25x12.5E (25x125E.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 0.0831 0.0289 0.023 1.432 1.034 16.940 0.162 4.601 27.694 0.10 58210. 0.6610 0.53 0.0223 0.0622 0.0817 0.0292 0.023 1.447 1.017 17.118 0.163 4.523 26.942 0.10 58244. 0.6376 1.05 0.0445 0.1210 0.0802 0.0295 0.023 1.460 0.998 17.279 0.165 4.439 26.195 0.10 58281. 0.6142 1.58 0.0668 0.1764 0.0785 0.0297 0.023 1.473 0.978 17.422 0.166 4.349 25.456 0.10 58321. 0.5908 2.11 0.0890 0.2285 0.0768 0.0299 0.024 1.483 0.956 17.541 0.168 4.253 24.726 0.10 58364. 0.5675 2.64 0.1113 0.2773 0.0750 0.0301 0.024 1.490 0.933 17.634 0.168 4.151 24.006 0.10 58410. 0.5443 3.16 0.1336 0.3229 0.0730 0.0302 0.024 1.496 0.909 17.696 0.169 4.043 23.296 0.10 58459. 0.5213 3.69 0.1558 0.3655 0.0709 0.0302 0.024 1.498 0.883 17.722 0.169 3.927 22.596 0.10 58511. 0.4983 4.22 0.1781 0.4049 0.0687 0.0302 0.024 1.497 0.855 17.709 0.169 3.805 21.907 0.10 58566. 0.4755 4.74 0.2004 0.4414 0.0664 0.0301 0.024 1.492 0.826 17.654 0.169 3.675 21.228 0.10 58625. 0.4529 5.27 0.2226 0.4750 0.0639 0.0299 0.024 1.483 0.795 17.550 0.168 3.538 20.557 0.10 58688. 0.4303 5.80 0.2449 0.5056 0.0613 0.0297 0.023 1.470 0.763 17.395 0.166 3.394 19.894 0.10 58754. 0.4078 6.32 0.2671 0.5334 0.0585 0.0293 0.023 1.452 0.729 17.183 0.164 3.242 19.237 0.10 58824. 0.3854 6.85 0.2894 0.5582 0.0557 0.0289 0.023 1.429 0.693 16.912 0.161 3.082 18.584 0.10 58898. 0.3631 7.38 0.3117 0.5800 0.0527 0.0283 0.022 1.401 0.656 16.581 0.158 2.916 17.932 0.10 58975. 0.3408 7.91 0.3339 0.5988 0.0495 0.0276 0.022 1.369 0.617 16.191 0.155 2.743 17.277 0.10 59057. 0.3185 8.43 0.3562 0.6142 0.0463 0.0269 0.021 1.331 0.577 15.742 0.150 2.565 16.616 0.10 59142. 0.2961 8.96 0.3784 0.6262 0.0430 0.0260 0.020 1.288 0.535 15.234 0.145 2.382 15.942 0.10 59231. 0.2738 9.49 0.4007 0.6342 0.0396 0.0250 0.020 1.240 0.493 14.667 0.140 2.194 15.251 0.10 59324. 0.2514 10.01 0.4230 0.6380 0.0361 0.0240 0.019 1.187 0.450 14.042 0.134 2.001 14.534 0.10 59421. 0.2288 10.54 0.4452 0.6368 0.0326 0.0228 0.018 1.129 0.406 13.360 0.128 1.806 13.782 0.10 59522. 0.2061 11.07 0.4675 0.6299 0.0290 0.0215 0.017 1.067 0.361 12.622 0.121 1.607 12.982 0.10 59627. 0.1831 11.59 0.4898 0.6160 0.0254 0.0202 0.016 1.000 0.316 11.830 0.113 1.406 12.120 0.10 59736. 0.1599 12.12 0.5120 0.5937 0.0217 0.0187 0.015 0.928 0.271 10.985 0.105 1.203 11.171 0.10 59849. 0.1364 12.65 0.5343 0.5604 0.0181 0.0172 0.014 0.853 0.225 10.090 0.096 1.000 10.106 0.10 59966. 0.1125 13.18 0.5565 0.5128 0.0144 0.0156 0.012 0.773 0.179 9.148 0.087 0.797 8.879 0.10 60087. 0.0882 13.70 0.5788 0.4457 0.0107 0.0139 0.011 0.690 0.134 8.164 0.078 0.594 7.419 0.10 60212. 0.0636 14.23 0.6011 0.3504 0.0071 0.0122 0.010 0.604 0.088 7.142 0.068 0.393 5.616 0.10 60342. 0.0392 14.76 0.6233 0.2121 0.0035 0.0104 0.008 0.515 0.044 6.089 0.058 0.196 3.279 0.10 60475. 0.0161 15.28 0.6456 0.0025 0.0000 0.0085 0.007 0.423 0.000 5.007 0.048 0.002 0.037 0.10 60610. 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 0.0835 0.0271 0.171 5.375 4.158 127.179 0.607 18.497 14.831 0.20 116418. 0.7098 1.06 0.0224 0.0669 0.0821 0.0275 0.173 5.440 4.088 128.716 0.615 18.184 14.406 0.20 116487. 0.6836 2.12 0.0447 0.1298 0.0806 0.0278 0.175 5.499 4.012 130.128 0.621 17.847 13.986 0.20 116561. 0.6575 3.18 0.0671 0.1890 0.0790 0.0280 0.176 5.552 3.931 131.383 0.627 17.487 13.573 0.20 116641. 0.6316 4.23 0.0894 0.2444 0.0772 0.0283 0.178 5.598 3.845 132.451 0.632 17.102 13.167 0.20 116727. 0.6060 5.29 0.1118 0.2963 0.0754 0.0284 0.179 5.633 3.753 133.299 0.636 16.691 12.768 0.20 116819. 0.5805 6.35 0.1341 0.3447 0.0734 0.0286 0.180 5.658 3.654 133.892 0.639 16.253 12.378 0.20 116918. 0.5554 7.41 0.1565 0.3897 0.0713 0.0286 0.180 5.671 3.549 134.197 0.641 15.788 11.997 0.20 117023. 0.5305 8.47 0.1789 0.4315 0.0691 0.0286 0.180 5.671 3.438 134.178 0.641 15.294 11.623 0.20 117135. 0.5059 9.53 0.2012 0.4702 0.0667 0.0285 0.179 5.655 3.321 133.800 0.639 14.771 11.257 0.20 117254. 0.4815 10.59 0.2236 0.5058 0.0642 0.0284 0.178 5.622 3.197 133.027 0.635 14.219 10.899 0.20 117380. 0.4574 11.64 0.2459 0.5385 0.0616 0.0281 0.177 5.571 3.066 131.821 0.629 13.636 10.548 0.20 117514. 0.4335 12.70 0.2683 0.5682 0.0588 0.0278 0.175 5.500 2.928 130.142 0.621 13.022 10.203 0.20 117655. 0.4097 13.76 0.2906 0.5950 0.0559 0.0273 0.172 5.408 2.783 127.970 0.611 12.378 9.863 0.20 117803. 0.3862 14.82 0.3130 0.6190 0.0529 0.0267 0.168 5.295 2.632 125.296 0.598 11.707 9.527 0.20 117960. 0.3628 15.88 0.3354 0.6400 0.0497 0.0260 0.164 5.161 2.475 122.121 0.583 11.010 9.193 0.20 118124. 0.3395 16.94 0.3577 0.6578 0.0465 0.0253 0.159 5.006 2.313 118.442 0.566 10.290 8.859 0.20 118295. 0.3163 18.00 0.3801 0.6724 0.0431 0.0244 0.153 4.829 2.147 114.261 0.546 9.550 8.523 0.20 118475. 0.2931 19.05 0.4024 0.6834 0.0397 0.0234 0.147 4.631 1.976 109.579 0.523 8.791 8.181 0.20 118662. 0.2699 20.11 0.4248 0.6903 0.0362 0.0223 0.140 4.412 1.802 104.401 0.498 8.016 7.829 0.20 118858. 0.2467 21.17 0.4471 0.6928 0.0326 0.0211 0.132 4.173 1.625 98.733 0.471 7.227 7.464 0.20 119061. 0.2233 22.23 0.4695 0.6898 0.0290 0.0197 0.124 3.913 1.445 92.583 0.442 6.426 7.078 0.20 119273. 0.1997 23.29 0.4919 0.6802 0.0254 0.0183 0.115 3.633 1.263 85.965 0.410 5.617 6.663 0.20 119492. 0.1757 24.35 0.5142 0.6624 0.0217 0.0168 0.106 3.334 1.080 78.895 0.377 4.802 6.206 0.20 119720. 0.1513 25.41 0.5366 0.6337 0.0180 0.0152 0.096 3.017 0.896 71.395 0.341 3.984 5.690 0.20 119956. 0.1264 26.46 0.5589 0.5899 0.0143 0.0135 0.085 2.683 0.712 63.495 0.303 3.166 5.085 0.20 120200. 0.1007 27.52 0.5813 0.5242 0.0106 0.0118 0.074 2.334 0.529 55.231 0.264 2.353 4.345 0.20 120453. 0.0742 28.58 0.6036 0.4243 0.0070 0.0100 0.063 1.971 0.348 46.647 0.223 1.549 3.386 0.20 120714. 0.0469 29.64 0.6260 0.2657 0.0034 0.0081 0.051 1.597 0.170 37.794 0.180 0.758 2.045 0.20 120982. 0.0198 30.70 0.6483 -0.0095 -0.0001 0.0061 0.038 1.212 -0.004 28.678 0.137 -0.020 -0.070 0.20 121252. 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 0.0841 0.0265 0.563 11.819 9.422 419.498 1.335 41.908 10.187 0.30 174620. 0.7339 1.59 0.0224 0.0689 0.0827 0.0269 0.570 11.971 9.263 424.876 1.352 41.203 9.889 0.30 174723. 0.7064 3.18 0.0447 0.1336 0.0812 0.0272 0.576 12.110 9.093 429.829 1.368 40.445 9.595 0.30 174835. 0.6791 4.77 0.0671 0.1944 0.0795 0.0274 0.582 12.235 8.910 434.249 1.382 39.633 9.307 0.30 174956. 0.6520 6.35 0.0895 0.2514 0.0778 0.0277 0.587 12.341 8.715 438.026 1.394 38.764 9.024 0.30 175085. 0.6253 7.94 0.1118 0.3046 0.0759 0.0279 0.591 12.426 8.506 441.048 1.404 37.836 8.748 0.30 175224. 0.5988 9.53 0.1342 0.3542 0.0739 0.0280 0.594 12.487 8.284 443.197 1.411 36.847 8.478 0.30 175372. 0.5727 11.12 0.1566 0.4004 0.0718 0.0281 0.596 12.519 8.047 444.354 1.414 35.795 8.214 0.30 175530. 0.5469 12.71 0.1789 0.4433 0.0696 0.0281 0.596 12.521 7.796 444.397 1.415 34.679 7.957 0.30 175698. 0.5215 14.30 0.2013 0.4830 0.0672 0.0280 0.594 12.487 7.531 443.206 1.411 33.496 7.707 0.30 175878. 0.4964 15.88 0.2236 0.5196 0.0647 0.0279 0.591 12.415 7.250 440.654 1.403 32.246 7.462 0.30 176067. 0.4716 17.47 0.2460 0.5533 0.0621 0.0276 0.585 12.301 6.953 436.607 1.390 30.927 7.223 0.30 176268. 0.4470 19.06 0.2684 0.5840 0.0593 0.0272 0.578 12.141 6.640 430.931 1.372 29.537 6.989 0.30 176480. 0.4227 20.65 0.2907 0.6119 0.0563 0.0268 0.568 11.933 6.313 423.548 1.348 28.078 6.760 0.30 176703. 0.3986 22.24 0.3131 0.6370 0.0533 0.0262 0.556 11.676 5.971 414.429 1.319 26.557 6.535 0.30 176938. 0.3748 23.83 0.3355 0.6593 0.0501 0.0255 0.541 11.370 5.616 403.565 1.285 24.979 6.312 0.30 177185. 0.3510 25.41 0.3578 0.6785 0.0469 0.0247 0.524 11.015 5.249 390.951 1.244 23.348 6.090 0.30 177443. 0.3275 27.00 0.3802 0.6946 0.0435 0.0238 0.505 10.610 4.872 376.589 1.199 21.670 5.868 0.30 177712. 0.3040 28.59 0.4026 0.7073 0.0400 0.0228 0.483 10.156 4.485 360.482 1.147 19.950 5.643 0.30 177994. 0.2805 30.18 0.4249 0.7163 0.0365 0.0217 0.459 9.654 4.090 342.642 1.091 18.193 5.414 0.30 178287. 0.2570 31.77 0.4473 0.7210 0.0329 0.0204 0.433 9.103 3.688 323.089 1.028 16.404 5.177 0.30 178593. 0.2334 33.36 0.4697 0.7207 0.0293 0.0191 0.405 8.504 3.280 301.854 0.961 14.589 4.928 0.30 178911. 0.2095 34.94 0.4920 0.7142 0.0256 0.0176 0.374 7.860 2.868 278.980 0.888 12.755 4.662 0.30 179240. 0.1853 36.53 0.5144 0.6998 0.0219 0.0161 0.341 7.171 2.452 254.526 0.810 10.907 4.370 0.30 179582. 0.1606 38.12 0.5367 0.6750 0.0182 0.0144 0.307 6.440 2.035 228.570 0.728 9.053 4.039 0.30 179937. 0.1352 39.71 0.5591 0.6353 0.0144 0.0127 0.270 5.669 1.619 201.214 0.640 7.201 3.649 0.30 180304. 0.1090 41.30 0.5815 0.5733 0.0108 0.0109 0.231 4.862 1.205 172.584 0.549 5.359 3.166 0.30 180683. 0.0816 42.89 0.6038 0.4748 0.0071 0.0090 0.192 4.024 0.795 142.836 0.455 3.538 2.526 0.30 181074. 0.0529 44.47 0.6262 0.3096 0.0035 0.0071 0.150 3.160 0.393 112.149 0.357 1.746 1.588 0.30 181477. 0.0234 46.06 0.6486 -0.0039 0.0000 0.0051 0.108 2.269 -0.003 80.524 0.256 -0.015 -0.019 0.30 181880. 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 0.0849 0.0263 1.325 20.882 16.910 988.248 2.359 75.214 7.761 0.40 232813. 0.7490 2.12 0.0224 0.0699 0.0835 0.0267 1.343 21.159 16.628 1001.335 2.391 73.959 7.532 0.40 232951. 0.7208 4.23 0.0447 0.1356 0.0820 0.0270 1.359 21.414 16.324 1013.397 2.419 72.609 7.306 0.40 233101. 0.6928 6.35 0.0671 0.1973 0.0803 0.0273 1.373 21.641 15.999 1024.170 2.445 71.162 7.085 0.40 233262. 0.6651 8.47 0.0894 0.2550 0.0786 0.0276 1.386 21.836 15.650 1033.390 2.467 69.612 6.869 0.40 233435. 0.6378 10.59 0.1118 0.3090 0.0767 0.0278 1.396 21.992 15.278 1040.784 2.485 67.955 6.658 0.40 233620. 0.6108 12.70 0.1342 0.3593 0.0747 0.0279 1.403 22.104 14.880 1046.070 2.497 66.188 6.452 0.40 233819. 0.5842 14.82 0.1565 0.4062 0.0726 0.0280 1.407 22.165 14.458 1048.953 2.504 64.308 6.252 0.40 234030. 0.5579 16.94 0.1789 0.4497 0.0703 0.0280 1.407 22.169 14.009 1049.143 2.505 62.310 6.056 0.40 234256. 0.5320 19.06 0.2012 0.4901 0.0679 0.0279 1.403 22.110 13.533 1046.345 2.498 60.193 5.866 0.40 234495. 0.5065 21.17 0.2236 0.5273 0.0654 0.0277 1.395 21.981 13.029 1040.256 2.483 57.955 5.681 0.40 234749. 0.4813 23.29 0.2459 0.5616 0.0627 0.0275 1.382 21.776 12.498 1030.557 2.460 55.591 5.501 0.40 235017. 0.4564 25.41 0.2683 0.5931 0.0599 0.0271 1.364 21.488 11.938 1016.917 2.428 53.099 5.325 0.40 235300. 0.4318 27.53 0.2907 0.6217 0.0570 0.0266 1.340 21.112 11.350 999.135 2.385 50.484 5.152 0.40 235598. 0.4074 29.64 0.3130 0.6476 0.0539 0.0261 1.310 20.648 10.736 977.139 2.333 47.755 4.984 0.40 235912. 0.3833 31.76 0.3354 0.6707 0.0507 0.0254 1.275 20.093 10.099 950.903 2.270 44.922 4.817 0.40 236241. 0.3593 33.88 0.3577 0.6910 0.0474 0.0245 1.234 19.449 9.441 920.412 2.197 41.993 4.652 0.40 236585. 0.3355 35.99 0.3801 0.7082 0.0440 0.0236 1.188 18.715 8.763 885.667 2.114 38.980 4.488 0.40 236945. 0.3118 38.11 0.4025 0.7222 0.0405 0.0226 1.135 17.891 8.069 846.678 2.021 35.889 4.322 0.40 237321. 0.2882 40.23 0.4248 0.7326 0.0369 0.0214 1.077 16.978 7.359 803.470 1.918 32.732 4.154 0.40 237713. 0.2645 42.35 0.4472 0.7390 0.0333 0.0202 1.014 15.977 6.636 756.090 1.805 29.517 3.981 0.40 238120. 0.2407 44.46 0.4695 0.7407 0.0296 0.0188 0.945 14.889 5.903 704.612 1.682 26.256 3.800 0.40 238544. 0.2167 46.58 0.4919 0.7365 0.0259 0.0173 0.871 13.717 5.161 649.140 1.550 22.958 3.606 0.40 238984. 0.1923 48.70 0.5143 0.7248 0.0222 0.0157 0.791 12.463 4.414 589.818 1.408 19.636 3.395 0.40 239440. 0.1674 50.82 0.5366 0.7029 0.0184 0.0140 0.706 11.132 3.665 526.836 1.258 16.302 3.155 0.40 239913. 0.1418 52.93 0.5590 0.6667 0.0146 0.0123 0.617 9.729 2.916 460.441 1.099 12.972 2.873 0.40 240401. 0.1151 55.05 0.5813 0.6081 0.0109 0.0104 0.524 8.261 2.172 390.944 0.933 9.660 2.520 0.40 240907. 0.0872 57.17 0.6037 0.5120 0.0072 0.0085 0.427 6.735 1.435 318.725 0.761 6.385 2.043 0.40 241429. 0.0574 59.29 0.6261 0.3434 0.0036 0.0065 0.328 5.161 0.711 244.227 0.583 3.164 1.321 0.40 241966. 0.0262 61.40 0.6484 -0.0008 0.0000 0.0045 0.224 3.537 -0.001 167.401 0.400 -0.005 -0.003 0.41 242501. 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 0.0860 0.0265 2.601 32.783 26.754 1939.283 3.704 119.000 6.257 0.50 290993. 0.7596 2.65 0.0224 0.0705 0.0845 0.0268 2.636 33.226 26.312 1965.493 3.754 117.037 6.072 0.50 291167. 0.7310 5.29 0.0447 0.1367 0.0830 0.0272 2.668 33.634 25.837 1989.643 3.800 114.923 5.890 0.50 291355. 0.7027 7.94 0.0671 0.1988 0.0814 0.0275 2.697 33.998 25.326 2011.206 3.841 112.652 5.712 0.50 291557. 0.6746 10.59 0.0894 0.2570 0.0796 0.0277 2.722 34.310 24.779 2029.655 3.876 110.218 5.537 0.50 291774. 0.6470 13.23 0.1118 0.3114 0.0777 0.0279 2.742 34.560 24.194 2044.434 3.905 107.614 5.368 0.50 292007. 0.6197 15.88 0.1342 0.3622 0.0757 0.0281 2.756 34.738 23.569 2054.981 3.925 104.834 5.202 0.50 292256. 0.5927 18.53 0.1565 0.4094 0.0736 0.0281 2.763 34.835 22.903 2060.713 3.936 101.872 5.041 0.50 292522. 0.5662 21.17 0.1789 0.4534 0.0713 0.0281 2.764 34.841 22.195 2061.038 3.936 98.723 4.884 0.50 292805. 0.5401 23.82 0.2012 0.4942 0.0689 0.0281 2.756 34.745 21.444 2055.375 3.925 95.383 4.732 0.50 293105. 0.5143 26.47 0.2236 0.5319 0.0664 0.0279 2.740 34.538 20.649 2043.125 3.902 91.848 4.584 0.50 293424. 0.4889 29.11 0.2460 0.5667 0.0637 0.0276 2.714 34.209 19.810 2023.646 3.865 88.113 4.440 0.50 293760. 0.4638 31.76 0.2683 0.5987 0.0608 0.0273 2.677 33.746 18.924 1996.282 3.813 84.174 4.300 0.50 294115. 0.4390 34.41 0.2907 0.6279 0.0578 0.0268 2.629 33.143 17.994 1960.616 3.745 80.037 4.163 0.50 294489. 0.4144 37.06 0.3130 0.6545 0.0547 0.0262 2.570 32.397 17.023 1916.488 3.660 75.716 4.029 0.50 294882. 0.3901 39.70 0.3354 0.6783 0.0515 0.0254 2.499 31.507 16.013 1863.843 3.560 71.228 3.897 0.50 295295. 0.3660 42.35 0.3578 0.6993 0.0481 0.0246 2.417 30.473 14.970 1802.659 3.443 66.587 3.767 0.50 295726. 0.3421 45.00 0.3801 0.7174 0.0447 0.0237 2.324 29.294 13.896 1732.933 3.310 61.809 3.637 0.50 296177. 0.3182 47.64 0.4025 0.7325 0.0411 0.0226 2.219 27.972 12.794 1654.687 3.160 56.907 3.507 0.50 296648. 0.2944 50.29 0.4248 0.7441 0.0375 0.0214 2.103 26.506 11.668 1567.975 2.995 51.898 3.375 0.50 297138. 0.2706 52.94 0.4472 0.7519 0.0338 0.0201 1.975 24.898 10.521 1472.889 2.813 46.796 3.240 0.50 297648. 0.2466 55.58 0.4696 0.7551 0.0301 0.0187 1.837 23.152 9.357 1369.575 2.616 41.618 3.099 0.50 298179. 0.2225 58.23 0.4919 0.7527 0.0263 0.0172 1.687 21.270 8.179 1258.244 2.403 36.381 2.948 0.50 298729. 0.1979 60.88 0.5143 0.7431 0.0225 0.0156 1.528 19.257 6.993 1139.186 2.176 31.105 2.784 0.50 299300. 0.1728 63.52 0.5366 0.7237 0.0186 0.0138 1.358 17.121 5.803 1012.787 1.934 25.810 2.599 0.50 299891. 0.1469 66.17 0.5590 0.6901 0.0148 0.0120 1.179 14.868 4.613 879.543 1.680 20.519 2.379 0.50 300502. 0.1199 68.82 0.5814 0.6342 0.0110 0.0101 0.992 12.511 3.430 740.084 1.413 15.258 2.102 0.50 301134. 0.0914 71.46 0.6037 0.5396 0.0073 0.0081 0.798 10.061 2.260 595.184 1.137 10.054 1.723 0.50 301787. 0.0608 74.11 0.6261 0.3670 0.0036 0.0061 0.598 7.535 1.110 445.742 0.851 4.937 1.130 0.51 302459. 0.0279 76.76 0.6484 -0.0126 -0.0001 0.0040 0.391 4.925 -0.024 291.345 0.556 -0.107 -0.037 0.51 303120. 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 0.0874 0.0268 4.557 47.867 39.148 3397.911 5.408 174.130 5.226 0.59 349154. 0.7674 3.18 0.0224 0.0707 0.0859 0.0272 4.619 48.524 38.511 3444.594 5.482 171.297 5.071 0.60 349364. 0.7386 6.36 0.0448 0.1373 0.0844 0.0276 4.677 49.130 37.824 3487.560 5.551 168.239 4.919 0.60 349592. 0.7101 9.55 0.0672 0.1997 0.0827 0.0279 4.728 49.669 37.084 3525.854 5.612 164.950 4.771 0.60 349837. 0.6818 12.73 0.0896 0.2581 0.0810 0.0281 4.772 50.129 36.290 3558.539 5.664 161.417 4.625 0.60 350100. 0.6540 15.91 0.1120 0.3128 0.0791 0.0283 4.807 50.497 35.439 3584.622 5.705 157.631 4.484 0.60 350382. 0.6265 19.09 0.1344 0.3638 0.0770 0.0285 4.832 50.757 34.528 3603.082 5.734 153.582 4.347 0.60 350684. 0.5995 22.28 0.1568 0.4114 0.0749 0.0285 4.845 50.895 33.557 3612.882 5.750 149.262 4.213 0.60 351005. 0.5728 25.46 0.1792 0.4557 0.0726 0.0285 4.845 50.896 32.523 3612.977 5.750 144.663 4.083 0.60 351348. 0.5465 28.64 0.2016 0.4968 0.0701 0.0285 4.831 50.746 31.425 3602.312 5.733 139.779 3.957 0.60 351711. 0.5206 31.82 0.2240 0.5349 0.0675 0.0283 4.801 50.429 30.262 3579.831 5.697 134.605 3.834 0.60 352096. 0.4950 35.01 0.2464 0.5701 0.0648 0.0280 4.753 49.930 29.032 3544.413 5.641 129.133 3.715 0.60 352503. 0.4698 38.19 0.2689 0.6026 0.0619 0.0276 4.687 49.233 27.733 3494.891 5.562 123.356 3.599 0.60 352933. 0.4449 41.37 0.2913 0.6323 0.0588 0.0271 4.600 48.325 26.367 3430.479 5.460 117.282 3.486 0.60 353385. 0.4202 44.55 0.3137 0.6594 0.0557 0.0265 4.494 47.204 24.940 3350.897 5.333 110.934 3.376 0.60 353860. 0.3957 47.74 0.3361 0.6838 0.0523 0.0257 4.366 45.868 23.457 3256.057 5.182 104.335 3.268 0.60 354358. 0.3714 50.92 0.3585 0.7055 0.0489 0.0249 4.219 44.317 21.922 3145.924 5.007 97.507 3.161 0.60 354879. 0.3473 54.10 0.3809 0.7244 0.0454 0.0239 4.051 42.550 20.340 3020.503 4.807 90.473 3.054 0.60 355423. 0.3233 57.28 0.4033 0.7403 0.0418 0.0228 3.862 40.569 18.717 2879.840 4.583 83.255 2.948 0.60 355991. 0.2993 60.47 0.4257 0.7529 0.0381 0.0215 3.653 38.374 17.058 2724.042 4.335 75.875 2.840 0.60 356583. 0.2753 63.65 0.4481 0.7618 0.0343 0.0202 3.424 35.968 15.368 2553.276 4.064 68.356 2.730 0.60 357198. 0.2512 66.83 0.4705 0.7662 0.0305 0.0187 3.175 33.356 13.652 2367.819 3.768 60.723 2.615 0.60 357838. 0.2268 70.01 0.4929 0.7651 0.0266 0.0171 2.907 30.542 11.916 2168.053 3.451 53.001 2.493 0.60 358502. 0.2020 73.20 0.5153 0.7570 0.0227 0.0154 2.621 27.533 10.166 1954.510 3.111 45.219 2.359 0.60 359190. 0.1766 76.38 0.5377 0.7392 0.0188 0.0137 2.317 24.341 8.410 1727.892 2.750 37.409 2.208 0.60 359902. 0.1503 79.56 0.5601 0.7071 0.0149 0.0118 1.997 20.977 6.656 1489.112 2.370 29.604 2.027 0.60 360639. 0.1228 82.74 0.5825 0.6520 0.0110 0.0098 1.662 17.458 4.911 1239.320 1.972 21.844 1.797 0.61 361400. 0.0935 85.93 0.6049 0.5555 0.0071 0.0077 1.314 13.804 3.186 979.938 1.560 14.171 1.475 0.61 362186. 0.0618 89.11 0.6273 0.3706 0.0033 0.0056 0.956 10.038 1.490 712.603 1.134 6.629 0.949 0.61 362995. 0.0272 92.29 0.6497 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 0.0891 0.0275 7.407 66.689 54.378 5523.079 7.535 241.875 4.466 0.69 407289. 0.7729 3.69 0.0223 0.0702 0.0877 0.0279 7.509 67.609 53.519 5599.291 7.638 238.051 4.335 0.69 407535. 0.7444 7.39 0.0446 0.1363 0.0862 0.0282 7.603 68.457 52.588 5669.478 7.734 233.913 4.207 0.69 407801. 0.7161 11.08 0.0669 0.1983 0.0846 0.0285 7.687 69.212 51.585 5732.021 7.820 229.451 4.082 0.69 408088. 0.6881 14.77 0.0892 0.2565 0.0828 0.0288 7.758 69.856 50.506 5785.346 7.892 224.649 3.960 0.69 408395. 0.6605 18.47 0.1114 0.3110 0.0809 0.0290 7.815 70.369 49.346 5827.821 7.950 219.492 3.841 0.69 408725. 0.6332 22.16 0.1337 0.3619 0.0789 0.0291 7.855 70.731 48.104 5857.805 7.991 213.966 3.725 0.69 409077. 0.6063 25.86 0.1560 0.4094 0.0767 0.0292 7.877 70.922 46.776 5873.605 8.013 208.060 3.612 0.70 409452. 0.5798 29.55 0.1783 0.4538 0.0744 0.0292 7.877 70.921 45.361 5873.536 8.013 201.764 3.503 0.70 409851. 0.5537 33.24 0.2006 0.4950 0.0719 0.0291 7.853 70.708 43.855 5855.896 7.989 195.067 3.397 0.70 410275. 0.5280 36.94 0.2229 0.5334 0.0693 0.0290 7.803 70.262 42.258 5818.999 7.938 187.963 3.294 0.70 410723. 0.5026 40.63 0.2452 0.5689 0.0665 0.0287 7.726 69.563 40.567 5761.074 7.859 180.442 3.194 0.70 411197. 0.4774 44.32 0.2675 0.6017 0.0636 0.0283 7.617 68.587 38.780 5680.245 7.749 172.494 3.097 0.70 411697. 0.4526 48.02 0.2898 0.6319 0.0605 0.0277 7.476 67.318 36.899 5575.128 7.606 164.126 3.002 0.70 412223. 0.4280 51.71 0.3120 0.6596 0.0573 0.0271 7.302 65.749 34.929 5445.205 7.428 155.366 2.910 0.70 412775. 0.4036 55.41 0.3343 0.6847 0.0539 0.0263 7.094 63.879 32.880 5290.329 7.217 146.249 2.819 0.70 413353. 0.3794 59.10 0.3566 0.7072 0.0504 0.0254 6.853 61.707 30.757 5110.469 6.972 136.805 2.730 0.70 413959. 0.3553 62.79 0.3789 0.7271 0.0468 0.0244 6.579 59.234 28.567 4905.654 6.692 127.066 2.641 0.70 414590. 0.3313 66.49 0.4012 0.7441 0.0431 0.0233 6.271 56.461 26.318 4675.983 6.379 117.063 2.553 0.70 415250. 0.3074 70.18 0.4235 0.7580 0.0394 0.0220 5.929 53.390 24.017 4421.627 6.032 106.825 2.464 0.70 415936. 0.2834 73.87 0.4458 0.7683 0.0355 0.0206 5.556 50.024 21.670 4142.869 5.652 96.387 2.372 0.70 416649. 0.2592 77.57 0.4681 0.7746 0.0316 0.0191 5.150 46.368 19.285 3840.142 5.239 85.780 2.278 0.70 417390. 0.2348 81.26 0.4904 0.7757 0.0277 0.0175 4.712 42.431 16.871 3514.064 4.794 75.040 2.178 0.70 418158. 0.2099 84.96 0.5126 0.7703 0.0237 0.0157 4.245 38.222 14.435 3165.516 4.318 64.208 2.068 0.70 418955. 0.1844 88.65 0.5349 0.7559 0.0197 0.0139 3.749 33.757 11.989 2795.681 3.814 53.325 1.945 0.70 419779. 0.1581 92.34 0.5572 0.7281 0.0156 0.0120 3.227 29.053 9.541 2406.112 3.282 42.440 1.799 0.70 420632. 0.1304 96.04 0.5795 0.6789 0.0116 0.0099 2.680 24.135 7.106 1998.809 2.727 31.606 1.612 0.71 421512. 0.1009 99.73 0.6018 0.5906 0.0077 0.0078 2.114 19.033 4.694 1576.263 2.150 20.881 1.351 0.71 422421. 0.0687 103.42 0.6241 0.4184 0.0038 0.0057 1.531 13.782 2.322 1141.432 1.557 10.329 0.923 0.71 423357. 0.0330 107.12 0.6464 -0.0055 0.0000 0.0034 0.930 8.373 -0.018 693.411 0.946 -0.079 -0.012 0.71 424277. 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 0.0914 0.0293 11.775 92.769 72.855 8780.555 10.481 324.061 3.763 0.79 465385. 0.7539 4.21 0.0222 0.0677 0.0901 0.0296 11.892 93.690 71.750 8867.750 10.585 319.142 3.670 0.79 465668. 0.7296 8.42 0.0445 0.1320 0.0885 0.0298 11.998 94.524 70.548 8946.656 10.679 313.796 3.577 0.79 465975. 0.7051 12.63 0.0667 0.1929 0.0869 0.0300 12.090 95.248 69.246 9015.203 10.761 308.005 3.484 0.79 466304. 0.6804 16.84 0.0889 0.2505 0.0851 0.0302 12.165 95.841 67.839 9071.260 10.828 301.747 3.392 0.79 466658. 0.6557 21.05 0.1112 0.3047 0.0832 0.0304 12.220 96.278 66.322 9112.627 10.877 295.002 3.301 0.79 467037. 0.6310 25.27 0.1334 0.3557 0.0812 0.0305 12.253 96.534 64.692 9136.907 10.906 287.749 3.211 0.79 467442. 0.6062 29.48 0.1556 0.4036 0.0790 0.0305 12.259 96.584 62.944 9141.641 10.912 279.973 3.123 0.79 467874. 0.5815 33.69 0.1779 0.4484 0.0767 0.0304 12.236 96.401 61.074 9124.267 10.891 271.658 3.036 0.79 468332. 0.5569 37.90 0.2001 0.4902 0.0742 0.0303 12.179 95.956 59.081 9082.146 10.841 262.793 2.951 0.79 468819. 0.5323 42.11 0.2223 0.5292 0.0715 0.0300 12.086 95.221 56.962 9012.578 10.758 253.367 2.867 0.80 469334. 0.5078 46.32 0.2446 0.5654 0.0687 0.0297 11.952 94.165 54.714 8912.692 10.639 243.368 2.784 0.80 469878. 0.4834 50.53 0.2668 0.5989 0.0657 0.0293 11.773 92.756 52.334 8779.346 10.480 232.782 2.704 0.80 470451. 0.4591 54.74 0.2890 0.6299 0.0625 0.0287 11.546 90.967 49.823 8609.931 10.277 221.614 2.625 0.80 471054. 0.4348 58.95 0.3113 0.6583 0.0592 0.0280 11.269 88.782 47.190 8403.185 10.031 209.901 2.547 0.80 471687. 0.4107 63.16 0.3335 0.6841 0.0558 0.0272 10.942 86.204 44.444 8159.155 9.739 197.687 2.471 0.80 472349. 0.3866 67.37 0.3557 0.7074 0.0522 0.0263 10.564 83.229 41.596 7877.540 9.403 185.017 2.395 0.80 473042. 0.3625 71.58 0.3780 0.7280 0.0485 0.0252 10.136 79.854 38.654 7558.098 9.022 171.933 2.320 0.80 473765. 0.3385 75.80 0.4002 0.7457 0.0447 0.0240 9.657 76.083 35.629 7201.252 8.596 158.477 2.244 0.80 474518. 0.3144 80.01 0.4224 0.7602 0.0408 0.0227 9.129 71.924 32.530 6807.601 8.126 144.692 2.167 0.80 475302. 0.2901 84.22 0.4447 0.7710 0.0369 0.0213 8.553 67.387 29.366 6378.177 7.613 130.619 2.088 0.80 476117. 0.2656 88.43 0.4669 0.7774 0.0328 0.0197 7.931 62.487 26.147 5914.384 7.060 116.304 2.005 0.80 476962. 0.2407 92.64 0.4891 0.7781 0.0287 0.0181 7.266 57.244 22.885 5418.113 6.467 101.794 1.916 0.80 477839. 0.2151 96.85 0.5114 0.7713 0.0246 0.0163 6.560 51.682 19.591 4891.687 5.839 87.141 1.817 0.80 478747. 0.1887 101.06 0.5336 0.7540 0.0204 0.0145 5.818 45.834 16.277 4338.137 5.178 72.402 1.702 0.80 479687. 0.1612 105.27 0.5558 0.7212 0.0163 0.0125 5.044 39.739 12.959 3761.227 4.490 57.640 1.563 0.81 480658. 0.1320 109.48 0.5781 0.6637 0.0121 0.0106 4.245 33.445 9.651 3165.529 3.779 42.928 1.383 0.81 481661. 0.1008 113.69 0.6003 0.5636 0.0080 0.0085 3.428 27.008 6.373 2556.336 3.051 28.346 1.131 0.81 482696. 0.0670 117.90 0.6225 0.3798 0.0039 0.0065 2.601 20.492 3.142 1939.602 2.315 13.977 0.735 0.81 483761. 0.0306 122.11 0.6448 -0.0084 -0.0001 0.0044 1.762 13.885 -0.045 1314.186 1.569 -0.201 -0.016 0.81 484812. 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 0.0939 0.0360 20.598 144.253 94.703 15360.098 16.298 421.240 2.797 0.89 523441. 0.6387 4.81 0.0226 0.0581 0.0926 0.0360 20.613 144.355 93.354 15370.967 16.309 415.241 2.755 0.89 523766. 0.6247 9.62 0.0452 0.1144 0.0911 0.0360 20.600 144.263 91.872 15361.253 16.299 408.647 2.713 0.89 524119. 0.6103 14.43 0.0677 0.1689 0.0895 0.0359 20.557 143.964 90.251 15329.422 16.265 401.434 2.670 0.89 524499. 0.5954 19.24 0.0903 0.2217 0.0878 0.0358 20.482 143.439 88.482 15273.471 16.206 393.569 2.628 0.89 524908. 0.5801 24.05 0.1129 0.2725 0.0858 0.0356 20.372 142.667 86.560 15191.229 16.118 385.018 2.584 0.89 525346. 0.5644 28.86 0.1355 0.3215 0.0838 0.0353 20.223 141.628 84.477 15080.614 16.001 375.753 2.541 0.89 525816. 0.5481 33.67 0.1580 0.3685 0.0815 0.0350 20.034 140.301 82.227 14939.300 15.851 365.747 2.496 0.89 526316. 0.5313 38.48 0.1806 0.4136 0.0791 0.0346 19.800 138.664 79.806 14765.026 15.666 354.976 2.452 0.89 526850. 0.5140 43.29 0.2032 0.4566 0.0766 0.0341 19.519 136.696 77.208 14555.491 15.444 343.423 2.406 0.89 527415. 0.4962 48.10 0.2258 0.4976 0.0738 0.0335 19.188 134.375 74.432 14308.293 15.182 331.075 2.359 0.89 528014. 0.4778 52.91 0.2483 0.5364 0.0709 0.0328 18.802 131.674 71.474 14020.771 14.876 317.917 2.312 0.90 528647. 0.4588 57.73 0.2709 0.5729 0.0678 0.0320 18.358 128.565 68.330 13689.729 14.525 303.932 2.264 0.90 529314. 0.4392 62.54 0.2935 0.6072 0.0645 0.0312 17.852 125.022 65.002 13312.404 14.125 289.128 2.215 0.90 530016. 0.4191 67.35 0.3161 0.6390 0.0610 0.0302 17.283 121.036 61.502 12887.999 13.675 273.560 2.164 0.90 530752. 0.3984 72.16 0.3387 0.6684 0.0574 0.0291 16.651 116.607 57.845 12416.382 13.174 257.294 2.113 0.90 531522. 0.3772 76.97 0.3612 0.6946 0.0536 0.0279 15.968 111.823 54.044 11907.018 12.634 240.387 2.059 0.90 532327. 0.3552 81.78 0.3838 0.7166 0.0497 0.0266 15.249 106.788 50.111 11370.902 12.065 222.895 1.999 0.90 533167. 0.3321 86.59 0.4064 0.7335 0.0457 0.0253 14.499 101.537 46.060 10811.671 11.472 204.875 1.932 0.90 534042. 0.3078 91.40 0.4290 0.7436 0.0416 0.0240 13.733 96.172 41.902 10240.503 10.866 186.381 1.856 0.90 534952. 0.2820 96.21 0.4515 0.7467 0.0373 0.0226 12.936 90.593 37.654 9646.435 10.235 167.484 1.770 0.90 535898. 0.2550 101.02 0.4741 0.7424 0.0331 0.0211 12.094 84.696 33.333 9018.437 9.569 148.263 1.676 0.90 536879. 0.2272 105.83 0.4967 0.7286 0.0287 0.0196 11.214 78.536 28.955 8362.598 8.873 128.790 1.570 0.90 537896. 0.1983 110.64 0.5193 0.7023 0.0243 0.0180 10.308 72.191 24.538 7686.910 8.156 109.143 1.448 0.90 538948. 0.1683 115.45 0.5418 0.6594 0.0199 0.0164 9.384 65.719 20.102 6997.802 7.425 89.412 1.303 0.91 540037. 0.1371 120.26 0.5644 0.5944 0.0155 0.0148 8.453 59.198 15.669 6303.462 6.688 69.698 1.128 0.91 541162. 0.1048 125.07 0.5870 0.4992 0.0112 0.0131 7.527 52.710 11.267 5612.578 5.955 50.114 0.910 0.91 542323. 0.0717 129.88 0.6096 0.3623 0.0069 0.0115 6.617 46.337 6.922 4933.983 5.235 30.787 0.636 0.91 543521. 0.0393 134.69 0.6322 0.1668 0.0026 0.0100 5.732 40.141 2.663 4274.202 4.535 11.843 0.283 0.91 544753. 0.0108 139.50 0.6547