26x15E (26x15E.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 0.0898 0.0325 0.031 1.957 1.307 23.155 0.221 5.816 25.611 0.10 61813. 0.6609 0.62 0.0250 0.0672 0.0885 0.0330 0.032 1.987 1.289 23.504 0.224 5.733 24.873 0.10 61854. 0.6373 1.23 0.0501 0.1305 0.0871 0.0334 0.032 2.015 1.269 23.838 0.228 5.643 24.141 0.10 61899. 0.6137 1.85 0.0751 0.1899 0.0856 0.0339 0.032 2.041 1.247 24.150 0.231 5.546 23.417 0.10 61947. 0.5901 2.47 0.1002 0.2454 0.0840 0.0343 0.033 2.065 1.223 24.433 0.233 5.440 22.704 0.10 62000. 0.5666 3.08 0.1252 0.2973 0.0822 0.0346 0.033 2.086 1.197 24.680 0.236 5.325 22.002 0.10 62057. 0.5433 3.70 0.1502 0.3456 0.0803 0.0349 0.033 2.103 1.169 24.883 0.238 5.201 21.314 0.10 62119. 0.5201 4.32 0.1753 0.3905 0.0782 0.0351 0.034 2.116 1.139 25.034 0.239 5.067 20.641 0.10 62185. 0.4972 4.93 0.2003 0.4320 0.0760 0.0352 0.034 2.124 1.107 25.126 0.240 4.924 19.982 0.10 62256. 0.4744 5.55 0.2253 0.4703 0.0736 0.0353 0.034 2.126 1.072 25.150 0.240 4.769 19.338 0.10 62332. 0.4519 6.16 0.2504 0.5056 0.0711 0.0352 0.034 2.121 1.035 25.097 0.240 4.604 18.708 0.10 62413. 0.4296 6.78 0.2754 0.5378 0.0684 0.0350 0.033 2.110 0.996 24.960 0.238 4.429 18.092 0.10 62499. 0.4074 7.40 0.3005 0.5671 0.0655 0.0347 0.033 2.090 0.954 24.732 0.236 4.242 17.488 0.10 62591. 0.3854 8.01 0.3255 0.5935 0.0624 0.0342 0.033 2.063 0.909 24.404 0.233 4.043 16.894 0.10 62687. 0.3635 8.63 0.3505 0.6170 0.0592 0.0336 0.032 2.026 0.862 23.969 0.229 3.833 16.308 0.10 62789. 0.3416 9.25 0.3756 0.6375 0.0558 0.0329 0.031 1.980 0.812 23.423 0.224 3.612 15.726 0.10 62897. 0.3198 9.86 0.4006 0.6549 0.0522 0.0319 0.031 1.924 0.760 22.769 0.217 3.382 15.145 0.10 63009. 0.2980 10.48 0.4256 0.6689 0.0485 0.0309 0.030 1.860 0.706 22.009 0.210 3.142 14.560 0.10 63127. 0.2762 11.10 0.4507 0.6793 0.0447 0.0297 0.028 1.787 0.651 21.145 0.202 2.896 13.965 0.10 63251. 0.2543 11.71 0.4757 0.6856 0.0408 0.0283 0.027 1.706 0.594 20.181 0.193 2.643 13.352 0.10 63380. 0.2323 12.33 0.5008 0.6872 0.0368 0.0268 0.026 1.616 0.536 19.120 0.183 2.384 12.714 0.10 63514. 0.2100 12.95 0.5258 0.6832 0.0327 0.0252 0.024 1.518 0.477 17.964 0.172 2.121 12.037 0.10 63654. 0.1876 13.56 0.5508 0.6723 0.0286 0.0234 0.022 1.413 0.417 16.717 0.160 1.854 11.308 0.10 63799. 0.1648 14.18 0.5759 0.6529 0.0245 0.0216 0.021 1.300 0.356 15.384 0.147 1.585 10.504 0.10 63949. 0.1415 14.79 0.6009 0.6223 0.0203 0.0196 0.019 1.181 0.295 13.969 0.133 1.314 9.594 0.11 64106. 0.1177 15.41 0.6259 0.5763 0.0161 0.0175 0.017 1.055 0.235 12.481 0.119 1.044 8.530 0.11 64267. 0.0933 16.03 0.6510 0.5084 0.0120 0.0153 0.015 0.923 0.174 10.926 0.104 0.775 7.236 0.11 64434. 0.0682 16.64 0.6760 0.4070 0.0079 0.0131 0.012 0.787 0.115 9.314 0.089 0.510 5.578 0.11 64607. 0.0426 17.26 0.7011 0.2504 0.0038 0.0107 0.010 0.647 0.056 7.656 0.073 0.248 3.309 0.11 64785. 0.0176 17.88 0.7261 -0.0089 -0.0001 0.0084 0.008 0.504 -0.001 5.962 0.057 -0.007 -0.114 0.11 64966. 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 0.0902 0.0307 0.235 7.394 5.256 174.959 0.835 23.378 13.626 0.21 123622. 0.7050 1.23 0.0251 0.0715 0.0890 0.0312 0.239 7.519 5.182 177.921 0.850 23.050 13.211 0.21 123705. 0.6787 2.47 0.0502 0.1386 0.0876 0.0317 0.242 7.639 5.102 180.765 0.863 22.692 12.801 0.21 123794. 0.6525 3.70 0.0752 0.2014 0.0861 0.0322 0.246 7.752 5.014 183.436 0.876 22.302 12.398 0.21 123892. 0.6265 4.94 0.1003 0.2599 0.0844 0.0326 0.249 7.855 4.919 185.878 0.888 21.879 12.003 0.21 123998. 0.6008 6.17 0.1254 0.3144 0.0827 0.0330 0.252 7.946 4.816 188.032 0.898 21.420 11.616 0.21 124113. 0.5753 7.41 0.1505 0.3651 0.0808 0.0333 0.255 8.023 4.704 189.834 0.906 20.923 11.239 0.21 124237. 0.5501 8.64 0.1756 0.4120 0.0787 0.0335 0.256 8.081 4.583 191.216 0.913 20.387 10.872 0.21 124370. 0.5253 9.88 0.2006 0.4554 0.0765 0.0337 0.258 8.119 4.454 192.112 0.917 19.811 10.515 0.21 124512. 0.5008 11.11 0.2257 0.4955 0.0741 0.0337 0.258 8.133 4.315 192.452 0.919 19.192 10.169 0.21 124665. 0.4767 12.35 0.2508 0.5323 0.0715 0.0337 0.258 8.121 4.166 192.170 0.918 18.529 9.832 0.21 124828. 0.4529 13.58 0.2759 0.5661 0.0688 0.0335 0.256 8.080 4.007 191.198 0.913 17.822 9.505 0.21 125000. 0.4294 14.82 0.3009 0.5969 0.0659 0.0332 0.254 8.007 3.838 189.472 0.905 17.071 9.187 0.21 125184. 0.4062 16.05 0.3260 0.6248 0.0628 0.0328 0.251 7.900 3.658 186.923 0.892 16.273 8.877 0.21 125378. 0.3832 17.29 0.3511 0.6499 0.0595 0.0322 0.246 7.754 3.469 183.484 0.876 15.428 8.574 0.21 125582. 0.3604 18.52 0.3762 0.6721 0.0561 0.0314 0.240 7.570 3.269 179.131 0.855 14.539 8.277 0.21 125798. 0.3377 19.76 0.4013 0.6915 0.0525 0.0305 0.233 7.348 3.060 173.871 0.830 13.611 7.983 0.21 126024. 0.3151 20.99 0.4263 0.7078 0.0488 0.0294 0.225 7.088 2.844 167.722 0.801 12.649 7.690 0.21 126261. 0.2927 22.23 0.4514 0.7208 0.0450 0.0282 0.216 6.791 2.621 160.701 0.767 11.656 7.396 0.21 126509. 0.2702 23.46 0.4765 0.7301 0.0411 0.0268 0.205 6.459 2.392 152.829 0.730 10.638 7.098 0.21 126767. 0.2477 24.70 0.5016 0.7352 0.0370 0.0253 0.193 6.091 2.158 144.127 0.688 9.597 6.790 0.21 127037. 0.2251 25.93 0.5267 0.7354 0.0330 0.0236 0.181 5.689 1.920 134.620 0.643 8.539 6.468 0.21 127317. 0.2023 27.17 0.5517 0.7295 0.0288 0.0218 0.167 5.255 1.679 124.338 0.594 7.468 6.124 0.21 127608. 0.1791 28.40 0.5768 0.7157 0.0247 0.0199 0.152 4.789 1.436 113.317 0.541 6.387 5.748 0.21 127910. 0.1554 29.64 0.6019 0.6915 0.0205 0.0178 0.136 4.294 1.192 101.603 0.485 5.302 5.322 0.21 128224. 0.1311 30.87 0.6270 0.6523 0.0163 0.0156 0.120 3.772 0.948 89.252 0.426 4.218 4.820 0.21 128548. 0.1059 32.11 0.6521 0.5907 0.0121 0.0134 0.102 3.226 0.706 76.331 0.364 3.141 4.197 0.21 128883. 0.0796 33.34 0.6771 0.4921 0.0080 0.0110 0.084 2.659 0.467 62.922 0.300 2.077 3.366 0.21 129229. 0.0519 34.58 0.7022 0.3251 0.0040 0.0086 0.066 2.076 0.232 49.123 0.235 1.033 2.144 0.21 129586. 0.0233 35.81 0.7273 0.0060 0.0001 0.0061 0.047 1.479 0.003 35.006 0.167 0.013 0.038 0.21 129949. 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 0.0908 0.0301 0.776 16.312 11.906 578.983 1.843 52.956 9.327 0.31 185426. 0.7263 1.87 0.0253 0.0740 0.0896 0.0306 0.790 16.605 11.739 589.387 1.876 52.216 9.034 0.31 185550. 0.6985 3.74 0.0506 0.1432 0.0882 0.0311 0.804 16.887 11.557 599.389 1.908 51.407 8.746 0.31 185686. 0.6710 5.60 0.0759 0.2079 0.0867 0.0316 0.816 17.152 11.359 608.795 1.938 50.524 8.463 0.31 185835. 0.6437 7.47 0.1012 0.2681 0.0850 0.0321 0.828 17.395 11.143 617.409 1.965 49.563 8.186 0.31 185996. 0.6167 9.34 0.1264 0.3241 0.0832 0.0325 0.838 17.609 10.908 625.018 1.989 48.519 7.916 0.31 186170. 0.5900 11.21 0.1517 0.3760 0.0813 0.0328 0.847 17.789 10.654 631.394 2.010 47.388 7.653 0.31 186358. 0.5638 13.08 0.1770 0.4241 0.0792 0.0331 0.853 17.927 10.379 636.303 2.025 46.166 7.398 0.31 186561. 0.5379 14.94 0.2023 0.4685 0.0769 0.0332 0.858 18.017 10.083 639.502 2.036 44.849 7.151 0.31 186778. 0.5125 16.81 0.2276 0.5094 0.0745 0.0333 0.859 18.053 9.765 640.749 2.040 43.434 6.912 0.31 187010. 0.4875 18.68 0.2529 0.5471 0.0719 0.0332 0.858 18.026 9.424 639.803 2.037 41.917 6.681 0.31 187258. 0.4628 20.55 0.2782 0.5816 0.0691 0.0331 0.853 17.931 9.060 636.429 2.026 40.298 6.457 0.31 187521. 0.4386 22.42 0.3035 0.6131 0.0662 0.0327 0.845 17.761 8.672 630.395 2.007 38.574 6.240 0.31 187801. 0.4147 24.28 0.3288 0.6418 0.0630 0.0323 0.833 17.509 8.260 621.456 1.978 36.742 6.029 0.31 188096. 0.3910 26.15 0.3540 0.6677 0.0597 0.0317 0.817 17.169 7.824 609.381 1.940 34.802 5.824 0.31 188408. 0.3676 28.02 0.3793 0.6907 0.0562 0.0309 0.797 16.738 7.365 594.088 1.891 32.761 5.623 0.31 188736. 0.3444 29.89 0.4046 0.7110 0.0525 0.0299 0.772 16.217 6.886 575.605 1.832 30.630 5.426 0.31 189080. 0.3214 31.75 0.4299 0.7283 0.0487 0.0288 0.743 15.608 6.389 553.987 1.763 28.420 5.231 0.31 189441. 0.2984 33.62 0.4552 0.7424 0.0448 0.0275 0.710 14.912 5.877 529.296 1.685 26.142 5.036 0.31 189819. 0.2755 35.49 0.4805 0.7530 0.0408 0.0261 0.673 14.132 5.352 501.598 1.597 23.805 4.839 0.31 190213. 0.2527 37.36 0.5058 0.7595 0.0367 0.0245 0.632 13.269 4.815 470.967 1.499 21.419 4.638 0.31 190623. 0.2297 39.23 0.5311 0.7613 0.0326 0.0227 0.587 12.326 4.270 437.494 1.393 18.993 4.427 0.31 191050. 0.2065 41.09 0.5564 0.7571 0.0284 0.0208 0.538 11.306 3.718 401.287 1.277 16.538 4.203 0.31 191494. 0.1829 42.96 0.5816 0.7452 0.0241 0.0188 0.486 10.213 3.162 362.479 1.154 14.065 3.957 0.31 191954. 0.1588 44.83 0.6069 0.7226 0.0199 0.0167 0.431 9.051 2.604 321.237 1.023 11.583 3.677 0.32 192431. 0.1339 46.70 0.6322 0.6845 0.0156 0.0144 0.372 7.826 2.047 277.769 0.884 9.107 3.343 0.32 192925. 0.1080 48.57 0.6575 0.6214 0.0114 0.0121 0.312 6.546 1.495 232.330 0.740 6.650 2.919 0.32 193436. 0.0805 50.43 0.6828 0.5145 0.0072 0.0096 0.248 5.219 0.950 185.227 0.590 4.227 2.327 0.32 193963. 0.0512 52.30 0.7081 0.3167 0.0032 0.0071 0.183 3.855 0.417 136.818 0.436 1.853 1.381 0.32 194506. 0.0201 54.17 0.7334 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 0.0917 0.0300 1.833 28.883 21.361 1366.862 3.263 95.012 7.088 0.41 247219. 0.7393 2.47 0.0251 0.0744 0.0904 0.0305 1.867 29.415 21.069 1392.052 3.323 93.716 6.865 0.41 247384. 0.7111 4.95 0.0502 0.1441 0.0891 0.0310 1.899 29.927 20.750 1416.303 3.381 92.298 6.645 0.41 247565. 0.6832 7.42 0.0754 0.2092 0.0876 0.0315 1.930 30.410 20.402 1439.156 3.436 90.748 6.430 0.41 247761. 0.6554 9.89 0.1005 0.2698 0.0859 0.0320 1.958 30.854 20.022 1460.139 3.486 89.060 6.220 0.41 247975. 0.6281 12.37 0.1256 0.3261 0.0842 0.0324 1.983 31.247 19.610 1478.747 3.530 87.224 6.015 0.41 248206. 0.6011 14.84 0.1507 0.3784 0.0822 0.0328 2.004 31.578 19.162 1494.438 3.568 85.232 5.816 0.41 248455. 0.5745 17.32 0.1758 0.4268 0.0802 0.0330 2.020 31.837 18.678 1506.657 3.597 83.078 5.623 0.41 248723. 0.5484 19.79 0.2009 0.4716 0.0779 0.0332 2.031 32.009 18.155 1514.824 3.616 80.754 5.436 0.41 249010. 0.5227 22.26 0.2261 0.5129 0.0755 0.0333 2.036 32.084 17.593 1518.363 3.625 78.254 5.255 0.41 249318. 0.4975 24.74 0.2512 0.5510 0.0729 0.0332 2.034 32.049 16.990 1516.698 3.621 75.573 5.081 0.41 249645. 0.4726 27.21 0.2763 0.5860 0.0702 0.0331 2.024 31.892 16.346 1509.270 3.603 72.708 4.912 0.41 249993. 0.4482 29.68 0.3014 0.6181 0.0672 0.0328 2.006 31.601 15.660 1495.527 3.570 69.656 4.749 0.41 250362. 0.4242 32.16 0.3265 0.6473 0.0641 0.0323 1.978 31.165 14.931 1474.894 3.521 66.411 4.592 0.41 250752. 0.4004 34.63 0.3517 0.6739 0.0608 0.0317 1.940 30.572 14.157 1446.800 3.454 62.972 4.438 0.42 251164. 0.3769 37.11 0.3768 0.6977 0.0573 0.0309 1.892 29.815 13.343 1410.993 3.368 59.350 4.289 0.42 251597. 0.3536 39.58 0.4019 0.7189 0.0536 0.0300 1.834 28.896 12.492 1367.512 3.265 55.564 4.143 0.42 252052. 0.3305 42.05 0.4270 0.7373 0.0498 0.0289 1.765 27.818 11.608 1316.479 3.143 51.634 3.999 0.42 252528. 0.3075 44.53 0.4521 0.7528 0.0459 0.0276 1.687 26.583 10.696 1258.036 3.003 47.578 3.856 0.42 253026. 0.2846 47.00 0.4772 0.7650 0.0419 0.0261 1.599 25.195 9.760 1192.336 2.846 43.414 3.713 0.42 253546. 0.2618 49.47 0.5024 0.7736 0.0378 0.0245 1.501 23.657 8.804 1119.551 2.673 39.160 3.567 0.42 254087. 0.2388 51.95 0.5275 0.7779 0.0336 0.0228 1.395 21.973 7.831 1039.886 2.483 34.832 3.416 0.42 254650. 0.2157 54.42 0.5526 0.7768 0.0294 0.0209 1.279 20.150 6.845 953.590 2.277 30.448 3.256 0.42 255235. 0.1922 56.90 0.5777 0.7689 0.0251 0.0189 1.155 18.193 5.851 860.974 2.055 26.027 3.083 0.42 255841. 0.1683 59.37 0.6028 0.7515 0.0208 0.0167 1.022 16.110 4.854 762.423 1.820 21.589 2.887 0.42 256470. 0.1436 61.84 0.6279 0.7203 0.0166 0.0144 0.883 13.913 3.857 658.418 1.572 17.155 2.657 0.42 257121. 0.1178 64.32 0.6531 0.6671 0.0123 0.0120 0.737 11.612 2.867 549.551 1.312 12.751 2.366 0.42 257793. 0.0904 66.79 0.6782 0.5747 0.0081 0.0096 0.585 9.224 1.889 436.541 1.042 8.402 1.963 0.42 258487. 0.0609 69.26 0.7033 0.4001 0.0040 0.0070 0.429 6.767 0.930 320.237 0.765 4.138 1.318 0.42 259203. 0.0287 71.74 0.7284 -0.0048 0.0000 0.0044 0.270 4.249 -0.007 201.074 0.480 -0.030 -0.015 0.42 259924. 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 0.0928 0.0301 3.602 45.412 33.779 2686.381 5.131 150.249 5.703 0.52 308997. 0.7481 3.09 0.0251 0.0748 0.0915 0.0307 3.670 46.269 33.330 2737.086 5.227 148.252 5.523 0.52 309204. 0.7196 6.18 0.0502 0.1449 0.0902 0.0313 3.736 47.095 32.837 2785.945 5.321 146.059 5.346 0.52 309430. 0.6914 9.27 0.0753 0.2103 0.0887 0.0318 3.798 47.874 32.297 2832.023 5.409 143.657 5.173 0.52 309677. 0.6634 12.36 0.1004 0.2712 0.0871 0.0323 3.855 48.590 31.707 2874.371 5.490 141.033 5.003 0.52 309945. 0.6358 15.46 0.1255 0.3278 0.0853 0.0327 3.905 49.225 31.064 2911.965 5.561 138.173 4.839 0.52 310234. 0.6086 18.55 0.1507 0.3804 0.0834 0.0330 3.948 49.762 30.365 2943.730 5.622 135.064 4.679 0.52 310547. 0.5818 21.64 0.1758 0.4291 0.0813 0.0333 3.981 50.181 29.607 2968.530 5.669 131.693 4.524 0.52 310883. 0.5555 24.73 0.2009 0.4742 0.0791 0.0335 4.003 50.464 28.788 2985.218 5.701 128.049 4.374 0.52 311243. 0.5296 27.82 0.2260 0.5158 0.0766 0.0336 4.013 50.589 27.906 2992.621 5.715 124.124 4.229 0.52 311628. 0.5042 30.91 0.2511 0.5542 0.0740 0.0335 4.009 50.538 26.958 2989.592 5.710 119.908 4.090 0.52 312039. 0.4792 34.00 0.2762 0.5896 0.0713 0.0334 3.990 50.291 25.943 2975.002 5.682 115.396 3.955 0.52 312475. 0.4547 37.09 0.3013 0.6221 0.0683 0.0331 3.953 49.830 24.861 2947.756 5.630 110.582 3.825 0.52 312938. 0.4304 40.18 0.3264 0.6518 0.0651 0.0326 3.898 49.137 23.710 2906.715 5.551 105.460 3.700 0.52 313427. 0.4066 43.28 0.3515 0.6788 0.0618 0.0320 3.823 48.190 22.488 2850.727 5.444 100.025 3.578 0.52 313942. 0.3829 46.37 0.3766 0.7032 0.0582 0.0312 3.727 46.982 21.199 2779.236 5.308 94.293 3.460 0.52 314485. 0.3595 49.46 0.4017 0.7251 0.0545 0.0302 3.610 45.512 19.851 2692.299 5.142 88.296 3.344 0.52 315054. 0.3363 52.55 0.4269 0.7443 0.0507 0.0291 3.473 43.785 18.450 2590.156 4.947 82.065 3.231 0.52 315650. 0.3132 55.64 0.4520 0.7607 0.0467 0.0277 3.316 41.806 17.003 2473.093 4.723 75.631 3.118 0.52 316273. 0.2902 58.73 0.4771 0.7740 0.0426 0.0263 3.140 39.580 15.517 2341.418 4.472 69.021 3.006 0.52 316923. 0.2672 61.82 0.5022 0.7838 0.0384 0.0246 2.944 37.113 13.998 2195.478 4.193 62.263 2.892 0.52 317600. 0.2442 64.91 0.5273 0.7895 0.0342 0.0228 2.730 34.412 12.452 2035.684 3.888 55.385 2.774 0.52 318304. 0.2209 68.00 0.5524 0.7902 0.0299 0.0209 2.498 31.485 10.885 1862.535 3.557 48.415 2.651 0.52 319036. 0.1974 71.10 0.5775 0.7844 0.0256 0.0188 2.248 28.343 9.304 1676.657 3.202 41.383 2.517 0.52 319794. 0.1732 74.19 0.6026 0.7697 0.0212 0.0166 1.983 24.999 7.716 1478.826 2.824 34.321 2.367 0.53 320580. 0.1484 77.28 0.6277 0.7416 0.0168 0.0143 1.703 21.469 6.130 1270.013 2.426 27.265 2.189 0.53 321393. 0.1223 80.37 0.6528 0.6921 0.0125 0.0118 1.410 17.774 4.553 1051.415 2.008 20.254 1.964 0.53 322233. 0.0946 83.46 0.6779 0.6032 0.0082 0.0093 1.106 13.938 2.997 824.496 1.575 13.330 1.649 0.53 323101. 0.0644 86.55 0.7031 0.4282 0.0040 0.0066 0.793 9.990 1.470 590.982 1.129 6.540 1.128 0.53 323995. 0.0309 89.64 0.7282 -0.0115 -0.0001 0.0039 0.471 5.943 -0.023 351.578 0.671 -0.101 -0.029 0.53 324892. 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 0.0942 0.0306 6.319 66.383 49.390 4712.308 7.500 219.688 4.754 0.62 370754. 0.7540 3.73 0.0252 0.0753 0.0930 0.0312 6.442 67.671 48.754 4803.763 7.645 216.856 4.603 0.62 371005. 0.7254 7.46 0.0505 0.1457 0.0917 0.0318 6.560 68.913 48.051 4891.931 7.786 213.732 4.455 0.62 371279. 0.6970 11.19 0.0757 0.2114 0.0902 0.0323 6.672 70.085 47.279 4975.100 7.918 210.295 4.310 0.62 371578. 0.6689 14.92 0.1010 0.2726 0.0886 0.0328 6.774 71.161 46.431 5051.523 8.040 206.524 4.169 0.62 371903. 0.6411 18.65 0.1262 0.3296 0.0868 0.0332 6.865 72.116 45.503 5119.314 8.148 202.397 4.032 0.62 372255. 0.6137 22.38 0.1515 0.3824 0.0849 0.0336 6.942 72.922 44.491 5176.509 8.239 197.894 3.898 0.62 372635. 0.5868 26.10 0.1767 0.4314 0.0828 0.0339 7.002 73.549 43.389 5221.036 8.310 192.995 3.769 0.62 373043. 0.5603 29.83 0.2020 0.4767 0.0805 0.0341 7.041 73.968 42.195 5250.782 8.357 187.684 3.645 0.62 373481. 0.5343 33.56 0.2272 0.5186 0.0780 0.0342 7.059 74.149 40.905 5263.639 8.377 181.945 3.525 0.62 373949. 0.5088 37.29 0.2524 0.5573 0.0754 0.0341 7.050 74.063 39.516 5257.498 8.368 175.767 3.409 0.62 374448. 0.4836 41.02 0.2777 0.5930 0.0725 0.0340 7.014 73.680 38.026 5230.331 8.324 169.138 3.298 0.62 374979. 0.4589 44.75 0.3029 0.6258 0.0695 0.0336 6.947 72.973 36.433 5180.155 8.244 162.053 3.190 0.62 375541. 0.4345 48.48 0.3282 0.6559 0.0663 0.0331 6.846 71.914 34.735 5104.939 8.125 154.502 3.086 0.62 376135. 0.4105 52.21 0.3534 0.6834 0.0628 0.0325 6.709 70.472 32.931 5002.618 7.962 146.476 2.986 0.62 376762. 0.3867 55.94 0.3787 0.7083 0.0592 0.0316 6.534 68.635 31.026 4872.191 7.754 138.002 2.888 0.62 377421. 0.3631 59.67 0.4039 0.7307 0.0554 0.0306 6.321 66.403 29.030 4713.783 7.502 129.126 2.793 0.62 378112. 0.3397 63.40 0.4292 0.7505 0.0514 0.0294 6.072 63.784 26.955 4527.853 7.206 119.896 2.700 0.62 378836. 0.3164 67.13 0.4544 0.7675 0.0473 0.0280 5.786 60.785 24.811 4314.932 6.867 110.358 2.608 0.63 379593. 0.2932 70.86 0.4796 0.7815 0.0431 0.0265 5.465 57.413 22.607 4075.606 6.487 100.554 2.516 0.63 380382. 0.2700 74.59 0.5049 0.7921 0.0388 0.0247 5.110 53.679 20.352 3810.515 6.065 90.527 2.423 0.63 381204. 0.2466 78.31 0.5301 0.7987 0.0344 0.0229 4.721 49.593 18.057 3520.440 5.603 80.318 2.326 0.63 382058. 0.2231 82.04 0.5554 0.8004 0.0300 0.0208 4.300 45.168 15.731 3206.315 5.103 69.970 2.225 0.63 382945. 0.1992 85.77 0.5806 0.7955 0.0255 0.0186 3.848 40.420 13.383 2869.312 4.567 59.530 2.116 0.63 383865. 0.1747 89.50 0.6059 0.7815 0.0210 0.0163 3.367 35.371 11.027 2510.894 3.996 49.046 1.992 0.63 384818. 0.1493 93.23 0.6311 0.7538 0.0165 0.0138 2.860 30.046 8.672 2132.887 3.395 38.574 1.844 0.63 385804. 0.1226 96.96 0.6564 0.7028 0.0121 0.0113 2.330 24.477 6.334 1737.560 2.765 28.173 1.653 0.63 386823. 0.0939 100.69 0.6816 0.6072 0.0077 0.0086 1.780 18.703 4.027 1327.684 2.113 17.911 1.376 0.63 387875. 0.0623 104.42 0.7068 0.4047 0.0034 0.0059 1.216 12.770 1.767 906.506 1.443 7.859 0.884 0.63 388958. 0.0265 108.15 0.7321 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 0.0960 0.0315 10.329 93.004 68.518 7702.453 10.508 304.766 4.035 0.72 432482. 0.7537 4.35 0.0252 0.0745 0.0948 0.0321 10.524 94.755 67.683 7847.410 10.705 301.056 3.912 0.72 432775. 0.7263 8.69 0.0504 0.1444 0.0936 0.0327 10.712 96.450 66.757 7987.798 10.897 296.936 3.791 0.72 433096. 0.6990 13.04 0.0756 0.2098 0.0921 0.0332 10.890 98.056 65.732 8120.837 11.078 292.376 3.671 0.72 433446. 0.6717 17.38 0.1009 0.2708 0.0905 0.0337 11.055 99.539 64.600 8243.664 11.246 287.342 3.554 0.72 433827. 0.6447 21.73 0.1261 0.3277 0.0888 0.0342 11.202 100.862 63.355 8353.184 11.395 281.802 3.440 0.72 434239. 0.6179 26.07 0.1513 0.3805 0.0869 0.0345 11.326 101.983 61.989 8446.077 11.522 275.726 3.329 0.72 434683. 0.5915 30.42 0.1765 0.4295 0.0848 0.0348 11.424 102.862 60.496 8518.848 11.621 269.085 3.221 0.72 435162. 0.5654 34.76 0.2017 0.4750 0.0825 0.0350 11.490 103.454 58.870 8567.875 11.688 261.854 3.116 0.72 435674. 0.5396 39.11 0.2269 0.5170 0.0800 0.0351 11.519 103.715 57.107 8589.468 11.718 254.011 3.016 0.72 436223. 0.5143 43.45 0.2521 0.5559 0.0774 0.0351 11.506 103.600 55.202 8579.967 11.705 245.538 2.918 0.72 436807. 0.4893 47.80 0.2773 0.5919 0.0745 0.0349 11.447 103.067 53.152 8535.791 11.644 236.421 2.824 0.72 437428. 0.4647 52.15 0.3026 0.6250 0.0714 0.0346 11.336 102.074 50.955 8453.551 11.532 226.650 2.734 0.73 438086. 0.4404 56.49 0.3278 0.6555 0.0681 0.0341 11.171 100.581 48.609 8329.952 11.364 216.213 2.647 0.73 438782. 0.4165 60.84 0.3530 0.6834 0.0646 0.0334 10.945 98.548 46.110 8161.595 11.134 205.097 2.563 0.73 439514. 0.3927 65.18 0.3782 0.7089 0.0609 0.0325 10.657 95.953 43.465 7946.620 10.841 193.332 2.481 0.73 440285. 0.3691 69.53 0.4034 0.7320 0.0570 0.0314 10.306 92.795 40.689 7685.156 10.484 180.984 2.401 0.73 441093. 0.3457 73.87 0.4286 0.7525 0.0530 0.0302 9.894 89.086 37.797 7377.988 10.065 168.120 2.324 0.73 441939. 0.3224 78.22 0.4538 0.7704 0.0488 0.0287 9.422 84.837 34.804 7026.049 9.585 154.807 2.247 0.73 442823. 0.2991 82.56 0.4790 0.7855 0.0445 0.0271 8.891 80.059 31.723 6630.344 9.045 141.105 2.170 0.73 443744. 0.2758 86.91 0.5043 0.7973 0.0400 0.0253 8.304 74.766 28.568 6192.000 8.447 127.072 2.093 0.73 444704. 0.2524 91.25 0.5295 0.8053 0.0355 0.0234 7.660 68.975 25.353 5712.376 7.793 112.770 2.013 0.73 445700. 0.2287 95.60 0.5547 0.8086 0.0310 0.0212 6.964 62.706 22.090 5193.185 7.084 98.258 1.929 0.73 446735. 0.2046 99.94 0.5799 0.8056 0.0263 0.0190 6.218 55.985 18.795 4636.595 6.325 83.602 1.839 0.73 447808. 0.1799 104.29 0.6051 0.7937 0.0217 0.0165 5.425 48.846 15.484 4045.342 5.519 68.871 1.736 0.74 448918. 0.1542 108.64 0.6303 0.7682 0.0171 0.0140 4.590 41.331 12.172 3422.935 4.670 54.143 1.613 0.74 450067. 0.1270 112.98 0.6555 0.7193 0.0124 0.0113 3.720 33.492 8.881 2773.777 3.784 39.503 1.452 0.74 451254. 0.0977 117.33 0.6808 0.6246 0.0079 0.0086 2.821 25.397 5.631 2103.337 2.869 25.048 1.214 0.74 452479. 0.0650 121.67 0.7060 0.4172 0.0034 0.0058 1.902 17.123 2.446 1418.082 1.935 10.878 0.782 0.74 453740. 0.0276 126.02 0.7312 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 0.0982 0.0354 17.345 136.651 91.528 12933.919 15.439 407.117 3.210 0.83 494168. 0.6930 4.94 0.0251 0.0679 0.0971 0.0359 17.556 138.319 90.518 13091.826 15.627 402.625 3.136 0.83 494502. 0.6733 9.88 0.0502 0.1326 0.0959 0.0363 17.755 139.880 89.386 13239.603 15.804 397.589 3.062 0.83 494868. 0.6534 14.82 0.0752 0.1942 0.0945 0.0366 17.934 141.295 88.121 13373.520 15.963 391.961 2.989 0.83 495267. 0.6331 19.76 0.1003 0.2526 0.0930 0.0370 18.090 142.525 86.711 13489.880 16.102 385.691 2.915 0.83 495701. 0.6127 24.70 0.1254 0.3079 0.0914 0.0372 18.218 143.528 85.146 13584.826 16.216 378.731 2.843 0.83 496171. 0.5920 29.64 0.1505 0.3601 0.0895 0.0374 18.311 144.262 83.416 13654.353 16.299 371.033 2.771 0.83 496679. 0.5711 34.58 0.1756 0.4093 0.0875 0.0375 18.364 144.685 81.510 13694.343 16.346 362.555 2.700 0.83 497225. 0.5501 39.52 0.2007 0.4556 0.0852 0.0375 18.373 144.751 79.420 13700.555 16.354 353.260 2.629 0.83 497811. 0.5288 44.46 0.2257 0.4990 0.0828 0.0374 18.330 144.413 77.139 13668.607 16.316 343.113 2.560 0.83 498437. 0.5074 49.40 0.2508 0.5395 0.0801 0.0372 18.230 143.625 74.660 13594.027 16.227 332.089 2.491 0.83 499105. 0.4858 54.34 0.2759 0.5773 0.0772 0.0369 18.067 142.339 71.980 13472.317 16.081 320.167 2.423 0.83 499813. 0.4640 59.28 0.3010 0.6125 0.0741 0.0364 17.834 140.507 69.094 13298.947 15.874 307.332 2.357 0.83 500564. 0.4421 64.22 0.3261 0.6449 0.0708 0.0358 17.526 138.079 66.001 13069.116 15.600 293.572 2.291 0.83 501358. 0.4200 69.16 0.3511 0.6748 0.0673 0.0350 17.135 134.997 62.695 12777.437 15.252 278.867 2.226 0.83 502193. 0.3977 74.11 0.3762 0.7022 0.0635 0.0340 16.655 131.221 59.183 12419.956 14.825 263.245 2.161 0.83 503071. 0.3752 79.05 0.4013 0.7270 0.0595 0.0329 16.087 126.739 55.483 11995.797 14.319 246.789 2.098 0.83 503992. 0.3527 83.99 0.4264 0.7490 0.0554 0.0315 15.433 121.590 51.617 11508.447 13.737 229.592 2.034 0.83 504955. 0.3298 88.93 0.4515 0.7680 0.0511 0.0300 14.698 115.801 47.604 10960.465 13.083 211.744 1.970 0.83 505961. 0.3067 93.87 0.4766 0.7836 0.0466 0.0284 13.883 109.374 43.464 10352.186 12.357 193.329 1.904 0.83 507009. 0.2833 98.81 0.5016 0.7955 0.0421 0.0265 12.989 102.334 39.215 9685.883 11.562 174.429 1.836 0.84 508099. 0.2595 103.75 0.5267 0.8028 0.0374 0.0246 12.018 94.688 34.876 8962.191 10.698 155.127 1.765 0.84 509231. 0.2352 108.69 0.5518 0.8043 0.0327 0.0224 10.977 86.483 30.464 8185.607 9.771 135.505 1.688 0.84 510406. 0.2103 113.63 0.5769 0.7979 0.0279 0.0202 9.873 77.785 26.000 7362.324 8.788 115.648 1.602 0.84 511623. 0.1843 118.57 0.6020 0.7801 0.0231 0.0178 8.716 68.668 21.504 6499.392 7.758 95.649 1.501 0.84 512883. 0.1570 123.51 0.6270 0.7448 0.0182 0.0154 7.517 59.222 16.999 5605.312 6.691 75.613 1.376 0.84 514185. 0.1280 128.45 0.6521 0.6814 0.0134 0.0128 6.290 49.553 12.513 4690.138 5.598 55.656 1.210 0.84 515530. 0.0966 133.39 0.6772 0.5686 0.0087 0.0103 5.049 39.779 8.072 3765.042 4.494 35.904 0.972 0.84 516917. 0.0623 138.33 0.7023 0.3590 0.0040 0.0078 3.812 30.030 3.709 2842.322 3.393 16.499 0.592 0.85 518346. 0.0257 143.27 0.7274 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 0.0990 0.0449 31.319 219.332 116.770 23354.572 24.780 519.391 2.268 0.93 555891. 0.5530 5.59 0.0252 0.0546 0.0981 0.0453 31.580 221.158 115.730 23549.008 24.986 514.767 2.229 0.93 556260. 0.5412 11.17 0.0504 0.1073 0.0971 0.0456 31.799 222.695 114.539 23712.709 25.160 509.470 2.191 0.93 556666. 0.5292 16.76 0.0756 0.1582 0.0959 0.0459 31.966 223.864 113.180 23837.166 25.292 503.423 2.154 0.93 557111. 0.5170 22.34 0.1008 0.2074 0.0946 0.0460 32.069 224.586 111.632 23914.062 25.374 496.540 2.117 0.93 557596. 0.5049 27.93 0.1260 0.2549 0.0931 0.0461 32.098 224.787 109.878 23935.465 25.396 488.736 2.082 0.93 558123. 0.4926 33.51 0.1512 0.3009 0.0915 0.0460 32.043 224.399 107.898 23894.158 25.352 479.930 2.048 0.93 558695. 0.4801 39.10 0.1764 0.3454 0.0896 0.0458 31.895 223.364 105.676 23783.945 25.236 470.048 2.015 0.93 559312. 0.4675 44.68 0.2016 0.3885 0.0875 0.0454 31.648 221.636 103.197 23599.914 25.040 459.021 1.983 0.93 559975. 0.4547 50.27 0.2268 0.4302 0.0852 0.0449 31.297 219.179 100.448 23338.299 24.763 446.793 1.952 0.93 560685. 0.4415 55.85 0.2520 0.4705 0.0826 0.0442 30.839 215.968 97.418 22996.445 24.400 433.317 1.921 0.93 561444. 0.4280 61.44 0.2773 0.5093 0.0798 0.0434 30.270 211.986 94.101 22572.416 23.950 418.559 1.891 0.93 562251. 0.4139 67.02 0.3025 0.5465 0.0767 0.0425 29.589 207.219 90.490 22064.775 23.411 402.497 1.860 0.93 563106. 0.3993 72.61 0.3277 0.5822 0.0734 0.0413 28.794 201.651 86.581 21471.943 22.782 385.114 1.829 0.93 564011. 0.3841 78.19 0.3529 0.6160 0.0698 0.0400 27.881 195.257 82.371 20791.133 22.060 366.387 1.797 0.93 564964. 0.3681 83.78 0.3781 0.6479 0.0660 0.0385 26.848 188.022 77.865 20020.713 21.243 346.345 1.764 0.93 565966. 0.3513 89.36 0.4033 0.6777 0.0620 0.0369 25.698 179.969 73.089 19163.172 20.333 325.101 1.730 0.94 567017. 0.3338 94.95 0.4285 0.7053 0.0577 0.0351 24.437 171.136 68.074 18222.666 19.335 302.792 1.694 0.94 568116. 0.3155 100.53 0.4537 0.7298 0.0533 0.0331 23.085 161.666 62.846 17214.248 18.265 279.537 1.656 0.94 569262. 0.2963 106.12 0.4789 0.7488 0.0487 0.0311 21.702 151.980 57.429 16182.962 17.171 255.443 1.610 0.94 570457. 0.2753 111.70 0.5041 0.7612 0.0440 0.0291 20.289 142.088 51.852 15129.621 16.053 230.639 1.554 0.94 571699. 0.2526 117.29 0.5293 0.7609 0.0391 0.0272 18.962 132.791 46.130 14139.708 15.003 205.186 1.480 0.94 572989. 0.2268 122.87 0.5545 0.7478 0.0342 0.0253 17.658 123.663 40.300 13167.710 13.971 179.256 1.388 0.94 574326. 0.1989 128.46 0.5797 0.7221 0.0292 0.0234 16.318 114.280 34.403 12168.649 12.911 153.024 1.282 0.94 575711. 0.1697 134.04 0.6049 0.6801 0.0241 0.0215 14.963 104.787 28.472 11157.806 11.839 126.642 1.157 0.95 577144. 0.1394 139.63 0.6301 0.6165 0.0191 0.0195 13.616 95.352 22.546 10153.168 10.773 100.286 1.007 0.95 578624. 0.1079 145.21 0.6553 0.5251 0.0141 0.0176 12.294 86.097 16.672 9167.622 9.727 74.157 0.825 0.95 580152. 0.0760 150.80 0.6805 0.3979 0.0092 0.0158 11.017 77.151 10.900 8215.083 8.716 48.485 0.602 0.95 581729. 0.0448 156.38 0.7057 0.2249 0.0045 0.0141 9.798 68.615 5.284 7306.146 7.752 23.505 0.328 0.95 583355. 0.0170 161.97 0.7309 -0.0096 -0.0002 0.0123 8.598 60.213 -0.190 6411.512 6.803 -0.846 -0.013 0.95 585045. 0.0000