27x13E (27x13E.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 0.0805 0.0271 0.031 1.975 1.364 23.372 0.223 6.066 26.464 0.11 66888. 0.6716 0.55 0.0216 0.0624 0.0791 0.0274 0.032 1.995 1.340 23.608 0.225 5.960 25.743 0.11 66926. 0.6476 1.11 0.0433 0.1214 0.0776 0.0277 0.032 2.013 1.314 23.821 0.227 5.846 25.028 0.11 66967. 0.6236 1.66 0.0649 0.1770 0.0760 0.0279 0.032 2.029 1.287 24.006 0.229 5.725 24.321 0.11 67011. 0.5997 2.21 0.0866 0.2292 0.0743 0.0281 0.032 2.042 1.258 24.158 0.231 5.596 23.623 0.11 67058. 0.5758 2.77 0.1082 0.2782 0.0725 0.0282 0.033 2.052 1.227 24.273 0.232 5.459 22.935 0.11 67108. 0.5522 3.32 0.1298 0.3239 0.0705 0.0283 0.033 2.058 1.195 24.344 0.232 5.313 22.256 0.11 67162. 0.5286 3.87 0.1515 0.3666 0.0685 0.0283 0.033 2.060 1.160 24.366 0.233 5.159 21.588 0.11 67219. 0.5052 4.43 0.1731 0.4062 0.0663 0.0283 0.033 2.057 1.123 24.335 0.232 4.995 20.930 0.11 67280. 0.4820 4.98 0.1948 0.4428 0.0640 0.0282 0.033 2.049 1.084 24.243 0.232 4.822 20.282 0.11 67344. 0.4589 5.53 0.2164 0.4765 0.0616 0.0280 0.032 2.036 1.043 24.086 0.230 4.639 19.642 0.11 67413. 0.4359 6.09 0.2381 0.5072 0.0590 0.0277 0.032 2.016 1.000 23.857 0.228 4.447 19.009 0.11 67485. 0.4131 6.64 0.2597 0.5351 0.0564 0.0274 0.032 1.991 0.954 23.551 0.225 4.245 18.381 0.11 67561. 0.3903 7.19 0.2813 0.5600 0.0536 0.0269 0.031 1.958 0.907 23.167 0.221 4.034 17.757 0.11 67642. 0.3675 7.75 0.3030 0.5819 0.0506 0.0264 0.030 1.919 0.858 22.703 0.217 3.815 17.134 0.11 67726. 0.3448 8.30 0.3246 0.6007 0.0476 0.0257 0.030 1.873 0.807 22.159 0.212 3.587 16.508 0.11 67815. 0.3222 8.85 0.3463 0.6162 0.0445 0.0250 0.029 1.820 0.754 21.536 0.206 3.353 15.876 0.11 67907. 0.2995 9.41 0.3679 0.6281 0.0413 0.0242 0.028 1.761 0.700 20.833 0.199 3.112 15.232 0.11 68004. 0.2769 9.96 0.3895 0.6362 0.0380 0.0233 0.027 1.695 0.644 20.050 0.191 2.865 14.570 0.11 68105. 0.2541 10.51 0.4112 0.6399 0.0347 0.0223 0.026 1.622 0.587 19.188 0.183 2.613 13.885 0.11 68211. 0.2313 11.07 0.4328 0.6387 0.0313 0.0212 0.024 1.542 0.530 18.248 0.174 2.356 13.165 0.11 68320. 0.2082 11.62 0.4545 0.6317 0.0278 0.0200 0.023 1.456 0.471 17.231 0.165 2.096 12.401 0.11 68435. 0.1850 12.17 0.4761 0.6178 0.0243 0.0187 0.022 1.364 0.412 16.140 0.154 1.832 11.576 0.11 68553. 0.1615 12.73 0.4977 0.5952 0.0208 0.0174 0.020 1.266 0.352 14.976 0.143 1.567 10.668 0.11 68676. 0.1376 13.28 0.5194 0.5617 0.0173 0.0160 0.018 1.162 0.292 13.743 0.131 1.300 9.648 0.11 68803. 0.1134 13.83 0.5410 0.5137 0.0137 0.0145 0.017 1.052 0.232 12.445 0.119 1.034 8.470 0.11 68935. 0.0887 14.39 0.5627 0.4457 0.0102 0.0129 0.015 0.937 0.173 11.088 0.106 0.768 7.066 0.11 69071. 0.0638 14.94 0.5843 0.3488 0.0067 0.0112 0.013 0.818 0.114 9.679 0.092 0.506 5.326 0.11 69212. 0.0390 15.49 0.6060 0.2076 0.0033 0.0096 0.011 0.695 0.055 8.224 0.079 0.247 3.057 0.11 69357. 0.0156 16.05 0.6276 -0.0087 -0.0001 0.0078 0.009 0.569 -0.002 6.727 0.064 -0.008 -0.124 0.11 69503. 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 0.0810 0.0256 0.236 7.442 5.486 176.084 0.841 24.401 14.131 0.21 133773. 0.7193 1.11 0.0217 0.0667 0.0796 0.0259 0.239 7.527 5.390 178.116 0.850 23.977 13.727 0.21 133849. 0.6926 2.22 0.0434 0.1296 0.0781 0.0261 0.241 7.606 5.288 179.966 0.859 23.522 13.328 0.21 133931. 0.6661 3.33 0.0651 0.1887 0.0765 0.0264 0.244 7.674 5.179 181.591 0.867 23.037 12.936 0.21 134019. 0.6398 4.44 0.0867 0.2441 0.0747 0.0266 0.245 7.732 5.063 182.951 0.874 22.519 12.552 0.21 134113. 0.6137 5.54 0.1084 0.2959 0.0729 0.0267 0.247 7.776 4.939 184.001 0.879 21.968 12.174 0.21 134214. 0.5880 6.65 0.1301 0.3444 0.0710 0.0268 0.248 7.806 4.807 184.697 0.882 21.381 11.805 0.21 134322. 0.5625 7.76 0.1518 0.3894 0.0689 0.0269 0.248 7.818 4.667 184.992 0.883 20.760 11.443 0.21 134437. 0.5372 8.87 0.1735 0.4313 0.0667 0.0268 0.248 7.812 4.519 184.842 0.883 20.101 11.089 0.21 134559. 0.5123 9.98 0.1952 0.4700 0.0644 0.0267 0.247 7.784 4.363 184.198 0.879 19.405 10.743 0.21 134689. 0.4876 11.09 0.2169 0.5058 0.0620 0.0266 0.245 7.734 4.198 183.011 0.874 18.671 10.403 0.21 134827. 0.4632 12.20 0.2386 0.5385 0.0594 0.0263 0.243 7.659 4.024 181.227 0.865 17.897 10.070 0.21 134972. 0.4390 13.31 0.2602 0.5684 0.0567 0.0260 0.240 7.557 3.841 178.806 0.854 17.084 9.743 0.21 135125. 0.4149 14.42 0.2819 0.5954 0.0539 0.0255 0.236 7.426 3.650 175.727 0.839 16.234 9.420 0.22 135286. 0.3911 15.53 0.3036 0.6195 0.0509 0.0250 0.231 7.268 3.451 171.981 0.821 15.350 9.101 0.22 135456. 0.3674 16.63 0.3253 0.6406 0.0479 0.0243 0.225 7.081 3.245 167.565 0.800 14.434 8.784 0.22 135634. 0.3439 17.74 0.3470 0.6586 0.0448 0.0236 0.218 6.866 3.033 162.474 0.776 13.489 8.466 0.22 135820. 0.3204 18.85 0.3687 0.6733 0.0415 0.0227 0.210 6.623 2.814 156.707 0.748 12.519 8.146 0.22 136015. 0.2970 19.96 0.3904 0.6844 0.0382 0.0218 0.202 6.350 2.591 150.263 0.717 11.525 7.821 0.22 136218. 0.2736 21.07 0.4120 0.6916 0.0349 0.0208 0.192 6.050 2.363 143.147 0.683 10.510 7.487 0.22 136430. 0.2501 22.18 0.4337 0.6942 0.0315 0.0197 0.182 5.721 2.131 135.363 0.646 9.477 7.139 0.22 136650. 0.2265 23.29 0.4554 0.6914 0.0280 0.0184 0.170 5.364 1.895 126.923 0.606 8.430 6.772 0.22 136879. 0.2026 24.40 0.4771 0.6822 0.0245 0.0171 0.158 4.980 1.657 117.842 0.563 7.371 6.378 0.22 137117. 0.1784 25.51 0.4988 0.6647 0.0209 0.0157 0.145 4.570 1.417 108.141 0.516 6.304 5.944 0.22 137364. 0.1538 26.62 0.5205 0.6364 0.0174 0.0142 0.131 4.135 1.177 97.849 0.467 5.234 5.454 0.22 137619. 0.1286 27.72 0.5422 0.5931 0.0138 0.0126 0.117 3.677 0.936 87.004 0.415 4.164 4.880 0.22 137884. 0.1026 28.83 0.5639 0.5280 0.0103 0.0110 0.101 3.197 0.697 75.652 0.361 3.099 4.177 0.22 138157. 0.0758 29.94 0.5855 0.4288 0.0068 0.0093 0.086 2.699 0.460 63.853 0.305 2.046 3.267 0.22 138440. 0.0481 31.05 0.6072 0.2709 0.0033 0.0075 0.069 2.184 0.227 51.673 0.247 1.008 1.990 0.22 138730. 0.0206 32.16 0.6289 -0.0047 0.0000 0.0057 0.052 1.653 -0.003 39.108 0.187 -0.013 -0.033 0.22 139021. 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 0.0816 0.0251 0.781 16.412 12.443 582.517 1.854 55.348 9.689 0.32 200650. 0.7427 1.67 0.0217 0.0687 0.0802 0.0254 0.791 16.612 12.228 589.631 1.877 54.391 9.406 0.32 200765. 0.7148 3.33 0.0434 0.1333 0.0787 0.0256 0.799 16.795 11.997 596.120 1.898 53.364 9.128 0.32 200888. 0.6871 5.00 0.0652 0.1940 0.0771 0.0259 0.807 16.956 11.751 601.839 1.916 52.267 8.856 0.32 201021. 0.6597 6.66 0.0869 0.2509 0.0754 0.0261 0.814 17.092 11.487 606.641 1.931 51.095 8.589 0.32 201163. 0.6326 8.33 0.1086 0.3041 0.0735 0.0263 0.819 17.197 11.207 610.375 1.943 49.847 8.328 0.32 201315. 0.6058 10.00 0.1303 0.3538 0.0716 0.0264 0.822 17.267 10.908 612.885 1.951 48.519 8.073 0.32 201478. 0.5794 11.66 0.1520 0.4000 0.0695 0.0264 0.823 17.299 10.591 614.012 1.954 47.110 7.824 0.32 201651. 0.5533 13.33 0.1738 0.4430 0.0673 0.0264 0.823 17.288 10.255 613.596 1.953 45.616 7.581 0.32 201836. 0.5276 14.99 0.1955 0.4827 0.0650 0.0263 0.820 17.228 9.900 611.472 1.946 44.037 7.344 0.32 202031. 0.5022 16.66 0.2172 0.5195 0.0625 0.0261 0.815 17.115 9.526 607.468 1.934 42.371 7.112 0.32 202238. 0.4771 18.33 0.2389 0.5533 0.0599 0.0259 0.806 16.944 9.131 601.399 1.914 40.614 6.886 0.32 202457. 0.4522 19.99 0.2606 0.5842 0.0572 0.0255 0.795 16.711 8.716 593.116 1.888 38.767 6.665 0.32 202688. 0.4276 21.66 0.2824 0.6122 0.0543 0.0251 0.781 16.413 8.281 582.547 1.854 36.836 6.448 0.32 202931. 0.4033 23.32 0.3041 0.6375 0.0514 0.0245 0.764 16.050 7.830 569.659 1.813 34.827 6.234 0.32 203187. 0.3791 24.99 0.3258 0.6598 0.0483 0.0238 0.744 15.621 7.362 554.430 1.765 32.745 6.023 0.32 203455. 0.3551 26.66 0.3475 0.6792 0.0451 0.0231 0.720 15.125 6.879 536.847 1.709 30.598 5.812 0.32 203735. 0.3313 28.32 0.3692 0.6954 0.0419 0.0222 0.693 14.563 6.383 516.901 1.645 28.391 5.601 0.32 204028. 0.3075 29.99 0.3910 0.7083 0.0385 0.0213 0.663 13.935 5.875 494.592 1.574 26.131 5.387 0.32 204334. 0.2838 31.65 0.4127 0.7174 0.0351 0.0202 0.630 13.240 5.356 469.926 1.496 23.823 5.169 0.32 204653. 0.2600 33.32 0.4344 0.7222 0.0317 0.0191 0.594 12.479 4.828 442.926 1.410 21.475 4.944 0.32 204984. 0.2361 34.99 0.4561 0.7220 0.0282 0.0178 0.555 11.654 4.293 413.626 1.317 19.094 4.707 0.32 205329. 0.2119 36.65 0.4778 0.7156 0.0246 0.0164 0.512 10.765 3.751 382.080 1.216 16.686 4.453 0.32 205687. 0.1874 38.32 0.4996 0.7013 0.0210 0.0150 0.467 9.815 3.206 348.364 1.109 14.262 4.175 0.33 206058. 0.1625 39.98 0.5213 0.6764 0.0174 0.0134 0.419 8.807 2.659 312.579 0.995 11.829 3.859 0.33 206443. 0.1368 41.65 0.5430 0.6367 0.0139 0.0118 0.369 7.744 2.113 274.859 0.875 9.398 3.487 0.33 206841. 0.1101 43.32 0.5647 0.5743 0.0103 0.0101 0.316 6.631 1.569 235.372 0.749 6.981 3.024 0.33 207252. 0.0823 44.98 0.5864 0.4748 0.0068 0.0084 0.261 5.475 1.032 194.326 0.619 4.589 2.408 0.33 207677. 0.0531 46.65 0.6082 0.3067 0.0033 0.0065 0.204 4.281 0.502 151.957 0.484 2.235 1.500 0.33 208114. 0.0231 48.31 0.6299 -0.0177 -0.0001 0.0047 0.145 3.046 -0.020 108.112 0.344 -0.089 -0.084 0.33 208545. 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 0.0826 0.0250 1.846 29.095 22.372 1376.905 3.287 99.512 7.370 0.43 267516. 0.7575 2.22 0.0217 0.0696 0.0811 0.0253 1.870 29.460 21.989 1394.204 3.328 97.807 7.154 0.43 267669. 0.7290 4.44 0.0434 0.1351 0.0796 0.0256 1.891 29.794 21.578 1409.991 3.366 95.978 6.941 0.43 267834. 0.7007 6.66 0.0651 0.1965 0.0780 0.0258 1.909 30.088 21.137 1423.910 3.399 94.020 6.733 0.43 268012. 0.6727 8.88 0.0868 0.2541 0.0763 0.0261 1.925 30.335 20.667 1435.608 3.427 91.928 6.530 0.43 268202. 0.6451 11.10 0.1085 0.3080 0.0744 0.0262 1.937 30.528 20.166 1444.717 3.449 89.697 6.331 0.43 268406. 0.6178 13.32 0.1302 0.3583 0.0724 0.0263 1.946 30.658 19.632 1450.861 3.464 87.322 6.137 0.43 268623. 0.5910 15.54 0.1519 0.4051 0.0704 0.0264 1.949 30.717 19.065 1453.654 3.470 84.800 5.949 0.43 268855. 0.5645 17.76 0.1736 0.4487 0.0681 0.0264 1.948 30.697 18.464 1452.707 3.468 82.126 5.765 0.43 269101. 0.5383 19.97 0.1953 0.4891 0.0658 0.0263 1.941 30.589 17.828 1447.626 3.456 79.297 5.586 0.43 269363. 0.5125 22.19 0.2170 0.5265 0.0633 0.0261 1.928 30.386 17.156 1437.997 3.433 76.310 5.411 0.43 269639. 0.4871 24.41 0.2387 0.5610 0.0607 0.0258 1.909 30.077 16.448 1423.371 3.398 73.159 5.241 0.43 269932. 0.4619 26.63 0.2604 0.5926 0.0579 0.0255 1.882 29.654 15.703 1403.379 3.350 69.846 5.075 0.43 270240. 0.4371 28.85 0.2821 0.6214 0.0551 0.0250 1.848 29.114 14.923 1377.833 3.289 66.379 4.913 0.43 270565. 0.4124 31.07 0.3038 0.6475 0.0521 0.0244 1.806 28.455 14.112 1346.648 3.215 62.770 4.753 0.43 270906. 0.3880 33.29 0.3255 0.6707 0.0490 0.0238 1.756 27.676 13.271 1309.771 3.127 59.030 4.596 0.43 271263. 0.3638 35.51 0.3472 0.6911 0.0458 0.0230 1.699 26.776 12.403 1267.166 3.025 55.170 4.440 0.43 271637. 0.3398 37.73 0.3689 0.7086 0.0425 0.0221 1.634 25.754 11.511 1218.810 2.910 51.202 4.284 0.43 272028. 0.3159 39.95 0.3906 0.7228 0.0391 0.0211 1.562 24.611 10.597 1164.700 2.781 47.136 4.127 0.43 272435. 0.2920 42.17 0.4123 0.7334 0.0357 0.0200 1.482 23.346 9.664 1104.854 2.638 42.984 3.967 0.43 272860. 0.2680 44.39 0.4340 0.7400 0.0322 0.0189 1.394 21.961 8.714 1039.320 2.481 38.759 3.803 0.43 273302. 0.2440 46.61 0.4557 0.7418 0.0286 0.0176 1.298 20.458 7.750 968.184 2.311 34.472 3.631 0.43 273762. 0.2197 48.83 0.4774 0.7379 0.0250 0.0162 1.196 18.839 6.776 891.572 2.128 30.139 3.447 0.43 274239. 0.1950 51.05 0.4991 0.7264 0.0214 0.0147 1.086 17.109 5.794 809.671 1.933 25.773 3.246 0.43 274733. 0.1698 53.27 0.5208 0.7048 0.0177 0.0131 0.969 15.272 4.809 722.726 1.725 21.392 3.018 0.43 275246. 0.1438 55.48 0.5425 0.6687 0.0141 0.0115 0.846 13.335 3.825 631.061 1.507 17.014 2.749 0.43 275776. 0.1168 57.70 0.5642 0.6103 0.0105 0.0097 0.718 11.307 2.846 535.087 1.277 12.658 2.412 0.44 276323. 0.0884 59.92 0.5859 0.5138 0.0069 0.0079 0.584 9.198 1.877 435.313 1.039 8.349 1.956 0.44 276889. 0.0582 62.14 0.6076 0.3435 0.0034 0.0060 0.446 7.022 0.924 332.322 0.793 4.109 1.261 0.44 277471. 0.0263 64.36 0.6293 -0.0099 -0.0001 0.0041 0.303 4.770 -0.018 225.724 0.539 -0.078 -0.035 0.44 278044. 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 0.0838 0.0252 3.639 45.871 35.487 2713.564 5.183 157.845 5.932 0.54 334363. 0.7679 2.78 0.0218 0.0703 0.0824 0.0255 3.686 46.460 34.884 2748.359 5.249 155.163 5.757 0.54 334557. 0.7389 5.57 0.0436 0.1364 0.0809 0.0258 3.728 46.996 34.235 2780.078 5.310 152.279 5.586 0.54 334766. 0.7102 8.35 0.0653 0.1984 0.0792 0.0261 3.766 47.468 33.541 2807.986 5.363 149.189 5.418 0.54 334990. 0.6819 11.14 0.0871 0.2565 0.0775 0.0263 3.797 47.863 32.797 2831.367 5.408 145.882 5.254 0.54 335231. 0.6539 13.92 0.1089 0.3109 0.0756 0.0265 3.821 48.169 32.003 2849.477 5.442 142.351 5.094 0.54 335488. 0.6263 16.71 0.1307 0.3617 0.0736 0.0266 3.837 48.373 31.157 2861.544 5.465 138.587 4.939 0.54 335763. 0.5991 19.49 0.1525 0.4091 0.0715 0.0266 3.844 48.462 30.257 2866.790 5.475 134.584 4.787 0.54 336055. 0.5723 22.28 0.1742 0.4531 0.0692 0.0266 3.841 48.422 29.302 2864.425 5.471 130.335 4.640 0.54 336366. 0.5458 25.06 0.1960 0.4940 0.0668 0.0265 3.827 48.240 28.291 2853.652 5.450 125.837 4.497 0.54 336697. 0.5198 27.84 0.2178 0.5319 0.0643 0.0263 3.800 47.901 27.222 2833.647 5.412 121.082 4.357 0.54 337046. 0.4940 30.63 0.2396 0.5669 0.0616 0.0260 3.760 47.392 26.093 2803.505 5.354 116.063 4.222 0.54 337415. 0.4686 33.41 0.2614 0.5990 0.0588 0.0257 3.705 46.698 24.906 2762.463 5.276 110.780 4.089 0.54 337804. 0.4435 36.20 0.2832 0.6284 0.0559 0.0252 3.634 45.814 23.662 2710.141 5.176 105.249 3.960 0.54 338214. 0.4186 38.98 0.3049 0.6551 0.0528 0.0246 3.549 44.735 22.367 2646.368 5.054 99.487 3.833 0.54 338644. 0.3940 41.77 0.3267 0.6791 0.0497 0.0239 3.448 43.462 21.024 2571.042 4.910 93.513 3.709 0.54 339095. 0.3696 44.55 0.3485 0.7003 0.0464 0.0231 3.331 41.992 19.637 2484.089 4.744 87.345 3.585 0.54 339567. 0.3453 47.34 0.3703 0.7186 0.0430 0.0222 3.199 40.325 18.211 2385.474 4.556 81.001 3.463 0.54 340060. 0.3211 50.12 0.3921 0.7337 0.0396 0.0211 3.051 38.461 16.749 2275.193 4.345 74.500 3.339 0.54 340574. 0.2970 52.91 0.4138 0.7453 0.0360 0.0200 2.888 36.400 15.256 2153.290 4.112 67.860 3.214 0.54 341109. 0.2728 55.69 0.4356 0.7531 0.0324 0.0188 2.709 34.145 13.737 2019.865 3.858 61.101 3.085 0.54 341666. 0.2485 58.47 0.4574 0.7562 0.0288 0.0174 2.515 31.698 12.195 1875.101 3.581 54.244 2.950 0.54 342245. 0.2239 61.26 0.4792 0.7536 0.0251 0.0160 2.306 29.063 10.636 1719.271 3.284 47.311 2.806 0.54 342846. 0.1989 64.04 0.5010 0.7435 0.0214 0.0144 2.082 26.249 9.066 1552.756 2.966 40.326 2.648 0.54 343469. 0.1733 66.83 0.5227 0.7233 0.0177 0.0128 1.845 23.262 7.490 1376.077 2.628 33.318 2.469 0.54 344114. 0.1468 69.61 0.5445 0.6882 0.0140 0.0111 1.596 20.115 5.916 1189.913 2.273 26.315 2.255 0.54 344781. 0.1192 72.40 0.5663 0.6294 0.0103 0.0092 1.334 16.822 4.351 995.126 1.901 19.353 1.983 0.54 345471. 0.0899 75.18 0.5881 0.5285 0.0066 0.0074 1.063 13.402 2.803 792.784 1.514 12.467 1.604 0.54 346183. 0.0583 77.97 0.6099 0.3400 0.0030 0.0054 0.783 9.874 1.281 584.096 1.116 5.697 0.995 0.55 346915. 0.0245 80.75 0.6316 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 0.0855 0.0257 6.413 67.366 52.113 4782.131 7.611 231.798 4.943 0.64 401185. 0.7754 3.32 0.0216 0.0699 0.0841 0.0260 6.496 68.234 51.248 4843.748 7.709 227.953 4.799 0.64 401418. 0.7466 6.64 0.0433 0.1356 0.0825 0.0263 6.571 69.025 50.318 4899.869 7.798 223.813 4.658 0.64 401669. 0.7180 9.96 0.0649 0.1974 0.0809 0.0266 6.637 69.720 49.318 4949.206 7.877 219.368 4.520 0.64 401938. 0.6898 13.28 0.0866 0.2553 0.0791 0.0268 6.692 70.301 48.248 4990.493 7.943 214.605 4.385 0.64 402227. 0.6619 16.60 0.1082 0.3096 0.0773 0.0270 6.735 70.751 47.102 5022.411 7.993 209.512 4.254 0.64 402535. 0.6345 19.92 0.1299 0.3603 0.0753 0.0271 6.764 71.050 45.880 5043.613 8.027 204.076 4.126 0.64 402865. 0.6074 23.24 0.1515 0.4077 0.0731 0.0272 6.776 71.178 44.579 5052.742 8.042 198.287 4.002 0.64 403215. 0.5806 26.56 0.1731 0.4519 0.0708 0.0271 6.770 71.117 43.196 5048.408 8.035 192.137 3.881 0.64 403588. 0.5543 29.88 0.1948 0.4930 0.0684 0.0270 6.744 70.847 41.731 5029.233 8.004 185.618 3.764 0.64 403983. 0.5284 33.20 0.2164 0.5312 0.0659 0.0269 6.697 70.348 40.180 4993.792 7.948 178.722 3.649 0.64 404401. 0.5027 36.52 0.2381 0.5665 0.0632 0.0266 6.625 69.598 38.543 4940.549 7.863 171.438 3.538 0.64 404842. 0.4774 39.84 0.2597 0.5992 0.0604 0.0262 6.528 68.577 36.817 4868.101 7.748 163.763 3.430 0.64 405307. 0.4523 43.16 0.2814 0.6291 0.0574 0.0257 6.404 67.275 35.008 4775.686 7.601 155.717 3.325 0.65 405796. 0.4275 46.48 0.3030 0.6565 0.0543 0.0251 6.253 65.688 33.122 4662.985 7.421 147.325 3.222 0.65 406309. 0.4029 49.80 0.3246 0.6813 0.0511 0.0244 6.075 63.812 31.163 4529.838 7.209 138.615 3.120 0.65 406846. 0.3786 53.12 0.3463 0.7034 0.0478 0.0235 5.868 61.647 29.140 4376.134 6.965 129.615 3.020 0.65 407408. 0.3543 56.44 0.3679 0.7227 0.0444 0.0226 5.635 59.191 27.057 4201.812 6.687 120.351 2.921 0.65 407995. 0.3302 59.76 0.3896 0.7391 0.0409 0.0215 5.373 56.445 24.921 4006.872 6.377 110.848 2.821 0.65 408607. 0.3060 63.08 0.4112 0.7522 0.0373 0.0204 5.084 53.410 22.737 3791.395 6.034 101.135 2.720 0.65 409244. 0.2819 66.40 0.4328 0.7617 0.0336 0.0191 4.768 50.087 20.513 3555.556 5.659 91.240 2.617 0.65 409907. 0.2576 69.72 0.4545 0.7670 0.0299 0.0177 4.425 46.483 18.254 3299.659 5.252 81.193 2.509 0.65 410595. 0.2330 73.04 0.4761 0.7669 0.0262 0.0163 4.055 42.602 15.968 3024.166 4.813 71.026 2.395 0.65 411309. 0.2080 76.36 0.4978 0.7600 0.0224 0.0147 3.661 38.454 13.663 2729.727 4.344 60.775 2.270 0.65 412049. 0.1824 79.68 0.5194 0.7439 0.0186 0.0130 3.242 34.052 11.349 2417.231 3.847 50.479 2.129 0.65 412815. 0.1559 83.00 0.5411 0.7141 0.0148 0.0112 2.800 29.411 9.034 2087.835 3.323 40.182 1.963 0.65 413607. 0.1282 86.32 0.5627 0.6627 0.0110 0.0094 2.337 24.554 6.730 1743.021 2.774 29.933 1.751 0.65 414426. 0.0987 89.64 0.5843 0.5727 0.0073 0.0074 1.857 19.505 4.448 1384.631 2.204 19.786 1.457 0.65 415271. 0.0668 92.96 0.6060 0.4012 0.0036 0.0055 1.361 14.296 2.203 1014.822 1.615 9.798 0.985 0.65 416140. 0.0318 96.28 0.6276 -0.0051 0.0000 0.0034 0.847 8.902 -0.017 631.945 1.006 -0.075 -0.012 0.66 416990. 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 0.0877 0.0267 10.567 95.145 72.752 7879.768 10.749 323.601 4.188 0.75 467969. 0.7762 3.87 0.0216 0.0690 0.0863 0.0270 10.691 96.266 71.581 7972.541 10.876 318.390 4.072 0.75 468243. 0.7488 7.73 0.0432 0.1342 0.0847 0.0273 10.805 97.287 70.315 8057.141 10.991 312.760 3.958 0.75 468538. 0.7213 11.60 0.0648 0.1956 0.0831 0.0275 10.905 98.185 68.952 8131.494 11.093 306.697 3.846 0.75 468854. 0.6941 15.46 0.0864 0.2533 0.0813 0.0277 10.988 98.933 67.487 8193.500 11.177 300.181 3.736 0.75 469194. 0.6670 19.33 0.1080 0.3074 0.0794 0.0279 11.051 99.506 65.916 8240.942 11.242 293.193 3.628 0.75 469557. 0.6401 23.20 0.1296 0.3582 0.0774 0.0280 11.092 99.876 64.235 8271.533 11.284 285.716 3.522 0.75 469944. 0.6135 27.06 0.1512 0.4057 0.0752 0.0280 11.108 100.013 62.441 8282.905 11.299 277.736 3.419 0.75 470356. 0.5872 30.93 0.1728 0.4500 0.0729 0.0280 11.094 99.889 60.531 8272.652 11.285 269.241 3.319 0.75 470793. 0.5611 34.80 0.1944 0.4913 0.0705 0.0279 11.048 99.475 58.502 8238.324 11.239 260.218 3.221 0.75 471257. 0.5354 38.66 0.2160 0.5298 0.0679 0.0277 10.966 98.740 56.353 8177.465 11.156 250.658 3.126 0.75 471747. 0.5099 42.53 0.2376 0.5655 0.0652 0.0274 10.845 97.652 54.080 8087.399 11.033 240.546 3.033 0.75 472264. 0.4847 46.39 0.2592 0.5985 0.0623 0.0270 10.682 96.182 51.681 7965.609 10.867 229.876 2.943 0.75 472809. 0.4597 50.26 0.2808 0.6290 0.0592 0.0264 10.474 94.311 49.161 7810.671 10.655 218.669 2.855 0.75 473381. 0.4350 54.13 0.3024 0.6570 0.0561 0.0258 10.221 92.034 46.530 7622.063 10.398 206.963 2.769 0.75 473982. 0.4105 57.99 0.3240 0.6825 0.0528 0.0251 9.923 89.347 43.795 7399.558 10.094 194.800 2.684 0.75 474611. 0.3861 61.86 0.3456 0.7054 0.0494 0.0242 9.579 86.250 40.966 7143.049 9.744 182.216 2.601 0.75 475268. 0.3618 65.72 0.3672 0.7257 0.0459 0.0232 9.189 82.742 38.051 6852.523 9.348 169.249 2.519 0.75 475954. 0.3376 69.59 0.3888 0.7431 0.0422 0.0221 8.754 78.825 35.058 6528.111 8.906 155.937 2.436 0.76 476668. 0.3134 73.46 0.4104 0.7574 0.0386 0.0209 8.274 74.502 31.996 6170.095 8.417 142.317 2.352 0.76 477412. 0.2891 77.32 0.4320 0.7682 0.0348 0.0196 7.750 69.779 28.874 5778.953 7.884 128.431 2.266 0.76 478185. 0.2646 81.19 0.4536 0.7748 0.0310 0.0181 7.182 64.665 25.701 5355.435 7.306 114.319 2.177 0.76 478987. 0.2398 85.06 0.4752 0.7761 0.0271 0.0166 6.572 59.173 22.488 4900.632 6.685 100.027 2.081 0.76 479819. 0.2145 88.92 0.4968 0.7706 0.0232 0.0150 5.922 53.322 19.246 4416.033 6.024 85.605 1.977 0.76 480681. 0.1885 92.79 0.5184 0.7556 0.0193 0.0132 5.235 47.135 15.987 3903.646 5.325 71.108 1.857 0.76 481573. 0.1614 96.65 0.5400 0.7265 0.0153 0.0114 4.514 40.644 12.724 3366.061 4.592 56.598 1.715 0.76 482495. 0.1329 100.52 0.5616 0.6747 0.0114 0.0095 3.764 33.888 9.474 2806.550 3.829 42.142 1.531 0.76 483448. 0.1024 104.39 0.5832 0.5823 0.0075 0.0075 2.989 26.916 6.254 2229.117 3.041 27.817 1.273 0.76 484431. 0.0692 108.25 0.6048 0.4048 0.0037 0.0055 2.197 19.783 3.081 1638.383 2.235 13.706 0.853 0.76 485442. 0.0325 112.12 0.6264 -0.0128 -0.0001 0.0035 1.383 12.452 -0.059 1031.241 1.407 -0.264 -0.026 0.76 486425. 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 0.0905 0.0310 18.327 144.392 98.055 13666.633 16.313 436.146 3.254 0.86 534695. 0.7003 4.42 0.0216 0.0618 0.0891 0.0311 18.382 144.823 96.558 13707.437 16.362 429.488 3.195 0.86 535011. 0.6823 8.83 0.0432 0.1214 0.0876 0.0312 18.417 145.099 94.930 13733.565 16.393 422.247 3.135 0.86 535352. 0.6638 13.25 0.0648 0.1786 0.0860 0.0312 18.430 145.198 93.166 13742.932 16.404 414.403 3.075 0.86 535718. 0.6450 17.66 0.0863 0.2334 0.0842 0.0312 18.417 145.097 91.260 13733.362 16.393 405.926 3.014 0.86 536110. 0.6257 22.08 0.1079 0.2858 0.0823 0.0311 18.375 144.771 89.206 13702.488 16.356 396.789 2.953 0.86 536530. 0.6061 26.49 0.1295 0.3358 0.0803 0.0310 18.302 144.195 86.998 13647.946 16.291 386.966 2.891 0.86 536977. 0.5861 30.91 0.1511 0.3834 0.0781 0.0308 18.194 143.342 84.631 13567.214 16.195 376.437 2.829 0.86 537453. 0.5656 35.32 0.1727 0.4285 0.0757 0.0305 18.047 142.185 82.101 13457.701 16.064 365.185 2.767 0.86 537959. 0.5449 39.74 0.1943 0.4712 0.0733 0.0302 17.858 140.694 79.405 13316.624 15.896 353.193 2.705 0.86 538494. 0.5237 44.15 0.2159 0.5114 0.0706 0.0298 17.622 138.839 76.540 13141.044 15.686 340.448 2.642 0.86 539060. 0.5023 48.57 0.2374 0.5491 0.0678 0.0293 17.336 136.584 73.501 12927.605 15.431 326.934 2.579 0.86 539657. 0.4805 52.98 0.2590 0.5843 0.0648 0.0287 16.994 133.890 70.287 12672.633 15.127 312.635 2.516 0.86 540285. 0.4583 57.40 0.2806 0.6171 0.0617 0.0281 16.593 130.732 66.902 12373.672 14.770 297.578 2.452 0.86 540945. 0.4359 61.82 0.3022 0.6474 0.0585 0.0273 16.132 127.095 63.357 12029.515 14.359 281.814 2.389 0.86 541636. 0.4132 66.23 0.3238 0.6750 0.0550 0.0264 15.611 122.995 59.666 11641.378 13.896 265.396 2.325 0.86 542360. 0.3902 70.65 0.3454 0.6993 0.0515 0.0254 15.043 118.519 55.839 11217.732 13.390 248.373 2.258 0.86 543116. 0.3666 75.06 0.3670 0.7201 0.0479 0.0244 14.422 113.623 51.889 10754.365 12.837 230.802 2.188 0.86 543904. 0.3426 79.48 0.3886 0.7372 0.0441 0.0233 13.750 108.328 47.827 10253.224 12.239 212.733 2.116 0.86 544724. 0.3180 83.89 0.4101 0.7495 0.0403 0.0220 13.032 102.671 43.664 9717.727 11.600 194.217 2.038 0.86 545578. 0.2927 88.31 0.4317 0.7572 0.0364 0.0207 12.258 96.575 39.415 9140.792 10.911 175.317 1.956 0.86 546464. 0.2668 92.72 0.4533 0.7589 0.0324 0.0193 11.432 90.070 35.092 8525.094 10.176 156.090 1.867 0.87 547384. 0.2404 97.14 0.4749 0.7532 0.0283 0.0179 10.561 83.204 30.710 7875.169 9.400 136.599 1.769 0.87 548337. 0.2130 101.55 0.4965 0.7376 0.0242 0.0163 9.650 76.025 26.284 7195.700 8.589 116.912 1.657 0.87 549323. 0.1846 105.97 0.5181 0.7086 0.0201 0.0147 8.706 68.593 21.832 6492.269 7.750 97.107 1.525 0.87 550344. 0.1549 110.38 0.5397 0.6607 0.0160 0.0131 7.740 60.976 17.372 5771.345 6.889 77.271 1.365 0.87 551398. 0.1237 114.80 0.5612 0.5854 0.0119 0.0114 6.759 53.253 12.926 5040.321 6.016 57.497 1.163 0.87 552487. 0.0909 119.22 0.5828 0.4689 0.0079 0.0098 5.776 45.505 8.519 4307.070 5.141 37.894 0.897 0.87 553610. 0.0569 123.63 0.6044 0.2869 0.0039 0.0081 4.800 37.820 4.177 3579.679 4.273 18.580 0.529 0.87 554765. 0.0235 128.05 0.6260 -0.0106 -0.0001 0.0065 3.819 30.089 -0.118 2847.888 3.399 -0.526 -0.019 0.87 555908. 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 0.0912 0.0406 34.174 239.324 125.070 25483.361 27.039 556.309 2.226 0.96 601485. 0.5410 5.19 0.0225 0.0499 0.0900 0.0406 34.205 239.541 123.433 25506.475 27.063 549.028 2.195 0.96 601847. 0.5300 10.38 0.0451 0.0985 0.0886 0.0406 34.175 239.329 121.610 25483.939 27.039 540.923 2.164 0.96 602239. 0.5187 15.56 0.0676 0.1457 0.0872 0.0405 34.073 238.616 119.588 25407.928 26.959 531.925 2.135 0.96 602664. 0.5073 20.75 0.0902 0.1916 0.0855 0.0403 33.892 237.353 117.352 25273.537 26.816 521.980 2.106 0.96 603123. 0.4958 25.94 0.1127 0.2363 0.0837 0.0399 33.626 235.491 114.888 25075.221 26.606 511.022 2.078 0.96 603617. 0.4841 31.13 0.1353 0.2799 0.0818 0.0395 33.269 232.985 112.185 24808.375 26.323 498.997 2.051 0.96 604148. 0.4721 36.32 0.1578 0.3224 0.0796 0.0390 32.814 229.804 109.230 24469.695 25.963 485.855 2.025 0.97 604715. 0.4599 41.50 0.1804 0.3637 0.0773 0.0383 32.261 225.929 106.016 24057.053 25.525 471.557 1.999 0.97 605320. 0.4473 46.69 0.2029 0.4039 0.0747 0.0375 31.607 221.351 102.535 23569.541 25.008 456.076 1.973 0.97 605964. 0.4342 51.88 0.2255 0.4429 0.0720 0.0367 30.853 216.067 98.783 23006.967 24.411 439.387 1.947 0.97 606646. 0.4206 57.07 0.2480 0.4807 0.0691 0.0356 29.998 210.078 94.754 22369.275 23.735 421.466 1.921 0.97 607368. 0.4064 62.26 0.2705 0.5170 0.0659 0.0345 29.042 203.386 90.448 21656.674 22.978 402.310 1.894 0.97 608129. 0.3915 67.45 0.2931 0.5518 0.0626 0.0333 27.990 196.017 85.877 20872.016 22.146 381.983 1.866 0.97 608930. 0.3758 72.63 0.3156 0.5848 0.0591 0.0319 26.847 188.010 81.065 20019.473 21.241 360.577 1.837 0.97 609771. 0.3594 77.82 0.3382 0.6159 0.0554 0.0304 25.618 179.403 76.031 19102.986 20.269 338.188 1.805 0.97 610651. 0.3421 83.01 0.3607 0.6444 0.0516 0.0289 24.319 170.308 70.797 18134.467 19.241 314.905 1.771 0.97 611571. 0.3238 88.20 0.3833 0.6676 0.0477 0.0274 23.029 161.277 65.375 17172.863 18.221 290.789 1.727 0.97 612531. 0.3034 93.39 0.4058 0.6845 0.0436 0.0258 21.751 152.329 59.789 16220.035 17.210 265.941 1.672 0.97 613531. 0.2809 98.57 0.4284 0.6891 0.0394 0.0245 20.618 144.388 54.049 15374.520 16.313 240.408 1.595 0.97 614571. 0.2548 103.76 0.4509 0.6765 0.0351 0.0234 19.703 137.984 48.171 14692.625 15.589 214.266 1.487 0.97 615651. 0.2243 108.95 0.4735 0.6534 0.0308 0.0223 18.768 131.436 42.212 13995.340 14.850 187.759 1.368 0.97 616771. 0.1932 114.14 0.4960 0.6181 0.0264 0.0212 17.826 124.836 36.202 13292.622 14.104 161.028 1.235 0.98 617932. 0.1615 119.33 0.5186 0.5686 0.0220 0.0201 16.889 118.274 30.179 12593.929 13.363 134.235 1.087 0.98 619134. 0.1298 124.51 0.5411 0.5027 0.0176 0.0190 15.971 111.848 24.182 11909.632 12.637 107.563 0.921 0.98 620377. 0.0984 129.70 0.5636 0.4188 0.0133 0.0179 15.079 105.603 18.260 11244.654 11.931 81.221 0.737 0.98 621662. 0.0684 134.89 0.5862 0.3151 0.0091 0.0169 14.220 99.588 12.459 10604.178 11.251 55.416 0.533 0.98 622991. 0.0409 140.08 0.6087 0.1900 0.0050 0.0159 13.398 93.826 6.815 9990.635 10.600 30.311 0.309 0.98 624370. 0.0176 145.27 0.6313 0.0398 0.0009 0.0149 12.572 88.041 1.292 9374.608 9.947 5.748 0.063 0.98 625833. 0.0015 150.46 0.6538