17x10N (17x10N.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 0.0913 0.0395 0.005 0.285 0.243 3.368 0.032 1.081 32.722 0.07 29236. 0.5567 0.42 0.0263 0.0590 0.0901 0.0401 0.005 0.289 0.240 3.416 0.033 1.067 31.849 0.07 29256. 0.5384 0.85 0.0525 0.1148 0.0888 0.0406 0.005 0.293 0.236 3.462 0.033 1.052 30.974 0.07 29278. 0.5198 1.27 0.0788 0.1673 0.0874 0.0411 0.005 0.296 0.233 3.506 0.033 1.035 30.099 0.07 29302. 0.5011 1.69 0.1050 0.2166 0.0859 0.0416 0.005 0.300 0.229 3.546 0.034 1.016 29.227 0.07 29328. 0.4822 2.11 0.1313 0.2627 0.0841 0.0420 0.005 0.303 0.224 3.582 0.034 0.996 28.361 0.07 29357. 0.4633 2.54 0.1575 0.3057 0.0823 0.0424 0.005 0.305 0.219 3.612 0.034 0.974 27.503 0.07 29389. 0.4443 2.96 0.1838 0.3457 0.0803 0.0427 0.005 0.307 0.214 3.636 0.035 0.950 26.654 0.07 29422. 0.4253 3.38 0.2100 0.3826 0.0781 0.0429 0.005 0.309 0.208 3.652 0.035 0.925 25.815 0.07 29459. 0.4062 3.80 0.2363 0.4166 0.0757 0.0429 0.005 0.309 0.202 3.659 0.035 0.897 24.986 0.07 29498. 0.3872 4.23 0.2625 0.4477 0.0732 0.0429 0.005 0.309 0.195 3.657 0.035 0.867 24.167 0.07 29539. 0.3682 4.65 0.2888 0.4760 0.0705 0.0428 0.005 0.308 0.188 3.643 0.035 0.834 23.356 0.07 29584. 0.3491 5.07 0.3150 0.5014 0.0676 0.0425 0.005 0.306 0.180 3.617 0.035 0.800 22.553 0.07 29631. 0.3301 5.49 0.3413 0.5239 0.0645 0.0420 0.005 0.302 0.172 3.578 0.034 0.763 21.754 0.07 29681. 0.3111 5.92 0.3675 0.5436 0.0612 0.0414 0.005 0.298 0.163 3.526 0.034 0.725 20.956 0.07 29733. 0.2920 6.34 0.3938 0.5602 0.0578 0.0406 0.005 0.292 0.154 3.460 0.033 0.684 20.157 0.07 29789. 0.2728 6.76 0.4200 0.5736 0.0542 0.0397 0.005 0.286 0.144 3.381 0.032 0.642 19.352 0.07 29848. 0.2537 7.18 0.4463 0.5838 0.0505 0.0386 0.004 0.278 0.134 3.287 0.031 0.597 18.535 0.07 29909. 0.2345 7.61 0.4725 0.5902 0.0466 0.0373 0.004 0.269 0.124 3.181 0.030 0.552 17.699 0.07 29973. 0.2152 8.03 0.4988 0.5927 0.0427 0.0359 0.004 0.259 0.114 3.061 0.029 0.505 16.837 0.07 30040. 0.1959 8.45 0.5250 0.5905 0.0387 0.0344 0.004 0.248 0.103 2.928 0.028 0.458 15.937 0.07 30110. 0.1764 8.87 0.5513 0.5830 0.0345 0.0327 0.004 0.235 0.092 2.783 0.027 0.409 14.986 0.07 30183. 0.1568 9.30 0.5775 0.5692 0.0304 0.0308 0.004 0.222 0.081 2.624 0.025 0.359 13.965 0.07 30259. 0.1370 9.72 0.6038 0.5475 0.0261 0.0288 0.003 0.207 0.070 2.454 0.023 0.309 12.850 0.07 30337. 0.1169 10.14 0.6300 0.5160 0.0218 0.0266 0.003 0.192 0.058 2.270 0.022 0.258 11.604 0.07 30419. 0.0965 10.57 0.6563 0.4714 0.0175 0.0244 0.003 0.175 0.047 2.075 0.020 0.207 10.177 0.07 30503. 0.0758 10.99 0.6825 0.4089 0.0131 0.0219 0.003 0.158 0.035 1.868 0.018 0.156 8.490 0.07 30590. 0.0548 11.41 0.7088 0.3210 0.0088 0.0194 0.002 0.139 0.023 1.650 0.016 0.104 6.418 0.07 30680. 0.0338 11.83 0.7350 0.1944 0.0044 0.0167 0.002 0.120 0.012 1.421 0.014 0.052 3.747 0.07 30773. 0.0140 12.26 0.7613 0.0042 0.0001 0.0139 0.002 0.100 0.000 1.183 0.011 0.001 0.079 0.07 30869. 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 0.0917 0.0352 0.032 1.014 0.976 23.984 0.115 4.343 18.466 0.13 58471. 0.6298 0.85 0.0264 0.0669 0.0905 0.0358 0.033 1.031 0.964 24.400 0.117 4.288 17.920 0.13 58511. 0.6073 1.70 0.0529 0.1297 0.0893 0.0364 0.033 1.048 0.950 24.805 0.118 4.227 17.376 0.13 58556. 0.5847 2.55 0.0793 0.1885 0.0878 0.0370 0.034 1.065 0.935 25.192 0.120 4.160 16.838 0.13 58604. 0.5620 3.40 0.1057 0.2433 0.0863 0.0375 0.034 1.080 0.919 25.552 0.122 4.086 16.306 0.13 58658. 0.5394 4.26 0.1322 0.2944 0.0846 0.0380 0.035 1.094 0.900 25.878 0.124 4.005 15.783 0.13 58716. 0.5170 5.11 0.1586 0.3418 0.0827 0.0384 0.035 1.106 0.881 26.160 0.125 3.917 15.270 0.14 58779. 0.4946 5.96 0.1850 0.3857 0.0807 0.0387 0.035 1.115 0.859 26.388 0.126 3.821 14.767 0.14 58847. 0.4724 6.81 0.2115 0.4261 0.0785 0.0390 0.036 1.122 0.836 26.554 0.127 3.717 14.275 0.14 58921. 0.4504 7.66 0.2379 0.4632 0.0761 0.0391 0.036 1.126 0.810 26.647 0.127 3.605 13.795 0.14 59000. 0.4286 8.51 0.2643 0.4971 0.0736 0.0391 0.036 1.127 0.783 26.658 0.127 3.484 13.325 0.14 59084. 0.4070 9.36 0.2907 0.5280 0.0708 0.0390 0.036 1.123 0.754 26.578 0.127 3.353 12.866 0.14 59174. 0.3856 10.21 0.3172 0.5559 0.0679 0.0387 0.035 1.116 0.723 26.398 0.126 3.214 12.417 0.14 59269. 0.3643 11.06 0.3436 0.5809 0.0648 0.0383 0.035 1.103 0.689 26.111 0.125 3.067 11.976 0.14 59370. 0.3432 11.91 0.3700 0.6029 0.0615 0.0377 0.034 1.087 0.654 25.710 0.123 2.910 11.542 0.14 59477. 0.3222 12.77 0.3965 0.6220 0.0580 0.0370 0.034 1.065 0.617 25.193 0.120 2.746 11.114 0.14 59590. 0.3014 13.62 0.4229 0.6380 0.0544 0.0360 0.033 1.038 0.579 24.559 0.117 2.574 10.688 0.14 59708. 0.2806 14.47 0.4493 0.6509 0.0506 0.0349 0.032 1.006 0.539 23.809 0.114 2.396 10.263 0.14 59832. 0.2600 15.32 0.4758 0.6604 0.0467 0.0337 0.031 0.970 0.497 22.945 0.110 2.213 9.834 0.14 59962. 0.2394 16.17 0.5022 0.6661 0.0427 0.0322 0.029 0.928 0.455 21.967 0.105 2.024 9.397 0.14 60098. 0.2188 17.02 0.5286 0.6676 0.0387 0.0306 0.028 0.882 0.412 20.877 0.100 1.832 8.948 0.14 60240. 0.1982 17.87 0.5551 0.6642 0.0345 0.0289 0.026 0.831 0.368 19.675 0.094 1.636 8.477 0.14 60387. 0.1774 18.72 0.5815 0.6546 0.0303 0.0269 0.025 0.776 0.323 18.361 0.088 1.436 7.976 0.14 60541. 0.1564 19.57 0.6079 0.6375 0.0261 0.0248 0.023 0.716 0.277 16.938 0.081 1.234 7.429 0.14 60700. 0.1351 20.42 0.6344 0.6102 0.0217 0.0226 0.021 0.651 0.231 15.407 0.074 1.030 6.815 0.14 60865. 0.1132 21.28 0.6608 0.5690 0.0174 0.0202 0.018 0.582 0.185 13.770 0.066 0.824 6.101 0.14 61036. 0.0906 22.13 0.6872 0.5073 0.0130 0.0177 0.016 0.508 0.139 12.031 0.057 0.617 5.230 0.14 61212. 0.0672 22.98 0.7137 0.4131 0.0087 0.0150 0.014 0.431 0.092 10.195 0.049 0.410 4.101 0.14 61395. 0.0430 23.83 0.7401 0.2624 0.0043 0.0121 0.011 0.349 0.046 8.270 0.039 0.204 2.511 0.14 61583. 0.0185 24.68 0.7665 -0.0022 0.0000 0.0092 0.008 0.265 0.000 6.261 0.030 -0.001 -0.021 0.14 61775. 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 0.0921 0.0335 0.103 2.169 2.206 76.986 0.245 9.811 12.995 0.20 87704. 0.6661 1.28 0.0265 0.0706 0.0909 0.0341 0.105 2.210 2.178 78.443 0.250 9.687 12.592 0.20 87765. 0.6414 2.56 0.0530 0.1368 0.0896 0.0347 0.107 2.250 2.147 79.867 0.254 9.550 12.194 0.20 87832. 0.6167 3.84 0.0795 0.1985 0.0882 0.0353 0.109 2.289 2.113 81.231 0.259 9.400 11.800 0.20 87906. 0.5921 5.12 0.1060 0.2560 0.0867 0.0359 0.111 2.325 2.076 82.508 0.263 9.235 11.413 0.20 87986. 0.5676 6.40 0.1324 0.3094 0.0850 0.0364 0.112 2.357 2.035 83.667 0.266 9.053 11.034 0.20 88073. 0.5433 7.68 0.1589 0.3588 0.0831 0.0368 0.114 2.386 1.991 84.678 0.270 8.855 10.664 0.20 88169. 0.5193 8.96 0.1854 0.4045 0.0811 0.0372 0.115 2.409 1.942 85.508 0.272 8.639 10.303 0.20 88271. 0.4956 10.23 0.2119 0.4465 0.0789 0.0374 0.115 2.426 1.890 86.123 0.274 8.405 9.951 0.20 88382. 0.4722 11.51 0.2384 0.4851 0.0765 0.0376 0.116 2.437 1.832 86.491 0.275 8.151 9.610 0.20 88501. 0.4490 12.79 0.2649 0.5203 0.0739 0.0376 0.116 2.439 1.771 86.577 0.276 7.877 9.278 0.20 88628. 0.4262 14.07 0.2914 0.5525 0.0712 0.0375 0.116 2.433 1.705 86.351 0.275 7.583 8.955 0.20 88763. 0.4036 15.35 0.3179 0.5816 0.0682 0.0373 0.115 2.417 1.634 85.782 0.273 7.269 8.641 0.20 88907. 0.3813 16.63 0.3444 0.6077 0.0651 0.0369 0.114 2.390 1.559 84.843 0.270 6.935 8.335 0.20 89059. 0.3592 17.91 0.3708 0.6310 0.0618 0.0363 0.112 2.353 1.480 83.512 0.266 6.581 8.036 0.20 89220. 0.3374 19.19 0.3973 0.6513 0.0583 0.0355 0.110 2.304 1.396 81.778 0.260 6.209 7.742 0.20 89390. 0.3157 20.47 0.4238 0.6688 0.0546 0.0346 0.107 2.244 1.309 79.638 0.253 5.821 7.453 0.20 89568. 0.2943 21.75 0.4503 0.6833 0.0509 0.0335 0.103 2.172 1.218 77.097 0.245 5.418 7.166 0.20 89755. 0.2730 23.03 0.4768 0.6945 0.0470 0.0322 0.099 2.089 1.125 74.157 0.236 5.003 6.880 0.20 89951. 0.2518 24.31 0.5033 0.7023 0.0430 0.0308 0.095 1.995 1.029 70.821 0.225 4.577 6.591 0.20 90155. 0.2308 25.59 0.5298 0.7061 0.0389 0.0292 0.090 1.890 0.931 67.092 0.214 4.142 6.295 0.21 90369. 0.2097 26.87 0.5563 0.7053 0.0347 0.0274 0.084 1.774 0.831 62.971 0.200 3.698 5.988 0.21 90591. 0.1885 28.14 0.5828 0.6988 0.0305 0.0254 0.078 1.647 0.730 58.462 0.186 3.247 5.664 0.21 90822. 0.1670 29.42 0.6092 0.6852 0.0262 0.0233 0.072 1.509 0.627 53.567 0.171 2.790 5.312 0.21 91062. 0.1452 30.70 0.6357 0.6619 0.0219 0.0210 0.065 1.361 0.524 48.293 0.154 2.329 4.917 0.21 91310. 0.1228 31.98 0.6622 0.6248 0.0175 0.0185 0.057 1.202 0.419 42.649 0.136 1.864 4.456 0.21 91568. 0.0996 33.26 0.6887 0.5668 0.0131 0.0159 0.049 1.033 0.314 36.648 0.117 1.397 3.887 0.21 91834. 0.0752 34.54 0.7152 0.4737 0.0087 0.0132 0.041 0.854 0.209 30.310 0.096 0.930 3.128 0.21 92109. 0.0494 35.82 0.7417 0.3143 0.0044 0.0103 0.032 0.667 0.104 23.657 0.075 0.464 2.002 0.21 92392. 0.0223 37.10 0.7682 0.0022 0.0000 0.0073 0.022 0.471 0.000 16.711 0.053 0.002 0.014 0.21 92680. 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 0.0925 0.0326 0.238 3.754 3.939 177.676 0.424 17.520 10.055 0.27 116936. 0.6888 1.71 0.0265 0.0729 0.0913 0.0332 0.243 3.829 3.890 181.226 0.433 17.302 9.735 0.27 117017. 0.6627 3.42 0.0531 0.1411 0.0901 0.0339 0.248 3.903 3.836 184.699 0.441 17.060 9.419 0.27 117106. 0.6367 5.13 0.0796 0.2047 0.0887 0.0345 0.252 3.973 3.776 188.030 0.449 16.794 9.108 0.27 117205. 0.6108 6.83 0.1061 0.2638 0.0871 0.0351 0.256 4.039 3.710 191.155 0.456 16.501 8.802 0.27 117312. 0.5852 8.54 0.1327 0.3185 0.0854 0.0356 0.260 4.099 3.637 194.001 0.463 16.179 8.504 0.27 117429. 0.5598 10.25 0.1592 0.3692 0.0836 0.0360 0.264 4.152 3.558 196.492 0.469 15.827 8.214 0.27 117557. 0.5348 11.96 0.1857 0.4159 0.0815 0.0364 0.266 4.195 3.472 198.550 0.474 15.443 7.931 0.27 117694. 0.5101 13.67 0.2123 0.4589 0.0793 0.0367 0.268 4.228 3.378 200.092 0.478 15.025 7.657 0.27 117842. 0.4857 15.38 0.2388 0.4983 0.0769 0.0369 0.270 4.248 3.276 201.039 0.480 14.572 7.392 0.27 118001. 0.4618 17.09 0.2653 0.5344 0.0744 0.0369 0.270 4.254 3.166 201.308 0.481 14.084 7.134 0.27 118171. 0.4382 18.80 0.2919 0.5673 0.0716 0.0368 0.269 4.244 3.048 200.825 0.479 13.559 6.885 0.27 118352. 0.4149 20.50 0.3184 0.5972 0.0686 0.0366 0.268 4.216 2.922 199.516 0.476 12.998 6.643 0.27 118545. 0.3920 22.21 0.3450 0.6241 0.0655 0.0362 0.265 4.169 2.788 197.314 0.471 12.401 6.409 0.27 118749. 0.3693 23.92 0.3715 0.6481 0.0621 0.0356 0.260 4.103 2.646 194.166 0.464 11.768 6.180 0.27 118964. 0.3470 25.63 0.3980 0.6693 0.0586 0.0349 0.255 4.016 2.496 190.042 0.454 11.102 5.957 0.27 119191. 0.3248 27.34 0.4246 0.6878 0.0549 0.0339 0.248 3.908 2.340 184.938 0.442 10.407 5.738 0.27 119430. 0.3030 29.05 0.4511 0.7033 0.0511 0.0328 0.240 3.779 2.178 178.861 0.427 9.687 5.523 0.27 119680. 0.2813 30.76 0.4776 0.7157 0.0472 0.0315 0.230 3.631 2.011 171.817 0.410 8.944 5.308 0.27 119942. 0.2598 32.46 0.5042 0.7249 0.0432 0.0300 0.220 3.461 1.839 163.812 0.391 8.182 5.093 0.27 120216. 0.2384 34.17 0.5307 0.7303 0.0391 0.0284 0.208 3.272 1.664 154.852 0.370 7.402 4.875 0.27 120501. 0.2170 35.88 0.5572 0.7314 0.0349 0.0266 0.194 3.063 1.486 144.940 0.346 6.608 4.649 0.27 120798. 0.1956 37.59 0.5838 0.7271 0.0306 0.0246 0.180 2.833 1.304 134.082 0.320 5.801 4.412 0.27 121107. 0.1739 39.30 0.6103 0.7160 0.0263 0.0224 0.164 2.584 1.121 122.288 0.292 4.984 4.156 0.27 121428. 0.1518 41.01 0.6368 0.6957 0.0220 0.0201 0.147 2.315 0.935 109.572 0.262 4.158 3.870 0.28 121761. 0.1291 42.72 0.6634 0.6620 0.0176 0.0176 0.129 2.028 0.748 95.957 0.229 3.326 3.535 0.28 122105. 0.1055 44.43 0.6899 0.6073 0.0132 0.0149 0.109 1.722 0.560 81.476 0.195 2.491 3.118 0.28 122461. 0.0805 46.13 0.7164 0.5162 0.0087 0.0121 0.089 1.398 0.372 66.173 0.158 1.656 2.552 0.28 122829. 0.0538 47.84 0.7430 0.3518 0.0044 0.0092 0.067 1.059 0.185 50.111 0.120 0.824 1.677 0.28 123208. 0.0249 49.55 0.7695 -0.0014 0.0000 0.0061 0.045 0.704 0.000 33.327 0.080 -0.002 -0.006 0.28 123591. 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 0.0930 0.0321 0.459 5.782 6.188 342.033 0.653 27.524 8.206 0.34 146164. 0.7045 2.14 0.0266 0.0744 0.0919 0.0328 0.468 5.902 6.112 349.129 0.667 27.186 7.940 0.34 146266. 0.6776 4.28 0.0531 0.1439 0.0906 0.0334 0.478 6.019 6.028 356.078 0.680 26.812 7.678 0.34 146378. 0.6507 6.41 0.0797 0.2086 0.0892 0.0341 0.486 6.132 5.935 362.752 0.693 26.399 7.421 0.34 146501. 0.6240 8.55 0.1062 0.2687 0.0877 0.0346 0.495 6.238 5.832 369.020 0.705 25.943 7.169 0.34 146636. 0.5976 10.69 0.1328 0.3244 0.0860 0.0352 0.503 6.335 5.720 374.739 0.716 25.442 6.923 0.34 146783. 0.5715 12.83 0.1593 0.3758 0.0841 0.0357 0.509 6.420 5.596 379.757 0.725 24.892 6.684 0.34 146942. 0.5458 14.96 0.1859 0.4233 0.0821 0.0360 0.515 6.490 5.461 383.919 0.733 24.292 6.452 0.34 147114. 0.5204 17.10 0.2125 0.4669 0.0799 0.0363 0.519 6.543 5.314 387.061 0.739 23.639 6.228 0.34 147300. 0.4955 19.24 0.2390 0.5070 0.0775 0.0365 0.522 6.576 5.155 389.021 0.743 22.930 6.010 0.34 147499. 0.4710 21.38 0.2656 0.5436 0.0749 0.0366 0.523 6.587 4.983 389.639 0.744 22.165 5.801 0.34 147712. 0.4469 23.51 0.2921 0.5771 0.0721 0.0365 0.521 6.572 4.798 388.764 0.742 21.341 5.598 0.34 147939. 0.4232 25.65 0.3187 0.6075 0.0691 0.0363 0.518 6.529 4.600 386.251 0.738 20.460 5.402 0.34 148180. 0.3999 27.79 0.3453 0.6349 0.0660 0.0359 0.512 6.457 4.389 381.967 0.730 19.522 5.212 0.34 148436. 0.3768 29.93 0.3718 0.6596 0.0626 0.0353 0.504 6.353 4.165 375.804 0.718 18.527 5.027 0.34 148706. 0.3541 32.07 0.3984 0.6815 0.0591 0.0345 0.493 6.216 3.930 367.701 0.702 17.480 4.848 0.34 148990. 0.3317 34.20 0.4249 0.7006 0.0554 0.0336 0.480 6.046 3.684 357.651 0.683 16.388 4.672 0.34 149289. 0.3095 36.34 0.4515 0.7169 0.0515 0.0325 0.464 5.843 3.429 345.663 0.660 15.254 4.500 0.34 149603. 0.2876 38.48 0.4780 0.7303 0.0476 0.0311 0.445 5.608 3.167 331.752 0.634 14.085 4.329 0.34 149931. 0.2659 40.62 0.5046 0.7406 0.0435 0.0297 0.424 5.341 2.897 315.928 0.603 12.886 4.159 0.34 150274. 0.2443 42.75 0.5312 0.7473 0.0394 0.0280 0.400 5.041 2.621 298.199 0.570 11.659 3.987 0.34 150632. 0.2228 44.89 0.5577 0.7498 0.0352 0.0262 0.374 4.709 2.340 278.575 0.532 10.409 3.810 0.34 151004. 0.2012 47.03 0.5843 0.7474 0.0309 0.0241 0.345 4.346 2.054 257.067 0.491 9.138 3.625 0.34 151391. 0.1793 49.17 0.6108 0.7385 0.0265 0.0219 0.313 3.950 1.765 233.693 0.446 7.851 3.426 0.34 151793. 0.1571 51.30 0.6374 0.7207 0.0221 0.0196 0.280 3.524 1.473 208.482 0.398 6.551 3.204 0.34 152209. 0.1342 53.44 0.6639 0.6900 0.0177 0.0170 0.243 3.068 1.178 181.479 0.347 5.242 2.945 0.34 152641. 0.1104 55.58 0.6905 0.6387 0.0133 0.0143 0.205 2.582 0.883 152.750 0.292 3.927 2.621 0.35 153087. 0.0850 57.72 0.7171 0.5506 0.0088 0.0115 0.164 2.069 0.587 122.387 0.234 2.612 2.176 0.35 153547. 0.0576 59.86 0.7436 0.3850 0.0044 0.0085 0.121 1.530 0.293 90.510 0.173 1.302 1.467 0.35 154021. 0.0274 61.99 0.7702 0.0005 0.0000 0.0054 0.077 0.967 0.000 57.186 0.109 0.001 0.002 0.35 154500. 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 0.0936 0.0319 0.787 8.271 8.968 587.126 0.934 39.891 6.928 0.40 175389. 0.7161 2.57 0.0266 0.0754 0.0925 0.0326 0.804 8.448 8.861 599.679 0.954 39.412 6.702 0.40 175511. 0.6885 5.14 0.0532 0.1459 0.0912 0.0333 0.821 8.621 8.741 611.981 0.974 38.879 6.478 0.40 175646. 0.6611 7.70 0.0798 0.2114 0.0898 0.0339 0.837 8.788 8.608 623.807 0.993 38.288 6.259 0.40 175794. 0.6338 10.27 0.1063 0.2722 0.0883 0.0345 0.851 8.944 8.461 634.923 1.011 37.636 6.044 0.40 175956. 0.6069 12.84 0.1329 0.3285 0.0866 0.0351 0.865 9.087 8.300 645.078 1.027 36.917 5.836 0.40 176133. 0.5803 15.41 0.1595 0.3805 0.0848 0.0355 0.877 9.213 8.122 654.004 1.041 36.127 5.633 0.41 176325. 0.5541 17.97 0.1861 0.4284 0.0827 0.0359 0.887 9.318 7.928 661.424 1.053 35.263 5.437 0.41 176532. 0.5283 20.54 0.2127 0.4725 0.0805 0.0362 0.895 9.397 7.716 667.050 1.062 34.321 5.247 0.41 176756. 0.5030 23.11 0.2393 0.5130 0.0781 0.0364 0.899 9.447 7.486 670.597 1.067 33.298 5.063 0.41 176995. 0.4782 25.68 0.2658 0.5501 0.0755 0.0365 0.901 9.463 7.237 671.782 1.069 32.191 4.886 0.41 177252. 0.4537 28.25 0.2924 0.5840 0.0727 0.0364 0.899 9.443 6.969 670.339 1.067 31.000 4.716 0.41 177525. 0.4297 30.81 0.3190 0.6148 0.0697 0.0362 0.893 9.382 6.683 666.013 1.060 29.724 4.551 0.41 177816. 0.4061 33.38 0.3456 0.6427 0.0665 0.0358 0.883 9.277 6.377 658.572 1.048 28.363 4.392 0.41 178123. 0.3828 35.95 0.3722 0.6678 0.0632 0.0352 0.869 9.126 6.052 647.823 1.031 26.920 4.237 0.41 178448. 0.3598 38.52 0.3988 0.6902 0.0596 0.0344 0.850 8.926 5.711 633.661 1.009 25.401 4.088 0.41 178791. 0.3372 41.09 0.4254 0.7100 0.0559 0.0335 0.826 8.679 5.354 616.069 0.981 23.814 3.942 0.41 179150. 0.3148 43.65 0.4519 0.7270 0.0520 0.0323 0.798 8.383 4.984 595.065 0.947 22.168 3.799 0.41 179528. 0.2927 46.22 0.4785 0.7411 0.0480 0.0310 0.765 8.039 4.602 570.673 0.908 20.469 3.658 0.41 179923. 0.2708 48.79 0.5051 0.7523 0.0439 0.0295 0.728 7.648 4.210 542.910 0.864 18.725 3.517 0.41 180335. 0.2491 51.36 0.5317 0.7600 0.0397 0.0278 0.686 7.210 3.809 511.794 0.815 16.942 3.376 0.41 180766. 0.2274 53.92 0.5583 0.7638 0.0355 0.0259 0.640 6.724 3.400 477.339 0.760 15.124 3.231 0.41 181214. 0.2056 56.49 0.5849 0.7628 0.0312 0.0239 0.589 6.192 2.985 439.564 0.700 13.277 3.080 0.41 181679. 0.1837 59.06 0.6114 0.7556 0.0268 0.0217 0.534 5.614 2.564 398.503 0.634 11.405 2.918 0.41 182162. 0.1613 61.63 0.6380 0.7400 0.0223 0.0192 0.475 4.990 2.139 354.206 0.564 9.514 2.739 0.41 182663. 0.1383 64.20 0.6646 0.7119 0.0179 0.0167 0.411 4.321 1.711 306.753 0.488 7.609 2.529 0.41 183182. 0.1142 66.76 0.6912 0.6635 0.0134 0.0139 0.344 3.610 1.281 256.259 0.408 5.696 2.267 0.41 183718. 0.0885 69.33 0.7178 0.5780 0.0089 0.0110 0.272 2.858 0.851 202.889 0.323 3.784 1.902 0.42 184272. 0.0605 71.90 0.7444 0.4111 0.0044 0.0080 0.197 2.069 0.422 146.858 0.234 1.878 1.304 0.42 184842. 0.0293 74.47 0.7710 -0.0058 0.0000 0.0048 0.118 1.243 -0.003 88.246 0.140 -0.015 -0.018 0.42 185415. 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 0.0943 0.0319 1.249 11.248 12.300 931.566 1.271 54.712 5.989 0.47 204609. 0.7250 3.00 0.0266 0.0761 0.0932 0.0326 1.277 11.495 12.156 951.999 1.299 54.071 5.792 0.47 204751. 0.6970 5.99 0.0532 0.1471 0.0920 0.0333 1.304 11.737 11.996 972.040 1.326 53.356 5.597 0.47 204909. 0.6691 8.99 0.0798 0.2131 0.0906 0.0339 1.329 11.970 11.817 991.321 1.352 52.562 5.407 0.47 205082. 0.6415 11.99 0.1064 0.2743 0.0891 0.0345 1.354 12.189 11.619 1009.460 1.377 51.682 5.221 0.47 205271. 0.6142 14.98 0.1330 0.3310 0.0874 0.0351 1.376 12.389 11.401 1026.047 1.400 50.710 5.040 0.47 205478. 0.5873 17.98 0.1596 0.3834 0.0856 0.0356 1.396 12.565 11.160 1040.649 1.420 49.640 4.864 0.47 205702. 0.5609 20.98 0.1861 0.4317 0.0835 0.0360 1.412 12.712 10.896 1052.809 1.436 48.467 4.694 0.47 205945. 0.5348 23.97 0.2127 0.4761 0.0813 0.0363 1.424 12.824 10.608 1062.067 1.449 47.184 4.530 0.47 206206. 0.5093 26.97 0.2393 0.5169 0.0789 0.0365 1.432 12.895 10.294 1067.957 1.457 45.789 4.372 0.47 206487. 0.4842 29.97 0.2659 0.5544 0.0763 0.0366 1.435 12.920 9.955 1070.024 1.460 44.278 4.220 0.47 206787. 0.4595 32.96 0.2925 0.5886 0.0735 0.0365 1.432 12.894 9.589 1067.833 1.457 42.650 4.073 0.47 207107. 0.4353 35.96 0.3191 0.6198 0.0705 0.0363 1.423 12.811 9.196 1060.980 1.447 40.903 3.931 0.47 207446. 0.4115 38.96 0.3457 0.6481 0.0673 0.0359 1.407 12.667 8.777 1049.087 1.431 39.039 3.795 0.47 207806. 0.3880 41.95 0.3723 0.6736 0.0639 0.0353 1.384 12.459 8.332 1031.842 1.408 37.060 3.662 0.48 208186. 0.3649 44.95 0.3989 0.6965 0.0603 0.0345 1.353 12.184 7.863 1009.074 1.377 34.975 3.534 0.48 208586. 0.3421 47.95 0.4255 0.7168 0.0565 0.0336 1.315 11.842 7.373 980.754 1.338 32.796 3.410 0.48 209007. 0.3196 50.94 0.4521 0.7344 0.0526 0.0324 1.270 11.434 6.865 946.910 1.292 30.534 3.288 0.48 209448. 0.2974 53.94 0.4787 0.7492 0.0486 0.0311 1.217 10.959 6.340 907.583 1.238 28.199 3.168 0.48 209910. 0.2753 56.94 0.5053 0.7612 0.0445 0.0295 1.157 10.418 5.801 862.806 1.177 25.801 3.049 0.48 210392. 0.2535 59.93 0.5319 0.7698 0.0402 0.0278 1.090 9.812 5.249 812.603 1.109 23.348 2.930 0.48 210894. 0.2317 62.93 0.5584 0.7748 0.0359 0.0259 1.015 9.140 4.687 756.999 1.033 20.847 2.808 0.48 211417. 0.2098 65.93 0.5850 0.7751 0.0316 0.0238 0.933 8.404 4.115 696.027 0.950 18.305 2.682 0.48 211961. 0.1878 68.92 0.6116 0.7696 0.0271 0.0215 0.844 7.604 3.536 629.739 0.859 15.729 2.547 0.48 212526. 0.1653 71.92 0.6382 0.7560 0.0226 0.0191 0.749 6.740 2.951 558.216 0.762 13.125 2.398 0.48 213111. 0.1422 74.92 0.6648 0.7303 0.0181 0.0165 0.646 5.815 2.361 481.587 0.657 10.502 2.224 0.48 213716. 0.1179 77.91 0.6914 0.6850 0.0136 0.0137 0.536 4.830 1.769 400.039 0.546 7.868 2.006 0.48 214342. 0.0921 80.91 0.7180 0.6031 0.0090 0.0107 0.421 3.789 1.176 313.837 0.428 5.233 1.700 0.48 214988. 0.0636 83.91 0.7446 0.4380 0.0045 0.0076 0.299 2.697 0.586 223.333 0.305 2.608 1.191 0.49 215654. 0.0315 86.90 0.7712 -0.0007 0.0000 0.0044 0.173 1.553 0.000 128.635 0.175 -0.002 -0.002 0.49 216322. 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 0.0952 0.0320 1.872 14.750 16.209 1396.049 1.666 72.096 5.266 0.54 233822. 0.7318 3.43 0.0266 0.0765 0.0941 0.0327 1.914 15.081 16.025 1427.436 1.704 71.279 5.092 0.54 233985. 0.7035 6.85 0.0532 0.1478 0.0929 0.0334 1.956 15.407 15.819 1458.250 1.741 70.363 4.920 0.54 234166. 0.6755 10.28 0.0798 0.2142 0.0915 0.0341 1.995 15.720 15.590 1487.915 1.776 69.342 4.752 0.54 234364. 0.6476 13.71 0.1064 0.2757 0.0900 0.0347 2.033 16.015 15.334 1515.846 1.809 68.207 4.588 0.54 234581. 0.6202 17.14 0.1331 0.3327 0.0884 0.0353 2.067 16.285 15.051 1541.408 1.840 66.949 4.429 0.54 234818. 0.5931 20.56 0.1597 0.3853 0.0865 0.0359 2.097 16.523 14.739 1563.930 1.867 65.559 4.275 0.54 235075. 0.5664 23.99 0.1863 0.4339 0.0845 0.0363 2.122 16.722 14.395 1582.720 1.889 64.031 4.125 0.54 235354. 0.5402 27.42 0.2129 0.4785 0.0823 0.0366 2.142 16.873 14.019 1597.066 1.906 62.356 3.981 0.54 235654. 0.5145 30.84 0.2395 0.5196 0.0799 0.0368 2.154 16.971 13.609 1606.256 1.917 60.531 3.843 0.54 235975. 0.4893 34.27 0.2661 0.5573 0.0773 0.0369 2.159 17.006 13.163 1609.594 1.921 58.549 3.709 0.54 236319. 0.4645 37.70 0.2927 0.5918 0.0744 0.0368 2.154 16.972 12.682 1606.420 1.918 56.410 3.581 0.54 236686. 0.4401 41.12 0.3193 0.6233 0.0714 0.0366 2.140 16.863 12.166 1596.118 1.905 54.113 3.457 0.54 237076. 0.4162 44.55 0.3459 0.6519 0.0682 0.0362 2.116 16.673 11.614 1578.122 1.884 51.657 3.338 0.54 237488. 0.3926 47.98 0.3725 0.6779 0.0647 0.0356 2.081 16.397 11.027 1551.957 1.853 49.048 3.223 0.54 237924. 0.3694 51.41 0.3992 0.7012 0.0611 0.0348 2.035 16.031 10.408 1517.358 1.811 46.297 3.111 0.54 238383. 0.3465 54.83 0.4258 0.7219 0.0573 0.0338 1.977 15.576 9.761 1474.280 1.760 43.418 3.003 0.54 238865. 0.3238 58.26 0.4524 0.7401 0.0534 0.0326 1.908 15.032 9.089 1422.776 1.698 40.428 2.898 0.55 239370. 0.3015 61.69 0.4790 0.7556 0.0493 0.0312 1.828 14.400 8.395 1362.910 1.627 37.341 2.794 0.55 239899. 0.2794 65.11 0.5056 0.7682 0.0451 0.0297 1.736 13.679 7.682 1294.733 1.545 34.169 2.691 0.55 240451. 0.2574 68.54 0.5322 0.7777 0.0408 0.0279 1.634 12.872 6.952 1218.289 1.454 30.922 2.588 0.55 241027. 0.2355 71.97 0.5588 0.7836 0.0364 0.0260 1.520 11.977 6.208 1133.616 1.353 27.611 2.484 0.55 241626. 0.2136 75.40 0.5854 0.7852 0.0320 0.0239 1.396 10.996 5.451 1040.765 1.242 24.245 2.375 0.55 242249. 0.1914 78.82 0.6120 0.7811 0.0275 0.0215 1.260 9.929 4.683 939.815 1.122 20.832 2.260 0.55 242895. 0.1688 82.25 0.6386 0.7692 0.0229 0.0190 1.114 8.779 3.908 830.891 0.992 17.382 2.133 0.55 243565. 0.1456 85.68 0.6653 0.7457 0.0184 0.0164 0.958 7.546 3.126 714.186 0.852 13.905 1.985 0.55 244258. 0.1212 89.10 0.6919 0.7030 0.0137 0.0135 0.791 6.233 2.341 589.989 0.704 10.413 1.800 0.55 244975. 0.0950 92.53 0.7185 0.6239 0.0091 0.0105 0.615 4.846 1.556 458.705 0.548 6.919 1.538 0.55 245714. 0.0662 95.96 0.7451 0.4596 0.0045 0.0074 0.430 3.390 0.773 320.875 0.383 3.438 1.093 0.55 246476. 0.0332 99.39 0.7717 -0.0065 0.0000 0.0040 0.237 1.866 -0.006 176.570 0.211 -0.026 -0.015 0.56 247236. 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 0.0961 0.0323 2.687 18.820 20.723 2004.010 2.126 92.178 4.690 0.61 263028. 0.7370 3.86 0.0266 0.0767 0.0951 0.0330 2.749 19.254 20.498 2050.229 2.175 91.177 4.535 0.61 263212. 0.7087 7.71 0.0532 0.1482 0.0939 0.0337 2.810 19.681 20.245 2095.650 2.224 90.051 4.382 0.61 263415. 0.6805 11.57 0.0799 0.2147 0.0926 0.0344 2.869 20.092 19.961 2139.419 2.270 88.788 4.232 0.61 263638. 0.6526 15.43 0.1065 0.2764 0.0911 0.0351 2.924 20.479 19.644 2180.669 2.314 87.376 4.086 0.61 263883. 0.6250 19.29 0.1331 0.3335 0.0895 0.0357 2.975 20.834 19.291 2218.452 2.354 85.804 3.944 0.61 264151. 0.5979 23.14 0.1597 0.3862 0.0877 0.0363 3.020 21.147 18.899 2251.785 2.389 84.061 3.807 0.61 264441. 0.5712 27.00 0.1864 0.4349 0.0857 0.0367 3.057 21.409 18.466 2279.638 2.419 82.137 3.674 0.61 264755. 0.5449 30.86 0.2130 0.4797 0.0834 0.0370 3.086 21.609 17.991 2300.967 2.441 80.022 3.546 0.61 265094. 0.5192 34.71 0.2396 0.5210 0.0810 0.0373 3.104 21.739 17.471 2314.729 2.456 77.709 3.423 0.61 265457. 0.4939 38.57 0.2662 0.5589 0.0784 0.0374 3.111 21.787 16.905 2319.914 2.462 75.193 3.305 0.61 265846. 0.4690 42.43 0.2928 0.5936 0.0756 0.0373 3.105 21.746 16.293 2315.549 2.457 72.470 3.191 0.61 266260. 0.4446 46.29 0.3195 0.6254 0.0725 0.0370 3.085 21.607 15.634 2300.752 2.441 69.540 3.082 0.61 266700. 0.4206 50.14 0.3461 0.6544 0.0692 0.0366 3.050 21.363 14.929 2274.709 2.414 66.403 2.977 0.61 267165. 0.3970 54.00 0.3727 0.6807 0.0658 0.0360 3.000 21.006 14.179 2236.728 2.373 63.067 2.875 0.61 267657. 0.3737 57.86 0.3993 0.7044 0.0621 0.0352 2.932 20.534 13.387 2186.426 2.320 59.543 2.777 0.61 268175. 0.3507 61.72 0.4260 0.7256 0.0582 0.0342 2.848 19.945 12.557 2123.743 2.253 55.854 2.682 0.61 268719. 0.3280 65.57 0.4526 0.7443 0.0542 0.0330 2.747 19.241 11.695 2048.758 2.174 52.018 2.589 0.61 269289. 0.3056 69.43 0.4792 0.7604 0.0501 0.0316 2.631 18.422 10.804 1961.579 2.081 48.054 2.498 0.61 269885. 0.2834 73.29 0.5058 0.7737 0.0459 0.0300 2.497 17.489 9.887 1862.290 1.976 43.979 2.408 0.61 270508. 0.2614 77.14 0.5324 0.7840 0.0415 0.0282 2.348 16.444 8.949 1750.961 1.858 39.807 2.318 0.62 271157. 0.2394 81.00 0.5591 0.7909 0.0371 0.0262 2.183 15.286 7.992 1627.650 1.727 35.550 2.227 0.62 271833. 0.2173 84.86 0.5857 0.7936 0.0326 0.0240 2.001 14.016 7.019 1492.436 1.584 31.220 2.133 0.62 272534. 0.1951 88.72 0.6123 0.7908 0.0280 0.0217 1.804 12.635 6.032 1345.431 1.428 26.829 2.033 0.62 273263. 0.1724 92.57 0.6389 0.7807 0.0233 0.0191 1.592 11.146 5.033 1186.819 1.259 22.388 1.924 0.62 274017. 0.1490 96.43 0.6656 0.7593 0.0187 0.0164 1.364 9.550 4.027 1016.880 1.079 17.911 1.796 0.62 274798. 0.1244 100.29 0.6922 0.7192 0.0140 0.0135 1.121 7.851 3.015 836.032 0.887 13.412 1.636 0.62 275605. 0.0980 104.14 0.7188 0.6432 0.0093 0.0104 0.865 6.056 2.003 644.869 0.684 8.910 1.409 0.62 276438. 0.0688 108.00 0.7454 0.4808 0.0046 0.0072 0.596 4.172 0.994 444.185 0.471 4.423 1.015 0.62 277296. 0.0350 111.86 0.7720 -0.0096 0.0000 0.0038 0.314 2.197 -0.010 233.963 0.248 -0.045 -0.020 0.62 278147. 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 0.0972 0.0327 3.741 23.578 25.880 2789.576 2.664 115.112 4.208 0.67 292225. 0.7389 4.31 0.0268 0.0769 0.0962 0.0335 3.828 24.126 25.613 2854.425 2.726 113.928 4.070 0.67 292430. 0.7109 8.62 0.0535 0.1486 0.0951 0.0343 3.914 24.667 25.311 2918.346 2.787 112.584 3.934 0.67 292657. 0.6831 12.93 0.0803 0.2154 0.0938 0.0350 3.996 25.189 24.970 2980.132 2.846 111.066 3.800 0.67 292908. 0.6555 17.24 0.1071 0.2773 0.0924 0.0357 4.075 25.682 24.585 3038.519 2.902 109.356 3.670 0.67 293182. 0.6281 21.55 0.1338 0.3347 0.0907 0.0363 4.147 26.136 24.155 3092.148 2.953 107.439 3.543 0.67 293482. 0.6010 25.86 0.1606 0.3877 0.0889 0.0368 4.210 26.536 23.674 3139.566 2.998 105.300 3.420 0.68 293808. 0.5744 30.17 0.1874 0.4366 0.0869 0.0373 4.263 26.872 23.140 3179.260 3.036 102.926 3.301 0.68 294162. 0.5481 34.47 0.2141 0.4816 0.0847 0.0377 4.304 27.129 22.550 3209.675 3.065 100.304 3.187 0.68 294542. 0.5223 38.78 0.2409 0.5231 0.0823 0.0379 4.331 27.295 21.903 3229.271 3.084 97.425 3.076 0.68 294951. 0.4969 43.09 0.2677 0.5612 0.0796 0.0380 4.340 27.356 21.196 3236.531 3.091 94.281 2.970 0.68 295388. 0.4720 47.40 0.2945 0.5961 0.0768 0.0379 4.332 27.301 20.429 3230.050 3.084 90.868 2.869 0.68 295854. 0.4475 51.71 0.3212 0.6282 0.0736 0.0377 4.303 27.119 19.601 3208.549 3.064 87.187 2.771 0.68 296349. 0.4234 56.02 0.3480 0.6574 0.0703 0.0372 4.252 26.801 18.714 3170.891 3.028 83.239 2.677 0.68 296873. 0.3997 60.33 0.3748 0.6840 0.0668 0.0366 4.179 26.338 17.768 3116.125 2.976 79.031 2.586 0.68 297426. 0.3763 64.64 0.4015 0.7081 0.0630 0.0357 4.082 25.726 16.768 3043.737 2.907 74.583 2.499 0.68 298008. 0.3532 68.95 0.4283 0.7297 0.0591 0.0347 3.961 24.965 15.720 2953.676 2.821 69.921 2.414 0.68 298620. 0.3303 73.26 0.4551 0.7488 0.0550 0.0334 3.817 24.056 14.629 2846.085 2.718 65.070 2.331 0.68 299261. 0.3078 77.57 0.4818 0.7653 0.0507 0.0319 3.649 23.000 13.502 2721.135 2.598 60.056 2.251 0.68 299932. 0.2854 81.88 0.5086 0.7792 0.0464 0.0303 3.458 21.798 12.342 2578.965 2.463 54.898 2.171 0.68 300632. 0.2632 86.19 0.5354 0.7900 0.0419 0.0284 3.245 20.452 11.154 2419.682 2.311 49.615 2.091 0.68 301361. 0.2410 90.50 0.5621 0.7975 0.0374 0.0263 3.008 18.962 9.942 2243.385 2.142 44.223 2.010 0.69 302120. 0.2188 94.81 0.5889 0.8008 0.0327 0.0241 2.749 17.329 8.709 2050.188 1.958 38.736 1.927 0.69 302909. 0.1962 99.11 0.6157 0.7987 0.0280 0.0216 2.468 15.554 7.457 1840.264 1.757 33.171 1.838 0.69 303727. 0.1732 103.42 0.6424 0.7890 0.0233 0.0189 2.164 13.641 6.192 1613.889 1.541 27.542 1.740 0.69 304574. 0.1495 107.73 0.6692 0.7678 0.0185 0.0161 1.839 11.592 4.916 1371.483 1.310 21.866 1.626 0.69 305452. 0.1244 112.04 0.6960 0.7269 0.0137 0.0131 1.493 9.413 3.634 1113.693 1.063 16.163 1.480 0.69 306358. 0.0974 116.35 0.7228 0.6463 0.0088 0.0099 1.128 7.112 2.350 841.461 0.804 10.455 1.267 0.69 307293. 0.0670 120.66 0.7495 0.4627 0.0040 0.0065 0.746 4.700 1.072 556.071 0.531 4.769 0.875 0.69 308256. 0.0313 124.97 0.7763 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 0.0985 0.0341 5.185 29.708 31.709 3866.286 3.356 141.041 3.720 0.74 321412. 0.7230 4.73 0.0267 0.0748 0.0975 0.0348 5.295 30.339 31.409 3948.366 3.428 139.709 3.608 0.74 321636. 0.6980 9.46 0.0534 0.1451 0.0965 0.0355 5.403 30.957 31.067 4028.883 3.498 138.184 3.497 0.74 321885. 0.6728 14.19 0.0801 0.2108 0.0952 0.0362 5.507 31.552 30.675 4106.285 3.565 136.443 3.388 0.74 322160. 0.6477 18.92 0.1068 0.2722 0.0939 0.0369 5.604 32.111 30.230 4178.989 3.628 134.465 3.281 0.74 322461. 0.6227 23.65 0.1336 0.3293 0.0923 0.0374 5.693 32.620 29.727 4245.291 3.685 132.227 3.176 0.74 322791. 0.5977 28.38 0.1603 0.3824 0.0905 0.0379 5.771 33.067 29.162 4303.394 3.736 129.711 3.074 0.74 323149. 0.5729 33.11 0.1870 0.4317 0.0886 0.0384 5.835 33.436 28.529 4351.432 3.778 126.896 2.974 0.74 323538. 0.5482 37.84 0.2137 0.4772 0.0864 0.0387 5.884 33.713 27.826 4387.469 3.809 123.769 2.877 0.74 323957. 0.5237 42.57 0.2404 0.5193 0.0840 0.0389 5.913 33.882 27.049 4409.542 3.828 120.315 2.782 0.74 324406. 0.4995 47.30 0.2671 0.5580 0.0813 0.0389 5.922 33.930 26.198 4415.706 3.833 116.526 2.691 0.74 324888. 0.4754 52.03 0.2938 0.5936 0.0785 0.0388 5.906 33.840 25.269 4404.068 3.823 112.397 2.602 0.75 325400. 0.4515 56.76 0.3205 0.6263 0.0753 0.0386 5.864 33.600 24.264 4372.850 3.796 107.927 2.517 0.75 325945. 0.4279 61.49 0.3473 0.6561 0.0720 0.0381 5.794 33.197 23.183 4320.390 3.751 103.118 2.434 0.75 326522. 0.4045 66.22 0.3740 0.6833 0.0684 0.0374 5.693 32.620 22.028 4245.230 3.685 97.982 2.354 0.75 327130. 0.3813 70.95 0.4007 0.7079 0.0646 0.0366 5.561 31.861 20.805 4146.466 3.600 92.539 2.276 0.75 327771. 0.3583 75.69 0.4274 0.7301 0.0606 0.0355 5.396 30.919 19.520 4023.834 3.493 86.824 2.200 0.75 328443. 0.3355 80.42 0.4541 0.7498 0.0565 0.0342 5.200 29.793 18.181 3877.379 3.366 80.868 2.127 0.75 329148. 0.3130 85.15 0.4808 0.7670 0.0521 0.0327 4.971 28.486 16.795 3707.226 3.218 74.703 2.055 0.75 329885. 0.2907 89.88 0.5075 0.7817 0.0477 0.0310 4.712 26.998 15.368 3513.543 3.050 68.356 1.984 0.75 330654. 0.2684 94.61 0.5342 0.7935 0.0432 0.0291 4.421 25.330 13.905 3296.504 2.862 61.848 1.913 0.75 331455. 0.2462 99.34 0.5610 0.8021 0.0385 0.0270 4.099 23.484 12.410 3056.295 2.653 55.200 1.842 0.75 332288. 0.2239 104.07 0.5877 0.8067 0.0338 0.0246 3.746 21.462 10.888 2793.157 2.425 48.431 1.768 0.75 333154. 0.2014 108.80 0.6144 0.8061 0.0290 0.0221 3.363 19.267 9.343 2507.447 2.177 41.559 1.690 0.76 334051. 0.1783 113.53 0.6411 0.7983 0.0242 0.0194 2.950 16.902 7.779 2199.719 1.910 34.602 1.604 0.76 334981. 0.1544 118.26 0.6678 0.7794 0.0193 0.0165 2.509 14.375 6.201 1870.853 1.624 27.581 1.503 0.76 335943. 0.1292 122.99 0.6945 0.7412 0.0143 0.0134 2.041 11.696 4.613 1522.153 1.321 20.520 1.375 0.76 336937. 0.1019 127.72 0.7212 0.6644 0.0094 0.0102 1.549 8.878 3.023 1155.455 1.003 13.445 1.187 0.76 337962. 0.0712 132.45 0.7479 0.4892 0.0045 0.0068 1.037 5.941 1.436 773.190 0.671 6.389 0.843 0.76 339018. 0.0349 137.18 0.7747 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 0.0997 0.0376 7.431 39.028 38.225 5540.985 4.409 170.026 3.129 0.81 350587. 0.6677 5.15 0.0266 0.0688 0.0989 0.0383 7.558 39.696 37.906 5635.756 4.485 168.607 3.051 0.81 350829. 0.6483 10.29 0.0533 0.1341 0.0979 0.0389 7.679 40.334 37.536 5726.316 4.557 166.960 2.973 0.81 351098. 0.6287 15.44 0.0799 0.1960 0.0968 0.0395 7.792 40.926 37.108 5810.476 4.624 165.056 2.897 0.81 351396. 0.6090 20.58 0.1065 0.2546 0.0955 0.0400 7.893 41.459 36.615 5886.120 4.684 162.863 2.821 0.81 351723. 0.5893 25.73 0.1332 0.3099 0.0941 0.0404 7.981 41.917 36.050 5951.159 4.736 160.352 2.748 0.81 352081. 0.5694 30.87 0.1598 0.3620 0.0924 0.0408 8.051 42.286 35.408 6003.552 4.777 157.494 2.675 0.81 352472. 0.5494 36.02 0.1864 0.4111 0.0905 0.0410 8.102 42.552 34.682 6041.309 4.808 154.265 2.604 0.81 352895. 0.5293 41.16 0.2131 0.4572 0.0884 0.0412 8.130 42.701 33.868 6062.470 4.824 150.643 2.534 0.81 353351. 0.5090 46.31 0.2397 0.5004 0.0860 0.0412 8.133 42.720 32.961 6065.099 4.826 146.610 2.465 0.81 353842. 0.4885 51.45 0.2663 0.5407 0.0834 0.0411 8.110 42.594 31.959 6047.266 4.812 142.155 2.397 0.81 354367. 0.4677 56.60 0.2930 0.5782 0.0805 0.0408 8.056 42.311 30.861 6007.091 4.780 137.270 2.330 0.81 354926. 0.4468 61.74 0.3196 0.6129 0.0774 0.0404 7.969 41.858 29.666 5942.751 4.729 131.955 2.264 0.81 355521. 0.4257 66.89 0.3462 0.6449 0.0740 0.0398 7.848 41.222 28.376 5852.485 4.657 126.215 2.199 0.81 356149. 0.4043 72.03 0.3729 0.6742 0.0704 0.0390 7.690 40.392 26.992 5734.638 4.563 120.059 2.135 0.81 356813. 0.3828 77.18 0.3995 0.7009 0.0666 0.0380 7.494 39.360 25.521 5588.114 4.447 113.516 2.071 0.82 357511. 0.3612 82.32 0.4261 0.7250 0.0625 0.0368 7.258 38.123 23.971 5412.535 4.307 106.624 2.009 0.82 358244. 0.3395 87.47 0.4528 0.7465 0.0583 0.0354 6.984 36.682 22.353 5207.878 4.144 99.427 1.947 0.82 359012. 0.3177 92.61 0.4794 0.7655 0.0539 0.0338 6.670 35.035 20.675 4974.116 3.958 91.962 1.885 0.82 359815. 0.2959 97.76 0.5061 0.7817 0.0494 0.0320 6.318 33.183 18.944 4711.144 3.749 84.264 1.824 0.82 360652. 0.2740 102.91 0.5327 0.7947 0.0448 0.0300 5.927 31.133 17.167 4420.121 3.517 76.360 1.762 0.82 361523. 0.2519 108.05 0.5593 0.8042 0.0400 0.0279 5.499 28.885 15.350 4100.934 3.263 68.276 1.698 0.82 362430. 0.2296 113.20 0.5860 0.8092 0.0352 0.0255 5.034 26.442 13.497 3754.024 2.987 60.034 1.631 0.82 363371. 0.2068 118.34 0.6126 0.8086 0.0303 0.0230 4.532 23.804 11.613 3379.485 2.689 51.657 1.559 0.82 364347. 0.1833 123.49 0.6392 0.7999 0.0253 0.0202 3.995 20.982 9.705 2978.940 2.371 43.167 1.478 0.83 365357. 0.1589 128.63 0.6659 0.7785 0.0203 0.0174 3.426 17.994 7.776 2554.660 2.033 34.587 1.381 0.83 366402. 0.1329 133.78 0.6925 0.7355 0.0152 0.0143 2.829 14.859 5.833 2109.603 1.679 25.946 1.254 0.83 367482. 0.1045 138.92 0.7191 0.6512 0.0101 0.0112 2.209 11.604 3.884 1647.450 1.311 17.275 1.069 0.83 368595. 0.0727 144.07 0.7458 0.4730 0.0051 0.0080 1.573 8.260 1.936 1172.672 0.933 8.612 0.749 0.83 369741. 0.0360 149.21 0.7724 -0.0037 0.0000 0.0047 0.922 4.841 -0.009 687.360 0.547 -0.038 -0.006 0.83 370879. 0.0000 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 0.1005 0.0441 11.061 53.629 45.209 8248.395 6.059 201.088 2.486 0.88 379771. 0.5769 5.58 0.0267 0.0596 0.0998 0.0447 11.218 54.391 44.895 8365.613 6.145 199.693 2.434 0.88 380029. 0.5629 11.17 0.0534 0.1167 0.0990 0.0453 11.365 55.100 44.526 8474.640 6.225 198.051 2.383 0.88 380317. 0.5489 16.75 0.0801 0.1714 0.0980 0.0458 11.494 55.728 44.092 8571.306 6.296 196.120 2.333 0.88 380636. 0.5347 22.34 0.1067 0.2238 0.0969 0.0462 11.602 56.249 43.583 8651.412 6.355 193.856 2.285 0.88 380988. 0.5206 27.92 0.1334 0.2740 0.0956 0.0465 11.681 56.636 42.988 8710.869 6.399 191.212 2.238 0.88 381375. 0.5066 33.51 0.1601 0.3222 0.0940 0.0467 11.729 56.864 42.299 8746.023 6.424 188.144 2.194 0.88 381797. 0.4924 39.09 0.1868 0.3686 0.0923 0.0468 11.739 56.915 41.505 8753.864 6.430 184.613 2.151 0.88 382255. 0.4782 44.68 0.2135 0.4130 0.0903 0.0466 11.710 56.774 40.599 8732.146 6.414 180.584 2.109 0.88 382751. 0.4638 50.26 0.2402 0.4557 0.0880 0.0464 11.639 56.431 39.575 8679.312 6.375 176.031 2.068 0.88 383285. 0.4491 55.85 0.2669 0.4965 0.0854 0.0459 11.525 55.878 38.430 8594.301 6.313 170.935 2.028 0.88 383857. 0.4340 61.43 0.2935 0.5355 0.0826 0.0453 11.367 55.111 37.160 8476.402 6.226 165.286 1.988 0.88 384468. 0.4184 67.02 0.3202 0.5725 0.0795 0.0445 11.164 54.127 35.765 8325.067 6.115 159.083 1.949 0.88 385116. 0.4022 72.60 0.3469 0.6074 0.0761 0.0435 10.916 52.923 34.248 8139.799 5.979 152.333 1.908 0.88 385803. 0.3855 78.19 0.3736 0.6401 0.0725 0.0423 10.621 51.494 32.610 7920.064 5.818 145.050 1.868 0.88 386528. 0.3681 83.77 0.4003 0.6706 0.0686 0.0410 10.280 49.840 30.861 7665.696 5.631 137.268 1.826 0.88 387290. 0.3501 89.35 0.4270 0.6987 0.0645 0.0394 9.893 47.964 29.010 7377.191 5.419 129.036 1.784 0.88 388091. 0.3316 94.94 0.4536 0.7243 0.0602 0.0377 9.462 45.873 27.071 7055.488 5.183 120.410 1.740 0.89 388929. 0.3125 100.52 0.4803 0.7473 0.0557 0.0358 8.986 43.569 25.054 6701.101 4.922 111.439 1.696 0.89 389805. 0.2930 106.11 0.5070 0.7675 0.0511 0.0337 8.467 41.053 22.969 6314.144 4.638 102.168 1.650 0.89 390718. 0.2729 111.69 0.5337 0.7846 0.0463 0.0315 7.905 38.327 20.826 5894.883 4.330 92.634 1.602 0.89 391669. 0.2524 117.28 0.5604 0.7968 0.0414 0.0291 7.312 35.451 18.629 5452.523 4.005 82.863 1.550 0.89 392658. 0.2309 122.86 0.5871 0.8014 0.0364 0.0267 6.698 32.473 16.385 4994.581 3.669 72.879 1.488 0.89 393683. 0.2079 128.45 0.6138 0.7951 0.0313 0.0242 6.073 29.442 14.097 4528.345 3.326 62.704 1.412 0.89 394747. 0.1830 134.03 0.6404 0.7772 0.0262 0.0216 5.415 26.256 11.777 4038.249 2.966 52.384 1.323 0.89 395847. 0.1567 139.62 0.6671 0.7419 0.0210 0.0189 4.733 22.946 9.431 3529.196 2.592 41.949 1.212 0.90 396985. 0.1285 145.20 0.6938 0.6786 0.0157 0.0161 4.032 19.550 7.068 3006.871 2.209 31.436 1.066 0.90 398159. 0.0978 150.79 0.7205 0.5684 0.0104 0.0132 3.323 16.109 4.697 2477.679 1.820 20.893 0.860 0.90 399371. 0.0643 156.37 0.7472 0.3722 0.0052 0.0104 2.613 12.669 2.333 1948.503 1.431 10.375 0.543 0.90 400618. 0.0286 161.95 0.7739 -0.0045 0.0000 0.0076 1.906 9.242 -0.020 1421.419 1.044 -0.089 -0.006 0.90 401869. 0.0000 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 0.0989 0.0501 15.697 70.669 51.599 11705.335 7.984 229.511 1.999 0.94 409042. 0.4957 6.14 0.0272 0.0528 0.0983 0.0507 15.891 71.543 51.291 11850.097 8.083 228.143 1.963 0.94 409320. 0.4853 12.27 0.0545 0.1037 0.0976 0.0513 16.078 72.382 50.930 11989.182 8.178 226.537 1.927 0.94 409631. 0.4746 18.41 0.0817 0.1526 0.0968 0.0518 16.250 73.159 50.505 12117.761 8.265 224.646 1.890 0.94 409976. 0.4637 24.55 0.1089 0.1996 0.0959 0.0523 16.402 73.841 50.005 12230.697 8.342 222.420 1.854 0.94 410358. 0.4526 30.68 0.1361 0.2447 0.0947 0.0527 16.525 74.395 49.416 12322.486 8.405 219.803 1.819 0.94 410777. 0.4413 36.82 0.1634 0.2880 0.0934 0.0530 16.612 74.786 48.727 12387.375 8.449 216.739 1.784 0.95 411236. 0.4299 42.96 0.1906 0.3296 0.0919 0.0531 16.655 74.981 47.925 12419.517 8.471 213.169 1.750 0.95 411737. 0.4182 49.09 0.2178 0.3696 0.0901 0.0531 16.646 74.941 46.996 12412.998 8.467 209.040 1.717 0.95 412279. 0.4063 55.23 0.2451 0.4080 0.0880 0.0529 16.578 74.633 45.930 12361.896 8.432 204.297 1.685 0.95 412865. 0.3942 61.37 0.2723 0.4451 0.0857 0.0524 16.441 74.019 44.715 12260.166 8.363 198.892 1.654 0.95 413494. 0.3818 67.51 0.2995 0.4807 0.0831 0.0518 16.229 73.062 43.342 12101.721 8.254 192.784 1.624 0.95 414167. 0.3691 73.64 0.3267 0.5152 0.0801 0.0508 15.932 71.728 41.803 11880.849 8.104 185.939 1.596 0.95 414885. 0.3561 79.78 0.3540 0.5486 0.0769 0.0496 15.547 69.993 40.094 11593.351 7.908 178.337 1.569 0.95 415647. 0.3428 85.92 0.3812 0.5809 0.0733 0.0481 15.070 67.847 38.215 11237.893 7.665 169.982 1.542 0.95 416453. 0.3291 92.05 0.4084 0.6122 0.0693 0.0463 14.506 65.305 36.176 10816.828 7.378 160.912 1.517 0.95 417304. 0.3149 98.19 0.4357 0.6421 0.0652 0.0442 13.860 62.400 33.992 10335.710 7.050 151.197 1.492 0.95 418198. 0.3002 104.33 0.4629 0.6705 0.0607 0.0419 13.143 59.171 31.680 9800.952 6.685 140.913 1.466 0.95 419135. 0.2848 110.46 0.4901 0.6971 0.0561 0.0394 12.363 55.658 29.258 9218.925 6.288 130.138 1.439 0.96 420115. 0.2687 116.60 0.5174 0.7214 0.0513 0.0368 11.525 51.887 26.740 8594.368 5.862 118.938 1.411 0.96 421138. 0.2519 122.74 0.5446 0.7428 0.0463 0.0339 10.635 47.880 24.139 7930.699 5.409 107.372 1.381 0.96 422202. 0.2341 128.87 0.5718 0.7601 0.0412 0.0310 9.706 43.696 21.468 7237.678 4.937 95.491 1.345 0.96 423309. 0.2152 135.01 0.5990 0.7655 0.0359 0.0281 8.808 39.653 18.729 6567.951 4.480 83.307 1.293 0.96 424457. 0.1932 141.15 0.6263 0.7426 0.0305 0.0257 8.067 36.318 15.916 6015.662 4.103 70.796 1.200 0.96 425647. 0.1652 147.28 0.6535 0.6998 0.0250 0.0234 7.332 33.009 13.065 5467.546 3.729 58.111 1.084 0.96 426879. 0.1352 153.42 0.6807 0.6320 0.0195 0.0210 6.597 29.700 10.192 4919.471 3.356 45.335 0.940 0.97 428151. 0.1035 159.56 0.7080 0.5304 0.0140 0.0187 5.873 26.438 7.320 4379.145 2.987 32.561 0.758 0.97 429464. 0.0708 165.69 0.7352 0.3827 0.0086 0.0165 5.167 23.260 4.475 3852.780 2.628 19.906 0.527 0.97 430818. 0.0385 171.83 0.7624 0.1721 0.0032 0.0143 4.485 20.192 1.685 3344.461 2.281 7.493 0.228 0.97 432211. 0.0102 177.97 0.7896