18x8 (18x8.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 0.0717 0.0282 0.004 0.270 0.240 3.199 0.031 1.066 33.990 0.07 25384. 0.5425 0.37 0.0218 0.0540 0.0704 0.0285 0.004 0.273 0.235 3.227 0.031 1.047 33.082 0.07 25397. 0.5232 0.74 0.0437 0.1050 0.0690 0.0287 0.004 0.275 0.231 3.253 0.031 1.026 32.174 0.07 25412. 0.5038 1.12 0.0655 0.1531 0.0675 0.0289 0.004 0.277 0.226 3.274 0.031 1.004 31.268 0.07 25428. 0.4843 1.49 0.0874 0.1983 0.0659 0.0290 0.004 0.278 0.220 3.291 0.031 0.980 30.366 0.07 25445. 0.4647 1.86 0.1092 0.2405 0.0642 0.0291 0.004 0.279 0.215 3.303 0.032 0.955 29.468 0.07 25463. 0.4450 2.23 0.1311 0.2799 0.0623 0.0292 0.004 0.280 0.208 3.309 0.032 0.927 28.575 0.07 25483. 0.4253 2.61 0.1529 0.3164 0.0604 0.0292 0.004 0.280 0.202 3.309 0.032 0.899 27.686 0.07 25504. 0.4056 2.98 0.1748 0.3500 0.0583 0.0291 0.004 0.279 0.195 3.303 0.032 0.868 26.801 0.07 25526. 0.3860 3.35 0.1966 0.3808 0.0562 0.0290 0.004 0.278 0.188 3.289 0.031 0.836 25.918 0.07 25550. 0.3663 3.72 0.2185 0.4087 0.0539 0.0288 0.004 0.276 0.180 3.268 0.031 0.802 25.037 0.07 25576. 0.3467 4.10 0.2403 0.4338 0.0516 0.0286 0.004 0.274 0.173 3.240 0.031 0.767 24.155 0.07 25602. 0.3271 4.47 0.2622 0.4559 0.0491 0.0283 0.004 0.271 0.164 3.203 0.031 0.731 23.271 0.07 25631. 0.3075 4.84 0.2840 0.4750 0.0466 0.0279 0.004 0.267 0.156 3.159 0.030 0.693 22.382 0.07 25661. 0.2880 5.21 0.3059 0.4910 0.0440 0.0274 0.004 0.262 0.147 3.106 0.030 0.654 21.484 0.07 25692. 0.2686 5.59 0.3277 0.5038 0.0413 0.0268 0.004 0.257 0.138 3.043 0.029 0.614 20.573 0.07 25725. 0.2492 5.96 0.3495 0.5131 0.0385 0.0262 0.004 0.251 0.129 2.972 0.028 0.573 19.645 0.07 25760. 0.2298 6.33 0.3714 0.5188 0.0356 0.0255 0.004 0.244 0.119 2.892 0.028 0.530 18.693 0.07 25797. 0.2104 6.70 0.3932 0.5204 0.0327 0.0247 0.004 0.237 0.109 2.802 0.027 0.487 17.710 0.07 25835. 0.1910 7.08 0.4151 0.5176 0.0297 0.0238 0.004 0.228 0.099 2.703 0.026 0.442 16.686 0.07 25875. 0.1715 7.45 0.4369 0.5096 0.0267 0.0229 0.003 0.219 0.089 2.594 0.025 0.397 15.609 0.07 25916. 0.1520 7.82 0.4588 0.4958 0.0236 0.0218 0.003 0.209 0.079 2.475 0.024 0.351 14.463 0.07 25959. 0.1324 8.19 0.4806 0.4751 0.0205 0.0207 0.003 0.198 0.068 2.346 0.022 0.304 13.229 0.07 26004. 0.1128 8.56 0.5025 0.4459 0.0173 0.0195 0.003 0.187 0.058 2.207 0.021 0.257 11.876 0.07 26051. 0.0931 8.94 0.5243 0.4063 0.0141 0.0182 0.003 0.174 0.047 2.059 0.020 0.209 10.369 0.07 26099. 0.0733 9.31 0.5462 0.3532 0.0108 0.0168 0.003 0.161 0.036 1.901 0.018 0.161 8.654 0.07 26150. 0.0537 9.68 0.5680 0.2823 0.0076 0.0153 0.002 0.146 0.025 1.733 0.017 0.113 6.651 0.07 26201. 0.0346 10.05 0.5899 0.1869 0.0044 0.0137 0.002 0.132 0.015 1.557 0.015 0.065 4.241 0.07 26255. 0.0167 10.43 0.6117 0.0560 0.0011 0.0121 0.002 0.116 0.004 1.371 0.013 0.016 1.225 0.07 26310. 0.0024 10.80 0.6335 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 0.0720 0.0247 0.030 0.946 0.964 22.380 0.107 4.286 19.530 0.14 50767. 0.6250 0.73 0.0215 0.0608 0.0708 0.0250 0.030 0.957 0.947 22.641 0.108 4.212 18.968 0.14 50794. 0.6017 1.46 0.0429 0.1181 0.0694 0.0252 0.031 0.967 0.929 22.877 0.109 4.131 18.412 0.14 50822. 0.5784 2.20 0.0644 0.1719 0.0679 0.0254 0.031 0.976 0.909 23.084 0.110 4.044 17.863 0.14 50854. 0.5552 2.93 0.0859 0.2223 0.0664 0.0256 0.031 0.983 0.888 23.255 0.111 3.950 17.322 0.14 50887. 0.5321 3.66 0.1073 0.2693 0.0647 0.0258 0.031 0.988 0.866 23.387 0.112 3.851 16.789 0.14 50923. 0.5092 4.39 0.1288 0.3131 0.0629 0.0259 0.031 0.992 0.842 23.476 0.112 3.744 16.265 0.14 50961. 0.4865 5.12 0.1502 0.3536 0.0610 0.0259 0.032 0.994 0.817 23.516 0.112 3.632 15.749 0.14 51002. 0.4639 5.85 0.1717 0.3911 0.0590 0.0259 0.032 0.993 0.790 23.505 0.112 3.513 15.242 0.14 51046. 0.4416 6.59 0.1932 0.4256 0.0569 0.0258 0.031 0.991 0.762 23.438 0.112 3.388 14.742 0.14 51092. 0.4194 7.32 0.2146 0.4571 0.0547 0.0257 0.031 0.985 0.732 23.313 0.111 3.258 14.249 0.14 51142. 0.3975 8.05 0.2361 0.4856 0.0524 0.0255 0.031 0.977 0.702 23.127 0.110 3.121 13.762 0.14 51194. 0.3758 8.78 0.2576 0.5112 0.0501 0.0252 0.031 0.967 0.670 22.877 0.109 2.979 13.280 0.14 51249. 0.3543 9.51 0.2790 0.5339 0.0476 0.0249 0.030 0.953 0.637 22.559 0.108 2.832 12.802 0.14 51307. 0.3330 10.24 0.3005 0.5535 0.0450 0.0244 0.030 0.937 0.603 22.172 0.106 2.680 12.326 0.14 51368. 0.3119 10.98 0.3220 0.5702 0.0424 0.0239 0.029 0.918 0.567 21.713 0.104 2.523 11.849 0.14 51433. 0.2909 11.71 0.3434 0.5836 0.0397 0.0233 0.028 0.895 0.531 21.180 0.101 2.362 11.371 0.14 51500. 0.2701 12.44 0.3649 0.5937 0.0369 0.0227 0.028 0.869 0.494 20.571 0.098 2.196 10.887 0.14 51571. 0.2494 13.17 0.3864 0.6002 0.0341 0.0219 0.027 0.840 0.456 19.884 0.095 2.027 10.394 0.14 51645. 0.2287 13.90 0.4078 0.6027 0.0311 0.0211 0.026 0.808 0.417 19.117 0.091 1.854 9.888 0.14 51722. 0.2081 14.63 0.4293 0.6006 0.0282 0.0201 0.024 0.772 0.377 18.269 0.087 1.677 9.362 0.14 51803. 0.1874 15.37 0.4507 0.5934 0.0252 0.0191 0.023 0.733 0.337 17.339 0.083 1.498 8.809 0.14 51886. 0.1666 16.10 0.4722 0.5800 0.0221 0.0180 0.022 0.690 0.296 16.327 0.078 1.316 8.218 0.14 51973. 0.1457 16.83 0.4937 0.5588 0.0190 0.0168 0.020 0.644 0.254 15.232 0.073 1.131 7.574 0.14 52064. 0.1245 17.56 0.5151 0.5279 0.0159 0.0155 0.019 0.594 0.212 14.054 0.067 0.945 6.857 0.14 52158. 0.1030 18.29 0.5366 0.4841 0.0127 0.0141 0.017 0.541 0.170 12.796 0.061 0.757 6.036 0.14 52255. 0.0812 19.02 0.5581 0.4222 0.0096 0.0126 0.015 0.484 0.128 11.458 0.055 0.569 5.062 0.15 52355. 0.0590 19.76 0.5795 0.3341 0.0064 0.0111 0.013 0.424 0.085 10.043 0.048 0.380 3.857 0.15 52459. 0.0367 20.49 0.6010 0.2047 0.0032 0.0094 0.011 0.362 0.043 8.555 0.041 0.191 2.279 0.15 52565. 0.0154 21.22 0.6225 0.0014 0.0000 0.0077 0.009 0.295 0.000 6.976 0.033 0.001 0.015 0.15 52670. 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 0.0724 0.0233 0.096 2.007 2.179 71.252 0.227 9.691 13.870 0.21 76149. 0.6674 1.10 0.0215 0.0649 0.0711 0.0236 0.097 2.034 2.141 72.188 0.230 9.523 13.452 0.21 76189. 0.6416 2.20 0.0431 0.1259 0.0697 0.0239 0.098 2.058 2.100 73.041 0.232 9.341 13.040 0.21 76233. 0.6160 3.30 0.0646 0.1830 0.0683 0.0241 0.099 2.079 2.056 73.793 0.235 9.144 12.636 0.21 76279. 0.5906 4.40 0.0861 0.2364 0.0667 0.0243 0.100 2.097 2.008 74.426 0.237 8.933 12.240 0.21 76330. 0.5654 5.51 0.1077 0.2861 0.0650 0.0245 0.100 2.111 1.958 74.923 0.238 8.708 11.852 0.21 76384. 0.5406 6.61 0.1292 0.3323 0.0632 0.0246 0.101 2.121 1.904 75.270 0.240 8.468 11.472 0.21 76442. 0.5160 7.71 0.1507 0.3751 0.0613 0.0246 0.101 2.126 1.847 75.451 0.240 8.214 11.101 0.21 76504. 0.4917 8.81 0.1723 0.4147 0.0593 0.0246 0.101 2.126 1.786 75.454 0.240 7.945 10.737 0.21 76570. 0.4678 9.91 0.1938 0.4510 0.0572 0.0246 0.101 2.121 1.723 75.266 0.240 7.662 10.381 0.21 76640. 0.4441 11.01 0.2153 0.4843 0.0550 0.0245 0.100 2.110 1.656 74.875 0.238 7.366 10.032 0.21 76714. 0.4208 12.11 0.2369 0.5145 0.0527 0.0243 0.100 2.092 1.587 74.269 0.236 7.057 9.689 0.21 76793. 0.3978 13.21 0.2584 0.5418 0.0503 0.0240 0.098 2.069 1.514 73.440 0.234 6.736 9.352 0.21 76876. 0.3752 14.32 0.2799 0.5661 0.0478 0.0236 0.097 2.039 1.439 72.377 0.230 6.402 9.020 0.22 76964. 0.3528 15.42 0.3015 0.5874 0.0452 0.0232 0.095 2.002 1.362 71.070 0.226 6.057 8.691 0.22 77057. 0.3306 16.52 0.3230 0.6057 0.0426 0.0227 0.093 1.958 1.282 69.511 0.221 5.702 8.364 0.22 77154. 0.3087 17.62 0.3446 0.6209 0.0398 0.0221 0.091 1.907 1.200 67.693 0.215 5.336 8.038 0.22 77256. 0.2870 18.72 0.3661 0.6328 0.0370 0.0214 0.088 1.848 1.115 65.606 0.209 4.961 7.711 0.22 77362. 0.2655 19.82 0.3876 0.6413 0.0342 0.0207 0.085 1.782 1.029 63.246 0.201 4.577 7.380 0.22 77474. 0.2440 20.92 0.4092 0.6459 0.0312 0.0198 0.081 1.707 0.941 60.605 0.193 4.185 7.041 0.22 77590. 0.2226 22.02 0.4307 0.6461 0.0283 0.0188 0.077 1.625 0.851 57.680 0.184 3.785 6.692 0.22 77712. 0.2012 23.13 0.4522 0.6413 0.0252 0.0178 0.073 1.535 0.760 54.466 0.173 3.379 6.326 0.22 77838. 0.1797 24.23 0.4738 0.6304 0.0222 0.0166 0.068 1.436 0.667 50.961 0.162 2.966 5.936 0.22 77970. 0.1580 25.33 0.4953 0.6119 0.0190 0.0154 0.063 1.329 0.573 47.166 0.150 2.549 5.511 0.22 78106. 0.1360 26.43 0.5168 0.5834 0.0159 0.0141 0.058 1.214 0.478 43.081 0.137 2.127 5.035 0.22 78248. 0.1135 27.53 0.5384 0.5413 0.0127 0.0126 0.052 1.091 0.383 38.711 0.123 1.703 4.485 0.22 78394. 0.0905 28.63 0.5599 0.4795 0.0095 0.0111 0.046 0.960 0.287 34.062 0.108 1.276 3.820 0.22 78546. 0.0667 29.73 0.5814 0.3872 0.0063 0.0095 0.039 0.821 0.191 29.145 0.093 0.849 2.970 0.22 78702. 0.0423 30.83 0.6030 0.2429 0.0032 0.0078 0.032 0.675 0.095 23.968 0.076 0.422 1.797 0.22 78863. 0.0180 31.93 0.6245 -0.0082 -0.0001 0.0060 0.025 0.519 -0.002 18.429 0.059 -0.011 -0.059 0.22 79016. 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 0.0728 0.0226 0.220 3.460 3.897 163.726 0.391 17.332 10.794 0.29 101530. 0.6946 1.49 0.0218 0.0681 0.0715 0.0229 0.223 3.509 3.828 166.054 0.396 17.029 10.457 0.29 101584. 0.6670 2.97 0.0436 0.1319 0.0701 0.0232 0.226 3.554 3.755 168.181 0.402 16.701 10.126 0.29 101642. 0.6396 4.46 0.0653 0.1915 0.0687 0.0234 0.228 3.593 3.675 170.059 0.406 16.347 9.802 0.29 101706. 0.6126 5.94 0.0871 0.2470 0.0671 0.0237 0.230 3.627 3.590 171.644 0.410 15.967 9.486 0.29 101774. 0.5859 7.43 0.1089 0.2987 0.0654 0.0238 0.232 3.653 3.498 172.896 0.413 15.560 9.177 0.29 101847. 0.5595 8.91 0.1307 0.3467 0.0635 0.0239 0.233 3.672 3.401 173.776 0.415 15.126 8.876 0.29 101926. 0.5335 10.40 0.1525 0.3911 0.0616 0.0240 0.234 3.682 3.297 174.246 0.416 14.665 8.582 0.29 102010. 0.5080 11.88 0.1743 0.4321 0.0596 0.0240 0.234 3.682 3.188 174.273 0.416 14.178 8.296 0.29 102099. 0.4828 13.37 0.1960 0.4698 0.0574 0.0240 0.233 3.673 3.072 173.826 0.415 13.666 8.017 0.29 102195. 0.4581 14.85 0.2178 0.5042 0.0551 0.0238 0.232 3.653 2.952 172.875 0.413 13.129 7.744 0.29 102296. 0.4337 16.34 0.2396 0.5355 0.0528 0.0236 0.230 3.622 2.826 171.393 0.409 12.568 7.478 0.29 102403. 0.4097 17.82 0.2614 0.5638 0.0503 0.0233 0.227 3.579 2.694 169.354 0.404 11.985 7.216 0.29 102516. 0.3861 19.31 0.2832 0.5891 0.0478 0.0230 0.224 3.523 2.558 166.732 0.398 11.380 6.960 0.29 102636. 0.3629 20.79 0.3049 0.6113 0.0452 0.0225 0.219 3.455 2.418 163.505 0.390 10.754 6.707 0.29 102761. 0.3399 22.28 0.3267 0.6305 0.0425 0.0220 0.214 3.374 2.273 159.650 0.381 10.108 6.456 0.29 102894. 0.3173 23.76 0.3485 0.6467 0.0397 0.0214 0.208 3.278 2.123 155.148 0.370 9.445 6.208 0.29 103032. 0.2949 25.25 0.3703 0.6595 0.0368 0.0207 0.201 3.169 1.970 149.979 0.358 8.764 5.959 0.29 103178. 0.2726 26.73 0.3921 0.6689 0.0339 0.0199 0.193 3.046 1.814 144.128 0.344 8.067 5.707 0.29 103329. 0.2506 28.22 0.4139 0.6744 0.0309 0.0190 0.184 2.907 1.654 137.579 0.328 7.355 5.452 0.29 103488. 0.2285 29.70 0.4356 0.6756 0.0278 0.0180 0.175 2.754 1.491 130.321 0.311 6.630 5.188 0.29 103653. 0.2065 31.19 0.4574 0.6716 0.0248 0.0169 0.164 2.585 1.325 122.346 0.292 5.893 4.912 0.29 103826. 0.1843 32.67 0.4792 0.6613 0.0216 0.0157 0.152 2.401 1.157 113.649 0.271 5.146 4.617 0.29 104005. 0.1619 34.16 0.5010 0.6430 0.0184 0.0144 0.140 2.202 0.987 104.230 0.249 4.389 4.294 0.29 104190. 0.1390 35.64 0.5228 0.6139 0.0152 0.0130 0.126 1.988 0.815 94.095 0.225 3.625 3.929 0.29 104383. 0.1156 37.13 0.5445 0.5695 0.0120 0.0115 0.112 1.759 0.642 83.255 0.199 2.857 3.499 0.29 104583. 0.0914 38.61 0.5663 0.5018 0.0088 0.0099 0.096 1.516 0.469 71.731 0.171 2.085 2.964 0.29 104789. 0.0662 40.10 0.5881 0.3954 0.0055 0.0082 0.080 1.258 0.295 59.547 0.142 1.314 2.249 0.29 105002. 0.0398 41.58 0.6099 0.2161 0.0023 0.0064 0.063 0.987 0.122 46.715 0.112 0.543 1.185 0.29 105220. 0.0135 43.07 0.6317 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 0.0733 0.0222 0.422 5.317 6.133 314.508 0.601 27.280 8.845 0.36 126907. 0.7140 1.84 0.0216 0.0692 0.0721 0.0225 0.428 5.395 6.028 319.159 0.610 26.812 8.566 0.36 126975. 0.6856 3.68 0.0432 0.1340 0.0707 0.0228 0.434 5.467 5.914 323.420 0.618 26.304 8.293 0.36 127047. 0.6574 5.53 0.0648 0.1945 0.0692 0.0231 0.439 5.531 5.790 327.199 0.625 25.756 8.027 0.36 127126. 0.6296 7.37 0.0865 0.2509 0.0677 0.0233 0.443 5.585 5.658 330.410 0.631 25.167 7.767 0.36 127211. 0.6022 9.21 0.1081 0.3034 0.0660 0.0235 0.447 5.629 5.516 332.971 0.636 24.535 7.514 0.36 127302. 0.5753 11.05 0.1297 0.3522 0.0641 0.0236 0.449 5.660 5.365 334.806 0.639 23.862 7.268 0.36 127399. 0.5487 12.90 0.1513 0.3973 0.0622 0.0237 0.450 5.677 5.204 335.845 0.641 23.147 7.028 0.36 127503. 0.5226 14.74 0.1729 0.4390 0.0602 0.0237 0.451 5.680 5.034 336.020 0.642 22.392 6.795 0.36 127614. 0.4970 16.58 0.1945 0.4774 0.0581 0.0237 0.450 5.668 4.855 335.270 0.640 21.596 6.568 0.36 127732. 0.4718 18.42 0.2161 0.5126 0.0558 0.0235 0.447 5.638 4.668 333.538 0.637 20.762 6.348 0.36 127857. 0.4471 20.26 0.2378 0.5448 0.0535 0.0233 0.444 5.591 4.472 330.769 0.632 19.891 6.132 0.36 127990. 0.4227 22.11 0.2594 0.5739 0.0510 0.0231 0.438 5.526 4.268 326.912 0.624 18.984 5.922 0.36 128130. 0.3988 23.95 0.2810 0.6001 0.0485 0.0227 0.432 5.442 4.057 321.919 0.615 18.043 5.715 0.36 128278. 0.3753 25.79 0.3026 0.6233 0.0459 0.0223 0.423 5.338 3.838 315.745 0.603 17.070 5.513 0.36 128433. 0.3521 27.63 0.3242 0.6436 0.0432 0.0218 0.413 5.212 3.612 308.346 0.589 16.067 5.313 0.36 128596. 0.3292 29.47 0.3458 0.6610 0.0404 0.0211 0.402 5.066 3.380 299.683 0.572 15.034 5.116 0.36 128767. 0.3066 31.32 0.3674 0.6753 0.0376 0.0204 0.389 4.898 3.142 289.718 0.553 13.974 4.919 0.36 128947. 0.2842 33.16 0.3891 0.6863 0.0346 0.0196 0.373 4.707 2.898 278.421 0.532 12.890 4.721 0.36 129134. 0.2620 35.00 0.4107 0.6937 0.0317 0.0188 0.356 4.493 2.649 265.760 0.508 11.782 4.521 0.36 129330. 0.2398 36.84 0.4323 0.6970 0.0286 0.0178 0.338 4.255 2.395 251.712 0.481 10.652 4.315 0.36 129534. 0.2177 38.69 0.4539 0.6957 0.0255 0.0167 0.317 3.994 2.137 236.261 0.451 9.504 4.102 0.36 129746. 0.1955 40.53 0.4755 0.6886 0.0224 0.0155 0.294 3.709 1.875 219.395 0.419 8.339 3.876 0.36 129967. 0.1730 42.37 0.4971 0.6743 0.0192 0.0142 0.270 3.400 1.610 201.112 0.384 7.159 3.630 0.36 130196. 0.1501 44.21 0.5188 0.6502 0.0160 0.0128 0.243 3.067 1.342 181.421 0.346 5.968 3.355 0.36 130434. 0.1267 46.05 0.5404 0.6123 0.0128 0.0113 0.215 2.711 1.072 160.344 0.306 4.769 3.033 0.36 130680. 0.1024 47.90 0.5620 0.5533 0.0096 0.0097 0.185 2.331 0.801 137.915 0.263 3.564 2.635 0.36 130934. 0.0769 49.74 0.5836 0.4592 0.0063 0.0081 0.153 1.930 0.530 114.182 0.218 2.358 2.106 0.36 131197. 0.0500 51.58 0.6052 0.2983 0.0031 0.0063 0.120 1.508 0.259 89.186 0.170 1.154 1.319 0.36 131466. 0.0219 53.42 0.6268 -0.0408 -0.0003 0.0043 0.083 1.041 -0.024 61.570 0.118 -0.105 -0.174 0.36 131683. 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 0.0740 0.0220 0.724 7.601 8.911 539.608 0.859 39.635 7.490 0.43 152282. 0.7288 2.21 0.0216 0.0703 0.0727 0.0224 0.735 7.718 8.760 547.879 0.872 38.962 7.252 0.43 152363. 0.6996 4.42 0.0433 0.1361 0.0714 0.0227 0.745 7.825 8.595 555.467 0.884 38.232 7.019 0.43 152450. 0.6708 6.64 0.0649 0.1975 0.0699 0.0230 0.754 7.920 8.418 562.207 0.895 37.442 6.791 0.43 152545. 0.6423 8.85 0.0865 0.2548 0.0683 0.0232 0.762 8.001 8.227 567.944 0.904 36.592 6.570 0.43 152647. 0.6143 11.06 0.1081 0.3081 0.0666 0.0234 0.768 8.065 8.022 572.536 0.911 35.680 6.355 0.43 152757. 0.5867 13.27 0.1298 0.3576 0.0648 0.0235 0.772 8.112 7.803 575.846 0.916 34.706 6.146 0.43 152874. 0.5596 15.48 0.1514 0.4034 0.0629 0.0236 0.775 8.139 7.570 577.749 0.920 33.672 5.943 0.43 152999. 0.5330 17.69 0.1730 0.4457 0.0608 0.0236 0.775 8.144 7.324 578.127 0.920 32.577 5.746 0.43 153133. 0.5069 19.91 0.1946 0.4847 0.0587 0.0236 0.774 8.126 7.065 576.872 0.918 31.424 5.555 0.43 153275. 0.4813 22.12 0.2163 0.5206 0.0564 0.0234 0.770 8.084 6.793 573.882 0.913 30.214 5.369 0.43 153426. 0.4561 24.33 0.2379 0.5533 0.0540 0.0232 0.763 8.016 6.508 569.063 0.906 28.950 5.188 0.43 153585. 0.4314 26.54 0.2595 0.5831 0.0516 0.0230 0.754 7.922 6.212 562.326 0.895 27.633 5.011 0.43 153754. 0.4071 28.75 0.2811 0.6099 0.0490 0.0226 0.742 7.798 5.905 553.586 0.881 26.266 4.838 0.43 153931. 0.3833 30.96 0.3028 0.6338 0.0464 0.0222 0.728 7.646 5.587 542.762 0.864 24.853 4.669 0.43 154118. 0.3598 33.18 0.3244 0.6549 0.0437 0.0216 0.710 7.463 5.259 529.782 0.843 23.394 4.503 0.43 154315. 0.3366 35.39 0.3460 0.6731 0.0409 0.0210 0.690 7.249 4.922 514.573 0.819 21.893 4.338 0.43 154521. 0.3138 37.60 0.3676 0.6882 0.0380 0.0203 0.667 7.002 4.576 497.074 0.791 20.353 4.175 0.43 154736. 0.2911 39.81 0.3893 0.7002 0.0350 0.0195 0.640 6.723 4.221 477.224 0.760 18.775 4.012 0.43 154962. 0.2687 42.02 0.4109 0.7087 0.0320 0.0186 0.610 6.409 3.859 454.974 0.724 17.164 3.847 0.43 155197. 0.2463 44.24 0.4325 0.7133 0.0290 0.0176 0.577 6.061 3.490 430.281 0.685 15.521 3.678 0.43 155442. 0.2240 46.45 0.4542 0.7134 0.0259 0.0165 0.541 5.679 3.114 403.115 0.642 13.851 3.504 0.43 155697. 0.2015 48.66 0.4758 0.7080 0.0227 0.0152 0.501 5.261 2.733 373.457 0.594 12.156 3.319 0.43 155963. 0.1789 50.87 0.4974 0.6956 0.0195 0.0139 0.458 4.808 2.347 341.303 0.543 10.439 3.119 0.43 156238. 0.1558 53.08 0.5190 0.6736 0.0163 0.0125 0.411 4.320 1.957 306.669 0.488 8.706 2.895 0.43 156524. 0.1320 55.29 0.5407 0.6381 0.0130 0.0110 0.362 3.798 1.565 269.592 0.429 6.959 2.632 0.43 156819. 0.1073 57.51 0.5623 0.5815 0.0097 0.0094 0.309 3.242 1.170 230.135 0.366 5.206 2.307 0.44 157125. 0.0813 59.72 0.5839 0.4890 0.0064 0.0077 0.253 2.654 0.776 188.382 0.300 3.450 1.868 0.44 157441. 0.0536 61.93 0.6055 0.3254 0.0032 0.0059 0.194 2.034 0.382 144.403 0.230 1.697 1.199 0.44 157764. 0.0241 64.14 0.6272 -0.0624 -0.0004 0.0038 0.126 1.322 -0.046 93.840 0.149 -0.204 -0.222 0.44 157942. 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 0.0748 0.0220 1.149 10.347 12.259 856.956 1.169 54.529 6.489 0.50 177652. 0.7406 2.58 0.0216 0.0710 0.0735 0.0224 1.167 10.511 12.054 870.478 1.187 53.618 6.281 0.50 177746. 0.7109 5.16 0.0432 0.1374 0.0722 0.0227 1.184 10.661 11.831 882.892 1.204 52.626 6.078 0.50 177849. 0.6815 7.74 0.0648 0.1994 0.0707 0.0230 1.199 10.794 11.590 893.930 1.219 51.553 5.881 0.50 177960. 0.6526 10.31 0.0864 0.2572 0.0691 0.0232 1.211 10.908 11.330 903.345 1.232 50.395 5.689 0.50 178079. 0.6242 12.89 0.1081 0.3110 0.0674 0.0234 1.222 10.999 11.050 910.898 1.243 49.152 5.502 0.50 178207. 0.5962 15.47 0.1297 0.3609 0.0656 0.0236 1.229 11.065 10.751 916.368 1.250 47.822 5.322 0.50 178345. 0.5688 18.05 0.1513 0.4072 0.0636 0.0236 1.233 11.103 10.433 919.551 1.254 46.408 5.146 0.50 178491. 0.5419 20.63 0.1729 0.4500 0.0616 0.0237 1.234 11.112 10.097 920.257 1.255 44.910 4.976 0.50 178647. 0.5155 23.21 0.1945 0.4895 0.0594 0.0236 1.231 11.088 9.742 918.312 1.253 43.330 4.812 0.50 178814. 0.4895 25.79 0.2161 0.5258 0.0572 0.0235 1.225 11.031 9.369 913.553 1.246 41.672 4.651 0.50 178990. 0.4641 28.36 0.2377 0.5591 0.0548 0.0233 1.215 10.938 8.979 905.830 1.236 39.938 4.496 0.50 179176. 0.4392 30.94 0.2593 0.5893 0.0523 0.0230 1.200 10.807 8.573 894.998 1.221 38.131 4.344 0.50 179373. 0.4147 33.52 0.2809 0.6167 0.0497 0.0227 1.181 10.637 8.151 880.925 1.202 36.255 4.197 0.50 179580. 0.3906 36.10 0.3026 0.6413 0.0471 0.0222 1.158 10.426 7.714 863.484 1.178 34.313 4.052 0.50 179799. 0.3669 38.68 0.3242 0.6630 0.0443 0.0217 1.130 10.174 7.264 842.554 1.149 32.309 3.910 0.50 180028. 0.3435 41.26 0.3458 0.6819 0.0415 0.0210 1.097 9.877 6.800 818.026 1.116 30.246 3.770 0.50 180268. 0.3205 43.84 0.3674 0.6979 0.0386 0.0203 1.059 9.536 6.324 789.795 1.077 28.129 3.632 0.50 180520. 0.2977 46.41 0.3890 0.7108 0.0356 0.0195 1.016 9.150 5.836 757.769 1.034 25.960 3.493 0.50 180783. 0.2751 48.99 0.4106 0.7204 0.0326 0.0186 0.968 8.716 5.338 721.866 0.985 23.743 3.354 0.50 181057. 0.2526 51.57 0.4322 0.7262 0.0295 0.0175 0.915 8.235 4.830 682.019 0.930 21.484 3.212 0.50 181343. 0.2301 54.15 0.4538 0.7277 0.0263 0.0164 0.856 7.706 4.313 638.177 0.871 19.185 3.065 0.50 181641. 0.2075 56.73 0.4754 0.7239 0.0231 0.0152 0.792 7.128 3.788 590.309 0.805 16.851 2.911 0.51 181950. 0.1847 59.31 0.4970 0.7134 0.0199 0.0138 0.722 6.501 3.257 538.410 0.734 14.488 2.744 0.51 182272. 0.1614 61.89 0.5187 0.6938 0.0166 0.0124 0.647 5.826 2.720 482.502 0.658 12.101 2.557 0.51 182605. 0.1375 64.46 0.5403 0.6611 0.0133 0.0109 0.567 5.103 2.180 422.645 0.577 9.696 2.339 0.51 182949. 0.1126 67.04 0.5619 0.6078 0.0100 0.0092 0.481 4.334 1.637 358.939 0.490 7.280 2.068 0.51 183306. 0.0862 69.62 0.5835 0.5189 0.0067 0.0075 0.391 3.520 1.093 291.522 0.398 4.860 1.700 0.51 183673. 0.0579 72.20 0.6051 0.3578 0.0034 0.0057 0.296 2.663 0.550 220.510 0.301 2.444 1.130 0.51 184051. 0.0273 74.78 0.6267 -0.0132 -0.0001 0.0037 0.192 1.726 -0.013 142.929 0.195 -0.056 -0.040 0.51 184374. 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 0.0757 0.0222 1.726 13.600 16.217 1287.230 1.537 72.132 5.714 0.57 203016. 0.7501 2.95 0.0217 0.0716 0.0745 0.0225 1.754 13.821 15.950 1308.143 1.561 70.946 5.530 0.57 203125. 0.7200 5.91 0.0433 0.1386 0.0731 0.0229 1.780 14.024 15.659 1327.351 1.584 69.653 5.351 0.57 203243. 0.6903 8.86 0.0650 0.2011 0.0717 0.0232 1.803 14.204 15.344 1344.437 1.605 68.250 5.177 0.57 203371. 0.6610 11.82 0.0866 0.2594 0.0701 0.0234 1.822 14.358 15.003 1359.012 1.622 66.732 5.007 0.57 203508. 0.6322 14.77 0.1083 0.3136 0.0684 0.0236 1.838 14.482 14.636 1370.707 1.636 65.099 4.843 0.57 203656. 0.6040 17.72 0.1300 0.3639 0.0665 0.0238 1.850 14.571 14.242 1379.178 1.646 63.349 4.684 0.57 203814. 0.5762 20.68 0.1516 0.4106 0.0646 0.0238 1.856 14.624 13.823 1384.110 1.652 61.485 4.530 0.57 203983. 0.5490 23.63 0.1733 0.4538 0.0625 0.0239 1.858 14.635 13.379 1385.213 1.653 59.508 4.381 0.57 204162. 0.5223 26.58 0.1950 0.4937 0.0603 0.0238 1.854 14.604 12.909 1382.219 1.650 57.420 4.236 0.57 204354. 0.4961 29.54 0.2166 0.5304 0.0580 0.0237 1.844 14.526 12.416 1374.884 1.641 55.226 4.096 0.57 204556. 0.4705 32.49 0.2383 0.5641 0.0556 0.0235 1.828 14.400 11.900 1362.978 1.627 52.930 3.960 0.57 204771. 0.4453 35.45 0.2599 0.5948 0.0531 0.0232 1.805 14.224 11.361 1346.287 1.607 50.536 3.828 0.57 204997. 0.4206 38.40 0.2816 0.6227 0.0505 0.0228 1.776 13.995 10.802 1324.611 1.581 48.048 3.699 0.57 205236. 0.3963 41.35 0.3033 0.6478 0.0477 0.0224 1.740 13.711 10.223 1297.760 1.549 45.472 3.573 0.57 205487. 0.3724 44.31 0.3249 0.6701 0.0450 0.0218 1.697 13.371 9.625 1265.556 1.511 42.812 3.450 0.57 205751. 0.3489 47.26 0.3466 0.6896 0.0421 0.0211 1.647 12.972 9.009 1227.832 1.466 40.073 3.328 0.57 206027. 0.3256 50.22 0.3682 0.7062 0.0391 0.0204 1.588 12.514 8.377 1184.432 1.414 37.261 3.208 0.58 206317. 0.3027 53.17 0.3899 0.7198 0.0361 0.0196 1.522 11.994 7.729 1135.220 1.355 34.379 3.088 0.58 206619. 0.2799 56.12 0.4116 0.7302 0.0330 0.0186 1.448 11.411 7.067 1080.071 1.289 31.434 2.968 0.58 206934. 0.2572 59.08 0.4332 0.7369 0.0299 0.0176 1.366 10.765 6.392 1018.879 1.216 28.430 2.845 0.58 207263. 0.2345 62.03 0.4549 0.7394 0.0266 0.0164 1.276 10.054 5.705 951.573 1.136 25.374 2.719 0.58 207605. 0.2117 64.98 0.4766 0.7368 0.0234 0.0151 1.178 9.277 5.007 878.106 1.048 22.271 2.586 0.58 207961. 0.1886 67.94 0.4982 0.7276 0.0201 0.0138 1.071 8.436 4.300 798.470 0.953 19.128 2.443 0.58 208329. 0.1651 70.89 0.5199 0.7094 0.0168 0.0123 0.956 7.530 3.586 712.704 0.851 15.952 2.282 0.58 208712. 0.1409 73.85 0.5415 0.6780 0.0134 0.0107 0.833 6.560 2.867 620.899 0.741 12.753 2.094 0.58 209108. 0.1156 76.80 0.5632 0.6259 0.0100 0.0090 0.702 5.528 2.144 523.214 0.625 9.538 1.859 0.58 209517. 0.0887 79.75 0.5849 0.5366 0.0066 0.0072 0.563 4.436 1.421 419.864 0.501 6.319 1.535 0.58 209939. 0.0596 82.71 0.6065 0.3690 0.0033 0.0054 0.417 3.286 0.698 311.016 0.371 3.104 1.018 0.58 210372. 0.0277 85.66 0.6282 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 0.0769 0.0224 2.488 17.423 20.833 1855.258 1.968 92.665 5.093 0.64 228374. 0.7578 3.34 0.0218 0.0722 0.0756 0.0228 2.530 17.715 20.497 1886.348 2.001 91.172 4.929 0.64 228497. 0.7274 6.68 0.0435 0.1396 0.0743 0.0232 2.568 17.984 20.130 1914.911 2.032 89.538 4.768 0.64 228632. 0.6973 10.02 0.0653 0.2026 0.0728 0.0235 2.602 18.222 19.730 1940.311 2.059 87.758 4.612 0.64 228777. 0.6678 13.36 0.0871 0.2613 0.0712 0.0237 2.631 18.426 19.296 1961.966 2.082 85.827 4.461 0.64 228933. 0.6388 16.70 0.1089 0.3158 0.0695 0.0239 2.654 18.588 18.827 1979.314 2.100 83.742 4.314 0.64 229101. 0.6102 20.04 0.1306 0.3666 0.0676 0.0241 2.671 18.706 18.324 1991.839 2.113 81.504 4.173 0.64 229281. 0.5822 23.38 0.1524 0.4136 0.0656 0.0242 2.681 18.774 17.786 1999.075 2.121 79.113 4.035 0.64 229473. 0.5548 26.72 0.1742 0.4572 0.0635 0.0242 2.683 18.788 17.215 2000.587 2.123 76.572 3.903 0.64 229678. 0.5279 30.06 0.1959 0.4974 0.0613 0.0241 2.677 18.745 16.611 1995.987 2.118 73.885 3.775 0.64 229895. 0.5015 33.40 0.2177 0.5345 0.0590 0.0240 2.662 18.641 15.975 1984.918 2.106 71.057 3.650 0.64 230126. 0.4756 36.74 0.2395 0.5685 0.0565 0.0238 2.638 18.473 15.309 1967.050 2.087 68.094 3.530 0.64 230371. 0.4502 40.08 0.2613 0.5997 0.0539 0.0235 2.604 18.239 14.613 1942.075 2.061 65.001 3.413 0.64 230628. 0.4253 43.42 0.2830 0.6280 0.0513 0.0231 2.561 17.935 13.890 1909.704 2.026 61.785 3.299 0.65 230900. 0.4008 46.76 0.3048 0.6535 0.0485 0.0226 2.507 17.559 13.141 1869.675 1.984 58.452 3.188 0.65 231186. 0.3767 50.10 0.3266 0.6763 0.0456 0.0220 2.443 17.109 12.367 1821.729 1.933 55.009 3.079 0.65 231486. 0.3530 53.44 0.3483 0.6963 0.0427 0.0214 2.368 16.582 11.570 1765.630 1.873 51.463 2.972 0.65 231801. 0.3296 56.78 0.3701 0.7135 0.0397 0.0206 2.281 15.976 10.751 1701.157 1.805 47.819 2.866 0.65 232130. 0.3064 60.12 0.3919 0.7277 0.0366 0.0197 2.183 15.290 9.911 1628.110 1.727 44.085 2.761 0.65 232473. 0.2834 63.46 0.4136 0.7387 0.0334 0.0187 2.074 14.522 9.053 1546.311 1.641 40.267 2.655 0.65 232832. 0.2604 66.80 0.4354 0.7462 0.0302 0.0176 1.952 13.670 8.177 1455.616 1.544 36.372 2.548 0.65 233206. 0.2375 70.14 0.4572 0.7494 0.0269 0.0164 1.818 12.734 7.286 1355.916 1.439 32.409 2.437 0.65 233595. 0.2145 73.48 0.4790 0.7476 0.0235 0.0151 1.672 11.712 6.381 1247.150 1.323 28.383 2.321 0.65 233999. 0.1911 76.82 0.5007 0.7391 0.0202 0.0137 1.514 10.606 5.464 1129.314 1.198 24.306 2.195 0.65 234418. 0.1672 80.16 0.5225 0.7215 0.0167 0.0121 1.344 9.415 4.538 1002.470 1.064 20.185 2.053 0.65 234853. 0.1426 83.50 0.5443 0.6905 0.0133 0.0105 1.162 8.140 3.605 866.766 0.920 16.033 1.886 0.65 235302. 0.1167 86.84 0.5660 0.6374 0.0098 0.0087 0.969 6.785 2.667 722.445 0.767 11.863 1.674 0.65 235767. 0.0891 90.18 0.5878 0.5438 0.0064 0.0069 0.764 5.352 1.728 569.838 0.605 7.687 1.376 0.65 236247. 0.0589 93.52 0.6096 0.3591 0.0029 0.0049 0.549 3.842 0.790 409.131 0.434 3.515 0.876 0.65 236737. 0.0254 96.86 0.6314 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 0.0782 0.0230 3.498 22.047 26.170 2608.457 2.491 116.404 4.551 0.71 253722. 0.7589 3.69 0.0217 0.0714 0.0770 0.0234 3.554 22.398 25.766 2649.938 2.531 114.606 4.410 0.71 253859. 0.7297 7.38 0.0433 0.1382 0.0757 0.0237 3.605 22.721 25.321 2688.133 2.567 112.628 4.272 0.71 254008. 0.7008 11.07 0.0650 0.2008 0.0742 0.0240 3.650 23.009 24.835 2722.177 2.599 110.464 4.138 0.71 254169. 0.6722 14.76 0.0866 0.2593 0.0727 0.0243 3.690 23.254 24.305 2751.271 2.627 108.108 4.007 0.71 254343. 0.6439 18.45 0.1083 0.3138 0.0709 0.0245 3.721 23.452 23.731 2774.619 2.650 105.555 3.879 0.71 254529. 0.6160 22.14 0.1299 0.3646 0.0691 0.0246 3.743 23.594 23.113 2791.491 2.666 102.806 3.755 0.71 254728. 0.5885 25.83 0.1516 0.4117 0.0671 0.0247 3.756 23.676 22.451 2801.200 2.675 99.860 3.635 0.71 254941. 0.5615 29.52 0.1732 0.4554 0.0650 0.0247 3.759 23.693 21.745 2803.116 2.677 96.723 3.519 0.72 255168. 0.5349 33.21 0.1949 0.4959 0.0628 0.0247 3.750 23.638 20.998 2796.649 2.671 93.398 3.405 0.72 255410. 0.5087 36.90 0.2165 0.5332 0.0604 0.0245 3.730 23.508 20.210 2781.250 2.656 89.892 3.296 0.72 255665. 0.4830 40.60 0.2382 0.5676 0.0579 0.0243 3.696 23.298 19.382 2756.414 2.632 86.213 3.189 0.72 255936. 0.4577 44.29 0.2598 0.5991 0.0554 0.0240 3.650 23.004 18.518 2721.683 2.599 82.368 3.086 0.72 256221. 0.4329 47.98 0.2815 0.6279 0.0527 0.0236 3.589 22.624 17.618 2676.627 2.556 78.365 2.985 0.72 256521. 0.4085 51.67 0.3031 0.6540 0.0499 0.0231 3.515 22.152 16.685 2620.881 2.503 74.213 2.887 0.72 256837. 0.3845 55.36 0.3248 0.6775 0.0470 0.0225 3.425 21.588 15.719 2554.102 2.439 69.920 2.792 0.72 257169. 0.3608 59.05 0.3464 0.6982 0.0440 0.0218 3.320 20.928 14.724 2475.974 2.364 65.494 2.697 0.72 257516. 0.3374 62.74 0.3681 0.7163 0.0410 0.0210 3.200 20.169 13.701 2386.205 2.279 60.943 2.604 0.72 257879. 0.3142 66.43 0.3897 0.7315 0.0378 0.0201 3.064 19.309 12.652 2284.521 2.182 56.277 2.512 0.72 258259. 0.2913 70.12 0.4114 0.7437 0.0346 0.0191 2.911 18.347 11.579 2170.679 2.073 51.504 2.419 0.72 258654. 0.2684 73.81 0.4330 0.7526 0.0313 0.0180 2.742 17.280 10.484 2044.474 1.952 46.631 2.326 0.72 259066. 0.2455 77.50 0.4547 0.7575 0.0280 0.0168 2.556 16.108 9.368 1905.749 1.820 41.669 2.230 0.72 259495. 0.2225 81.19 0.4763 0.7577 0.0246 0.0155 2.353 14.829 8.234 1754.412 1.675 36.626 2.129 0.72 259940. 0.1991 84.88 0.4980 0.7519 0.0212 0.0140 2.133 13.443 7.085 1590.448 1.519 31.514 2.021 0.72 260402. 0.1753 88.57 0.5196 0.7378 0.0177 0.0125 1.896 11.951 5.923 1413.927 1.350 26.346 1.900 0.72 260880. 0.1507 92.26 0.5413 0.7115 0.0142 0.0108 1.643 10.354 4.751 1225.042 1.170 21.133 1.759 0.72 261376. 0.1250 95.95 0.5629 0.6656 0.0107 0.0090 1.373 8.656 3.573 1024.140 0.978 15.892 1.582 0.73 261887. 0.0975 99.64 0.5846 0.5839 0.0072 0.0072 1.089 6.861 2.392 811.743 0.775 10.640 1.337 0.73 262415. 0.0674 103.33 0.6062 0.4233 0.0036 0.0052 0.789 4.973 1.212 588.361 0.562 5.391 0.934 0.73 262956. 0.0335 107.02 0.6279 -0.0184 -0.0001 0.0030 0.457 2.879 -0.029 340.634 0.325 -0.131 -0.039 0.73 263372. 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 0.0798 0.0248 5.013 28.723 32.296 3738.138 3.245 143.654 3.919 0.79 279059. 0.7260 4.07 0.0217 0.0681 0.0786 0.0251 5.072 29.059 31.822 3781.867 3.283 141.542 3.816 0.79 279211. 0.7018 8.14 0.0434 0.1326 0.0773 0.0253 5.124 29.357 31.296 3820.627 3.317 139.203 3.715 0.79 279376. 0.6775 12.21 0.0651 0.1935 0.0759 0.0255 5.167 29.609 30.716 3853.401 3.345 136.626 3.615 0.79 279554. 0.6532 16.28 0.0868 0.2510 0.0743 0.0257 5.202 29.808 30.081 3879.247 3.368 133.802 3.517 0.79 279747. 0.6288 20.35 0.1085 0.3051 0.0726 0.0258 5.226 29.946 29.389 3897.295 3.383 130.724 3.420 0.79 279953. 0.6044 24.42 0.1302 0.3560 0.0708 0.0259 5.239 30.019 28.640 3906.753 3.392 127.392 3.325 0.79 280175. 0.5801 28.49 0.1519 0.4036 0.0688 0.0259 5.239 30.020 27.834 3906.887 3.392 123.806 3.231 0.79 280412. 0.5557 32.56 0.1736 0.4481 0.0666 0.0258 5.226 29.944 26.972 3897.041 3.383 119.972 3.139 0.79 280664. 0.5315 36.63 0.1954 0.4895 0.0644 0.0257 5.199 29.787 26.056 3876.587 3.365 115.896 3.049 0.79 280932. 0.5073 40.70 0.2171 0.5280 0.0620 0.0255 5.156 29.544 25.087 3844.906 3.338 111.587 2.959 0.79 281216. 0.4832 44.77 0.2388 0.5636 0.0595 0.0252 5.098 29.209 24.068 3801.383 3.300 107.053 2.872 0.79 281517. 0.4592 48.84 0.2605 0.5964 0.0568 0.0248 5.023 28.779 23.000 3745.400 3.251 102.306 2.785 0.79 281834. 0.4355 52.91 0.2822 0.6263 0.0541 0.0244 4.930 28.249 21.887 3676.349 3.192 97.354 2.700 0.79 282167. 0.4118 56.98 0.3039 0.6536 0.0512 0.0238 4.819 27.613 20.731 3593.638 3.120 92.210 2.617 0.79 282518. 0.3884 61.05 0.3256 0.6781 0.0483 0.0232 4.689 26.868 19.533 3496.682 3.036 86.885 2.534 0.79 282886. 0.3650 65.12 0.3473 0.6999 0.0452 0.0224 4.539 26.009 18.298 3384.919 2.939 81.389 2.452 0.79 283271. 0.3419 69.19 0.3690 0.7190 0.0421 0.0216 4.369 25.032 17.026 3257.793 2.828 75.734 2.371 0.79 283674. 0.3189 73.26 0.3907 0.7352 0.0388 0.0206 4.177 23.934 15.722 3114.792 2.704 69.930 2.289 0.79 284095. 0.2959 77.33 0.4124 0.7484 0.0355 0.0196 3.963 22.709 14.386 2955.442 2.566 63.989 2.208 0.79 284533. 0.2730 81.40 0.4341 0.7583 0.0322 0.0184 3.727 21.357 13.022 2779.412 2.413 57.921 2.125 0.79 284990. 0.2500 85.47 0.4558 0.7642 0.0287 0.0171 3.469 19.875 11.632 2586.605 2.245 51.738 2.040 0.79 285464. 0.2268 89.54 0.4775 0.7654 0.0252 0.0157 3.187 18.263 10.218 2376.833 2.063 45.451 1.950 0.79 285957. 0.2032 93.61 0.4992 0.7604 0.0217 0.0142 2.884 16.523 8.785 2150.291 1.867 39.075 1.853 0.80 286469. 0.1790 97.68 0.5209 0.7468 0.0181 0.0126 2.558 14.656 7.334 1907.431 1.656 32.623 1.744 0.80 286998. 0.1540 101.75 0.5426 0.7203 0.0145 0.0109 2.211 12.670 5.871 1648.963 1.431 26.113 1.615 0.80 287546. 0.1275 105.82 0.5644 0.6726 0.0109 0.0091 1.845 10.572 4.398 1375.925 1.194 19.563 1.450 0.80 288112. 0.0991 109.89 0.5861 0.5858 0.0072 0.0072 1.461 8.373 2.922 1089.672 0.946 12.995 1.216 0.80 288696. 0.0678 113.96 0.6078 0.4136 0.0036 0.0052 1.061 6.082 1.445 791.494 0.687 6.425 0.828 0.80 289294. 0.0324 118.03 0.6295 PROP RPM = 12000 V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM (mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - - 0.00 0.0000 0.0000 0.0814 0.0292 7.672 40.297 39.216 5721.104 4.553 174.432 3.109 0.86 304385. 0.6347 4.51 0.0220 0.0603 0.0803 0.0294 7.714 40.516 38.676 5752.164 4.577 172.032 3.050 0.86 304553. 0.6183 9.01 0.0441 0.1182 0.0790 0.0295 7.742 40.664 38.071 5773.206 4.594 169.342 2.991 0.86 304736. 0.6016 13.52 0.0661 0.1739 0.0776 0.0295 7.755 40.733 37.397 5783.011 4.602 166.344 2.933 0.86 304935. 0.5847 18.03 0.0881 0.2273 0.0761 0.0295 7.752 40.716 36.651 5780.551 4.600 163.024 2.876 0.86 305149. 0.5675 22.54 0.1102 0.2785 0.0744 0.0294 7.731 40.606 35.830 5764.949 4.588 159.371 2.819 0.86 305380. 0.5501 27.04 0.1322 0.3275 0.0725 0.0293 7.691 40.398 34.933 5735.522 4.564 155.381 2.763 0.86 305629. 0.5322 31.55 0.1543 0.3743 0.0705 0.0290 7.633 40.090 33.960 5691.781 4.529 151.055 2.706 0.86 305894. 0.5141 36.06 0.1763 0.4189 0.0683 0.0288 7.555 39.679 32.913 5633.413 4.483 146.399 2.650 0.86 306177. 0.4956 40.57 0.1983 0.4612 0.0660 0.0284 7.456 39.164 31.794 5560.265 4.425 141.420 2.594 0.86 306479. 0.4767 45.07 0.2204 0.5013 0.0635 0.0279 7.338 38.544 30.605 5472.192 4.355 136.132 2.537 0.86 306798. 0.4575 49.58 0.2424 0.5389 0.0609 0.0274 7.200 37.817 29.350 5369.049 4.273 130.547 2.479 0.86 307136. 0.4379 54.09 0.2644 0.5742 0.0582 0.0268 7.041 36.984 28.031 5250.701 4.178 124.681 2.421 0.86 307493. 0.4179 58.60 0.2865 0.6069 0.0553 0.0261 6.862 36.040 26.652 5116.791 4.072 118.549 2.363 0.86 307868. 0.3976 63.10 0.3085 0.6370 0.0523 0.0253 6.661 34.984 25.217 4966.842 3.952 112.165 2.303 0.86 308263. 0.3770 67.61 0.3305 0.6646 0.0493 0.0245 6.437 33.811 23.729 4800.226 3.820 105.545 2.242 0.86 308677. 0.3560 72.12 0.3526 0.6893 0.0461 0.0236 6.190 32.514 22.190 4616.187 3.673 98.702 2.180 0.86 309110. 0.3348 76.62 0.3746 0.7112 0.0428 0.0225 5.919 31.090 20.605 4413.927 3.512 91.650 2.117 0.86 309564. 0.3133 81.13 0.3966 0.7301 0.0394 0.0214 5.623 29.531 18.976 4192.703 3.336 84.405 2.053 0.86 310037. 0.2915 85.64 0.4187 0.7458 0.0359 0.0202 5.299 27.835 17.307 3951.789 3.145 76.981 1.986 0.86 310530. 0.2694 90.15 0.4407 0.7578 0.0324 0.0188 4.949 25.994 15.601 3690.490 2.937 69.393 1.917 0.87 311043. 0.2469 94.65 0.4628 0.7645 0.0288 0.0174 4.576 24.037 13.861 3412.567 2.716 61.655 1.842 0.87 311577. 0.2236 99.16 0.4848 0.7624 0.0251 0.0160 4.193 22.023 12.090 3126.661 2.488 53.777 1.754 0.87 312131. 0.1988 103.67 0.5068 0.7515 0.0214 0.0144 3.786 19.886 10.293 2823.238 2.247 45.784 1.654 0.87 312705. 0.1729 108.18 0.5289 0.7283 0.0176 0.0128 3.357 17.630 8.474 2503.046 1.992 37.694 1.536 0.87 313300. 0.1457 112.68 0.5509 0.6859 0.0138 0.0111 2.908 15.275 6.639 2168.724 1.726 29.531 1.389 0.87 313915. 0.1166 117.19 0.5729 0.6129 0.0100 0.0093 2.444 12.836 4.793 1822.439 1.450 21.321 1.193 0.87 314550. 0.0851 121.70 0.5950 0.4853 0.0061 0.0075 1.968 10.336 2.943 1467.451 1.168 13.090 0.910 0.87 315205. 0.0509 126.20 0.6170 0.2474 0.0023 0.0056 1.482 7.783 1.090 1104.963 0.879 4.846 0.447 0.87 315870. 0.0152 130.71 0.6390 PROP RPM = 13000 V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM (mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - - 0.00 0.0000 0.0000 0.0815 0.0349 11.648 56.472 46.077 8685.662 6.380 204.953 2.406 0.93 329745. 0.5324 4.91 0.0222 0.0509 0.0805 0.0351 11.717 56.806 45.538 8737.082 6.418 202.554 2.364 0.93 329924. 0.5200 9.83 0.0444 0.1001 0.0795 0.0352 11.765 57.043 44.926 8773.503 6.445 199.829 2.323 0.93 330120. 0.5075 14.74 0.0665 0.1475 0.0782 0.0353 11.790 57.162 44.233 8791.752 6.458 196.749 2.282 0.93 330333. 0.4947 19.66 0.0887 0.1933 0.0769 0.0353 11.786 57.142 43.455 8788.754 6.456 193.287 2.243 0.93 330564. 0.4819 24.57 0.1109 0.2375 0.0753 0.0352 11.750 56.966 42.585 8761.624 6.436 189.417 2.205 0.93 330813. 0.4690 29.49 0.1331 0.2802 0.0736 0.0350 11.677 56.616 41.619 8707.908 6.396 185.122 2.168 0.93 331082. 0.4559 34.40 0.1553 0.3216 0.0717 0.0346 11.567 56.083 40.556 8625.828 6.336 180.392 2.133 0.93 331370. 0.4427 39.32 0.1774 0.3617 0.0697 0.0342 11.418 55.358 39.394 8514.354 6.254 175.223 2.099 0.93 331678. 0.4294 44.23 0.1996 0.4006 0.0674 0.0336 11.229 54.441 38.134 8373.282 6.151 169.621 2.066 0.93 332007. 0.4158 49.15 0.2218 0.4382 0.0651 0.0329 11.001 53.334 36.779 8203.101 6.026 163.594 2.034 0.93 332356. 0.4020 54.06 0.2440 0.4745 0.0625 0.0321 10.735 52.045 35.332 8004.862 5.880 157.158 2.002 0.93 332726. 0.3879 58.98 0.2661 0.5094 0.0598 0.0312 10.433 50.583 33.797 7779.917 5.715 150.329 1.970 0.93 333118. 0.3734 63.89 0.2883 0.5429 0.0569 0.0302 10.098 48.957 32.178 7529.773 5.531 143.128 1.938 0.93 333530. 0.3584 68.80 0.3105 0.5747 0.0539 0.0291 9.730 47.176 30.481 7255.925 5.330 135.579 1.905 0.93 333964. 0.3429 73.72 0.3327 0.6047 0.0508 0.0279 9.333 45.247 28.710 6959.299 5.112 127.702 1.871 0.93 334419. 0.3268 78.63 0.3549 0.6327 0.0475 0.0267 8.905 43.174 26.870 6640.383 4.878 119.518 1.835 0.93 334896. 0.3101 83.55 0.3770 0.6584 0.0442 0.0253 8.448 40.958 24.965 6299.484 4.627 111.047 1.798 0.93 335395. 0.2928 88.46 0.3992 0.6815 0.0407 0.0238 7.961 38.600 23.002 5936.871 4.361 102.311 1.757 0.94 335915. 0.2747 93.38 0.4214 0.7017 0.0371 0.0223 7.446 36.102 20.983 5552.643 4.079 93.334 1.714 0.94 336458. 0.2559 98.29 0.4436 0.7183 0.0335 0.0207 6.902 33.462 18.916 5146.661 3.781 84.138 1.667 0.94 337022. 0.2363 103.21 0.4658 0.7308 0.0297 0.0189 6.328 30.681 16.805 4718.916 3.466 74.747 1.615 0.94 337609. 0.2158 108.12 0.4879 0.7309 0.0259 0.0173 5.778 28.015 14.648 4308.815 3.165 65.155 1.542 0.94 338218. 0.1924 113.04 0.5101 0.7080 0.0220 0.0159 5.299 25.692 12.447 3951.542 2.903 55.366 1.429 0.94 338849. 0.1643 117.95 0.5323 0.6680 0.0181 0.0144 4.811 23.326 10.218 3587.624 2.635 45.452 1.292 0.94 339502. 0.1346 122.87 0.5545 0.6049 0.0141 0.0129 4.317 20.930 7.970 3219.098 2.365 35.449 1.123 0.94 340178. 0.1033 127.78 0.5767 0.5087 0.0101 0.0114 3.825 18.544 5.710 2852.164 2.095 25.399 0.908 0.94 340876. 0.0707 132.70 0.5988 0.3658 0.0061 0.0100 3.338 16.184 3.451 2489.109 1.828 15.348 0.629 0.94 341594. 0.0381 137.61 0.6210 0.1532 0.0021 0.0085 2.856 13.847 1.193 2129.811 1.564 5.305 0.254 0.95 342326. 0.0090 142.52 0.6432