17x6E (17x6E.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 0.0652 0.0235 0.003 0.167 0.171 1.974 0.019 0.763 39.389 0.07 26829. 0.5645 0.27 0.0170 0.0459 0.0638 0.0236 0.003 0.167 0.168 1.978 0.019 0.746 38.469 0.07 26840. 0.5455 0.54 0.0339 0.0896 0.0623 0.0236 0.003 0.167 0.164 1.981 0.019 0.729 37.542 0.07 26852. 0.5263 0.82 0.0509 0.1311 0.0608 0.0236 0.003 0.168 0.160 1.982 0.019 0.712 36.608 0.07 26865. 0.5069 1.09 0.0678 0.1703 0.0592 0.0236 0.003 0.167 0.156 1.982 0.019 0.693 35.667 0.07 26878. 0.4874 1.36 0.0848 0.2072 0.0576 0.0236 0.003 0.167 0.151 1.979 0.019 0.674 34.719 0.07 26892. 0.4677 1.63 0.1018 0.2418 0.0558 0.0235 0.003 0.167 0.147 1.973 0.019 0.653 33.762 0.07 26907. 0.4479 1.91 0.1187 0.2740 0.0540 0.0234 0.003 0.166 0.142 1.966 0.019 0.632 32.796 0.07 26923. 0.4280 2.18 0.1357 0.3038 0.0521 0.0233 0.003 0.165 0.137 1.955 0.019 0.610 31.820 0.07 26939. 0.4079 2.45 0.1527 0.3312 0.0502 0.0231 0.003 0.164 0.132 1.942 0.019 0.587 30.831 0.07 26957. 0.3877 2.72 0.1696 0.3560 0.0481 0.0229 0.003 0.163 0.127 1.926 0.018 0.563 29.829 0.07 26975. 0.3674 2.99 0.1866 0.3782 0.0460 0.0227 0.003 0.161 0.121 1.906 0.018 0.539 28.810 0.07 26994. 0.3470 3.27 0.2035 0.3978 0.0439 0.0224 0.003 0.159 0.115 1.884 0.018 0.513 27.771 0.07 27014. 0.3265 3.54 0.2205 0.4145 0.0416 0.0221 0.002 0.157 0.109 1.859 0.018 0.487 26.711 0.07 27035. 0.3059 3.81 0.2375 0.4282 0.0393 0.0218 0.002 0.155 0.103 1.831 0.017 0.460 25.624 0.07 27057. 0.2852 4.08 0.2544 0.4388 0.0369 0.0214 0.002 0.152 0.097 1.799 0.017 0.432 24.507 0.07 27080. 0.2645 4.36 0.2714 0.4460 0.0345 0.0210 0.002 0.149 0.091 1.764 0.017 0.404 23.355 0.07 27104. 0.2436 4.63 0.2883 0.4497 0.0320 0.0205 0.002 0.146 0.084 1.725 0.016 0.375 22.161 0.07 27128. 0.2227 4.90 0.3053 0.4494 0.0295 0.0201 0.002 0.142 0.078 1.684 0.016 0.345 20.920 0.07 27154. 0.2018 5.17 0.3223 0.4450 0.0269 0.0195 0.002 0.138 0.071 1.638 0.016 0.315 19.622 0.07 27181. 0.1808 5.45 0.3392 0.4359 0.0243 0.0189 0.002 0.134 0.064 1.590 0.015 0.285 18.259 0.07 27209. 0.1599 5.72 0.3562 0.4216 0.0217 0.0183 0.002 0.130 0.057 1.538 0.015 0.254 16.819 0.07 27237. 0.1390 5.99 0.3732 0.4014 0.0190 0.0176 0.002 0.125 0.050 1.482 0.014 0.222 15.288 0.07 27267. 0.1183 6.26 0.3901 0.3747 0.0163 0.0169 0.002 0.120 0.043 1.423 0.014 0.190 13.649 0.07 27298. 0.0978 6.53 0.4071 0.3404 0.0135 0.0162 0.002 0.115 0.036 1.361 0.013 0.159 11.882 0.07 27330. 0.0777 6.81 0.4240 0.2972 0.0108 0.0154 0.002 0.109 0.028 1.295 0.012 0.127 9.961 0.07 27364. 0.0582 7.08 0.4410 0.2437 0.0081 0.0146 0.002 0.104 0.021 1.227 0.012 0.094 7.854 0.07 27398. 0.0396 7.35 0.4580 0.1779 0.0053 0.0138 0.002 0.098 0.014 1.155 0.011 0.063 5.522 0.07 27433. 0.0227 7.62 0.4749 0.0972 0.0026 0.0129 0.001 0.091 0.007 1.081 0.010 0.031 2.910 0.07 27469. 0.0084 7.90 0.4919 -0.0024 -0.0001 0.0120 0.001 0.085 0.000 1.004 0.010 -0.001 -0.070 0.07 27506. 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 0.0654 0.0211 0.019 0.598 0.688 14.159 0.068 3.062 22.050 0.13 53657. 0.6333 0.55 0.0170 0.0516 0.0640 0.0211 0.019 0.600 0.674 14.204 0.068 2.997 21.516 0.13 53679. 0.6113 1.09 0.0341 0.1006 0.0626 0.0212 0.019 0.602 0.658 14.235 0.068 2.929 20.980 0.13 53704. 0.5893 1.64 0.0511 0.1470 0.0610 0.0212 0.019 0.602 0.642 14.252 0.068 2.857 20.445 0.13 53729. 0.5672 2.19 0.0681 0.1909 0.0595 0.0212 0.019 0.602 0.626 14.252 0.068 2.783 19.909 0.13 53756. 0.5451 2.73 0.0852 0.2322 0.0578 0.0212 0.019 0.602 0.608 14.235 0.068 2.705 19.374 0.13 53785. 0.5230 3.28 0.1022 0.2709 0.0560 0.0211 0.019 0.600 0.590 14.198 0.068 2.623 18.839 0.13 53815. 0.5008 3.83 0.1192 0.3071 0.0542 0.0210 0.019 0.598 0.571 14.139 0.068 2.538 18.303 0.13 53846. 0.4786 4.37 0.1363 0.3407 0.0523 0.0209 0.019 0.594 0.551 14.057 0.067 2.449 17.765 0.13 53880. 0.4563 4.92 0.1533 0.3716 0.0503 0.0208 0.019 0.590 0.530 13.950 0.067 2.356 17.225 0.13 53915. 0.4340 5.47 0.1703 0.3999 0.0483 0.0206 0.019 0.584 0.508 13.818 0.066 2.261 16.682 0.13 53951. 0.4117 6.01 0.1874 0.4254 0.0462 0.0203 0.018 0.577 0.486 13.661 0.065 2.162 16.135 0.13 53990. 0.3893 6.56 0.2044 0.4482 0.0440 0.0201 0.018 0.570 0.463 13.476 0.064 2.059 15.581 0.13 54030. 0.3670 7.11 0.2214 0.4680 0.0417 0.0197 0.018 0.561 0.439 13.264 0.063 1.954 15.019 0.13 54072. 0.3446 7.65 0.2384 0.4848 0.0394 0.0194 0.017 0.550 0.415 13.024 0.062 1.845 14.448 0.13 54116. 0.3221 8.20 0.2555 0.4985 0.0370 0.0190 0.017 0.539 0.390 12.755 0.061 1.734 13.863 0.13 54162. 0.2996 8.75 0.2725 0.5087 0.0346 0.0185 0.017 0.526 0.364 12.456 0.059 1.620 13.264 0.13 54210. 0.2771 9.30 0.2895 0.5153 0.0321 0.0181 0.016 0.512 0.338 12.126 0.058 1.504 12.645 0.14 54260. 0.2545 9.84 0.3066 0.5178 0.0296 0.0175 0.016 0.497 0.311 11.766 0.056 1.385 12.002 0.14 54312. 0.2318 10.39 0.3236 0.5160 0.0270 0.0169 0.015 0.481 0.284 11.375 0.054 1.264 11.331 0.14 54366. 0.2091 10.94 0.3406 0.5093 0.0244 0.0163 0.015 0.463 0.257 10.953 0.052 1.141 10.624 0.14 54422. 0.1863 11.48 0.3577 0.4970 0.0217 0.0156 0.014 0.444 0.229 10.500 0.050 1.017 9.873 0.14 54480. 0.1634 12.03 0.3747 0.4782 0.0190 0.0149 0.013 0.423 0.200 10.015 0.048 0.891 9.069 0.14 54540. 0.1405 12.58 0.3917 0.4519 0.0163 0.0141 0.013 0.401 0.172 9.500 0.045 0.764 8.197 0.14 54603. 0.1176 13.12 0.4088 0.4166 0.0136 0.0133 0.012 0.378 0.143 8.955 0.043 0.636 7.241 0.14 54667. 0.0948 13.67 0.4258 0.3703 0.0108 0.0125 0.011 0.354 0.114 8.381 0.040 0.508 6.179 0.14 54734. 0.0723 14.22 0.4428 0.3103 0.0081 0.0116 0.010 0.329 0.085 7.779 0.037 0.380 4.979 0.14 54803. 0.0504 14.76 0.4599 0.2329 0.0054 0.0106 0.010 0.302 0.057 7.151 0.034 0.252 3.598 0.14 54874. 0.0297 15.31 0.4769 0.1326 0.0027 0.0097 0.009 0.275 0.028 6.499 0.031 0.126 1.975 0.14 54947. 0.0115 15.86 0.4939 -0.0001 0.0000 0.0087 0.008 0.246 0.000 5.818 0.028 0.000 -0.002 0.14 55020. 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 0.0657 0.0201 0.061 1.281 1.555 45.458 0.145 6.916 15.515 0.20 80484. 0.6697 0.84 0.0174 0.0554 0.0643 0.0201 0.061 1.285 1.521 45.624 0.145 6.767 15.125 0.20 80519. 0.6458 1.67 0.0347 0.1080 0.0628 0.0202 0.061 1.289 1.486 45.743 0.146 6.610 14.736 0.20 80556. 0.6219 2.51 0.0521 0.1578 0.0612 0.0202 0.061 1.291 1.449 45.809 0.146 6.446 14.349 0.20 80595. 0.5979 3.34 0.0694 0.2047 0.0596 0.0202 0.061 1.291 1.410 45.816 0.146 6.274 13.963 0.20 80637. 0.5741 4.18 0.0868 0.2488 0.0579 0.0202 0.061 1.289 1.370 45.758 0.146 6.093 13.579 0.20 80680. 0.5502 5.02 0.1042 0.2902 0.0561 0.0201 0.061 1.286 1.328 45.627 0.145 5.905 13.197 0.20 80727. 0.5264 5.85 0.1215 0.3288 0.0542 0.0200 0.061 1.280 1.283 45.418 0.145 5.708 12.815 0.20 80775. 0.5025 6.69 0.1389 0.3646 0.0522 0.0199 0.061 1.271 1.237 45.125 0.144 5.502 12.434 0.20 80827. 0.4787 7.52 0.1562 0.3976 0.0502 0.0197 0.060 1.261 1.189 44.742 0.142 5.289 12.054 0.20 80881. 0.4550 8.36 0.1736 0.4278 0.0481 0.0195 0.059 1.247 1.139 44.268 0.141 5.067 11.672 0.20 80938. 0.4312 9.20 0.1910 0.4551 0.0459 0.0193 0.059 1.231 1.088 43.698 0.139 4.838 11.289 0.20 80997. 0.4075 10.03 0.2083 0.4795 0.0437 0.0190 0.058 1.212 1.034 43.029 0.137 4.601 10.903 0.20 81059. 0.3838 10.87 0.2257 0.5009 0.0414 0.0186 0.057 1.191 0.979 42.259 0.135 4.357 10.512 0.20 81124. 0.3601 11.70 0.2430 0.5191 0.0390 0.0183 0.055 1.166 0.923 41.385 0.132 4.106 10.116 0.20 81193. 0.3364 12.54 0.2604 0.5339 0.0365 0.0178 0.054 1.138 0.865 40.403 0.129 3.848 9.712 0.20 81264. 0.3127 13.38 0.2778 0.5452 0.0340 0.0173 0.053 1.108 0.806 39.312 0.125 3.585 9.298 0.20 81338. 0.2890 14.21 0.2951 0.5527 0.0315 0.0168 0.051 1.074 0.745 38.109 0.121 3.315 8.871 0.20 81415. 0.2651 15.05 0.3125 0.5560 0.0289 0.0162 0.049 1.037 0.684 36.793 0.117 3.041 8.427 0.20 81496. 0.2412 15.88 0.3298 0.5545 0.0262 0.0156 0.047 0.996 0.621 35.362 0.113 2.761 7.963 0.20 81579. 0.2172 16.72 0.3472 0.5476 0.0235 0.0149 0.045 0.953 0.557 33.816 0.108 2.478 7.471 0.20 81666. 0.1930 17.56 0.3646 0.5346 0.0208 0.0142 0.043 0.906 0.492 32.154 0.102 2.190 6.946 0.20 81756. 0.1687 18.39 0.3819 0.5142 0.0180 0.0134 0.041 0.856 0.427 30.379 0.097 1.900 6.378 0.20 81850. 0.1443 19.23 0.3993 0.4850 0.0153 0.0126 0.038 0.803 0.361 28.491 0.091 1.608 5.754 0.20 81947. 0.1197 20.06 0.4167 0.4448 0.0125 0.0117 0.036 0.746 0.295 26.494 0.084 1.314 5.057 0.20 82047. 0.0951 20.90 0.4340 0.3907 0.0097 0.0108 0.033 0.687 0.229 24.393 0.078 1.020 4.264 0.20 82151. 0.0707 21.74 0.4514 0.3182 0.0069 0.0098 0.030 0.625 0.163 22.193 0.071 0.727 3.340 0.20 82258. 0.0467 22.57 0.4687 0.2209 0.0041 0.0088 0.027 0.561 0.098 19.901 0.063 0.436 2.232 0.20 82368. 0.0242 23.41 0.4861 0.0878 0.0014 0.0077 0.023 0.494 0.033 17.520 0.056 0.147 0.856 0.20 82481. 0.0054 24.24 0.5035 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 0.0660 0.0195 0.141 2.214 2.778 104.782 0.250 12.356 12.025 0.27 107309. 0.6938 1.10 0.0171 0.0564 0.0646 0.0196 0.141 2.223 2.719 105.186 0.251 12.094 11.725 0.27 107355. 0.6693 2.19 0.0342 0.1099 0.0631 0.0196 0.141 2.229 2.657 105.480 0.252 11.819 11.426 0.27 107404. 0.6448 3.29 0.0512 0.1605 0.0616 0.0197 0.142 2.232 2.592 105.649 0.252 11.531 11.130 0.27 107456. 0.6203 4.39 0.0683 0.2084 0.0600 0.0197 0.142 2.233 2.525 105.681 0.252 11.230 10.835 0.27 107510. 0.5960 5.48 0.0854 0.2534 0.0583 0.0196 0.142 2.231 2.454 105.561 0.252 10.914 10.543 0.27 107567. 0.5717 6.58 0.1025 0.2958 0.0565 0.0196 0.141 2.225 2.380 105.274 0.251 10.584 10.252 0.27 107628. 0.5475 7.68 0.1196 0.3353 0.0547 0.0195 0.141 2.215 2.302 104.804 0.250 10.240 9.963 0.27 107692. 0.5233 8.77 0.1366 0.3721 0.0528 0.0194 0.140 2.200 2.221 104.137 0.249 9.881 9.675 0.27 107759. 0.4992 9.87 0.1537 0.4063 0.0508 0.0192 0.138 2.182 2.137 103.262 0.247 9.507 9.389 0.27 107829. 0.4751 10.97 0.1708 0.4376 0.0487 0.0190 0.137 2.159 2.050 102.172 0.244 9.120 9.102 0.27 107903. 0.4512 12.06 0.1879 0.4662 0.0466 0.0188 0.135 2.131 1.960 100.859 0.241 8.719 8.815 0.27 107981. 0.4273 13.16 0.2050 0.4920 0.0444 0.0185 0.133 2.099 1.867 99.314 0.237 8.306 8.528 0.27 108062. 0.4034 14.26 0.2221 0.5149 0.0421 0.0181 0.131 2.061 1.771 97.531 0.233 7.879 8.238 0.27 108147. 0.3796 15.35 0.2391 0.5348 0.0397 0.0178 0.128 2.018 1.673 95.504 0.228 7.441 7.945 0.27 108235. 0.3557 16.45 0.2562 0.5515 0.0373 0.0173 0.125 1.970 1.572 93.224 0.223 6.992 7.648 0.27 108328. 0.3319 17.55 0.2733 0.5650 0.0349 0.0169 0.122 1.916 1.468 90.686 0.216 6.531 7.344 0.27 108424. 0.3081 18.64 0.2904 0.5748 0.0324 0.0164 0.118 1.857 1.363 87.886 0.210 6.061 7.032 0.27 108525. 0.2842 19.74 0.3075 0.5807 0.0298 0.0158 0.114 1.792 1.255 84.818 0.202 5.581 6.710 0.27 108629. 0.2602 20.84 0.3245 0.5823 0.0272 0.0152 0.109 1.722 1.145 81.479 0.195 5.093 6.374 0.27 108737. 0.2361 21.93 0.3416 0.5789 0.0246 0.0145 0.104 1.645 1.034 77.868 0.186 4.597 6.020 0.27 108850. 0.2119 23.03 0.3587 0.5698 0.0219 0.0138 0.099 1.563 0.921 73.984 0.177 4.095 5.644 0.27 108967. 0.1874 24.13 0.3758 0.5540 0.0192 0.0130 0.094 1.476 0.806 69.829 0.167 3.587 5.238 0.27 109088. 0.1628 25.22 0.3929 0.5301 0.0164 0.0122 0.088 1.382 0.691 65.406 0.156 3.075 4.794 0.27 109214. 0.1380 26.32 0.4099 0.4960 0.0137 0.0113 0.081 1.283 0.575 60.722 0.145 2.560 4.299 0.27 109344. 0.1129 27.42 0.4270 0.4490 0.0109 0.0104 0.075 1.179 0.459 55.786 0.133 2.044 3.736 0.27 109478. 0.0877 28.51 0.4441 0.3850 0.0082 0.0094 0.068 1.069 0.344 50.610 0.121 1.529 3.080 0.27 109617. 0.0625 29.61 0.4612 0.2974 0.0054 0.0084 0.061 0.955 0.228 45.211 0.108 1.016 2.291 0.27 109760. 0.0379 30.71 0.4783 0.1760 0.0027 0.0074 0.053 0.837 0.114 39.602 0.095 0.508 1.307 0.27 109906. 0.0153 31.80 0.4953 -0.0005 0.0000 0.0063 0.045 0.713 0.000 33.723 0.081 -0.001 -0.003 0.27 110048. 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 0.0664 0.0192 0.270 3.404 4.367 201.395 0.385 19.425 9.835 0.34 134133. 0.7115 1.38 0.0172 0.0580 0.0650 0.0193 0.271 3.418 4.274 202.202 0.386 19.011 9.587 0.34 134191. 0.6861 2.76 0.0344 0.1130 0.0635 0.0193 0.272 3.428 4.176 202.785 0.387 18.576 9.341 0.34 134253. 0.6608 4.14 0.0516 0.1651 0.0619 0.0194 0.272 3.434 4.074 203.118 0.388 18.120 9.097 0.34 134318. 0.6356 5.52 0.0688 0.2143 0.0603 0.0194 0.272 3.435 3.966 203.173 0.388 17.642 8.855 0.34 134387. 0.6104 6.90 0.0860 0.2606 0.0586 0.0193 0.272 3.430 3.854 202.921 0.388 17.142 8.614 0.34 134459. 0.5854 8.28 0.1032 0.3041 0.0568 0.0193 0.271 3.420 3.736 202.331 0.386 16.620 8.376 0.34 134536. 0.5605 9.66 0.1204 0.3447 0.0549 0.0192 0.270 3.404 3.614 201.371 0.385 16.074 8.140 0.34 134616. 0.5356 11.04 0.1376 0.3826 0.0530 0.0191 0.268 3.381 3.486 200.011 0.382 15.505 7.905 0.34 134701. 0.5109 12.42 0.1548 0.4177 0.0510 0.0189 0.266 3.351 3.353 198.232 0.379 14.913 7.671 0.34 134790. 0.4862 13.80 0.1720 0.4501 0.0489 0.0187 0.263 3.314 3.215 196.016 0.374 14.298 7.438 0.34 134884. 0.4617 15.18 0.1892 0.4796 0.0467 0.0184 0.259 3.268 3.072 193.347 0.369 13.663 7.206 0.34 134982. 0.4372 16.56 0.2064 0.5063 0.0445 0.0181 0.255 3.215 2.924 190.211 0.363 13.006 6.973 0.34 135085. 0.4127 17.94 0.2236 0.5300 0.0421 0.0178 0.250 3.154 2.772 186.590 0.356 12.330 6.739 0.34 135192. 0.3884 19.32 0.2408 0.5508 0.0398 0.0174 0.245 3.085 2.616 182.472 0.348 11.635 6.502 0.34 135304. 0.3640 20.70 0.2580 0.5684 0.0373 0.0169 0.238 3.006 2.456 177.843 0.340 10.922 6.263 0.34 135421. 0.3397 22.08 0.2751 0.5826 0.0348 0.0165 0.232 2.919 2.291 172.691 0.330 10.192 6.018 0.34 135543. 0.3154 23.46 0.2923 0.5933 0.0323 0.0159 0.224 2.823 2.124 167.004 0.319 9.446 5.768 0.34 135670. 0.2910 24.84 0.3095 0.6000 0.0297 0.0153 0.216 2.718 1.953 160.775 0.307 8.686 5.509 0.34 135802. 0.2665 26.22 0.3267 0.6023 0.0270 0.0147 0.207 2.603 1.779 153.997 0.294 7.912 5.239 0.34 135939. 0.2419 27.60 0.3439 0.5995 0.0244 0.0140 0.197 2.479 1.602 146.666 0.280 7.125 4.954 0.34 136082. 0.2171 28.98 0.3611 0.5909 0.0216 0.0132 0.186 2.346 1.423 138.782 0.265 6.329 4.650 0.34 136230. 0.1920 30.36 0.3783 0.5753 0.0189 0.0124 0.175 2.203 1.242 130.349 0.249 5.524 4.322 0.34 136383. 0.1667 31.74 0.3955 0.5511 0.0161 0.0116 0.163 2.052 1.060 121.375 0.232 4.713 3.960 0.34 136542. 0.1411 33.12 0.4127 0.5160 0.0133 0.0107 0.150 1.891 0.876 111.874 0.214 3.898 3.553 0.34 136706. 0.1152 34.50 0.4299 0.4667 0.0105 0.0097 0.137 1.722 0.693 101.867 0.195 3.082 3.085 0.34 136876. 0.0889 35.88 0.4471 0.3981 0.0078 0.0087 0.123 1.545 0.510 91.379 0.175 2.268 2.531 0.34 137052. 0.0625 37.26 0.4643 0.3019 0.0050 0.0077 0.108 1.360 0.328 80.444 0.154 1.458 1.848 0.34 137233. 0.0366 38.64 0.4815 0.1639 0.0022 0.0066 0.093 1.168 0.147 69.091 0.132 0.656 0.968 0.34 137418. 0.0129 40.02 0.4987 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 0.0669 0.0190 0.463 4.863 6.336 345.187 0.549 28.183 8.326 0.40 160954. 0.7254 1.65 0.0171 0.0586 0.0655 0.0191 0.465 4.882 6.202 346.577 0.552 27.587 8.117 0.40 161024. 0.6997 3.29 0.0342 0.1141 0.0640 0.0192 0.466 4.896 6.061 347.579 0.553 26.960 7.910 0.40 161097. 0.6741 4.94 0.0513 0.1667 0.0624 0.0192 0.467 4.904 5.914 348.144 0.554 26.304 7.704 0.40 161175. 0.6486 6.58 0.0683 0.2165 0.0608 0.0192 0.467 4.906 5.759 348.228 0.554 25.616 7.501 0.40 161257. 0.6231 8.23 0.0854 0.2633 0.0591 0.0192 0.466 4.899 5.597 347.779 0.554 24.897 7.300 0.40 161344. 0.5979 9.87 0.1025 0.3073 0.0573 0.0191 0.465 4.885 5.428 346.746 0.552 24.145 7.101 0.40 161436. 0.5727 11.52 0.1196 0.3486 0.0555 0.0190 0.463 4.861 5.252 345.071 0.549 23.360 6.903 0.40 161532. 0.5476 13.16 0.1367 0.3871 0.0535 0.0189 0.460 4.828 5.068 342.704 0.545 22.541 6.707 0.40 161633. 0.5227 14.81 0.1538 0.4228 0.0515 0.0187 0.455 4.784 4.876 339.610 0.541 21.689 6.512 0.40 161739. 0.4978 16.46 0.1709 0.4558 0.0494 0.0185 0.450 4.730 4.678 335.756 0.534 20.806 6.319 0.40 161851. 0.4731 18.10 0.1879 0.4861 0.0472 0.0183 0.444 4.664 4.472 331.117 0.527 19.892 6.126 0.40 161967. 0.4484 19.75 0.2050 0.5136 0.0450 0.0180 0.437 4.588 4.260 325.666 0.518 18.948 5.933 0.40 162090. 0.4239 21.39 0.2221 0.5382 0.0427 0.0176 0.428 4.499 4.041 319.375 0.508 17.975 5.739 0.40 162217. 0.3994 23.04 0.2392 0.5599 0.0403 0.0172 0.419 4.398 3.816 312.220 0.497 16.976 5.544 0.40 162351. 0.3749 24.68 0.2563 0.5786 0.0379 0.0168 0.408 4.285 3.586 304.178 0.484 15.950 5.347 0.40 162490. 0.3505 26.33 0.2734 0.5940 0.0354 0.0163 0.396 4.159 3.350 295.227 0.470 14.900 5.146 0.40 162635. 0.3261 27.97 0.2905 0.6060 0.0328 0.0157 0.383 4.020 3.109 285.349 0.454 13.827 4.941 0.41 162786. 0.3016 29.62 0.3075 0.6141 0.0302 0.0151 0.368 3.867 2.862 274.527 0.437 12.732 4.729 0.41 162943. 0.2770 31.27 0.3246 0.6180 0.0276 0.0145 0.352 3.701 2.612 262.751 0.418 11.618 4.509 0.41 163106. 0.2523 32.91 0.3417 0.6171 0.0249 0.0138 0.335 3.522 2.358 250.013 0.398 10.487 4.277 0.41 163275. 0.2273 34.56 0.3588 0.6106 0.0222 0.0130 0.317 3.329 2.100 236.313 0.376 9.340 4.031 0.41 163451. 0.2022 36.20 0.3759 0.5974 0.0194 0.0122 0.297 3.122 1.839 221.656 0.353 8.182 3.764 0.41 163633. 0.1767 37.85 0.3930 0.5759 0.0166 0.0114 0.276 2.903 1.577 206.055 0.328 7.014 3.471 0.41 163821. 0.1509 39.49 0.4101 0.5439 0.0139 0.0105 0.254 2.670 1.313 189.533 0.302 5.839 3.142 0.41 164016. 0.1246 41.14 0.4271 0.4981 0.0111 0.0095 0.231 2.425 1.048 172.123 0.274 4.662 2.762 0.41 164218. 0.0979 42.78 0.4442 0.4335 0.0083 0.0085 0.206 2.168 0.784 153.871 0.245 3.487 2.311 0.41 164426. 0.0708 44.43 0.4613 0.3415 0.0055 0.0074 0.181 1.899 0.521 134.834 0.215 2.318 1.753 0.41 164641. 0.0438 46.07 0.4784 0.2076 0.0028 0.0063 0.154 1.621 0.261 115.065 0.183 1.160 1.028 0.41 164861. 0.0182 47.72 0.4955 -0.0008 0.0000 0.0052 0.126 1.328 -0.001 94.272 0.150 -0.004 -0.004 0.41 165071. 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 0.0675 0.0190 0.734 6.605 8.703 547.011 0.746 38.710 7.216 0.47 187772. 0.7369 1.92 0.0171 0.0593 0.0661 0.0191 0.736 6.631 8.519 549.201 0.749 37.891 7.035 0.47 187854. 0.7108 3.84 0.0342 0.1155 0.0646 0.0191 0.739 6.650 8.325 550.759 0.751 37.030 6.856 0.47 187940. 0.6848 5.76 0.0513 0.1688 0.0630 0.0192 0.740 6.660 8.122 551.609 0.752 36.128 6.679 0.47 188031. 0.6589 7.69 0.0684 0.2191 0.0614 0.0192 0.740 6.661 7.910 551.675 0.753 35.183 6.503 0.47 188128. 0.6331 9.61 0.0855 0.2666 0.0596 0.0191 0.739 6.652 7.687 550.877 0.751 34.194 6.330 0.47 188229. 0.6075 11.53 0.1026 0.3112 0.0578 0.0191 0.736 6.631 7.455 549.131 0.749 33.160 6.158 0.47 188337. 0.5820 13.45 0.1197 0.3531 0.0560 0.0190 0.733 6.597 7.212 546.344 0.745 32.081 5.988 0.47 188449. 0.5567 15.37 0.1368 0.3922 0.0540 0.0188 0.727 6.550 6.959 542.435 0.740 30.955 5.819 0.47 188568. 0.5314 17.29 0.1539 0.4285 0.0519 0.0187 0.721 6.488 6.696 537.344 0.733 29.784 5.652 0.47 188693. 0.5063 19.22 0.1710 0.4621 0.0498 0.0184 0.712 6.412 6.423 531.021 0.724 28.568 5.486 0.47 188823. 0.4813 21.14 0.1881 0.4930 0.0476 0.0182 0.702 6.320 6.140 523.424 0.714 27.311 5.321 0.47 188960. 0.4564 23.06 0.2052 0.5211 0.0454 0.0179 0.690 6.212 5.848 514.508 0.702 26.013 5.155 0.47 189103. 0.4316 24.98 0.2223 0.5465 0.0430 0.0175 0.676 6.088 5.547 504.230 0.688 24.675 4.990 0.47 189253. 0.4068 26.90 0.2394 0.5689 0.0406 0.0171 0.661 5.947 5.238 492.551 0.672 23.299 4.824 0.47 189409. 0.3822 28.82 0.2565 0.5883 0.0382 0.0166 0.643 5.789 4.921 479.434 0.654 21.888 4.655 0.47 189572. 0.3575 30.74 0.2736 0.6044 0.0357 0.0161 0.623 5.613 4.596 464.842 0.634 20.443 4.485 0.47 189741. 0.3328 32.67 0.2907 0.6172 0.0331 0.0156 0.602 5.418 4.264 448.746 0.612 18.967 4.310 0.47 189918. 0.3081 34.59 0.3078 0.6262 0.0305 0.0150 0.578 5.206 3.926 431.122 0.588 17.461 4.130 0.47 190102. 0.2833 36.51 0.3249 0.6310 0.0278 0.0143 0.552 4.974 3.581 411.950 0.562 15.928 3.943 0.47 190292. 0.2583 38.43 0.3420 0.6311 0.0251 0.0136 0.525 4.724 3.231 391.220 0.534 14.371 3.746 0.47 190491. 0.2331 40.35 0.3591 0.6256 0.0223 0.0128 0.495 4.455 2.876 368.930 0.503 12.794 3.536 0.47 190696. 0.2076 42.27 0.3762 0.6133 0.0195 0.0120 0.463 4.167 2.518 345.090 0.471 11.200 3.309 0.47 190909. 0.1818 44.19 0.3933 0.5927 0.0167 0.0111 0.429 3.861 2.156 319.722 0.436 9.592 3.059 0.47 191129. 0.1555 46.12 0.4104 0.5615 0.0139 0.0102 0.393 3.536 1.793 292.863 0.400 7.976 2.777 0.47 191357. 0.1287 48.04 0.4275 0.5160 0.0111 0.0092 0.355 3.195 1.429 264.569 0.361 6.357 2.450 0.47 191593. 0.1014 49.96 0.4446 0.4507 0.0083 0.0082 0.315 2.836 1.066 234.914 0.320 4.741 2.058 0.48 191836. 0.0735 51.88 0.4617 0.3562 0.0055 0.0071 0.274 2.463 0.704 203.991 0.278 3.133 1.566 0.48 192087. 0.0455 53.80 0.4788 0.2154 0.0027 0.0060 0.231 2.075 0.346 171.889 0.234 1.540 0.913 0.48 192345. 0.0186 55.72 0.4959 -0.0128 -0.0001 0.0048 0.185 1.665 -0.016 137.903 0.188 -0.071 -0.053 0.48 192581. 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 0.0682 0.0191 1.098 8.654 11.491 819.102 0.978 51.111 6.363 0.54 214586. 0.7467 2.23 0.0173 0.0606 0.0668 0.0191 1.103 8.688 11.244 822.354 0.982 50.015 6.202 0.54 214681. 0.7199 4.46 0.0347 0.1180 0.0652 0.0192 1.106 8.712 10.985 824.607 0.984 48.861 6.042 0.54 214782. 0.6932 6.68 0.0520 0.1724 0.0636 0.0192 1.107 8.724 10.713 825.740 0.986 47.651 5.884 0.54 214888. 0.6667 8.91 0.0694 0.2238 0.0619 0.0192 1.107 8.723 10.428 825.635 0.986 46.383 5.729 0.54 215001. 0.6404 11.14 0.0867 0.2722 0.0602 0.0192 1.105 8.708 10.129 824.168 0.984 45.055 5.575 0.54 215120. 0.6142 13.37 0.1041 0.3177 0.0583 0.0191 1.101 8.676 9.817 821.201 0.980 43.666 5.422 0.54 215245. 0.5881 15.59 0.1214 0.3604 0.0564 0.0190 1.095 8.628 9.491 816.591 0.975 42.215 5.272 0.54 215377. 0.5622 17.82 0.1388 0.4002 0.0543 0.0188 1.087 8.560 9.150 810.210 0.967 40.700 5.122 0.54 215516. 0.5364 20.05 0.1561 0.4372 0.0522 0.0187 1.075 8.473 8.796 801.963 0.957 39.124 4.975 0.54 215662. 0.5107 22.28 0.1735 0.4715 0.0501 0.0184 1.062 8.365 8.428 791.777 0.945 37.488 4.828 0.54 215815. 0.4852 24.50 0.1908 0.5030 0.0478 0.0181 1.045 8.236 8.047 779.580 0.931 35.794 4.682 0.54 215975. 0.4598 26.73 0.2082 0.5316 0.0455 0.0178 1.026 8.086 7.654 765.306 0.914 34.045 4.536 0.54 216143. 0.4344 28.96 0.2255 0.5574 0.0431 0.0174 1.004 7.912 7.249 748.889 0.894 32.243 4.390 0.54 216318. 0.4092 31.19 0.2429 0.5802 0.0406 0.0170 0.979 7.715 6.832 730.266 0.872 30.390 4.244 0.54 216501. 0.3840 33.41 0.2602 0.5999 0.0380 0.0165 0.951 7.495 6.405 709.379 0.847 28.489 4.095 0.54 216692. 0.3588 35.64 0.2776 0.6163 0.0354 0.0160 0.920 7.250 5.967 686.173 0.819 26.542 3.944 0.54 216891. 0.3335 37.87 0.2949 0.6292 0.0328 0.0154 0.886 6.979 5.520 660.605 0.789 24.553 3.790 0.54 217098. 0.3082 40.10 0.3123 0.6382 0.0301 0.0147 0.848 6.684 5.064 632.636 0.755 22.524 3.631 0.54 217313. 0.2828 42.32 0.3296 0.6428 0.0273 0.0140 0.808 6.363 4.600 602.242 0.719 20.460 3.464 0.54 217537. 0.2572 44.55 0.3470 0.6424 0.0245 0.0132 0.764 6.016 4.129 569.407 0.680 18.365 3.289 0.54 217769. 0.2313 46.78 0.3643 0.6359 0.0217 0.0124 0.716 5.643 3.652 534.136 0.638 16.243 3.101 0.54 218010. 0.2051 49.01 0.3816 0.6222 0.0188 0.0115 0.666 5.245 3.170 496.449 0.593 14.098 2.896 0.54 218260. 0.1785 51.24 0.3990 0.5991 0.0159 0.0106 0.612 4.822 2.684 456.390 0.545 11.939 2.667 0.54 218518. 0.1513 53.46 0.4163 0.5639 0.0130 0.0096 0.555 4.374 2.196 414.027 0.494 9.769 2.406 0.54 218786. 0.1234 55.69 0.4337 0.5120 0.0101 0.0086 0.495 3.903 1.708 369.458 0.441 7.598 2.097 0.54 219062. 0.0949 57.92 0.4510 0.4358 0.0073 0.0075 0.433 3.411 1.222 322.816 0.385 5.434 1.716 0.54 219348. 0.0657 60.15 0.4684 0.3220 0.0044 0.0064 0.368 2.898 0.738 274.256 0.327 3.284 1.221 0.54 219642. 0.0363 62.37 0.4857 0.1438 0.0015 0.0052 0.300 2.365 0.260 223.849 0.267 1.155 0.526 0.54 219941. 0.0093 64.60 0.5031 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 0.0691 0.0192 1.577 11.042 14.732 1175.717 1.247 65.527 5.683 0.61 241393. 0.7551 2.47 0.0171 0.0599 0.0677 0.0193 1.583 11.083 14.421 1180.158 1.252 64.146 5.543 0.61 241499. 0.7286 4.93 0.0341 0.1168 0.0661 0.0193 1.587 11.112 14.095 1183.183 1.255 62.693 5.403 0.61 241612. 0.7022 7.40 0.0512 0.1708 0.0645 0.0194 1.589 11.125 13.752 1184.626 1.257 61.170 5.265 0.61 241731. 0.6759 9.87 0.0683 0.2218 0.0629 0.0193 1.588 11.122 13.394 1184.322 1.257 59.575 5.129 0.61 241856. 0.6498 12.33 0.0854 0.2700 0.0611 0.0193 1.585 11.102 13.018 1182.100 1.254 57.906 4.995 0.61 241988. 0.6239 14.80 0.1024 0.3154 0.0593 0.0192 1.579 11.061 12.626 1177.776 1.250 56.161 4.862 0.61 242127. 0.5981 17.26 0.1195 0.3581 0.0573 0.0191 1.571 10.999 12.216 1171.155 1.243 54.337 4.731 0.61 242273. 0.5724 19.73 0.1366 0.3980 0.0553 0.0190 1.558 10.913 11.789 1162.050 1.233 52.436 4.601 0.61 242427. 0.5469 22.20 0.1536 0.4352 0.0532 0.0188 1.543 10.803 11.344 1150.325 1.221 50.456 4.473 0.61 242588. 0.5215 24.66 0.1707 0.4698 0.0511 0.0186 1.523 10.667 10.882 1135.876 1.205 48.402 4.345 0.61 242757. 0.4962 27.13 0.1878 0.5017 0.0488 0.0183 1.500 10.505 10.404 1118.608 1.187 46.276 4.218 0.61 242933. 0.4710 29.60 0.2049 0.5309 0.0465 0.0179 1.473 10.316 9.910 1098.426 1.165 44.080 4.092 0.61 243118. 0.4459 32.06 0.2219 0.5574 0.0441 0.0176 1.442 10.098 9.401 1075.244 1.141 41.818 3.966 0.61 243311. 0.4209 34.53 0.2390 0.5811 0.0417 0.0171 1.407 9.851 8.878 1048.974 1.113 39.491 3.839 0.61 243513. 0.3960 36.99 0.2561 0.6019 0.0391 0.0167 1.367 9.575 8.342 1019.536 1.082 37.104 3.711 0.61 243722. 0.3710 39.46 0.2732 0.6195 0.0366 0.0161 1.323 9.268 7.792 986.855 1.047 34.658 3.581 0.61 243941. 0.3461 41.93 0.2902 0.6339 0.0339 0.0155 1.275 8.930 7.230 950.867 1.009 32.159 3.449 0.61 244168. 0.3210 44.39 0.3073 0.6447 0.0312 0.0149 1.222 8.560 6.657 911.517 0.967 29.610 3.312 0.61 244405. 0.2959 46.86 0.3244 0.6514 0.0285 0.0142 1.165 8.159 6.073 868.767 0.922 27.015 3.171 0.61 244650. 0.2705 49.33 0.3414 0.6535 0.0257 0.0134 1.103 7.725 5.481 822.594 0.873 24.379 3.022 0.61 244905. 0.2449 51.79 0.3585 0.6502 0.0229 0.0126 1.037 7.259 4.880 772.993 0.820 21.707 2.864 0.61 245169. 0.2190 54.26 0.3756 0.6403 0.0201 0.0118 0.966 6.762 4.273 719.988 0.764 19.006 2.692 0.61 245442. 0.1926 56.72 0.3927 0.6222 0.0172 0.0108 0.890 6.232 3.661 663.627 0.704 16.283 2.502 0.61 245725. 0.1657 59.19 0.4097 0.5934 0.0143 0.0099 0.810 5.672 3.045 603.993 0.641 13.544 2.287 0.61 246018. 0.1381 61.66 0.4268 0.5500 0.0114 0.0088 0.726 5.083 2.428 541.208 0.574 10.800 2.035 0.61 246320. 0.1098 64.12 0.4439 0.4859 0.0085 0.0078 0.638 4.465 1.812 475.439 0.504 8.059 1.728 0.61 246632. 0.0805 66.59 0.4609 0.3901 0.0056 0.0066 0.546 3.821 1.199 406.893 0.432 5.333 1.336 0.61 246954. 0.0507 69.06 0.4780 0.2418 0.0028 0.0055 0.450 3.153 0.591 335.772 0.356 2.630 0.799 0.61 247284. 0.0213 71.52 0.4951 -0.0133 -0.0001 0.0043 0.349 2.445 -0.024 260.332 0.276 -0.108 -0.042 0.61 247582. 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 0.0702 0.0195 2.191 13.812 18.468 1634.136 1.560 82.146 5.126 0.67 268194. 0.7626 2.75 0.0172 0.0604 0.0687 0.0195 2.199 13.862 18.077 1640.013 1.566 80.408 5.000 0.67 268314. 0.7358 5.51 0.0343 0.1177 0.0672 0.0196 2.204 13.894 17.666 1643.856 1.570 78.579 4.874 0.67 268440. 0.7092 8.26 0.0515 0.1721 0.0655 0.0196 2.207 13.908 17.235 1645.428 1.571 76.661 4.751 0.67 268574. 0.6828 11.01 0.0686 0.2235 0.0638 0.0196 2.205 13.900 16.783 1644.500 1.570 74.651 4.629 0.67 268715. 0.6564 13.77 0.0858 0.2721 0.0620 0.0195 2.200 13.869 16.310 1640.833 1.567 72.547 4.509 0.67 268864. 0.6303 16.52 0.1029 0.3179 0.0601 0.0195 2.191 13.812 15.815 1634.167 1.561 70.347 4.390 0.67 269020. 0.6043 19.28 0.1201 0.3610 0.0582 0.0193 2.178 13.728 15.298 1624.225 1.551 68.047 4.272 0.67 269185. 0.5784 22.03 0.1372 0.4014 0.0561 0.0192 2.160 13.614 14.759 1610.745 1.538 65.648 4.156 0.67 269358. 0.5527 24.78 0.1544 0.4390 0.0540 0.0190 2.137 13.469 14.197 1593.528 1.522 63.149 4.041 0.67 269539. 0.5271 27.54 0.1716 0.4741 0.0518 0.0187 2.109 13.291 13.614 1572.432 1.502 60.556 3.927 0.67 269729. 0.5016 30.29 0.1887 0.5064 0.0495 0.0184 2.075 13.078 13.011 1547.324 1.478 57.871 3.814 0.67 269928. 0.4762 33.04 0.2059 0.5361 0.0471 0.0181 2.036 12.831 12.387 1518.075 1.450 55.097 3.701 0.67 270136. 0.4509 35.80 0.2230 0.5631 0.0446 0.0177 1.991 12.548 11.744 1484.564 1.418 52.239 3.588 0.67 270353. 0.4257 38.55 0.2402 0.5873 0.0421 0.0172 1.940 12.228 11.083 1446.672 1.381 49.299 3.475 0.67 270579. 0.4005 41.30 0.2573 0.6086 0.0396 0.0167 1.883 11.869 10.405 1404.285 1.341 46.282 3.361 0.67 270815. 0.3753 44.06 0.2745 0.6268 0.0369 0.0162 1.820 11.472 9.711 1357.303 1.296 43.192 3.245 0.67 271060. 0.3500 46.81 0.2916 0.6417 0.0342 0.0155 1.751 11.036 9.000 1305.636 1.247 40.034 3.127 0.68 271316. 0.3247 49.57 0.3088 0.6529 0.0315 0.0149 1.675 10.559 8.276 1249.214 1.193 36.812 3.005 0.68 271581. 0.2992 52.32 0.3259 0.6602 0.0287 0.0141 1.593 10.041 7.539 1187.982 1.134 33.532 2.878 0.68 271857. 0.2736 55.07 0.3431 0.6627 0.0258 0.0134 1.505 9.483 6.790 1121.912 1.071 30.200 2.745 0.68 272142. 0.2476 57.83 0.3603 0.6598 0.0229 0.0125 1.409 8.883 6.031 1051.004 1.004 26.824 2.603 0.68 272439. 0.2212 60.58 0.3774 0.6501 0.0200 0.0116 1.308 8.243 5.263 975.294 0.931 23.411 2.448 0.68 272745. 0.1944 63.33 0.3946 0.6318 0.0171 0.0107 1.200 7.564 4.490 894.860 0.855 19.970 2.276 0.68 273063. 0.1669 66.09 0.4117 0.6023 0.0141 0.0096 1.086 6.845 3.712 809.830 0.773 16.511 2.079 0.68 273391. 0.1387 68.84 0.4289 0.5573 0.0111 0.0086 0.966 6.089 2.933 720.394 0.688 13.045 1.846 0.68 273730. 0.1095 71.59 0.4460 0.4894 0.0082 0.0075 0.841 5.298 2.155 626.813 0.599 9.585 1.559 0.68 274080. 0.0792 74.35 0.4632 0.3858 0.0053 0.0063 0.710 4.475 1.382 529.405 0.506 6.146 1.184 0.68 274441. 0.0482 77.10 0.4803 0.2202 0.0023 0.0051 0.575 3.621 0.615 428.454 0.409 2.737 0.651 0.68 274810. 0.0177 79.86 0.4975 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 0.0715 0.0198 2.973 17.034 22.758 2216.889 1.925 101.226 4.656 0.74 294986. 0.7689 3.03 0.0172 0.0604 0.0700 0.0199 2.983 17.090 22.277 2224.183 1.931 99.087 4.543 0.74 295119. 0.7422 6.06 0.0343 0.1178 0.0684 0.0199 2.989 17.125 21.771 2228.676 1.935 96.836 4.431 0.74 295259. 0.7156 9.09 0.0515 0.1722 0.0667 0.0200 2.991 17.135 21.240 2230.035 1.936 94.474 4.320 0.74 295408. 0.6892 12.12 0.0687 0.2238 0.0650 0.0199 2.988 17.119 20.683 2227.942 1.934 91.997 4.211 0.74 295565. 0.6629 15.16 0.0858 0.2726 0.0631 0.0199 2.980 17.074 20.100 2222.074 1.929 89.404 4.103 0.74 295730. 0.6367 18.19 0.1030 0.3186 0.0612 0.0198 2.966 16.997 19.490 2212.081 1.920 86.692 3.996 0.74 295904. 0.6107 21.22 0.1202 0.3619 0.0592 0.0197 2.947 16.886 18.853 2197.589 1.908 83.856 3.891 0.74 296086. 0.5848 24.25 0.1373 0.4026 0.0571 0.0195 2.921 16.737 18.187 2178.241 1.891 80.896 3.787 0.74 296278. 0.5591 27.28 0.1545 0.4406 0.0550 0.0193 2.888 16.549 17.494 2153.760 1.870 77.814 3.684 0.74 296479. 0.5334 30.31 0.1717 0.4760 0.0527 0.0190 2.848 16.320 16.774 2123.952 1.844 74.613 3.582 0.74 296690. 0.5079 33.34 0.1888 0.5088 0.0504 0.0187 2.801 16.049 16.029 2088.640 1.813 71.298 3.481 0.74 296910. 0.4824 36.37 0.2060 0.5390 0.0479 0.0183 2.746 15.734 15.259 2047.661 1.778 67.872 3.380 0.74 297140. 0.4570 39.40 0.2232 0.5665 0.0454 0.0179 2.683 15.374 14.465 2000.852 1.737 64.342 3.279 0.74 297380. 0.4317 42.43 0.2403 0.5912 0.0429 0.0174 2.612 14.969 13.649 1948.063 1.691 60.710 3.178 0.74 297631. 0.4064 45.47 0.2575 0.6131 0.0402 0.0169 2.533 14.516 12.811 1889.158 1.640 56.983 3.076 0.74 297892. 0.3811 48.50 0.2747 0.6319 0.0375 0.0163 2.446 14.015 11.952 1824.017 1.583 53.165 2.972 0.74 298163. 0.3557 51.53 0.2918 0.6475 0.0348 0.0157 2.350 13.466 11.075 1752.540 1.521 49.261 2.866 0.74 298445. 0.3302 54.56 0.3090 0.6594 0.0320 0.0150 2.246 12.868 10.179 1674.656 1.454 45.278 2.757 0.74 298738. 0.3045 57.59 0.3262 0.6674 0.0291 0.0142 2.133 12.220 9.268 1590.325 1.381 41.224 2.643 0.74 299043. 0.2786 60.62 0.3433 0.6706 0.0262 0.0134 2.011 11.522 8.342 1499.553 1.302 37.104 2.523 0.74 299358. 0.2523 63.65 0.3605 0.6681 0.0233 0.0125 1.881 10.776 7.403 1402.389 1.217 32.929 2.394 0.74 299685. 0.2255 66.68 0.3777 0.6588 0.0203 0.0116 1.742 9.981 6.454 1298.950 1.128 28.708 2.254 0.74 300023. 0.1982 69.71 0.3948 0.6407 0.0173 0.0106 1.595 9.139 5.497 1189.420 1.033 24.451 2.096 0.75 300373. 0.1701 72.75 0.4120 0.6107 0.0142 0.0096 1.440 8.253 4.535 1074.067 0.932 20.171 1.915 0.75 300735. 0.1412 75.78 0.4292 0.5644 0.0112 0.0085 1.278 7.325 3.571 953.254 0.828 15.882 1.699 0.75 301109. 0.1111 78.81 0.4463 0.4939 0.0082 0.0074 1.110 6.358 2.608 827.448 0.718 11.601 1.430 0.75 301495. 0.0799 81.84 0.4635 0.3854 0.0052 0.0062 0.935 5.357 1.651 697.208 0.605 7.344 1.074 0.75 301893. 0.0478 84.87 0.4807 0.2105 0.0022 0.0050 0.755 4.326 0.702 563.012 0.489 3.124 0.566 0.75 302299. 0.0164 87.90 0.4978 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 0.0731 0.0206 4.002 21.022 27.683 2984.605 2.375 123.132 4.207 0.81 321764. 0.7662 3.30 0.0171 0.0595 0.0715 0.0206 4.007 21.046 27.101 2988.021 2.378 120.547 4.114 0.81 321911. 0.7414 6.60 0.0343 0.1163 0.0699 0.0206 4.007 21.047 26.489 2988.163 2.378 117.825 4.021 0.81 322066. 0.7164 9.90 0.0514 0.1704 0.0682 0.0206 4.002 21.022 25.847 2984.631 2.375 114.966 3.928 0.81 322230. 0.6913 13.20 0.0685 0.2219 0.0664 0.0205 3.992 20.969 25.173 2976.999 2.369 111.967 3.835 0.81 322402. 0.6661 16.49 0.0856 0.2707 0.0646 0.0204 3.976 20.883 24.466 2964.821 2.359 108.826 3.743 0.81 322584. 0.6409 19.79 0.1028 0.3168 0.0626 0.0203 3.953 20.762 23.728 2947.625 2.346 105.540 3.651 0.81 322775. 0.6157 23.09 0.1199 0.3604 0.0606 0.0202 3.922 20.602 22.955 2924.890 2.328 102.104 3.560 0.81 322976. 0.5904 26.39 0.1370 0.4013 0.0585 0.0200 3.884 20.399 22.148 2896.134 2.305 98.515 3.469 0.81 323186. 0.5651 29.69 0.1541 0.4397 0.0562 0.0197 3.837 20.153 21.308 2861.217 2.277 94.776 3.378 0.81 323407. 0.5397 32.99 0.1713 0.4754 0.0539 0.0194 3.781 19.860 20.434 2819.648 2.244 90.892 3.287 0.81 323638. 0.5144 36.29 0.1884 0.5085 0.0516 0.0191 3.716 19.519 19.530 2771.162 2.205 86.867 3.196 0.81 323879. 0.4890 39.59 0.2055 0.5390 0.0491 0.0187 3.642 19.128 18.594 2715.632 2.161 82.708 3.106 0.81 324131. 0.4636 42.89 0.2226 0.5668 0.0465 0.0183 3.557 18.685 17.630 2652.737 2.111 78.420 3.014 0.81 324394. 0.4382 46.18 0.2398 0.5917 0.0439 0.0178 3.463 18.188 16.638 2582.284 2.055 74.008 2.922 0.81 324667. 0.4127 49.48 0.2569 0.6138 0.0412 0.0173 3.358 17.638 15.620 2504.147 1.993 69.478 2.829 0.81 324952. 0.3871 52.78 0.2740 0.6326 0.0385 0.0167 3.243 17.034 14.577 2418.340 1.924 64.837 2.734 0.81 325249. 0.3613 56.08 0.2912 0.6480 0.0357 0.0160 3.118 16.375 13.510 2324.761 1.850 60.091 2.636 0.81 325557. 0.3354 59.38 0.3083 0.6596 0.0328 0.0153 2.982 15.661 12.421 2223.453 1.769 55.247 2.534 0.81 325876. 0.3091 62.68 0.3254 0.6667 0.0299 0.0146 2.836 14.894 11.312 2114.512 1.683 50.314 2.426 0.81 326208. 0.2825 65.98 0.3425 0.6687 0.0269 0.0138 2.680 14.074 10.184 1998.151 1.590 45.300 2.312 0.81 326552. 0.2554 69.28 0.3597 0.6644 0.0239 0.0129 2.514 13.204 9.042 1874.599 1.492 40.217 2.188 0.81 326908. 0.2277 72.58 0.3768 0.6524 0.0208 0.0120 2.339 12.285 7.886 1744.194 1.388 35.075 2.051 0.81 327276. 0.1993 75.88 0.3939 0.6307 0.0177 0.0111 2.156 11.322 6.719 1607.399 1.279 29.888 1.896 0.81 327657. 0.1701 79.17 0.4110 0.5961 0.0146 0.0101 1.964 10.317 5.546 1464.790 1.166 24.670 1.717 0.81 328051. 0.1400 82.47 0.4282 0.5441 0.0115 0.0091 1.766 9.277 4.370 1317.053 1.048 19.438 1.505 0.81 328458. 0.1089 85.77 0.4453 0.4677 0.0084 0.0080 1.562 8.206 3.195 1165.001 0.927 14.212 1.244 0.81 328877. 0.0770 89.07 0.4624 0.3554 0.0053 0.0070 1.354 7.111 2.026 1009.548 0.803 9.011 0.910 0.82 329309. 0.0448 92.37 0.4795 0.1869 0.0023 0.0059 1.142 5.997 0.866 851.428 0.678 3.854 0.462 0.82 329751. 0.0149 95.67 0.4967 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 0.0750 0.0227 5.609 27.196 33.323 4182.908 3.073 148.221 3.613 0.87 348526. 0.7221 3.55 0.0170 0.0553 0.0734 0.0226 5.583 27.070 32.637 4163.489 3.058 145.170 3.555 0.87 348686. 0.7031 7.09 0.0340 0.1087 0.0718 0.0224 5.552 26.919 31.914 4140.220 3.041 141.954 3.496 0.87 348855. 0.6837 10.64 0.0510 0.1603 0.0701 0.0223 5.515 26.740 31.154 4112.779 3.021 138.574 3.436 0.87 349033. 0.6638 14.19 0.0680 0.2098 0.0683 0.0221 5.472 26.532 30.357 4080.758 2.998 135.026 3.374 0.87 349221. 0.6435 17.73 0.0850 0.2574 0.0664 0.0219 5.423 26.291 29.521 4043.749 2.970 131.308 3.311 0.87 349418. 0.6228 21.28 0.1020 0.3029 0.0644 0.0217 5.366 26.015 28.646 4001.269 2.939 127.415 3.247 0.87 349626. 0.6016 24.82 0.1190 0.3463 0.0624 0.0214 5.301 25.700 27.730 3952.790 2.904 123.344 3.182 0.87 349843. 0.5800 28.37 0.1360 0.3875 0.0602 0.0211 5.227 25.342 26.774 3897.731 2.863 119.091 3.116 0.87 350072. 0.5581 31.92 0.1530 0.4265 0.0580 0.0208 5.144 24.938 25.777 3835.587 2.817 114.656 3.048 0.88 350310. 0.5357 35.46 0.1700 0.4630 0.0556 0.0204 5.053 24.499 24.740 3768.029 2.768 110.045 2.978 0.88 350560. 0.5128 39.01 0.1869 0.4969 0.0532 0.0200 4.954 24.021 23.666 3694.538 2.714 105.265 2.905 0.88 350821. 0.4893 42.56 0.2039 0.5279 0.0507 0.0196 4.848 23.504 22.554 3615.101 2.656 100.322 2.830 0.88 351093. 0.4652 46.10 0.2209 0.5561 0.0482 0.0191 4.732 22.943 21.408 3528.807 2.592 95.222 2.752 0.88 351376. 0.4407 49.65 0.2379 0.5811 0.0455 0.0186 4.609 22.345 20.228 3436.757 2.525 89.973 2.670 0.88 351672. 0.4156 53.20 0.2549 0.6022 0.0428 0.0181 4.479 21.717 19.015 3340.251 2.454 84.579 2.582 0.88 351979. 0.3898 56.74 0.2719 0.6192 0.0400 0.0176 4.343 21.056 17.772 3238.523 2.379 79.051 2.489 0.88 352298. 0.3632 60.29 0.2889 0.6321 0.0371 0.0170 4.196 20.345 16.501 3129.215 2.299 73.396 2.392 0.88 352629. 0.3363 63.84 0.3059 0.6406 0.0342 0.0163 4.040 19.586 15.203 3012.438 2.213 67.623 2.289 0.88 352973. 0.3090 67.38 0.3229 0.6439 0.0312 0.0157 3.873 18.780 13.881 2888.413 2.122 61.743 2.180 0.88 353329. 0.2811 70.93 0.3399 0.6412 0.0282 0.0149 3.698 17.929 12.537 2757.644 2.026 55.766 2.062 0.88 353698. 0.2528 74.47 0.3569 0.6314 0.0251 0.0142 3.515 17.040 11.174 2620.844 1.925 49.704 1.934 0.88 354080. 0.2238 78.02 0.3739 0.6131 0.0220 0.0134 3.324 16.116 9.795 2478.781 1.821 43.570 1.792 0.88 354474. 0.1942 81.57 0.3909 0.5845 0.0189 0.0126 3.127 15.163 8.404 2332.124 1.713 37.380 1.634 0.88 354883. 0.1640 85.11 0.4079 0.5433 0.0158 0.0118 2.926 14.185 7.004 2181.797 1.603 31.152 1.456 0.88 355304. 0.1334 88.66 0.4249 0.4865 0.0126 0.0110 2.721 13.191 5.599 2028.880 1.490 24.905 1.252 0.88 355740. 0.1025 92.21 0.4419 0.4104 0.0094 0.0102 2.514 12.187 4.196 1874.465 1.377 18.663 1.015 0.88 356188. 0.0720 95.75 0.4589 0.3099 0.0063 0.0093 2.306 11.181 2.799 1719.703 1.263 12.449 0.738 0.88 356651. 0.0428 99.30 0.4759 0.1783 0.0032 0.0085 2.099 10.178 1.414 1565.394 1.150 6.287 0.410 0.88 357125. 0.0169 102.85 0.4929 0.0030 0.0000 0.0076 1.882 9.126 0.020 1403.590 1.031 0.090 0.007 0.88 357584. 0.0000 PROP RPM = 14000 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 0.0272 8.390 37.773 39.485 6256.524 4.268 175.631 2.863 0.94 375285. 0.6227 3.86 0.0172 0.0480 0.0750 0.0269 8.302 37.374 38.697 6190.528 4.223 172.125 2.835 0.94 375460. 0.6105 7.73 0.0344 0.0951 0.0734 0.0266 8.204 36.935 37.862 6117.818 4.173 168.410 2.807 0.94 375645. 0.5979 11.59 0.0516 0.1411 0.0717 0.0262 8.098 36.455 36.980 6038.346 4.119 164.486 2.778 0.94 375840. 0.5847 15.45 0.0688 0.1861 0.0699 0.0258 7.982 35.934 36.050 5951.948 4.060 160.350 2.747 0.94 376047. 0.5710 19.31 0.0859 0.2299 0.0680 0.0254 7.856 35.369 35.071 5858.427 3.996 155.998 2.715 0.94 376264. 0.5566 23.18 0.1031 0.2725 0.0660 0.0250 7.721 34.760 34.044 5757.534 3.927 151.426 2.682 0.94 376492. 0.5417 27.04 0.1203 0.3137 0.0639 0.0245 7.575 34.104 32.965 5648.936 3.853 146.630 2.647 0.94 376732. 0.5261 30.90 0.1375 0.3536 0.0617 0.0240 7.419 33.400 31.836 5532.221 3.773 141.605 2.610 0.94 376984. 0.5098 34.76 0.1547 0.3919 0.0595 0.0235 7.251 32.644 30.655 5406.975 3.688 136.352 2.571 0.94 377247. 0.4929 38.63 0.1719 0.4286 0.0571 0.0229 7.071 31.835 29.424 5273.064 3.597 130.878 2.531 0.94 377523. 0.4752 42.49 0.1891 0.4632 0.0546 0.0223 6.884 30.992 28.145 5133.344 3.501 125.191 2.487 0.94 377810. 0.4567 46.35 0.2063 0.4951 0.0520 0.0217 6.696 30.145 26.821 4993.056 3.406 119.299 2.436 0.94 378110. 0.4368 50.21 0.2234 0.5239 0.0494 0.0211 6.505 29.285 25.452 4850.682 3.309 113.210 2.380 0.94 378423. 0.4156 54.08 0.2406 0.5497 0.0466 0.0204 6.306 28.390 24.042 4702.396 3.207 106.938 2.319 0.94 378749. 0.3936 57.94 0.2578 0.5713 0.0438 0.0198 6.110 27.507 22.592 4556.132 3.108 100.488 2.249 0.94 379088. 0.3700 61.80 0.2750 0.5861 0.0409 0.0192 5.934 26.713 21.103 4424.706 3.018 93.866 2.163 0.94 379439. 0.3440 65.66 0.2922 0.5925 0.0380 0.0187 5.785 26.046 19.577 4314.200 2.943 87.078 2.058 0.95 379805. 0.3152 69.53 0.3094 0.5934 0.0349 0.0182 5.630 25.347 18.019 4198.442 2.864 80.150 1.947 0.95 380183. 0.2861 73.39 0.3266 0.5879 0.0319 0.0177 5.471 24.629 16.433 4079.388 2.783 73.096 1.827 0.95 380576. 0.2564 77.25 0.3438 0.5755 0.0287 0.0172 5.306 23.887 14.823 3956.615 2.699 65.932 1.699 0.95 380982. 0.2265 81.11 0.3610 0.5554 0.0256 0.0166 5.138 23.130 13.192 3831.195 2.613 58.676 1.562 0.95 381402. 0.1964 84.98 0.3781 0.5266 0.0224 0.0161 4.967 22.363 11.544 3704.151 2.527 51.349 1.414 0.95 381837. 0.1663 88.84 0.3953 0.4882 0.0192 0.0155 4.797 21.595 9.886 3576.899 2.440 43.973 1.254 0.95 382286. 0.1364 92.70 0.4125 0.4393 0.0159 0.0150 4.627 20.831 8.223 3450.393 2.353 36.575 1.081 0.95 382750. 0.1073 96.56 0.4297 0.3789 0.0127 0.0144 4.459 20.076 6.561 3325.263 2.268 29.184 0.895 0.95 383229. 0.0794 100.43 0.4469 0.3061 0.0095 0.0139 4.294 19.333 4.909 3202.322 2.184 21.833 0.695 0.95 383723. 0.0533 104.29 0.4641 0.2202 0.0063 0.0134 4.133 18.607 3.272 3081.979 2.102 14.556 0.482 0.95 384232. 0.0302 108.15 0.4813 0.1203 0.0032 0.0129 3.974 17.890 1.657 2963.182 2.021 7.372 0.254 0.95 384758. 0.0113 112.01 0.4985 0.0013 0.0000 0.0123 3.786 17.044 0.017 2823.061 1.926 0.074 0.003 0.95 385299. 0.0000