21x13WE (21x13WE.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 0.1000 0.0396 0.013 0.820 0.620 9.706 0.093 2.756 28.959 0.08 44125. 0.6370 0.53 0.0264 0.0649 0.0986 0.0402 0.013 0.832 0.611 9.848 0.094 2.719 28.159 0.08 44157. 0.6152 1.05 0.0529 0.1261 0.0972 0.0407 0.013 0.844 0.602 9.983 0.095 2.679 27.361 0.08 44193. 0.5933 1.58 0.0793 0.1837 0.0956 0.0413 0.014 0.855 0.592 10.111 0.097 2.634 26.570 0.08 44232. 0.5713 2.10 0.1057 0.2377 0.0938 0.0417 0.014 0.864 0.581 10.226 0.098 2.586 25.788 0.08 44274. 0.5494 2.63 0.1322 0.2882 0.0919 0.0421 0.014 0.873 0.570 10.327 0.099 2.534 25.017 0.08 44319. 0.5276 3.15 0.1586 0.3354 0.0898 0.0425 0.014 0.880 0.557 10.411 0.099 2.477 24.259 0.08 44368. 0.5058 3.68 0.1850 0.3793 0.0876 0.0427 0.014 0.885 0.543 10.473 0.100 2.415 23.514 0.08 44421. 0.4841 4.20 0.2114 0.4200 0.0852 0.0429 0.014 0.888 0.528 10.511 0.100 2.349 22.784 0.08 44478. 0.4626 4.73 0.2379 0.4577 0.0826 0.0429 0.014 0.889 0.512 10.522 0.100 2.277 22.068 0.08 44538. 0.4412 5.26 0.2643 0.4923 0.0798 0.0428 0.014 0.888 0.495 10.501 0.100 2.200 21.366 0.08 44603. 0.4199 5.78 0.2907 0.5241 0.0768 0.0426 0.014 0.883 0.476 10.445 0.100 2.118 20.678 0.08 44672. 0.3987 6.31 0.3172 0.5531 0.0737 0.0422 0.014 0.875 0.456 10.352 0.099 2.030 20.001 0.08 44745. 0.3776 6.83 0.3436 0.5792 0.0703 0.0417 0.014 0.863 0.435 10.216 0.098 1.937 19.334 0.08 44822. 0.3565 7.36 0.3700 0.6024 0.0667 0.0409 0.013 0.848 0.413 10.036 0.096 1.838 18.674 0.08 44903. 0.3354 7.88 0.3965 0.6227 0.0629 0.0400 0.013 0.829 0.390 9.810 0.094 1.733 18.016 0.08 44989. 0.3142 8.41 0.4229 0.6399 0.0589 0.0389 0.013 0.806 0.365 9.539 0.091 1.624 17.357 0.08 45079. 0.2930 8.94 0.4493 0.6538 0.0548 0.0376 0.012 0.780 0.339 9.225 0.088 1.510 16.691 0.08 45173. 0.2717 9.46 0.4758 0.6640 0.0505 0.0362 0.012 0.750 0.313 8.869 0.085 1.392 16.010 0.08 45272. 0.2503 9.99 0.5022 0.6701 0.0461 0.0346 0.011 0.716 0.286 8.472 0.081 1.272 15.306 0.08 45374. 0.2287 10.51 0.5286 0.6714 0.0416 0.0328 0.011 0.679 0.258 8.036 0.077 1.148 14.569 0.08 45481. 0.2068 11.04 0.5550 0.6670 0.0371 0.0309 0.010 0.639 0.230 7.563 0.072 1.022 13.785 0.08 45592. 0.1847 11.56 0.5815 0.6558 0.0325 0.0288 0.009 0.596 0.201 7.053 0.067 0.895 12.936 0.08 45708. 0.1621 12.09 0.6079 0.6359 0.0278 0.0266 0.009 0.550 0.172 6.509 0.062 0.766 11.998 0.08 45828. 0.1391 12.61 0.6343 0.6048 0.0231 0.0242 0.008 0.501 0.143 5.932 0.057 0.636 10.936 0.08 45952. 0.1156 13.14 0.6608 0.5585 0.0184 0.0217 0.007 0.450 0.114 5.327 0.051 0.506 9.696 0.09 46080. 0.0914 13.67 0.6872 0.4910 0.0137 0.0192 0.006 0.397 0.085 4.695 0.045 0.377 8.196 0.09 46213. 0.0667 14.19 0.7136 0.3917 0.0090 0.0165 0.005 0.341 0.056 4.040 0.039 0.249 6.296 0.09 46350. 0.0417 14.72 0.7401 0.2417 0.0045 0.0137 0.005 0.285 0.028 3.367 0.032 0.124 3.746 0.09 46491. 0.0175 15.24 0.7665 0.0020 0.0000 0.0109 0.004 0.227 0.000 2.681 0.026 0.001 0.030 0.09 46635. 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 0.1004 0.0371 0.098 3.076 2.489 72.795 0.348 11.069 15.506 0.17 88249. 0.6834 1.06 0.0266 0.0697 0.0990 0.0377 0.099 3.128 2.455 74.007 0.353 10.921 15.048 0.17 88314. 0.6588 2.11 0.0531 0.1351 0.0976 0.0383 0.101 3.177 2.419 75.174 0.359 10.759 14.594 0.17 88385. 0.6342 3.17 0.0797 0.1965 0.0960 0.0389 0.102 3.223 2.379 76.273 0.364 10.582 14.147 0.17 88463. 0.6097 4.22 0.1062 0.2538 0.0942 0.0394 0.104 3.266 2.335 77.281 0.369 10.388 13.707 0.17 88548. 0.5853 5.28 0.1328 0.3073 0.0923 0.0399 0.105 3.304 2.288 78.173 0.373 10.177 13.276 0.17 88639. 0.5611 6.34 0.1593 0.3571 0.0902 0.0403 0.106 3.335 2.237 78.922 0.377 9.949 12.854 0.17 88738. 0.5371 7.39 0.1859 0.4032 0.0880 0.0405 0.107 3.360 2.181 79.502 0.380 9.701 12.443 0.17 88845. 0.5134 8.45 0.2124 0.4460 0.0855 0.0407 0.107 3.376 2.121 79.882 0.381 9.433 12.042 0.17 88959. 0.4900 9.50 0.2390 0.4855 0.0829 0.0408 0.107 3.382 2.056 80.035 0.382 9.145 11.652 0.17 89081. 0.4668 10.56 0.2655 0.5219 0.0801 0.0408 0.107 3.378 1.986 79.930 0.382 8.836 11.272 0.17 89211. 0.4439 11.62 0.2921 0.5552 0.0771 0.0406 0.107 3.361 1.912 79.539 0.380 8.504 10.903 0.17 89350. 0.4212 12.67 0.3186 0.5857 0.0739 0.0402 0.106 3.332 1.832 78.833 0.376 8.151 10.543 0.17 89497. 0.3988 13.73 0.3452 0.6134 0.0705 0.0397 0.104 3.287 1.748 77.779 0.371 7.774 10.191 0.17 89653. 0.3764 14.78 0.3717 0.6382 0.0669 0.0389 0.102 3.227 1.658 76.352 0.365 7.373 9.847 0.17 89817. 0.3542 15.84 0.3983 0.6603 0.0630 0.0380 0.100 3.150 1.563 74.543 0.356 6.951 9.508 0.17 89990. 0.3321 16.90 0.4248 0.6794 0.0590 0.0369 0.097 3.058 1.463 72.360 0.345 6.509 9.172 0.17 90171. 0.3100 17.95 0.4514 0.6955 0.0549 0.0356 0.094 2.950 1.360 69.810 0.333 6.050 8.837 0.17 90361. 0.2880 19.01 0.4779 0.7082 0.0506 0.0341 0.090 2.827 1.254 66.904 0.319 5.576 8.498 0.17 90559. 0.2659 20.06 0.5045 0.7171 0.0462 0.0325 0.085 2.690 1.144 63.652 0.304 5.089 8.153 0.17 90767. 0.2437 21.12 0.5310 0.7218 0.0416 0.0306 0.081 2.538 1.032 60.062 0.287 4.592 7.795 0.17 90982. 0.2213 22.18 0.5576 0.7213 0.0370 0.0286 0.075 2.373 0.918 56.147 0.268 4.085 7.419 0.17 91207. 0.1987 23.23 0.5841 0.7145 0.0324 0.0265 0.070 2.194 0.803 51.921 0.248 3.572 7.015 0.17 91440. 0.1756 24.29 0.6107 0.6996 0.0277 0.0242 0.064 2.003 0.687 47.398 0.226 3.054 6.570 0.17 91681. 0.1521 25.34 0.6372 0.6739 0.0230 0.0217 0.057 1.800 0.570 42.597 0.203 2.534 6.065 0.17 91931. 0.1279 26.40 0.6638 0.6329 0.0183 0.0191 0.050 1.587 0.453 37.542 0.179 2.013 5.469 0.17 92190. 0.1028 27.46 0.6903 0.5693 0.0136 0.0165 0.043 1.363 0.336 32.261 0.154 1.496 4.729 0.17 92458. 0.0766 28.51 0.7169 0.4687 0.0089 0.0137 0.036 1.132 0.221 26.787 0.128 0.985 3.750 0.17 92734. 0.0493 29.57 0.7434 0.3018 0.0044 0.0108 0.028 0.894 0.109 21.160 0.101 0.483 2.328 0.17 93018. 0.0214 30.62 0.7700 -0.0065 -0.0001 0.0079 0.021 0.651 -0.002 15.410 0.074 -0.007 -0.048 0.17 93308. 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 0.1008 0.0362 0.321 6.745 5.624 239.410 0.762 25.018 10.656 0.25 132369. 0.7061 1.59 0.0266 0.0718 0.0995 0.0368 0.327 6.864 5.550 243.634 0.776 24.686 10.332 0.25 132467. 0.6801 3.17 0.0532 0.1392 0.0980 0.0374 0.332 6.979 5.468 247.711 0.788 24.323 10.013 0.25 132574. 0.6542 4.76 0.0797 0.2023 0.0964 0.0380 0.337 7.088 5.379 251.561 0.801 23.925 9.698 0.25 132691. 0.6285 6.34 0.1063 0.2611 0.0947 0.0386 0.342 7.187 5.281 255.104 0.812 23.490 9.390 0.25 132818. 0.6029 7.93 0.1329 0.3159 0.0928 0.0390 0.346 7.276 5.175 258.254 0.822 23.017 9.088 0.25 132956. 0.5776 9.51 0.1595 0.3668 0.0907 0.0394 0.350 7.351 5.059 260.919 0.831 22.502 8.794 0.25 133105. 0.5527 11.10 0.1861 0.4140 0.0884 0.0397 0.353 7.410 4.933 263.005 0.837 21.944 8.508 0.25 133265. 0.5280 12.69 0.2126 0.4577 0.0860 0.0400 0.355 7.450 4.798 264.411 0.842 21.341 8.230 0.25 133437. 0.5037 14.27 0.2392 0.4981 0.0834 0.0401 0.355 7.467 4.652 265.037 0.844 20.690 7.961 0.25 133621. 0.4797 15.86 0.2658 0.5352 0.0806 0.0400 0.355 7.460 4.495 264.782 0.843 19.992 7.699 0.25 133817. 0.4561 17.44 0.2924 0.5694 0.0776 0.0398 0.353 7.425 4.326 263.544 0.839 19.243 7.446 0.25 134026. 0.4327 19.03 0.3190 0.6006 0.0743 0.0395 0.350 7.360 4.146 261.221 0.831 18.444 7.200 0.25 134247. 0.4096 20.61 0.3455 0.6291 0.0709 0.0389 0.346 7.261 3.955 257.705 0.820 17.591 6.961 0.25 134481. 0.3868 22.20 0.3721 0.6548 0.0672 0.0382 0.339 7.125 3.751 252.900 0.805 16.685 6.727 0.25 134728. 0.3641 23.79 0.3987 0.6777 0.0634 0.0373 0.331 6.953 3.536 246.779 0.786 15.729 6.499 0.25 134988. 0.3415 25.37 0.4253 0.6980 0.0594 0.0362 0.321 6.744 3.311 239.359 0.762 14.729 6.275 0.25 135260. 0.3190 26.96 0.4519 0.7152 0.0552 0.0349 0.309 6.499 3.078 230.668 0.734 13.690 6.052 0.25 135546. 0.2967 28.54 0.4784 0.7294 0.0509 0.0334 0.296 6.219 2.837 220.736 0.703 12.617 5.829 0.25 135844. 0.2743 30.13 0.5050 0.7400 0.0464 0.0317 0.281 5.905 2.589 209.595 0.667 11.516 5.603 0.25 136156. 0.2519 31.72 0.5316 0.7467 0.0419 0.0298 0.265 5.558 2.336 197.279 0.628 10.389 5.370 0.25 136480. 0.2293 33.30 0.5582 0.7486 0.0373 0.0278 0.247 5.179 2.078 183.825 0.585 9.243 5.127 0.25 136817. 0.2065 34.89 0.5848 0.7446 0.0326 0.0256 0.227 4.769 1.817 169.279 0.539 8.082 4.868 0.25 137168. 0.1834 36.47 0.6113 0.7331 0.0279 0.0232 0.206 4.330 1.554 153.695 0.489 6.910 4.585 0.25 137531. 0.1597 38.06 0.6379 0.7113 0.0231 0.0207 0.184 3.864 1.289 137.140 0.437 5.733 4.263 0.25 137907. 0.1352 39.64 0.6645 0.6748 0.0184 0.0181 0.161 3.372 1.025 119.693 0.381 4.558 3.883 0.26 138296. 0.1098 41.23 0.6911 0.6156 0.0137 0.0153 0.136 2.858 0.762 101.453 0.323 3.389 3.406 0.26 138698. 0.0831 42.82 0.7177 0.5181 0.0090 0.0125 0.111 2.325 0.502 82.539 0.263 2.234 2.760 0.26 139113. 0.0547 44.40 0.7443 0.3464 0.0044 0.0095 0.085 1.777 0.247 63.090 0.201 1.101 1.779 0.26 139541. 0.0247 45.99 0.7708 -0.0029 0.0000 0.0065 0.058 1.217 -0.001 43.203 0.138 -0.006 -0.014 0.26 139975. 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 0.1014 0.0358 0.753 11.860 10.057 561.277 1.340 44.733 8.127 0.33 176484. 0.7201 2.12 0.0266 0.0730 0.1001 0.0364 0.766 12.077 9.925 571.540 1.364 44.148 7.877 0.33 176615. 0.6934 4.23 0.0532 0.1415 0.0986 0.0371 0.780 12.287 9.781 581.457 1.388 43.506 7.630 0.33 176758. 0.6667 6.35 0.0798 0.2055 0.0970 0.0377 0.792 12.485 9.623 590.839 1.411 42.801 7.387 0.33 176915. 0.6403 8.46 0.1064 0.2652 0.0953 0.0382 0.804 12.668 9.449 599.489 1.431 42.031 7.149 0.33 177084. 0.6141 10.58 0.1329 0.3207 0.0934 0.0387 0.814 12.830 9.260 607.200 1.450 41.191 6.917 0.33 177269. 0.5882 12.69 0.1595 0.3723 0.0913 0.0391 0.823 12.969 9.055 613.749 1.465 40.276 6.692 0.33 177467. 0.5626 14.81 0.1861 0.4201 0.0891 0.0395 0.830 13.078 8.832 618.907 1.478 39.283 6.472 0.33 177681. 0.5374 16.92 0.2127 0.4644 0.0866 0.0397 0.835 13.152 8.590 622.433 1.486 38.209 6.260 0.33 177911. 0.5126 19.04 0.2393 0.5052 0.0840 0.0398 0.837 13.187 8.330 624.084 1.490 37.051 6.054 0.33 178157. 0.4882 21.15 0.2659 0.5429 0.0812 0.0398 0.836 13.177 8.050 623.613 1.489 35.805 5.855 0.33 178419. 0.4641 23.27 0.2925 0.5775 0.0781 0.0396 0.832 13.117 7.749 620.775 1.482 34.469 5.662 0.33 178698. 0.4404 25.38 0.3191 0.6093 0.0749 0.0392 0.825 13.002 7.428 615.324 1.469 33.040 5.475 0.33 178993. 0.4170 27.50 0.3457 0.6382 0.0715 0.0387 0.814 12.826 7.085 606.996 1.449 31.516 5.295 0.34 179306. 0.3938 29.61 0.3723 0.6645 0.0678 0.0380 0.799 12.585 6.721 595.561 1.422 29.896 5.119 0.34 179636. 0.3708 31.73 0.3988 0.6881 0.0639 0.0370 0.779 12.276 6.337 580.942 1.387 28.186 4.947 0.34 179983. 0.3480 33.84 0.4254 0.7091 0.0598 0.0359 0.755 11.900 5.934 563.176 1.344 26.396 4.779 0.34 180347. 0.3253 35.96 0.4520 0.7272 0.0556 0.0346 0.727 11.460 5.516 542.326 1.295 24.536 4.613 0.34 180728. 0.3027 38.07 0.4786 0.7424 0.0513 0.0331 0.695 10.955 5.084 518.464 1.238 22.615 4.448 0.34 181127. 0.2802 40.19 0.5052 0.7542 0.0468 0.0313 0.659 10.389 4.641 491.663 1.174 20.641 4.281 0.34 181542. 0.2577 42.30 0.5318 0.7623 0.0422 0.0295 0.620 9.762 4.187 462.002 1.103 18.623 4.110 0.34 181976. 0.2350 44.42 0.5584 0.7659 0.0376 0.0274 0.576 9.077 3.725 429.574 1.026 16.569 3.933 0.34 182426. 0.2121 46.53 0.5850 0.7640 0.0328 0.0252 0.529 8.336 3.257 394.486 0.942 14.488 3.745 0.34 182893. 0.1889 48.65 0.6116 0.7550 0.0281 0.0228 0.479 7.541 2.785 356.870 0.852 12.389 3.540 0.34 183378. 0.1651 50.76 0.6382 0.7362 0.0233 0.0202 0.425 6.696 2.311 316.885 0.757 10.280 3.308 0.34 183880. 0.1405 52.88 0.6647 0.7032 0.0185 0.0175 0.368 5.805 1.837 274.729 0.656 8.173 3.034 0.34 184399. 0.1149 54.99 0.6913 0.6479 0.0138 0.0147 0.309 4.874 1.367 230.641 0.551 6.079 2.688 0.34 184936. 0.0878 57.11 0.7179 0.5537 0.0091 0.0118 0.248 3.907 0.902 184.914 0.441 4.010 2.212 0.34 185490. 0.0587 59.22 0.7445 0.3804 0.0045 0.0088 0.185 2.914 0.445 137.887 0.329 1.981 1.465 0.34 186060. 0.0273 61.34 0.7711 -0.0005 0.0000 0.0057 0.120 1.897 0.000 89.780 0.214 -0.002 -0.002 0.34 186638. 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 0.1022 0.0357 1.467 18.489 15.829 1093.707 2.089 70.406 6.564 0.42 220592. 0.7297 2.65 0.0266 0.0738 0.1008 0.0364 1.494 18.836 15.625 1114.238 2.128 69.501 6.361 0.42 220756. 0.7025 5.29 0.0532 0.1429 0.0994 0.0370 1.521 19.171 15.401 1134.095 2.166 68.505 6.160 0.42 220936. 0.6754 7.94 0.0798 0.2074 0.0978 0.0376 1.546 19.489 15.155 1152.900 2.202 67.412 5.962 0.42 221132. 0.6486 10.58 0.1064 0.2676 0.0961 0.0382 1.569 19.783 14.886 1170.261 2.235 66.213 5.770 0.42 221345. 0.6220 13.23 0.1330 0.3236 0.0942 0.0387 1.590 20.045 14.592 1185.763 2.265 64.903 5.581 0.42 221575. 0.5957 15.87 0.1596 0.3756 0.0921 0.0391 1.608 20.268 14.270 1198.961 2.290 63.475 5.399 0.42 221824. 0.5698 18.52 0.1862 0.4238 0.0898 0.0395 1.622 20.444 13.922 1209.391 2.310 61.923 5.221 0.42 222093. 0.5443 21.16 0.2128 0.4684 0.0874 0.0397 1.631 20.566 13.544 1216.580 2.323 60.242 5.049 0.42 222381. 0.5192 23.81 0.2394 0.5096 0.0848 0.0398 1.636 20.624 13.135 1220.037 2.330 58.426 4.883 0.42 222689. 0.4945 26.45 0.2660 0.5476 0.0819 0.0398 1.635 20.611 12.696 1219.273 2.329 56.470 4.723 0.42 223017. 0.4702 29.10 0.2926 0.5826 0.0789 0.0396 1.628 20.519 12.224 1213.797 2.318 54.371 4.568 0.42 223366. 0.4462 31.74 0.3192 0.6148 0.0756 0.0393 1.613 20.338 11.719 1203.119 2.298 52.125 4.418 0.42 223737. 0.4226 34.39 0.3458 0.6441 0.0722 0.0387 1.591 20.061 11.180 1186.721 2.266 49.727 4.273 0.42 224129. 0.3992 37.03 0.3724 0.6709 0.0685 0.0380 1.561 19.679 10.606 1164.131 2.223 47.176 4.132 0.42 224542. 0.3760 39.68 0.3990 0.6950 0.0645 0.0371 1.522 19.190 10.000 1135.187 2.168 44.481 3.996 0.42 224977. 0.3531 42.32 0.4256 0.7165 0.0604 0.0359 1.475 18.594 9.366 1099.952 2.101 41.659 3.862 0.42 225433. 0.3302 44.97 0.4522 0.7354 0.0562 0.0346 1.420 17.894 8.706 1058.551 2.022 38.724 3.730 0.42 225910. 0.3075 47.61 0.4788 0.7513 0.0518 0.0330 1.356 17.093 8.024 1011.124 1.931 35.692 3.600 0.42 226410. 0.2849 50.26 0.5054 0.7641 0.0473 0.0313 1.284 16.191 7.324 957.815 1.829 32.576 3.468 0.42 226930. 0.2622 52.90 0.5320 0.7733 0.0426 0.0293 1.205 15.193 6.607 898.783 1.717 29.389 3.334 0.42 227472. 0.2395 55.55 0.5586 0.7782 0.0379 0.0272 1.119 14.102 5.878 834.209 1.593 26.144 3.196 0.42 228036. 0.2165 58.19 0.5852 0.7779 0.0332 0.0249 1.025 12.920 5.138 764.308 1.460 22.856 3.049 0.42 228621. 0.1931 60.84 0.6118 0.7708 0.0283 0.0225 0.924 11.653 4.393 689.343 1.317 19.538 2.890 0.42 229228. 0.1692 63.48 0.6384 0.7544 0.0235 0.0199 0.818 10.306 3.643 609.635 1.164 16.205 2.711 0.43 229856. 0.1446 66.13 0.6650 0.7242 0.0187 0.0172 0.705 8.885 2.895 525.580 1.004 12.875 2.498 0.43 230506. 0.1187 68.77 0.6916 0.6719 0.0139 0.0143 0.587 7.398 2.151 437.664 0.836 9.565 2.229 0.43 231178. 0.0913 71.42 0.7182 0.5802 0.0091 0.0113 0.465 5.857 1.416 346.473 0.662 6.296 1.853 0.43 231871. 0.0616 74.06 0.7449 0.4049 0.0045 0.0082 0.339 4.272 0.695 252.696 0.483 3.090 1.247 0.43 232584. 0.0290 76.71 0.7715 -0.0098 -0.0001 0.0051 0.210 2.649 -0.010 156.702 0.299 -0.045 -0.029 0.43 233304. 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 0.1031 0.0358 2.545 26.733 22.999 1897.708 3.020 102.299 5.497 0.50 264691. 0.7366 3.17 0.0266 0.0740 0.1018 0.0365 2.594 27.245 22.711 1934.066 3.078 101.017 5.326 0.50 264888. 0.7092 6.34 0.0531 0.1434 0.1004 0.0372 2.641 27.741 22.392 1969.268 3.134 99.601 5.158 0.50 265104. 0.6819 9.51 0.0797 0.2082 0.0988 0.0378 2.686 28.211 22.042 2002.636 3.187 98.043 4.992 0.50 265339. 0.6549 12.68 0.1063 0.2686 0.0971 0.0384 2.727 28.646 21.657 2033.487 3.236 96.331 4.831 0.50 265595. 0.6281 15.85 0.1329 0.3248 0.0952 0.0389 2.764 29.034 21.236 2061.070 3.280 94.456 4.673 0.50 265872. 0.6017 19.03 0.1594 0.3770 0.0931 0.0394 2.796 29.366 20.775 2084.608 3.318 92.408 4.520 0.50 266171. 0.5757 22.20 0.1860 0.4254 0.0909 0.0397 2.821 29.629 20.274 2103.278 3.347 90.178 4.372 0.50 266494. 0.5500 25.37 0.2126 0.4702 0.0884 0.0400 2.838 29.812 19.730 2116.245 3.368 87.758 4.229 0.50 266840. 0.5248 28.54 0.2392 0.5117 0.0858 0.0401 2.847 29.902 19.141 2122.644 3.378 85.139 4.090 0.50 267210. 0.5000 31.71 0.2657 0.5500 0.0829 0.0401 2.845 29.887 18.506 2121.612 3.377 82.316 3.956 0.50 267604. 0.4756 34.88 0.2923 0.5852 0.0799 0.0399 2.833 29.756 17.824 2112.290 3.362 79.281 3.827 0.50 268024. 0.4515 38.05 0.3189 0.6177 0.0766 0.0396 2.808 29.496 17.093 2093.814 3.332 76.031 3.703 0.50 268468. 0.4277 41.22 0.3455 0.6474 0.0731 0.0390 2.770 29.094 16.312 2065.283 3.287 72.557 3.582 0.50 268939. 0.4043 44.39 0.3720 0.6745 0.0694 0.0383 2.717 28.538 15.481 2025.854 3.224 68.857 3.466 0.50 269435. 0.3810 47.56 0.3986 0.6991 0.0654 0.0373 2.649 27.825 14.601 1975.198 3.144 64.945 3.353 0.50 269956. 0.3580 50.73 0.4252 0.7212 0.0613 0.0361 2.566 26.954 13.679 1913.418 3.045 60.844 3.243 0.50 270504. 0.3351 53.90 0.4518 0.7406 0.0570 0.0348 2.468 25.930 12.719 1840.730 2.930 56.576 3.134 0.50 271077. 0.3123 57.08 0.4783 0.7573 0.0526 0.0332 2.357 24.756 11.727 1757.379 2.797 52.163 3.027 0.51 271676. 0.2896 60.25 0.5049 0.7710 0.0480 0.0314 2.231 23.436 10.707 1663.621 2.648 47.625 2.919 0.51 272300. 0.2669 63.42 0.5315 0.7812 0.0433 0.0295 2.092 21.972 9.663 1559.732 2.482 42.982 2.810 0.51 272950. 0.2441 66.59 0.5581 0.7875 0.0385 0.0273 1.939 20.370 8.600 1446.034 2.301 38.253 2.698 0.51 273626. 0.2210 69.76 0.5846 0.7887 0.0337 0.0250 1.774 18.636 7.522 1322.907 2.105 33.457 2.579 0.51 274328. 0.1976 72.93 0.6112 0.7835 0.0288 0.0225 1.597 16.775 6.434 1190.809 1.895 28.617 2.451 0.51 275055. 0.1737 76.10 0.6378 0.7694 0.0239 0.0198 1.408 14.796 5.340 1050.309 1.672 23.753 2.306 0.51 275808. 0.1489 79.27 0.6644 0.7421 0.0190 0.0170 1.210 12.708 4.247 902.104 1.436 18.891 2.135 0.51 276587. 0.1230 82.44 0.6909 0.6935 0.0142 0.0141 1.002 10.524 3.160 747.052 1.189 14.057 1.919 0.51 277391. 0.0953 85.61 0.7175 0.6060 0.0094 0.0111 0.786 8.258 2.087 586.193 0.933 9.282 1.615 0.51 278221. 0.0652 88.78 0.7441 0.4336 0.0046 0.0079 0.564 5.927 1.033 420.752 0.670 4.596 1.114 0.51 279076. 0.0316 91.95 0.7707 0.0027 0.0000 0.0047 0.337 3.542 0.004 251.423 0.400 0.017 0.007 0.51 279939. 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 0.1042 0.0362 4.080 36.740 31.646 3042.755 4.151 140.763 4.717 0.58 308777. 0.7415 3.70 0.0266 0.0741 0.1029 0.0369 4.160 37.458 31.262 3102.218 4.232 139.055 4.571 0.58 309007. 0.7141 7.40 0.0531 0.1435 0.1015 0.0376 4.237 38.154 30.837 3159.848 4.311 137.161 4.426 0.58 309260. 0.6868 11.09 0.0797 0.2084 0.1000 0.0382 4.311 38.814 30.366 3214.535 4.385 135.070 4.285 0.58 309535. 0.6597 14.79 0.1063 0.2689 0.0983 0.0388 4.379 39.425 29.848 3265.150 4.454 132.765 4.146 0.58 309834. 0.6329 18.49 0.1328 0.3252 0.0964 0.0394 4.439 39.973 29.279 3310.467 4.516 130.232 4.012 0.58 310158. 0.6065 22.19 0.1594 0.3775 0.0944 0.0398 4.491 40.440 28.655 3349.201 4.569 127.458 3.881 0.58 310508. 0.5804 25.89 0.1860 0.4260 0.0921 0.0402 4.533 40.812 27.974 3380.011 4.611 124.429 3.754 0.58 310885. 0.5548 29.58 0.2125 0.4710 0.0897 0.0405 4.562 41.072 27.233 3401.519 4.640 121.133 3.631 0.58 311290. 0.5295 33.28 0.2391 0.5126 0.0870 0.0406 4.576 41.203 26.430 3412.323 4.655 117.561 3.513 0.58 311723. 0.5046 36.98 0.2657 0.5511 0.0842 0.0406 4.574 41.187 25.562 3411.020 4.653 113.701 3.399 0.59 312184. 0.4802 40.68 0.2922 0.5866 0.0811 0.0404 4.554 41.008 24.628 3396.208 4.633 109.545 3.289 0.59 312675. 0.4561 44.38 0.3188 0.6193 0.0778 0.0400 4.515 40.649 23.626 3366.500 4.593 105.087 3.183 0.59 313195. 0.4323 48.07 0.3453 0.6493 0.0743 0.0395 4.453 40.093 22.553 3320.440 4.530 100.317 3.081 0.59 313745. 0.4088 51.77 0.3719 0.6768 0.0705 0.0387 4.367 39.323 21.410 3256.641 4.443 95.230 2.982 0.59 314325. 0.3855 55.47 0.3985 0.7018 0.0665 0.0378 4.257 38.331 20.199 3174.517 4.331 89.843 2.886 0.59 314935. 0.3624 59.17 0.4250 0.7244 0.0623 0.0366 4.123 37.120 18.927 3074.212 4.194 84.189 2.793 0.59 315575. 0.3395 62.87 0.4516 0.7444 0.0580 0.0352 3.964 35.694 17.603 2956.083 4.033 78.299 2.701 0.59 316244. 0.3166 66.56 0.4782 0.7618 0.0535 0.0336 3.782 34.057 16.233 2820.532 3.848 72.204 2.610 0.59 316944. 0.2939 70.26 0.5047 0.7762 0.0488 0.0317 3.578 32.215 14.823 2667.985 3.640 65.932 2.520 0.59 317673. 0.2711 73.96 0.5313 0.7874 0.0441 0.0297 3.351 30.173 13.379 2498.897 3.409 59.510 2.428 0.59 318432. 0.2482 77.66 0.5579 0.7947 0.0392 0.0275 3.103 27.938 11.908 2313.795 3.156 52.965 2.334 0.59 319221. 0.2251 81.36 0.5844 0.7972 0.0343 0.0251 2.834 25.517 10.415 2113.299 2.883 46.324 2.235 0.59 320040. 0.2016 85.05 0.6110 0.7936 0.0293 0.0226 2.545 22.920 8.907 1898.160 2.589 39.618 2.128 0.59 320889. 0.1775 88.75 0.6376 0.7814 0.0243 0.0199 2.239 20.156 7.391 1669.306 2.277 32.877 2.008 0.59 321767. 0.1526 92.45 0.6641 0.7565 0.0193 0.0170 1.915 17.241 5.876 1427.880 1.948 26.135 1.866 0.60 322676. 0.1264 96.15 0.6907 0.7106 0.0144 0.0140 1.576 14.191 4.368 1175.285 1.603 19.431 1.686 0.60 323614. 0.0985 99.85 0.7173 0.6259 0.0095 0.0109 1.225 11.027 2.879 913.235 1.246 12.806 1.430 0.60 324582. 0.0678 103.54 0.7438 0.4534 0.0047 0.0077 0.863 7.773 1.418 643.752 0.878 6.305 0.999 0.60 325579. 0.0332 107.24 0.7704 -0.0069 0.0000 0.0044 0.493 4.441 -0.012 367.803 0.502 -0.053 -0.015 0.60 326582. 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 0.1056 0.0368 6.185 48.728 41.875 4612.065 5.505 186.258 4.118 0.67 352848. 0.7446 4.22 0.0265 0.0739 0.1043 0.0375 6.308 49.697 41.388 4703.750 5.615 184.095 3.991 0.67 353111. 0.7174 8.44 0.0531 0.1431 0.1030 0.0382 6.427 50.637 40.847 4792.805 5.721 181.686 3.866 0.67 353400. 0.6903 12.67 0.0796 0.2078 0.1015 0.0389 6.541 51.532 40.246 4877.502 5.822 179.013 3.743 0.67 353714. 0.6634 16.89 0.1062 0.2682 0.0998 0.0395 6.646 52.362 39.581 4956.026 5.916 176.054 3.622 0.67 354057. 0.6368 21.11 0.1327 0.3244 0.0979 0.0401 6.741 53.106 38.846 5026.458 6.000 172.789 3.505 0.67 354428. 0.6105 25.33 0.1592 0.3767 0.0959 0.0405 6.822 53.744 38.039 5086.794 6.072 169.198 3.392 0.67 354829. 0.5845 29.56 0.1858 0.4252 0.0937 0.0409 6.886 54.252 37.155 5134.936 6.129 165.263 3.282 0.67 355261. 0.5589 33.78 0.2123 0.4702 0.0912 0.0412 6.931 54.610 36.189 5168.759 6.170 160.968 3.176 0.67 355725. 0.5338 38.00 0.2389 0.5120 0.0886 0.0413 6.955 54.793 35.139 5186.094 6.190 156.298 3.073 0.67 356221. 0.5090 42.22 0.2654 0.5506 0.0857 0.0413 6.953 54.779 34.001 5184.797 6.189 151.239 2.974 0.67 356750. 0.4846 46.44 0.2919 0.5863 0.0826 0.0411 6.923 54.546 32.774 5162.719 6.163 145.780 2.879 0.67 357312. 0.4606 50.67 0.3185 0.6192 0.0793 0.0408 6.863 54.070 31.455 5117.741 6.109 139.911 2.788 0.67 357907. 0.4369 54.89 0.3450 0.6495 0.0757 0.0402 6.769 53.330 30.041 5047.681 6.025 133.622 2.699 0.67 358537. 0.4134 59.11 0.3716 0.6774 0.0719 0.0395 6.639 52.302 28.530 4950.375 5.909 126.902 2.614 0.67 359201. 0.3901 63.33 0.3981 0.7028 0.0679 0.0385 6.470 50.976 26.928 4824.828 5.759 119.774 2.531 0.67 359899. 0.3670 67.55 0.4246 0.7259 0.0636 0.0372 6.264 49.353 25.243 4671.218 5.576 112.280 2.451 0.67 360631. 0.3441 71.78 0.4512 0.7465 0.0592 0.0358 6.021 47.439 23.485 4490.105 5.360 104.463 2.372 0.67 361397. 0.3212 76.00 0.4777 0.7646 0.0546 0.0341 5.742 45.242 21.665 4282.122 5.111 96.364 2.295 0.67 362197. 0.2984 80.22 0.5042 0.7798 0.0499 0.0323 5.428 42.768 19.789 4047.942 4.832 88.021 2.217 0.67 363031. 0.2756 84.44 0.5308 0.7919 0.0450 0.0302 5.080 40.024 17.867 3788.279 4.522 79.471 2.139 0.68 363899. 0.2526 88.67 0.5573 0.8003 0.0401 0.0279 4.699 37.020 15.906 3503.953 4.183 70.749 2.059 0.68 364800. 0.2294 92.89 0.5839 0.8042 0.0351 0.0255 4.286 33.766 13.915 3195.917 3.815 61.894 1.975 0.68 365736. 0.2058 97.11 0.6104 0.8022 0.0300 0.0228 3.842 30.273 11.903 2865.331 3.420 52.944 1.884 0.68 366705. 0.1816 101.33 0.6369 0.7919 0.0249 0.0200 3.371 26.557 9.879 2513.618 3.000 43.942 1.783 0.68 367708. 0.1566 105.55 0.6635 0.7694 0.0198 0.0171 2.873 22.637 7.854 2142.542 2.557 34.934 1.663 0.68 368745. 0.1302 109.78 0.6900 0.7265 0.0147 0.0140 2.353 18.535 5.839 1754.300 2.094 25.971 1.510 0.68 369816. 0.1019 114.00 0.7166 0.6451 0.0097 0.0108 1.813 14.280 3.846 1351.620 1.613 17.109 1.291 0.68 370921. 0.0707 118.22 0.7431 0.4740 0.0048 0.0075 1.258 9.908 1.891 937.781 1.119 8.411 0.915 0.68 372059. 0.0351 122.44 0.7696 -0.0109 -0.0001 0.0041 0.690 5.434 -0.023 514.345 0.614 -0.102 -0.020 0.69 373201. 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 0.1072 0.0381 9.129 63.934 53.807 6807.694 7.223 239.335 3.585 0.75 396898. 0.7348 4.74 0.0265 0.0724 0.1060 0.0388 9.295 65.091 53.222 6930.960 7.354 236.730 3.483 0.75 397193. 0.7100 9.48 0.0530 0.1406 0.1047 0.0395 9.455 66.217 52.565 7050.805 7.481 233.809 3.381 0.75 397518. 0.6850 14.23 0.0795 0.2046 0.1032 0.0401 9.608 67.288 51.831 7164.888 7.602 230.545 3.281 0.75 397872. 0.6600 18.97 0.1060 0.2646 0.1016 0.0407 9.750 68.283 51.013 7270.776 7.715 226.908 3.182 0.75 398258. 0.6351 23.71 0.1325 0.3207 0.0998 0.0412 9.878 69.175 50.106 7365.835 7.815 222.869 3.085 0.75 398676. 0.6102 28.45 0.1590 0.3730 0.0978 0.0417 9.987 69.940 49.101 7447.246 7.902 218.403 2.990 0.75 399128. 0.5855 33.19 0.1855 0.4217 0.0956 0.0420 10.074 70.548 47.995 7512.000 7.970 213.482 2.898 0.75 399615. 0.5610 37.93 0.2120 0.4669 0.0932 0.0423 10.134 70.970 46.782 7556.982 8.018 208.085 2.808 0.75 400138. 0.5366 42.68 0.2384 0.5090 0.0905 0.0424 10.164 71.177 45.456 7578.984 8.042 202.190 2.720 0.75 400697. 0.5125 47.42 0.2649 0.5479 0.0877 0.0424 10.158 71.137 44.015 7574.743 8.037 195.780 2.636 0.75 401293. 0.4886 52.16 0.2914 0.5839 0.0846 0.0422 10.113 70.820 42.455 7540.966 8.001 188.840 2.554 0.75 401926. 0.4649 56.90 0.3179 0.6172 0.0812 0.0418 10.023 70.195 40.773 7474.365 7.931 181.357 2.474 0.75 402598. 0.4414 61.64 0.3444 0.6479 0.0776 0.0413 9.885 69.229 38.966 7371.562 7.821 173.319 2.398 0.75 403307. 0.4182 66.39 0.3709 0.6762 0.0738 0.0405 9.694 67.891 37.030 7229.101 7.670 164.711 2.323 0.75 404055. 0.3950 71.13 0.3974 0.7021 0.0697 0.0394 9.448 66.163 34.972 7045.052 7.475 155.557 2.252 0.76 404841. 0.3720 75.87 0.4239 0.7257 0.0653 0.0382 9.145 64.044 32.804 6819.487 7.236 145.912 2.182 0.76 405666. 0.3492 80.61 0.4504 0.7469 0.0608 0.0367 8.788 61.544 30.538 6553.218 6.953 135.832 2.114 0.76 406528. 0.3264 85.35 0.4769 0.7657 0.0561 0.0350 8.378 58.670 28.186 6247.235 6.629 125.372 2.046 0.76 407428. 0.3036 90.09 0.5034 0.7818 0.0513 0.0330 7.916 55.434 25.760 5902.632 6.263 114.581 1.979 0.76 408366. 0.2807 94.84 0.5299 0.7949 0.0464 0.0309 7.403 51.846 23.270 5520.625 5.858 103.507 1.912 0.76 409342. 0.2577 99.58 0.5564 0.8043 0.0413 0.0286 6.843 47.921 20.728 5102.615 5.414 92.199 1.843 0.76 410355. 0.2344 104.32 0.5829 0.8093 0.0361 0.0260 6.236 43.673 18.144 4650.308 4.934 80.704 1.770 0.76 411406. 0.2106 109.06 0.6094 0.8084 0.0309 0.0233 5.586 39.123 15.529 4165.811 4.420 69.074 1.691 0.76 412495. 0.1862 113.80 0.6359 0.7991 0.0257 0.0204 4.897 34.295 12.896 3651.796 3.875 57.362 1.602 0.76 413621. 0.1607 118.54 0.6623 0.7771 0.0204 0.0174 4.173 29.222 10.258 3111.621 3.302 45.629 1.495 0.77 414786. 0.1338 123.29 0.6888 0.7337 0.0152 0.0143 3.419 23.943 7.631 2549.480 2.705 33.940 1.358 0.77 415988. 0.1048 128.03 0.7153 0.6498 0.0100 0.0110 2.642 18.506 5.029 1970.500 2.091 22.370 1.158 0.77 417227. 0.0725 132.77 0.7418 0.4728 0.0049 0.0077 1.852 12.967 2.473 1380.720 1.465 10.999 0.812 0.77 418504. 0.0357 137.51 0.7683 -0.0111 -0.0001 0.0044 1.051 7.358 -0.032 783.463 0.831 -0.141 -0.018 0.77 419786. 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 0.1090 0.0426 14.014 88.331 67.536 10450.542 9.980 300.402 2.931 0.83 440920. 0.6731 5.26 0.0265 0.0661 0.1079 0.0432 14.191 89.440 66.869 10581.860 10.105 297.432 2.866 0.83 441248. 0.6549 10.52 0.0529 0.1292 0.1067 0.0437 14.356 90.482 66.112 10705.080 10.223 294.068 2.801 0.83 441608. 0.6364 15.78 0.0794 0.1894 0.1053 0.0441 14.506 91.429 65.259 10817.092 10.330 290.272 2.736 0.83 442001. 0.6176 21.05 0.1058 0.2465 0.1037 0.0445 14.637 92.255 64.299 10914.832 10.423 286.002 2.672 0.83 442430. 0.5987 26.31 0.1323 0.3008 0.1020 0.0449 14.745 92.933 63.223 10995.044 10.499 281.216 2.608 0.83 442896. 0.5794 31.57 0.1587 0.3522 0.1001 0.0451 14.824 93.435 62.023 11054.511 10.556 275.879 2.545 0.83 443399. 0.5600 36.83 0.1852 0.4008 0.0979 0.0453 14.872 93.735 60.691 11089.907 10.590 269.953 2.482 0.83 443942. 0.5403 42.09 0.2117 0.4466 0.0955 0.0453 14.882 93.801 59.219 11097.765 10.598 263.406 2.420 0.83 444524. 0.5204 47.35 0.2381 0.4897 0.0929 0.0452 14.851 93.605 57.601 11074.526 10.575 256.210 2.359 0.84 445147. 0.5003 52.61 0.2646 0.5302 0.0901 0.0450 14.773 93.114 55.832 11016.530 10.520 248.339 2.299 0.84 445812. 0.4799 57.88 0.2910 0.5681 0.0870 0.0446 14.644 92.299 53.905 10920.017 10.428 239.772 2.239 0.84 446519. 0.4593 63.14 0.3175 0.6034 0.0836 0.0440 14.458 91.125 51.819 10781.165 10.295 230.491 2.180 0.84 447267. 0.4385 68.40 0.3439 0.6362 0.0800 0.0432 14.209 89.560 49.568 10595.981 10.118 220.480 2.122 0.84 448058. 0.4174 73.66 0.3704 0.6666 0.0761 0.0423 13.893 87.566 47.150 10360.042 9.893 209.721 2.064 0.84 448892. 0.3960 78.92 0.3969 0.6945 0.0719 0.0411 13.505 85.119 44.568 10070.546 9.617 198.239 2.007 0.84 449768. 0.3744 84.18 0.4233 0.7200 0.0675 0.0397 13.044 82.217 41.839 9727.233 9.289 186.101 1.951 0.84 450686. 0.3526 89.44 0.4498 0.7429 0.0629 0.0381 12.514 78.873 38.980 9331.662 8.911 173.381 1.895 0.84 451646. 0.3305 94.71 0.4762 0.7628 0.0581 0.0363 11.920 75.129 36.004 8888.682 8.488 160.146 1.837 0.84 452648. 0.3080 99.97 0.5027 0.7795 0.0531 0.0343 11.261 70.976 32.928 8397.328 8.019 146.465 1.779 0.84 453692. 0.2852 105.23 0.5292 0.7922 0.0480 0.0321 10.543 66.451 29.765 7861.947 7.508 132.396 1.717 0.84 454777. 0.2618 110.49 0.5556 0.8004 0.0428 0.0297 9.765 61.549 26.530 7281.935 6.954 118.005 1.652 0.85 455903. 0.2378 115.75 0.5821 0.8030 0.0375 0.0272 8.932 56.296 23.236 6660.533 6.360 103.355 1.582 0.85 457071. 0.2131 121.01 0.6085 0.7977 0.0321 0.0245 8.049 50.735 19.899 6002.499 5.732 88.510 1.504 0.85 458281. 0.1874 126.27 0.6350 0.7813 0.0267 0.0217 7.126 44.913 16.533 5313.683 5.074 73.540 1.411 0.85 459531. 0.1603 131.54 0.6614 0.7478 0.0212 0.0188 6.171 38.892 13.157 4601.439 4.394 58.521 1.297 0.85 460824. 0.1314 136.80 0.6879 0.6873 0.0158 0.0158 5.195 32.742 9.788 3873.786 3.699 43.537 1.146 0.85 462157. 0.1002 142.06 0.7144 0.5802 0.0104 0.0128 4.211 26.542 6.450 3140.247 2.999 28.690 0.932 0.85 463532. 0.0661 147.32 0.7408 0.3847 0.0051 0.0098 3.233 20.376 3.166 2410.713 2.302 14.082 0.596 0.86 464948. 0.0296 152.58 0.7673 -0.0094 -0.0001 0.0069 2.266 14.281 -0.052 1689.617 1.613 -0.233 -0.014 0.86 466378. 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 0.1096 0.0513 22.456 128.667 82.176 16745.152 14.537 365.517 2.226 0.92 484974. 0.5638 5.82 0.0266 0.0558 0.1087 0.0518 22.670 129.895 81.498 16904.859 14.675 362.502 2.187 0.92 485330. 0.5516 11.64 0.0532 0.1096 0.1076 0.0523 22.856 130.964 80.716 17044.090 14.796 359.023 2.148 0.92 485722. 0.5392 17.46 0.0798 0.1615 0.1064 0.0526 23.007 131.829 79.816 17156.607 14.894 355.022 2.110 0.92 486152. 0.5267 23.28 0.1064 0.2116 0.1051 0.0528 23.115 132.443 78.785 17236.508 14.963 350.434 2.073 0.92 486622. 0.5142 29.10 0.1330 0.2599 0.1035 0.0530 23.170 132.763 77.608 17278.113 14.999 345.199 2.037 0.92 487134. 0.5015 34.92 0.1596 0.3065 0.1017 0.0530 23.168 132.749 76.272 17276.355 14.998 339.259 2.002 0.92 487689. 0.4886 40.74 0.1862 0.3516 0.0997 0.0528 23.102 132.369 74.766 17226.857 14.955 332.557 1.969 0.92 488289. 0.4756 46.56 0.2128 0.3950 0.0974 0.0525 22.966 131.592 73.077 17125.803 14.867 325.045 1.935 0.92 488934. 0.4623 52.38 0.2394 0.4370 0.0949 0.0520 22.757 130.395 71.196 16969.973 14.732 316.679 1.903 0.92 489626. 0.4486 58.20 0.2661 0.4773 0.0922 0.0514 22.471 128.754 69.114 16756.457 14.547 307.421 1.871 0.92 490365. 0.4346 64.02 0.2927 0.5161 0.0891 0.0505 22.103 126.650 66.825 16482.574 14.309 297.237 1.839 0.92 491152. 0.4200 69.84 0.3193 0.5532 0.0858 0.0495 21.652 124.061 64.321 16145.667 14.016 286.101 1.807 0.92 491986. 0.4049 75.66 0.3459 0.5886 0.0821 0.0483 21.112 120.967 61.598 15742.991 13.667 273.988 1.775 0.92 492868. 0.3892 81.48 0.3725 0.6222 0.0782 0.0468 20.481 117.352 58.652 15272.529 13.258 260.884 1.742 0.92 493798. 0.3727 87.30 0.3991 0.6538 0.0740 0.0452 19.758 113.208 55.489 14733.216 12.790 246.817 1.708 0.92 494776. 0.3556 93.12 0.4257 0.6833 0.0695 0.0433 18.945 108.550 52.130 14127.051 12.264 231.874 1.674 0.92 495800. 0.3377 98.94 0.4523 0.7105 0.0648 0.0413 18.046 103.400 48.596 13456.824 11.682 216.155 1.638 0.93 496872. 0.3190 104.76 0.4789 0.7347 0.0599 0.0390 17.074 97.830 44.907 12731.880 11.053 199.747 1.600 0.93 497989. 0.2996 110.58 0.5055 0.7540 0.0548 0.0367 16.066 92.054 41.079 11980.129 10.400 182.721 1.555 0.93 499153. 0.2785 116.40 0.5321 0.7677 0.0495 0.0343 15.013 86.023 37.134 11195.266 9.719 165.173 1.504 0.93 500363. 0.2562 122.22 0.5587 0.7707 0.0441 0.0320 13.989 80.152 33.082 10431.260 9.056 147.151 1.438 0.93 501618. 0.2312 128.04 0.5853 0.7622 0.0386 0.0296 12.966 74.295 28.948 9669.008 8.394 128.761 1.358 0.93 502919. 0.2041 133.86 0.6119 0.7418 0.0330 0.0272 11.913 68.259 24.758 8883.468 7.712 110.124 1.264 0.93 504265. 0.1757 139.68 0.6385 0.7054 0.0274 0.0248 10.842 62.126 20.536 8085.251 7.019 91.343 1.152 0.94 505657. 0.1459 145.50 0.6651 0.6476 0.0217 0.0223 9.770 55.981 16.308 7285.532 6.325 72.539 1.015 0.94 507095. 0.1146 151.32 0.6917 0.5606 0.0161 0.0199 8.715 49.933 12.107 6498.426 5.641 53.854 0.845 0.94 508578. 0.0822 157.14 0.7183 0.4342 0.0106 0.0176 7.690 44.064 7.969 5734.635 4.978 35.448 0.630 0.94 510107. 0.0497 162.96 0.7449 0.2546 0.0052 0.0153 6.710 38.449 3.931 5003.875 4.344 17.486 0.356 0.94 511682. 0.0197 168.78 0.7716 0.0002 0.0000 0.0132 5.761 33.008 0.002 4295.819 3.729 0.009 0.000 0.94 513307. 0.0000