20.5x20.5E(CD) (205x205E(CD).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 0.1085 0.0551 0.017 1.063 0.635 12.571 0.120 2.823 22.897 0.08 41274. 0.5170 0.77 0.0395 0.0758 0.1081 0.0562 0.017 1.084 0.632 12.822 0.122 2.812 22.366 0.08 41317. 0.5041 1.55 0.0789 0.1479 0.1076 0.0575 0.018 1.108 0.630 13.103 0.125 2.801 21.801 0.08 41367. 0.4904 2.32 0.1184 0.2157 0.1072 0.0588 0.018 1.134 0.627 13.412 0.128 2.789 21.207 0.08 41424. 0.4760 3.09 0.1578 0.2792 0.1066 0.0603 0.018 1.162 0.624 13.746 0.131 2.775 20.588 0.08 41488. 0.4610 3.87 0.1973 0.3383 0.1060 0.0618 0.019 1.192 0.620 14.101 0.135 2.759 19.951 0.08 41562. 0.4454 4.64 0.2367 0.3927 0.1052 0.0634 0.019 1.223 0.616 14.470 0.138 2.739 19.303 0.08 41644. 0.4294 5.41 0.2762 0.4427 0.1043 0.0651 0.020 1.255 0.610 14.845 0.142 2.715 18.650 0.08 41735. 0.4130 6.19 0.3157 0.4883 0.1032 0.0667 0.020 1.286 0.604 15.214 0.145 2.685 17.999 0.08 41836. 0.3964 6.96 0.3551 0.5297 0.1018 0.0683 0.021 1.316 0.596 15.566 0.149 2.649 17.357 0.08 41947. 0.3797 7.73 0.3946 0.5672 0.1001 0.0697 0.021 1.343 0.586 15.885 0.152 2.606 16.727 0.08 42068. 0.3629 8.51 0.4340 0.6010 0.0981 0.0708 0.022 1.366 0.574 16.157 0.154 2.553 16.114 0.08 42199. 0.3461 9.28 0.4735 0.6315 0.0957 0.0718 0.022 1.383 0.560 16.366 0.156 2.491 15.520 0.08 42340. 0.3292 10.06 0.5130 0.6589 0.0929 0.0723 0.022 1.394 0.544 16.496 0.158 2.418 14.948 0.08 42492. 0.3124 10.83 0.5524 0.6834 0.0897 0.0725 0.022 1.397 0.525 16.531 0.158 2.334 14.396 0.08 42653. 0.2956 11.60 0.5919 0.7052 0.0860 0.0721 0.022 1.391 0.503 16.453 0.157 2.237 13.864 0.08 42825. 0.2787 12.38 0.6313 0.7244 0.0817 0.0712 0.022 1.373 0.478 16.243 0.155 2.127 13.352 0.08 43007. 0.2617 13.15 0.6708 0.7411 0.0769 0.0696 0.021 1.342 0.450 15.883 0.152 2.003 12.856 0.08 43199. 0.2445 13.92 0.7102 0.7551 0.0717 0.0674 0.021 1.299 0.419 15.370 0.147 1.865 12.372 0.08 43401. 0.2271 14.70 0.7497 0.7662 0.0659 0.0645 0.020 1.244 0.386 14.713 0.141 1.716 11.892 0.08 43612. 0.2094 15.47 0.7892 0.7736 0.0599 0.0611 0.019 1.177 0.350 13.927 0.133 1.558 11.407 0.08 43832. 0.1914 16.24 0.8286 0.7764 0.0535 0.0571 0.017 1.101 0.313 13.024 0.124 1.393 10.904 0.08 44062. 0.1729 17.02 0.8681 0.7734 0.0470 0.0527 0.016 1.016 0.275 12.018 0.115 1.222 10.368 0.09 44301. 0.1540 17.79 0.9075 0.7627 0.0402 0.0479 0.015 0.923 0.235 10.919 0.104 1.047 9.780 0.09 44549. 0.1345 18.56 0.9470 0.7414 0.0334 0.0427 0.013 0.823 0.196 9.738 0.093 0.870 9.110 0.09 44805. 0.1142 19.34 0.9864 0.7045 0.0266 0.0372 0.011 0.717 0.155 8.486 0.081 0.692 8.311 0.09 45070. 0.0929 20.11 1.0259 0.6436 0.0197 0.0315 0.010 0.606 0.115 7.174 0.069 0.514 7.300 0.09 45343. 0.0703 20.88 1.0654 0.5416 0.0130 0.0255 0.008 0.492 0.076 5.816 0.056 0.337 5.916 0.09 45625. 0.0462 21.66 1.1048 0.3604 0.0063 0.0194 0.006 0.374 0.037 4.427 0.042 0.165 3.796 0.09 45914. 0.0207 22.43 1.1443 -0.0084 -0.0001 0.0133 0.004 0.255 -0.001 3.023 0.029 -0.003 -0.086 0.09 46212. 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 0.1087 0.0522 0.128 4.026 2.545 95.254 0.455 11.320 12.118 0.16 82547. 0.5480 1.55 0.0396 0.0805 0.1084 0.0533 0.130 4.112 2.536 97.308 0.465 11.281 11.822 0.16 82633. 0.5337 3.11 0.0793 0.1568 0.1080 0.0546 0.134 4.209 2.527 99.605 0.476 11.240 11.507 0.16 82733. 0.5185 4.66 0.1189 0.2284 0.1075 0.0560 0.137 4.316 2.516 102.136 0.488 11.193 11.175 0.16 82848. 0.5025 6.22 0.1585 0.2951 0.1070 0.0575 0.141 4.432 2.505 104.879 0.501 11.140 10.831 0.16 82979. 0.4859 7.77 0.1982 0.3569 0.1064 0.0591 0.145 4.556 2.490 107.801 0.515 11.077 10.478 0.16 83126. 0.4687 9.32 0.2378 0.4136 0.1057 0.0608 0.149 4.685 2.473 110.848 0.529 11.000 10.120 0.16 83292. 0.4511 10.88 0.2774 0.4654 0.1048 0.0625 0.153 4.816 2.452 113.951 0.544 10.906 9.760 0.16 83476. 0.4332 12.43 0.3171 0.5124 0.1036 0.0641 0.157 4.946 2.426 117.023 0.559 10.790 9.402 0.17 83679. 0.4151 13.98 0.3567 0.5549 0.1023 0.0657 0.161 5.070 2.394 119.960 0.573 10.648 9.051 0.17 83903. 0.3969 15.54 0.3963 0.5932 0.1006 0.0672 0.164 5.183 2.355 122.646 0.586 10.474 8.708 0.17 84146. 0.3788 17.09 0.4360 0.6276 0.0986 0.0685 0.168 5.281 2.307 124.953 0.597 10.264 8.376 0.17 84410. 0.3607 18.65 0.4756 0.6585 0.0962 0.0695 0.170 5.357 2.251 126.752 0.605 10.014 8.056 0.17 84695. 0.3426 20.20 0.5153 0.6863 0.0934 0.0701 0.172 5.406 2.185 127.909 0.611 9.720 7.749 0.17 85001. 0.3247 21.75 0.5549 0.7110 0.0901 0.0703 0.172 5.422 2.109 128.290 0.613 9.380 7.456 0.17 85327. 0.3069 23.31 0.5945 0.7331 0.0863 0.0700 0.171 5.399 2.021 127.749 0.610 8.989 7.175 0.17 85673. 0.2891 24.86 0.6342 0.7528 0.0821 0.0691 0.169 5.330 1.921 126.120 0.602 8.542 6.907 0.17 86040. 0.2713 26.42 0.6738 0.7701 0.0772 0.0676 0.165 5.209 1.807 123.261 0.589 8.038 6.650 0.17 86427. 0.2534 27.97 0.7134 0.7850 0.0719 0.0653 0.160 5.035 1.682 119.140 0.569 7.480 6.402 0.17 86834. 0.2353 29.52 0.7531 0.7974 0.0661 0.0624 0.153 4.811 1.546 113.834 0.544 6.877 6.161 0.17 87260. 0.2171 31.08 0.7927 0.8066 0.0599 0.0589 0.144 4.541 1.403 107.452 0.513 6.238 5.920 0.17 87705. 0.1987 32.63 0.8323 0.8120 0.0535 0.0549 0.134 4.230 1.253 100.098 0.478 5.572 5.676 0.17 88169. 0.1801 34.19 0.8720 0.8124 0.0469 0.0504 0.123 3.883 1.098 91.871 0.439 4.884 5.421 0.17 88650. 0.1610 35.74 0.9116 0.8063 0.0402 0.0454 0.111 3.502 0.940 82.857 0.396 4.182 5.147 0.17 89149. 0.1415 37.29 0.9512 0.7910 0.0333 0.0401 0.098 3.091 0.780 73.145 0.349 3.471 4.839 0.17 89666. 0.1212 38.85 0.9909 0.7619 0.0265 0.0344 0.084 2.655 0.620 62.828 0.300 2.757 4.474 0.17 90200. 0.0998 40.40 1.0305 0.7104 0.0196 0.0285 0.070 2.198 0.460 52.005 0.248 2.046 4.011 0.17 90751. 0.0771 41.95 1.0701 0.6179 0.0129 0.0224 0.055 1.724 0.302 40.792 0.195 1.344 3.359 0.17 91319. 0.0523 43.51 1.1098 0.4367 0.0063 0.0161 0.039 1.239 0.148 29.315 0.140 0.658 2.289 0.17 91903. 0.0250 45.06 1.1494 -0.0054 0.0000 0.0097 0.024 0.749 -0.001 17.712 0.085 -0.005 -0.027 0.17 92502. 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 0.1090 0.0511 0.422 8.858 5.737 314.396 1.001 25.520 8.277 0.25 123819. 0.5620 2.33 0.0397 0.0826 0.1086 0.0522 0.431 9.055 5.719 321.385 1.023 25.437 8.071 0.25 123949. 0.5471 4.67 0.0794 0.1607 0.1082 0.0535 0.441 9.275 5.699 329.217 1.048 25.348 7.851 0.25 124099. 0.5313 7.00 0.1191 0.2340 0.1078 0.0549 0.453 9.519 5.677 337.861 1.075 25.250 7.621 0.25 124271. 0.5147 9.34 0.1588 0.3022 0.1073 0.0564 0.466 9.783 5.651 347.249 1.105 25.136 7.381 0.25 124468. 0.4974 11.67 0.1985 0.3652 0.1067 0.0580 0.479 10.066 5.621 357.266 1.137 25.001 7.136 0.25 124690. 0.4795 14.01 0.2382 0.4229 0.1060 0.0597 0.493 10.361 5.583 367.736 1.171 24.835 6.887 0.25 124939. 0.4613 16.34 0.2779 0.4755 0.1052 0.0615 0.507 10.662 5.537 378.427 1.205 24.630 6.637 0.25 125216. 0.4427 18.68 0.3176 0.5232 0.1041 0.0632 0.522 10.961 5.480 389.040 1.238 24.376 6.389 0.25 125522. 0.4240 21.01 0.3573 0.5661 0.1027 0.0648 0.535 11.248 5.409 399.221 1.271 24.061 6.146 0.25 125857. 0.4052 23.35 0.3970 0.6048 0.1011 0.0664 0.548 11.511 5.323 408.567 1.301 23.675 5.909 0.25 126224. 0.3864 25.68 0.4367 0.6395 0.0991 0.0677 0.559 11.739 5.217 416.643 1.326 23.207 5.680 0.25 126621. 0.3678 28.02 0.4764 0.6706 0.0967 0.0687 0.567 11.917 5.092 422.993 1.346 22.648 5.460 0.25 127050. 0.3492 30.35 0.5161 0.6985 0.0939 0.0694 0.573 12.035 4.943 427.158 1.360 21.989 5.249 0.25 127510. 0.3308 32.69 0.5558 0.7234 0.0906 0.0696 0.575 12.077 4.771 428.671 1.365 21.222 5.048 0.25 128000. 0.3126 35.02 0.5955 0.7457 0.0868 0.0693 0.573 12.031 4.573 427.025 1.359 20.339 4.857 0.25 128522. 0.2944 37.36 0.6352 0.7656 0.0825 0.0685 0.565 11.880 4.346 421.647 1.342 19.330 4.675 0.25 129074. 0.2762 39.69 0.6749 0.7832 0.0777 0.0669 0.553 11.609 4.089 412.042 1.312 18.188 4.501 0.25 129657. 0.2580 42.03 0.7146 0.7987 0.0723 0.0647 0.534 11.216 3.805 398.101 1.267 16.924 4.335 0.25 130269. 0.2397 44.36 0.7543 0.8117 0.0664 0.0617 0.510 10.708 3.498 380.071 1.210 15.557 4.174 0.25 130910. 0.2213 46.70 0.7940 0.8220 0.0602 0.0582 0.481 10.095 3.172 358.317 1.141 14.110 4.015 0.25 131580. 0.2027 49.03 0.8337 0.8288 0.0538 0.0541 0.447 9.387 2.832 333.192 1.061 12.599 3.856 0.25 132277. 0.1839 51.36 0.8734 0.8312 0.0471 0.0495 0.409 8.594 2.482 305.022 0.971 11.042 3.691 0.26 133002. 0.1649 53.70 0.9131 0.8278 0.0404 0.0445 0.368 7.723 2.125 274.111 0.873 9.452 3.516 0.26 133753. 0.1453 56.03 0.9529 0.8160 0.0335 0.0391 0.323 6.783 1.763 240.761 0.766 7.843 3.322 0.26 134531. 0.1250 58.37 0.9926 0.7917 0.0266 0.0333 0.275 5.784 1.400 205.292 0.653 6.229 3.094 0.26 135334. 0.1038 60.70 1.0323 0.7464 0.0197 0.0273 0.225 4.735 1.039 168.058 0.535 4.622 2.805 0.26 136163. 0.0810 63.04 1.0720 0.6614 0.0130 0.0210 0.174 3.647 0.683 129.459 0.412 3.039 2.393 0.26 137017. 0.0561 65.37 1.1117 0.4851 0.0064 0.0146 0.121 2.534 0.336 89.944 0.286 1.493 1.692 0.26 137896. 0.0278 67.71 1.1514 0.0001 0.0000 0.0081 0.067 1.409 0.000 49.996 0.159 0.000 0.000 0.26 138797. 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 0.1092 0.0505 0.989 15.585 10.221 737.539 1.761 45.461 6.285 0.33 165089. 0.5696 3.12 0.0397 0.0837 0.1088 0.0517 1.011 15.936 10.190 754.181 1.800 45.323 6.128 0.33 165262. 0.5545 6.23 0.0795 0.1628 0.1085 0.0530 1.036 16.331 10.156 772.865 1.845 45.176 5.960 0.33 165463. 0.5384 9.35 0.1192 0.2371 0.1081 0.0544 1.064 16.768 10.120 793.529 1.894 45.012 5.784 0.33 165693. 0.5216 12.46 0.1590 0.3061 0.1076 0.0559 1.094 17.243 10.077 816.023 1.948 44.823 5.601 0.33 165955. 0.5040 15.58 0.1987 0.3697 0.1071 0.0576 1.127 17.751 10.026 840.078 2.006 44.596 5.413 0.33 166251. 0.4859 18.70 0.2384 0.4281 0.1064 0.0593 1.160 18.284 9.963 865.288 2.066 44.317 5.223 0.33 166583. 0.4673 21.81 0.2782 0.4811 0.1056 0.0611 1.195 18.829 9.885 891.096 2.127 43.968 5.031 0.33 166953. 0.4484 24.93 0.3179 0.5292 0.1045 0.0628 1.229 19.372 9.787 916.795 2.189 43.533 4.842 0.33 167362. 0.4294 28.04 0.3577 0.5724 0.1032 0.0645 1.263 19.895 9.665 941.530 2.248 42.989 4.656 0.33 167810. 0.4103 31.16 0.3974 0.6113 0.1016 0.0661 1.293 20.377 9.514 964.327 2.302 42.318 4.475 0.33 168300. 0.3912 34.28 0.4372 0.6462 0.0997 0.0674 1.320 20.795 9.330 984.124 2.349 41.499 4.300 0.33 168831. 0.3723 37.39 0.4769 0.6774 0.0973 0.0685 1.341 21.127 9.109 999.812 2.387 40.516 4.132 0.33 169403. 0.3535 40.51 0.5166 0.7054 0.0945 0.0692 1.355 21.348 8.847 1010.270 2.412 39.351 3.972 0.33 170017. 0.3349 43.63 0.5564 0.7304 0.0912 0.0695 1.360 21.434 8.541 1014.356 2.422 37.992 3.819 0.33 170673. 0.3164 46.74 0.5961 0.7529 0.0875 0.0693 1.356 21.360 8.188 1010.843 2.413 36.422 3.674 0.33 171370. 0.2980 49.86 0.6359 0.7730 0.0831 0.0684 1.339 21.096 7.784 998.343 2.383 34.623 3.536 0.34 172108. 0.2797 52.97 0.6756 0.7909 0.0782 0.0668 1.308 20.616 7.325 975.649 2.329 32.584 3.406 0.34 172887. 0.2613 56.09 0.7153 0.8067 0.0728 0.0646 1.264 19.915 6.817 942.476 2.250 30.322 3.281 0.34 173705. 0.2428 59.21 0.7551 0.8203 0.0669 0.0616 1.206 19.005 6.267 899.400 2.147 27.875 3.160 0.34 174562. 0.2243 62.32 0.7948 0.8313 0.0607 0.0580 1.136 17.903 5.684 847.276 2.023 25.280 3.043 0.34 175457. 0.2056 65.44 0.8346 0.8391 0.0542 0.0539 1.055 16.629 5.075 786.952 1.879 22.573 2.925 0.34 176388. 0.1868 68.55 0.8743 0.8429 0.0475 0.0493 0.964 15.197 4.447 719.204 1.717 19.780 2.805 0.34 177356. 0.1676 71.67 0.9140 0.8413 0.0407 0.0442 0.865 13.624 3.806 644.768 1.539 16.930 2.677 0.34 178360. 0.1481 74.79 0.9538 0.8320 0.0337 0.0387 0.757 11.926 3.158 564.376 1.347 14.045 2.538 0.34 179399. 0.1278 77.90 0.9935 0.8110 0.0268 0.0328 0.642 10.118 2.507 478.809 1.143 11.151 2.375 0.34 180472. 0.1066 81.02 1.0333 0.7703 0.0199 0.0266 0.522 8.218 1.860 388.928 0.928 8.272 2.169 0.35 181580. 0.0838 84.13 1.0730 0.6911 0.0130 0.0203 0.397 6.249 1.222 295.715 0.706 5.434 1.874 0.35 182721. 0.0587 87.25 1.1128 0.5192 0.0064 0.0137 0.269 4.232 0.599 200.279 0.478 2.666 1.357 0.35 183894. 0.0298 90.37 1.1525 -0.0021 0.0000 0.0071 0.139 2.193 -0.001 103.799 0.248 -0.005 -0.005 0.35 185097. 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 0.1094 0.0503 1.925 24.262 16.006 1435.215 2.741 71.195 5.058 0.41 206357. 0.5737 3.90 0.0398 0.0843 0.1091 0.0515 1.968 24.812 15.961 1467.782 2.803 70.995 4.932 0.41 206574. 0.5586 7.79 0.0795 0.1639 0.1088 0.0528 2.017 25.432 15.914 1504.437 2.873 70.784 4.798 0.41 206824. 0.5425 11.69 0.1193 0.2387 0.1084 0.0542 2.072 26.119 15.861 1545.080 2.951 70.551 4.656 0.41 207112. 0.5256 15.59 0.1591 0.3081 0.1080 0.0558 2.131 26.869 15.800 1589.440 3.036 70.280 4.509 0.41 207439. 0.5080 19.49 0.1988 0.3722 0.1075 0.0574 2.195 27.673 15.727 1637.017 3.126 69.954 4.357 0.41 207810. 0.4898 23.38 0.2386 0.4309 0.1069 0.0592 2.262 28.518 15.636 1687.031 3.222 69.548 4.204 0.41 208225. 0.4712 27.28 0.2783 0.4843 0.1061 0.0610 2.331 29.387 15.521 1738.403 3.320 69.037 4.050 0.41 208687. 0.4522 31.18 0.3181 0.5326 0.1051 0.0628 2.400 30.255 15.376 1789.740 3.418 68.391 3.897 0.41 209198. 0.4331 35.07 0.3579 0.5761 0.1039 0.0645 2.467 31.093 15.192 1839.349 3.513 67.576 3.746 0.41 209760. 0.4139 38.97 0.3976 0.6151 0.1023 0.0661 2.528 31.870 14.964 1885.278 3.601 66.560 3.600 0.41 210372. 0.3948 42.87 0.4374 0.6501 0.1004 0.0675 2.582 32.548 14.683 1925.388 3.677 65.311 3.459 0.41 211036. 0.3757 46.77 0.4772 0.6814 0.0981 0.0687 2.625 33.090 14.343 1957.440 3.738 63.800 3.324 0.42 211753. 0.3568 50.66 0.5169 0.7095 0.0953 0.0694 2.654 33.457 13.939 1979.162 3.780 62.000 3.194 0.42 212521. 0.3381 54.56 0.5567 0.7347 0.0920 0.0697 2.666 33.610 13.464 1988.258 3.797 59.889 3.072 0.42 213342. 0.3195 58.46 0.5964 0.7573 0.0883 0.0695 2.658 33.509 12.914 1982.264 3.786 57.441 2.955 0.42 214215. 0.3010 62.36 0.6362 0.7775 0.0840 0.0687 2.626 33.106 12.281 1958.414 3.740 54.627 2.844 0.42 215139. 0.2826 66.25 0.6760 0.7957 0.0790 0.0671 2.567 32.360 11.562 1914.274 3.656 51.428 2.740 0.42 216113. 0.2641 70.15 0.7157 0.8118 0.0736 0.0649 2.480 31.260 10.763 1849.212 3.532 47.873 2.640 0.42 217138. 0.2455 74.05 0.7555 0.8259 0.0677 0.0619 2.366 29.825 9.896 1764.318 3.370 44.019 2.544 0.42 218210. 0.2269 77.94 0.7953 0.8375 0.0614 0.0583 2.228 28.083 8.977 1661.272 3.173 39.929 2.451 0.42 219330. 0.2081 81.84 0.8350 0.8461 0.0548 0.0541 2.068 26.062 8.016 1541.747 2.945 35.655 2.358 0.42 220497. 0.1893 85.74 0.8748 0.8510 0.0480 0.0494 1.887 23.790 7.025 1407.293 2.688 31.245 2.264 0.43 221709. 0.1701 89.64 0.9145 0.8508 0.0411 0.0442 1.689 21.289 6.012 1259.373 2.405 26.741 2.165 0.43 222965. 0.1505 93.53 0.9543 0.8435 0.0341 0.0386 1.474 18.586 4.987 1099.458 2.100 22.181 2.057 0.43 224265. 0.1302 97.43 0.9941 0.8253 0.0271 0.0326 1.246 15.706 3.958 929.110 1.774 17.604 1.932 0.43 225608. 0.1090 101.33 1.0338 0.7882 0.0201 0.0263 1.006 12.680 2.934 750.070 1.433 13.051 1.774 0.43 226994. 0.0861 105.22 1.0736 0.7138 0.0132 0.0198 0.757 9.540 1.925 564.320 1.078 8.564 1.547 0.43 228422. 0.0609 109.12 1.1134 0.5460 0.0064 0.0131 0.502 6.324 0.941 374.112 0.715 4.187 1.141 0.44 229890. 0.0314 113.02 1.1531 -0.0098 -0.0001 0.0064 0.244 3.074 -0.008 181.826 0.347 -0.035 -0.020 0.44 231394. 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 0.1097 0.0504 3.329 34.974 23.107 2482.675 3.951 102.782 4.222 0.49 247622. 0.5752 4.67 0.0397 0.0844 0.1094 0.0515 3.405 35.766 23.049 2538.900 4.041 102.522 4.118 0.49 247882. 0.5604 9.35 0.0795 0.1642 0.1091 0.0528 3.490 36.660 22.988 2602.369 4.142 102.251 4.007 0.49 248182. 0.5445 14.02 0.1192 0.2391 0.1088 0.0543 3.584 37.654 22.921 2672.960 4.254 101.953 3.889 0.49 248526. 0.5278 18.70 0.1590 0.3088 0.1084 0.0558 3.688 38.743 22.844 2750.271 4.377 101.608 3.767 0.49 248919. 0.5104 23.37 0.1987 0.3732 0.1080 0.0575 3.800 39.915 22.749 2833.482 4.510 101.188 3.642 0.49 249363. 0.4923 28.05 0.2385 0.4321 0.1074 0.0593 3.918 41.153 22.631 2921.297 4.649 100.661 3.514 0.49 249860. 0.4738 32.72 0.2782 0.4856 0.1067 0.0611 4.039 42.429 22.479 3011.877 4.794 99.987 3.385 0.49 250414. 0.4550 37.40 0.3180 0.5341 0.1058 0.0630 4.161 43.710 22.285 3102.813 4.938 99.122 3.258 0.50 251027. 0.4359 42.07 0.3577 0.5777 0.1046 0.0648 4.279 44.954 22.036 3191.136 5.079 98.017 3.132 0.50 251700. 0.4168 46.75 0.3975 0.6169 0.1031 0.0664 4.390 46.112 21.723 3273.389 5.210 96.622 3.010 0.50 252434. 0.3977 51.42 0.4372 0.6520 0.1013 0.0679 4.487 47.132 21.333 3345.747 5.325 94.887 2.892 0.50 253230. 0.3786 56.10 0.4770 0.6834 0.0990 0.0691 4.565 47.955 20.856 3404.182 5.418 92.767 2.779 0.50 254089. 0.3597 60.77 0.5167 0.7116 0.0963 0.0699 4.619 48.524 20.284 3444.605 5.482 90.224 2.671 0.50 255012. 0.3410 65.45 0.5565 0.7369 0.0931 0.0703 4.644 48.782 19.609 3462.895 5.511 87.220 2.568 0.50 255996. 0.3224 70.12 0.5962 0.7597 0.0894 0.0701 4.633 48.666 18.822 3454.682 5.498 83.718 2.471 0.50 257043. 0.3039 74.80 0.6360 0.7801 0.0850 0.0693 4.580 48.108 17.913 3415.081 5.435 79.676 2.379 0.50 258152. 0.2854 79.47 0.6757 0.7985 0.0801 0.0678 4.479 47.047 16.876 3339.715 5.315 75.064 2.292 0.50 259321. 0.2669 84.15 0.7155 0.8150 0.0746 0.0655 4.328 45.463 15.720 3227.278 5.136 69.921 2.209 0.51 260551. 0.2483 88.82 0.7552 0.8295 0.0687 0.0625 4.130 43.382 14.463 3079.560 4.901 64.331 2.130 0.51 261838. 0.2296 93.50 0.7949 0.8416 0.0623 0.0589 3.888 40.845 13.126 2899.474 4.615 58.385 2.053 0.51 263182. 0.2109 98.17 0.8347 0.8510 0.0557 0.0546 3.607 37.894 11.727 2689.969 4.281 52.163 1.977 0.51 264581. 0.1919 102.85 0.8744 0.8569 0.0488 0.0498 3.291 34.567 10.282 2453.789 3.905 45.734 1.901 0.51 266035. 0.1727 107.52 0.9142 0.8581 0.0418 0.0445 2.942 30.900 8.804 2193.527 3.491 39.161 1.820 0.51 267543. 0.1531 112.20 0.9539 0.8526 0.0347 0.0388 2.564 26.932 7.307 1911.795 3.043 32.500 1.733 0.51 269102. 0.1328 116.87 0.9937 0.8369 0.0275 0.0327 2.161 22.699 5.803 1611.366 2.565 25.810 1.633 0.52 270713. 0.1115 121.55 1.0334 0.8033 0.0204 0.0263 1.737 18.248 4.305 1295.344 2.062 19.151 1.508 0.52 272376. 0.0887 126.22 1.0732 0.7341 0.0134 0.0196 1.297 13.626 2.829 967.264 1.539 12.584 1.327 0.52 274088. 0.0633 130.89 1.1129 0.5727 0.0066 0.0128 0.846 8.891 1.389 631.171 1.005 6.178 0.998 0.52 275849. 0.0333 135.57 1.1527 -0.0006 0.0000 0.0059 0.391 4.104 -0.001 291.353 0.464 -0.003 -0.001 0.52 277652. 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 0.1100 0.0506 5.313 47.841 31.540 3962.078 5.405 140.288 3.611 0.57 288884. 0.5748 5.45 0.0397 0.0842 0.1098 0.0518 5.433 48.915 31.470 4051.065 5.526 139.978 3.523 0.57 289186. 0.5603 10.90 0.0795 0.1640 0.1095 0.0531 5.568 50.132 31.399 4151.884 5.664 139.661 3.430 0.57 289536. 0.5448 16.36 0.1192 0.2389 0.1092 0.0545 5.719 51.492 31.321 4264.459 5.818 139.317 3.331 0.58 289937. 0.5285 21.81 0.1589 0.3086 0.1089 0.0561 5.885 52.987 31.232 4388.258 5.986 138.919 3.228 0.58 290394. 0.5114 27.26 0.1987 0.3730 0.1086 0.0578 6.064 54.603 31.122 4522.105 6.169 138.431 3.122 0.58 290911. 0.4936 32.71 0.2384 0.4321 0.1081 0.0596 6.255 56.317 30.982 4664.045 6.363 137.808 3.013 0.58 291490. 0.4754 38.16 0.2781 0.4858 0.1074 0.0615 6.452 58.094 30.799 4811.227 6.563 136.996 2.904 0.58 292136. 0.4568 43.62 0.3179 0.5344 0.1066 0.0634 6.651 59.888 30.560 4959.835 6.766 135.931 2.795 0.58 292849. 0.4379 49.07 0.3576 0.5781 0.1055 0.0653 6.846 61.642 30.249 5105.086 6.964 134.546 2.687 0.58 293633. 0.4190 54.52 0.3973 0.6174 0.1041 0.0670 7.029 63.287 29.848 5241.329 7.150 132.765 2.583 0.58 294489. 0.4000 59.97 0.4371 0.6525 0.1023 0.0685 7.191 64.747 29.343 5362.229 7.315 130.518 2.482 0.58 295417. 0.3811 65.42 0.4768 0.6841 0.1002 0.0698 7.323 65.940 28.718 5461.065 7.450 127.736 2.385 0.58 296419. 0.3623 70.87 0.5165 0.7124 0.0975 0.0707 7.417 66.785 27.959 5530.987 7.545 124.361 2.293 0.58 297494. 0.3436 76.33 0.5563 0.7378 0.0944 0.0711 7.463 67.197 27.055 5565.123 7.592 120.340 2.205 0.58 298643. 0.3251 81.78 0.5960 0.7607 0.0907 0.0710 7.451 67.090 25.994 5556.269 7.580 115.620 2.122 0.59 299865. 0.3067 87.23 0.6357 0.7814 0.0864 0.0703 7.371 66.368 24.762 5496.464 7.498 110.139 2.043 0.59 301158. 0.2882 92.68 0.6754 0.8001 0.0814 0.0688 7.213 64.943 23.349 5378.425 7.337 103.857 1.969 0.59 302523. 0.2697 98.13 0.7152 0.8169 0.0759 0.0665 6.973 62.784 21.767 5199.676 7.093 96.819 1.899 0.59 303957. 0.2511 103.59 0.7549 0.8318 0.0699 0.0634 6.655 59.925 20.041 4962.898 6.770 89.143 1.832 0.59 305459. 0.2324 109.04 0.7946 0.8445 0.0635 0.0597 6.266 56.422 18.200 4672.746 6.374 80.954 1.767 0.59 307027. 0.2136 114.49 0.8344 0.8546 0.0567 0.0554 5.812 52.332 16.269 4334.034 5.912 72.366 1.703 0.59 308660. 0.1947 119.94 0.8741 0.8614 0.0498 0.0505 5.299 47.710 14.271 3951.250 5.390 63.478 1.638 0.60 310356. 0.1754 125.39 0.9138 0.8638 0.0426 0.0451 4.732 42.607 12.225 3528.664 4.814 54.376 1.571 0.60 312115. 0.1557 130.85 0.9536 0.8600 0.0354 0.0393 4.118 37.076 10.149 3070.555 4.189 45.142 1.499 0.60 313934. 0.1354 136.30 0.9933 0.8464 0.0281 0.0330 3.462 31.170 8.062 2581.482 3.522 35.858 1.416 0.60 315813. 0.1140 141.75 1.0330 0.8159 0.0209 0.0264 2.771 24.953 5.982 2066.548 2.819 26.607 1.313 0.61 317752. 0.0910 147.20 1.0728 0.7510 0.0137 0.0196 2.054 18.494 3.929 1531.600 2.089 17.478 1.164 0.61 319748. 0.0654 152.65 1.1125 0.5946 0.0067 0.0126 1.319 11.874 1.926 983.360 1.341 8.569 0.889 0.61 321802. 0.0350 158.11 1.1522 -0.0047 0.0000 0.0055 0.575 5.180 -0.006 428.973 0.585 -0.029 -0.007 0.61 323903. 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 0.1103 0.0512 8.018 63.167 41.317 5978.731 7.137 183.779 3.134 0.66 330142. 0.5711 6.23 0.0397 0.0836 0.1101 0.0523 8.193 64.550 41.240 6109.649 7.293 183.435 3.062 0.66 330486. 0.5573 12.45 0.0794 0.1629 0.1099 0.0536 8.393 66.125 41.164 6258.696 7.471 183.097 2.983 0.66 330885. 0.5425 18.68 0.1191 0.2375 0.1097 0.0550 8.617 67.892 41.083 6425.958 7.670 182.739 2.900 0.66 331342. 0.5269 24.90 0.1588 0.3071 0.1095 0.0566 8.865 69.846 40.991 6610.882 7.891 182.329 2.812 0.66 331863. 0.5104 31.13 0.1985 0.3715 0.1092 0.0583 9.135 71.970 40.877 6811.965 8.131 181.821 2.722 0.66 332452. 0.4933 37.36 0.2382 0.4306 0.1088 0.0602 9.423 74.238 40.728 7026.549 8.387 181.157 2.629 0.66 333112. 0.4756 43.58 0.2779 0.4844 0.1082 0.0621 9.723 76.605 40.528 7250.605 8.655 180.266 2.535 0.66 333848. 0.4575 49.81 0.3176 0.5331 0.1075 0.0640 10.029 79.014 40.257 7478.585 8.927 179.064 2.442 0.66 334662. 0.4391 56.04 0.3573 0.5771 0.1065 0.0660 10.330 81.388 39.895 7703.352 9.195 177.454 2.349 0.66 335555. 0.4206 62.26 0.3970 0.6165 0.1053 0.0678 10.616 83.638 39.419 7916.278 9.449 175.334 2.259 0.66 336531. 0.4019 68.49 0.4367 0.6518 0.1036 0.0694 10.872 85.658 38.804 8107.514 9.678 172.601 2.171 0.66 337591. 0.3833 74.71 0.4764 0.6835 0.1016 0.0708 11.085 87.337 38.030 8266.395 9.867 169.155 2.087 0.66 338734. 0.3648 80.94 0.5161 0.7119 0.0990 0.0718 11.240 88.558 37.075 8381.933 10.005 164.911 2.006 0.67 339962. 0.3463 87.17 0.5558 0.7375 0.0959 0.0723 11.322 89.204 35.924 8443.068 10.078 159.791 1.930 0.67 341274. 0.3279 93.39 0.5955 0.7606 0.0923 0.0723 11.316 89.154 34.560 8438.415 10.073 153.722 1.858 0.67 342669. 0.3096 99.62 0.6353 0.7814 0.0880 0.0716 11.205 88.280 32.963 8355.641 9.974 146.618 1.789 0.67 344147. 0.2912 105.85 0.6750 0.8004 0.0831 0.0701 10.974 86.459 31.120 8183.274 9.768 138.422 1.725 0.67 345706. 0.2728 112.07 0.7147 0.8175 0.0776 0.0678 10.617 83.644 29.044 7916.854 9.450 129.186 1.664 0.67 347344. 0.2542 118.30 0.7544 0.8329 0.0715 0.0647 10.138 79.874 26.768 7560.021 9.024 119.064 1.606 0.68 349060. 0.2355 124.52 0.7941 0.8462 0.0650 0.0610 9.548 75.223 24.331 7119.780 8.499 108.224 1.550 0.68 350852. 0.2167 130.75 0.8338 0.8570 0.0581 0.0566 8.856 69.769 21.767 6603.555 7.882 96.822 1.495 0.68 352718. 0.1977 136.98 0.8735 0.8647 0.0510 0.0515 8.071 63.586 19.108 6018.340 7.184 84.991 1.440 0.68 354656. 0.1784 143.20 0.9132 0.8684 0.0437 0.0460 7.202 56.744 16.378 5370.755 6.411 72.851 1.383 0.68 356664. 0.1587 149.43 0.9529 0.8661 0.0363 0.0400 6.259 49.313 13.605 4667.449 5.571 60.513 1.322 0.69 358742. 0.1382 155.65 0.9926 0.8546 0.0289 0.0335 5.251 41.369 10.811 3915.548 4.674 48.088 1.252 0.69 360888. 0.1167 161.88 1.0323 0.8270 0.0214 0.0267 4.188 32.998 8.024 3123.206 3.728 35.690 1.165 0.69 363101. 0.0936 168.11 1.0720 0.7659 0.0141 0.0197 3.084 24.300 5.270 2299.974 2.745 23.442 1.039 0.69 365380. 0.0676 174.33 1.1117 0.6137 0.0069 0.0125 1.954 15.395 2.580 1457.086 1.739 11.475 0.803 0.70 367724. 0.0366 180.56 1.1514 -0.0110 0.0000 0.0052 0.814 6.411 -0.019 606.809 0.724 -0.083 -0.014 0.70 370121. 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 0.1106 0.0531 11.831 82.851 52.436 8822.012 9.360 233.237 2.696 0.74 371395. 0.5534 6.99 0.0396 0.0808 0.1105 0.0541 12.072 84.539 52.356 9001.757 9.551 232.878 2.638 0.74 371781. 0.5411 13.98 0.0792 0.1578 0.1103 0.0554 12.347 86.470 52.281 9207.416 9.769 232.547 2.575 0.74 372227. 0.5279 20.97 0.1189 0.2306 0.1102 0.0568 12.658 88.648 52.207 9439.328 10.015 232.216 2.509 0.74 372739. 0.5138 27.96 0.1585 0.2989 0.1100 0.0583 13.004 91.068 52.124 9696.947 10.289 231.848 2.438 0.74 373323. 0.4990 34.95 0.1981 0.3623 0.1098 0.0600 13.381 93.711 52.021 9978.374 10.587 231.391 2.365 0.74 373982. 0.4834 41.94 0.2377 0.4209 0.1095 0.0618 13.786 96.544 51.883 10280.067 10.907 230.775 2.289 0.74 374721. 0.4674 48.93 0.2774 0.4746 0.1091 0.0637 14.210 99.516 51.689 10596.493 11.243 229.912 2.212 0.74 375544. 0.4509 55.92 0.3170 0.5236 0.1085 0.0657 14.644 102.553 51.415 10919.876 11.586 228.693 2.136 0.74 376455. 0.4341 62.91 0.3566 0.5680 0.1077 0.0676 15.073 105.560 51.032 11240.100 11.926 226.992 2.059 0.74 377455. 0.4170 69.90 0.3962 0.6081 0.1066 0.0694 15.482 108.422 50.510 11544.791 12.249 224.669 1.984 0.74 378548. 0.3998 76.89 0.4359 0.6444 0.1051 0.0711 15.851 111.004 49.815 11819.748 12.541 221.579 1.912 0.75 379734. 0.3825 83.88 0.4755 0.6771 0.1032 0.0725 16.159 113.162 48.916 12049.601 12.785 217.579 1.841 0.75 381015. 0.3650 90.87 0.5151 0.7067 0.1008 0.0735 16.385 114.749 47.783 12218.519 12.964 212.540 1.774 0.75 382391. 0.3476 97.86 0.5547 0.7333 0.0979 0.0740 16.509 115.614 46.391 12310.651 13.062 206.348 1.709 0.75 383862. 0.3300 104.85 0.5943 0.7574 0.0943 0.0740 16.508 115.605 44.716 12309.652 13.061 198.897 1.648 0.75 385427. 0.3123 111.84 0.6340 0.7791 0.0902 0.0734 16.357 114.552 42.732 12197.610 12.942 190.072 1.589 0.75 387085. 0.2944 118.83 0.6736 0.7988 0.0853 0.0719 16.035 112.293 40.420 11957.031 12.687 179.787 1.533 0.76 388835. 0.2763 125.83 0.7132 0.8165 0.0797 0.0696 15.528 108.747 37.791 11579.423 12.286 168.095 1.480 0.76 390674. 0.2580 132.82 0.7528 0.8325 0.0736 0.0666 14.843 103.945 34.889 11068.177 11.744 155.188 1.430 0.76 392600. 0.2394 139.81 0.7925 0.8464 0.0670 0.0627 13.990 97.973 31.764 10432.212 11.069 141.288 1.381 0.76 394612. 0.2206 146.80 0.8321 0.8581 0.0601 0.0582 12.984 90.926 28.462 9681.905 10.273 126.601 1.333 0.76 396706. 0.2016 153.79 0.8717 0.8668 0.0528 0.0531 11.839 82.907 25.024 8827.973 9.367 111.306 1.286 0.77 398880. 0.1823 160.78 0.9113 0.8715 0.0453 0.0474 10.569 74.014 21.484 7881.045 8.362 95.561 1.236 0.77 401134. 0.1625 167.77 0.9509 0.8703 0.0377 0.0412 9.189 64.352 17.876 6852.188 7.270 79.513 1.183 0.77 403465. 0.1418 174.76 0.9906 0.8595 0.0300 0.0346 7.716 54.036 14.232 5753.810 6.105 63.306 1.122 0.77 405872. 0.1200 181.75 1.0302 0.8316 0.0223 0.0277 6.169 43.205 10.586 4600.477 4.881 47.088 1.044 0.78 408354. 0.0963 188.74 1.0698 0.7675 0.0147 0.0205 4.572 32.022 6.973 3409.683 3.618 31.016 0.928 0.78 410910. 0.0694 195.73 1.1094 0.6064 0.0072 0.0132 2.953 20.681 3.431 2202.115 2.337 15.262 0.707 0.78 413539. 0.0371 202.72 1.1491 -0.0005 0.0000 0.0060 1.342 9.395 -0.001 1000.385 1.061 -0.006 -0.001 0.79 416226. 0.0000 PROP RPM = 10000 V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM (mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - - 0.00 0.0000 0.0000 0.1108 0.0582 17.788 112.117 64.849 13264.764 12.667 288.448 2.217 0.82 412642. 0.5062 7.76 0.0396 0.0741 0.1107 0.0592 18.106 114.120 64.764 13501.737 12.893 288.069 2.176 0.82 413070. 0.4963 15.53 0.0792 0.1450 0.1106 0.0604 18.472 116.426 64.692 13774.594 13.154 287.750 2.130 0.82 413564. 0.4857 23.29 0.1188 0.2125 0.1105 0.0618 18.887 119.042 64.628 14084.091 13.449 287.466 2.081 0.82 414132. 0.4743 31.06 0.1584 0.2763 0.1103 0.0633 19.351 121.963 64.564 14429.712 13.779 287.179 2.029 0.82 414778. 0.4622 38.82 0.1980 0.3361 0.1102 0.0649 19.859 125.170 64.486 14809.070 14.142 286.832 1.975 0.82 415508. 0.4496 46.58 0.2376 0.3919 0.1100 0.0667 20.407 128.620 64.377 15217.276 14.531 286.351 1.919 0.82 416327. 0.4364 54.35 0.2772 0.4435 0.1097 0.0686 20.982 132.247 64.216 15646.370 14.941 285.631 1.862 0.82 417239. 0.4228 62.11 0.3169 0.4912 0.1093 0.0705 21.570 135.951 63.971 16084.603 15.360 284.543 1.804 0.83 418248. 0.4090 69.87 0.3565 0.5351 0.1087 0.0724 22.149 139.603 63.608 16516.721 15.772 282.930 1.747 0.83 419356. 0.3949 77.64 0.3961 0.5755 0.1078 0.0742 22.695 143.044 63.086 16923.818 16.161 280.609 1.691 0.83 420567. 0.3807 85.40 0.4357 0.6127 0.1066 0.0758 23.178 146.087 62.360 17283.855 16.505 277.379 1.636 0.83 421882. 0.3663 93.17 0.4753 0.6471 0.1049 0.0771 23.566 148.534 61.384 17573.381 16.781 273.036 1.584 0.83 423303. 0.3519 100.93 0.5149 0.6790 0.1027 0.0779 23.829 150.189 60.114 17769.135 16.968 267.389 1.534 0.83 424830. 0.3372 108.69 0.5545 0.7085 0.1000 0.0783 23.936 150.864 58.512 17849.010 17.045 260.263 1.487 0.83 426464. 0.3224 116.46 0.5941 0.7359 0.0966 0.0780 23.860 150.383 56.542 17792.129 16.990 251.499 1.441 0.84 428203. 0.3072 124.22 0.6337 0.7612 0.0926 0.0771 23.570 148.561 54.167 17576.502 16.784 240.934 1.398 0.84 430046. 0.2916 131.98 0.6733 0.7845 0.0878 0.0753 23.040 145.215 51.357 17180.625 16.406 228.436 1.356 0.84 431991. 0.2754 139.75 0.7129 0.8058 0.0822 0.0728 22.254 140.265 48.122 16594.990 15.847 214.048 1.315 0.84 434037. 0.2586 147.51 0.7525 0.8250 0.0761 0.0694 21.224 133.771 44.515 15826.646 15.113 198.002 1.276 0.84 436179. 0.2413 155.28 0.7921 0.8418 0.0694 0.0653 19.968 125.858 40.599 14890.436 14.219 180.583 1.237 0.85 438417. 0.2234 163.04 0.8317 0.8554 0.0623 0.0605 18.516 116.706 36.434 13807.724 13.185 162.056 1.197 0.85 440746. 0.2048 170.80 0.8713 0.8651 0.0548 0.0552 16.887 106.433 32.073 12592.271 12.025 142.660 1.155 0.85 443164. 0.1855 178.57 0.9110 0.8690 0.0471 0.0494 15.104 95.198 27.564 11263.044 10.755 122.604 1.110 0.85 445670. 0.1652 186.33 0.9506 0.8645 0.0392 0.0431 13.191 83.142 22.952 9836.688 9.393 102.089 1.058 0.86 448261. 0.1437 194.10 0.9902 0.8467 0.0312 0.0365 11.174 70.429 18.281 8332.574 7.957 81.312 0.995 0.86 450937. 0.1206 201.86 1.0298 0.8048 0.0232 0.0297 9.092 57.304 13.594 6779.730 6.474 60.466 0.909 0.86 453695. 0.0950 209.62 1.0694 0.7152 0.0153 0.0229 6.990 44.054 8.943 5212.148 4.977 39.777 0.778 0.87 456534. 0.0660 217.39 1.1090 0.5166 0.0075 0.0161 4.916 30.983 4.381 3665.616 3.500 19.485 0.542 0.87 459454. 0.0322 225.15 1.1486 -0.0071 -0.0001 0.0095 2.917 18.385 -0.034 2175.214 2.077 -0.153 -0.007 0.87 462446. 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 0.1098 0.0659 26.838 153.779 77.725 20013.240 17.374 345.721 1.762 0.90 453948. 0.4402 8.60 0.0399 0.0653 0.1096 0.0669 27.250 156.140 77.627 20320.465 17.641 345.285 1.733 0.90 454419. 0.4327 17.20 0.0798 0.1283 0.1095 0.0681 27.731 158.894 77.551 20678.916 17.952 344.948 1.701 0.90 454965. 0.4246 25.80 0.1197 0.1885 0.1095 0.0695 28.283 162.055 77.493 21090.377 18.309 344.688 1.667 0.90 455591. 0.4159 34.41 0.1596 0.2458 0.1094 0.0710 28.906 165.627 77.444 21555.209 18.712 344.472 1.630 0.90 456305. 0.4065 43.01 0.1995 0.2999 0.1093 0.0727 29.598 169.593 77.393 22071.369 19.161 344.246 1.590 0.91 457112. 0.3966 51.61 0.2393 0.3506 0.1092 0.0746 30.352 173.913 77.323 22633.564 19.649 343.934 1.550 0.91 458018. 0.3862 60.21 0.2792 0.3979 0.1091 0.0765 31.155 178.513 77.210 23232.199 20.168 343.432 1.507 0.91 459026. 0.3755 68.81 0.3191 0.4418 0.1088 0.0786 31.986 183.275 77.023 23852.010 20.706 342.599 1.465 0.91 460143. 0.3644 77.41 0.3590 0.4826 0.1084 0.0806 32.816 188.031 76.721 24470.967 21.244 341.256 1.422 0.91 461370. 0.3531 86.01 0.3989 0.5205 0.1077 0.0825 33.596 192.503 76.249 25052.891 21.749 339.156 1.380 0.91 462712. 0.3417 94.61 0.4388 0.5560 0.1067 0.0842 34.286 196.453 75.554 25566.988 22.195 336.066 1.340 0.91 464170. 0.3303 103.22 0.4787 0.5893 0.1053 0.0856 34.830 199.570 74.575 25972.615 22.547 331.709 1.302 0.91 465746. 0.3188 111.82 0.5186 0.6210 0.1035 0.0864 35.170 201.521 73.247 26226.580 22.768 325.803 1.267 0.92 467443. 0.3073 120.42 0.5585 0.6513 0.1010 0.0866 35.253 201.995 71.510 26288.170 22.821 318.076 1.234 0.92 469259. 0.2958 129.02 0.5984 0.6807 0.0979 0.0861 35.030 200.714 69.304 26121.543 22.677 308.266 1.203 0.92 471195. 0.2840 137.62 0.6382 0.7090 0.0940 0.0846 34.457 197.436 66.572 25694.902 22.306 296.114 1.175 0.92 473248. 0.2718 146.22 0.6781 0.7363 0.0894 0.0823 33.499 191.945 63.263 24980.348 21.686 281.396 1.149 0.92 475417. 0.2590 154.82 0.7180 0.7625 0.0839 0.0790 32.156 184.252 59.390 23979.096 20.817 264.166 1.123 0.93 477699. 0.2454 163.43 0.7579 0.7871 0.0777 0.0748 30.461 174.538 55.017 22714.871 19.719 244.716 1.099 0.93 480091. 0.2310 172.03 0.7978 0.8097 0.0709 0.0699 28.455 163.045 50.226 21219.180 18.421 223.404 1.074 0.93 482588. 0.2157 180.63 0.8377 0.8288 0.0637 0.0644 26.205 150.152 45.090 19541.166 16.964 200.561 1.047 0.93 485187. 0.1992 189.23 0.8776 0.8420 0.0560 0.0584 23.776 136.234 39.676 17729.949 15.392 176.480 1.015 0.94 487886. 0.1812 197.83 0.9175 0.8469 0.0481 0.0521 21.211 121.537 34.055 15817.170 13.731 151.475 0.977 0.94 490682. 0.1615 206.43 0.9574 0.8318 0.0399 0.0459 18.704 107.169 28.263 13947.229 12.108 125.715 0.919 0.94 493573. 0.1385 215.03 0.9973 0.7927 0.0316 0.0398 16.198 92.813 22.393 12078.923 10.486 99.603 0.841 0.95 496556. 0.1128 223.63 1.0371 0.7195 0.0234 0.0337 13.706 78.533 16.536 10220.577 8.873 73.554 0.734 0.95 499630. 0.0846 232.24 1.0770 0.5916 0.0152 0.0277 11.291 64.698 10.787 8419.970 7.310 47.980 0.581 0.95 502794. 0.0541 240.84 1.1169 0.3738 0.0074 0.0222 9.017 51.665 5.249 6723.844 5.837 23.345 0.354 0.96 506048. 0.0230 249.44 1.1568 -0.0005 0.0000 0.0170 6.924 39.675 -0.005 5163.435 4.482 -0.023 0.000 0.96 509401. 0.0000