18x12E (18x12E.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 0.0975 0.0408 0.006 0.391 0.326 4.630 0.044 1.451 31.959 0.07 29880. 0.5950 0.48 0.0280 0.0651 0.0965 0.0415 0.006 0.398 0.323 4.707 0.045 1.435 31.098 0.07 29903. 0.5759 0.96 0.0561 0.1266 0.0953 0.0422 0.006 0.404 0.319 4.782 0.046 1.418 30.232 0.07 29927. 0.5564 1.43 0.0841 0.1845 0.0940 0.0428 0.007 0.410 0.314 4.856 0.046 1.399 29.367 0.07 29955. 0.5368 1.91 0.1121 0.2388 0.0925 0.0434 0.007 0.416 0.310 4.926 0.047 1.377 28.505 0.07 29985. 0.5170 2.39 0.1401 0.2896 0.0910 0.0440 0.007 0.422 0.304 4.991 0.048 1.354 27.651 0.07 30017. 0.4972 2.87 0.1682 0.3369 0.0892 0.0445 0.007 0.427 0.298 5.050 0.048 1.327 26.807 0.07 30053. 0.4774 3.34 0.1962 0.3809 0.0873 0.0450 0.007 0.431 0.292 5.099 0.049 1.299 25.977 0.07 30091. 0.4576 3.82 0.2242 0.4216 0.0852 0.0453 0.007 0.434 0.285 5.137 0.049 1.268 25.160 0.07 30133. 0.4378 4.30 0.2523 0.4592 0.0829 0.0455 0.007 0.436 0.277 5.162 0.049 1.233 24.360 0.07 30178. 0.4181 4.78 0.2803 0.4938 0.0804 0.0456 0.007 0.437 0.269 5.172 0.049 1.196 23.576 0.07 30226. 0.3985 5.26 0.3083 0.5255 0.0776 0.0456 0.007 0.437 0.260 5.165 0.049 1.155 22.808 0.07 30277. 0.3789 5.73 0.3363 0.5543 0.0747 0.0453 0.007 0.434 0.250 5.139 0.049 1.111 22.055 0.07 30332. 0.3594 6.21 0.3644 0.5804 0.0715 0.0449 0.007 0.430 0.239 5.091 0.049 1.064 21.314 0.07 30390. 0.3398 6.69 0.3924 0.6036 0.0681 0.0443 0.007 0.424 0.228 5.021 0.048 1.014 20.583 0.07 30452. 0.3203 7.17 0.4204 0.6238 0.0645 0.0435 0.007 0.416 0.216 4.927 0.047 0.959 19.856 0.07 30517. 0.3006 7.64 0.4485 0.6410 0.0606 0.0424 0.006 0.406 0.203 4.809 0.046 0.902 19.129 0.07 30585. 0.2808 8.12 0.4765 0.6549 0.0565 0.0411 0.006 0.394 0.189 4.664 0.045 0.841 18.394 0.07 30657. 0.2608 8.60 0.5045 0.6651 0.0523 0.0396 0.006 0.380 0.175 4.495 0.043 0.778 17.643 0.07 30732. 0.2405 9.08 0.5325 0.6712 0.0478 0.0380 0.006 0.364 0.160 4.303 0.041 0.712 16.865 0.07 30810. 0.2199 9.56 0.5606 0.6723 0.0433 0.0361 0.005 0.346 0.145 4.089 0.039 0.644 16.049 0.07 30892. 0.1990 10.03 0.5886 0.6676 0.0386 0.0340 0.005 0.326 0.129 3.855 0.037 0.574 15.179 0.07 30977. 0.1777 10.51 0.6166 0.6558 0.0338 0.0318 0.005 0.304 0.113 3.602 0.034 0.503 14.233 0.07 31066. 0.1560 10.99 0.6447 0.6351 0.0289 0.0294 0.004 0.282 0.097 3.332 0.032 0.431 13.184 0.07 31158. 0.1338 11.47 0.6727 0.6029 0.0241 0.0269 0.004 0.257 0.081 3.045 0.029 0.358 11.994 0.07 31253. 0.1109 11.94 0.7007 0.5553 0.0192 0.0242 0.004 0.232 0.064 2.744 0.026 0.285 10.604 0.07 31351. 0.0876 12.42 0.7288 0.4861 0.0143 0.0214 0.003 0.205 0.048 2.429 0.023 0.213 8.927 0.07 31453. 0.0636 12.90 0.7568 0.3856 0.0095 0.0186 0.003 0.178 0.032 2.104 0.020 0.141 6.818 0.07 31558. 0.0395 13.38 0.7848 0.2361 0.0047 0.0156 0.002 0.150 0.016 1.771 0.017 0.070 4.026 0.07 31666. 0.0165 13.86 0.8128 0.0037 0.0001 0.0126 0.002 0.121 0.000 1.432 0.014 0.001 0.061 0.07 31778. 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 0.0979 0.0379 0.046 1.452 1.309 34.363 0.164 5.824 17.284 0.14 59760. 0.6447 0.96 0.0282 0.0707 0.0968 0.0386 0.047 1.480 1.295 35.014 0.167 5.762 16.780 0.14 59805. 0.6226 1.92 0.0564 0.1371 0.0956 0.0393 0.048 1.507 1.280 35.663 0.170 5.692 16.276 0.14 59855. 0.6002 2.88 0.0845 0.1993 0.0943 0.0400 0.049 1.534 1.262 36.297 0.173 5.615 15.774 0.14 59910. 0.5777 3.84 0.1127 0.2574 0.0929 0.0407 0.049 1.560 1.243 36.905 0.176 5.529 15.278 0.14 59970. 0.5553 4.80 0.1409 0.3114 0.0913 0.0413 0.050 1.584 1.222 37.473 0.179 5.435 14.790 0.14 60036. 0.5329 5.76 0.1691 0.3616 0.0896 0.0419 0.051 1.605 1.198 37.986 0.181 5.331 14.310 0.14 60107. 0.5107 6.72 0.1972 0.4080 0.0876 0.0424 0.052 1.624 1.173 38.428 0.183 5.216 13.840 0.14 60185. 0.4886 7.68 0.2254 0.4509 0.0855 0.0428 0.052 1.639 1.144 38.781 0.185 5.090 13.382 0.14 60269. 0.4666 8.65 0.2536 0.4903 0.0832 0.0430 0.052 1.649 1.113 39.028 0.186 4.951 12.937 0.14 60360. 0.4449 9.61 0.2818 0.5266 0.0807 0.0432 0.053 1.655 1.079 39.151 0.187 4.801 12.504 0.14 60457. 0.4235 10.57 0.3100 0.5598 0.0779 0.0431 0.052 1.654 1.043 39.133 0.187 4.637 12.083 0.14 60561. 0.4022 11.53 0.3381 0.5900 0.0749 0.0429 0.052 1.646 1.003 38.955 0.186 4.460 11.675 0.14 60671. 0.3811 12.49 0.3663 0.6174 0.0717 0.0426 0.052 1.631 0.960 38.603 0.184 4.269 11.277 0.14 60788. 0.3601 13.45 0.3945 0.6420 0.0683 0.0420 0.051 1.609 0.914 38.064 0.182 4.064 10.888 0.14 60913. 0.3393 14.41 0.4227 0.6637 0.0646 0.0411 0.050 1.577 0.865 37.326 0.178 3.846 10.507 0.14 61044. 0.3185 15.37 0.4508 0.6826 0.0607 0.0401 0.049 1.537 0.812 36.379 0.174 3.614 10.130 0.14 61182. 0.2976 16.33 0.4790 0.6983 0.0566 0.0388 0.047 1.488 0.757 35.214 0.168 3.368 9.754 0.14 61326. 0.2767 17.29 0.5072 0.7107 0.0523 0.0373 0.045 1.430 0.700 33.840 0.162 3.112 9.376 0.14 61478. 0.2556 18.25 0.5354 0.7193 0.0478 0.0356 0.043 1.364 0.640 32.268 0.154 2.845 8.990 0.14 61636. 0.2344 19.21 0.5636 0.7236 0.0432 0.0336 0.041 1.289 0.578 30.511 0.146 2.570 8.591 0.15 61802. 0.2129 20.17 0.5917 0.7225 0.0385 0.0315 0.038 1.208 0.515 28.578 0.136 2.290 8.170 0.15 61974. 0.1911 21.13 0.6199 0.7149 0.0337 0.0292 0.036 1.119 0.451 26.480 0.126 2.004 7.717 0.15 62152. 0.1688 22.09 0.6481 0.6990 0.0288 0.0267 0.032 1.024 0.385 24.227 0.116 1.715 7.217 0.15 62338. 0.1461 23.05 0.6763 0.6719 0.0239 0.0241 0.029 0.923 0.320 21.832 0.104 1.423 6.648 0.15 62530. 0.1226 24.02 0.7044 0.6293 0.0190 0.0213 0.026 0.816 0.254 19.307 0.092 1.132 5.977 0.15 62729. 0.0983 24.98 0.7326 0.5636 0.0141 0.0184 0.022 0.704 0.189 16.669 0.080 0.841 5.148 0.15 62935. 0.0730 25.94 0.7608 0.4613 0.0093 0.0154 0.019 0.589 0.125 13.938 0.067 0.554 4.057 0.15 63147. 0.0467 26.90 0.7890 0.2947 0.0046 0.0123 0.015 0.471 0.061 11.134 0.053 0.273 2.499 0.15 63366. 0.0202 27.86 0.8172 -0.0021 0.0000 0.0091 0.011 0.350 0.000 8.282 0.040 -0.001 -0.017 0.15 63590. 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 0.0982 0.0367 0.151 3.163 2.956 112.267 0.357 13.148 11.942 0.21 89638. 0.6693 1.44 0.0282 0.0733 0.0971 0.0374 0.154 3.227 2.924 114.531 0.365 13.008 11.582 0.21 89706. 0.6456 2.89 0.0565 0.1420 0.0960 0.0381 0.157 3.290 2.890 116.791 0.372 12.853 11.222 0.21 89781. 0.6218 4.33 0.0847 0.2063 0.0947 0.0389 0.160 3.353 2.851 119.007 0.379 12.680 10.865 0.21 89863. 0.5980 5.77 0.1129 0.2661 0.0932 0.0396 0.162 3.413 2.808 121.136 0.386 12.488 10.512 0.21 89954. 0.5742 7.22 0.1412 0.3217 0.0917 0.0402 0.165 3.469 2.760 123.133 0.392 12.276 10.166 0.21 90053. 0.5505 8.66 0.1694 0.3732 0.0899 0.0408 0.168 3.520 2.707 124.945 0.398 12.041 9.827 0.21 90161. 0.5271 10.11 0.1976 0.4208 0.0880 0.0413 0.170 3.564 2.649 126.515 0.403 11.783 9.497 0.21 90278. 0.5039 11.55 0.2259 0.4646 0.0859 0.0417 0.171 3.600 2.585 127.786 0.407 11.499 9.176 0.21 90405. 0.4809 12.99 0.2541 0.5049 0.0835 0.0420 0.173 3.626 2.515 128.695 0.410 11.187 8.864 0.21 90541. 0.4583 14.44 0.2823 0.5420 0.0810 0.0422 0.173 3.640 2.439 129.180 0.411 10.848 8.563 0.22 90687. 0.4359 15.88 0.3106 0.5758 0.0782 0.0422 0.173 3.639 2.356 129.178 0.411 10.478 8.271 0.22 90843. 0.4138 17.32 0.3388 0.6067 0.0752 0.0420 0.172 3.624 2.266 128.632 0.409 10.078 7.989 0.22 91010. 0.3920 18.77 0.3670 0.6348 0.0720 0.0416 0.171 3.592 2.169 127.486 0.406 9.646 7.715 0.22 91186. 0.3704 20.21 0.3953 0.6601 0.0686 0.0411 0.169 3.541 2.064 125.694 0.400 9.183 7.450 0.22 91373. 0.3489 21.66 0.4235 0.6826 0.0649 0.0402 0.165 3.472 1.953 123.216 0.392 8.689 7.191 0.22 91571. 0.3276 23.10 0.4517 0.7024 0.0610 0.0392 0.161 3.381 1.835 120.012 0.382 8.163 6.936 0.22 91778. 0.3063 24.54 0.4799 0.7192 0.0568 0.0379 0.156 3.270 1.710 116.056 0.369 7.607 6.684 0.22 91996. 0.2850 25.99 0.5082 0.7328 0.0525 0.0364 0.149 3.138 1.580 111.372 0.355 7.026 6.433 0.22 92225. 0.2635 27.43 0.5364 0.7430 0.0480 0.0346 0.142 2.986 1.444 105.998 0.337 6.422 6.178 0.22 92463. 0.2420 28.87 0.5646 0.7490 0.0433 0.0327 0.134 2.817 1.304 99.974 0.318 5.801 5.917 0.22 92712. 0.2203 30.32 0.5929 0.7501 0.0386 0.0305 0.125 2.630 1.161 93.334 0.297 5.166 5.644 0.22 92971. 0.1983 31.76 0.6211 0.7452 0.0337 0.0281 0.115 2.426 1.016 86.113 0.274 4.520 5.352 0.22 93240. 0.1759 33.21 0.6493 0.7325 0.0289 0.0256 0.105 2.207 0.869 78.347 0.249 3.866 5.032 0.22 93519. 0.1529 34.65 0.6776 0.7091 0.0240 0.0229 0.094 1.974 0.721 70.078 0.223 3.208 4.669 0.22 93809. 0.1293 36.09 0.7058 0.6706 0.0190 0.0200 0.082 1.729 0.573 61.353 0.195 2.550 4.238 0.22 94108. 0.1046 37.54 0.7340 0.6089 0.0142 0.0171 0.070 1.471 0.426 52.228 0.166 1.895 3.701 0.22 94418. 0.0787 38.98 0.7623 0.5086 0.0093 0.0140 0.057 1.205 0.281 42.773 0.136 1.249 2.977 0.22 94737. 0.0514 40.42 0.7905 0.3358 0.0046 0.0108 0.044 0.932 0.138 33.065 0.105 0.614 1.895 0.22 95066. 0.0230 41.87 0.8187 -0.0021 0.0000 0.0076 0.031 0.653 -0.001 23.186 0.074 -0.003 -0.011 0.22 95403. 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 0.0986 0.0361 0.351 5.529 5.276 261.674 0.625 23.466 9.144 0.29 119514. 0.6847 1.93 0.0283 0.0749 0.0975 0.0368 0.358 5.645 5.220 267.159 0.638 23.220 8.863 0.29 119605. 0.6601 3.85 0.0565 0.1450 0.0964 0.0376 0.366 5.761 5.159 272.641 0.651 22.945 8.582 0.29 119705. 0.6354 5.78 0.0848 0.2104 0.0951 0.0383 0.373 5.875 5.090 278.024 0.664 22.641 8.304 0.29 119815. 0.6107 7.71 0.1130 0.2713 0.0937 0.0390 0.380 5.984 5.014 283.207 0.676 22.302 8.030 0.29 119936. 0.5861 9.63 0.1413 0.3278 0.0921 0.0397 0.386 6.087 4.929 288.077 0.688 21.926 7.761 0.29 120068. 0.5617 11.56 0.1696 0.3801 0.0903 0.0403 0.392 6.181 4.836 292.508 0.698 21.511 7.499 0.29 120213. 0.5376 13.49 0.1978 0.4283 0.0884 0.0408 0.397 6.262 4.733 296.366 0.708 21.052 7.243 0.29 120369. 0.5137 15.42 0.2261 0.4728 0.0863 0.0413 0.402 6.329 4.619 299.507 0.715 20.547 6.995 0.29 120538. 0.4901 17.34 0.2544 0.5136 0.0840 0.0416 0.405 6.377 4.495 301.781 0.720 19.993 6.756 0.29 120720. 0.4669 19.27 0.2826 0.5511 0.0814 0.0418 0.406 6.403 4.359 303.038 0.723 19.388 6.524 0.29 120916. 0.4440 21.20 0.3109 0.5854 0.0787 0.0418 0.407 6.405 4.211 303.128 0.724 18.729 6.300 0.29 121125. 0.4214 23.12 0.3391 0.6168 0.0757 0.0416 0.405 6.379 4.050 301.906 0.721 18.014 6.084 0.29 121347. 0.3992 25.05 0.3674 0.6453 0.0724 0.0412 0.401 6.323 3.877 299.240 0.714 17.244 5.876 0.29 121583. 0.3771 26.98 0.3957 0.6711 0.0690 0.0407 0.396 6.234 3.691 295.017 0.704 16.416 5.674 0.29 121833. 0.3554 28.90 0.4239 0.6941 0.0652 0.0398 0.388 6.110 3.492 289.136 0.690 15.533 5.478 0.29 122097. 0.3337 30.83 0.4522 0.7145 0.0613 0.0388 0.378 5.948 3.281 281.502 0.672 14.593 5.286 0.29 122375. 0.3121 32.76 0.4804 0.7320 0.0571 0.0375 0.365 5.749 3.057 272.049 0.649 13.599 5.097 0.29 122666. 0.2905 34.68 0.5087 0.7465 0.0527 0.0359 0.350 5.512 2.823 260.830 0.623 12.558 4.910 0.29 122971. 0.2689 36.61 0.5370 0.7577 0.0482 0.0342 0.332 5.239 2.581 247.938 0.592 11.479 4.721 0.29 123290. 0.2472 38.54 0.5652 0.7651 0.0435 0.0322 0.313 4.933 2.331 233.462 0.557 10.367 4.528 0.29 123623. 0.2254 40.47 0.5935 0.7678 0.0388 0.0300 0.292 4.596 2.075 217.484 0.519 9.231 4.328 0.29 123969. 0.2032 42.39 0.6218 0.7648 0.0339 0.0276 0.268 4.228 1.815 200.088 0.478 8.075 4.115 0.29 124328. 0.1807 44.32 0.6500 0.7544 0.0290 0.0250 0.243 3.832 1.553 181.362 0.433 6.906 3.883 0.29 124701. 0.1577 46.25 0.6783 0.7339 0.0241 0.0222 0.216 3.411 1.288 161.404 0.385 5.729 3.620 0.29 125088. 0.1339 48.17 0.7065 0.6986 0.0191 0.0193 0.188 2.965 1.024 140.333 0.335 4.553 3.308 0.29 125488. 0.1091 50.10 0.7348 0.6404 0.0142 0.0163 0.159 2.499 0.760 118.287 0.282 3.382 2.916 0.29 125901. 0.0829 52.03 0.7631 0.5427 0.0094 0.0132 0.128 2.017 0.501 95.433 0.228 2.227 2.379 0.29 126328. 0.0549 53.95 0.7913 0.3669 0.0046 0.0099 0.097 1.521 0.246 71.967 0.172 1.095 1.551 0.29 126768. 0.0251 55.88 0.8196 -0.0034 0.0000 0.0066 0.064 1.016 -0.001 48.078 0.115 -0.007 -0.014 0.30 127218. 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 0.0990 0.0358 0.680 8.568 8.282 506.869 0.968 36.840 7.411 0.36 149388. 0.6953 2.41 0.0283 0.0758 0.0980 0.0365 0.694 8.753 8.197 517.788 0.989 36.460 7.180 0.36 149501. 0.6701 4.82 0.0565 0.1468 0.0969 0.0373 0.709 8.938 8.102 528.712 1.010 36.037 6.950 0.36 149626. 0.6449 7.23 0.0848 0.2130 0.0956 0.0381 0.723 9.119 7.996 539.454 1.030 35.566 6.723 0.36 149764. 0.6197 9.64 0.1131 0.2746 0.0942 0.0388 0.737 9.294 7.878 549.812 1.050 35.042 6.499 0.36 149915. 0.5946 12.05 0.1413 0.3316 0.0926 0.0395 0.750 9.459 7.747 559.559 1.069 34.459 6.280 0.36 150081. 0.5698 14.45 0.1696 0.3844 0.0909 0.0401 0.762 9.609 7.602 568.449 1.086 33.813 6.066 0.36 150261. 0.5452 16.86 0.1979 0.4330 0.0890 0.0407 0.773 9.741 7.441 576.211 1.100 33.098 5.857 0.36 150457. 0.5209 19.27 0.2261 0.4779 0.0869 0.0411 0.781 9.848 7.264 582.560 1.113 32.311 5.656 0.36 150669. 0.4969 21.68 0.2544 0.5191 0.0845 0.0414 0.787 9.926 7.070 587.202 1.121 31.446 5.461 0.36 150897. 0.4733 24.09 0.2827 0.5569 0.0820 0.0416 0.791 9.971 6.857 589.832 1.126 30.500 5.273 0.36 151142. 0.4501 26.50 0.3109 0.5916 0.0792 0.0416 0.791 9.976 6.625 590.153 1.127 29.469 5.092 0.36 151403. 0.4272 28.91 0.3392 0.6232 0.0762 0.0415 0.788 9.938 6.374 587.876 1.123 28.350 4.917 0.36 151682. 0.4047 31.32 0.3675 0.6521 0.0730 0.0411 0.781 9.851 6.102 582.738 1.113 27.141 4.749 0.36 151977. 0.3824 33.73 0.3957 0.6782 0.0695 0.0405 0.770 9.712 5.810 574.508 1.097 25.843 4.587 0.36 152290. 0.3604 36.14 0.4240 0.7017 0.0657 0.0397 0.755 9.517 5.498 562.989 1.075 24.455 4.429 0.36 152620. 0.3386 38.55 0.4523 0.7226 0.0618 0.0387 0.735 9.263 5.166 547.987 1.047 22.979 4.276 0.36 152968. 0.3168 40.96 0.4805 0.7407 0.0576 0.0373 0.710 8.949 4.815 529.369 1.011 21.416 4.125 0.36 153332. 0.2951 43.36 0.5088 0.7559 0.0532 0.0358 0.680 8.574 4.447 507.229 0.969 19.779 3.976 0.36 153714. 0.2733 45.77 0.5371 0.7680 0.0486 0.0340 0.646 8.144 4.065 481.751 0.920 18.080 3.827 0.36 154113. 0.2515 48.18 0.5653 0.7763 0.0439 0.0320 0.608 7.660 3.672 453.106 0.865 16.331 3.675 0.36 154529. 0.2296 50.59 0.5936 0.7804 0.0391 0.0297 0.565 7.125 3.269 421.459 0.805 14.542 3.518 0.36 154962. 0.2074 53.00 0.6219 0.7790 0.0342 0.0273 0.519 6.542 2.860 386.973 0.739 12.722 3.352 0.36 155412. 0.1848 55.41 0.6502 0.7705 0.0293 0.0247 0.469 5.914 2.446 349.822 0.668 10.881 3.172 0.36 155878. 0.1617 57.82 0.6784 0.7524 0.0243 0.0219 0.416 5.244 2.030 310.205 0.592 9.029 2.968 0.37 156362. 0.1379 60.23 0.7067 0.7200 0.0193 0.0189 0.360 4.536 1.613 268.355 0.513 7.177 2.727 0.37 156862. 0.1129 62.64 0.7350 0.6652 0.0143 0.0158 0.301 3.796 1.199 224.552 0.429 5.334 2.422 0.37 157379. 0.0865 65.05 0.7632 0.5707 0.0094 0.0126 0.240 3.028 0.790 179.130 0.342 3.515 2.001 0.37 157913. 0.0580 67.46 0.7915 0.3946 0.0047 0.0093 0.178 2.240 0.390 132.485 0.253 1.734 1.334 0.37 158463. 0.0272 69.87 0.8198 0.0003 0.0000 0.0060 0.114 1.437 0.000 84.993 0.162 0.001 0.001 0.37 159025. 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 0.0996 0.0357 1.172 12.308 11.995 873.683 1.391 53.352 6.227 0.43 179257. 0.7030 2.89 0.0283 0.0765 0.0986 0.0365 1.197 12.579 11.874 892.924 1.421 52.816 6.032 0.43 179393. 0.6775 5.78 0.0566 0.1480 0.0975 0.0372 1.223 12.850 11.739 912.193 1.452 52.217 5.837 0.43 179543. 0.6520 8.68 0.0848 0.2147 0.0962 0.0380 1.249 13.117 11.589 931.164 1.482 51.547 5.645 0.43 179709. 0.6264 11.57 0.1131 0.2767 0.0948 0.0388 1.273 13.375 11.421 949.479 1.511 50.800 5.456 0.43 179891. 0.6010 14.46 0.1414 0.3341 0.0933 0.0395 1.296 13.619 11.234 966.741 1.539 49.968 5.271 0.43 180090. 0.5759 17.35 0.1697 0.3872 0.0916 0.0401 1.318 13.841 11.026 982.511 1.564 49.044 5.090 0.43 180307. 0.5510 20.24 0.1979 0.4362 0.0896 0.0407 1.336 14.035 10.796 996.313 1.586 48.020 4.915 0.43 180543. 0.5264 23.14 0.2262 0.4813 0.0875 0.0411 1.351 14.195 10.542 1007.644 1.604 46.890 4.745 0.43 180797. 0.5022 26.03 0.2545 0.5228 0.0852 0.0415 1.362 14.312 10.262 1015.983 1.617 45.645 4.581 0.43 181072. 0.4784 28.92 0.2828 0.5608 0.0827 0.0417 1.369 14.380 9.955 1020.794 1.625 44.282 4.423 0.43 181366. 0.4550 31.81 0.3111 0.5958 0.0799 0.0417 1.370 14.391 9.621 1021.548 1.626 42.793 4.272 0.43 181680. 0.4319 34.71 0.3393 0.6277 0.0769 0.0416 1.365 14.337 9.257 1017.738 1.620 41.176 4.126 0.43 182015. 0.4092 37.60 0.3676 0.6568 0.0736 0.0412 1.353 14.212 8.864 1008.896 1.606 39.427 3.985 0.43 182370. 0.3868 40.49 0.3959 0.6833 0.0701 0.0406 1.334 14.011 8.441 994.614 1.583 37.547 3.849 0.43 182746. 0.3646 43.38 0.4242 0.7072 0.0663 0.0398 1.307 13.728 7.989 974.540 1.551 35.536 3.718 0.43 183143. 0.3426 46.27 0.4525 0.7284 0.0623 0.0387 1.272 13.359 7.508 948.337 1.509 33.394 3.591 0.43 183561. 0.3207 49.17 0.4807 0.7470 0.0581 0.0374 1.228 12.900 6.998 915.761 1.457 31.125 3.466 0.43 183999. 0.2989 52.06 0.5090 0.7629 0.0537 0.0358 1.176 12.354 6.463 876.970 1.396 28.747 3.343 0.43 184458. 0.2770 54.95 0.5373 0.7756 0.0491 0.0340 1.116 11.724 5.908 832.278 1.325 26.279 3.220 0.43 184938. 0.2551 57.84 0.5656 0.7849 0.0443 0.0319 1.049 11.016 5.336 781.989 1.245 23.736 3.095 0.44 185437. 0.2331 60.73 0.5938 0.7899 0.0395 0.0297 0.974 10.233 4.751 726.388 1.156 21.134 2.967 0.44 185958. 0.2108 63.63 0.6221 0.7898 0.0345 0.0272 0.893 9.379 4.156 665.762 1.060 18.487 2.832 0.44 186498. 0.1882 66.52 0.6504 0.7830 0.0295 0.0245 0.805 8.458 3.554 600.420 0.956 15.809 2.685 0.44 187059. 0.1650 69.41 0.6787 0.7668 0.0245 0.0217 0.712 7.476 2.948 530.713 0.845 13.115 2.520 0.44 187639. 0.1410 72.30 0.7070 0.7368 0.0194 0.0187 0.613 6.439 2.342 457.054 0.727 10.418 2.324 0.44 188240. 0.1160 75.19 0.7352 0.6846 0.0144 0.0155 0.510 5.352 1.740 379.939 0.605 7.738 2.077 0.44 188861. 0.0893 78.09 0.7635 0.5925 0.0095 0.0122 0.402 4.226 1.145 299.966 0.477 5.091 1.731 0.44 189502. 0.0604 80.98 0.7918 0.4153 0.0047 0.0089 0.292 3.069 0.562 217.839 0.347 2.499 1.170 0.44 190163. 0.0286 83.87 0.8201 -0.0060 0.0000 0.0055 0.180 1.891 -0.005 134.209 0.214 -0.022 -0.016 0.44 190837. 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 0.1003 0.0357 1.864 16.786 16.436 1390.158 1.896 73.108 5.363 0.50 209122. 0.7087 3.37 0.0283 0.0768 0.0993 0.0365 1.906 17.162 16.276 1421.353 1.939 72.396 5.194 0.50 209280. 0.6831 6.75 0.0566 0.1487 0.0982 0.0374 1.948 17.540 16.097 1452.633 1.982 71.598 5.026 0.50 209456. 0.6573 10.12 0.0848 0.2157 0.0970 0.0381 1.989 17.912 15.896 1483.464 2.024 70.704 4.860 0.50 209649. 0.6316 13.50 0.1131 0.2779 0.0956 0.0389 2.029 18.272 15.671 1513.275 2.064 69.703 4.697 0.50 209862. 0.6061 16.87 0.1414 0.3356 0.0941 0.0396 2.067 18.612 15.419 1541.411 2.103 68.585 4.537 0.50 210095. 0.5808 20.24 0.1697 0.3889 0.0924 0.0403 2.102 18.923 15.139 1567.159 2.138 67.339 4.382 0.50 210348. 0.5557 23.62 0.1979 0.4380 0.0905 0.0409 2.132 19.196 14.828 1589.748 2.169 65.955 4.231 0.50 210623. 0.5310 26.99 0.2262 0.4833 0.0884 0.0414 2.157 19.420 14.484 1608.358 2.194 64.423 4.085 0.50 210921. 0.5067 30.37 0.2545 0.5250 0.0860 0.0417 2.175 19.587 14.104 1622.139 2.213 62.734 3.944 0.50 211241. 0.4828 33.74 0.2828 0.5632 0.0835 0.0419 2.186 19.684 13.687 1630.224 2.224 60.878 3.808 0.50 211585. 0.4592 37.11 0.3110 0.5984 0.0807 0.0420 2.188 19.703 13.230 1631.751 2.226 58.849 3.678 0.50 211952. 0.4361 40.49 0.3393 0.6305 0.0777 0.0418 2.180 19.632 12.734 1625.894 2.218 56.641 3.552 0.50 212343. 0.4132 43.86 0.3676 0.6599 0.0744 0.0414 2.162 19.463 12.196 1611.890 2.199 54.250 3.432 0.50 212759. 0.3907 47.24 0.3959 0.6867 0.0709 0.0409 2.131 19.187 11.618 1589.074 2.168 51.675 3.316 0.50 213198. 0.3684 50.61 0.4242 0.7109 0.0671 0.0400 2.088 18.799 10.998 1556.878 2.124 48.918 3.204 0.50 213662. 0.3464 53.98 0.4524 0.7325 0.0631 0.0389 2.031 18.290 10.337 1514.756 2.066 45.979 3.095 0.50 214150. 0.3244 57.36 0.4807 0.7516 0.0588 0.0376 1.961 17.657 9.637 1462.301 1.995 42.864 2.989 0.51 214662. 0.3025 60.73 0.5090 0.7680 0.0543 0.0360 1.877 16.901 8.902 1399.749 1.910 39.595 2.885 0.51 215198. 0.2805 64.11 0.5373 0.7814 0.0496 0.0341 1.780 16.030 8.138 1327.602 1.811 36.200 2.780 0.51 215757. 0.2586 67.48 0.5655 0.7915 0.0448 0.0320 1.671 15.049 7.352 1246.351 1.700 32.700 2.675 0.51 216341. 0.2365 70.85 0.5938 0.7975 0.0399 0.0297 1.551 13.964 6.546 1156.459 1.578 29.118 2.567 0.51 216948. 0.2141 74.23 0.6221 0.7986 0.0349 0.0272 1.419 12.780 5.727 1058.391 1.444 25.472 2.454 0.51 217579. 0.1914 77.60 0.6504 0.7932 0.0299 0.0245 1.278 11.503 4.897 952.647 1.300 21.781 2.331 0.51 218233. 0.1682 80.97 0.6786 0.7788 0.0248 0.0216 1.126 10.140 4.062 839.799 1.146 18.067 2.194 0.51 218911. 0.1441 84.35 0.7069 0.7510 0.0197 0.0185 0.966 8.700 3.226 720.520 0.983 14.350 2.031 0.51 219613. 0.1189 87.72 0.7352 0.7014 0.0146 0.0153 0.799 7.192 2.395 595.618 0.813 10.654 1.824 0.51 220337. 0.0920 91.10 0.7635 0.6120 0.0096 0.0120 0.625 5.628 1.575 466.070 0.636 7.004 1.532 0.51 221085. 0.0627 94.47 0.7918 0.4349 0.0047 0.0086 0.447 4.021 0.771 333.033 0.454 3.429 1.050 0.52 221856. 0.0301 97.84 0.8200 -0.0104 -0.0001 0.0051 0.265 2.385 -0.011 197.547 0.269 -0.047 -0.024 0.52 222641. 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 0.1011 0.0360 2.799 22.054 21.636 2087.376 2.492 96.238 4.701 0.57 238981. 0.7129 3.85 0.0282 0.0769 0.1001 0.0368 2.863 22.557 21.434 2135.005 2.548 95.340 4.554 0.57 239162. 0.6872 7.70 0.0565 0.1488 0.0990 0.0376 2.927 23.062 21.207 2182.838 2.606 94.328 4.407 0.57 239362. 0.6615 11.56 0.0848 0.2159 0.0979 0.0384 2.991 23.561 20.951 2230.058 2.662 93.190 4.261 0.57 239583. 0.6358 15.41 0.1130 0.2782 0.0965 0.0392 3.052 24.044 20.664 2275.788 2.717 91.911 4.118 0.57 239826. 0.6103 19.26 0.1412 0.3359 0.0950 0.0399 3.110 24.501 20.341 2319.026 2.768 90.478 3.978 0.57 240092. 0.5849 23.11 0.1695 0.3893 0.0933 0.0406 3.163 24.920 19.981 2358.677 2.815 88.874 3.842 0.57 240382. 0.5599 26.97 0.1978 0.4386 0.0914 0.0412 3.210 25.289 19.579 2393.559 2.857 87.087 3.710 0.57 240696. 0.5351 30.82 0.2260 0.4840 0.0894 0.0417 3.249 25.594 19.133 2422.418 2.892 85.102 3.582 0.57 241037. 0.5108 34.67 0.2542 0.5258 0.0871 0.0421 3.277 25.821 18.639 2443.946 2.917 82.907 3.459 0.57 241403. 0.4868 38.52 0.2825 0.5642 0.0845 0.0423 3.295 25.957 18.096 2456.817 2.933 80.490 3.341 0.57 241796. 0.4633 42.38 0.3108 0.5995 0.0817 0.0424 3.299 25.988 17.500 2459.718 2.936 77.841 3.227 0.57 242216. 0.4401 46.23 0.3390 0.6319 0.0787 0.0422 3.287 25.900 16.851 2451.376 2.926 74.952 3.118 0.57 242663. 0.4172 50.08 0.3672 0.6615 0.0754 0.0419 3.260 25.680 16.146 2430.624 2.901 71.818 3.013 0.58 243138. 0.3947 53.93 0.3955 0.6885 0.0719 0.0413 3.214 25.319 15.386 2396.444 2.861 68.437 2.912 0.58 243640. 0.3724 57.78 0.4238 0.7130 0.0681 0.0404 3.149 24.807 14.571 2347.966 2.803 64.812 2.815 0.58 244170. 0.3503 61.64 0.4520 0.7351 0.0640 0.0393 3.063 24.135 13.701 2284.370 2.727 60.944 2.720 0.58 244728. 0.3283 65.49 0.4803 0.7546 0.0597 0.0380 2.957 23.297 12.778 2205.010 2.632 56.838 2.628 0.58 245313. 0.3063 69.34 0.5085 0.7716 0.0552 0.0363 2.830 22.295 11.809 2110.198 2.519 52.525 2.538 0.58 245925. 0.2843 73.19 0.5368 0.7857 0.0504 0.0345 2.683 21.138 10.800 2000.694 2.388 48.039 2.448 0.58 246564. 0.2623 77.05 0.5650 0.7965 0.0456 0.0323 2.517 19.834 9.760 1877.247 2.241 43.413 2.358 0.58 247231. 0.2402 80.90 0.5932 0.8035 0.0406 0.0300 2.334 18.390 8.695 1740.567 2.078 38.673 2.266 0.58 247924. 0.2178 84.75 0.6215 0.8058 0.0355 0.0274 2.134 16.813 7.609 1591.361 1.900 33.847 2.169 0.58 248645. 0.1950 88.60 0.6497 0.8019 0.0304 0.0246 1.918 15.113 6.510 1430.396 1.707 28.959 2.064 0.58 249392. 0.1717 92.45 0.6780 0.7893 0.0252 0.0217 1.688 13.297 5.404 1258.540 1.502 24.036 1.947 0.58 250165. 0.1476 96.31 0.7063 0.7639 0.0201 0.0185 1.444 11.377 4.296 1076.823 1.285 19.107 1.809 0.59 250966. 0.1222 100.16 0.7345 0.7174 0.0149 0.0153 1.189 9.366 3.193 886.480 1.058 14.204 1.634 0.59 251793. 0.0952 104.01 0.7628 0.6317 0.0098 0.0119 0.924 7.280 2.104 689.006 0.822 9.361 1.385 0.59 252646. 0.0655 107.86 0.7910 0.4578 0.0048 0.0084 0.652 5.137 1.038 486.181 0.580 4.616 0.968 0.59 253526. 0.0321 111.72 0.8193 0.0002 0.0000 0.0048 0.375 2.954 0.000 279.632 0.334 0.001 0.000 0.59 254422. 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 0.1020 0.0363 4.024 28.182 27.631 3000.805 3.184 122.902 4.176 0.64 268833. 0.7156 4.33 0.0282 0.0768 0.1011 0.0371 4.117 28.835 27.386 3070.409 3.258 121.815 4.046 0.64 269036. 0.6901 8.66 0.0565 0.1487 0.1000 0.0380 4.211 29.493 27.110 3140.474 3.332 120.584 3.915 0.64 269261. 0.6646 12.99 0.0847 0.2157 0.0989 0.0388 4.304 30.144 26.797 3209.788 3.406 119.192 3.787 0.64 269510. 0.6390 17.33 0.1129 0.2780 0.0976 0.0396 4.395 30.776 26.443 3277.044 3.477 117.621 3.660 0.64 269783. 0.6135 21.66 0.1412 0.3357 0.0961 0.0404 4.480 31.374 26.045 3340.773 3.545 115.849 3.536 0.64 270083. 0.5883 25.99 0.1694 0.3891 0.0945 0.0411 4.559 31.925 25.598 3399.354 3.607 113.859 3.415 0.64 270409. 0.5633 30.32 0.1976 0.4385 0.0926 0.0417 4.628 32.410 25.097 3451.035 3.662 111.630 3.298 0.64 270763. 0.5387 34.65 0.2259 0.4839 0.0906 0.0423 4.685 32.813 24.538 3493.965 3.707 109.144 3.185 0.64 271147. 0.5144 38.98 0.2541 0.5258 0.0883 0.0427 4.729 33.116 23.917 3526.226 3.741 106.384 3.076 0.64 271559. 0.4904 43.32 0.2824 0.5643 0.0857 0.0429 4.755 33.301 23.232 3545.859 3.762 103.335 2.972 0.65 272002. 0.4669 47.65 0.3106 0.5997 0.0830 0.0430 4.762 33.348 22.478 3550.934 3.768 99.982 2.871 0.65 272475. 0.4437 51.98 0.3388 0.6323 0.0799 0.0428 4.747 33.242 21.654 3539.588 3.756 96.317 2.775 0.65 272979. 0.4209 56.31 0.3671 0.6622 0.0766 0.0425 4.707 32.965 20.758 3510.104 3.724 92.331 2.682 0.65 273514. 0.3984 60.64 0.3953 0.6895 0.0730 0.0419 4.641 32.503 19.789 3460.983 3.672 88.022 2.593 0.65 274080. 0.3761 64.97 0.4235 0.7143 0.0692 0.0410 4.547 31.846 18.748 3390.955 3.598 83.393 2.508 0.65 274677. 0.3540 69.31 0.4518 0.7368 0.0651 0.0399 4.424 30.981 17.636 3298.842 3.500 78.446 2.425 0.65 275305. 0.3320 73.64 0.4800 0.7567 0.0607 0.0385 4.269 29.899 16.454 3183.675 3.378 73.188 2.344 0.65 275963. 0.3100 77.97 0.5082 0.7742 0.0561 0.0368 4.085 28.605 15.210 3045.853 3.232 67.656 2.265 0.65 276653. 0.2880 82.30 0.5365 0.7889 0.0514 0.0349 3.871 27.108 13.916 2886.471 3.063 61.896 2.187 0.65 277373. 0.2659 86.63 0.5647 0.8006 0.0464 0.0327 3.630 25.419 12.579 2706.641 2.872 55.950 2.108 0.65 278123. 0.2437 90.96 0.5929 0.8085 0.0414 0.0303 3.362 23.548 11.208 2507.401 2.660 49.852 2.027 0.65 278903. 0.2213 95.29 0.6212 0.8118 0.0362 0.0277 3.071 21.504 9.811 2289.793 2.430 43.637 1.943 0.66 279713. 0.1984 99.63 0.6494 0.8093 0.0310 0.0249 2.756 19.299 8.395 2054.941 2.180 37.339 1.853 0.66 280554. 0.1750 103.96 0.6777 0.7984 0.0257 0.0218 2.419 16.943 6.968 1804.117 1.914 30.993 1.752 0.66 281424. 0.1507 108.29 0.7059 0.7750 0.0204 0.0186 2.064 14.452 5.538 1538.831 1.633 24.635 1.632 0.66 282324. 0.1252 112.62 0.7341 0.7310 0.0152 0.0153 1.691 11.842 4.116 1260.898 1.338 18.307 1.481 0.66 283254. 0.0979 116.95 0.7624 0.6481 0.0100 0.0118 1.304 9.133 2.710 972.521 1.032 12.055 1.264 0.66 284213. 0.0678 121.28 0.7906 0.4752 0.0049 0.0082 0.907 6.352 1.333 676.346 0.718 5.928 0.894 0.66 285202. 0.0336 125.62 0.8188 -0.0049 0.0000 0.0045 0.503 3.520 -0.007 374.793 0.398 -0.033 -0.009 0.66 286208. 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 0.1030 0.0370 5.634 35.507 34.459 4200.932 4.012 153.273 3.720 0.71 298676. 0.7119 4.81 0.0282 0.0761 0.1022 0.0379 5.760 36.304 34.176 4295.134 4.102 152.014 3.609 0.71 298901. 0.6878 9.62 0.0564 0.1474 0.1012 0.0387 5.888 37.108 33.853 4390.324 4.192 150.578 3.497 0.71 299151. 0.6633 14.42 0.0846 0.2141 0.1001 0.0396 6.014 37.907 33.485 4484.896 4.283 148.942 3.386 0.71 299427. 0.6388 19.23 0.1128 0.2763 0.0988 0.0404 6.138 38.687 33.067 4577.094 4.371 147.083 3.277 0.71 299731. 0.6142 24.04 0.1410 0.3340 0.0974 0.0411 6.256 39.429 32.593 4664.909 4.455 144.972 3.169 0.71 300063. 0.5898 28.85 0.1692 0.3875 0.0958 0.0419 6.365 40.115 32.056 4746.088 4.532 142.584 3.063 0.72 300426. 0.5654 33.66 0.1975 0.4369 0.0940 0.0425 6.461 40.724 31.451 4818.177 4.601 139.893 2.961 0.72 300820. 0.5413 38.47 0.2257 0.4825 0.0920 0.0430 6.542 41.235 30.772 4878.538 4.659 136.875 2.861 0.72 301246. 0.5174 43.27 0.2539 0.5245 0.0897 0.0434 6.604 41.622 30.015 4924.416 4.702 133.506 2.765 0.72 301705. 0.4937 48.08 0.2821 0.5632 0.0872 0.0437 6.642 41.864 29.174 4952.954 4.730 129.767 2.672 0.72 302197. 0.4704 52.89 0.3103 0.5988 0.0844 0.0438 6.653 41.934 28.246 4961.287 4.738 125.638 2.582 0.72 302724. 0.4474 57.70 0.3385 0.6315 0.0814 0.0436 6.634 41.810 27.227 4946.631 4.724 121.108 2.497 0.72 303284. 0.4247 62.51 0.3667 0.6616 0.0781 0.0433 6.580 41.470 26.116 4906.399 4.685 116.166 2.414 0.72 303879. 0.4022 67.31 0.3949 0.6892 0.0745 0.0427 6.488 40.895 24.912 4838.388 4.620 110.809 2.335 0.72 304509. 0.3800 72.12 0.4231 0.7144 0.0706 0.0418 6.358 40.070 23.615 4740.806 4.527 105.041 2.259 0.72 305173. 0.3579 76.93 0.4513 0.7372 0.0664 0.0407 6.185 38.982 22.227 4612.013 4.404 98.864 2.186 0.72 305871. 0.3359 81.74 0.4795 0.7577 0.0620 0.0393 5.968 37.618 20.748 4450.609 4.250 92.286 2.114 0.72 306603. 0.3140 86.55 0.5077 0.7757 0.0574 0.0375 5.709 35.982 19.189 4257.048 4.065 85.353 2.045 0.72 307369. 0.2919 91.36 0.5360 0.7911 0.0525 0.0356 5.408 34.087 17.564 4032.875 3.851 78.123 1.975 0.72 308169. 0.2699 96.16 0.5642 0.8035 0.0475 0.0333 5.069 31.947 15.883 3779.667 3.609 70.647 1.906 0.73 309003. 0.2476 100.97 0.5924 0.8124 0.0423 0.0309 4.692 29.574 14.158 3498.914 3.341 62.973 1.835 0.73 309870. 0.2251 105.78 0.6206 0.8169 0.0371 0.0282 4.281 26.981 12.398 3192.132 3.048 55.144 1.762 0.73 310770. 0.2022 110.59 0.6488 0.8157 0.0317 0.0252 3.837 24.182 10.612 2860.988 2.732 47.203 1.682 0.73 311703. 0.1787 115.40 0.6770 0.8063 0.0263 0.0221 3.363 21.193 8.811 2507.421 2.394 39.193 1.594 0.73 312669. 0.1542 120.21 0.7052 0.7848 0.0209 0.0188 2.861 18.035 7.006 2133.777 2.038 31.162 1.489 0.73 313668. 0.1285 125.01 0.7334 0.7427 0.0156 0.0154 2.337 14.732 5.207 1742.949 1.664 23.162 1.355 0.73 314700. 0.1008 129.82 0.7616 0.6612 0.0102 0.0118 1.795 11.314 3.429 1338.528 1.278 15.251 1.162 0.73 315764. 0.0701 134.63 0.7898 0.4876 0.0050 0.0082 1.240 7.817 1.684 924.865 0.883 7.493 0.826 0.74 316861. 0.0350 139.44 0.8180 -0.0074 0.0000 0.0045 0.679 4.277 -0.013 506.020 0.483 -0.060 -0.012 0.74 317977. 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 0.1041 0.0394 7.973 45.685 42.148 5945.518 5.161 187.474 3.215 0.79 328508. 0.6805 5.28 0.0282 0.0725 0.1033 0.0402 8.126 46.563 41.835 6059.798 5.261 186.081 3.131 0.79 328755. 0.6602 10.56 0.0563 0.1410 0.1025 0.0409 8.280 47.445 41.475 6174.605 5.360 184.481 3.047 0.79 329029. 0.6396 15.84 0.0845 0.2057 0.1014 0.0417 8.432 48.315 41.062 6287.830 5.459 182.642 2.962 0.79 329332. 0.6187 21.12 0.1126 0.2664 0.1003 0.0424 8.579 49.155 40.587 6397.177 5.554 180.532 2.878 0.79 329665. 0.5976 26.40 0.1408 0.3234 0.0989 0.0431 8.717 49.946 40.044 6500.064 5.643 178.115 2.794 0.79 330030. 0.5764 31.68 0.1689 0.3766 0.0974 0.0437 8.842 50.665 39.424 6593.646 5.724 175.356 2.712 0.79 330428. 0.5551 36.96 0.1971 0.4263 0.0956 0.0442 8.951 51.289 38.718 6674.854 5.795 172.219 2.631 0.79 330861. 0.5337 42.24 0.2253 0.4725 0.0937 0.0447 9.039 51.793 37.921 6740.470 5.852 168.672 2.552 0.79 331330. 0.5122 47.52 0.2534 0.5154 0.0915 0.0450 9.102 52.151 37.024 6787.149 5.892 164.684 2.474 0.79 331834. 0.4908 52.80 0.2816 0.5552 0.0890 0.0451 9.134 52.338 36.022 6811.439 5.913 160.226 2.399 0.79 332376. 0.4693 58.08 0.3097 0.5920 0.0862 0.0451 9.132 52.326 34.909 6809.841 5.912 155.276 2.325 0.79 332955. 0.4478 63.36 0.3379 0.6259 0.0832 0.0449 9.091 52.088 33.681 6778.883 5.885 149.814 2.254 0.79 333572. 0.4263 68.64 0.3661 0.6572 0.0799 0.0445 9.005 51.599 32.336 6715.233 5.830 143.829 2.184 0.79 334227. 0.4049 73.92 0.3942 0.6858 0.0763 0.0438 8.872 50.835 30.871 6615.848 5.743 137.316 2.116 0.79 334920. 0.3833 79.20 0.4224 0.7120 0.0724 0.0429 8.687 49.776 29.289 6478.021 5.624 130.277 2.051 0.79 335650. 0.3618 84.47 0.4505 0.7357 0.0682 0.0417 8.447 48.402 27.589 6299.202 5.468 122.718 1.987 0.79 336418. 0.3401 89.75 0.4787 0.7570 0.0637 0.0403 8.149 46.695 25.775 6076.988 5.276 114.648 1.924 0.79 337223. 0.3184 95.03 0.5068 0.7758 0.0589 0.0385 7.793 44.655 23.858 5811.556 5.045 106.118 1.862 0.80 338066. 0.2965 100.31 0.5350 0.7918 0.0540 0.0365 7.382 42.299 21.853 5504.915 4.779 97.203 1.801 0.80 338945. 0.2744 105.59 0.5632 0.8049 0.0489 0.0342 6.918 39.641 19.777 5158.974 4.479 87.969 1.739 0.80 339861. 0.2521 110.87 0.5913 0.8144 0.0436 0.0316 6.405 36.699 17.642 4776.058 4.146 78.472 1.675 0.80 340814. 0.2294 116.15 0.6195 0.8192 0.0382 0.0289 5.845 33.492 15.461 4358.713 3.784 68.769 1.609 0.80 341802. 0.2062 121.43 0.6476 0.8179 0.0327 0.0259 5.243 30.044 13.245 3909.995 3.394 58.912 1.536 0.80 342827. 0.1823 126.71 0.6758 0.8077 0.0272 0.0228 4.604 26.383 11.006 3433.498 2.981 48.955 1.454 0.80 343887. 0.1572 131.99 0.7040 0.7836 0.0216 0.0194 3.934 22.541 8.758 2933.521 2.547 38.956 1.354 0.80 344984. 0.1306 137.27 0.7321 0.7363 0.0161 0.0160 3.239 18.559 6.515 2415.354 2.097 28.979 1.223 0.81 346116. 0.1018 142.55 0.7603 0.6455 0.0106 0.0125 2.528 14.486 4.293 1885.288 1.637 19.097 1.033 0.81 347283. 0.0698 147.83 0.7884 0.4594 0.0052 0.0089 1.811 10.377 2.111 1350.537 1.172 9.388 0.709 0.81 348486. 0.0336 153.11 0.8166 -0.0066 0.0000 0.0054 1.097 6.283 -0.018 817.675 0.710 -0.079 -0.010 0.81 349712. 0.0000 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 0.1051 0.0450 11.824 62.106 50.652 8817.516 7.017 225.299 2.606 0.86 358331. 0.6045 5.76 0.0282 0.0645 0.1045 0.0457 11.998 63.019 50.324 8947.003 7.120 223.841 2.551 0.86 358599. 0.5900 11.53 0.0564 0.1262 0.1037 0.0463 12.168 63.912 49.944 9073.844 7.221 222.149 2.497 0.86 358897. 0.5751 17.29 0.0845 0.1851 0.1028 0.0469 12.330 64.764 49.501 9194.801 7.317 220.181 2.442 0.86 359226. 0.5600 23.05 0.1127 0.2413 0.1017 0.0475 12.480 65.549 48.987 9306.304 7.406 217.892 2.388 0.86 359589. 0.5447 28.82 0.1409 0.2948 0.1004 0.0480 12.612 66.245 48.390 9405.016 7.484 215.238 2.334 0.86 359987. 0.5292 34.58 0.1691 0.3457 0.0990 0.0484 12.722 66.823 47.700 9487.098 7.550 212.171 2.281 0.86 360422. 0.5134 40.34 0.1972 0.3941 0.0974 0.0487 12.805 67.257 46.907 9548.706 7.599 208.643 2.228 0.86 360896. 0.4975 46.11 0.2254 0.4400 0.0955 0.0489 12.855 67.519 46.000 9585.958 7.628 204.610 2.177 0.86 361408. 0.4812 51.87 0.2536 0.4834 0.0933 0.0490 12.867 67.583 44.970 9595.065 7.636 200.026 2.126 0.86 361961. 0.4647 57.63 0.2818 0.5245 0.0909 0.0489 12.837 67.422 43.807 9572.250 7.617 194.855 2.076 0.86 362554. 0.4479 63.40 0.3099 0.5632 0.0882 0.0486 12.758 67.011 42.505 9513.885 7.571 189.061 2.026 0.86 363189. 0.4307 69.16 0.3381 0.5996 0.0852 0.0481 12.628 66.326 41.056 9416.533 7.493 182.619 1.978 0.86 363865. 0.4131 74.93 0.3663 0.6337 0.0819 0.0473 12.441 65.343 39.459 9277.025 7.382 175.512 1.929 0.86 364583. 0.3950 80.69 0.3945 0.6654 0.0783 0.0464 12.193 64.044 37.709 9092.543 7.236 167.731 1.881 0.86 365342. 0.3766 86.45 0.4227 0.6947 0.0743 0.0452 11.882 62.410 35.810 8860.565 7.051 159.281 1.833 0.86 366143. 0.3576 92.22 0.4508 0.7216 0.0701 0.0438 11.504 60.423 33.761 8578.460 6.827 150.168 1.785 0.87 366985. 0.3381 97.98 0.4790 0.7460 0.0655 0.0421 11.055 58.066 31.566 8243.818 6.560 140.405 1.737 0.87 367868. 0.3181 103.74 0.5072 0.7677 0.0607 0.0401 10.536 55.339 29.239 7856.648 6.252 130.055 1.688 0.87 368791. 0.2975 109.51 0.5354 0.7860 0.0556 0.0379 9.956 52.291 26.800 7423.973 5.908 119.205 1.637 0.87 369754. 0.2763 115.27 0.5635 0.8001 0.0504 0.0355 9.322 48.965 24.266 6951.739 5.532 107.937 1.583 0.87 370757. 0.2542 121.03 0.5917 0.8087 0.0450 0.0329 8.642 45.390 21.655 6444.143 5.128 96.322 1.524 0.87 371800. 0.2312 126.80 0.6199 0.8104 0.0394 0.0301 7.920 41.597 18.982 5905.729 4.700 84.430 1.458 0.87 372882. 0.2070 132.56 0.6481 0.8036 0.0338 0.0272 7.153 37.568 16.262 5333.754 4.244 72.333 1.383 0.87 374003. 0.1818 138.32 0.6762 0.7848 0.0280 0.0242 6.350 33.355 13.512 4735.492 3.768 60.102 1.294 0.88 375163. 0.1551 144.09 0.7044 0.7476 0.0223 0.0210 5.524 29.013 10.749 4119.077 3.278 47.809 1.184 0.88 376361. 0.1265 149.85 0.7326 0.6815 0.0166 0.0178 4.685 24.605 7.990 3493.278 2.780 35.539 1.037 0.88 377599. 0.0956 155.61 0.7608 0.5672 0.0109 0.0146 3.846 20.201 5.257 2868.084 2.282 23.385 0.831 0.88 378875. 0.0621 161.38 0.7890 0.3667 0.0053 0.0115 3.023 15.878 2.576 2254.259 1.794 11.458 0.518 0.88 380189. 0.0271 167.14 0.8171 -0.0069 -0.0001 0.0085 2.224 11.683 -0.035 1658.616 1.320 -0.154 -0.009 0.89 381532. 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 0.1044 0.0518 17.290 83.826 59.006 12892.854 9.471 262.459 2.076 0.93 388220. 0.5198 6.29 0.0284 0.0561 0.1038 0.0525 17.539 85.034 58.706 13078.683 9.607 261.123 2.036 0.93 388505. 0.5085 12.57 0.0567 0.1100 0.1032 0.0532 17.784 86.225 58.352 13261.848 9.742 259.552 1.996 0.93 388823. 0.4970 18.86 0.0851 0.1617 0.1025 0.0539 18.019 87.362 57.935 13436.755 9.870 257.694 1.956 0.93 389176. 0.4852 25.15 0.1135 0.2112 0.1016 0.0546 18.234 88.404 57.440 13597.034 9.988 255.494 1.916 0.93 389565. 0.4734 31.44 0.1419 0.2587 0.1006 0.0551 18.420 89.304 56.855 13735.493 10.090 252.889 1.877 0.93 389994. 0.4615 37.72 0.1702 0.3043 0.0993 0.0556 18.566 90.013 56.163 13844.446 10.170 249.811 1.840 0.93 390463. 0.4495 44.01 0.1986 0.3481 0.0979 0.0559 18.662 90.478 55.349 13916.013 10.222 246.191 1.804 0.93 390976. 0.4375 50.30 0.2270 0.3902 0.0962 0.0560 18.697 90.651 54.397 13942.627 10.242 241.959 1.770 0.93 391532. 0.4255 56.58 0.2554 0.4308 0.0943 0.0559 18.664 90.488 53.293 13917.468 10.223 237.049 1.737 0.93 392133. 0.4133 62.87 0.2837 0.4701 0.0920 0.0555 18.553 89.950 52.023 13834.806 10.163 231.400 1.706 0.93 392780. 0.4010 69.16 0.3121 0.5080 0.0895 0.0550 18.359 89.010 50.576 13690.267 10.056 224.962 1.676 0.93 393474. 0.3885 75.45 0.3405 0.5446 0.0866 0.0541 18.078 87.649 48.941 13480.831 9.902 217.691 1.647 0.93 394214. 0.3755 81.73 0.3688 0.5799 0.0833 0.0530 17.708 85.853 47.114 13204.712 9.700 209.561 1.618 0.93 395002. 0.3621 88.02 0.3972 0.6136 0.0798 0.0516 17.247 83.620 45.090 12861.182 9.447 200.560 1.590 0.94 395835. 0.3481 94.31 0.4256 0.6457 0.0758 0.0500 16.696 80.948 42.870 12450.267 9.145 190.688 1.562 0.94 396715. 0.3333 100.59 0.4540 0.6760 0.0716 0.0481 16.055 77.839 40.458 11972.006 8.794 179.957 1.533 0.94 397640. 0.3178 106.88 0.4823 0.7041 0.0670 0.0459 15.322 74.288 37.856 11425.938 8.393 168.381 1.503 0.94 398611. 0.3014 113.17 0.5107 0.7300 0.0620 0.0434 14.502 70.311 35.081 10814.234 7.944 156.039 1.471 0.94 399626. 0.2841 119.46 0.5391 0.7531 0.0569 0.0407 13.604 65.955 32.162 10144.198 7.452 143.054 1.438 0.94 400685. 0.2658 125.74 0.5675 0.7709 0.0515 0.0379 12.665 61.404 29.119 9444.299 6.937 129.520 1.398 0.94 401789. 0.2460 132.03 0.5958 0.7813 0.0459 0.0350 11.704 56.743 25.975 8727.403 6.411 115.535 1.350 0.94 402935. 0.2243 138.32 0.6242 0.7769 0.0402 0.0323 10.796 52.344 22.740 8050.718 5.914 101.149 1.281 0.95 404124. 0.1992 144.60 0.6526 0.7567 0.0344 0.0297 9.908 48.037 19.443 7388.339 5.427 86.484 1.194 0.95 405355. 0.1716 150.89 0.6809 0.7202 0.0285 0.0269 9.003 43.649 16.114 6713.413 4.931 71.675 1.089 0.95 406629. 0.1425 157.18 0.7093 0.6613 0.0226 0.0242 8.098 39.263 12.778 6038.860 4.436 56.835 0.960 0.95 407945. 0.1118 163.47 0.7377 0.5721 0.0167 0.0216 7.211 34.962 9.465 5377.347 3.950 42.099 0.798 0.95 409303. 0.0801 169.75 0.7661 0.4422 0.0110 0.0190 6.355 30.814 6.209 4739.285 3.481 27.619 0.594 0.96 410704. 0.0483 176.04 0.7944 0.2582 0.0054 0.0166 5.544 26.879 3.050 4134.152 3.037 13.566 0.335 0.96 412149. 0.0190 182.33 0.8228 0.0004 0.0000 0.0143 4.771 23.129 0.004 3557.374 2.613 0.018 0.001 0.96 413650. 0.0000