18x5.5MR (18x55MR.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 0.0720 0.0249 0.004 0.239 0.241 2.825 0.027 1.072 38.696 0.07 36929. 0.6193 0.27 0.0156 0.0441 0.0704 0.0249 0.004 0.239 0.235 2.824 0.027 1.047 37.828 0.07 36945. 0.5984 0.53 0.0312 0.0862 0.0687 0.0249 0.004 0.238 0.230 2.820 0.027 1.022 36.945 0.07 36962. 0.5772 0.80 0.0468 0.1261 0.0668 0.0248 0.004 0.238 0.224 2.813 0.027 0.995 36.051 0.07 36980. 0.5557 1.06 0.0624 0.1639 0.0650 0.0247 0.004 0.237 0.217 2.805 0.027 0.967 35.145 0.07 36998. 0.5341 1.33 0.0780 0.1995 0.0630 0.0246 0.004 0.236 0.211 2.794 0.027 0.938 34.222 0.07 37018. 0.5122 1.60 0.0936 0.2329 0.0610 0.0245 0.004 0.235 0.204 2.780 0.027 0.907 33.285 0.07 37038. 0.4901 1.86 0.1092 0.2639 0.0589 0.0244 0.004 0.234 0.197 2.763 0.026 0.876 32.328 0.07 37059. 0.4677 2.13 0.1248 0.2925 0.0567 0.0242 0.004 0.232 0.190 2.744 0.026 0.844 31.352 0.07 37081. 0.4451 2.39 0.1404 0.3185 0.0544 0.0240 0.004 0.230 0.182 2.721 0.026 0.810 30.350 0.07 37104. 0.4221 2.66 0.1560 0.3419 0.0521 0.0238 0.004 0.228 0.174 2.695 0.026 0.775 29.322 0.07 37128. 0.3989 2.93 0.1717 0.3626 0.0497 0.0235 0.004 0.225 0.166 2.666 0.025 0.739 28.265 0.07 37153. 0.3755 3.19 0.1873 0.3803 0.0472 0.0232 0.004 0.223 0.158 2.633 0.025 0.702 27.176 0.07 37179. 0.3519 3.46 0.2029 0.3949 0.0446 0.0229 0.003 0.220 0.149 2.598 0.025 0.664 26.052 0.07 37205. 0.3281 3.72 0.2185 0.4063 0.0420 0.0226 0.003 0.216 0.140 2.559 0.024 0.625 24.889 0.07 37233. 0.3040 3.99 0.2341 0.4142 0.0393 0.0222 0.003 0.213 0.131 2.517 0.024 0.585 23.682 0.07 37262. 0.2799 4.26 0.2497 0.4184 0.0365 0.0218 0.003 0.209 0.122 2.472 0.024 0.544 22.426 0.07 37291. 0.2556 4.52 0.2653 0.4186 0.0337 0.0214 0.003 0.205 0.113 2.423 0.023 0.502 21.114 0.07 37322. 0.2311 4.79 0.2809 0.4143 0.0308 0.0209 0.003 0.200 0.103 2.370 0.023 0.459 19.740 0.07 37354. 0.2067 5.05 0.2965 0.4054 0.0279 0.0204 0.003 0.196 0.093 2.314 0.022 0.415 18.296 0.07 37387. 0.1822 5.32 0.3121 0.3912 0.0249 0.0199 0.003 0.191 0.083 2.254 0.022 0.371 16.772 0.07 37421. 0.1579 5.59 0.3277 0.3712 0.0219 0.0193 0.003 0.185 0.073 2.191 0.021 0.326 15.157 0.07 37456. 0.1337 5.85 0.3433 0.3448 0.0188 0.0187 0.003 0.180 0.063 2.124 0.020 0.280 13.440 0.07 37493. 0.1099 6.12 0.3589 0.3113 0.0157 0.0181 0.003 0.174 0.053 2.053 0.020 0.234 11.607 0.07 37530. 0.0867 6.38 0.3745 0.2698 0.0126 0.0174 0.003 0.167 0.042 1.978 0.019 0.187 9.642 0.07 37569. 0.0645 6.65 0.3901 0.2195 0.0094 0.0168 0.003 0.161 0.032 1.901 0.018 0.140 7.531 0.07 37608. 0.0436 6.92 0.4057 0.1594 0.0063 0.0160 0.002 0.154 0.021 1.820 0.017 0.094 5.256 0.07 37649. 0.0249 7.18 0.4213 0.0873 0.0032 0.0153 0.002 0.147 0.011 1.735 0.017 0.047 2.774 0.07 37691. 0.0093 7.45 0.4369 0.0004 0.0000 0.0145 0.002 0.139 0.000 1.646 0.016 0.000 0.012 0.07 37732. 0.0000 7.71 0.4525 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 0.0723 0.0229 0.028 0.877 0.967 20.751 0.099 4.303 21.144 0.14 73857. 0.6779 0.52 0.0151 0.0468 0.0707 0.0229 0.028 0.876 0.946 20.738 0.099 4.207 20.687 0.14 73889. 0.6558 1.03 0.0303 0.0915 0.0690 0.0228 0.028 0.875 0.923 20.709 0.099 4.107 20.224 0.14 73922. 0.6335 1.55 0.0454 0.1341 0.0672 0.0228 0.028 0.873 0.900 20.656 0.099 4.002 19.759 0.14 73956. 0.6110 2.06 0.0606 0.1746 0.0654 0.0227 0.028 0.870 0.876 20.587 0.098 3.895 19.291 0.14 73992. 0.5884 2.58 0.0757 0.2129 0.0635 0.0226 0.027 0.866 0.850 20.496 0.098 3.782 18.817 0.14 74029. 0.5656 3.10 0.0908 0.2489 0.0616 0.0225 0.027 0.861 0.824 20.382 0.097 3.665 18.339 0.14 74068. 0.5427 3.61 0.1060 0.2828 0.0596 0.0223 0.027 0.856 0.797 20.246 0.097 3.545 17.854 0.14 74109. 0.5196 4.13 0.1211 0.3143 0.0575 0.0221 0.027 0.849 0.769 20.083 0.096 3.420 17.363 0.14 74151. 0.4963 4.64 0.1362 0.3434 0.0553 0.0219 0.027 0.841 0.740 19.895 0.095 3.290 16.863 0.14 74195. 0.4728 5.16 0.1514 0.3700 0.0530 0.0217 0.026 0.832 0.709 19.678 0.094 3.156 16.353 0.14 74241. 0.4490 5.68 0.1665 0.3940 0.0507 0.0214 0.026 0.821 0.678 19.434 0.093 3.017 15.832 0.14 74289. 0.4251 6.19 0.1817 0.4153 0.0483 0.0211 0.026 0.810 0.646 19.163 0.091 2.875 15.298 0.14 74338. 0.4009 6.71 0.1968 0.4338 0.0458 0.0208 0.025 0.797 0.613 18.864 0.090 2.729 14.750 0.14 74389. 0.3766 7.23 0.2119 0.4493 0.0433 0.0204 0.025 0.783 0.580 18.537 0.089 2.579 14.186 0.14 74442. 0.3521 7.74 0.2271 0.4616 0.0407 0.0200 0.024 0.768 0.545 18.180 0.087 2.425 13.603 0.14 74497. 0.3274 8.26 0.2422 0.4705 0.0381 0.0196 0.024 0.752 0.510 17.794 0.085 2.268 12.998 0.14 74554. 0.3026 8.77 0.2574 0.4757 0.0354 0.0192 0.023 0.734 0.474 17.376 0.083 2.107 12.367 0.14 74613. 0.2775 9.29 0.2725 0.4768 0.0327 0.0187 0.023 0.715 0.437 16.928 0.081 1.944 11.708 0.14 74673. 0.2523 9.81 0.2876 0.4735 0.0298 0.0181 0.022 0.695 0.399 16.448 0.079 1.777 11.014 0.14 74736. 0.2269 10.32 0.3028 0.4652 0.0270 0.0176 0.021 0.673 0.361 15.935 0.076 1.607 10.281 0.14 74801. 0.2014 10.84 0.3179 0.4514 0.0241 0.0170 0.021 0.650 0.322 15.389 0.073 1.434 9.501 0.14 74868. 0.1758 11.35 0.3330 0.4313 0.0211 0.0163 0.020 0.626 0.283 14.811 0.071 1.259 8.666 0.14 74937. 0.1503 11.87 0.3482 0.4041 0.0182 0.0157 0.019 0.600 0.243 14.199 0.068 1.081 7.765 0.14 75008. 0.1248 12.39 0.3633 0.3686 0.0152 0.0149 0.018 0.573 0.203 13.555 0.065 0.902 6.788 0.14 75082. 0.0997 12.90 0.3785 0.3235 0.0121 0.0142 0.017 0.544 0.162 12.879 0.061 0.722 5.719 0.14 75157. 0.0751 13.42 0.3936 0.2673 0.0091 0.0134 0.016 0.514 0.122 12.174 0.058 0.542 4.543 0.14 75235. 0.0517 13.93 0.4087 0.1976 0.0061 0.0126 0.015 0.484 0.082 11.442 0.055 0.363 3.235 0.14 75315. 0.0301 14.45 0.4239 0.1110 0.0031 0.0118 0.014 0.451 0.041 10.679 0.051 0.184 1.753 0.14 75396. 0.0116 14.97 0.4390 0.0010 0.0000 0.0109 0.013 0.417 0.000 9.874 0.047 0.001 0.015 0.14 75472. 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 0.0726 0.0220 0.090 1.899 2.185 67.390 0.215 9.719 14.706 0.21 110784. 0.7086 0.78 0.0152 0.0489 0.0710 0.0220 0.090 1.897 2.136 67.343 0.214 9.503 14.389 0.21 110831. 0.6856 1.55 0.0303 0.0957 0.0693 0.0220 0.090 1.894 2.086 67.237 0.214 9.277 14.069 0.21 110881. 0.6623 2.33 0.0455 0.1403 0.0675 0.0219 0.090 1.889 2.032 67.047 0.213 9.040 13.749 0.21 110933. 0.6389 3.10 0.0607 0.1827 0.0657 0.0218 0.090 1.882 1.977 66.801 0.213 8.796 13.427 0.21 110987. 0.6155 3.88 0.0759 0.2228 0.0638 0.0217 0.089 1.873 1.920 66.478 0.212 8.542 13.102 0.21 111043. 0.5919 4.65 0.0910 0.2607 0.0618 0.0216 0.089 1.861 1.861 66.069 0.210 8.278 12.776 0.21 111102. 0.5681 5.43 0.1062 0.2963 0.0598 0.0214 0.088 1.848 1.800 65.583 0.209 8.005 12.446 0.21 111163. 0.5443 6.21 0.1214 0.3296 0.0577 0.0212 0.087 1.831 1.736 65.002 0.207 7.722 12.113 0.21 111227. 0.5203 6.98 0.1365 0.3604 0.0555 0.0210 0.086 1.812 1.670 64.328 0.205 7.428 11.775 0.21 111294. 0.4961 7.76 0.1517 0.3888 0.0532 0.0208 0.085 1.791 1.602 63.552 0.202 7.125 11.432 0.21 111362. 0.4716 8.53 0.1669 0.4146 0.0509 0.0205 0.084 1.766 1.531 62.679 0.200 6.811 11.081 0.21 111434. 0.4470 9.31 0.1820 0.4377 0.0485 0.0202 0.083 1.739 1.459 61.708 0.196 6.489 10.724 0.21 111508. 0.4222 10.09 0.1972 0.4579 0.0460 0.0198 0.081 1.708 1.385 60.635 0.193 6.159 10.358 0.21 111585. 0.3973 10.86 0.2124 0.4752 0.0435 0.0194 0.080 1.675 1.308 59.460 0.189 5.820 9.981 0.21 111665. 0.3722 11.64 0.2276 0.4894 0.0409 0.0190 0.078 1.639 1.230 58.178 0.185 5.473 9.593 0.21 111748. 0.3469 12.41 0.2427 0.5001 0.0382 0.0185 0.076 1.600 1.151 56.787 0.181 5.118 9.190 0.21 111833. 0.3213 13.19 0.2579 0.5071 0.0355 0.0181 0.074 1.558 1.069 55.285 0.176 4.755 8.770 0.21 111922. 0.2956 13.96 0.2731 0.5100 0.0327 0.0175 0.072 1.512 0.986 53.669 0.171 4.385 8.331 0.22 112013. 0.2696 14.74 0.2882 0.5084 0.0299 0.0170 0.070 1.463 0.901 51.936 0.165 4.007 7.868 0.22 112108. 0.2435 15.52 0.3034 0.5018 0.0271 0.0164 0.067 1.411 0.815 50.085 0.159 3.624 7.377 0.22 112206. 0.2171 16.29 0.3186 0.4894 0.0241 0.0157 0.065 1.356 0.727 48.115 0.153 3.234 6.853 0.22 112306. 0.1905 17.07 0.3338 0.4705 0.0212 0.0150 0.062 1.297 0.638 46.024 0.146 2.838 6.288 0.22 112410. 0.1637 17.84 0.3489 0.4439 0.0182 0.0143 0.059 1.234 0.548 43.814 0.139 2.438 5.674 0.22 112518. 0.1369 18.62 0.3641 0.4082 0.0152 0.0136 0.056 1.169 0.457 41.484 0.132 2.034 5.001 0.22 112628. 0.1102 19.39 0.3793 0.3617 0.0122 0.0128 0.052 1.100 0.366 39.041 0.124 1.629 4.254 0.22 112742. 0.0839 20.17 0.3944 0.3023 0.0091 0.0119 0.049 1.028 0.275 36.494 0.116 1.223 3.418 0.22 112859. 0.0584 20.95 0.4096 0.2266 0.0061 0.0111 0.045 0.954 0.184 33.847 0.108 0.819 2.467 0.22 112979. 0.0345 21.72 0.4248 0.1296 0.0031 0.0102 0.042 0.876 0.093 31.091 0.099 0.415 1.361 0.22 113101. 0.0135 22.50 0.4399 0.0011 0.0000 0.0092 0.038 0.794 0.001 28.170 0.090 0.003 0.011 0.22 113213. 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 0.0729 0.0216 0.210 3.306 3.904 156.462 0.374 17.366 11.318 0.29 147709. 0.7290 1.03 0.0152 0.0502 0.0713 0.0215 0.210 3.303 3.817 156.332 0.373 16.979 11.075 0.29 147772. 0.7054 2.07 0.0304 0.0983 0.0696 0.0215 0.209 3.298 3.726 156.062 0.373 16.575 10.830 0.29 147838. 0.6815 3.10 0.0455 0.1441 0.0678 0.0214 0.209 3.288 3.631 155.587 0.371 16.152 10.586 0.29 147907. 0.6576 4.14 0.0607 0.1876 0.0660 0.0214 0.208 3.275 3.533 154.970 0.370 15.716 10.341 0.29 147980. 0.6337 5.17 0.0759 0.2290 0.0641 0.0212 0.207 3.258 3.431 154.168 0.368 15.262 10.095 0.29 148055. 0.6096 6.21 0.0911 0.2680 0.0621 0.0211 0.205 3.236 3.325 153.153 0.366 14.790 9.848 0.29 148134. 0.5854 7.24 0.1062 0.3048 0.0601 0.0209 0.204 3.211 3.216 151.951 0.363 14.303 9.598 0.29 148216. 0.5611 8.28 0.1214 0.3392 0.0579 0.0207 0.202 3.180 3.102 150.513 0.359 13.797 9.347 0.29 148301. 0.5366 9.31 0.1366 0.3712 0.0557 0.0205 0.200 3.145 2.984 148.848 0.355 13.273 9.093 0.29 148390. 0.5120 10.35 0.1518 0.4008 0.0535 0.0202 0.197 3.105 2.862 146.932 0.351 12.730 8.835 0.29 148482. 0.4872 11.38 0.1669 0.4277 0.0511 0.0200 0.194 3.059 2.736 144.777 0.346 12.171 8.572 0.29 148578. 0.4622 12.42 0.1821 0.4521 0.0487 0.0196 0.191 3.009 2.607 142.378 0.340 11.596 8.305 0.29 148677. 0.4371 13.45 0.1973 0.4736 0.0462 0.0193 0.187 2.953 2.474 139.730 0.334 11.005 8.031 0.29 148780. 0.4118 14.49 0.2125 0.4922 0.0437 0.0189 0.183 2.891 2.338 136.826 0.327 10.400 7.751 0.29 148886. 0.3863 15.52 0.2276 0.5077 0.0411 0.0184 0.179 2.824 2.199 133.658 0.319 9.780 7.462 0.29 148997. 0.3607 16.56 0.2428 0.5198 0.0384 0.0179 0.175 2.752 2.056 130.222 0.311 9.146 7.162 0.29 149111. 0.3348 17.59 0.2580 0.5283 0.0357 0.0174 0.170 2.673 1.911 126.508 0.302 8.499 6.850 0.29 149229. 0.3087 18.63 0.2732 0.5327 0.0329 0.0169 0.164 2.589 1.762 122.513 0.292 7.838 6.524 0.29 149351. 0.2823 19.66 0.2883 0.5326 0.0301 0.0163 0.159 2.498 1.611 118.229 0.282 7.164 6.179 0.29 149478. 0.2556 20.69 0.3035 0.5274 0.0272 0.0157 0.152 2.402 1.457 113.652 0.271 6.479 5.813 0.29 149608. 0.2287 21.73 0.3187 0.5165 0.0243 0.0150 0.146 2.299 1.300 108.779 0.260 5.784 5.422 0.29 149743. 0.2015 22.76 0.3339 0.4988 0.0213 0.0143 0.139 2.189 1.142 103.609 0.247 5.078 4.998 0.29 149881. 0.1741 23.80 0.3491 0.4731 0.0183 0.0135 0.132 2.074 0.981 98.142 0.234 4.365 4.535 0.29 150025. 0.1464 24.83 0.3642 0.4380 0.0153 0.0127 0.124 1.952 0.819 92.382 0.221 3.645 4.023 0.29 150172. 0.1187 25.87 0.3794 0.3913 0.0123 0.0119 0.116 1.824 0.657 86.340 0.206 2.921 3.450 0.29 150324. 0.0911 26.90 0.3946 0.3304 0.0092 0.0110 0.107 1.691 0.494 80.043 0.191 2.199 2.801 0.29 150480. 0.0642 27.94 0.4098 0.2511 0.0062 0.0101 0.099 1.553 0.332 73.497 0.175 1.478 2.050 0.29 150640. 0.0385 28.97 0.4249 0.1471 0.0032 0.0092 0.089 1.409 0.170 66.685 0.159 0.758 1.159 0.29 150803. 0.0156 30.01 0.4401 0.0051 0.0001 0.0082 0.080 1.256 0.005 59.456 0.142 0.023 0.039 0.29 150950. 0.0001 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 0.0734 0.0213 0.405 5.110 6.139 302.289 0.577 27.308 9.212 0.36 184630. 0.7440 1.32 0.0155 0.0522 0.0717 0.0213 0.405 5.105 5.999 301.976 0.577 26.685 9.011 0.36 184711. 0.7195 2.64 0.0310 0.1021 0.0700 0.0213 0.404 5.095 5.853 301.377 0.576 26.036 8.809 0.36 184796. 0.6948 3.97 0.0466 0.1497 0.0682 0.0212 0.403 5.077 5.700 300.349 0.574 25.354 8.608 0.36 184885. 0.6699 5.29 0.0621 0.1949 0.0663 0.0211 0.401 5.055 5.542 299.024 0.571 24.651 8.406 0.36 184978. 0.6451 6.61 0.0776 0.2378 0.0643 0.0210 0.399 5.026 5.377 297.294 0.568 23.918 8.204 0.36 185076. 0.6201 7.93 0.0931 0.2783 0.0622 0.0208 0.396 4.989 5.206 295.133 0.564 23.156 8.001 0.36 185177. 0.5951 9.26 0.1086 0.3164 0.0601 0.0206 0.392 4.946 5.029 292.559 0.559 22.368 7.796 0.36 185283. 0.5699 10.58 0.1241 0.3521 0.0579 0.0204 0.388 4.894 4.845 289.504 0.553 21.551 7.591 0.36 185393. 0.5447 11.90 0.1397 0.3852 0.0556 0.0202 0.383 4.834 4.654 285.947 0.546 20.702 7.383 0.36 185507. 0.5192 13.22 0.1552 0.4158 0.0533 0.0199 0.378 4.765 4.457 281.876 0.538 19.824 7.171 0.36 185626. 0.4935 14.55 0.1707 0.4437 0.0509 0.0196 0.372 4.688 4.253 277.298 0.530 18.919 6.957 0.36 185750. 0.4677 15.87 0.1862 0.4688 0.0484 0.0192 0.365 4.601 4.044 272.204 0.520 17.988 6.739 0.36 185878. 0.4417 17.19 0.2017 0.4910 0.0458 0.0188 0.357 4.506 3.829 266.582 0.509 17.032 6.515 0.36 186011. 0.4156 18.51 0.2172 0.5102 0.0432 0.0184 0.349 4.402 3.609 260.416 0.497 16.053 6.286 0.36 186149. 0.3893 19.84 0.2328 0.5260 0.0405 0.0179 0.340 4.289 3.383 253.692 0.485 15.049 6.049 0.36 186292. 0.3627 21.16 0.2483 0.5383 0.0377 0.0174 0.330 4.165 3.153 246.395 0.471 14.023 5.803 0.36 186440. 0.3359 22.48 0.2638 0.5467 0.0349 0.0168 0.320 4.032 2.917 238.512 0.456 12.975 5.547 0.36 186593. 0.3088 23.80 0.2793 0.5507 0.0320 0.0162 0.308 3.888 2.676 230.027 0.439 11.905 5.278 0.36 186751. 0.2815 25.13 0.2948 0.5499 0.0291 0.0156 0.296 3.735 2.432 220.932 0.422 10.816 4.992 0.36 186915. 0.2537 26.45 0.3103 0.5434 0.0261 0.0149 0.283 3.571 2.182 211.218 0.403 9.708 4.687 0.36 187084. 0.2257 27.77 0.3259 0.5305 0.0231 0.0142 0.269 3.396 1.930 200.878 0.384 8.583 4.357 0.36 187259. 0.1973 29.09 0.3414 0.5098 0.0200 0.0134 0.255 3.210 1.673 189.911 0.363 7.444 3.997 0.36 187439. 0.1685 30.42 0.3569 0.4798 0.0169 0.0126 0.239 3.014 1.415 178.323 0.341 6.292 3.598 0.36 187625. 0.1395 31.74 0.3724 0.4384 0.0138 0.0117 0.223 2.808 1.154 166.129 0.317 5.133 3.151 0.36 187816. 0.1103 33.06 0.3879 0.3827 0.0107 0.0108 0.206 2.593 0.893 153.368 0.293 3.971 2.640 0.36 188014. 0.0813 34.38 0.4034 0.3087 0.0076 0.0099 0.188 2.368 0.633 140.096 0.268 2.814 2.048 0.36 188216. 0.0531 35.71 0.4190 0.2095 0.0045 0.0089 0.169 2.135 0.373 126.275 0.241 1.657 1.338 0.36 188423. 0.0266 37.03 0.4345 0.0735 0.0013 0.0079 0.150 1.890 0.112 111.825 0.214 0.496 0.453 0.36 188628. 0.0049 38.35 0.4500 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 0.0212 0.698 7.329 8.911 520.247 0.828 39.636 7.769 0.43 221547. 0.7560 1.59 0.0155 0.0530 0.0723 0.0212 0.697 7.319 8.707 519.590 0.827 38.729 7.601 0.43 221645. 0.7311 3.18 0.0311 0.1036 0.0705 0.0212 0.695 7.303 8.495 518.452 0.825 37.785 7.432 0.43 221748. 0.7061 4.77 0.0466 0.1519 0.0687 0.0211 0.693 7.277 8.272 516.546 0.822 36.792 7.263 0.43 221856. 0.6809 6.36 0.0622 0.1979 0.0668 0.0210 0.689 7.242 8.041 514.093 0.818 35.769 7.095 0.43 221968. 0.6558 7.95 0.0777 0.2414 0.0648 0.0209 0.685 7.198 7.802 510.941 0.813 34.702 6.926 0.43 222086. 0.6306 9.54 0.0933 0.2826 0.0627 0.0207 0.680 7.142 7.553 507.007 0.807 33.594 6.757 0.43 222208. 0.6053 11.13 0.1088 0.3214 0.0606 0.0205 0.674 7.077 7.295 502.345 0.800 32.447 6.586 0.43 222336. 0.5799 12.72 0.1244 0.3578 0.0583 0.0203 0.666 6.999 7.027 496.824 0.791 31.257 6.415 0.43 222469. 0.5544 14.31 0.1399 0.3917 0.0560 0.0200 0.658 6.908 6.749 490.413 0.781 30.022 6.242 0.43 222607. 0.5287 15.90 0.1555 0.4230 0.0537 0.0197 0.648 6.805 6.462 483.085 0.769 28.743 6.067 0.43 222750. 0.5028 17.49 0.1710 0.4517 0.0512 0.0194 0.637 6.689 6.166 474.855 0.756 27.426 5.890 0.43 222899. 0.4767 19.08 0.1866 0.4776 0.0487 0.0190 0.625 6.560 5.861 465.706 0.741 26.072 5.709 0.43 223054. 0.4505 20.67 0.2021 0.5007 0.0461 0.0186 0.611 6.418 5.549 455.616 0.725 24.681 5.524 0.43 223215. 0.4242 22.26 0.2177 0.5207 0.0434 0.0182 0.596 6.263 5.228 444.557 0.708 23.255 5.334 0.43 223381. 0.3976 23.85 0.2332 0.5374 0.0407 0.0177 0.580 6.093 4.900 432.502 0.688 21.795 5.139 0.43 223554. 0.3708 25.45 0.2488 0.5506 0.0379 0.0171 0.562 5.909 4.564 419.428 0.668 20.302 4.936 0.43 223732. 0.3437 27.04 0.2643 0.5599 0.0351 0.0165 0.544 5.710 4.221 405.308 0.645 18.776 4.724 0.43 223917. 0.3164 28.63 0.2799 0.5649 0.0321 0.0159 0.523 5.496 3.871 390.120 0.621 17.220 4.501 0.43 224108. 0.2887 30.22 0.2954 0.5649 0.0292 0.0153 0.501 5.266 3.515 373.843 0.595 15.636 4.265 0.43 224305. 0.2607 31.81 0.3110 0.5594 0.0262 0.0146 0.478 5.022 3.153 356.464 0.567 14.024 4.012 0.43 224509. 0.2322 33.40 0.3265 0.5472 0.0231 0.0138 0.453 4.761 2.785 337.973 0.538 12.388 3.738 0.43 224719. 0.2033 34.99 0.3421 0.5272 0.0200 0.0130 0.427 4.485 2.413 318.368 0.507 10.731 3.437 0.43 224937. 0.1740 36.58 0.3576 0.4976 0.0169 0.0122 0.399 4.193 2.036 297.660 0.474 9.058 3.103 0.43 225161. 0.1443 38.17 0.3732 0.4560 0.0138 0.0113 0.370 3.886 1.657 275.878 0.439 7.372 2.725 0.43 225391. 0.1144 39.76 0.3887 0.3992 0.0106 0.0103 0.339 3.565 1.278 253.095 0.403 5.684 2.290 0.43 225629. 0.0844 41.35 0.4043 0.3225 0.0075 0.0094 0.308 3.232 0.900 229.407 0.365 4.002 1.779 0.43 225873. 0.0550 42.94 0.4198 0.2177 0.0043 0.0084 0.275 2.884 0.522 204.743 0.326 2.322 1.156 0.43 226122. 0.0272 44.53 0.4354 0.0704 0.0012 0.0073 0.240 2.521 0.142 178.927 0.285 0.633 0.361 0.43 226367. 0.0044 46.12 0.4509 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 0.0747 0.0213 1.109 9.990 12.247 827.318 1.129 54.473 6.714 0.50 258458. 0.7659 1.84 0.0154 0.0530 0.0730 0.0212 1.108 9.974 11.968 826.057 1.127 53.234 6.571 0.50 258573. 0.7411 3.68 0.0308 0.1037 0.0712 0.0212 1.105 9.951 11.679 824.092 1.124 51.949 6.428 0.50 258692. 0.7161 5.52 0.0463 0.1521 0.0694 0.0211 1.101 9.912 11.375 820.880 1.120 50.597 6.285 0.50 258818. 0.6910 7.36 0.0617 0.1982 0.0675 0.0210 1.095 9.862 11.061 816.749 1.114 49.201 6.143 0.50 258948. 0.6660 9.20 0.0771 0.2420 0.0655 0.0209 1.088 9.799 10.735 811.569 1.107 47.751 6.000 0.50 259085. 0.6408 11.04 0.0925 0.2834 0.0634 0.0207 1.080 9.721 10.396 805.092 1.098 46.241 5.857 0.50 259227. 0.6156 12.88 0.1079 0.3226 0.0613 0.0205 1.069 9.629 10.045 797.488 1.088 44.682 5.713 0.50 259374. 0.5903 14.72 0.1233 0.3593 0.0591 0.0203 1.057 9.521 9.681 788.482 1.076 43.062 5.569 0.50 259529. 0.5649 16.56 0.1388 0.3937 0.0568 0.0200 1.043 9.395 9.304 778.097 1.061 41.384 5.424 0.50 259689. 0.5393 18.40 0.1542 0.4255 0.0544 0.0197 1.028 9.252 8.913 766.226 1.045 39.646 5.276 0.50 259855. 0.5135 20.24 0.1696 0.4549 0.0519 0.0194 1.010 9.091 8.511 752.914 1.027 37.855 5.127 0.50 260027. 0.4876 22.08 0.1850 0.4815 0.0494 0.0190 0.990 8.913 8.097 738.138 1.007 36.014 4.975 0.50 260206. 0.4615 23.92 0.2004 0.5054 0.0468 0.0186 0.968 8.716 7.672 721.861 0.985 34.124 4.820 0.50 260392. 0.4352 25.76 0.2159 0.5264 0.0441 0.0181 0.944 8.501 7.236 704.040 0.960 32.186 4.662 0.50 260584. 0.4088 27.60 0.2313 0.5442 0.0414 0.0176 0.918 8.267 6.790 684.636 0.934 30.202 4.498 0.50 260783. 0.3821 29.44 0.2467 0.5586 0.0386 0.0171 0.890 8.013 6.334 663.608 0.905 28.173 4.329 0.50 260989. 0.3552 31.28 0.2621 0.5694 0.0358 0.0165 0.859 7.739 5.868 640.917 0.874 26.101 4.153 0.50 261202. 0.3279 33.12 0.2775 0.5760 0.0329 0.0159 0.827 7.444 5.393 616.526 0.841 23.987 3.967 0.50 261423. 0.3003 34.95 0.2930 0.5779 0.0299 0.0152 0.792 7.129 4.909 590.403 0.805 21.834 3.771 0.50 261650. 0.2723 36.79 0.3084 0.5744 0.0269 0.0145 0.754 6.792 4.416 562.526 0.767 19.644 3.561 0.50 261885. 0.2439 38.63 0.3238 0.5646 0.0239 0.0137 0.715 6.434 3.917 532.877 0.727 17.421 3.334 0.50 262127. 0.2151 40.47 0.3392 0.5473 0.0208 0.0129 0.672 6.055 3.410 501.452 0.684 15.169 3.085 0.50 262378. 0.1857 42.31 0.3546 0.5208 0.0177 0.0120 0.628 5.654 2.899 468.265 0.639 12.893 2.808 0.50 262635. 0.1558 44.15 0.3700 0.4828 0.0145 0.0111 0.581 5.233 2.383 433.355 0.591 10.600 2.494 0.50 262901. 0.1255 45.99 0.3855 0.4301 0.0114 0.0102 0.532 4.791 1.866 396.819 0.541 8.300 2.133 0.50 263174. 0.0950 47.83 0.4009 0.3580 0.0082 0.0092 0.481 4.333 1.351 358.834 0.490 6.008 1.707 0.50 263455. 0.0647 49.67 0.4163 0.2586 0.0051 0.0082 0.428 3.856 0.836 319.319 0.436 3.718 1.187 0.50 263743. 0.0354 51.51 0.4317 0.1181 0.0020 0.0072 0.373 3.358 0.321 278.138 0.379 1.426 0.523 0.50 264030. 0.0096 53.35 0.4471 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 0.0756 0.0214 1.667 13.131 16.183 1242.853 1.484 71.982 5.906 0.57 295363. 0.7745 2.07 0.0152 0.0526 0.0739 0.0214 1.664 13.107 15.819 1240.599 1.481 70.364 5.784 0.57 295492. 0.7499 4.15 0.0304 0.1029 0.0721 0.0213 1.659 13.073 15.443 1237.384 1.477 68.692 5.661 0.57 295628. 0.7252 6.22 0.0456 0.1510 0.0703 0.0212 1.653 13.020 15.048 1232.311 1.471 66.933 5.539 0.57 295770. 0.7004 8.29 0.0608 0.1969 0.0684 0.0211 1.644 12.951 14.639 1225.781 1.463 65.113 5.417 0.57 295918. 0.6756 10.36 0.0760 0.2406 0.0664 0.0210 1.633 12.867 14.215 1217.816 1.454 63.230 5.294 0.57 296072. 0.6507 12.44 0.0912 0.2820 0.0643 0.0208 1.620 12.761 13.774 1207.848 1.442 61.266 5.172 0.57 296232. 0.6258 14.51 0.1064 0.3212 0.0622 0.0206 1.604 12.639 13.319 1196.259 1.428 59.241 5.050 0.57 296399. 0.6008 16.58 0.1216 0.3582 0.0600 0.0204 1.586 12.494 12.845 1182.536 1.412 57.135 4.927 0.57 296573. 0.5756 18.66 0.1368 0.3928 0.0577 0.0201 1.565 12.328 12.356 1166.855 1.393 54.960 4.803 0.57 296754. 0.5504 20.73 0.1520 0.4251 0.0553 0.0198 1.541 12.139 11.849 1148.933 1.371 52.704 4.678 0.57 296941. 0.5249 22.80 0.1672 0.4549 0.0529 0.0194 1.514 11.927 11.326 1128.873 1.347 50.380 4.551 0.57 297135. 0.4993 24.87 0.1824 0.4822 0.0504 0.0191 1.484 11.692 10.789 1106.643 1.321 47.991 4.422 0.57 297336. 0.4735 26.95 0.1976 0.5069 0.0478 0.0186 1.451 11.434 10.238 1082.196 1.292 45.539 4.291 0.57 297545. 0.4476 29.02 0.2128 0.5288 0.0452 0.0182 1.415 11.151 9.673 1055.473 1.260 43.025 4.157 0.57 297761. 0.4214 31.09 0.2280 0.5478 0.0425 0.0177 1.376 10.844 9.094 1026.416 1.225 40.452 4.019 0.57 297984. 0.3951 33.17 0.2432 0.5636 0.0397 0.0171 1.334 10.512 8.503 994.963 1.188 37.821 3.876 0.57 298215. 0.3684 35.24 0.2584 0.5759 0.0369 0.0166 1.289 10.154 7.899 961.060 1.147 35.133 3.728 0.57 298454. 0.3415 37.31 0.2736 0.5843 0.0340 0.0159 1.240 9.769 7.282 924.653 1.104 32.393 3.572 0.57 298701. 0.3143 39.38 0.2888 0.5884 0.0311 0.0153 1.188 9.358 6.655 885.695 1.057 29.601 3.408 0.57 298956. 0.2866 41.46 0.3040 0.5875 0.0281 0.0145 1.132 8.919 6.016 844.150 1.008 26.761 3.233 0.57 299218. 0.2585 43.53 0.3192 0.5808 0.0251 0.0138 1.073 8.452 5.368 799.989 0.955 23.877 3.044 0.57 299490. 0.2299 45.60 0.3344 0.5672 0.0220 0.0130 1.010 7.958 4.711 753.203 0.899 20.954 2.837 0.57 299769. 0.2007 47.68 0.3496 0.5451 0.0189 0.0121 0.944 7.436 4.046 703.803 0.840 17.999 2.608 0.57 300057. 0.1710 49.75 0.3648 0.5124 0.0158 0.0112 0.874 6.887 3.376 651.833 0.778 15.018 2.349 0.58 300354. 0.1407 51.82 0.3800 0.4662 0.0126 0.0103 0.801 6.312 2.703 597.400 0.713 12.023 2.052 0.58 300659. 0.1100 53.89 0.3952 0.4024 0.0095 0.0093 0.725 5.713 2.031 540.746 0.645 9.032 1.703 0.58 300973. 0.0791 55.97 0.4104 0.3140 0.0064 0.0083 0.646 5.092 1.360 481.915 0.575 6.049 1.280 0.58 301294. 0.0487 58.04 0.4256 0.1892 0.0032 0.0072 0.564 4.446 0.690 420.769 0.502 3.068 0.744 0.58 301620. 0.0201 60.11 0.4408 -0.0009 0.0000 0.0061 0.476 3.753 -0.003 355.180 0.424 -0.011 -0.003 0.58 301890. 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 0.0766 0.0217 2.400 16.808 20.770 1789.734 1.899 92.386 5.264 0.64 332258. 0.7820 2.37 0.0155 0.0536 0.0749 0.0216 2.395 16.771 20.293 1785.753 1.895 90.265 5.154 0.64 332408. 0.7569 4.75 0.0309 0.1050 0.0731 0.0215 2.388 16.720 19.802 1780.363 1.889 88.077 5.045 0.64 332565. 0.7318 7.12 0.0464 0.1541 0.0712 0.0214 2.377 16.643 19.284 1772.196 1.880 85.773 4.935 0.64 332729. 0.7065 9.50 0.0619 0.2009 0.0692 0.0213 2.363 16.545 18.747 1761.747 1.869 83.387 4.827 0.64 332900. 0.6812 11.87 0.0774 0.2455 0.0671 0.0212 2.346 16.427 18.192 1749.116 1.856 80.919 4.717 0.64 333078. 0.6559 14.24 0.0928 0.2877 0.0650 0.0210 2.325 16.280 17.613 1733.463 1.839 78.341 4.608 0.64 333264. 0.6305 16.62 0.1083 0.3277 0.0628 0.0208 2.300 16.109 17.015 1715.300 1.820 75.682 4.499 0.64 333458. 0.6050 18.99 0.1238 0.3654 0.0605 0.0205 2.272 15.908 16.393 1693.942 1.797 72.918 4.389 0.64 333659. 0.5794 21.36 0.1393 0.4008 0.0581 0.0202 2.239 15.679 15.750 1669.537 1.771 70.057 4.279 0.64 333868. 0.5536 23.74 0.1547 0.4337 0.0557 0.0199 2.202 15.419 15.084 1641.777 1.742 67.092 4.167 0.64 334085. 0.5276 26.11 0.1702 0.4641 0.0531 0.0195 2.160 15.127 14.397 1610.776 1.709 64.038 4.054 0.64 334310. 0.5014 28.49 0.1857 0.4919 0.0505 0.0191 2.114 14.805 13.691 1576.487 1.673 60.897 3.939 0.64 334543. 0.4751 30.86 0.2012 0.5170 0.0478 0.0186 2.064 14.452 12.966 1538.834 1.633 57.674 3.822 0.64 334785. 0.4486 33.23 0.2166 0.5393 0.0451 0.0181 2.008 14.066 12.223 1497.729 1.589 54.369 3.702 0.64 335036. 0.4219 35.61 0.2321 0.5585 0.0423 0.0176 1.949 13.646 11.463 1453.083 1.542 50.986 3.578 0.64 335295. 0.3949 37.98 0.2476 0.5744 0.0394 0.0170 1.884 13.193 10.685 1404.809 1.491 47.527 3.450 0.64 335563. 0.3676 40.35 0.2630 0.5867 0.0365 0.0164 1.814 12.705 9.891 1352.823 1.435 43.994 3.316 0.64 335840. 0.3400 42.73 0.2785 0.5948 0.0335 0.0157 1.739 12.181 9.081 1297.047 1.376 40.391 3.175 0.65 336126. 0.3119 45.10 0.2940 0.5983 0.0305 0.0150 1.659 11.621 8.256 1237.418 1.313 36.721 3.026 0.65 336421. 0.2834 47.48 0.3095 0.5964 0.0274 0.0142 1.574 11.024 7.417 1173.882 1.246 32.990 2.866 0.65 336726. 0.2544 49.85 0.3249 0.5882 0.0242 0.0134 1.484 10.391 6.565 1106.410 1.174 29.202 2.691 0.65 337041. 0.2248 52.22 0.3404 0.5722 0.0210 0.0125 1.388 9.720 5.703 1034.998 1.098 25.366 2.499 0.65 337365. 0.1945 54.60 0.3559 0.5465 0.0178 0.0116 1.287 9.013 4.831 959.681 1.018 21.489 2.283 0.65 337699. 0.1636 56.97 0.3714 0.5086 0.0146 0.0107 1.181 8.270 3.953 880.560 0.934 17.584 2.036 0.65 338043. 0.1320 59.34 0.3868 0.4545 0.0113 0.0097 1.070 7.493 3.073 797.869 0.847 13.670 1.747 0.65 338398. 0.0998 61.72 0.4023 0.3785 0.0081 0.0086 0.955 6.687 2.196 711.994 0.755 9.768 1.399 0.65 338762. 0.0676 64.09 0.4178 0.2701 0.0049 0.0075 0.835 5.848 1.320 622.722 0.661 5.871 0.961 0.65 339134. 0.0360 66.47 0.4333 0.1101 0.0016 0.0064 0.710 4.974 0.441 529.628 0.562 1.962 0.378 0.65 339501. 0.0082 68.84 0.4487 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 0.0779 0.0220 3.348 21.101 26.077 2496.483 2.384 115.990 4.738 0.71 369140. 0.7887 2.59 0.0152 0.0528 0.0762 0.0220 3.339 21.046 25.487 2489.951 2.378 113.367 4.643 0.71 369306. 0.7641 5.18 0.0304 0.1034 0.0744 0.0219 3.328 20.975 24.880 2481.550 2.370 110.667 4.548 0.71 369479. 0.7394 7.78 0.0456 0.1518 0.0725 0.0218 3.312 20.873 24.242 2469.536 2.358 107.830 4.453 0.71 369660. 0.7146 10.37 0.0608 0.1981 0.0705 0.0216 3.291 20.743 23.580 2454.162 2.344 104.884 4.358 0.71 369848. 0.6898 12.96 0.0760 0.2422 0.0684 0.0215 3.267 20.590 22.898 2436.007 2.326 101.848 4.263 0.71 370044. 0.6650 15.55 0.0912 0.2842 0.0663 0.0213 3.237 20.401 22.184 2413.654 2.305 98.674 4.169 0.71 370248. 0.6401 18.15 0.1065 0.3241 0.0641 0.0211 3.202 20.183 21.449 2387.936 2.280 95.405 4.074 0.71 370460. 0.6151 20.74 0.1217 0.3617 0.0618 0.0208 3.162 19.929 20.684 2357.822 2.252 92.002 3.979 0.71 370681. 0.5899 23.33 0.1369 0.3972 0.0595 0.0205 3.116 19.641 19.895 2323.715 2.219 88.492 3.883 0.71 370909. 0.5646 25.92 0.1521 0.4303 0.0570 0.0202 3.064 19.313 19.076 2284.987 2.182 84.849 3.787 0.71 371146. 0.5391 28.51 0.1673 0.4611 0.0545 0.0198 3.006 18.949 18.232 2241.849 2.141 81.096 3.689 0.72 371392. 0.5134 31.11 0.1825 0.4895 0.0519 0.0194 2.943 18.546 17.365 2194.265 2.095 77.238 3.589 0.72 371647. 0.4876 33.70 0.1977 0.5153 0.0492 0.0189 2.873 18.106 16.475 2142.140 2.046 73.279 3.488 0.72 371910. 0.4615 36.29 0.2129 0.5385 0.0465 0.0184 2.797 17.626 15.562 2085.361 1.991 69.222 3.385 0.72 372183. 0.4353 38.88 0.2281 0.5589 0.0437 0.0178 2.714 17.106 14.629 2023.818 1.933 65.069 3.279 0.72 372465. 0.4088 41.47 0.2433 0.5761 0.0409 0.0173 2.625 16.544 13.674 1957.395 1.869 60.822 3.169 0.72 372756. 0.3819 44.07 0.2585 0.5900 0.0380 0.0166 2.529 15.941 12.699 1885.987 1.801 56.486 3.054 0.72 373057. 0.3548 46.66 0.2737 0.6001 0.0350 0.0160 2.427 15.294 11.705 1809.502 1.728 52.063 2.934 0.72 373367. 0.3272 49.25 0.2889 0.6060 0.0320 0.0152 2.317 14.604 10.692 1727.859 1.650 47.559 2.807 0.72 373688. 0.2992 51.84 0.3041 0.6070 0.0289 0.0145 2.201 13.870 9.662 1641.002 1.567 42.977 2.671 0.72 374018. 0.2706 54.44 0.3194 0.6021 0.0258 0.0137 2.077 13.092 8.616 1548.901 1.479 38.325 2.523 0.72 374359. 0.2414 57.03 0.3346 0.5903 0.0226 0.0128 1.947 12.269 7.556 1451.562 1.386 33.610 2.361 0.72 374710. 0.2116 59.62 0.3498 0.5698 0.0194 0.0119 1.809 11.402 6.484 1349.049 1.288 28.842 2.180 0.72 375071. 0.1810 62.21 0.3650 0.5384 0.0162 0.0109 1.665 10.493 5.403 1241.501 1.186 24.033 1.974 0.72 375443. 0.1496 64.80 0.3802 0.4926 0.0129 0.0100 1.514 9.544 4.317 1129.196 1.078 19.201 1.734 0.72 375826. 0.1174 67.40 0.3954 0.4277 0.0097 0.0089 1.358 8.560 3.232 1012.710 0.967 14.375 1.447 0.72 376219. 0.0848 69.99 0.4106 0.3352 0.0064 0.0079 1.196 7.541 2.149 892.204 0.852 9.560 1.093 0.72 376622. 0.0522 72.58 0.4258 0.2007 0.0032 0.0068 1.029 6.487 1.067 767.510 0.733 4.748 0.631 0.72 377030. 0.0212 75.17 0.4410 -0.0160 -0.0002 0.0056 0.848 5.342 -0.068 632.007 0.604 -0.301 -0.049 0.72 377320. 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 0.0796 0.0226 4.566 26.162 32.202 3404.852 2.956 143.237 4.290 0.79 406007. 0.7935 2.88 0.0153 0.0530 0.0777 0.0225 4.550 26.073 31.466 3393.235 2.946 139.961 4.206 0.79 406193. 0.7691 5.75 0.0307 0.1039 0.0759 0.0224 4.531 25.964 30.708 3379.014 2.933 136.590 4.122 0.79 406388. 0.7446 8.63 0.0460 0.1527 0.0739 0.0223 4.506 25.820 29.914 3360.269 2.917 133.058 4.038 0.79 406591. 0.7199 11.50 0.0613 0.1994 0.0719 0.0221 4.475 25.638 29.087 3336.670 2.897 129.378 3.954 0.79 406802. 0.6951 14.38 0.0767 0.2439 0.0698 0.0219 4.438 25.428 28.235 3309.283 2.873 125.589 3.870 0.79 407022. 0.6703 17.25 0.0920 0.2863 0.0676 0.0217 4.393 25.174 27.344 3276.170 2.844 121.626 3.786 0.79 407252. 0.6453 20.13 0.1073 0.3266 0.0653 0.0215 4.343 24.883 26.426 3238.391 2.811 117.542 3.701 0.79 407490. 0.6202 23.00 0.1227 0.3647 0.0629 0.0212 4.284 24.547 25.470 3194.578 2.773 113.291 3.616 0.79 407737. 0.5949 25.88 0.1380 0.4005 0.0605 0.0208 4.218 24.168 24.484 3145.234 2.730 108.904 3.531 0.79 407994. 0.5695 28.75 0.1533 0.4341 0.0580 0.0205 4.143 23.740 23.460 3089.587 2.682 104.352 3.444 0.79 408260. 0.5438 31.63 0.1687 0.4654 0.0554 0.0201 4.061 23.266 22.406 3027.933 2.629 99.661 3.356 0.79 408536. 0.5179 34.50 0.1840 0.4942 0.0527 0.0196 3.970 22.746 21.322 2960.240 2.570 94.840 3.267 0.79 408821. 0.4918 37.38 0.1993 0.5204 0.0499 0.0191 3.871 22.179 20.209 2886.428 2.506 89.892 3.176 0.79 409116. 0.4654 40.25 0.2147 0.5439 0.0471 0.0186 3.763 21.564 19.069 2806.418 2.436 84.820 3.082 0.79 409422. 0.4387 43.13 0.2300 0.5644 0.0442 0.0180 3.648 20.901 17.902 2720.124 2.361 79.629 2.985 0.79 409737. 0.4117 46.00 0.2454 0.5817 0.0413 0.0174 3.523 20.189 16.709 2627.457 2.281 74.321 2.884 0.79 410064. 0.3843 48.88 0.2607 0.5954 0.0383 0.0168 3.391 19.428 15.490 2528.369 2.195 68.900 2.779 0.79 410400. 0.3565 51.75 0.2760 0.6051 0.0352 0.0161 3.249 18.617 14.247 2422.843 2.103 63.372 2.667 0.79 410748. 0.3282 54.63 0.2914 0.6102 0.0321 0.0153 3.099 17.757 12.982 2310.916 2.006 57.742 2.548 0.79 411106. 0.2993 57.50 0.3067 0.6098 0.0289 0.0145 2.940 16.848 11.694 2192.655 1.903 52.016 2.419 0.79 411476. 0.2697 60.38 0.3220 0.6030 0.0257 0.0137 2.774 15.892 10.387 2068.200 1.795 46.201 2.278 0.79 411857. 0.2393 63.25 0.3374 0.5882 0.0224 0.0128 2.599 14.890 9.062 1937.772 1.682 40.309 2.121 0.79 412249. 0.2082 66.13 0.3527 0.5636 0.0191 0.0119 2.416 13.844 7.723 1801.689 1.564 34.351 1.944 0.79 412653. 0.1761 69.00 0.3680 0.5266 0.0157 0.0110 2.227 12.758 6.372 1660.401 1.441 28.344 1.741 0.79 413069. 0.1432 71.88 0.3834 0.4734 0.0124 0.0100 2.031 11.638 5.016 1514.595 1.315 22.313 1.502 0.79 413497. 0.1097 74.76 0.3987 0.3988 0.0090 0.0090 1.831 10.491 3.663 1365.367 1.185 16.294 1.217 0.79 413936. 0.0759 77.63 0.4140 0.2941 0.0057 0.0080 1.626 9.319 2.311 1212.862 1.053 10.280 0.864 0.79 414385. 0.0428 80.51 0.4294 0.1452 0.0024 0.0070 1.417 8.121 0.958 1056.834 0.917 4.263 0.411 0.79 414835. 0.0131 83.38 0.4447 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 0.0816 0.0238 6.263 32.898 39.290 4670.684 3.717 174.761 3.815 0.86 442848. 0.7796 3.15 0.0154 0.0518 0.0797 0.0237 6.222 32.682 38.389 4639.944 3.692 170.754 3.753 0.86 443056. 0.7579 6.30 0.0308 0.1018 0.0778 0.0235 6.177 32.443 37.460 4606.022 3.665 166.621 3.689 0.86 443273. 0.7360 9.45 0.0462 0.1500 0.0758 0.0233 6.125 32.172 36.492 4567.616 3.635 162.316 3.624 0.86 443498. 0.7136 12.59 0.0616 0.1964 0.0736 0.0231 6.065 31.858 35.479 4523.024 3.599 157.812 3.558 0.86 443734. 0.6908 15.74 0.0770 0.2409 0.0715 0.0228 6.000 31.513 34.437 4474.095 3.560 153.176 3.491 0.86 443978. 0.6678 18.89 0.0924 0.2835 0.0692 0.0226 5.925 31.121 33.347 4418.422 3.516 148.328 3.423 0.86 444233. 0.6444 22.04 0.1077 0.3241 0.0669 0.0222 5.843 30.690 32.223 4357.132 3.467 143.328 3.354 0.86 444497. 0.6207 25.19 0.1231 0.3625 0.0645 0.0219 5.754 30.220 31.053 4290.429 3.414 138.123 3.283 0.86 444771. 0.5963 28.34 0.1385 0.3986 0.0620 0.0215 5.658 29.716 29.845 4218.862 3.357 132.752 3.209 0.86 445056. 0.5714 31.48 0.1539 0.4323 0.0594 0.0211 5.553 29.164 28.592 4140.560 3.295 127.175 3.132 0.86 445351. 0.5459 34.63 0.1693 0.4633 0.0567 0.0207 5.442 28.581 27.299 4057.807 3.229 121.428 3.051 0.86 445656. 0.5197 37.78 0.1847 0.4914 0.0539 0.0203 5.324 27.964 25.971 3970.127 3.159 115.519 2.967 0.86 445972. 0.4929 40.93 0.2001 0.5168 0.0511 0.0198 5.197 27.298 24.608 3875.541 3.084 109.455 2.880 0.86 446299. 0.4657 44.08 0.2155 0.5390 0.0482 0.0193 5.061 26.583 23.210 3774.142 3.003 103.240 2.789 0.86 446636. 0.4381 47.23 0.2309 0.5579 0.0452 0.0187 4.916 25.822 21.780 3666.116 2.917 96.878 2.695 0.86 446985. 0.4099 50.37 0.2463 0.5730 0.0422 0.0181 4.763 25.019 20.318 3551.985 2.827 90.375 2.595 0.86 447345. 0.3812 53.52 0.2617 0.5838 0.0391 0.0175 4.602 24.170 18.825 3431.585 2.731 83.734 2.488 0.86 447717. 0.3519 56.67 0.2771 0.5899 0.0359 0.0169 4.432 23.280 17.303 3305.196 2.630 76.962 2.374 0.86 448100. 0.3220 59.82 0.2925 0.5905 0.0327 0.0162 4.255 22.350 15.752 3173.171 2.525 70.065 2.252 0.86 448496. 0.2913 62.97 0.3078 0.5846 0.0294 0.0155 4.071 21.385 14.175 3036.052 2.416 63.052 2.118 0.86 448903. 0.2599 66.12 0.3232 0.5712 0.0261 0.0148 3.881 20.386 12.575 2894.348 2.303 55.932 1.971 0.86 449323. 0.2278 69.27 0.3386 0.5488 0.0227 0.0140 3.686 19.360 10.953 2748.604 2.187 48.717 1.807 0.86 449755. 0.1950 72.41 0.3540 0.5158 0.0193 0.0133 3.486 18.310 9.313 2599.579 2.069 41.424 1.625 0.86 450199. 0.1616 75.56 0.3694 0.4701 0.0159 0.0125 3.283 17.244 7.660 2448.236 1.948 34.072 1.419 0.86 450657. 0.1280 78.71 0.3848 0.4091 0.0125 0.0117 3.079 16.170 6.001 2295.782 1.827 26.694 1.186 0.86 451127. 0.0947 81.86 0.4002 0.3300 0.0090 0.0109 2.875 15.101 4.346 2143.893 1.706 19.332 0.919 0.86 451610. 0.0625 85.01 0.4156 0.2284 0.0056 0.0102 2.672 14.035 2.692 1992.661 1.586 11.975 0.613 0.86 452104. 0.0328 88.16 0.4310 0.0986 0.0022 0.0094 2.469 12.967 1.036 1840.931 1.465 4.607 0.255 0.86 452597. 0.0085 91.30 0.4464 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 0.0837 0.0271 9.064 43.947 47.327 6759.310 4.965 210.511 3.176 0.93 479669. 0.7122 3.39 0.0153 0.0467 0.0818 0.0268 8.957 43.426 46.267 6679.214 4.906 205.795 3.142 0.93 479896. 0.6967 6.79 0.0306 0.0924 0.0799 0.0265 8.844 42.877 45.168 6594.643 4.844 200.908 3.107 0.93 480132. 0.6806 10.18 0.0459 0.1370 0.0779 0.0261 8.725 42.300 44.031 6506.002 4.779 195.849 3.070 0.93 480379. 0.6640 13.58 0.0613 0.1804 0.0758 0.0257 8.596 41.674 42.836 6409.692 4.708 190.534 3.031 0.93 480636. 0.6467 16.97 0.0766 0.2225 0.0736 0.0253 8.460 41.015 41.603 6308.334 4.634 185.052 2.991 0.93 480902. 0.6289 20.36 0.0919 0.2633 0.0713 0.0249 8.314 40.310 40.317 6199.897 4.554 179.330 2.949 0.93 481180. 0.6105 23.76 0.1072 0.3027 0.0690 0.0244 8.160 39.562 38.986 6084.789 4.470 173.410 2.906 0.93 481468. 0.5915 27.15 0.1225 0.3405 0.0665 0.0239 7.995 38.763 37.602 5961.909 4.379 167.253 2.861 0.93 481767. 0.5718 30.55 0.1378 0.3766 0.0640 0.0234 7.823 37.929 36.173 5833.720 4.285 160.896 2.812 0.93 482076. 0.5514 33.94 0.1532 0.4103 0.0614 0.0229 7.651 37.094 34.687 5705.328 4.191 154.288 2.758 0.93 482397. 0.5294 37.33 0.1685 0.4413 0.0586 0.0224 7.479 36.260 33.155 5576.923 4.097 147.473 2.696 0.93 482729. 0.5061 40.73 0.1838 0.4690 0.0559 0.0219 7.312 35.453 31.579 5452.923 4.006 140.462 2.627 0.93 483072. 0.4812 44.12 0.1991 0.4911 0.0530 0.0215 7.177 34.795 29.958 5351.665 3.931 133.254 2.539 0.93 483426. 0.4530 47.52 0.2144 0.5092 0.0501 0.0211 7.041 34.139 28.297 5250.734 3.857 125.865 2.444 0.93 483793. 0.4239 50.91 0.2297 0.5233 0.0470 0.0207 6.900 33.453 26.597 5145.284 3.780 118.303 2.345 0.93 484171. 0.3942 54.30 0.2451 0.5330 0.0440 0.0202 6.753 32.742 24.859 5035.847 3.699 110.573 2.239 0.93 484561. 0.3639 57.70 0.2604 0.5379 0.0408 0.0198 6.602 32.011 23.085 4923.461 3.617 102.683 2.127 0.93 484963. 0.3331 61.09 0.2757 0.5374 0.0376 0.0193 6.450 31.271 21.277 4809.679 3.533 94.639 2.006 0.93 485377. 0.3017 64.49 0.2910 0.5309 0.0344 0.0188 6.295 30.520 19.436 4694.100 3.448 86.453 1.878 0.93 485804. 0.2699 67.88 0.3063 0.5180 0.0311 0.0184 6.139 29.762 17.566 4577.568 3.363 78.135 1.741 0.93 486244. 0.2378 71.27 0.3216 0.4978 0.0277 0.0179 5.982 29.004 15.669 4460.963 3.277 69.698 1.593 0.93 486697. 0.2056 74.67 0.3370 0.4698 0.0243 0.0174 5.827 28.253 13.749 4345.471 3.192 61.157 1.435 0.93 487163. 0.1735 78.06 0.3523 0.4332 0.0209 0.0170 5.676 27.517 11.810 4232.262 3.109 52.533 1.266 0.93 487642. 0.1418 81.46 0.3676 0.3874 0.0174 0.0165 5.528 26.800 9.859 4122.041 3.028 43.852 1.085 0.93 488134. 0.1110 84.85 0.3829 0.3320 0.0140 0.0161 5.386 26.112 7.903 4016.131 2.950 35.151 0.893 0.94 488641. 0.0818 88.24 0.3982 0.2668 0.0105 0.0157 5.252 25.463 5.955 3916.289 2.877 26.486 0.690 0.94 489161. 0.0549 91.64 0.4135 0.1913 0.0071 0.0153 5.126 24.851 4.013 3822.193 2.808 17.850 0.476 0.94 489694. 0.0311 95.03 0.4289 0.1051 0.0037 0.0150 5.004 24.262 2.076 3731.553 2.741 9.234 0.252 0.94 490238. 0.0119 98.43 0.4442 0.0040 0.0001 0.0145 4.851 23.520 0.074 3617.526 2.657 0.329 0.009 0.94 490752. 0.0001