35 0.0228 0.0516 0.0929 0.0411 0.003 0.219 0.194 2.589 0.025 0.863 34.000 0.06 30498. 0.5493 0.69 0.0457 0.1006 0.0912 0.0414 0.003 0.220 0.190 2.605 0.025 0.847 33.146 0.06 30519. 0.5304 1.04 0.0685 0.1470 0.0893 0.0416 0.004 0.221 0.186 2.619 0.025 0.829 32.292 0.06 30542. 0.5114 1.38 0.0914 0.1908 0.0873 0.0418 0.004 0.222 0.182 2.630 0.025 0.811 31.439 0.06 30567. 0.4923 1.73 0.1142 0.2320 0.0852 0.0419 0.004 0.223 0.178 2.637 0.025 0.791 30.587 0.06 30593. 0.4731 2.08 0.1370 0.2707 0.0829 0.0420 0.004 0.223 0.173 2.641 0.025 0.770 29.738 0.06 30621. 0.4538 2.42 0.1599 0.3068 0.0805 0.0419 0.004 0.223 0.168 2.639 0.025 0.748 28.890 0.06 30651. 0.4344 2.77 0.1827 0.3403 0.0779 0.0418 0.004 0.223 0.163 2.633 0.025 0.724 28.044 0.06 30683. 0.4149 3.11 0.2055 0.3713 0.0753 0.0417 0.004 0.222 0.157 2.621 0.025 0.699 27.199 0.06 30717. 0.3954 3.46 0.2284 0.3998 0.0724 0.0414 0.003 0.220 0.151 2.603 0.025 0.673 26.353 0.06 30752. 0.3759 3.81 0.2512 0.4256 0.0694 0.0410 0.003 0.218 0.145 2.579 0.025 0.645 25.506 0.06 30790. 0.3562 4.15 0.2741 0.4488 0.0663 0.0405 0.003 0.215 0.139 2.548 0.024 0.616 24.655 0.06 30829. 0.3365 4.50 0.2969 0.4693 0.0631 0.0399 0.003 0.212 0.132 2.511 0.024 0.586 23.797 0.06 30871. 0.3168 4.84 0.3197 0.4870 0.0597 0.0392 0.003 0.209 0.125 2.467 0.024 0.555 22.931 0.06 30915. 0.2970 5.19 0.3426 0.5018 0.0563 0.0384 0.003 0.204 0.117 2.417 0.023 0.523 22.051 0.06 30960. 0.2772 5.54 0.3654 0.5134 0.0527 0.0375 0.003 0.199 0.110 2.359 0.023 0.489 21.153 0.06 31008. 0.2573 5.88 0.3882 0.5217 0.0490 0.0365 0.003 0.194 0.102 2.295 0.022 0.455 20.231 0.06 31058. 0.2374 6.23 0.4111 0.5264 0.0452 0.0353 0.003 0.188 0.094 2.223 0.021 0.420 19.278 0.06 31110. 0.2173 6.57 0.4339 0.5271 0.0414 0.0341 0.003 0.181 0.086 2.145 0.020 0.385 18.286 0.06 31165. 0.1972 6.92 0.4568 0.5231 0.0375 0.0327 0.003 0.174 0.078 2.059 0.020 0.348 17.243 0.06 31221. 0.1769 7.27 0.4796 0.5140 0.0335 0.0312 0.003 0.166 0.070 1.966 0.019 0.311 16.134 0.06 31280. 0.1565 7.61 0.5024 0.4986 0.0294 0.0297 0.003 0.158 0.061 1.866 0.018 0.273 14.941 0.06 31340. 0.1358 7.96 0.5253 0.4758 0.0253 0.0279 0.002 0.149 0.053 1.758 0.017 0.235 13.638 0.06 31404. 0.1150 8.30 0.5481 0.4439 0.0212 0.0261 0.002 0.139 0.044 1.644 0.016 0.197 12.192 0.06 31469. 0.0940 8.65 0.5710 0.4002 0.0170 0.0242 0.002 0.129 0.035 1.522 0.015 0.157 10.553 0.06 31536. 0.0728 9.00 0.5938 0.3413 0.0127 0.0221 0.002 0.118 0.027 1.393 0.013 0.118 8.653 0.06 31606. 0.0517 9.34 0.6166 0.2616 0.0085 0.0200 0.002 0.106 0.018 1.257 0.012 0.079 6.388 0.06 31678. 0.0312 9.69 0.6395 0.1526 0.0042 0.0177 0.001 0.094 0.009 1.115 0.011 0.039 3.593 0.06 31752. 0.0124 10.03 0.6623 -0.0006 0.0000 0.0154 0.001 0.082 0.000 0.967 0.009 0.000 -0.015 0.06 31827. 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 0.0950 0.0363 0.024 0.772 0.794 18.256 0.087 3.531 19.721 0.13 60955. 0.6444 0.71 0.0233 0.0594 0.0933 0.0366 0.025 0.779 0.780 18.431 0.088 3.469 19.191 0.13 60996. 0.6215 1.41 0.0466 0.1156 0.0916 0.0369 0.025 0.786 0.765 18.589 0.089 3.402 18.665 0.13 61039. 0.5986 2.12 0.0699 0.1686 0.0897 0.0372 0.025 0.791 0.749 18.724 0.089 3.331 18.142 0.13 61087. 0.5758 2.83 0.0933 0.2184 0.0876 0.0374 0.025 0.796 0.732 18.834 0.090 3.255 17.626 0.13 61137. 0.5530 3.53 0.1166 0.2650 0.0854 0.0376 0.025 0.799 0.714 18.913 0.090 3.174 17.115 0.13 61191. 0.5302 4.24 0.1399 0.3087 0.0831 0.0377 0.025 0.801 0.694 18.958 0.091 3.088 16.610 0.13 61249. 0.5075 4.95 0.1632 0.3493 0.0806 0.0377 0.025 0.801 0.674 18.964 0.091 2.996 16.112 0.13 61311. 0.4850 5.65 0.1865 0.3870 0.0780 0.0376 0.025 0.800 0.652 18.927 0.090 2.899 15.620 0.13 61377. 0.4625 6.36 0.2098 0.4218 0.0753 0.0374 0.025 0.796 0.629 18.842 0.090 2.796 15.133 0.13 61446. 0.4400 7.06 0.2331 0.4538 0.0723 0.0372 0.025 0.791 0.604 18.706 0.089 2.688 14.652 0.13 61520. 0.4177 7.77 0.2564 0.4829 0.0693 0.0368 0.025 0.782 0.579 18.515 0.088 2.574 14.176 0.13 61597. 0.3955 8.48 0.2798 0.5093 0.0661 0.0363 0.024 0.772 0.552 18.267 0.087 2.455 13.702 0.13 61679. 0.3733 9.18 0.3031 0.5327 0.0627 0.0357 0.024 0.759 0.524 17.962 0.086 2.331 13.231 0.13 61765. 0.3512 9.89 0.3264 0.5533 0.0593 0.0350 0.024 0.744 0.495 17.597 0.084 2.202 12.761 0.13 61855. 0.3293 10.60 0.3497 0.5709 0.0557 0.0341 0.023 0.726 0.465 17.173 0.082 2.069 12.288 0.13 61950. 0.3074 11.30 0.3730 0.5853 0.0520 0.0332 0.022 0.705 0.435 16.687 0.080 1.933 11.811 0.13 62049. 0.2855 12.01 0.3963 0.5963 0.0482 0.0321 0.022 0.682 0.403 16.140 0.077 1.793 11.325 0.13 62153. 0.2637 12.72 0.4196 0.6036 0.0444 0.0309 0.021 0.656 0.371 15.530 0.074 1.649 10.827 0.13 62261. 0.2418 13.42 0.4430 0.6068 0.0404 0.0295 0.020 0.628 0.338 14.856 0.071 1.502 10.312 0.13 62373. 0.2198 14.13 0.4663 0.6052 0.0364 0.0280 0.019 0.597 0.304 14.117 0.067 1.353 9.771 0.13 62490. 0.1976 14.84 0.4896 0.5981 0.0323 0.0264 0.018 0.563 0.270 13.314 0.064 1.201 9.196 0.13 62612. 0.1752 15.54 0.5129 0.5842 0.0282 0.0247 0.017 0.526 0.235 12.445 0.059 1.046 8.573 0.13 62738. 0.1525 16.25 0.5362 0.5617 0.0240 0.0229 0.015 0.486 0.200 11.510 0.055 0.890 7.885 0.13 62869. 0.1293 16.96 0.5595 0.5279 0.0197 0.0209 0.014 0.444 0.165 10.511 0.050 0.732 7.102 0.13 63004. 0.1057 17.66 0.5828 0.4787 0.0154 0.0188 0.013 0.399 0.129 9.448 0.045 0.573 6.183 0.13 63144. 0.0814 18.37 0.6062 0.4074 0.0111 0.0165 0.011 0.352 0.093 8.323 0.040 0.413 5.059 0.13 63289. 0.0565 19.07 0.6295 0.3018 0.0068 0.0142 0.010 0.302 0.057 7.139 0.034 0.253 3.610 0.13 63438. 0.0316 19.78 0.6528 0.1391 0.0025 0.0117 0.008 0.249 0.021 5.898 0.028 0.093 1.603 0.13 63591. 0.0085 20.49 0.6761 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 0.0954 0.0344 0.078 1.649 1.793 58.520 0.186 7.977 13.899 0.19 91430. 0.6826 1.05 0.0232 0.0625 0.0938 0.0348 0.079 1.666 1.762 59.142 0.188 7.838 13.515 0.19 91491. 0.6579 2.11 0.0464 0.1214 0.0920 0.0351 0.080 1.682 1.729 59.705 0.190 7.690 13.134 0.19 91557. 0.6333 3.16 0.0696 0.1769 0.0901 0.0354 0.081 1.696 1.693 60.195 0.192 7.531 12.758 0.19 91627. 0.6088 4.22 0.0928 0.2291 0.0880 0.0357 0.081 1.707 1.655 60.598 0.193 7.361 12.388 0.19 91703. 0.5844 5.27 0.1160 0.2779 0.0859 0.0358 0.082 1.716 1.614 60.899 0.194 7.180 12.023 0.19 91784. 0.5602 6.33 0.1392 0.3235 0.0836 0.0360 0.082 1.721 1.571 61.085 0.194 6.987 11.664 0.19 91870. 0.5361 7.38 0.1624 0.3660 0.0811 0.0360 0.082 1.723 1.525 61.140 0.195 6.782 11.312 0.19 91962. 0.5123 8.44 0.1856 0.4055 0.0785 0.0359 0.082 1.720 1.476 61.050 0.194 6.565 10.966 0.19 92060. 0.4886 9.49 0.2088 0.4421 0.0758 0.0358 0.082 1.713 1.424 60.800 0.194 6.335 10.625 0.19 92163. 0.4650 10.54 0.2320 0.4757 0.0729 0.0355 0.081 1.701 1.370 60.375 0.192 6.093 10.291 0.19 92273. 0.4417 11.60 0.2552 0.5065 0.0698 0.0352 0.080 1.684 1.312 59.765 0.190 5.838 9.961 0.19 92388. 0.4185 12.65 0.2784 0.5345 0.0666 0.0347 0.079 1.661 1.253 58.961 0.188 5.571 9.635 0.19 92510. 0.3955 13.71 0.3016 0.5597 0.0633 0.0341 0.078 1.633 1.190 57.960 0.184 5.294 9.314 0.19 92638. 0.3726 14.76 0.3248 0.5821 0.0599 0.0334 0.076 1.599 1.126 56.757 0.181 5.006 8.994 0.19 92773. 0.3499 15.82 0.3480 0.6016 0.0563 0.0326 0.074 1.559 1.059 55.349 0.176 4.709 8.676 0.19 92914. 0.3274 16.87 0.3712 0.6181 0.0527 0.0316 0.072 1.514 0.990 53.732 0.171 4.403 8.357 0.19 93061. 0.3049 17.93 0.3944 0.6314 0.0489 0.0306 0.070 1.462 0.919 51.902 0.165 4.090 8.035 0.19 93215. 0.2825 18.98 0.4176 0.6413 0.0451 0.0293 0.067 1.405 0.847 49.856 0.159 3.768 7.707 0.19 93376. 0.2602 20.03 0.4408 0.6474 0.0411 0.0280 0.064 1.341 0.773 47.591 0.151 3.440 7.371 0.19 93543. 0.2377 21.09 0.4640 0.6491 0.0371 0.0265 0.060 1.271 0.698 45.103 0.144 3.105 7.021 0.19 93717. 0.2151 22.14 0.4872 0.6457 0.0331 0.0250 0.057 1.194 0.622 42.391 0.135 2.765 6.652 0.19 93898. 0.1923 23.20 0.5104 0.6361 0.0289 0.0232 0.053 1.112 0.544 39.453 0.126 2.420 6.254 0.19 94086. 0.1692 24.25 0.5336 0.6184 0.0248 0.0214 0.049 1.022 0.465 36.289 0.116 2.070 5.816 0.19 94281. 0.1455 25.31 0.5568 0.5902 0.0205 0.0194 0.044 0.927 0.386 32.902 0.105 1.716 5.320 0.19 94482. 0.1212 26.36 0.5800 0.5472 0.0163 0.0172 0.039 0.825 0.306 29.294 0.093 1.360 4.735 0.19 94690. 0.0960 27.42 0.6032 0.4822 0.0120 0.0150 0.034 0.718 0.225 25.470 0.081 1.002 4.012 0.19 94905. 0.0698 28.47 0.6264 0.3819 0.0077 0.0126 0.029 0.604 0.145 21.441 0.068 0.643 3.060 0.19 95127. 0.0427 29.53 0.6496 0.2186 0.0034 0.0101 0.023 0.485 0.064 17.215 0.055 0.285 1.689 0.19 95355. 0.0157 30.58 0.6728 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 0.0959 0.0335 0.181 2.851 3.203 134.932 0.322 14.247 10.767 0.25 121904. 0.7067 1.40 0.0231 0.0642 0.0942 0.0339 0.183 2.883 3.148 136.449 0.326 14.003 10.465 0.25 121984. 0.6809 2.80 0.0461 0.1246 0.0924 0.0342 0.185 2.912 3.089 137.827 0.329 13.741 10.166 0.25 122071. 0.6553 4.19 0.0692 0.1816 0.0906 0.0345 0.186 2.938 3.026 139.031 0.332 13.460 9.873 0.25 122165. 0.6298 5.59 0.0923 0.2350 0.0885 0.0348 0.188 2.959 2.959 140.030 0.334 13.160 9.584 0.25 122265. 0.6045 6.99 0.1154 0.2851 0.0864 0.0350 0.189 2.975 2.887 140.791 0.336 12.840 9.300 0.25 122372. 0.5795 8.39 0.1384 0.3318 0.0841 0.0351 0.189 2.985 2.810 141.280 0.337 12.500 9.022 0.25 122487. 0.5546 9.79 0.1615 0.3754 0.0817 0.0351 0.190 2.989 2.729 141.460 0.338 12.137 8.749 0.25 122608. 0.5300 11.19 0.1846 0.4160 0.0791 0.0351 0.189 2.986 2.642 141.297 0.337 11.753 8.482 0.25 122738. 0.5056 12.58 0.2076 0.4535 0.0763 0.0350 0.189 2.974 2.551 140.756 0.336 11.347 8.220 0.25 122875. 0.4815 13.98 0.2307 0.4882 0.0735 0.0347 0.187 2.954 2.455 139.803 0.334 10.918 7.964 0.25 123020. 0.4576 15.38 0.2538 0.5200 0.0704 0.0344 0.186 2.925 2.353 138.409 0.330 10.467 7.712 0.25 123173. 0.4339 16.78 0.2769 0.5491 0.0673 0.0339 0.183 2.886 2.247 136.557 0.326 9.996 7.464 0.25 123334. 0.4104 18.18 0.2999 0.5754 0.0639 0.0333 0.180 2.836 2.137 134.235 0.320 9.505 7.221 0.26 123504. 0.3871 19.58 0.3230 0.5990 0.0605 0.0326 0.176 2.777 2.023 131.433 0.314 8.996 6.980 0.26 123682. 0.3640 20.97 0.3461 0.6198 0.0570 0.0318 0.172 2.708 1.904 128.141 0.306 8.471 6.741 0.26 123868. 0.3411 22.37 0.3692 0.6378 0.0533 0.0309 0.167 2.628 1.783 124.351 0.297 7.930 6.502 0.26 124063. 0.3184 23.77 0.3922 0.6527 0.0496 0.0298 0.161 2.537 1.658 120.053 0.287 7.374 6.263 0.26 124267. 0.2957 25.17 0.4153 0.6644 0.0458 0.0286 0.155 2.435 1.530 115.239 0.275 6.805 6.022 0.26 124479. 0.2731 26.57 0.4384 0.6726 0.0419 0.0273 0.147 2.322 1.399 109.902 0.262 6.224 5.775 0.26 124700. 0.2505 27.97 0.4614 0.6768 0.0379 0.0258 0.140 2.198 1.266 104.032 0.248 5.632 5.520 0.26 124930. 0.2278 29.36 0.4845 0.6762 0.0338 0.0242 0.131 2.063 1.131 97.627 0.233 5.029 5.253 0.26 125169. 0.2048 30.76 0.5076 0.6699 0.0297 0.0225 0.122 1.916 0.993 90.681 0.216 4.417 4.967 0.26 125417. 0.1815 32.16 0.5307 0.6563 0.0255 0.0207 0.112 1.758 0.854 83.195 0.199 3.798 4.655 0.26 125674. 0.1577 33.56 0.5537 0.6329 0.0213 0.0187 0.101 1.588 0.713 75.172 0.179 3.171 4.302 0.26 125940. 0.1332 34.96 0.5768 0.5958 0.0171 0.0165 0.089 1.408 0.571 66.620 0.159 2.540 3.888 0.26 126215. 0.1077 36.36 0.5999 0.5380 0.0128 0.0143 0.077 1.216 0.428 57.550 0.137 1.905 3.376 0.26 126499. 0.0810 37.75 0.6229 0.4463 0.0085 0.0119 0.064 1.014 0.285 47.984 0.115 1.269 2.697 0.26 126792. 0.0528 39.15 0.6460 0.2922 0.0043 0.0094 0.051 0.802 0.142 37.943 0.091 0.633 1.702 0.26 127093. 0.0236 40.55 0.6691 -0.0028 0.0000 0.0068 0.037 0.578 -0.001 27.370 0.065 -0.004 -0.016 0.26 127384. 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 0.0964 0.0330 0.348 4.388 5.033 259.560 0.496 22.388 8.795 0.32 152373. 0.7236 1.75 0.0231 0.0656 0.0948 0.0334 0.352 4.439 4.947 262.600 0.502 22.006 8.545 0.32 152475. 0.6970 3.50 0.0462 0.1273 0.0930 0.0337 0.356 4.486 4.855 265.363 0.507 21.595 8.299 0.32 152584. 0.6706 5.25 0.0693 0.1854 0.0911 0.0340 0.359 4.527 4.756 267.783 0.511 21.156 8.056 0.32 152701. 0.6443 7.00 0.0924 0.2400 0.0891 0.0343 0.362 4.561 4.651 269.798 0.515 20.686 7.818 0.32 152827. 0.6183 8.75 0.1155 0.2910 0.0869 0.0345 0.364 4.587 4.538 271.342 0.518 20.184 7.585 0.32 152961. 0.5925 10.50 0.1386 0.3387 0.0846 0.0346 0.365 4.604 4.417 272.344 0.520 19.649 7.357 0.32 153105. 0.5671 12.25 0.1617 0.3832 0.0822 0.0347 0.366 4.610 4.290 272.736 0.521 19.080 7.134 0.32 153258. 0.5418 14.00 0.1848 0.4245 0.0796 0.0346 0.365 4.606 4.154 272.447 0.520 18.477 6.916 0.32 153420. 0.5169 15.75 0.2079 0.4628 0.0768 0.0345 0.364 4.588 4.010 271.408 0.518 17.838 6.702 0.32 153592. 0.4922 17.50 0.2310 0.4982 0.0739 0.0343 0.361 4.557 3.859 269.551 0.515 17.165 6.493 0.32 153774. 0.4678 19.25 0.2541 0.5308 0.0709 0.0339 0.358 4.510 3.700 266.820 0.510 16.456 6.289 0.32 153966. 0.4436 21.00 0.2772 0.5606 0.0677 0.0335 0.353 4.449 3.533 263.179 0.503 15.715 6.089 0.32 154169. 0.4197 22.75 0.3003 0.5878 0.0643 0.0329 0.347 4.372 3.359 258.603 0.494 14.943 5.892 0.32 154381. 0.3961 24.50 0.3234 0.6122 0.0609 0.0322 0.339 4.278 3.180 253.073 0.483 14.143 5.699 0.32 154605. 0.3726 26.25 0.3465 0.6338 0.0573 0.0313 0.331 4.168 2.994 246.569 0.471 13.316 5.507 0.32 154838. 0.3494 28.00 0.3697 0.6527 0.0537 0.0304 0.321 4.041 2.802 239.074 0.457 12.465 5.316 0.32 155083. 0.3264 29.75 0.3928 0.6687 0.0499 0.0293 0.309 3.898 2.606 230.570 0.440 11.591 5.126 0.32 155338. 0.3035 31.50 0.4159 0.6815 0.0461 0.0281 0.296 3.737 2.405 221.038 0.422 10.696 4.934 0.32 155604. 0.2806 33.25 0.4390 0.6909 0.0421 0.0268 0.282 3.558 2.199 210.463 0.402 9.781 4.739 0.32 155882. 0.2577 35.00 0.4621 0.6965 0.0381 0.0253 0.267 3.361 1.990 198.830 0.380 8.849 4.538 0.32 156170. 0.2348 36.76 0.4852 0.6975 0.0340 0.0237 0.250 3.146 1.776 186.130 0.355 7.901 4.329 0.32 156470. 0.2116 38.51 0.5083 0.6930 0.0299 0.0219 0.231 2.914 1.560 172.355 0.329 6.939 4.105 0.32 156780. 0.1880 40.26 0.5314 0.6814 0.0257 0.0200 0.211 2.663 1.341 157.504 0.301 5.964 3.861 0.32 157102. 0.1640 42.01 0.5545 0.6603 0.0214 0.0180 0.190 2.393 1.119 141.584 0.270 4.978 3.586 0.32 157436. 0.1391 43.76 0.5776 0.6256 0.0172 0.0158 0.167 2.106 0.896 124.610 0.238 3.985 3.261 0.32 157781. 0.1132 45.51 0.6007 0.5699 0.0129 0.0136 0.143 1.802 0.671 106.609 0.204 2.987 2.857 0.32 158137. 0.0859 47.26 0.6238 0.4789 0.0086 0.0111 0.117 1.481 0.447 87.619 0.167 1.986 2.312 0.32 158504. 0.0566 49.01 0.6469 0.3194 0.0042 0.0086 0.091 1.144 0.222 67.688 0.129 0.987 1.487 0.32 158881. 0.0257 50.76 0.6700 -0.0090 -0.0001 0.0059 0.063 0.788 -0.004 46.643 0.089 -0.019 -0.040 0.32 159238. 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 0.0971 0.0328 0.597 6.273 7.297 445.290 0.709 32.458 7.433 0.38 182839. 0.7363 2.10 0.0231 0.0665 0.0954 0.0332 0.604 6.348 7.173 450.656 0.717 31.907 7.220 0.38 182961. 0.7091 4.20 0.0462 0.1292 0.0936 0.0335 0.611 6.417 7.040 455.536 0.725 31.315 7.010 0.38 183092. 0.6821 6.31 0.0694 0.1881 0.0917 0.0338 0.617 6.477 6.898 459.815 0.732 30.681 6.804 0.38 183234. 0.6553 8.41 0.0925 0.2434 0.0897 0.0341 0.621 6.528 6.745 463.383 0.737 30.001 6.602 0.38 183385. 0.6288 10.51 0.1156 0.2951 0.0875 0.0343 0.625 6.566 6.582 466.122 0.742 29.275 6.404 0.38 183547. 0.6026 12.61 0.1387 0.3435 0.0852 0.0344 0.627 6.592 6.408 467.912 0.745 28.502 6.211 0.38 183720. 0.5766 14.71 0.1619 0.3885 0.0828 0.0345 0.628 6.602 6.223 468.630 0.746 27.679 6.023 0.38 183904. 0.5510 16.82 0.1850 0.4305 0.0802 0.0344 0.628 6.595 6.026 468.153 0.745 26.806 5.839 0.38 184100. 0.5256 18.92 0.2081 0.4694 0.0774 0.0343 0.625 6.570 5.819 466.359 0.742 25.881 5.659 0.38 184307. 0.5006 21.02 0.2312 0.5053 0.0745 0.0341 0.621 6.524 5.599 463.130 0.737 24.905 5.484 0.38 184526. 0.4758 23.12 0.2544 0.5385 0.0714 0.0337 0.615 6.457 5.368 458.368 0.730 23.878 5.312 0.38 184758. 0.4514 25.23 0.2775 0.5689 0.0682 0.0333 0.606 6.367 5.127 452.007 0.719 22.803 5.144 0.38 185001. 0.4272 27.33 0.3006 0.5966 0.0648 0.0327 0.595 6.255 4.875 444.003 0.707 21.684 4.980 0.38 185257. 0.4032 29.43 0.3237 0.6217 0.0614 0.0320 0.582 6.118 4.614 434.324 0.691 20.523 4.818 0.38 185526. 0.3796 31.53 0.3468 0.6440 0.0578 0.0311 0.567 5.958 4.344 422.934 0.673 19.323 4.659 0.38 185807. 0.3561 33.63 0.3700 0.6637 0.0541 0.0302 0.550 5.773 4.067 409.803 0.652 18.088 4.501 0.38 186101. 0.3329 35.74 0.3931 0.6804 0.0503 0.0291 0.530 5.563 3.781 394.899 0.629 16.820 4.343 0.38 186408. 0.3097 37.84 0.4162 0.6942 0.0464 0.0278 0.507 5.328 3.489 378.191 0.602 15.521 4.185 0.38 186728. 0.2867 39.94 0.4393 0.7047 0.0424 0.0265 0.482 5.066 3.191 359.651 0.572 14.194 4.025 0.38 187062. 0.2637 42.04 0.4625 0.7114 0.0384 0.0250 0.455 4.779 2.887 339.253 0.540 12.842 3.860 0.38 187409. 0.2405 44.14 0.4856 0.7138 0.0343 0.0233 0.425 4.465 2.578 316.979 0.504 11.465 3.688 0.39 187769. 0.2172 46.25 0.5087 0.7109 0.0301 0.0215 0.393 4.125 2.264 292.818 0.466 10.068 3.506 0.39 188143. 0.1935 48.35 0.5318 0.7011 0.0259 0.0196 0.358 3.758 1.945 266.767 0.425 8.653 3.308 0.39 188530. 0.1692 50.45 0.5550 0.6820 0.0216 0.0176 0.320 3.365 1.624 238.839 0.380 7.223 3.084 0.39 188931. 0.1441 52.55 0.5781 0.6496 0.0173 0.0154 0.280 2.945 1.300 209.059 0.333 5.781 2.820 0.39 189346. 0.1179 54.66 0.6012 0.5963 0.0130 0.0131 0.238 2.500 0.974 177.476 0.282 4.331 2.489 0.39 189774. 0.0901 56.76 0.6243 0.5067 0.0086 0.0106 0.193 2.031 0.647 144.158 0.229 2.879 2.036 0.39 190215. 0.0601 58.86 0.6475 0.3441 0.0043 0.0080 0.146 1.538 0.321 109.190 0.174 1.428 1.333 0.39 190668. 0.0277 60.96 0.6706 -0.0132 -0.0001 0.0053 0.097 1.017 -0.008 72.175 0.115 -0.035 -0.049 0.39 191089. 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 0.0978 0.0327 0.947 8.527 10.013 706.190 0.963 44.537 6.431 0.44 213299. 0.7463 2.45 0.0231 0.0672 0.0962 0.0331 0.959 8.632 9.844 714.884 0.975 43.787 6.246 0.44 213442. 0.7187 4.91 0.0463 0.1305 0.0944 0.0335 0.969 8.727 9.663 722.792 0.986 42.979 6.064 0.44 213596. 0.6912 7.36 0.0694 0.1899 0.0925 0.0338 0.979 8.811 9.468 729.728 0.995 42.113 5.885 0.44 213761. 0.6641 9.82 0.0926 0.2457 0.0905 0.0341 0.986 8.881 9.259 735.511 1.003 41.185 5.710 0.44 213939. 0.6372 12.27 0.1157 0.2980 0.0883 0.0343 0.992 8.935 9.036 739.954 1.009 40.193 5.539 0.44 214129. 0.6106 14.73 0.1388 0.3468 0.0860 0.0344 0.996 8.970 8.798 742.861 1.013 39.134 5.372 0.44 214331. 0.5843 17.18 0.1620 0.3923 0.0835 0.0345 0.998 8.984 8.545 744.035 1.015 38.008 5.209 0.44 214547. 0.5584 19.63 0.1851 0.4347 0.0809 0.0344 0.997 8.975 8.276 743.279 1.014 36.812 5.050 0.45 214776. 0.5328 22.09 0.2083 0.4740 0.0781 0.0343 0.993 8.940 7.991 740.396 1.010 35.545 4.895 0.45 215019. 0.5075 24.54 0.2314 0.5105 0.0751 0.0341 0.986 8.877 7.690 735.195 1.003 34.207 4.744 0.45 215275. 0.4825 27.00 0.2545 0.5441 0.0721 0.0337 0.976 8.785 7.374 727.518 0.992 32.799 4.597 0.45 215546. 0.4578 29.45 0.2777 0.5750 0.0688 0.0332 0.962 8.661 7.042 717.258 0.978 31.324 4.453 0.45 215831. 0.4334 31.90 0.3008 0.6032 0.0654 0.0326 0.945 8.505 6.697 704.345 0.961 29.788 4.313 0.45 216131. 0.4093 34.36 0.3240 0.6288 0.0619 0.0319 0.924 8.316 6.339 688.725 0.940 28.194 4.174 0.45 216445. 0.3854 36.81 0.3471 0.6517 0.0583 0.0311 0.899 8.094 5.968 670.346 0.914 26.547 4.038 0.45 216774. 0.3618 39.27 0.3702 0.6720 0.0546 0.0301 0.871 7.838 5.587 649.156 0.886 24.851 3.904 0.45 217118. 0.3384 41.72 0.3934 0.6895 0.0508 0.0290 0.838 7.548 5.195 625.106 0.853 23.110 3.770 0.45 217478. 0.3151 44.18 0.4165 0.7041 0.0468 0.0277 0.802 7.222 4.794 598.144 0.816 21.326 3.636 0.45 217852. 0.2919 46.63 0.4397 0.7155 0.0428 0.0263 0.762 6.861 4.385 568.227 0.775 19.503 3.500 0.45 218242. 0.2688 49.08 0.4628 0.7232 0.0388 0.0248 0.718 6.464 3.967 535.313 0.730 17.644 3.361 0.45 218648. 0.2455 51.54 0.4859 0.7268 0.0346 0.0231 0.670 6.030 3.542 499.373 0.681 15.753 3.217 0.45 219069. 0.2220 53.99 0.5091 0.7252 0.0304 0.0213 0.617 5.559 3.110 460.388 0.628 13.833 3.064 0.45 219506. 0.1982 56.45 0.5322 0.7171 0.0261 0.0194 0.561 5.051 2.673 418.356 0.571 11.888 2.898 0.45 219958. 0.1737 58.90 0.5554 0.6999 0.0218 0.0173 0.501 4.507 2.231 373.295 0.509 9.922 2.710 0.45 220427. 0.1485 61.36 0.5785 0.6696 0.0174 0.0151 0.436 3.927 1.785 325.249 0.444 7.940 2.489 0.45 220911. 0.1220 63.81 0.6016 0.6185 0.0131 0.0127 0.368 3.312 1.337 274.294 0.374 5.948 2.211 0.45 221412. 0.0938 66.26 0.6248 0.5307 0.0087 0.0102 0.296 2.663 0.888 220.544 0.301 3.951 1.827 0.45 221927. 0.0631 68.72 0.6479 0.3661 0.0043 0.0076 0.220 1.982 0.440 164.135 0.224 1.956 1.215 0.45 222456. 0.0296 71.17 0.6711 -0.0183 -0.0001 0.0048 0.140 1.259 -0.013 104.260 0.142 -0.060 -0.059 0.45 222937. 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 0.0988 0.0328 1.419 11.178 13.203 1057.967 1.263 58.725 5.660 0.51 243752. 0.7542 2.81 0.0232 0.0676 0.0971 0.0333 1.437 11.318 12.982 1071.219 1.279 57.745 5.497 0.51 243916. 0.7263 5.61 0.0463 0.1313 0.0953 0.0336 1.453 11.445 12.745 1083.265 1.293 56.688 5.336 0.51 244093. 0.6986 8.42 0.0695 0.1912 0.0934 0.0340 1.467 11.557 12.489 1093.827 1.306 55.553 5.179 0.51 244283. 0.6712 11.23 0.0926 0.2473 0.0914 0.0342 1.479 11.650 12.216 1102.627 1.316 54.336 5.025 0.51 244487. 0.6441 14.03 0.1158 0.2999 0.0892 0.0344 1.488 11.721 11.923 1109.384 1.324 53.034 4.875 0.51 244705. 0.6173 16.84 0.1389 0.3490 0.0869 0.0346 1.494 11.768 11.611 1113.797 1.329 51.644 4.728 0.51 244937. 0.5908 19.65 0.1621 0.3949 0.0844 0.0346 1.496 11.786 11.278 1115.570 1.332 50.164 4.585 0.51 245185. 0.5647 22.45 0.1852 0.4376 0.0817 0.0346 1.494 11.774 10.924 1114.401 1.330 48.591 4.446 0.51 245448. 0.5389 25.26 0.2084 0.4773 0.0789 0.0345 1.489 11.727 10.549 1109.999 1.325 46.923 4.311 0.51 245726. 0.5135 28.07 0.2315 0.5141 0.0760 0.0342 1.478 11.644 10.153 1102.070 1.315 45.161 4.179 0.51 246021. 0.4883 30.87 0.2547 0.5481 0.0728 0.0338 1.462 11.520 9.736 1090.374 1.302 43.306 4.050 0.51 246331. 0.4634 33.68 0.2778 0.5794 0.0696 0.0334 1.441 11.355 9.299 1074.751 1.283 41.362 3.924 0.51 246658. 0.4389 36.48 0.3010 0.6081 0.0662 0.0328 1.415 11.147 8.844 1055.094 1.259 39.336 3.802 0.51 247002. 0.4146 39.29 0.3242 0.6341 0.0626 0.0320 1.383 10.896 8.371 1031.323 1.231 37.234 3.682 0.51 247362. 0.3906 42.10 0.3473 0.6576 0.0590 0.0311 1.346 10.601 7.882 1003.359 1.198 35.061 3.563 0.51 247740. 0.3669 44.90 0.3705 0.6785 0.0552 0.0301 1.302 10.260 7.379 971.129 1.159 32.823 3.447 0.51 248134. 0.3433 47.71 0.3936 0.6966 0.0513 0.0290 1.253 9.874 6.862 934.558 1.116 30.524 3.331 0.51 248546. 0.3200 50.52 0.4168 0.7119 0.0474 0.0277 1.198 9.441 6.333 893.570 1.067 28.169 3.215 0.51 248975. 0.2967 53.32 0.4399 0.7241 0.0433 0.0263 1.137 8.960 5.792 848.098 1.012 25.762 3.098 0.51 249422. 0.2734 56.13 0.4631 0.7328 0.0392 0.0248 1.070 8.432 5.240 798.081 0.953 23.308 2.978 0.51 249886. 0.2500 58.94 0.4862 0.7375 0.0350 0.0231 0.997 7.855 4.679 743.474 0.887 20.810 2.854 0.51 250368. 0.2264 61.74 0.5094 0.7371 0.0307 0.0212 0.918 7.229 4.108 684.249 0.817 18.274 2.723 0.51 250869. 0.2024 64.55 0.5325 0.7304 0.0264 0.0193 0.832 6.555 3.531 620.404 0.741 15.704 2.581 0.51 251387. 0.1779 67.36 0.5557 0.7150 0.0220 0.0171 0.740 5.832 2.947 551.963 0.659 13.107 2.421 0.52 251923. 0.1524 70.16 0.5788 0.6867 0.0176 0.0149 0.642 5.061 2.358 478.998 0.572 10.487 2.233 0.52 252478. 0.1257 72.97 0.6020 0.6379 0.0132 0.0125 0.539 4.243 1.766 401.622 0.479 7.854 1.994 0.52 253050. 0.0972 75.78 0.6251 0.5520 0.0088 0.0099 0.429 3.381 1.172 320.009 0.382 5.214 1.662 0.52 253640. 0.0660 78.58 0.6483 0.3864 0.0043 0.0073 0.314 2.476 0.580 234.367 0.280 2.578 1.122 0.52 254246. 0.0313 81.39 0.6715 -0.0245 -0.0002 0.0044 0.192 1.513 -0.022 143.167 0.171 -0.097 -0.069 0.52 254780. 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 0.0999 0.0331 2.036 14.262 16.895 1518.592 1.611 75.151 5.046 0.57 274196. 0.7607 3.16 0.0232 0.0679 0.0982 0.0335 2.062 14.443 16.616 1537.892 1.632 73.910 4.901 0.57 274381. 0.7326 6.32 0.0463 0.1318 0.0964 0.0339 2.086 14.608 16.315 1555.426 1.650 72.571 4.758 0.57 274582. 0.7048 9.48 0.0695 0.1919 0.0945 0.0342 2.106 14.752 15.992 1570.789 1.667 71.131 4.618 0.57 274797. 0.6772 12.64 0.0927 0.2482 0.0925 0.0345 2.124 14.872 15.644 1583.573 1.680 69.585 4.481 0.57 275027. 0.6499 15.80 0.1158 0.3010 0.0903 0.0347 2.137 14.964 15.272 1593.364 1.691 67.928 4.347 0.57 275274. 0.6230 18.95 0.1390 0.3504 0.0879 0.0349 2.145 15.024 14.874 1599.736 1.697 66.158 4.217 0.57 275537. 0.5964 22.11 0.1622 0.3965 0.0854 0.0349 2.149 15.047 14.449 1602.257 1.700 64.271 4.090 0.57 275817. 0.5702 25.27 0.1853 0.4395 0.0827 0.0349 2.146 15.031 13.998 1600.493 1.698 62.264 3.967 0.57 276114. 0.5443 28.43 0.2085 0.4795 0.0799 0.0348 2.138 14.970 13.520 1594.015 1.691 60.135 3.847 0.57 276429. 0.5187 31.59 0.2317 0.5166 0.0769 0.0345 2.122 14.861 13.014 1582.411 1.679 57.884 3.730 0.57 276762. 0.4935 34.75 0.2548 0.5509 0.0738 0.0341 2.099 14.701 12.480 1565.330 1.661 55.513 3.616 0.57 277112. 0.4685 37.91 0.2780 0.5826 0.0705 0.0336 2.069 14.487 11.921 1542.535 1.637 53.027 3.505 0.57 277482. 0.4439 41.07 0.3012 0.6116 0.0670 0.0330 2.030 14.217 11.339 1513.872 1.606 50.434 3.397 0.57 277870. 0.4195 44.23 0.3243 0.6381 0.0634 0.0322 1.984 13.892 10.734 1479.237 1.570 47.743 3.291 0.57 278277. 0.3954 47.39 0.3475 0.6621 0.0598 0.0314 1.929 13.510 10.108 1438.517 1.526 44.960 3.187 0.57 278703. 0.3716 50.55 0.3707 0.6835 0.0559 0.0303 1.866 13.069 9.463 1391.610 1.477 42.093 3.084 0.58 279148. 0.3480 53.70 0.3938 0.7022 0.0520 0.0292 1.795 12.570 8.801 1338.410 1.420 39.148 2.983 0.58 279612. 0.3245 56.86 0.4170 0.7182 0.0480 0.0279 1.715 12.010 8.123 1278.811 1.357 36.129 2.881 0.58 280096. 0.3011 60.02 0.4402 0.7311 0.0439 0.0264 1.626 11.389 7.429 1212.717 1.287 33.044 2.779 0.58 280600. 0.2777 63.18 0.4633 0.7407 0.0397 0.0249 1.529 10.707 6.722 1140.041 1.210 29.897 2.674 0.58 281124. 0.2543 66.34 0.4865 0.7464 0.0355 0.0231 1.422 9.962 6.001 1060.719 1.125 26.695 2.566 0.58 281668. 0.2306 69.50 0.5097 0.7472 0.0312 0.0212 1.307 9.154 5.270 974.710 1.034 23.442 2.452 0.58 282232. 0.2065 72.66 0.5328 0.7419 0.0268 0.0192 1.183 8.283 4.529 882.009 0.936 20.145 2.329 0.58 282816. 0.1818 75.82 0.5560 0.7281 0.0223 0.0171 1.050 7.350 3.780 782.659 0.830 16.812 2.190 0.58 283421. 0.1562 78.98 0.5792 0.7017 0.0179 0.0148 0.908 6.356 3.024 676.755 0.718 13.451 2.027 0.58 284045. 0.1293 82.14 0.6023 0.6551 0.0134 0.0123 0.757 5.301 2.264 564.467 0.599 10.071 1.819 0.58 284690. 0.1004 85.29 0.6255 0.5713 0.0089 0.0097 0.598 4.189 1.502 446.049 0.473 6.683 1.528 0.58 285355. 0.0687 88.45 0.6487 0.4052 0.0044 0.0070 0.432 3.022 0.741 321.803 0.341 3.297 1.045 0.58 286037. 0.0330 91.61 0.6718 -0.0328 -0.0002 0.0041 0.253 1.774 -0.034 188.912 0.200 -0.151 -0.082 0.58 286613. 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 0.1012 0.0335 2.829 17.828 21.128 2109.240 2.014 93.978 4.543 0.63 304629. 0.7659 3.51 0.0232 0.0679 0.0995 0.0340 2.865 18.058 20.784 2136.416 2.040 92.448 4.413 0.63 304837. 0.7377 7.02 0.0464 0.1319 0.0977 0.0343 2.898 18.266 20.412 2161.076 2.064 90.794 4.284 0.63 305060. 0.7098 10.54 0.0695 0.1921 0.0958 0.0347 2.927 18.448 20.012 2182.653 2.084 89.012 4.159 0.63 305301. 0.6822 14.05 0.0927 0.2485 0.0938 0.0350 2.951 18.600 19.581 2200.579 2.101 87.096 4.036 0.63 305558. 0.6549 17.56 0.1159 0.3015 0.0915 0.0352 2.969 18.716 19.119 2214.274 2.114 85.041 3.916 0.64 305834. 0.6280 21.07 0.1391 0.3510 0.0892 0.0353 2.981 18.790 18.624 2223.132 2.123 82.841 3.800 0.64 306128. 0.6014 24.58 0.1622 0.3973 0.0866 0.0354 2.986 18.819 18.096 2226.551 2.126 80.493 3.686 0.64 306441. 0.5751 28.10 0.1854 0.4405 0.0840 0.0353 2.982 18.797 17.534 2223.926 2.124 77.993 3.576 0.64 306773. 0.5492 31.61 0.2086 0.4807 0.0811 0.0352 2.970 18.719 16.938 2214.668 2.115 75.339 3.469 0.64 307125. 0.5236 35.12 0.2318 0.5180 0.0781 0.0349 2.948 18.580 16.306 2198.196 2.099 72.530 3.365 0.64 307496. 0.4983 38.63 0.2550 0.5526 0.0749 0.0346 2.915 18.375 15.640 2174.029 2.076 69.569 3.263 0.64 307888. 0.4733 42.14 0.2781 0.5846 0.0715 0.0340 2.872 18.103 14.942 2141.828 2.045 66.462 3.164 0.64 308300. 0.4486 45.65 0.3013 0.6140 0.0681 0.0334 2.818 17.761 14.213 2101.393 2.007 63.220 3.068 0.64 308733. 0.4241 49.17 0.3245 0.6409 0.0644 0.0326 2.753 17.349 13.456 2052.572 1.960 59.853 2.973 0.64 309187. 0.4000 52.68 0.3477 0.6653 0.0607 0.0317 2.676 16.864 12.673 1995.226 1.905 56.370 2.881 0.64 309662. 0.3761 56.19 0.3709 0.6872 0.0568 0.0307 2.587 16.306 11.866 1929.218 1.842 52.781 2.790 0.64 310159. 0.3524 59.70 0.3940 0.7065 0.0528 0.0295 2.487 15.674 11.037 1854.405 1.771 49.092 2.700 0.64 310677. 0.3289 63.21 0.4172 0.7232 0.0488 0.0281 2.374 14.966 10.187 1770.645 1.691 45.311 2.609 0.64 311216. 0.3054 66.73 0.4404 0.7368 0.0446 0.0267 2.250 14.181 9.318 1677.807 1.602 41.445 2.519 0.64 311778. 0.2820 70.24 0.4636 0.7473 0.0404 0.0250 2.113 13.319 8.431 1575.771 1.505 37.501 2.427 0.64 312361. 0.2584 73.75 0.4867 0.7539 0.0360 0.0233 1.964 12.378 7.528 1464.449 1.398 33.486 2.332 0.64 312967. 0.2346 77.26 0.5099 0.7558 0.0317 0.0214 1.802 11.358 6.611 1343.786 1.283 29.407 2.232 0.64 313595. 0.2104 80.77 0.5331 0.7518 0.0272 0.0193 1.628 10.259 5.682 1213.777 1.159 25.273 2.123 0.64 314246. 0.1856 84.29 0.5563 0.7396 0.0227 0.0171 1.441 9.082 4.742 1074.477 1.026 21.091 2.002 0.64 314918. 0.1598 87.80 0.5795 0.7152 0.0182 0.0147 1.242 7.827 3.793 926.024 0.884 16.873 1.858 0.65 315614. 0.1327 91.31 0.6026 0.6707 0.0136 0.0122 1.031 6.497 2.840 768.655 0.734 12.631 1.676 0.65 316331. 0.1035 94.82 0.6258 0.5891 0.0090 0.0096 0.808 5.094 1.883 602.728 0.576 8.377 1.417 0.65 317071. 0.0713 98.33 0.6490 0.4231 0.0044 0.0068 0.575 3.623 0.928 428.667 0.409 4.126 0.981 0.65 317829. 0.0347 101.84 0.6722 -0.0443 -0.0003 0.0038 0.324 2.039 -0.053 241.238 0.230 -0.235 -0.099 0.65 318424. 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 0.1027 0.0341 3.834 21.971 25.947 2859.326 2.482 115.414 4.116 0.70 335049. 0.7689 3.86 0.0232 0.0678 0.1010 0.0346 3.883 22.250 25.533 2895.618 2.514 113.571 3.999 0.70 335278. 0.7411 7.73 0.0464 0.1316 0.0993 0.0350 3.927 22.503 25.084 2928.620 2.542 111.573 3.885 0.70 335526. 0.7135 11.59 0.0696 0.1918 0.0973 0.0353 3.966 22.725 24.599 2957.536 2.567 109.415 3.772 0.70 335792. 0.6862 15.46 0.0928 0.2482 0.0953 0.0356 3.998 22.910 24.076 2981.584 2.588 107.089 3.662 0.70 336077. 0.6590 19.32 0.1159 0.3012 0.0930 0.0358 4.023 23.051 23.514 2999.932 2.604 104.589 3.555 0.70 336383. 0.6322 23.19 0.1391 0.3508 0.0907 0.0360 4.039 23.142 22.911 3011.725 2.615 101.910 3.450 0.70 336708. 0.6057 27.05 0.1623 0.3972 0.0881 0.0360 4.045 23.175 22.267 3016.107 2.618 99.045 3.349 0.70 337055. 0.5795 30.92 0.1855 0.4405 0.0854 0.0360 4.039 23.145 21.581 3012.223 2.615 95.990 3.250 0.70 337422. 0.5536 34.78 0.2087 0.4808 0.0825 0.0358 4.022 23.046 20.851 2999.242 2.604 92.744 3.153 0.70 337812. 0.5280 38.65 0.2319 0.5184 0.0794 0.0355 3.991 22.870 20.077 2976.387 2.584 89.304 3.060 0.70 338223. 0.5028 42.51 0.2551 0.5533 0.0762 0.0351 3.947 22.613 19.261 2942.983 2.555 85.673 2.968 0.70 338657. 0.4778 46.38 0.2783 0.5856 0.0728 0.0346 3.887 22.272 18.404 2898.586 2.516 81.861 2.880 0.70 339113. 0.4531 50.24 0.3015 0.6153 0.0693 0.0339 3.812 21.845 17.509 2842.930 2.468 77.880 2.793 0.70 339591. 0.4287 54.11 0.3247 0.6426 0.0656 0.0331 3.722 21.329 16.579 2775.822 2.410 73.743 2.709 0.70 340093. 0.4045 57.97 0.3478 0.6675 0.0618 0.0322 3.617 20.724 15.616 2697.088 2.341 69.461 2.626 0.70 340618. 0.3806 61.84 0.3710 0.6899 0.0579 0.0311 3.495 20.028 14.624 2606.556 2.263 65.046 2.545 0.70 341166. 0.3569 65.70 0.3942 0.7098 0.0538 0.0299 3.358 19.241 13.603 2504.047 2.174 60.507 2.464 0.70 341738. 0.3333 69.57 0.4174 0.7270 0.0497 0.0285 3.204 18.360 12.557 2389.374 2.074 55.854 2.384 0.70 342334. 0.3098 73.43 0.4406 0.7414 0.0455 0.0270 3.034 17.384 11.487 2262.366 1.964 51.095 2.303 0.70 342954. 0.2862 77.30 0.4638 0.7527 0.0411 0.0253 2.847 16.312 10.395 2122.858 1.843 46.237 2.221 0.71 343597. 0.2626 81.16 0.4870 0.7602 0.0367 0.0235 2.643 15.143 9.283 1970.732 1.711 41.291 2.137 0.71 344265. 0.2387 85.03 0.5102 0.7633 0.0323 0.0216 2.422 13.876 8.153 1805.921 1.568 36.265 2.048 0.71 344958. 0.2144 88.89 0.5334 0.7606 0.0277 0.0194 2.184 12.513 7.007 1628.423 1.414 31.168 1.952 0.71 345675. 0.1895 92.76 0.5566 0.7499 0.0231 0.0172 1.929 11.052 5.848 1438.340 1.249 26.012 1.844 0.71 346417. 0.1635 96.62 0.5797 0.7273 0.0185 0.0148 1.657 9.496 4.678 1235.900 1.073 20.809 1.717 0.71 347183. 0.1362 100.49 0.6029 0.6849 0.0139 0.0122 1.370 7.849 3.501 1021.492 0.887 15.574 1.555 0.71 347974. 0.1067 104.35 0.6261 0.6052 0.0092 0.0095 1.067 6.114 2.321 795.706 0.691 10.323 1.323 0.71 348788. 0.0739 108.22 0.6493 0.4390 0.0045 0.0067 0.750 4.297 1.141 559.268 0.486 5.074 0.925 0.71 349623. 0.0362 112.08 0.6725 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 0.1044 0.0355 5.177 27.194 31.409 3860.830 3.072 139.708 3.690 0.76 365451. 0.7584 4.22 0.0232 0.0666 0.1028 0.0359 5.232 27.478 30.920 3901.133 3.104 137.533 3.595 0.76 365703. 0.7331 8.45 0.0465 0.1296 0.1010 0.0362 5.280 27.732 30.388 3937.241 3.133 135.166 3.501 0.76 365975. 0.7077 12.67 0.0697 0.1893 0.0991 0.0365 5.321 27.950 29.811 3968.212 3.158 132.600 3.407 0.76 366268. 0.6823 16.89 0.0929 0.2455 0.0971 0.0367 5.355 28.126 29.188 3993.113 3.178 129.827 3.315 0.76 366582. 0.6569 21.12 0.1161 0.2985 0.0948 0.0369 5.379 28.251 28.516 4010.941 3.192 126.837 3.225 0.76 366918. 0.6315 25.34 0.1394 0.3483 0.0924 0.0370 5.392 28.319 27.793 4020.637 3.200 123.625 3.135 0.76 367277. 0.6062 29.56 0.1626 0.3950 0.0898 0.0370 5.392 28.323 27.019 4021.108 3.200 120.182 3.048 0.76 367658. 0.5810 33.79 0.1858 0.4387 0.0871 0.0369 5.379 28.253 26.193 4011.232 3.192 116.505 2.962 0.76 368063. 0.5559 38.01 0.2091 0.4795 0.0842 0.0367 5.351 28.103 25.312 3989.890 3.175 112.590 2.878 0.76 368492. 0.5309 42.23 0.2323 0.5175 0.0811 0.0364 5.305 27.864 24.378 3955.991 3.148 108.434 2.795 0.76 368944. 0.5061 46.46 0.2555 0.5528 0.0778 0.0359 5.241 27.530 23.391 3908.550 3.110 104.042 2.714 0.76 369421. 0.4814 50.68 0.2787 0.5855 0.0743 0.0354 5.159 27.096 22.352 3846.886 3.061 99.424 2.635 0.76 369923. 0.4569 54.90 0.3020 0.6158 0.0707 0.0347 5.056 26.558 21.267 3770.555 3.001 94.596 2.558 0.77 370449. 0.4327 59.13 0.3252 0.6435 0.0670 0.0338 4.934 25.915 20.138 3679.205 2.928 89.576 2.483 0.77 371001. 0.4086 63.35 0.3484 0.6688 0.0631 0.0329 4.791 25.163 18.969 3572.519 2.843 84.376 2.408 0.77 371578. 0.3847 67.57 0.3716 0.6918 0.0591 0.0317 4.627 24.302 17.763 3450.197 2.746 79.011 2.335 0.77 372180. 0.3609 71.80 0.3949 0.7122 0.0549 0.0305 4.441 23.328 16.523 3311.951 2.636 73.494 2.263 0.77 372808. 0.3373 76.02 0.4181 0.7301 0.0507 0.0290 4.234 22.240 15.251 3157.546 2.513 67.835 2.191 0.77 373462. 0.3137 80.24 0.4413 0.7452 0.0464 0.0275 4.005 21.038 13.949 2986.795 2.377 62.045 2.118 0.77 374141. 0.2901 84.46 0.4646 0.7571 0.0420 0.0257 3.754 19.719 12.620 2799.552 2.228 56.134 2.045 0.77 374848. 0.2664 88.69 0.4878 0.7654 0.0375 0.0239 3.481 18.283 11.266 2595.746 2.066 50.112 1.969 0.77 375580. 0.2423 92.91 0.5110 0.7692 0.0329 0.0218 3.186 16.731 9.890 2375.429 1.890 43.990 1.888 0.77 376339. 0.2178 97.13 0.5342 0.7670 0.0282 0.0197 2.868 15.065 8.494 2138.816 1.702 37.780 1.801 0.77 377125. 0.1925 101.36 0.5575 0.7565 0.0235 0.0173 2.530 13.286 7.080 1886.305 1.501 31.494 1.703 0.77 377938. 0.1661 105.58 0.5807 0.7334 0.0188 0.0149 2.170 11.400 5.654 1618.528 1.288 25.148 1.584 0.77 378777. 0.1382 109.80 0.6039 0.6890 0.0140 0.0123 1.792 9.413 4.217 1336.392 1.063 18.759 1.431 0.78 379643. 0.1078 114.03 0.6272 0.6045 0.0092 0.0096 1.396 7.333 2.776 1041.124 0.829 12.347 1.209 0.78 380535. 0.0739 118.25 0.6504 0.4273 0.0044 0.0068 0.985 5.171 1.334 734.162 0.584 5.934 0.824 0.78 381448. 0.0349 122.47 0.6736 PROP RPM = 13000 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 0.0389 7.210 34.958 37.569 5376.739 3.950 167.106 3.169 0.83 395829. 0.7124 4.58 0.0232 0.0623 0.1048 0.0391 7.249 35.144 37.007 5405.387 3.971 164.605 3.105 0.83 396104. 0.6928 9.15 0.0465 0.1220 0.1031 0.0393 7.279 35.289 36.391 5427.696 3.987 161.868 3.041 0.83 396401. 0.6728 13.73 0.0697 0.1791 0.1012 0.0394 7.299 35.388 35.721 5442.786 3.998 158.886 2.977 0.83 396720. 0.6525 18.30 0.0929 0.2337 0.0991 0.0394 7.308 35.433 34.993 5449.763 4.003 155.649 2.912 0.83 397064. 0.6318 22.88 0.1162 0.2856 0.0969 0.0394 7.305 35.419 34.205 5447.661 4.002 152.145 2.848 0.83 397431. 0.6108 27.45 0.1394 0.3350 0.0945 0.0393 7.289 35.340 33.356 5435.443 3.993 148.367 2.783 0.83 397822. 0.5895 32.03 0.1626 0.3818 0.0919 0.0391 7.258 35.188 32.443 5412.025 3.975 144.306 2.719 0.83 398239. 0.5679 36.61 0.1858 0.4260 0.0891 0.0389 7.210 34.955 31.465 5376.249 3.949 139.957 2.655 0.83 398681. 0.5461 41.18 0.2091 0.4676 0.0862 0.0385 7.143 34.634 30.422 5326.886 3.913 135.316 2.590 0.83 399149. 0.5240 45.76 0.2323 0.5068 0.0830 0.0381 7.057 34.216 29.312 5262.667 3.866 130.380 2.526 0.83 399644. 0.5016 50.33 0.2555 0.5434 0.0797 0.0375 6.950 33.695 28.137 5182.400 3.807 125.151 2.463 0.83 400164. 0.4790 54.91 0.2788 0.5775 0.0762 0.0368 6.819 33.063 26.899 5085.274 3.735 119.645 2.399 0.83 400712. 0.4563 59.48 0.3020 0.6092 0.0725 0.0360 6.666 32.319 25.602 4970.790 3.651 113.878 2.336 0.83 401286. 0.4335 64.06 0.3252 0.6384 0.0687 0.0350 6.489 31.459 24.252 4838.568 3.554 107.872 2.273 0.83 401887. 0.4106 68.64 0.3485 0.6652 0.0647 0.0339 6.287 30.481 22.852 4688.203 3.444 101.646 2.211 0.83 402515. 0.3876 73.21 0.3717 0.6896 0.0606 0.0327 6.060 29.383 21.407 4519.236 3.320 95.217 2.148 0.83 403171. 0.3645 77.79 0.3949 0.7113 0.0564 0.0313 5.809 28.163 19.919 4331.571 3.182 88.599 2.086 0.83 403855. 0.3414 82.36 0.4181 0.7301 0.0521 0.0298 5.532 26.823 18.392 4125.527 3.030 81.806 2.022 0.83 404566. 0.3180 86.94 0.4414 0.7458 0.0477 0.0282 5.231 25.361 16.828 3900.636 2.865 74.851 1.957 0.83 405306. 0.2944 91.51 0.4646 0.7578 0.0432 0.0265 4.905 23.779 15.231 3657.389 2.687 67.747 1.889 0.83 406073. 0.2703 96.09 0.4878 0.7656 0.0385 0.0246 4.553 22.073 13.603 3394.986 2.494 60.505 1.817 0.83 406870. 0.2458 100.66 0.5111 0.7681 0.0338 0.0225 4.175 20.242 11.947 3113.378 2.287 53.139 1.740 0.84 407694. 0.2206 105.24 0.5343 0.7636 0.0291 0.0204 3.773 18.292 10.266 2813.437 2.067 45.661 1.655 0.84 408548. 0.1945 109.82 0.5575 0.7490 0.0243 0.0181 3.348 16.231 8.563 2496.478 1.834 38.087 1.556 0.84 409430. 0.1669 114.39 0.5808 0.7192 0.0194 0.0157 2.902 14.069 6.842 2163.949 1.590 30.435 1.434 0.84 410340. 0.1376 118.97 0.6040 0.6649 0.0145 0.0131 2.438 11.819 5.109 1817.786 1.335 22.725 1.275 0.84 411280. 0.1057 123.54 0.6272 0.5666 0.0095 0.0106 1.958 9.495 3.369 1460.372 1.073 14.983 1.046 0.84 412247. 0.0704 128.12 0.6504 0.3787 0.0046 0.0079 1.467 7.114 1.626 1094.234 0.804 7.234 0.674 0.84 413238. 0.0315 132.69 0.6737 PROP RPM = 14000 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 0.1082 0.0453 10.492 47.234 44.282 7823.703 5.336 196.967 2.567 0.89 426200. 0.6265 4.98 0.0235 0.0552 0.1067 0.0454 10.501 47.274 43.665 7830.284 5.341 194.223 2.529 0.89 426497. 0.6129 9.96 0.0469 0.1088 0.1050 0.0453 10.491 47.233 42.981 7823.509 5.336 191.180 2.492 0.89 426820. 0.5991 14.93 0.0704 0.1607 0.1032 0.0452 10.464 47.108 42.228 7802.794 5.322 187.829 2.455 0.89 427168. 0.5850 19.91 0.0939 0.2111 0.1011 0.0450 10.416 46.894 41.401 7767.342 5.298 184.152 2.418 0.89 427543. 0.5705 24.89 0.1173 0.2598 0.0989 0.0447 10.348 46.586 40.498 7716.390 5.263 180.136 2.380 0.89 427946. 0.5556 29.87 0.1408 0.3068 0.0965 0.0443 10.258 46.180 39.516 7649.173 5.217 175.768 2.343 0.89 428376. 0.5402 34.85 0.1643 0.3522 0.0939 0.0438 10.145 45.672 38.453 7565.004 5.160 171.039 2.305 0.89 428834. 0.5243 39.83 0.1878 0.3959 0.0911 0.0432 10.008 45.058 37.307 7463.243 5.091 165.941 2.267 0.89 429321. 0.5079 44.80 0.2112 0.4377 0.0881 0.0425 9.848 44.334 36.077 7343.288 5.009 160.472 2.228 0.89 429836. 0.4909 49.78 0.2347 0.4777 0.0849 0.0417 9.661 43.496 34.764 7204.448 4.914 154.630 2.189 0.89 430381. 0.4732 54.76 0.2582 0.5157 0.0815 0.0408 9.449 42.539 33.368 7046.037 4.806 148.421 2.148 0.89 430955. 0.4550 59.74 0.2816 0.5517 0.0779 0.0398 9.210 41.463 31.894 6867.706 4.684 141.863 2.106 0.89 431558. 0.4362 64.72 0.3051 0.5855 0.0741 0.0386 8.944 40.265 30.346 6669.332 4.549 134.980 2.064 0.89 432191. 0.4169 69.70 0.3286 0.6173 0.0702 0.0374 8.651 38.945 28.732 6450.789 4.400 127.798 2.020 0.89 432854. 0.3971 74.67 0.3520 0.6467 0.0661 0.0360 8.330 37.502 27.055 6211.768 4.237 120.340 1.975 0.89 433546. 0.3768 79.65 0.3755 0.6738 0.0619 0.0345 7.981 35.932 25.321 5951.691 4.060 112.626 1.930 0.89 434269. 0.3561 84.63 0.3990 0.6984 0.0575 0.0328 7.604 34.232 23.533 5670.018 3.867 104.675 1.883 0.90 435022. 0.3349 89.61 0.4224 0.7199 0.0530 0.0311 7.201 32.421 21.696 5370.139 3.663 96.504 1.832 0.90 435805. 0.3130 94.59 0.4459 0.7373 0.0484 0.0293 6.778 30.514 19.813 5054.226 3.447 88.128 1.778 0.90 436619. 0.2902 99.57 0.4694 0.7494 0.0437 0.0274 6.337 28.531 17.887 4725.760 3.223 79.562 1.717 0.90 437464. 0.2663 104.54 0.4928 0.7519 0.0389 0.0255 5.902 26.571 15.920 4401.198 3.002 70.811 1.641 0.90 438340. 0.2401 109.52 0.5163 0.7467 0.0340 0.0235 5.443 24.506 13.918 4059.050 2.769 61.907 1.555 0.90 439247. 0.2128 114.50 0.5398 0.7312 0.0290 0.0214 4.963 22.344 11.886 3700.935 2.524 52.868 1.457 0.90 440185. 0.1842 119.48 0.5633 0.7012 0.0240 0.0193 4.465 20.103 9.828 3329.709 2.271 43.716 1.339 0.90 441154. 0.1539 124.46 0.5867 0.6505 0.0189 0.0171 3.954 17.801 7.750 2948.503 2.011 34.473 1.192 0.90 442155. 0.1217 129.44 0.6102 0.5688 0.0138 0.0148 3.434 15.459 5.659 2560.572 1.747 25.172 1.002 0.91 443186. 0.0875 134.41 0.6337 0.4390 0.0087 0.0126 2.910 13.099 3.564 2169.715 1.480 15.852 0.745 0.91 444248. 0.0516 139.39 0.6571 0.2294 0.0036 0.0103 2.386 10.741 1.472 1779.034 1.213 6.549 0.375 0.91 445333. 0.0167 144.37 0.6806