15x8E (15x8E.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 0.0879 0.0358 0.002 0.138 0.142 1.633 0.016 0.631 39.397 0.06 20945. 0.5804 0.33 0.0231 0.0554 0.0866 0.0362 0.002 0.139 0.140 1.648 0.016 0.621 38.452 0.06 20958. 0.5622 0.66 0.0463 0.1081 0.0851 0.0365 0.002 0.140 0.137 1.661 0.016 0.611 37.503 0.06 20972. 0.5437 0.99 0.0694 0.1580 0.0836 0.0367 0.002 0.141 0.135 1.674 0.016 0.600 36.551 0.06 20987. 0.5251 1.31 0.0926 0.2052 0.0819 0.0370 0.002 0.142 0.132 1.684 0.016 0.588 35.599 0.06 21004. 0.5063 1.64 0.1157 0.2497 0.0801 0.0371 0.002 0.143 0.129 1.693 0.016 0.575 34.649 0.06 21022. 0.4874 1.97 0.1389 0.2914 0.0782 0.0373 0.002 0.144 0.126 1.699 0.016 0.561 33.701 0.06 21041. 0.4683 2.30 0.1620 0.3305 0.0762 0.0373 0.002 0.144 0.123 1.702 0.016 0.547 32.758 0.06 21062. 0.4492 2.63 0.1851 0.3668 0.0740 0.0373 0.002 0.144 0.119 1.702 0.016 0.531 31.818 0.06 21084. 0.4300 2.96 0.2083 0.4005 0.0716 0.0373 0.002 0.144 0.116 1.698 0.016 0.514 30.881 0.06 21107. 0.4107 3.29 0.2314 0.4316 0.0692 0.0371 0.002 0.143 0.112 1.690 0.016 0.496 29.946 0.06 21132. 0.3913 3.62 0.2546 0.4599 0.0665 0.0368 0.002 0.142 0.107 1.678 0.016 0.477 29.012 0.06 21158. 0.3718 3.94 0.2777 0.4855 0.0637 0.0365 0.002 0.140 0.103 1.661 0.016 0.457 28.074 0.06 21186. 0.3521 4.27 0.3009 0.5083 0.0608 0.0360 0.002 0.139 0.098 1.639 0.016 0.436 27.130 0.06 21215. 0.3323 4.60 0.3240 0.5281 0.0577 0.0354 0.002 0.136 0.093 1.613 0.015 0.414 26.175 0.06 21246. 0.3124 4.93 0.3471 0.5448 0.0544 0.0347 0.002 0.134 0.088 1.581 0.015 0.391 25.202 0.06 21279. 0.2922 5.26 0.3703 0.5581 0.0510 0.0339 0.002 0.130 0.082 1.543 0.015 0.366 24.204 0.06 21313. 0.2717 5.59 0.3934 0.5677 0.0475 0.0329 0.002 0.127 0.077 1.501 0.014 0.341 23.171 0.06 21349. 0.2510 5.92 0.4166 0.5732 0.0439 0.0319 0.002 0.123 0.071 1.452 0.014 0.315 22.095 0.06 21386. 0.2299 6.25 0.4397 0.5740 0.0401 0.0307 0.002 0.118 0.065 1.399 0.013 0.288 20.963 0.06 21425. 0.2085 6.57 0.4629 0.5696 0.0362 0.0294 0.002 0.113 0.058 1.341 0.013 0.260 19.760 0.06 21465. 0.1869 6.90 0.4860 0.5589 0.0323 0.0281 0.002 0.108 0.052 1.279 0.012 0.232 18.468 0.06 21507. 0.1649 7.23 0.5092 0.5411 0.0283 0.0266 0.002 0.102 0.046 1.213 0.012 0.203 17.066 0.06 21551. 0.1426 7.56 0.5323 0.5146 0.0242 0.0251 0.002 0.097 0.039 1.142 0.011 0.174 15.524 0.06 21596. 0.1200 7.89 0.5554 0.4775 0.0201 0.0234 0.001 0.090 0.032 1.067 0.010 0.144 13.805 0.06 21643. 0.0973 8.22 0.5786 0.4272 0.0160 0.0217 0.001 0.084 0.026 0.989 0.009 0.115 11.858 0.06 21692. 0.0746 8.55 0.6017 0.3603 0.0119 0.0199 0.001 0.077 0.019 0.908 0.009 0.086 9.615 0.06 21742. 0.0522 8.88 0.6249 0.2716 0.0079 0.0181 0.001 0.070 0.013 0.824 0.008 0.056 6.979 0.06 21794. 0.0307 9.20 0.6480 0.1537 0.0038 0.0162 0.001 0.062 0.006 0.738 0.007 0.028 3.810 0.06 21847. 0.0117 9.53 0.6712 -0.0047 -0.0001 0.0143 0.001 0.055 0.000 0.650 0.006 -0.001 -0.113 0.06 21902. 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 0.0882 0.0326 0.016 0.503 0.569 11.893 0.057 2.532 21.712 0.12 41889. 0.6408 0.66 0.0232 0.0612 0.0869 0.0330 0.016 0.508 0.561 12.027 0.057 2.494 21.146 0.12 41915. 0.6194 1.32 0.0465 0.1192 0.0855 0.0333 0.016 0.514 0.551 12.153 0.058 2.453 20.582 0.12 41944. 0.5979 1.98 0.0697 0.1739 0.0839 0.0337 0.016 0.518 0.541 12.267 0.059 2.408 20.020 0.12 41975. 0.5763 2.64 0.0930 0.2254 0.0822 0.0339 0.017 0.523 0.531 12.368 0.059 2.361 19.463 0.12 42008. 0.5546 3.30 0.1162 0.2738 0.0804 0.0342 0.017 0.526 0.519 12.452 0.059 2.309 18.910 0.12 42044. 0.5330 3.96 0.1395 0.3191 0.0785 0.0343 0.017 0.529 0.507 12.516 0.060 2.254 18.365 0.12 42083. 0.5114 4.62 0.1627 0.3613 0.0765 0.0344 0.017 0.531 0.493 12.556 0.060 2.195 17.825 0.12 42124. 0.4898 5.28 0.1860 0.4006 0.0743 0.0345 0.017 0.531 0.479 12.569 0.060 2.132 17.293 0.12 42169. 0.4683 5.94 0.2092 0.4370 0.0719 0.0344 0.017 0.530 0.464 12.553 0.060 2.064 16.768 0.12 42216. 0.4468 6.61 0.2325 0.4705 0.0694 0.0343 0.017 0.528 0.448 12.502 0.060 1.992 16.250 0.12 42266. 0.4254 7.27 0.2557 0.5012 0.0668 0.0341 0.017 0.525 0.431 12.416 0.059 1.916 15.737 0.12 42319. 0.4040 7.93 0.2790 0.5291 0.0639 0.0337 0.016 0.519 0.413 12.290 0.059 1.835 15.228 0.12 42375. 0.3826 8.59 0.3022 0.5542 0.0610 0.0333 0.016 0.512 0.393 12.123 0.058 1.750 14.722 0.12 42434. 0.3612 9.25 0.3255 0.5763 0.0579 0.0327 0.016 0.503 0.373 11.913 0.057 1.661 14.215 0.12 42497. 0.3398 9.91 0.3487 0.5953 0.0546 0.0320 0.016 0.493 0.352 11.657 0.056 1.567 13.706 0.12 42562. 0.3182 10.57 0.3720 0.6111 0.0512 0.0311 0.015 0.480 0.330 11.355 0.054 1.469 13.190 0.12 42631. 0.2965 11.23 0.3952 0.6233 0.0476 0.0302 0.015 0.465 0.307 11.005 0.053 1.367 12.663 0.12 42703. 0.2746 11.89 0.4185 0.6317 0.0439 0.0291 0.014 0.448 0.283 10.609 0.051 1.261 12.120 0.12 42778. 0.2524 12.55 0.4417 0.6356 0.0401 0.0279 0.014 0.430 0.259 10.169 0.049 1.152 11.554 0.12 42857. 0.2300 13.21 0.4650 0.6345 0.0363 0.0266 0.013 0.409 0.234 9.687 0.046 1.041 10.957 0.12 42938. 0.2073 13.87 0.4882 0.6275 0.0323 0.0251 0.012 0.387 0.208 9.164 0.044 0.927 10.319 0.12 43023. 0.1843 14.53 0.5115 0.6133 0.0283 0.0236 0.012 0.364 0.183 8.603 0.041 0.812 9.628 0.12 43111. 0.1609 15.19 0.5347 0.5903 0.0242 0.0220 0.011 0.338 0.156 8.004 0.038 0.696 8.864 0.12 43203. 0.1371 15.85 0.5580 0.5562 0.0202 0.0202 0.010 0.311 0.130 7.371 0.035 0.578 8.003 0.12 43297. 0.1129 16.51 0.5812 0.5075 0.0161 0.0184 0.009 0.283 0.104 6.705 0.032 0.461 7.010 0.12 43395. 0.0883 17.17 0.6045 0.4390 0.0120 0.0165 0.008 0.254 0.077 6.010 0.029 0.344 5.832 0.12 43496. 0.0634 17.83 0.6277 0.3428 0.0079 0.0145 0.007 0.224 0.051 5.291 0.025 0.228 4.385 0.12 43601. 0.0388 18.49 0.6510 0.2054 0.0039 0.0125 0.006 0.192 0.025 4.550 0.022 0.113 2.533 0.12 43709. 0.0158 19.15 0.6742 0.0021 0.0000 0.0104 0.005 0.160 0.000 3.794 0.018 0.001 0.026 0.12 43819. 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 0.0885 0.0313 0.052 1.084 1.285 38.464 0.122 5.715 15.152 0.18 62833. 0.6719 1.01 0.0237 0.0652 0.0871 0.0317 0.052 1.097 1.265 38.948 0.124 5.628 14.735 0.18 62873. 0.6483 2.02 0.0474 0.1268 0.0857 0.0320 0.053 1.110 1.244 39.404 0.125 5.533 14.319 0.18 62917. 0.6247 3.03 0.0711 0.1848 0.0841 0.0324 0.053 1.122 1.221 39.821 0.127 5.431 13.908 0.18 62964. 0.6012 4.04 0.0948 0.2391 0.0824 0.0327 0.054 1.132 1.196 40.190 0.128 5.321 13.501 0.18 63016. 0.5776 5.05 0.1185 0.2900 0.0806 0.0329 0.054 1.141 1.170 40.498 0.129 5.203 13.100 0.18 63071. 0.5542 6.06 0.1422 0.3376 0.0786 0.0331 0.055 1.148 1.141 40.734 0.130 5.075 12.705 0.18 63131. 0.5309 7.07 0.1659 0.3818 0.0765 0.0332 0.055 1.152 1.110 40.885 0.130 4.938 12.316 0.18 63195. 0.5076 8.08 0.1896 0.4228 0.0742 0.0333 0.055 1.153 1.077 40.940 0.130 4.792 11.935 0.18 63263. 0.4846 9.09 0.2133 0.4607 0.0718 0.0332 0.055 1.152 1.042 40.886 0.130 4.635 11.561 0.18 63336. 0.4616 10.10 0.2370 0.4956 0.0692 0.0331 0.055 1.147 1.005 40.710 0.130 4.468 11.193 0.18 63413. 0.4388 11.11 0.2607 0.5276 0.0664 0.0328 0.054 1.138 0.965 40.403 0.129 4.291 10.831 0.18 63496. 0.4161 12.12 0.2844 0.5565 0.0635 0.0325 0.054 1.126 0.923 39.953 0.127 4.104 10.473 0.18 63583. 0.3935 13.13 0.3082 0.5826 0.0605 0.0320 0.053 1.109 0.878 39.353 0.125 3.905 10.120 0.18 63675. 0.3709 14.14 0.3319 0.6056 0.0572 0.0314 0.052 1.087 0.831 38.595 0.123 3.697 9.768 0.18 63771. 0.3484 15.15 0.3556 0.6255 0.0539 0.0306 0.051 1.061 0.782 37.673 0.120 3.479 9.416 0.18 63873. 0.3257 16.16 0.3793 0.6420 0.0503 0.0297 0.049 1.031 0.731 36.580 0.116 3.251 9.061 0.18 63980. 0.3030 17.17 0.4030 0.6550 0.0467 0.0287 0.047 0.995 0.677 35.314 0.112 3.013 8.700 0.18 64091. 0.2801 18.18 0.4267 0.6639 0.0429 0.0275 0.045 0.955 0.622 33.883 0.108 2.768 8.330 0.18 64208. 0.2570 19.19 0.4504 0.6684 0.0390 0.0262 0.043 0.910 0.566 32.294 0.103 2.516 7.944 0.18 64330. 0.2337 20.20 0.4741 0.6676 0.0350 0.0248 0.041 0.861 0.508 30.551 0.097 2.258 7.537 0.18 64456. 0.2101 21.21 0.4978 0.6604 0.0309 0.0233 0.038 0.808 0.449 28.662 0.091 1.996 7.102 0.18 64588. 0.1861 22.22 0.5215 0.6456 0.0268 0.0216 0.036 0.750 0.389 26.631 0.085 1.731 6.626 0.18 64725. 0.1617 23.23 0.5452 0.6208 0.0226 0.0199 0.033 0.689 0.329 24.467 0.078 1.463 6.096 0.18 64867. 0.1367 24.24 0.5689 0.5832 0.0185 0.0180 0.030 0.625 0.268 22.177 0.071 1.193 5.487 0.18 65014. 0.1112 25.25 0.5926 0.5277 0.0143 0.0161 0.027 0.557 0.208 19.773 0.063 0.924 4.766 0.18 65166. 0.0850 26.26 0.6163 0.4465 0.0102 0.0140 0.023 0.486 0.148 17.267 0.055 0.657 3.878 0.18 65324. 0.0583 27.27 0.6400 0.3261 0.0061 0.0119 0.020 0.414 0.088 14.677 0.047 0.393 2.728 0.18 65486. 0.0317 28.28 0.6637 0.1405 0.0021 0.0098 0.016 0.339 0.030 12.019 0.038 0.134 1.133 0.18 65653. 0.0077 29.29 0.6874 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 0.0888 0.0305 0.119 1.881 2.292 89.010 0.212 10.197 11.681 0.24 83775. 0.6919 1.35 0.0237 0.0671 0.0875 0.0309 0.121 1.906 2.257 90.194 0.215 10.041 11.353 0.24 83829. 0.6672 2.70 0.0474 0.1303 0.0860 0.0313 0.122 1.929 2.220 91.312 0.218 9.873 11.026 0.24 83888. 0.6426 4.04 0.0712 0.1897 0.0844 0.0317 0.124 1.951 2.179 92.340 0.220 9.692 10.703 0.24 83951. 0.6180 5.39 0.0949 0.2454 0.0827 0.0320 0.125 1.970 2.135 93.250 0.223 9.496 10.384 0.24 84020. 0.5935 6.74 0.1186 0.2975 0.0809 0.0322 0.126 1.987 2.087 94.017 0.224 9.285 10.071 0.24 84094. 0.5692 8.09 0.1423 0.3461 0.0789 0.0324 0.127 1.999 2.036 94.612 0.226 9.058 9.763 0.24 84174. 0.5450 9.43 0.1660 0.3913 0.0768 0.0326 0.127 2.007 1.982 95.004 0.227 8.814 9.461 0.24 84259. 0.5210 10.78 0.1898 0.4332 0.0745 0.0326 0.128 2.011 1.923 95.164 0.227 8.553 9.165 0.24 84350. 0.4972 12.13 0.2135 0.4720 0.0721 0.0326 0.127 2.009 1.860 95.061 0.227 8.275 8.876 0.24 84448. 0.4736 13.48 0.2372 0.5077 0.0695 0.0325 0.127 2.000 1.793 94.668 0.226 7.977 8.593 0.24 84551. 0.4501 14.82 0.2609 0.5404 0.0667 0.0322 0.126 1.985 1.722 93.958 0.224 7.661 8.315 0.24 84661. 0.4269 16.17 0.2846 0.5701 0.0638 0.0319 0.125 1.963 1.647 92.904 0.222 7.326 8.041 0.24 84777. 0.4037 17.52 0.3083 0.5969 0.0607 0.0314 0.123 1.933 1.568 91.487 0.218 6.973 7.772 0.24 84900. 0.3807 18.87 0.3321 0.6208 0.0575 0.0308 0.120 1.895 1.484 89.688 0.214 6.601 7.505 0.24 85029. 0.3577 20.21 0.3558 0.6416 0.0541 0.0300 0.117 1.849 1.396 87.490 0.209 6.212 7.240 0.24 85165. 0.3347 21.56 0.3795 0.6592 0.0506 0.0291 0.114 1.794 1.305 84.879 0.203 5.804 6.973 0.24 85307. 0.3116 22.91 0.4032 0.6733 0.0469 0.0281 0.110 1.730 1.210 81.849 0.195 5.380 6.703 0.24 85456. 0.2884 24.26 0.4269 0.6835 0.0430 0.0269 0.105 1.657 1.111 78.417 0.187 4.943 6.427 0.24 85612. 0.2650 25.61 0.4507 0.6894 0.0391 0.0256 0.100 1.576 1.010 74.597 0.178 4.493 6.142 0.24 85774. 0.2415 26.95 0.4744 0.6903 0.0351 0.0241 0.094 1.488 0.907 70.403 0.168 4.034 5.842 0.24 85944. 0.2176 28.30 0.4981 0.6851 0.0311 0.0226 0.088 1.391 0.802 65.849 0.157 3.566 5.522 0.24 86120. 0.1934 29.65 0.5218 0.6725 0.0269 0.0209 0.082 1.288 0.695 60.949 0.146 3.092 5.174 0.24 86302. 0.1687 31.00 0.5455 0.6502 0.0228 0.0191 0.075 1.177 0.588 55.720 0.133 2.614 4.785 0.24 86492. 0.1435 32.34 0.5693 0.6150 0.0186 0.0172 0.067 1.060 0.480 50.184 0.120 2.135 4.337 0.24 86688. 0.1175 33.69 0.5930 0.5619 0.0144 0.0152 0.059 0.938 0.372 44.367 0.106 1.655 3.804 0.24 86892. 0.0908 35.04 0.6167 0.4820 0.0103 0.0131 0.051 0.809 0.265 38.301 0.091 1.179 3.138 0.24 87102. 0.0632 36.39 0.6404 0.3598 0.0062 0.0110 0.043 0.677 0.159 32.027 0.076 0.708 2.255 0.24 87319. 0.0352 37.73 0.6641 0.1631 0.0022 0.0088 0.034 0.541 0.056 25.589 0.061 0.247 0.986 0.24 87542. 0.0091 39.08 0.6878 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 0.0892 0.0301 0.230 2.897 3.597 171.396 0.327 16.000 9.519 0.30 104716. 0.7062 1.66 0.0234 0.0673 0.0879 0.0305 0.233 2.937 3.543 173.728 0.332 15.761 9.251 0.30 104783. 0.6812 3.32 0.0467 0.1307 0.0864 0.0309 0.236 2.974 3.486 175.936 0.336 15.504 8.986 0.30 104855. 0.6562 4.98 0.0701 0.1903 0.0849 0.0312 0.239 3.009 3.423 177.972 0.340 15.226 8.724 0.30 104933. 0.6314 6.63 0.0934 0.2462 0.0832 0.0316 0.241 3.039 3.356 179.790 0.343 14.926 8.465 0.30 105017. 0.6066 8.29 0.1168 0.2985 0.0814 0.0318 0.243 3.065 3.283 181.336 0.346 14.602 8.211 0.30 105108. 0.5820 9.95 0.1401 0.3474 0.0795 0.0320 0.245 3.086 3.205 182.557 0.349 14.255 7.963 0.30 105205. 0.5576 11.61 0.1635 0.3929 0.0774 0.0322 0.246 3.100 3.121 183.397 0.350 13.882 7.719 0.30 105310. 0.5334 13.27 0.1868 0.4351 0.0752 0.0323 0.246 3.107 3.031 183.799 0.351 13.483 7.481 0.30 105421. 0.5095 14.93 0.2102 0.4743 0.0728 0.0323 0.246 3.105 2.935 183.706 0.351 13.057 7.248 0.30 105540. 0.4857 16.59 0.2335 0.5104 0.0702 0.0321 0.245 3.095 2.833 183.063 0.350 12.602 7.020 0.30 105667. 0.4622 18.24 0.2569 0.5436 0.0676 0.0319 0.244 3.074 2.725 181.819 0.347 12.120 6.797 0.30 105801. 0.4389 19.90 0.2802 0.5740 0.0647 0.0316 0.241 3.042 2.610 179.925 0.344 11.608 6.579 0.30 105943. 0.4157 21.56 0.3036 0.6016 0.0617 0.0311 0.238 2.998 2.488 177.339 0.339 11.068 6.364 0.30 106092. 0.3927 23.22 0.3269 0.6263 0.0585 0.0306 0.233 2.942 2.361 174.024 0.332 10.500 6.153 0.30 106250. 0.3698 24.88 0.3503 0.6481 0.0552 0.0298 0.228 2.873 2.227 169.950 0.325 9.904 5.943 0.30 106415. 0.3469 26.54 0.3736 0.6670 0.0517 0.0290 0.221 2.791 2.087 165.086 0.315 9.282 5.733 0.30 106588. 0.3240 28.20 0.3970 0.6826 0.0481 0.0280 0.214 2.695 1.941 159.413 0.304 8.633 5.522 0.30 106770. 0.3009 29.85 0.4203 0.6947 0.0444 0.0269 0.205 2.586 1.790 152.952 0.292 7.962 5.308 0.30 106959. 0.2778 31.51 0.4437 0.7030 0.0405 0.0256 0.195 2.464 1.635 145.734 0.278 7.272 5.089 0.30 107157. 0.2545 33.17 0.4670 0.7067 0.0366 0.0242 0.185 2.329 1.476 137.785 0.263 6.567 4.860 0.30 107363. 0.2310 34.83 0.4904 0.7052 0.0326 0.0227 0.173 2.183 1.315 129.128 0.247 5.848 4.618 0.30 107577. 0.2071 36.49 0.5137 0.6971 0.0285 0.0210 0.161 2.025 1.151 119.791 0.229 5.119 4.358 0.30 107799. 0.1829 38.15 0.5371 0.6807 0.0244 0.0193 0.147 1.856 0.985 109.804 0.210 4.383 4.070 0.30 108030. 0.1581 39.80 0.5605 0.6534 0.0203 0.0174 0.133 1.677 0.819 99.204 0.189 3.643 3.744 0.30 108268. 0.1325 41.46 0.5838 0.6109 0.0162 0.0155 0.118 1.488 0.652 88.037 0.168 2.901 3.361 0.30 108515. 0.1062 43.12 0.6072 0.5462 0.0121 0.0134 0.102 1.291 0.486 76.361 0.146 2.163 2.889 0.30 108771. 0.0788 44.78 0.6305 0.4465 0.0080 0.0113 0.086 1.086 0.322 64.247 0.123 1.433 2.274 0.30 109034. 0.0505 46.44 0.6539 0.2866 0.0040 0.0091 0.069 0.875 0.161 51.778 0.099 0.715 1.408 0.30 109306. 0.0221 48.10 0.6772 0.0066 0.0001 0.0068 0.052 0.660 0.003 39.014 0.075 0.012 0.031 0.30 109581. 0.0001 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 0.0896 0.0299 0.394 4.140 5.206 293.854 0.468 23.156 8.036 0.36 125655. 0.7172 1.99 0.0234 0.0682 0.0883 0.0303 0.400 4.198 5.129 297.969 0.474 22.813 7.807 0.36 125735. 0.6916 3.99 0.0468 0.1325 0.0869 0.0307 0.405 4.252 5.045 301.868 0.480 22.442 7.581 0.36 125822. 0.6661 5.98 0.0701 0.1928 0.0853 0.0310 0.410 4.303 4.955 305.469 0.486 22.041 7.358 0.36 125916. 0.6407 7.97 0.0935 0.2494 0.0836 0.0314 0.414 4.348 4.858 308.685 0.491 21.608 7.138 0.36 126018. 0.6154 9.96 0.1169 0.3024 0.0818 0.0316 0.418 4.387 4.753 311.428 0.496 21.142 6.922 0.36 126127. 0.5904 11.96 0.1403 0.3518 0.0799 0.0319 0.421 4.418 4.640 313.600 0.499 20.640 6.711 0.36 126244. 0.5655 13.95 0.1637 0.3978 0.0778 0.0320 0.423 4.439 4.519 315.103 0.502 20.101 6.505 0.36 126370. 0.5409 15.94 0.1871 0.4406 0.0756 0.0321 0.424 4.449 4.389 315.838 0.503 19.524 6.303 0.36 126504. 0.5166 17.94 0.2104 0.4802 0.0732 0.0321 0.423 4.447 4.251 315.704 0.502 18.907 6.107 0.36 126648. 0.4925 19.93 0.2338 0.5167 0.0706 0.0320 0.422 4.432 4.103 314.604 0.501 18.249 5.915 0.36 126800. 0.4687 21.92 0.2572 0.5504 0.0679 0.0317 0.419 4.401 3.945 312.447 0.497 17.549 5.727 0.36 126961. 0.4450 23.91 0.2806 0.5812 0.0651 0.0314 0.415 4.355 3.779 309.147 0.492 16.808 5.544 0.36 127132. 0.4216 25.91 0.3040 0.6092 0.0620 0.0309 0.409 4.291 3.603 304.630 0.485 16.025 5.364 0.36 127312. 0.3983 27.90 0.3274 0.6344 0.0588 0.0304 0.401 4.210 3.418 298.831 0.476 15.201 5.187 0.36 127502. 0.3751 29.89 0.3507 0.6568 0.0555 0.0296 0.391 4.109 3.223 291.695 0.464 14.337 5.012 0.36 127701. 0.3520 31.89 0.3741 0.6762 0.0520 0.0288 0.380 3.989 3.020 283.167 0.451 13.434 4.838 0.36 127909. 0.3289 33.88 0.3975 0.6925 0.0484 0.0278 0.366 3.849 2.809 273.216 0.435 12.493 4.663 0.36 128128. 0.3057 35.87 0.4209 0.7054 0.0446 0.0266 0.351 3.689 2.590 261.876 0.417 11.520 4.486 0.36 128356. 0.2824 37.86 0.4443 0.7145 0.0407 0.0253 0.334 3.510 2.365 249.200 0.397 10.519 4.304 0.36 128594. 0.2589 39.86 0.4676 0.7192 0.0368 0.0239 0.315 3.314 2.135 235.232 0.374 9.495 4.116 0.36 128842. 0.2352 41.85 0.4910 0.7187 0.0327 0.0224 0.295 3.099 1.900 220.015 0.350 8.453 3.918 0.36 129099. 0.2113 43.84 0.5144 0.7119 0.0286 0.0207 0.273 2.868 1.663 203.596 0.324 7.395 3.704 0.36 129366. 0.1868 45.83 0.5378 0.6969 0.0245 0.0189 0.249 2.621 1.423 186.027 0.296 6.327 3.468 0.36 129644. 0.1618 47.83 0.5612 0.6711 0.0203 0.0170 0.224 2.358 1.181 167.375 0.266 5.253 3.201 0.36 129931. 0.1361 49.82 0.5846 0.6300 0.0162 0.0150 0.198 2.081 0.939 147.723 0.235 4.179 2.885 0.36 130228. 0.1094 51.81 0.6079 0.5662 0.0120 0.0129 0.171 1.792 0.699 127.174 0.202 3.109 2.493 0.36 130535. 0.0815 53.81 0.6313 0.4659 0.0079 0.0108 0.142 1.491 0.461 105.854 0.168 2.050 1.975 0.36 130852. 0.0525 55.80 0.6547 0.3002 0.0039 0.0085 0.113 1.182 0.227 83.913 0.134 1.010 1.227 0.36 131179. 0.0229 57.79 0.6781 -0.0036 0.0000 0.0062 0.082 0.865 -0.002 61.438 0.098 -0.009 -0.014 0.37 131509. 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 0.0902 0.0298 0.624 5.616 7.128 465.148 0.635 31.706 6.951 0.42 146592. 0.7259 2.33 0.0234 0.0688 0.0888 0.0302 0.633 5.697 7.023 471.805 0.644 31.240 6.752 0.42 146686. 0.7000 4.65 0.0468 0.1337 0.0874 0.0306 0.641 5.773 6.910 478.116 0.652 30.735 6.555 0.42 146787. 0.6741 6.98 0.0702 0.1946 0.0859 0.0310 0.649 5.843 6.787 483.947 0.660 30.190 6.361 0.42 146897. 0.6483 9.30 0.0936 0.2516 0.0842 0.0313 0.656 5.906 6.655 489.162 0.667 29.600 6.171 0.42 147016. 0.6227 11.63 0.1169 0.3050 0.0824 0.0316 0.662 5.960 6.512 493.613 0.673 28.964 5.984 0.42 147144. 0.5973 13.95 0.1403 0.3548 0.0804 0.0318 0.667 6.003 6.358 497.147 0.678 28.280 5.801 0.42 147281. 0.5721 16.28 0.1637 0.4012 0.0783 0.0320 0.670 6.033 6.193 499.605 0.682 27.545 5.622 0.42 147428. 0.5473 18.60 0.1871 0.4443 0.0761 0.0320 0.672 6.047 6.015 500.823 0.683 26.756 5.448 0.42 147585. 0.5227 20.93 0.2105 0.4843 0.0737 0.0320 0.671 6.045 5.826 500.642 0.683 25.913 5.278 0.42 147752. 0.4983 23.25 0.2339 0.5212 0.0711 0.0319 0.669 6.024 5.623 498.905 0.681 25.013 5.112 0.42 147930. 0.4742 25.58 0.2573 0.5552 0.0684 0.0317 0.664 5.983 5.408 495.462 0.676 24.056 4.951 0.42 148119. 0.4504 27.91 0.2807 0.5864 0.0655 0.0314 0.657 5.919 5.180 490.178 0.669 23.042 4.793 0.42 148318. 0.4268 30.23 0.3040 0.6148 0.0625 0.0309 0.648 5.831 4.939 482.930 0.659 21.970 4.639 0.42 148529. 0.4033 32.56 0.3274 0.6405 0.0593 0.0303 0.635 5.719 4.686 473.615 0.646 20.841 4.487 0.42 148750. 0.3800 34.88 0.3508 0.6633 0.0559 0.0296 0.620 5.580 4.419 462.141 0.630 19.657 4.337 0.42 148983. 0.3567 37.21 0.3742 0.6832 0.0524 0.0287 0.601 5.415 4.141 448.423 0.612 18.419 4.189 0.42 149227. 0.3334 39.53 0.3976 0.7001 0.0487 0.0277 0.580 5.221 3.851 432.406 0.590 17.130 4.040 0.42 149482. 0.3101 41.86 0.4210 0.7137 0.0449 0.0265 0.555 5.001 3.551 414.145 0.565 15.795 3.889 0.42 149749. 0.2867 44.18 0.4444 0.7236 0.0410 0.0252 0.528 4.754 3.243 393.722 0.537 14.423 3.735 0.42 150026. 0.2631 46.51 0.4678 0.7292 0.0370 0.0237 0.498 4.482 2.927 371.209 0.506 13.019 3.576 0.42 150316. 0.2393 48.84 0.4911 0.7298 0.0330 0.0222 0.465 4.186 2.605 346.674 0.473 11.589 3.409 0.42 150616. 0.2152 51.16 0.5145 0.7242 0.0288 0.0205 0.429 3.866 2.279 320.191 0.437 10.139 3.229 0.42 150929. 0.1907 53.49 0.5379 0.7107 0.0247 0.0187 0.391 3.524 1.950 291.847 0.398 8.674 3.031 0.42 151252. 0.1656 55.81 0.5613 0.6864 0.0205 0.0167 0.351 3.161 1.619 261.750 0.357 7.201 2.805 0.42 151588. 0.1396 58.14 0.5847 0.6471 0.0163 0.0147 0.308 2.778 1.288 230.033 0.314 5.727 2.539 0.42 151935. 0.1127 60.46 0.6081 0.5849 0.0121 0.0126 0.264 2.377 0.958 196.864 0.269 4.260 2.207 0.42 152293. 0.0845 62.79 0.6315 0.4852 0.0080 0.0104 0.218 1.962 0.631 162.448 0.222 2.808 1.763 0.42 152663. 0.0548 65.11 0.6549 0.3166 0.0039 0.0081 0.170 1.534 0.311 127.031 0.173 1.382 1.109 0.43 153045. 0.0242 67.44 0.6782 -0.0050 0.0000 0.0058 0.122 1.096 -0.003 90.740 0.124 -0.015 -0.017 0.43 153429. 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 0.0908 0.0298 0.932 7.341 9.375 694.777 0.829 41.701 6.120 0.48 167526. 0.7331 2.66 0.0234 0.0693 0.0895 0.0302 0.945 7.447 9.239 704.898 0.841 41.094 5.945 0.48 167633. 0.7068 5.32 0.0468 0.1345 0.0880 0.0306 0.958 7.549 9.091 714.497 0.853 40.436 5.771 0.48 167749. 0.6806 7.97 0.0702 0.1957 0.0865 0.0310 0.970 7.643 8.931 723.368 0.863 39.724 5.600 0.48 167875. 0.6546 10.63 0.0936 0.2531 0.0848 0.0313 0.981 7.726 8.758 731.305 0.873 38.953 5.432 0.48 168011. 0.6288 13.29 0.1169 0.3068 0.0830 0.0316 0.990 7.798 8.571 738.086 0.881 38.122 5.267 0.48 168158. 0.6032 15.95 0.1403 0.3569 0.0811 0.0319 0.997 7.855 8.369 743.475 0.887 37.226 5.106 0.48 168315. 0.5778 18.60 0.1637 0.4036 0.0790 0.0320 1.002 7.895 8.153 747.233 0.892 36.263 4.949 0.48 168483. 0.5527 21.26 0.1871 0.4470 0.0767 0.0321 1.005 7.915 7.920 749.112 0.894 35.229 4.796 0.48 168663. 0.5279 23.92 0.2105 0.4872 0.0743 0.0321 1.004 7.912 7.672 748.867 0.894 34.123 4.646 0.48 168855. 0.5034 26.58 0.2339 0.5245 0.0717 0.0320 1.001 7.884 7.406 746.263 0.891 32.942 4.501 0.48 169059. 0.4792 29.23 0.2573 0.5588 0.0690 0.0318 0.994 7.830 7.123 741.073 0.885 31.685 4.360 0.48 169275. 0.4552 31.89 0.2807 0.5903 0.0661 0.0314 0.983 7.745 6.824 733.089 0.875 30.352 4.222 0.48 169503. 0.4314 34.55 0.3040 0.6190 0.0630 0.0310 0.968 7.629 6.507 722.125 0.862 28.942 4.087 0.48 169744. 0.4078 37.21 0.3274 0.6451 0.0598 0.0303 0.949 7.480 6.173 708.024 0.845 27.458 3.955 0.48 169998. 0.3843 39.87 0.3508 0.6683 0.0564 0.0296 0.926 7.297 5.823 690.651 0.824 25.900 3.824 0.48 170264. 0.3610 42.52 0.3742 0.6888 0.0528 0.0287 0.898 7.077 5.457 669.873 0.800 24.271 3.695 0.48 170543. 0.3376 45.18 0.3976 0.7062 0.0491 0.0277 0.866 6.821 5.075 645.605 0.771 22.573 3.565 0.48 170835. 0.3142 47.84 0.4210 0.7204 0.0453 0.0265 0.829 6.529 4.680 617.928 0.738 20.815 3.435 0.48 171140. 0.2907 50.50 0.4444 0.7310 0.0414 0.0252 0.787 6.201 4.273 586.966 0.701 19.008 3.302 0.48 171458. 0.2670 53.15 0.4678 0.7375 0.0374 0.0237 0.741 5.841 3.857 552.825 0.660 17.158 3.165 0.48 171788. 0.2432 55.81 0.4911 0.7391 0.0333 0.0221 0.691 5.448 3.434 515.609 0.615 15.274 3.021 0.48 172132. 0.2190 58.47 0.5145 0.7346 0.0291 0.0204 0.638 5.023 3.004 475.431 0.568 13.362 2.866 0.48 172489. 0.1943 61.13 0.5379 0.7224 0.0249 0.0185 0.580 4.569 2.570 432.423 0.516 11.432 2.696 0.48 172860. 0.1691 63.78 0.5613 0.6997 0.0207 0.0166 0.519 4.086 2.134 386.747 0.462 9.490 2.502 0.48 173243. 0.1430 66.44 0.5847 0.6620 0.0164 0.0145 0.454 3.577 1.697 338.607 0.404 7.547 2.273 0.48 173639. 0.1158 69.10 0.6081 0.6014 0.0122 0.0124 0.387 3.046 1.262 288.260 0.344 5.612 1.985 0.48 174049. 0.0872 71.76 0.6315 0.5027 0.0081 0.0101 0.317 2.494 0.832 236.021 0.282 3.699 1.598 0.49 174472. 0.0570 74.42 0.6549 0.3318 0.0040 0.0078 0.244 1.926 0.409 182.262 0.218 1.818 1.017 0.49 174908. 0.0254 77.07 0.6782 -0.0064 -0.0001 0.0055 0.171 1.344 -0.005 127.162 0.152 -0.024 -0.019 0.49 175347. 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 0.0915 0.0299 1.332 9.328 11.961 993.233 1.054 53.204 5.462 0.54 188456. 0.7390 2.99 0.0234 0.0695 0.0902 0.0303 1.352 9.466 11.789 1007.920 1.069 52.439 5.305 0.54 188577. 0.7126 5.98 0.0468 0.1350 0.0888 0.0308 1.370 9.597 11.603 1021.853 1.084 51.608 5.150 0.54 188708. 0.6862 8.97 0.0701 0.1965 0.0872 0.0311 1.388 9.718 11.400 1034.733 1.098 50.708 4.997 0.54 188850. 0.6600 11.96 0.0935 0.2541 0.0856 0.0315 1.403 9.826 11.181 1046.260 1.110 49.734 4.847 0.54 189003. 0.6340 14.95 0.1169 0.3080 0.0837 0.0318 1.416 9.918 10.944 1056.109 1.121 48.681 4.700 0.54 189168. 0.6083 17.94 0.1403 0.3583 0.0818 0.0320 1.427 9.992 10.689 1063.943 1.129 47.545 4.557 0.54 189346. 0.5828 20.93 0.1637 0.4052 0.0797 0.0322 1.434 10.043 10.414 1069.411 1.135 46.322 4.417 0.54 189536. 0.5576 23.91 0.1871 0.4488 0.0774 0.0323 1.438 10.069 10.119 1072.157 1.138 45.009 4.281 0.54 189739. 0.5327 26.90 0.2104 0.4893 0.0750 0.0323 1.437 10.066 9.803 1071.825 1.137 43.602 4.148 0.54 189955. 0.5080 29.89 0.2338 0.5267 0.0724 0.0322 1.432 10.031 9.465 1068.073 1.133 42.099 4.019 0.54 190185. 0.4837 32.88 0.2572 0.5613 0.0697 0.0319 1.422 9.960 9.105 1060.574 1.125 40.498 3.894 0.54 190428. 0.4596 35.87 0.2806 0.5931 0.0667 0.0316 1.407 9.852 8.723 1049.027 1.113 38.799 3.772 0.54 190685. 0.4357 38.86 0.3040 0.6222 0.0637 0.0311 1.385 9.703 8.319 1033.164 1.096 37.002 3.652 0.54 190957. 0.4120 41.85 0.3274 0.6486 0.0604 0.0305 1.358 9.511 7.893 1012.755 1.075 35.109 3.535 0.54 191242. 0.3885 44.84 0.3507 0.6722 0.0570 0.0297 1.324 9.275 7.446 987.607 1.048 33.121 3.420 0.54 191542. 0.3650 47.83 0.3741 0.6931 0.0534 0.0288 1.284 8.993 6.978 957.530 1.016 31.040 3.306 0.54 191857. 0.3416 50.82 0.3975 0.7111 0.0497 0.0278 1.237 8.663 6.491 922.395 0.979 28.871 3.192 0.54 192186. 0.3181 53.81 0.4209 0.7259 0.0458 0.0266 1.183 8.286 5.986 882.320 0.936 26.625 3.077 0.54 192529. 0.2945 56.80 0.4443 0.7372 0.0418 0.0252 1.123 7.865 5.467 837.477 0.889 24.315 2.961 0.54 192887. 0.2708 59.79 0.4677 0.7445 0.0378 0.0237 1.057 7.401 4.935 788.024 0.836 21.950 2.840 0.54 193259. 0.2468 62.78 0.4910 0.7470 0.0336 0.0221 0.984 6.894 4.393 734.111 0.779 19.541 2.714 0.54 193646. 0.2225 65.76 0.5144 0.7436 0.0294 0.0203 0.906 6.348 3.844 675.898 0.717 17.096 2.579 0.54 194048. 0.1978 68.75 0.5378 0.7327 0.0252 0.0185 0.823 5.762 3.288 613.579 0.651 14.627 2.431 0.54 194464. 0.1724 71.74 0.5612 0.7114 0.0209 0.0165 0.734 5.141 2.730 547.390 0.581 12.142 2.262 0.54 194896. 0.1462 74.73 0.5846 0.6754 0.0166 0.0144 0.641 4.486 2.171 477.627 0.507 9.656 2.061 0.54 195342. 0.1188 77.72 0.6080 0.6165 0.0124 0.0122 0.543 3.800 1.614 404.661 0.429 7.180 1.809 0.55 195803. 0.0899 80.71 0.6313 0.5189 0.0081 0.0099 0.441 3.089 1.064 328.954 0.349 4.731 1.466 0.55 196279. 0.0592 83.70 0.6547 0.3463 0.0040 0.0076 0.337 2.358 0.522 251.049 0.266 2.324 0.944 0.55 196769. 0.0267 86.69 0.6781 -0.0077 -0.0001 0.0052 0.230 1.608 -0.008 171.183 0.182 -0.034 -0.020 0.55 197262. 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 0.0924 0.0301 1.840 11.599 14.904 1372.341 1.310 66.295 4.926 0.59 209381. 0.7439 3.32 0.0234 0.0696 0.0911 0.0306 1.868 11.773 14.693 1392.913 1.330 65.356 4.785 0.60 209516. 0.7174 6.64 0.0467 0.1352 0.0897 0.0310 1.894 11.938 14.464 1412.430 1.349 64.334 4.645 0.60 209662. 0.6910 9.96 0.0701 0.1968 0.0881 0.0314 1.918 12.091 14.214 1430.473 1.366 63.226 4.507 0.60 209820. 0.6647 13.28 0.0935 0.2545 0.0864 0.0317 1.940 12.227 13.944 1446.622 1.381 62.024 4.372 0.60 209991. 0.6386 16.60 0.1169 0.3086 0.0846 0.0320 1.958 12.344 13.652 1460.423 1.395 60.724 4.240 0.60 210175. 0.6128 19.92 0.1402 0.3590 0.0827 0.0323 1.973 12.437 13.336 1471.401 1.405 59.319 4.111 0.60 210373. 0.5873 23.24 0.1636 0.4061 0.0806 0.0325 1.983 12.501 12.996 1479.067 1.412 57.806 3.985 0.60 210584. 0.5620 26.56 0.1870 0.4498 0.0783 0.0325 1.989 12.534 12.630 1482.920 1.416 56.178 3.863 0.60 210810. 0.5370 29.88 0.2104 0.4905 0.0759 0.0325 1.988 12.530 12.237 1482.467 1.416 54.432 3.744 0.60 211051. 0.5123 33.20 0.2337 0.5281 0.0733 0.0324 1.981 12.486 11.818 1477.229 1.411 52.565 3.629 0.60 211307. 0.4879 36.52 0.2571 0.5630 0.0705 0.0322 1.967 12.397 11.370 1466.746 1.401 50.576 3.516 0.60 211578. 0.4638 39.84 0.2805 0.5950 0.0675 0.0318 1.945 12.261 10.895 1450.603 1.385 48.462 3.407 0.60 211865. 0.4399 43.16 0.3039 0.6244 0.0644 0.0313 1.916 12.073 10.392 1428.424 1.364 46.225 3.300 0.60 212167. 0.4161 46.48 0.3272 0.6511 0.0611 0.0307 1.877 11.832 9.862 1399.891 1.337 43.866 3.195 0.60 212485. 0.3925 49.80 0.3506 0.6752 0.0577 0.0299 1.830 11.535 9.305 1364.736 1.303 41.389 3.093 0.60 212818. 0.3690 53.12 0.3740 0.6965 0.0541 0.0290 1.774 11.180 8.722 1322.697 1.263 38.794 2.991 0.60 213168. 0.3455 56.44 0.3974 0.7150 0.0503 0.0279 1.708 10.765 8.113 1273.592 1.216 36.089 2.889 0.60 213534. 0.3220 59.76 0.4207 0.7304 0.0464 0.0267 1.633 10.291 7.483 1217.574 1.163 33.286 2.788 0.60 213915. 0.2983 63.08 0.4441 0.7423 0.0424 0.0253 1.549 9.761 6.835 1154.887 1.103 30.401 2.684 0.60 214313. 0.2745 66.40 0.4675 0.7504 0.0382 0.0238 1.456 9.177 6.171 1085.751 1.037 27.447 2.578 0.60 214727. 0.2505 69.72 0.4908 0.7538 0.0341 0.0222 1.355 8.540 5.494 1010.374 0.965 24.437 2.466 0.60 215157. 0.2261 73.04 0.5142 0.7515 0.0298 0.0204 1.246 7.852 4.807 928.985 0.887 21.382 2.347 0.60 215604. 0.2013 76.36 0.5376 0.7418 0.0255 0.0185 1.129 7.116 4.113 841.850 0.804 18.294 2.216 0.60 216066. 0.1758 79.68 0.5610 0.7220 0.0212 0.0164 1.005 6.333 3.415 749.301 0.716 15.188 2.067 0.60 216546. 0.1494 83.00 0.5843 0.6876 0.0168 0.0143 0.874 5.509 2.715 651.754 0.622 12.078 1.890 0.61 217041. 0.1218 86.32 0.6077 0.6305 0.0125 0.0121 0.737 4.646 2.019 549.729 0.525 8.981 1.666 0.61 217553. 0.0926 89.64 0.6311 0.5342 0.0082 0.0097 0.595 3.752 1.330 443.872 0.424 5.917 1.359 0.61 218082. 0.0613 92.96 0.6545 0.3605 0.0040 0.0074 0.449 2.831 0.653 334.951 0.320 2.905 0.884 0.61 218626. 0.0280 96.28 0.6778 -0.0088 -0.0001 0.0049 0.299 1.887 -0.010 223.271 0.213 -0.046 -0.021 0.61 219172. 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 0.0934 0.0304 2.475 14.184 18.227 1845.893 1.602 81.072 4.479 0.65 230301. 0.7480 3.65 0.0234 0.0696 0.0921 0.0309 2.513 14.399 17.973 1873.911 1.627 79.945 4.350 0.65 230450. 0.7215 7.30 0.0467 0.1352 0.0907 0.0313 2.549 14.603 17.697 1900.495 1.650 78.717 4.224 0.65 230611. 0.6950 10.95 0.0701 0.1968 0.0891 0.0317 2.582 14.792 17.397 1925.078 1.671 77.381 4.099 0.65 230786. 0.6688 14.60 0.0934 0.2545 0.0874 0.0321 2.611 14.961 17.071 1947.075 1.690 75.931 3.977 0.65 230974. 0.6427 18.25 0.1168 0.3086 0.0856 0.0324 2.636 15.105 16.717 1965.873 1.707 74.359 3.857 0.65 231177. 0.6169 21.90 0.1402 0.3591 0.0837 0.0327 2.656 15.220 16.335 1980.826 1.720 72.658 3.740 0.66 231395. 0.5913 25.55 0.1635 0.4062 0.0816 0.0328 2.670 15.301 15.922 1991.262 1.729 70.821 3.627 0.66 231629. 0.5661 29.20 0.1869 0.4501 0.0793 0.0329 2.677 15.341 15.477 1996.505 1.733 68.843 3.516 0.66 231878. 0.5411 32.85 0.2102 0.4909 0.0768 0.0329 2.677 15.336 15.000 1995.882 1.733 66.720 3.409 0.66 232143. 0.5164 36.50 0.2336 0.5288 0.0742 0.0328 2.667 15.281 14.489 1988.739 1.726 64.447 3.304 0.66 232425. 0.4920 40.15 0.2570 0.5638 0.0714 0.0326 2.648 15.171 13.944 1974.463 1.714 62.021 3.203 0.66 232724. 0.4679 43.80 0.2803 0.5961 0.0685 0.0322 2.618 15.003 13.364 1952.484 1.695 59.442 3.104 0.66 233040. 0.4439 47.45 0.3037 0.6258 0.0653 0.0317 2.578 14.771 12.749 1922.299 1.669 56.710 3.008 0.66 233373. 0.4202 51.10 0.3270 0.6528 0.0620 0.0311 2.526 14.472 12.101 1883.477 1.635 53.826 2.914 0.66 233723. 0.3966 54.75 0.3504 0.6773 0.0585 0.0303 2.462 14.105 11.420 1835.655 1.594 50.796 2.822 0.66 234091. 0.3730 58.40 0.3738 0.6990 0.0548 0.0293 2.385 13.666 10.706 1778.489 1.544 47.621 2.730 0.66 234476. 0.3495 62.05 0.3971 0.7180 0.0510 0.0282 2.295 13.153 9.961 1711.727 1.486 44.308 2.640 0.66 234878. 0.3259 65.70 0.4205 0.7340 0.0471 0.0270 2.193 12.567 9.189 1635.563 1.420 40.873 2.548 0.66 235298. 0.3022 69.35 0.4438 0.7466 0.0430 0.0256 2.079 11.913 8.394 1550.332 1.346 37.337 2.456 0.66 235736. 0.2783 73.00 0.4672 0.7555 0.0388 0.0240 1.953 11.190 7.580 1456.332 1.264 33.715 2.361 0.66 236192. 0.2542 76.65 0.4906 0.7598 0.0346 0.0223 1.816 10.403 6.749 1353.851 1.175 30.021 2.261 0.66 236665. 0.2298 80.30 0.5139 0.7586 0.0303 0.0205 1.667 9.553 5.906 1243.195 1.079 26.271 2.155 0.66 237156. 0.2049 83.95 0.5373 0.7501 0.0259 0.0185 1.508 8.642 5.054 1124.733 0.976 22.481 2.038 0.66 237665. 0.1792 87.60 0.5606 0.7318 0.0215 0.0165 1.340 7.675 4.196 998.911 0.867 18.666 1.905 0.66 238192. 0.1527 91.25 0.5840 0.6990 0.0171 0.0143 1.162 6.657 3.337 866.297 0.752 14.845 1.747 0.67 238737. 0.1249 94.90 0.6074 0.6437 0.0127 0.0120 0.976 5.591 2.482 727.599 0.632 11.039 1.547 0.67 239300. 0.0953 98.55 0.6307 0.5489 0.0084 0.0096 0.783 4.485 1.635 583.702 0.507 7.273 1.271 0.67 239880. 0.0635 102.20 0.6541 0.3744 0.0041 0.0072 0.584 3.348 0.803 435.672 0.378 3.571 0.836 0.67 240478. 0.0293 105.85 0.6774 -0.0098 -0.0001 0.0047 0.381 2.182 -0.013 283.930 0.246 -0.059 -0.021 0.67 241078. 0.0000 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 0.0945 0.0309 3.264 17.146 21.956 2434.326 1.937 97.659 4.091 0.71 251215. 0.7498 3.98 0.0233 0.0693 0.0932 0.0314 3.313 17.402 21.658 2470.660 1.966 96.334 3.976 0.71 251377. 0.7238 7.96 0.0467 0.1347 0.0918 0.0318 3.360 17.646 21.332 2505.266 1.994 94.886 3.862 0.71 251553. 0.6978 11.94 0.0700 0.1962 0.0903 0.0322 3.403 17.872 20.978 2537.385 2.019 93.308 3.750 0.71 251744. 0.6718 15.91 0.0934 0.2539 0.0886 0.0326 3.441 18.075 20.591 2566.236 2.042 91.590 3.639 0.71 251951. 0.6460 19.89 0.1167 0.3080 0.0868 0.0329 3.475 18.250 20.172 2590.964 2.062 89.723 3.531 0.71 252173. 0.6204 23.87 0.1400 0.3585 0.0849 0.0332 3.501 18.388 19.716 2610.684 2.078 87.699 3.425 0.71 252411. 0.5950 27.85 0.1634 0.4056 0.0827 0.0333 3.519 18.486 19.224 2624.468 2.088 85.509 3.322 0.71 252667. 0.5698 31.83 0.1867 0.4496 0.0805 0.0334 3.529 18.534 18.693 2631.369 2.094 83.147 3.222 0.72 252939. 0.5450 35.81 0.2101 0.4905 0.0780 0.0334 3.528 18.528 18.122 2630.467 2.093 80.606 3.125 0.72 253230. 0.5203 39.79 0.2334 0.5285 0.0754 0.0333 3.515 18.460 17.510 2620.885 2.086 77.883 3.030 0.72 253538. 0.4960 43.76 0.2567 0.5638 0.0726 0.0330 3.489 18.326 16.855 2601.805 2.070 74.972 2.938 0.72 253865. 0.4719 47.74 0.2801 0.5963 0.0696 0.0327 3.450 18.119 16.159 2572.481 2.047 71.874 2.849 0.72 254210. 0.4480 51.72 0.3034 0.6263 0.0664 0.0322 3.396 17.836 15.420 2532.241 2.015 68.589 2.762 0.72 254574. 0.4243 55.70 0.3268 0.6537 0.0630 0.0315 3.326 17.472 14.640 2480.523 1.974 65.118 2.677 0.72 254957. 0.4007 59.68 0.3501 0.6785 0.0595 0.0307 3.241 17.023 13.819 2416.848 1.923 61.467 2.593 0.72 255358. 0.3771 63.66 0.3735 0.7007 0.0558 0.0297 3.139 16.487 12.959 2340.778 1.863 57.640 2.511 0.72 255779. 0.3536 67.64 0.3968 0.7202 0.0519 0.0286 3.020 15.862 12.060 2251.967 1.792 53.642 2.429 0.72 256219. 0.3300 71.61 0.4201 0.7368 0.0479 0.0273 2.884 15.148 11.128 2150.657 1.711 49.496 2.347 0.72 256677. 0.3062 75.59 0.4435 0.7501 0.0438 0.0259 2.732 14.350 10.167 2037.297 1.621 45.224 2.264 0.72 257155. 0.2823 79.57 0.4668 0.7598 0.0395 0.0243 2.564 13.469 9.183 1912.285 1.522 40.846 2.178 0.72 257652. 0.2582 83.55 0.4902 0.7651 0.0352 0.0226 2.382 12.509 8.179 1776.014 1.413 36.379 2.089 0.72 258168. 0.2337 87.53 0.5135 0.7649 0.0308 0.0207 2.184 11.473 7.159 1628.922 1.296 31.842 1.993 0.72 258704. 0.2086 91.51 0.5368 0.7576 0.0264 0.0187 1.973 10.365 6.127 1471.536 1.171 27.253 1.889 0.72 259259. 0.1829 95.49 0.5602 0.7406 0.0219 0.0166 1.749 9.188 5.088 1304.511 1.038 22.633 1.769 0.73 259833. 0.1561 99.46 0.5835 0.7093 0.0174 0.0143 1.514 7.950 4.048 1128.683 0.898 18.004 1.627 0.73 260427. 0.1280 103.44 0.6069 0.6552 0.0130 0.0120 1.267 6.657 3.011 945.118 0.752 13.391 1.445 0.73 261040. 0.0981 107.42 0.6302 0.5611 0.0085 0.0096 1.013 5.319 1.984 755.149 0.601 8.824 1.192 0.73 261673. 0.0656 111.40 0.6535 0.3850 0.0042 0.0071 0.751 3.947 0.974 560.382 0.446 4.332 0.788 0.73 262325. 0.0304 115.38 0.6769 -0.0103 -0.0001 0.0046 0.485 2.546 -0.016 361.515 0.288 -0.072 -0.020 0.73 262978. 0.0000 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 0.0958 0.0321 4.304 20.867 26.122 3209.439 2.358 116.192 3.692 0.77 272119. 0.7381 4.30 0.0233 0.0679 0.0946 0.0325 4.358 21.131 25.779 3250.044 2.387 114.667 3.598 0.77 272296. 0.7146 8.61 0.0466 0.1322 0.0932 0.0328 4.410 21.381 25.403 3288.513 2.416 112.995 3.504 0.77 272487. 0.6908 12.91 0.0699 0.1931 0.0917 0.0332 4.458 21.611 24.992 3323.958 2.442 111.165 3.410 0.77 272695. 0.6669 17.22 0.0932 0.2504 0.0900 0.0335 4.500 21.816 24.543 3355.464 2.465 109.168 3.318 0.77 272919. 0.6429 21.52 0.1165 0.3044 0.0882 0.0338 4.535 21.989 24.054 3382.022 2.484 106.991 3.226 0.77 273160. 0.6189 25.83 0.1399 0.3550 0.0863 0.0340 4.563 22.123 23.521 3402.568 2.499 104.623 3.135 0.77 273419. 0.5948 30.13 0.1632 0.4024 0.0842 0.0341 4.581 22.210 22.944 3415.966 2.509 102.055 3.046 0.77 273697. 0.5708 34.43 0.1865 0.4467 0.0819 0.0342 4.588 22.243 22.320 3421.052 2.513 99.278 2.959 0.77 273993. 0.5469 38.74 0.2098 0.4880 0.0794 0.0341 4.582 22.214 21.647 3416.649 2.510 96.284 2.874 0.78 274308. 0.5230 43.04 0.2331 0.5265 0.0767 0.0340 4.562 22.116 20.924 3401.593 2.499 93.068 2.790 0.78 274643. 0.4992 47.35 0.2564 0.5621 0.0739 0.0337 4.526 21.942 20.149 3374.756 2.479 89.625 2.708 0.78 274998. 0.4755 51.65 0.2797 0.5951 0.0709 0.0333 4.472 21.684 19.324 3335.076 2.450 85.954 2.628 0.78 275373. 0.4519 55.96 0.3030 0.6255 0.0677 0.0328 4.401 21.336 18.448 3281.587 2.411 82.055 2.550 0.78 275768. 0.4284 60.26 0.3263 0.6533 0.0643 0.0321 4.309 20.893 17.521 3213.441 2.360 77.932 2.473 0.78 276183. 0.4049 64.56 0.3496 0.6786 0.0607 0.0313 4.197 20.350 16.544 3129.918 2.299 73.589 2.398 0.78 276618. 0.3815 68.87 0.3729 0.7013 0.0569 0.0303 4.064 19.703 15.520 3030.392 2.226 69.033 2.323 0.78 277074. 0.3580 73.17 0.3963 0.7214 0.0530 0.0291 3.908 18.948 14.449 2914.372 2.141 64.270 2.249 0.78 277551. 0.3344 77.48 0.4196 0.7385 0.0489 0.0278 3.731 18.089 13.337 2782.201 2.044 59.325 2.174 0.78 278048. 0.3106 81.78 0.4429 0.7525 0.0447 0.0263 3.533 17.129 12.191 2634.532 1.935 54.225 2.099 0.78 278565. 0.2867 86.09 0.4662 0.7627 0.0404 0.0247 3.315 16.072 11.015 2472.000 1.816 48.994 2.021 0.78 279104. 0.2624 90.39 0.4895 0.7685 0.0360 0.0229 3.078 14.923 9.814 2295.286 1.686 43.654 1.939 0.78 279663. 0.2377 94.69 0.5128 0.7687 0.0315 0.0210 2.823 13.687 8.594 2105.124 1.546 38.226 1.852 0.78 280242. 0.2123 99.00 0.5361 0.7614 0.0270 0.0190 2.551 12.369 7.359 1902.420 1.397 32.732 1.754 0.78 280843. 0.1862 103.30 0.5594 0.7439 0.0224 0.0169 2.264 10.977 6.114 1688.313 1.240 27.196 1.643 0.79 281464. 0.1589 107.61 0.5827 0.7111 0.0178 0.0146 1.964 9.520 4.866 1464.199 1.076 21.644 1.507 0.79 282106. 0.1301 111.91 0.6060 0.6542 0.0133 0.0123 1.652 8.009 3.621 1231.811 0.905 16.107 1.333 0.79 282770. 0.0993 116.22 0.6294 0.5555 0.0088 0.0099 1.332 6.458 2.387 993.251 0.730 10.619 1.090 0.79 283454. 0.0659 120.52 0.6527 0.3744 0.0043 0.0075 1.007 4.882 1.173 750.949 0.552 5.218 0.709 0.79 284158. 0.0300 124.82 0.6760 -0.0091 -0.0001 0.0051 0.679 3.290 -0.019 506.023 0.372 -0.083 -0.017 0.79 284865. 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 0.0973 0.0349 5.844 26.311 30.753 4358.014 2.973 136.791 3.201 0.83 293013. 0.6943 4.63 0.0233 0.0637 0.0960 0.0351 5.891 26.522 30.367 4392.992 2.996 135.073 3.135 0.83 293203. 0.6759 9.27 0.0466 0.1247 0.0947 0.0354 5.933 26.712 29.941 4424.509 3.018 133.179 3.069 0.83 293410. 0.6570 13.90 0.0699 0.1830 0.0932 0.0356 5.970 26.876 29.474 4451.602 3.036 131.099 3.003 0.83 293635. 0.6378 18.53 0.0932 0.2386 0.0916 0.0358 5.999 27.007 28.961 4473.292 3.051 128.817 2.936 0.83 293877. 0.6182 23.17 0.1165 0.2915 0.0898 0.0359 6.019 27.099 28.399 4488.515 3.062 126.321 2.870 0.83 294138. 0.5982 27.80 0.1398 0.3416 0.0879 0.0360 6.029 27.144 27.787 4496.120 3.067 123.595 2.803 0.83 294418. 0.5780 32.43 0.1631 0.3891 0.0858 0.0359 6.028 27.137 27.120 4494.908 3.066 120.628 2.737 0.83 294719. 0.5575 37.07 0.1864 0.4339 0.0835 0.0359 6.013 27.069 26.396 4483.625 3.058 117.409 2.670 0.83 295039. 0.5367 41.70 0.2097 0.4761 0.0810 0.0357 5.982 26.932 25.613 4460.982 3.043 113.928 2.604 0.83 295381. 0.5156 46.33 0.2330 0.5157 0.0783 0.0354 5.935 26.719 24.770 4425.703 3.019 110.177 2.539 0.84 295743. 0.4942 50.97 0.2563 0.5526 0.0755 0.0350 5.869 26.423 23.865 4376.552 2.985 106.152 2.473 0.84 296127. 0.4726 55.60 0.2796 0.5871 0.0724 0.0345 5.783 26.035 22.898 4312.352 2.941 101.850 2.408 0.84 296532. 0.4508 60.23 0.3029 0.6189 0.0692 0.0338 5.675 25.550 21.869 4231.999 2.887 97.272 2.344 0.84 296959. 0.4287 64.87 0.3262 0.6482 0.0657 0.0331 5.544 24.961 20.778 4134.487 2.820 92.421 2.279 0.84 297408. 0.4064 69.50 0.3495 0.6750 0.0621 0.0321 5.389 24.263 19.628 4018.917 2.741 87.306 2.215 0.84 297879. 0.3839 74.13 0.3728 0.6989 0.0583 0.0311 5.210 23.456 18.420 3885.144 2.650 81.931 2.150 0.84 298371. 0.3610 78.77 0.3961 0.7197 0.0543 0.0299 5.006 22.539 17.155 3733.315 2.546 76.305 2.084 0.84 298886. 0.3377 83.40 0.4194 0.7373 0.0501 0.0285 4.778 21.510 15.840 3562.802 2.430 70.457 2.017 0.84 299422. 0.3140 88.04 0.4427 0.7511 0.0458 0.0270 4.526 20.378 14.483 3375.382 2.302 64.419 1.946 0.84 299981. 0.2897 92.67 0.4660 0.7606 0.0414 0.0254 4.252 19.144 13.089 3171.006 2.163 58.220 1.872 0.84 300561. 0.2650 97.30 0.4893 0.7650 0.0369 0.0236 3.957 17.812 11.665 2950.386 2.012 51.886 1.793 0.84 301164. 0.2396 101.94 0.5126 0.7627 0.0323 0.0217 3.641 16.392 10.216 2715.053 1.852 45.442 1.707 0.84 301789. 0.2134 106.57 0.5359 0.7517 0.0277 0.0197 3.308 14.891 8.749 2466.558 1.682 38.917 1.609 0.85 302436. 0.1862 111.20 0.5592 0.7284 0.0230 0.0176 2.960 13.324 7.270 2206.924 1.505 32.338 1.494 0.85 303106. 0.1576 115.84 0.5825 0.6875 0.0183 0.0155 2.600 11.704 5.786 1938.540 1.322 25.736 1.354 0.85 303797. 0.1274 120.47 0.6058 0.6197 0.0136 0.0133 2.232 10.046 4.305 1664.062 1.135 19.147 1.173 0.85 304512. 0.0952 125.10 0.6291 0.5087 0.0090 0.0111 1.860 8.372 2.836 1386.631 0.946 12.614 0.928 0.85 305248. 0.0611 129.74 0.6524 0.3230 0.0044 0.0089 1.488 6.699 1.389 1109.651 0.757 6.180 0.568 0.85 306007. 0.0262 134.37 0.6757 -0.0097 -0.0001 0.0067 1.118 5.035 -0.030 834.039 0.569 -0.135 -0.016 0.85 306770. 0.0000 PROP RPM = 15000 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 0.0984 0.0399 8.234 34.599 35.728 6140.271 3.909 158.917 2.639 0.89 313906. 0.6171 5.03 0.0236 0.0573 0.0973 0.0401 8.264 34.726 35.306 6162.669 3.923 157.039 2.598 0.89 314112. 0.6040 10.06 0.0472 0.1128 0.0960 0.0402 8.285 34.811 34.836 6177.816 3.933 154.951 2.558 0.89 314337. 0.5905 15.10 0.0709 0.1666 0.0945 0.0402 8.294 34.849 34.315 6184.492 3.937 152.635 2.517 0.89 314581. 0.5767 20.13 0.0945 0.2185 0.0929 0.0402 8.290 34.832 33.739 6181.489 3.935 150.072 2.476 0.89 314845. 0.5625 25.16 0.1181 0.2685 0.0912 0.0401 8.271 34.753 33.103 6167.598 3.926 147.244 2.434 0.89 315131. 0.5479 30.19 0.1417 0.3168 0.0893 0.0399 8.236 34.607 32.404 6141.629 3.910 144.132 2.393 0.89 315438. 0.5329 35.22 0.1653 0.3631 0.0872 0.0397 8.184 34.386 31.637 6102.461 3.885 140.721 2.351 0.89 315767. 0.5174 40.26 0.1889 0.4076 0.0848 0.0393 8.112 34.085 30.800 6048.906 3.851 136.996 2.309 0.89 316119. 0.5014 45.29 0.2126 0.4501 0.0823 0.0389 8.019 33.695 29.888 5979.855 3.807 132.944 2.267 0.89 316494. 0.4848 50.32 0.2362 0.4906 0.0796 0.0383 7.905 33.214 28.902 5894.459 3.753 128.557 2.224 0.90 316892. 0.4677 55.35 0.2598 0.5291 0.0767 0.0377 7.767 32.635 27.839 5791.694 3.687 123.830 2.180 0.90 317314. 0.4500 60.38 0.2834 0.5653 0.0736 0.0369 7.604 31.953 26.699 5670.576 3.610 118.759 2.136 0.90 317760. 0.4317 65.42 0.3070 0.5994 0.0702 0.0360 7.416 31.161 25.483 5530.118 3.521 113.346 2.090 0.90 318230. 0.4127 70.45 0.3306 0.6311 0.0666 0.0349 7.200 30.256 24.190 5369.376 3.418 107.596 2.043 0.90 318724. 0.3931 75.48 0.3543 0.6603 0.0629 0.0337 6.957 29.231 22.823 5187.490 3.302 101.518 1.996 0.90 319242. 0.3729 80.51 0.3779 0.6869 0.0589 0.0324 6.684 28.084 21.385 4983.937 3.173 95.119 1.946 0.90 319784. 0.3520 85.54 0.4015 0.7097 0.0548 0.0310 6.388 26.844 19.877 4763.865 3.033 88.412 1.892 0.90 320350. 0.3300 90.58 0.4251 0.7284 0.0504 0.0294 6.071 25.509 18.309 4526.951 2.882 81.437 1.834 0.90 320941. 0.3070 95.61 0.4487 0.7418 0.0460 0.0278 5.735 24.099 16.689 4276.871 2.723 74.231 1.770 0.90 321555. 0.2828 100.64 0.4723 0.7473 0.0414 0.0262 5.395 22.670 15.024 4023.165 2.561 66.825 1.694 0.90 322194. 0.2568 105.67 0.4960 0.7450 0.0367 0.0244 5.039 21.172 13.322 3757.283 2.392 59.258 1.608 0.90 322857. 0.2296 110.71 0.5196 0.7335 0.0319 0.0226 4.665 19.603 11.593 3478.896 2.215 51.564 1.511 0.90 323544. 0.2013 115.74 0.5432 0.7100 0.0271 0.0207 4.278 17.977 9.842 3190.356 2.031 43.778 1.399 0.91 324255. 0.1717 120.77 0.5668 0.6703 0.0223 0.0188 3.882 16.313 8.080 2894.966 1.843 35.941 1.266 0.91 324991. 0.1408 125.80 0.5904 0.6085 0.0174 0.0169 3.482 14.632 6.316 2596.794 1.653 28.096 1.103 0.91 325751. 0.1085 130.83 0.6140 0.5161 0.0126 0.0150 3.084 12.958 4.562 2299.557 1.464 20.292 0.900 0.91 326535. 0.0752 135.87 0.6377 0.3809 0.0078 0.0131 2.692 11.310 2.830 2007.238 1.278 12.588 0.640 0.91 327345. 0.0421 140.90 0.6613 0.1843 0.0031 0.0112 2.311 9.712 1.134 1723.589 1.097 5.044 0.298 0.91 328177. 0.0124 145.93 0.6849 PROP RPM = 16000 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 0.0980 0.0455 11.382 44.837 40.473 8487.651 5.066 180.024 2.163 0.95 334842. 0.5382 5.36 0.0236 0.0500 0.0970 0.0457 11.435 45.046 40.065 8527.203 5.089 178.210 2.131 0.95 335056. 0.5277 10.71 0.0471 0.0986 0.0959 0.0458 11.473 45.196 39.606 8555.498 5.106 176.167 2.100 0.95 335290. 0.5169 16.07 0.0707 0.1458 0.0946 0.0459 11.492 45.272 39.090 8569.884 5.115 173.872 2.069 0.95 335545. 0.5060 21.43 0.0943 0.1915 0.0932 0.0459 11.489 45.260 38.511 8567.716 5.113 171.297 2.039 0.95 335821. 0.4949 26.78 0.1179 0.2360 0.0917 0.0458 11.461 45.148 37.863 8546.475 5.101 168.416 2.009 0.95 336121. 0.4837 32.14 0.1414 0.2791 0.0899 0.0456 11.404 44.923 37.141 8503.890 5.075 165.202 1.981 0.95 336444. 0.4723 37.50 0.1650 0.3211 0.0880 0.0452 11.316 44.575 36.338 8438.022 5.036 161.631 1.953 0.95 336791. 0.4606 42.86 0.1886 0.3619 0.0858 0.0447 11.194 44.097 35.450 8347.422 4.982 157.683 1.926 0.95 337163. 0.4486 48.21 0.2121 0.4015 0.0835 0.0441 11.038 43.482 34.474 8231.013 4.913 153.338 1.900 0.95 337561. 0.4363 53.57 0.2357 0.4399 0.0809 0.0433 10.846 42.727 33.405 8088.123 4.827 148.585 1.873 0.95 337983. 0.4235 58.93 0.2593 0.4771 0.0781 0.0424 10.619 41.830 32.242 7918.408 4.726 143.413 1.847 0.96 338432. 0.4102 64.28 0.2828 0.5129 0.0750 0.0414 10.355 40.791 30.984 7721.671 4.609 137.818 1.820 0.96 338907. 0.3963 69.64 0.3064 0.5473 0.0717 0.0402 10.055 39.608 29.631 7497.844 4.475 131.800 1.793 0.96 339407. 0.3817 75.00 0.3300 0.5800 0.0682 0.0388 9.718 38.284 28.185 7247.027 4.325 125.366 1.764 0.96 339933. 0.3663 80.35 0.3536 0.6109 0.0645 0.0373 9.346 36.818 26.647 6969.571 4.160 118.527 1.734 0.96 340485. 0.3502 85.71 0.3771 0.6398 0.0606 0.0357 8.939 35.213 25.022 6665.812 3.978 111.296 1.703 0.96 341063. 0.3331 91.07 0.4007 0.6661 0.0564 0.0340 8.499 33.480 23.312 6337.712 3.783 103.692 1.668 0.96 341667. 0.3151 96.43 0.4243 0.6878 0.0521 0.0322 8.047 31.700 21.527 6000.798 3.581 95.752 1.627 0.96 342296. 0.2953 101.78 0.4478 0.7044 0.0476 0.0303 7.582 29.867 19.679 5653.805 3.374 87.531 1.579 0.96 342951. 0.2739 107.14 0.4714 0.7130 0.0430 0.0285 7.122 28.056 17.775 5310.945 3.170 79.064 1.518 0.96 343632. 0.2504 112.50 0.4950 0.7042 0.0383 0.0269 6.738 26.542 15.818 5024.313 2.999 70.358 1.428 0.96 344338. 0.2222 117.85 0.5186 0.6842 0.0335 0.0254 6.350 25.015 13.826 4735.386 2.826 61.499 1.324 0.96 345070. 0.1926 123.21 0.5421 0.6513 0.0286 0.0238 5.958 23.472 11.812 4443.248 2.652 52.541 1.206 0.97 345827. 0.1621 128.57 0.5657 0.6028 0.0237 0.0222 5.568 21.932 9.789 4151.712 2.478 43.541 1.069 0.97 346610. 0.1309 133.92 0.5893 0.5355 0.0188 0.0207 5.182 20.411 7.770 3863.862 2.306 34.563 0.912 0.97 347418. 0.0995 139.28 0.6128 0.4462 0.0140 0.0192 4.805 18.930 5.773 3583.342 2.139 25.677 0.731 0.97 348253. 0.0687 144.64 0.6364 0.3310 0.0092 0.0178 4.444 17.506 3.814 3313.848 1.978 16.963 0.522 0.97 349115. 0.0399 150.00 0.6600 0.1865 0.0046 0.0164 4.100 16.149 1.911 3057.077 1.825 8.502 0.284 0.97 350005. 0.0153 155.35 0.6836 0.0062 0.0001 0.0150 3.757 14.801 0.056 2801.887 1.672 0.249 0.009 0.97 350940. 0.0001