20.5x13.5EPN (205x135EPN.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 0.0963 0.0388 0.011 0.713 0.542 8.435 0.081 2.411 29.144 0.08 39187. 0.6141 0.54 0.0279 0.0673 0.0952 0.0395 0.012 0.725 0.536 8.579 0.082 2.383 28.322 0.08 39216. 0.5933 1.08 0.0558 0.1306 0.0939 0.0401 0.012 0.737 0.529 8.721 0.083 2.352 27.500 0.08 39248. 0.5724 1.63 0.0837 0.1901 0.0926 0.0408 0.012 0.749 0.521 8.857 0.085 2.318 26.682 0.08 39283. 0.5513 2.17 0.1116 0.2457 0.0911 0.0414 0.012 0.760 0.513 8.986 0.086 2.280 25.871 0.08 39322. 0.5301 2.71 0.1395 0.2977 0.0894 0.0419 0.012 0.770 0.503 9.105 0.087 2.238 25.070 0.08 39364. 0.5090 3.25 0.1674 0.3460 0.0876 0.0424 0.012 0.778 0.493 9.209 0.088 2.193 24.281 0.08 39410. 0.4880 3.79 0.1953 0.3908 0.0856 0.0428 0.012 0.786 0.482 9.296 0.089 2.143 23.507 0.08 39460. 0.4670 4.33 0.2232 0.4322 0.0834 0.0431 0.013 0.791 0.470 9.361 0.089 2.088 22.749 0.08 39514. 0.4462 4.88 0.2511 0.4703 0.0811 0.0433 0.013 0.795 0.456 9.402 0.090 2.029 22.007 0.08 39571. 0.4255 5.42 0.2790 0.5054 0.0785 0.0433 0.013 0.796 0.442 9.415 0.090 1.965 21.283 0.08 39633. 0.4049 5.96 0.3069 0.5374 0.0757 0.0432 0.013 0.794 0.426 9.396 0.090 1.896 20.574 0.08 39699. 0.3845 6.50 0.3348 0.5665 0.0727 0.0430 0.013 0.790 0.409 9.341 0.089 1.821 19.881 0.08 39769. 0.3641 7.04 0.3627 0.5927 0.0696 0.0426 0.012 0.782 0.391 9.247 0.088 1.741 19.201 0.08 39844. 0.3439 7.58 0.3906 0.6161 0.0661 0.0419 0.012 0.770 0.372 9.112 0.087 1.656 18.531 0.08 39923. 0.3236 8.13 0.4185 0.6365 0.0625 0.0411 0.012 0.755 0.352 8.931 0.085 1.565 17.868 0.08 40006. 0.3034 8.67 0.4464 0.6538 0.0587 0.0401 0.012 0.736 0.330 8.703 0.083 1.469 17.207 0.08 40094. 0.2830 9.21 0.4743 0.6678 0.0546 0.0388 0.011 0.712 0.307 8.429 0.080 1.367 16.542 0.08 40185. 0.2625 9.75 0.5023 0.6782 0.0504 0.0373 0.011 0.685 0.284 8.110 0.077 1.262 15.866 0.08 40282. 0.2419 10.29 0.5302 0.6845 0.0461 0.0357 0.010 0.655 0.259 7.749 0.074 1.153 15.171 0.08 40382. 0.2211 10.83 0.5581 0.6860 0.0416 0.0338 0.010 0.621 0.234 7.349 0.070 1.041 14.445 0.08 40487. 0.2000 11.38 0.5860 0.6819 0.0370 0.0318 0.009 0.584 0.208 6.911 0.066 0.927 13.675 0.08 40596. 0.1787 11.92 0.6139 0.6709 0.0324 0.0296 0.009 0.544 0.182 6.437 0.061 0.811 12.841 0.08 40710. 0.1569 12.46 0.6418 0.6511 0.0277 0.0273 0.008 0.501 0.156 5.930 0.057 0.693 11.921 0.08 40827. 0.1347 13.00 0.6697 0.6199 0.0230 0.0248 0.007 0.456 0.129 5.393 0.051 0.575 10.877 0.08 40949. 0.1120 13.54 0.6976 0.5732 0.0183 0.0222 0.006 0.408 0.103 4.827 0.046 0.457 9.655 0.08 41076. 0.0886 14.08 0.7255 0.5044 0.0136 0.0195 0.006 0.358 0.076 4.237 0.040 0.339 8.170 0.08 41206. 0.0646 14.63 0.7534 0.4025 0.0089 0.0167 0.005 0.307 0.050 3.627 0.035 0.223 6.278 0.08 41341. 0.0403 15.17 0.7813 0.2468 0.0044 0.0138 0.004 0.254 0.025 3.001 0.029 0.109 3.712 0.08 41480. 0.0166 15.71 0.8092 -0.0056 -0.0001 0.0109 0.003 0.200 0.000 2.364 0.023 -0.002 -0.082 0.08 41623. 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 0.0967 0.0363 0.085 2.664 2.176 63.033 0.301 9.679 15.658 0.16 78373. 0.6611 1.09 0.0280 0.0724 0.0955 0.0370 0.086 2.715 2.151 64.252 0.307 9.568 15.185 0.16 78431. 0.6374 2.17 0.0560 0.1402 0.0943 0.0377 0.088 2.766 2.123 65.456 0.313 9.445 14.713 0.16 78495. 0.6137 3.26 0.0840 0.2037 0.0930 0.0383 0.089 2.816 2.093 66.625 0.318 9.308 14.247 0.16 78566. 0.5899 4.35 0.1120 0.2628 0.0915 0.0390 0.091 2.863 2.059 67.734 0.323 9.158 13.787 0.16 78644. 0.5662 5.43 0.1400 0.3177 0.0898 0.0396 0.092 2.906 2.022 68.760 0.328 8.992 13.335 0.16 78729. 0.5427 6.52 0.1680 0.3686 0.0880 0.0401 0.093 2.945 1.981 69.675 0.333 8.809 12.893 0.16 78821. 0.5193 7.61 0.1960 0.4157 0.0860 0.0405 0.094 2.977 1.936 70.450 0.336 8.609 12.462 0.16 78921. 0.4962 8.70 0.2240 0.4591 0.0838 0.0409 0.095 3.003 1.886 71.055 0.339 8.391 12.042 0.16 79029. 0.4734 9.78 0.2520 0.4990 0.0814 0.0411 0.096 3.020 1.833 71.460 0.341 8.153 11.635 0.16 79145. 0.4509 10.87 0.2800 0.5356 0.0788 0.0412 0.096 3.027 1.775 71.633 0.342 7.895 11.239 0.16 79270. 0.4286 11.96 0.3080 0.5690 0.0761 0.0412 0.096 3.024 1.712 71.545 0.342 7.617 10.856 0.16 79402. 0.4066 13.04 0.3360 0.5995 0.0731 0.0409 0.095 3.007 1.645 71.164 0.340 7.317 10.484 0.16 79544. 0.3849 14.13 0.3640 0.6271 0.0699 0.0405 0.094 2.978 1.573 70.463 0.336 6.995 10.122 0.16 79694. 0.3633 15.22 0.3919 0.6518 0.0664 0.0399 0.093 2.934 1.495 69.415 0.331 6.651 9.770 0.16 79853. 0.3419 16.30 0.4199 0.6737 0.0628 0.0391 0.091 2.873 1.413 67.992 0.325 6.284 9.425 0.16 80020. 0.3206 17.39 0.4479 0.6927 0.0589 0.0381 0.089 2.797 1.325 66.174 0.316 5.896 9.085 0.16 80196. 0.2994 18.48 0.4759 0.7087 0.0548 0.0368 0.086 2.703 1.234 63.968 0.305 5.488 8.748 0.16 80381. 0.2781 19.57 0.5039 0.7214 0.0506 0.0353 0.082 2.594 1.138 61.390 0.293 5.063 8.410 0.16 80575. 0.2568 20.65 0.5319 0.7304 0.0462 0.0336 0.078 2.470 1.040 58.455 0.279 4.625 8.068 0.16 80777. 0.2355 21.74 0.5599 0.7352 0.0417 0.0317 0.074 2.332 0.939 55.180 0.263 4.175 7.715 0.17 80988. 0.2139 22.83 0.5879 0.7350 0.0371 0.0297 0.069 2.180 0.835 51.581 0.246 3.715 7.345 0.17 81208. 0.1921 23.91 0.6159 0.7285 0.0324 0.0274 0.064 2.015 0.730 47.674 0.228 3.249 6.949 0.17 81436. 0.1700 25.00 0.6439 0.7141 0.0277 0.0250 0.058 1.837 0.625 43.479 0.208 2.778 6.515 0.17 81673. 0.1474 26.09 0.6719 0.6888 0.0230 0.0224 0.052 1.649 0.518 39.017 0.186 2.305 6.023 0.17 81919. 0.1241 27.17 0.6999 0.6484 0.0183 0.0197 0.046 1.450 0.412 34.314 0.164 1.832 5.443 0.17 82173. 0.1000 28.26 0.7279 0.5851 0.0136 0.0169 0.039 1.242 0.306 29.398 0.140 1.362 4.723 0.17 82435. 0.0748 29.35 0.7559 0.4845 0.0090 0.0140 0.033 1.027 0.202 24.307 0.116 0.898 3.766 0.17 82707. 0.0484 30.44 0.7839 0.3159 0.0044 0.0110 0.026 0.806 0.100 19.080 0.091 0.443 2.368 0.17 82986. 0.0214 31.52 0.8119 0.0008 0.0000 0.0079 0.018 0.582 0.000 13.760 0.066 0.001 0.006 0.17 83273. 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 0.0970 0.0353 0.277 5.828 4.916 206.859 0.658 21.866 10.779 0.24 117556. 0.6841 1.63 0.0280 0.0748 0.0959 0.0360 0.283 5.947 4.860 211.096 0.672 21.618 10.443 0.24 117644. 0.6590 3.27 0.0561 0.1448 0.0947 0.0367 0.289 6.066 4.798 215.292 0.685 21.343 10.109 0.24 117741. 0.6338 4.90 0.0841 0.2101 0.0934 0.0374 0.294 6.181 4.730 219.371 0.698 21.038 9.779 0.24 117847. 0.6087 6.53 0.1122 0.2708 0.0919 0.0381 0.299 6.290 4.654 223.256 0.711 20.700 9.455 0.24 117964. 0.5838 8.17 0.1402 0.3272 0.0902 0.0387 0.304 6.392 4.570 226.858 0.722 20.327 9.137 0.24 118092. 0.5591 9.80 0.1683 0.3793 0.0884 0.0392 0.309 6.482 4.478 230.086 0.732 19.917 8.827 0.24 118231. 0.5346 11.44 0.1963 0.4274 0.0864 0.0397 0.312 6.560 4.377 232.838 0.741 19.467 8.526 0.24 118382. 0.5105 13.07 0.2244 0.4717 0.0842 0.0401 0.315 6.621 4.266 235.011 0.748 18.975 8.233 0.24 118544. 0.4867 14.70 0.2524 0.5124 0.0818 0.0403 0.317 6.663 4.145 236.499 0.753 18.439 7.950 0.24 118719. 0.4633 16.34 0.2805 0.5498 0.0793 0.0404 0.318 6.683 4.014 237.193 0.755 17.856 7.677 0.24 118906. 0.4402 17.97 0.3085 0.5839 0.0765 0.0404 0.318 6.677 3.873 236.987 0.754 17.226 7.412 0.25 119106. 0.4175 19.60 0.3366 0.6150 0.0734 0.0402 0.316 6.643 3.720 235.777 0.751 16.548 7.157 0.25 119319. 0.3951 21.24 0.3646 0.6433 0.0702 0.0398 0.313 6.578 3.556 233.464 0.743 15.819 6.909 0.25 119545. 0.3730 22.87 0.3927 0.6687 0.0668 0.0392 0.308 6.479 3.381 229.953 0.732 15.040 6.670 0.25 119784. 0.3510 24.50 0.4207 0.6914 0.0631 0.0384 0.302 6.343 3.195 225.144 0.717 14.210 6.436 0.25 120036. 0.3293 26.14 0.4488 0.7113 0.0592 0.0373 0.294 6.169 2.997 218.973 0.697 13.330 6.207 0.25 120302. 0.3076 27.77 0.4768 0.7283 0.0551 0.0360 0.284 5.958 2.789 211.456 0.673 12.405 5.982 0.25 120580. 0.2860 29.40 0.5049 0.7423 0.0508 0.0345 0.272 5.709 2.573 202.642 0.645 11.443 5.758 0.25 120872. 0.2644 31.04 0.5329 0.7528 0.0464 0.0328 0.258 5.426 2.349 192.586 0.613 10.449 5.533 0.25 121177. 0.2427 32.67 0.5610 0.7595 0.0419 0.0309 0.243 5.109 2.120 181.341 0.577 9.429 5.302 0.25 121494. 0.2210 34.31 0.5890 0.7614 0.0372 0.0288 0.227 4.760 1.886 168.961 0.538 8.389 5.063 0.25 121825. 0.1990 35.94 0.6171 0.7576 0.0325 0.0265 0.209 4.381 1.649 155.504 0.495 7.333 4.808 0.25 122169. 0.1767 37.57 0.6451 0.7463 0.0278 0.0240 0.189 3.973 1.409 141.033 0.449 6.266 4.531 0.25 122526. 0.1539 39.21 0.6732 0.7248 0.0231 0.0214 0.168 3.539 1.168 125.626 0.400 5.195 4.217 0.25 122895. 0.1304 40.84 0.7012 0.6886 0.0183 0.0186 0.147 3.081 0.927 109.369 0.348 4.125 3.846 0.25 123278. 0.1060 42.47 0.7293 0.6295 0.0136 0.0157 0.124 2.602 0.689 92.370 0.294 3.063 3.381 0.25 123673. 0.0803 44.11 0.7573 0.5314 0.0089 0.0127 0.100 2.106 0.453 74.754 0.238 2.015 2.748 0.25 124081. 0.0529 45.74 0.7854 0.3567 0.0044 0.0097 0.076 1.597 0.222 56.669 0.180 0.989 1.779 0.25 124502. 0.0240 47.37 0.8134 -0.0050 0.0000 0.0065 0.051 1.078 -0.002 38.253 0.122 -0.009 -0.024 0.25 124932. 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 0.0975 0.0348 0.649 10.229 8.784 484.108 1.156 39.072 8.230 0.33 156735. 0.6982 2.18 0.0281 0.0761 0.0965 0.0356 0.663 10.447 8.686 494.382 1.180 38.637 7.969 0.33 156852. 0.6723 4.36 0.0561 0.1473 0.0952 0.0363 0.677 10.662 8.577 504.569 1.205 38.152 7.710 0.33 156982. 0.6464 6.54 0.0842 0.2137 0.0939 0.0370 0.690 10.871 8.456 514.488 1.228 37.614 7.455 0.33 157124. 0.6205 8.72 0.1123 0.2753 0.0924 0.0377 0.703 11.071 8.322 523.950 1.251 37.018 7.205 0.33 157281. 0.5949 10.90 0.1403 0.3325 0.0908 0.0383 0.714 11.257 8.174 532.745 1.272 36.359 6.959 0.33 157451. 0.5695 13.08 0.1684 0.3853 0.0890 0.0389 0.725 11.424 8.011 540.645 1.291 35.633 6.721 0.33 157637. 0.5445 15.26 0.1965 0.4340 0.0870 0.0394 0.734 11.567 7.831 547.409 1.307 34.835 6.489 0.33 157838. 0.5198 17.43 0.2245 0.4788 0.0848 0.0398 0.741 11.681 7.635 552.787 1.320 33.960 6.265 0.33 158055. 0.4955 19.61 0.2526 0.5200 0.0824 0.0400 0.746 11.760 7.420 556.519 1.329 33.006 6.048 0.33 158289. 0.4715 21.79 0.2807 0.5578 0.0798 0.0402 0.749 11.798 7.187 558.344 1.333 31.969 5.839 0.33 158539. 0.4480 23.97 0.3087 0.5924 0.0770 0.0401 0.748 11.791 6.935 558.003 1.332 30.845 5.637 0.33 158806. 0.4249 26.15 0.3368 0.6240 0.0740 0.0399 0.745 11.733 6.662 555.243 1.326 29.634 5.442 0.33 159091. 0.4021 28.33 0.3648 0.6526 0.0707 0.0395 0.737 11.618 6.370 549.824 1.313 28.333 5.255 0.33 159393. 0.3796 30.51 0.3929 0.6786 0.0673 0.0389 0.726 11.443 6.057 541.515 1.293 26.941 5.073 0.33 159712. 0.3574 32.69 0.4210 0.7018 0.0636 0.0381 0.711 11.201 5.723 530.076 1.265 25.456 4.897 0.33 160049. 0.3353 34.87 0.4490 0.7223 0.0596 0.0371 0.691 10.890 5.369 515.343 1.230 23.881 4.725 0.33 160404. 0.3134 37.05 0.4771 0.7401 0.0555 0.0358 0.667 10.509 4.997 497.348 1.187 22.226 4.557 0.33 160776. 0.2916 39.23 0.5052 0.7550 0.0512 0.0342 0.639 10.063 4.609 476.206 1.137 20.503 4.390 0.33 161165. 0.2698 41.41 0.5332 0.7667 0.0467 0.0325 0.606 9.552 4.209 452.043 1.079 18.723 4.223 0.33 161572. 0.2480 43.59 0.5613 0.7746 0.0422 0.0306 0.570 8.980 3.798 424.987 1.015 16.895 4.054 0.33 161996. 0.2261 45.77 0.5894 0.7782 0.0375 0.0284 0.530 8.350 3.379 395.165 0.943 15.031 3.879 0.33 162438. 0.2041 47.94 0.6174 0.7763 0.0328 0.0261 0.486 7.664 2.954 362.716 0.866 13.138 3.694 0.33 162897. 0.1817 50.12 0.6455 0.7675 0.0280 0.0236 0.440 6.927 2.524 327.797 0.783 11.227 3.493 0.33 163373. 0.1588 52.30 0.6736 0.7489 0.0232 0.0209 0.390 6.140 2.093 290.590 0.694 9.308 3.266 0.33 163866. 0.1352 54.48 0.7016 0.7163 0.0185 0.0181 0.337 5.310 1.662 251.310 0.600 7.391 2.999 0.33 164377. 0.1106 56.66 0.7297 0.6612 0.0137 0.0151 0.282 4.442 1.234 210.218 0.502 5.487 2.662 0.33 164905. 0.0846 58.84 0.7578 0.5665 0.0090 0.0121 0.225 3.542 0.812 167.623 0.400 3.610 2.196 0.33 165450. 0.0566 61.02 0.7858 0.3905 0.0044 0.0089 0.166 2.618 0.399 123.887 0.296 1.773 1.460 0.34 166012. 0.0264 63.20 0.8139 -0.0045 0.0000 0.0057 0.106 1.677 -0.003 79.342 0.189 -0.013 -0.016 0.34 166585. 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 0.0982 0.0347 1.263 15.919 13.813 941.701 1.799 61.441 6.653 0.41 195910. 0.7078 2.75 0.0283 0.0775 0.0971 0.0354 1.291 16.269 13.662 962.381 1.838 60.767 6.439 0.41 196057. 0.6812 5.49 0.0566 0.1500 0.0959 0.0362 1.318 16.615 13.492 982.903 1.877 60.013 6.226 0.41 196221. 0.6546 8.24 0.0849 0.2174 0.0945 0.0369 1.345 16.954 13.304 1002.901 1.915 59.174 6.017 0.41 196401. 0.6281 10.99 0.1132 0.2799 0.0931 0.0376 1.371 17.276 13.094 1021.986 1.952 58.242 5.811 0.41 196599. 0.6019 13.74 0.1415 0.3379 0.0914 0.0383 1.394 17.576 12.861 1039.726 1.986 57.207 5.611 0.41 196815. 0.5759 16.48 0.1698 0.3913 0.0896 0.0389 1.416 17.845 12.604 1055.654 2.016 56.064 5.416 0.41 197050. 0.5503 19.23 0.1981 0.4406 0.0876 0.0394 1.434 18.076 12.321 1069.276 2.042 54.804 5.226 0.41 197305. 0.5251 21.98 0.2264 0.4859 0.0854 0.0398 1.448 18.258 12.010 1080.076 2.063 53.421 5.044 0.41 197581. 0.5003 24.72 0.2547 0.5276 0.0829 0.0400 1.458 18.384 11.670 1087.523 2.077 51.908 4.867 0.41 197877. 0.4759 27.47 0.2830 0.5657 0.0803 0.0402 1.463 18.444 11.300 1091.083 2.084 50.261 4.697 0.41 198195. 0.4520 30.22 0.3113 0.6006 0.0775 0.0401 1.462 18.430 10.898 1090.223 2.082 48.474 4.534 0.41 198534. 0.4284 32.97 0.3396 0.6325 0.0744 0.0399 1.454 18.332 10.464 1084.428 2.071 46.544 4.377 0.41 198896. 0.4052 35.71 0.3679 0.6615 0.0711 0.0395 1.439 18.142 9.998 1073.213 2.050 44.469 4.225 0.41 199279. 0.3824 38.46 0.3962 0.6878 0.0675 0.0389 1.416 17.853 9.498 1056.103 2.017 42.246 4.079 0.41 199685. 0.3598 41.21 0.4245 0.7113 0.0637 0.0380 1.385 17.456 8.964 1032.608 1.972 39.873 3.938 0.41 200113. 0.3374 43.95 0.4528 0.7322 0.0597 0.0369 1.344 16.946 8.398 1002.427 1.914 37.355 3.800 0.41 200563. 0.3152 46.70 0.4811 0.7504 0.0555 0.0356 1.295 16.324 7.803 965.648 1.844 34.709 3.665 0.41 201035. 0.2931 49.45 0.5094 0.7657 0.0511 0.0340 1.237 15.595 7.184 922.507 1.762 31.955 3.532 0.41 201530. 0.2710 52.20 0.5377 0.7778 0.0465 0.0322 1.171 14.762 6.545 873.259 1.668 29.111 3.399 0.41 202047. 0.2489 54.94 0.5660 0.7863 0.0419 0.0301 1.097 13.831 5.889 818.159 1.563 26.193 3.265 0.41 202586. 0.2267 57.69 0.5944 0.7904 0.0371 0.0279 1.016 12.805 5.219 757.469 1.447 23.216 3.125 0.41 203147. 0.2044 60.44 0.6227 0.7891 0.0323 0.0255 0.927 11.689 4.541 691.480 1.321 20.196 2.978 0.41 203729. 0.1817 63.18 0.6510 0.7806 0.0274 0.0228 0.832 10.490 3.856 620.518 1.185 17.149 2.818 0.42 204334. 0.1584 65.93 0.6793 0.7621 0.0225 0.0201 0.731 9.212 3.168 544.969 1.041 14.092 2.637 0.42 204961. 0.1343 68.68 0.7076 0.7285 0.0176 0.0171 0.624 7.866 2.482 465.294 0.889 11.041 2.420 0.42 205609. 0.1091 71.43 0.7359 0.6700 0.0128 0.0141 0.512 6.458 1.802 382.048 0.730 8.016 2.140 0.42 206279. 0.0822 74.17 0.7642 0.5646 0.0081 0.0109 0.397 5.002 1.133 295.893 0.565 5.038 1.736 0.42 206971. 0.0529 76.92 0.7925 0.3529 0.0034 0.0076 0.278 3.509 0.479 207.603 0.396 2.131 1.047 0.42 207684. 0.0207 79.67 0.8208 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 0.0989 0.0348 2.187 22.974 20.047 1630.882 2.596 89.169 5.575 0.49 235077. 0.7145 3.27 0.0281 0.0773 0.0979 0.0355 2.236 23.485 19.835 1667.138 2.653 88.228 5.397 0.49 235252. 0.6879 6.53 0.0561 0.1495 0.0967 0.0363 2.284 23.993 19.599 1703.173 2.711 87.176 5.219 0.49 235447. 0.6614 9.80 0.0842 0.2168 0.0954 0.0370 2.331 24.488 19.335 1738.355 2.767 86.001 5.045 0.49 235661. 0.6349 13.07 0.1122 0.2792 0.0940 0.0378 2.376 24.962 19.041 1772.009 2.820 84.693 4.874 0.49 235896. 0.6087 16.34 0.1403 0.3371 0.0924 0.0384 2.418 25.405 18.714 1803.392 2.870 83.239 4.707 0.49 236152. 0.5828 19.60 0.1683 0.3905 0.0906 0.0390 2.456 25.803 18.352 1831.699 2.915 81.627 4.544 0.49 236432. 0.5572 22.87 0.1964 0.4398 0.0886 0.0396 2.489 26.147 17.952 1856.077 2.954 79.849 4.387 0.49 236734. 0.5320 26.14 0.2244 0.4852 0.0864 0.0400 2.515 26.422 17.512 1875.636 2.985 77.893 4.235 0.49 237061. 0.5072 29.41 0.2525 0.5270 0.0841 0.0403 2.534 26.617 17.030 1889.459 3.007 75.750 4.088 0.49 237412. 0.4829 32.67 0.2805 0.5653 0.0815 0.0404 2.543 26.718 16.505 1896.625 3.019 73.413 3.947 0.49 237789. 0.4590 35.94 0.3086 0.6005 0.0786 0.0404 2.543 26.712 15.934 1896.216 3.018 70.874 3.811 0.49 238191. 0.4355 39.21 0.3366 0.6327 0.0756 0.0402 2.531 26.587 15.317 1887.342 3.004 68.128 3.681 0.49 238619. 0.4123 42.47 0.3647 0.6620 0.0723 0.0398 2.507 26.331 14.652 1869.158 2.975 65.171 3.555 0.49 239072. 0.3895 45.74 0.3927 0.6887 0.0688 0.0392 2.469 25.932 13.939 1840.855 2.930 62.002 3.434 0.49 239552. 0.3670 49.01 0.4208 0.7128 0.0650 0.0384 2.416 25.379 13.178 1801.592 2.867 58.615 3.318 0.49 240059. 0.3447 52.28 0.4488 0.7343 0.0610 0.0373 2.348 24.663 12.368 1750.749 2.786 55.014 3.204 0.49 240591. 0.3225 55.54 0.4769 0.7533 0.0568 0.0360 2.264 23.784 11.516 1688.378 2.687 51.224 3.094 0.49 241150. 0.3005 58.81 0.5049 0.7696 0.0525 0.0344 2.166 22.749 10.628 1614.860 2.570 47.272 2.985 0.49 241735. 0.2785 62.08 0.5330 0.7829 0.0479 0.0326 2.053 21.562 9.709 1530.633 2.436 43.184 2.877 0.49 242346. 0.2566 65.34 0.5610 0.7929 0.0433 0.0306 1.926 20.231 8.764 1436.132 2.286 38.983 2.768 0.50 242983. 0.2345 68.61 0.5891 0.7990 0.0385 0.0284 1.786 18.761 7.800 1331.808 2.120 34.693 2.656 0.50 243646. 0.2123 71.88 0.6171 0.8002 0.0337 0.0260 1.634 17.160 6.820 1218.145 1.939 30.335 2.539 0.50 244335. 0.1898 75.15 0.6452 0.7951 0.0288 0.0233 1.469 15.435 5.830 1095.695 1.744 25.932 2.413 0.50 245049. 0.1668 78.41 0.6732 0.7812 0.0239 0.0206 1.294 13.595 4.835 965.099 1.536 21.507 2.272 0.50 245789. 0.1430 81.68 0.7013 0.7542 0.0190 0.0176 1.109 11.652 3.841 827.126 1.316 17.085 2.106 0.50 246555. 0.1182 84.95 0.7293 0.7061 0.0141 0.0145 0.916 9.617 2.854 682.701 1.087 12.694 1.896 0.50 247346. 0.0917 88.22 0.7574 0.6188 0.0093 0.0114 0.715 7.507 1.880 532.931 0.848 8.362 1.600 0.50 248163. 0.0628 91.48 0.7854 0.4448 0.0046 0.0081 0.508 5.341 0.927 379.125 0.603 4.123 1.109 0.50 249005. 0.0306 94.75 0.8135 0.0004 0.0000 0.0047 0.298 3.133 0.001 222.437 0.354 0.002 0.001 0.50 249863. 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 0.0999 0.0350 3.499 31.505 27.542 2609.198 3.559 122.507 4.788 0.57 274234. 0.7192 3.81 0.0280 0.0774 0.0989 0.0358 3.578 32.219 27.264 2668.336 3.640 121.268 4.634 0.57 274440. 0.6926 7.62 0.0561 0.1497 0.0977 0.0366 3.657 32.930 26.950 2727.204 3.720 119.876 4.482 0.57 274667. 0.6660 11.43 0.0841 0.2171 0.0965 0.0374 3.734 33.625 26.600 2784.757 3.799 118.315 4.332 0.57 274917. 0.6396 15.24 0.1122 0.2797 0.0950 0.0381 3.808 34.291 26.207 2839.906 3.874 116.569 4.186 0.57 275191. 0.6133 19.05 0.1402 0.3376 0.0934 0.0388 3.877 34.913 25.769 2891.416 3.944 114.621 4.042 0.57 275491. 0.5873 22.86 0.1682 0.3912 0.0917 0.0394 3.940 35.475 25.282 2937.971 4.008 112.454 3.903 0.57 275817. 0.5617 26.67 0.1963 0.4406 0.0897 0.0400 3.994 35.960 24.742 2978.164 4.063 110.054 3.768 0.57 276171. 0.5365 30.48 0.2243 0.4862 0.0876 0.0404 4.037 36.351 24.147 3010.533 4.107 107.405 3.638 0.57 276553. 0.5117 34.29 0.2524 0.5281 0.0852 0.0407 4.068 36.629 23.493 3033.586 4.138 104.496 3.513 0.57 276963. 0.4873 38.10 0.2804 0.5666 0.0826 0.0409 4.084 36.777 22.777 3045.809 4.155 101.314 3.392 0.57 277403. 0.4633 41.91 0.3084 0.6020 0.0798 0.0409 4.084 36.776 21.998 3045.708 4.155 97.849 3.276 0.57 277873. 0.4398 45.73 0.3365 0.6344 0.0767 0.0407 4.066 36.608 21.154 3031.829 4.136 94.094 3.165 0.57 278373. 0.4166 49.54 0.3645 0.6640 0.0734 0.0403 4.027 36.258 20.244 3002.798 4.096 90.044 3.058 0.57 278904. 0.3938 53.35 0.3926 0.6910 0.0699 0.0397 3.966 35.708 19.266 2957.302 4.034 85.694 2.955 0.57 279465. 0.3712 57.16 0.4206 0.7155 0.0661 0.0388 3.881 34.944 18.220 2893.993 3.948 81.041 2.856 0.57 280056. 0.3489 60.97 0.4486 0.7375 0.0620 0.0377 3.771 33.952 17.106 2811.815 3.836 76.087 2.759 0.57 280679. 0.3267 64.78 0.4767 0.7570 0.0578 0.0364 3.635 32.732 15.932 2710.808 3.698 70.864 2.666 0.58 281331. 0.3045 68.59 0.5047 0.7739 0.0533 0.0348 3.475 31.292 14.706 2591.580 3.535 65.412 2.574 0.58 282014. 0.2825 72.40 0.5328 0.7880 0.0487 0.0329 3.292 29.641 13.437 2454.840 3.349 59.767 2.483 0.58 282728. 0.2605 76.21 0.5608 0.7988 0.0440 0.0309 3.086 27.787 12.132 2301.306 3.139 53.962 2.391 0.58 283471. 0.2384 80.02 0.5888 0.8060 0.0392 0.0286 2.859 25.740 10.798 2131.714 2.908 48.029 2.297 0.58 284245. 0.2161 83.83 0.6169 0.8084 0.0342 0.0261 2.611 23.508 9.442 1946.857 2.656 41.998 2.200 0.58 285049. 0.1935 87.64 0.6449 0.8048 0.0293 0.0235 2.344 21.102 8.071 1747.631 2.384 35.901 2.095 0.58 285882. 0.1703 91.45 0.6730 0.7929 0.0243 0.0206 2.059 18.536 6.693 1535.089 2.094 29.771 1.978 0.58 286745. 0.1464 95.26 0.7010 0.7683 0.0193 0.0176 1.757 15.824 5.315 1310.485 1.788 23.642 1.840 0.58 287639. 0.1214 99.07 0.7291 0.7230 0.0143 0.0144 1.442 12.984 3.946 1075.339 1.467 17.554 1.665 0.58 288562. 0.0946 102.88 0.7571 0.6387 0.0094 0.0112 1.115 10.040 2.596 831.473 1.134 11.547 1.416 0.59 289514. 0.0653 106.69 0.7851 0.4652 0.0046 0.0078 0.779 7.016 1.274 581.048 0.793 5.668 0.995 0.59 290496. 0.0321 110.50 0.8132 -0.0075 0.0000 0.0044 0.437 3.935 -0.011 325.899 0.445 -0.049 -0.015 0.59 291494. 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 0.1010 0.0355 5.289 41.666 36.371 3943.707 4.707 161.779 4.183 0.65 313381. 0.7221 4.35 0.0280 0.0772 0.1000 0.0363 5.411 42.628 36.024 4034.690 4.816 160.234 4.050 0.65 313615. 0.6957 8.70 0.0560 0.1494 0.0989 0.0371 5.532 43.587 35.631 4125.484 4.924 158.488 3.917 0.65 313874. 0.6693 13.05 0.0840 0.2167 0.0977 0.0379 5.652 44.527 35.189 4214.473 5.031 156.519 3.787 0.65 314160. 0.6430 17.40 0.1121 0.2792 0.0963 0.0387 5.766 45.430 34.691 4299.924 5.133 154.304 3.659 0.65 314474. 0.6169 21.75 0.1401 0.3371 0.0948 0.0394 5.874 46.275 34.132 4379.918 5.228 151.820 3.535 0.65 314817. 0.5911 26.10 0.1681 0.3906 0.0930 0.0400 5.971 47.041 33.508 4452.389 5.315 149.042 3.413 0.65 315190. 0.5656 30.45 0.1961 0.4401 0.0911 0.0406 6.055 47.704 32.813 4515.157 5.390 145.950 3.296 0.65 315595. 0.5404 34.80 0.2241 0.4857 0.0890 0.0410 6.123 48.241 32.042 4565.948 5.450 142.524 3.183 0.65 316032. 0.5157 39.16 0.2521 0.5277 0.0866 0.0414 6.172 48.626 31.193 4602.445 5.494 138.745 3.074 0.65 316502. 0.4914 43.51 0.2801 0.5663 0.0840 0.0416 6.199 48.836 30.260 4622.309 5.517 134.597 2.969 0.65 317005. 0.4675 47.86 0.3082 0.6019 0.0812 0.0416 6.200 48.846 29.241 4623.239 5.519 130.066 2.869 0.65 317543. 0.4440 52.21 0.3362 0.6345 0.0781 0.0414 6.173 48.632 28.135 4603.000 5.494 125.142 2.772 0.65 318115. 0.4209 56.56 0.3642 0.6644 0.0748 0.0410 6.114 48.172 26.938 4559.476 5.442 119.819 2.680 0.65 318722. 0.3981 60.91 0.3922 0.6918 0.0712 0.0404 6.022 47.445 25.650 4490.667 5.360 114.089 2.591 0.66 319364. 0.3755 65.26 0.4202 0.7166 0.0674 0.0395 5.893 46.430 24.269 4394.543 5.246 107.948 2.505 0.66 320041. 0.3532 69.61 0.4482 0.7391 0.0633 0.0384 5.725 45.108 22.797 4269.419 5.096 101.399 2.422 0.66 320753. 0.3310 73.96 0.4762 0.7591 0.0590 0.0370 5.519 43.479 21.242 4115.243 4.912 94.483 2.341 0.66 321499. 0.3088 78.31 0.5042 0.7766 0.0545 0.0354 5.274 41.553 19.616 3932.938 4.695 87.250 2.262 0.66 322280. 0.2868 82.66 0.5323 0.7915 0.0498 0.0335 4.993 39.341 17.930 3723.603 4.445 79.751 2.184 0.66 323096. 0.2647 87.01 0.5603 0.8032 0.0450 0.0314 4.678 36.856 16.194 3488.356 4.164 72.032 2.106 0.66 323945. 0.2425 91.36 0.5883 0.8114 0.0400 0.0290 4.329 34.108 14.418 3228.331 3.854 64.133 2.026 0.66 324829. 0.2202 95.71 0.6163 0.8151 0.0350 0.0265 3.949 31.112 12.612 2944.757 3.515 56.098 1.943 0.66 325747. 0.1975 100.06 0.6443 0.8131 0.0299 0.0237 3.539 27.882 10.784 2639.017 3.150 47.968 1.853 0.66 326699. 0.1742 104.41 0.6723 0.8030 0.0248 0.0208 3.101 24.435 8.945 2312.725 2.761 39.787 1.754 0.67 327684. 0.1502 108.77 0.7003 0.7809 0.0197 0.0177 2.639 20.791 7.105 1967.822 2.349 31.602 1.638 0.67 328704. 0.1249 113.12 0.7284 0.7386 0.0146 0.0144 2.155 16.975 5.276 1606.646 1.918 23.466 1.489 0.67 329758. 0.0979 117.47 0.7564 0.6579 0.0096 0.0111 1.652 13.017 3.470 1232.043 1.471 15.435 1.278 0.67 330845. 0.0681 121.82 0.7844 0.4866 0.0047 0.0076 1.136 8.953 1.702 847.432 1.012 7.572 0.911 0.67 331965. 0.0340 126.17 0.8124 -0.0094 0.0000 0.0041 0.611 4.815 -0.017 455.759 0.544 -0.076 -0.017 0.67 333103. 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 0.1023 0.0365 7.756 54.315 46.616 5783.539 6.137 207.350 3.656 0.73 352513. 0.7144 4.89 0.0280 0.0760 0.1014 0.0373 7.924 55.494 46.206 5909.061 6.270 205.525 3.547 0.73 352775. 0.6901 9.77 0.0559 0.1473 0.1003 0.0381 8.093 56.675 45.739 6034.764 6.403 203.447 3.438 0.73 353067. 0.6655 14.66 0.0839 0.2140 0.0992 0.0389 8.259 57.836 45.208 6158.437 6.534 201.085 3.330 0.73 353388. 0.6408 19.55 0.1119 0.2762 0.0978 0.0396 8.419 58.956 44.606 6277.688 6.661 198.407 3.223 0.73 353740. 0.6161 24.43 0.1399 0.3340 0.0964 0.0403 8.569 60.009 43.925 6389.839 6.780 195.379 3.118 0.73 354126. 0.5915 29.32 0.1678 0.3876 0.0947 0.0410 8.706 60.968 43.158 6491.949 6.888 191.968 3.015 0.73 354546. 0.5670 34.21 0.1958 0.4372 0.0928 0.0416 8.825 61.803 42.299 6580.862 6.983 188.145 2.915 0.73 355001. 0.5427 39.10 0.2238 0.4830 0.0907 0.0420 8.922 62.483 41.340 6653.275 7.059 183.880 2.818 0.73 355493. 0.5187 43.98 0.2517 0.5253 0.0883 0.0423 8.993 62.976 40.276 6705.728 7.115 179.149 2.724 0.73 356023. 0.4949 48.87 0.2797 0.5642 0.0858 0.0425 9.031 63.248 39.103 6734.701 7.146 173.930 2.634 0.73 356590. 0.4714 53.76 0.3077 0.6000 0.0829 0.0425 9.034 63.266 37.816 6736.655 7.148 168.204 2.546 0.74 357196. 0.4481 58.64 0.3356 0.6329 0.0799 0.0424 8.996 62.998 36.411 6708.089 7.118 161.957 2.462 0.74 357840. 0.4252 63.53 0.3636 0.6632 0.0765 0.0420 8.912 62.412 34.887 6645.654 7.051 155.179 2.381 0.74 358524. 0.4026 68.42 0.3916 0.6909 0.0729 0.0413 8.779 61.478 33.243 6546.188 6.946 147.865 2.303 0.74 359246. 0.3801 73.30 0.4196 0.7161 0.0690 0.0405 8.591 60.167 31.476 6406.594 6.798 140.005 2.228 0.74 360008. 0.3578 78.19 0.4475 0.7391 0.0649 0.0393 8.347 58.454 29.587 6224.267 6.604 131.604 2.156 0.74 360809. 0.3357 83.08 0.4755 0.7597 0.0605 0.0379 8.045 56.338 27.587 5998.926 6.365 122.708 2.086 0.74 361649. 0.3136 87.97 0.5035 0.7779 0.0559 0.0362 7.687 53.830 25.491 5731.892 6.082 113.386 2.017 0.74 362528. 0.2915 92.85 0.5314 0.7935 0.0511 0.0343 7.275 50.947 23.315 5424.819 5.756 103.704 1.949 0.74 363445. 0.2694 97.74 0.5594 0.8062 0.0462 0.0321 6.812 47.703 21.070 5079.398 5.389 93.720 1.881 0.74 364400. 0.2472 102.63 0.5874 0.8154 0.0412 0.0297 6.299 44.115 18.771 4697.416 4.984 83.492 1.812 0.74 365393. 0.2248 107.51 0.6154 0.8204 0.0360 0.0270 5.741 40.203 16.428 4280.837 4.542 73.073 1.741 0.75 366425. 0.2019 112.40 0.6433 0.8198 0.0308 0.0242 5.139 35.987 14.055 3831.943 4.066 62.518 1.664 0.75 367494. 0.1785 117.29 0.6713 0.8112 0.0256 0.0212 4.497 31.494 11.665 3353.479 3.558 51.885 1.578 0.75 368601. 0.1542 122.17 0.6993 0.7906 0.0203 0.0180 3.820 26.754 9.271 2848.815 3.023 41.236 1.476 0.75 369746. 0.1286 127.06 0.7272 0.7494 0.0151 0.0147 3.114 21.808 6.888 2322.125 2.464 30.637 1.345 0.75 370929. 0.1011 131.95 0.7552 0.6687 0.0099 0.0112 2.385 16.703 4.533 1778.538 1.887 20.163 1.156 0.75 372149. 0.0704 136.83 0.7832 0.4945 0.0049 0.0077 1.642 11.497 2.225 1224.182 1.299 9.897 0.824 0.75 373406. 0.0352 141.72 0.8112 -0.0095 0.0000 0.0042 0.891 6.240 -0.022 664.490 0.705 -0.099 -0.015 0.76 374683. 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 0.1036 0.0402 11.712 73.820 58.332 8733.794 8.340 259.461 3.029 0.81 391626. 0.6622 5.42 0.0279 0.0703 0.1028 0.0409 11.910 75.070 57.876 8881.627 8.481 257.431 2.956 0.81 391916. 0.6436 10.85 0.0559 0.1370 0.1019 0.0416 12.106 76.302 57.351 9027.481 8.621 255.095 2.881 0.81 392239. 0.6246 16.27 0.0838 0.2002 0.1008 0.0422 12.295 77.493 56.747 9168.316 8.755 252.412 2.807 0.81 392595. 0.6053 21.69 0.1117 0.2600 0.0996 0.0428 12.473 78.613 56.055 9300.877 8.882 249.335 2.734 0.81 392986. 0.5858 27.12 0.1397 0.3163 0.0982 0.0434 12.635 79.634 55.265 9421.640 8.997 245.818 2.661 0.81 393414. 0.5661 32.54 0.1676 0.3692 0.0966 0.0439 12.776 80.523 54.365 9526.827 9.097 241.815 2.588 0.81 393881. 0.5462 37.96 0.1955 0.4189 0.0948 0.0442 12.891 81.247 53.346 9612.527 9.179 237.282 2.517 0.81 394388. 0.5262 43.38 0.2235 0.4654 0.0927 0.0445 12.974 81.773 52.198 9674.770 9.239 232.178 2.447 0.82 394935. 0.5061 48.81 0.2514 0.5089 0.0905 0.0447 13.021 82.067 50.914 9709.508 9.272 226.467 2.378 0.82 395524. 0.4858 54.23 0.2794 0.5494 0.0879 0.0447 13.025 82.094 49.487 9712.673 9.275 220.117 2.311 0.82 396156. 0.4653 59.65 0.3073 0.5871 0.0851 0.0446 12.981 81.819 47.910 9680.172 9.244 213.102 2.245 0.82 396831. 0.4447 65.08 0.3352 0.6219 0.0820 0.0442 12.884 81.208 46.179 9607.893 9.175 205.402 2.180 0.82 397549. 0.4240 70.50 0.3632 0.6541 0.0787 0.0437 12.729 80.226 44.290 9491.736 9.064 197.003 2.116 0.82 398310. 0.4032 75.92 0.3911 0.6837 0.0751 0.0429 12.509 78.840 42.243 9327.684 8.907 187.898 2.054 0.82 399115. 0.3821 81.35 0.4190 0.7107 0.0711 0.0419 12.219 77.012 40.036 9111.481 8.701 178.078 1.993 0.82 399963. 0.3609 86.77 0.4470 0.7353 0.0669 0.0407 11.853 74.709 37.667 8838.914 8.441 167.542 1.933 0.82 400854. 0.3395 92.19 0.4749 0.7573 0.0625 0.0392 11.410 71.917 35.150 8508.638 8.125 156.347 1.874 0.82 401789. 0.3180 97.62 0.5028 0.7767 0.0578 0.0374 10.893 68.658 32.504 8123.032 7.757 144.580 1.815 0.82 402766. 0.2962 103.04 0.5308 0.7931 0.0529 0.0354 10.306 64.960 29.749 7685.533 7.339 132.324 1.756 0.82 403786. 0.2741 108.46 0.5587 0.8061 0.0478 0.0331 9.652 60.835 26.902 7197.539 6.873 119.659 1.695 0.83 404848. 0.2517 113.89 0.5866 0.8151 0.0426 0.0307 8.933 56.305 23.979 6661.598 6.361 106.657 1.633 0.83 405952. 0.2288 119.31 0.6146 0.8192 0.0373 0.0280 8.154 51.395 20.996 6080.623 5.807 93.389 1.566 0.83 407098. 0.2054 124.73 0.6425 0.8163 0.0319 0.0251 7.321 46.146 17.969 5459.576 5.214 79.926 1.493 0.83 408286. 0.1811 130.15 0.6705 0.8034 0.0265 0.0221 6.443 40.609 14.915 4804.535 4.588 66.342 1.408 0.83 409515. 0.1556 135.58 0.6984 0.7750 0.0211 0.0190 5.528 34.842 11.851 4122.260 3.936 52.712 1.304 0.83 410785. 0.1285 141.00 0.7263 0.7209 0.0156 0.0157 4.588 28.915 8.796 3421.029 3.267 39.124 1.166 0.83 412097. 0.0990 146.42 0.7543 0.6200 0.0103 0.0125 3.635 22.908 5.772 2710.344 2.588 25.673 0.966 0.84 413451. 0.0664 151.85 0.7822 0.4229 0.0050 0.0092 2.683 16.911 2.803 2000.794 1.911 12.466 0.635 0.84 414845. 0.0304 157.27 0.8101 -0.0223 -0.0002 0.0060 1.744 10.994 -0.093 1300.680 1.242 -0.413 -0.032 0.84 416263. 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 0.1044 0.0481 18.656 106.894 71.076 13911.521 12.077 316.145 2.317 0.89 430751. 0.5592 5.98 0.0280 0.0596 0.1037 0.0487 18.898 108.283 70.619 14092.243 12.234 314.114 2.273 0.89 431067. 0.5467 11.96 0.0560 0.1169 0.1029 0.0493 19.127 109.597 70.084 14263.241 12.382 311.736 2.229 0.89 431418. 0.5340 17.94 0.0840 0.1719 0.1020 0.0499 19.336 110.793 69.458 14418.865 12.517 308.951 2.185 0.89 431807. 0.5212 23.92 0.1120 0.2246 0.1009 0.0503 19.516 111.825 68.727 14553.291 12.634 305.696 2.142 0.90 432235. 0.5083 29.90 0.1400 0.2753 0.0997 0.0507 19.660 112.650 67.875 14660.559 12.727 301.906 2.100 0.90 432705. 0.4952 35.88 0.1680 0.3239 0.0982 0.0510 19.760 113.220 66.887 14734.825 12.792 297.513 2.059 0.90 433218. 0.4820 41.86 0.1961 0.3706 0.0965 0.0511 19.808 113.495 65.749 14770.602 12.823 292.452 2.019 0.90 433776. 0.4686 47.85 0.2241 0.4153 0.0946 0.0511 19.797 113.436 64.448 14762.962 12.816 286.663 1.980 0.90 434380. 0.4550 53.83 0.2521 0.4582 0.0925 0.0509 19.723 113.011 62.970 14707.588 12.768 280.093 1.942 0.90 435031. 0.4411 59.81 0.2801 0.4993 0.0900 0.0505 19.580 112.190 61.307 14600.715 12.675 272.693 1.904 0.90 435731. 0.4268 65.79 0.3081 0.5386 0.0873 0.0499 19.363 110.948 59.448 14439.051 12.535 264.424 1.867 0.90 436478. 0.4121 71.77 0.3361 0.5759 0.0843 0.0492 19.069 109.261 57.387 14219.515 12.344 255.256 1.831 0.90 437274. 0.3969 77.75 0.3641 0.6113 0.0809 0.0482 18.693 107.107 55.119 13939.166 12.101 245.168 1.794 0.90 438118. 0.3811 83.73 0.3921 0.6447 0.0773 0.0470 18.231 104.462 52.640 13594.984 11.802 234.145 1.756 0.90 439011. 0.3647 89.71 0.4201 0.6759 0.0733 0.0456 17.680 101.302 49.950 13183.702 11.445 222.178 1.718 0.90 439953. 0.3476 95.69 0.4481 0.7048 0.0691 0.0439 17.033 97.596 47.046 12701.419 11.026 209.263 1.680 0.90 440942. 0.3298 101.67 0.4761 0.7313 0.0645 0.0420 16.291 93.347 43.946 12148.470 10.546 195.472 1.641 0.90 441979. 0.3113 107.65 0.5041 0.7553 0.0597 0.0399 15.459 88.579 40.675 11527.879 10.008 180.922 1.600 0.91 443064. 0.2921 113.63 0.5321 0.7756 0.0547 0.0375 14.556 83.405 37.257 10854.517 9.423 165.718 1.557 0.91 444195. 0.2720 119.61 0.5601 0.7903 0.0495 0.0351 13.606 77.962 33.712 10146.178 8.808 149.952 1.507 0.91 445372. 0.2505 125.59 0.5882 0.7978 0.0441 0.0325 12.619 72.305 30.063 9410.024 8.169 133.718 1.449 0.91 446595. 0.2274 131.58 0.6162 0.7942 0.0387 0.0300 11.630 66.636 26.324 8672.206 7.528 117.091 1.377 0.91 447865. 0.2022 137.56 0.6442 0.7801 0.0331 0.0273 10.593 60.696 22.528 7899.130 6.857 100.204 1.294 0.91 449180. 0.1757 143.54 0.6722 0.7512 0.0275 0.0246 9.525 54.578 18.695 7102.904 6.166 83.157 1.194 0.91 450540. 0.1477 149.52 0.7002 0.7012 0.0218 0.0218 8.444 48.384 14.852 6296.876 5.466 66.062 1.070 0.92 451946. 0.1180 155.50 0.7282 0.6206 0.0162 0.0190 7.368 42.218 11.029 5494.398 4.770 49.055 0.910 0.92 453397. 0.0865 161.48 0.7562 0.4948 0.0107 0.0163 6.315 36.184 7.256 4709.092 4.088 32.275 0.699 0.92 454894. 0.0539 167.46 0.7842 0.3007 0.0052 0.0137 5.303 30.384 3.571 3954.305 3.433 15.885 0.410 0.92 456436. 0.0222 173.44 0.8122 0.0000 0.0000 0.0112 4.336 24.843 0.000 3233.159 2.807 0.001 0.000 0.92 458020. 0.0000