15x7E (15x7E.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 0.0807 0.0317 0.002 0.122 0.130 1.446 0.014 0.579 40.863 0.06 20957. 0.5769 0.30 0.0208 0.0517 0.0793 0.0319 0.002 0.123 0.128 1.455 0.014 0.569 39.913 0.06 20969. 0.5586 0.59 0.0416 0.1009 0.0778 0.0321 0.002 0.124 0.126 1.462 0.014 0.559 38.956 0.06 20981. 0.5400 0.89 0.0624 0.1476 0.0763 0.0322 0.002 0.124 0.123 1.469 0.014 0.547 37.995 0.06 20995. 0.5213 1.18 0.0832 0.1918 0.0746 0.0323 0.002 0.125 0.120 1.473 0.014 0.535 37.032 0.06 21009. 0.5024 1.48 0.1040 0.2335 0.0728 0.0324 0.002 0.125 0.117 1.476 0.014 0.522 36.067 0.06 21024. 0.4834 1.77 0.1248 0.2727 0.0709 0.0324 0.002 0.125 0.114 1.477 0.014 0.508 35.100 0.06 21041. 0.4642 2.07 0.1456 0.3094 0.0688 0.0324 0.002 0.125 0.111 1.476 0.014 0.494 34.131 0.06 21058. 0.4449 2.36 0.1664 0.3435 0.0667 0.0323 0.002 0.124 0.108 1.472 0.014 0.479 33.159 0.06 21076. 0.4255 2.66 0.1872 0.3751 0.0644 0.0322 0.002 0.124 0.104 1.465 0.014 0.462 32.184 0.06 21096. 0.4059 2.95 0.2080 0.4041 0.0621 0.0319 0.002 0.123 0.100 1.455 0.014 0.445 31.202 0.06 21117. 0.3862 3.25 0.2288 0.4304 0.0596 0.0317 0.002 0.122 0.096 1.443 0.014 0.427 30.213 0.06 21139. 0.3664 3.54 0.2496 0.4540 0.0569 0.0313 0.002 0.121 0.092 1.427 0.014 0.409 29.212 0.06 21162. 0.3464 3.84 0.2704 0.4747 0.0542 0.0309 0.002 0.119 0.087 1.407 0.013 0.389 28.195 0.06 21186. 0.3262 4.14 0.2912 0.4924 0.0514 0.0304 0.002 0.117 0.083 1.384 0.013 0.369 27.158 0.06 21211. 0.3058 4.43 0.3120 0.5069 0.0484 0.0298 0.002 0.115 0.078 1.357 0.013 0.347 26.094 0.06 21238. 0.2852 4.73 0.3327 0.5179 0.0453 0.0291 0.002 0.112 0.073 1.326 0.013 0.325 24.995 0.06 21266. 0.2643 5.02 0.3535 0.5252 0.0421 0.0283 0.002 0.109 0.068 1.291 0.012 0.302 23.854 0.06 21295. 0.2432 5.32 0.3743 0.5283 0.0388 0.0275 0.002 0.106 0.063 1.253 0.012 0.279 22.662 0.06 21326. 0.2218 5.61 0.3951 0.5267 0.0354 0.0266 0.002 0.102 0.057 1.212 0.012 0.254 21.407 0.06 21357. 0.2002 5.91 0.4159 0.5200 0.0320 0.0256 0.002 0.099 0.052 1.167 0.011 0.230 20.075 0.06 21390. 0.1785 6.20 0.4367 0.5072 0.0285 0.0245 0.001 0.095 0.046 1.118 0.011 0.205 18.651 0.06 21424. 0.1565 6.50 0.4575 0.4876 0.0250 0.0234 0.001 0.090 0.040 1.067 0.010 0.179 17.114 0.06 21460. 0.1343 6.79 0.4783 0.4599 0.0214 0.0222 0.001 0.086 0.034 1.013 0.010 0.153 15.439 0.06 21497. 0.1121 7.09 0.4991 0.4225 0.0177 0.0210 0.001 0.081 0.029 0.955 0.009 0.127 13.595 0.06 21535. 0.0900 7.39 0.5199 0.3736 0.0141 0.0196 0.001 0.076 0.023 0.895 0.009 0.101 11.538 0.06 21574. 0.0681 7.68 0.5407 0.3104 0.0105 0.0183 0.001 0.070 0.017 0.833 0.008 0.075 9.217 0.06 21615. 0.0469 7.98 0.5615 0.2293 0.0069 0.0169 0.001 0.065 0.011 0.768 0.007 0.049 6.559 0.06 21657. 0.0270 8.27 0.5823 0.1256 0.0033 0.0154 0.001 0.059 0.005 0.701 0.007 0.024 3.465 0.06 21701. 0.0099 8.57 0.6031 -0.0080 -0.0002 0.0139 0.001 0.053 0.000 0.633 0.006 -0.001 -0.212 0.06 21745. 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 0.0810 0.0287 0.014 0.442 0.523 10.467 0.050 2.326 22.659 0.12 41914. 0.6409 0.59 0.0209 0.0575 0.0796 0.0289 0.014 0.446 0.514 10.550 0.050 2.286 22.092 0.12 41937. 0.6195 1.19 0.0418 0.1120 0.0781 0.0291 0.014 0.449 0.504 10.624 0.051 2.243 21.526 0.12 41962. 0.5979 1.78 0.0626 0.1635 0.0765 0.0293 0.014 0.452 0.494 10.687 0.051 2.197 20.963 0.12 41989. 0.5763 2.37 0.0835 0.2122 0.0748 0.0295 0.014 0.454 0.483 10.737 0.051 2.148 20.402 0.12 42018. 0.5546 2.97 0.1044 0.2580 0.0730 0.0295 0.014 0.455 0.471 10.772 0.051 2.096 19.844 0.12 42049. 0.5329 3.56 0.1253 0.3010 0.0711 0.0296 0.014 0.456 0.459 10.791 0.052 2.041 19.291 0.12 42082. 0.5112 4.15 0.1462 0.3412 0.0691 0.0296 0.014 0.456 0.446 10.790 0.052 1.983 18.741 0.12 42117. 0.4895 4.75 0.1670 0.3785 0.0669 0.0295 0.014 0.455 0.432 10.768 0.051 1.921 18.196 0.12 42154. 0.4678 5.34 0.1879 0.4132 0.0647 0.0294 0.014 0.453 0.417 10.724 0.051 1.856 17.653 0.12 42193. 0.4461 5.93 0.2088 0.4450 0.0623 0.0292 0.014 0.450 0.402 10.654 0.051 1.788 17.113 0.12 42235. 0.4244 6.53 0.2297 0.4741 0.0598 0.0290 0.014 0.446 0.386 10.557 0.050 1.716 16.574 0.12 42279. 0.4027 7.12 0.2506 0.5004 0.0571 0.0286 0.014 0.441 0.369 10.432 0.050 1.640 16.034 0.12 42326. 0.3809 7.71 0.2714 0.5237 0.0544 0.0282 0.014 0.434 0.351 10.277 0.049 1.561 15.492 0.12 42374. 0.3590 8.30 0.2923 0.5441 0.0515 0.0277 0.014 0.426 0.332 10.090 0.048 1.479 14.945 0.12 42426. 0.3371 8.90 0.3132 0.5613 0.0485 0.0271 0.013 0.417 0.313 9.871 0.047 1.393 14.390 0.12 42479. 0.3150 9.49 0.3341 0.5752 0.0454 0.0264 0.013 0.406 0.293 9.618 0.046 1.304 13.823 0.12 42535. 0.2928 10.08 0.3550 0.5853 0.0422 0.0256 0.013 0.394 0.272 9.333 0.045 1.212 13.240 0.12 42594. 0.2703 10.68 0.3758 0.5915 0.0389 0.0247 0.012 0.381 0.251 9.015 0.043 1.117 12.635 0.12 42655. 0.2477 11.27 0.3967 0.5931 0.0355 0.0238 0.012 0.366 0.229 8.666 0.041 1.020 12.003 0.12 42719. 0.2249 11.86 0.4176 0.5895 0.0321 0.0227 0.011 0.350 0.207 8.287 0.040 0.921 11.335 0.12 42786. 0.2018 12.46 0.4385 0.5800 0.0286 0.0216 0.011 0.333 0.184 7.878 0.038 0.820 10.620 0.12 42855. 0.1784 13.05 0.4594 0.5634 0.0250 0.0204 0.010 0.314 0.162 7.440 0.036 0.718 9.847 0.12 42926. 0.1548 13.64 0.4802 0.5382 0.0214 0.0191 0.009 0.295 0.138 6.974 0.033 0.615 8.999 0.12 43000. 0.1309 14.24 0.5011 0.5025 0.0178 0.0178 0.009 0.274 0.115 6.481 0.031 0.512 8.051 0.12 43077. 0.1068 14.83 0.5220 0.4533 0.0142 0.0164 0.008 0.252 0.092 5.964 0.028 0.408 6.972 0.12 43157. 0.0826 15.42 0.5429 0.3865 0.0106 0.0149 0.007 0.229 0.068 5.423 0.026 0.304 5.717 0.12 43239. 0.0585 16.02 0.5638 0.2962 0.0070 0.0133 0.007 0.206 0.045 4.863 0.023 0.201 4.218 0.12 43324. 0.0351 16.61 0.5846 0.1726 0.0035 0.0118 0.006 0.181 0.022 4.285 0.020 0.100 2.371 0.12 43411. 0.0139 17.20 0.6055 -0.0002 0.0000 0.0101 0.005 0.156 0.000 3.692 0.018 0.000 -0.003 0.12 43500. 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 0.0813 0.0274 0.045 0.951 1.180 33.747 0.107 5.250 15.864 0.18 62870. 0.6742 0.89 0.0209 0.0605 0.0799 0.0277 0.046 0.959 1.160 34.046 0.108 5.159 15.453 0.18 62905. 0.6510 1.79 0.0419 0.1177 0.0784 0.0279 0.046 0.967 1.138 34.314 0.109 5.062 15.044 0.18 62943. 0.6278 2.68 0.0628 0.1718 0.0768 0.0281 0.046 0.973 1.115 34.546 0.110 4.959 14.638 0.18 62983. 0.6046 3.57 0.0838 0.2228 0.0751 0.0282 0.047 0.979 1.090 34.734 0.111 4.849 14.236 0.18 63027. 0.5814 4.46 0.1047 0.2707 0.0733 0.0283 0.047 0.982 1.064 34.871 0.111 4.732 13.838 0.18 63073. 0.5583 5.36 0.1257 0.3156 0.0713 0.0284 0.047 0.985 1.036 34.950 0.111 4.608 13.444 0.18 63123. 0.5353 6.25 0.1466 0.3576 0.0693 0.0284 0.047 0.985 1.006 34.962 0.111 4.476 13.055 0.18 63176. 0.5123 7.14 0.1676 0.3966 0.0671 0.0284 0.047 0.983 0.975 34.902 0.111 4.337 12.670 0.18 63232. 0.4894 8.03 0.1885 0.4328 0.0649 0.0283 0.047 0.979 0.942 34.761 0.111 4.189 12.290 0.18 63291. 0.4666 8.93 0.2094 0.4661 0.0625 0.0281 0.046 0.973 0.907 34.533 0.110 4.034 11.913 0.18 63354. 0.4438 9.82 0.2304 0.4966 0.0599 0.0278 0.046 0.964 0.870 34.211 0.109 3.871 11.539 0.18 63421. 0.4211 10.71 0.2513 0.5243 0.0573 0.0275 0.045 0.952 0.832 33.790 0.108 3.700 11.167 0.18 63491. 0.3984 11.60 0.2723 0.5491 0.0545 0.0270 0.045 0.937 0.792 33.264 0.106 3.521 10.795 0.18 63564. 0.3757 12.50 0.2932 0.5709 0.0516 0.0265 0.044 0.919 0.750 32.628 0.104 3.335 10.422 0.18 63641. 0.3530 13.39 0.3142 0.5896 0.0486 0.0259 0.043 0.898 0.706 31.877 0.101 3.140 10.046 0.18 63722. 0.3302 14.28 0.3351 0.6050 0.0455 0.0252 0.042 0.874 0.661 31.007 0.099 2.938 9.664 0.18 63807. 0.3072 15.17 0.3561 0.6168 0.0423 0.0244 0.040 0.846 0.614 30.021 0.096 2.730 9.273 0.18 63896. 0.2842 16.07 0.3770 0.6247 0.0390 0.0235 0.039 0.815 0.566 28.922 0.092 2.516 8.870 0.18 63988. 0.2609 16.96 0.3980 0.6282 0.0356 0.0225 0.037 0.781 0.516 27.712 0.088 2.296 8.450 0.18 64085. 0.2375 17.85 0.4189 0.6267 0.0321 0.0215 0.035 0.744 0.466 26.392 0.084 2.073 8.008 0.18 64185. 0.2138 18.74 0.4398 0.6193 0.0286 0.0203 0.033 0.703 0.415 24.967 0.079 1.845 7.536 0.18 64289. 0.1899 19.64 0.4608 0.6048 0.0250 0.0190 0.031 0.660 0.363 23.437 0.075 1.615 7.026 0.18 64397. 0.1656 20.53 0.4817 0.5816 0.0214 0.0177 0.029 0.614 0.311 21.808 0.069 1.382 6.463 0.18 64509. 0.1409 21.42 0.5027 0.5474 0.0178 0.0163 0.027 0.566 0.258 20.083 0.064 1.148 5.829 0.18 64625. 0.1159 22.31 0.5236 0.4989 0.0141 0.0148 0.024 0.515 0.205 18.269 0.058 0.914 5.100 0.18 64745. 0.0904 23.21 0.5446 0.4309 0.0105 0.0133 0.022 0.461 0.153 16.374 0.052 0.680 4.236 0.18 64869. 0.0648 24.10 0.5655 0.3354 0.0069 0.0117 0.019 0.406 0.101 14.407 0.046 0.449 3.175 0.18 64997. 0.0394 24.99 0.5865 0.1988 0.0034 0.0101 0.017 0.349 0.050 12.379 0.039 0.220 1.815 0.18 65129. 0.0158 25.88 0.6074 -0.0046 -0.0001 0.0084 0.014 0.290 -0.001 10.295 0.033 -0.004 -0.040 0.18 65262. 0.0000 PROP RPM = 4000 V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM (mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - - 0.00 0.0000 0.0000 0.0816 0.0267 0.105 1.647 2.106 77.943 0.186 9.368 12.257 0.24 83824. 0.6958 1.19 0.0210 0.0623 0.0802 0.0270 0.106 1.663 2.070 78.680 0.188 9.207 11.933 0.24 83871. 0.6716 2.38 0.0419 0.1212 0.0787 0.0272 0.106 1.677 2.031 79.345 0.189 9.035 11.611 0.24 83922. 0.6473 3.57 0.0629 0.1769 0.0771 0.0274 0.107 1.689 1.990 79.921 0.191 8.851 11.293 0.24 83976. 0.6231 4.76 0.0838 0.2292 0.0754 0.0276 0.108 1.699 1.946 80.392 0.192 8.655 10.978 0.24 84035. 0.5990 5.95 0.1048 0.2784 0.0736 0.0277 0.108 1.706 1.899 80.740 0.193 8.446 10.667 0.24 84097. 0.5750 7.15 0.1258 0.3245 0.0716 0.0278 0.109 1.710 1.849 80.948 0.193 8.225 10.361 0.24 84163. 0.5511 8.34 0.1467 0.3676 0.0696 0.0278 0.109 1.712 1.796 80.998 0.193 7.990 10.058 0.24 84234. 0.5273 9.53 0.1677 0.4077 0.0674 0.0277 0.108 1.709 1.740 80.872 0.193 7.741 9.761 0.24 84309. 0.5037 10.72 0.1886 0.4448 0.0651 0.0276 0.108 1.702 1.681 80.551 0.192 7.478 9.467 0.24 84388. 0.4802 11.91 0.2096 0.4791 0.0627 0.0274 0.107 1.691 1.619 80.021 0.191 7.202 9.177 0.24 84472. 0.4568 13.10 0.2306 0.5106 0.0602 0.0272 0.106 1.675 1.554 79.264 0.189 6.911 8.891 0.24 84561. 0.4335 14.29 0.2515 0.5392 0.0575 0.0268 0.105 1.654 1.485 78.266 0.187 6.606 8.606 0.24 84654. 0.4103 15.48 0.2725 0.5649 0.0548 0.0264 0.103 1.627 1.413 77.014 0.184 6.286 8.324 0.24 84753. 0.3871 16.67 0.2934 0.5877 0.0519 0.0259 0.101 1.595 1.338 75.496 0.180 5.953 8.041 0.24 84856. 0.3639 17.86 0.3144 0.6075 0.0488 0.0253 0.099 1.557 1.260 73.698 0.176 5.606 7.757 0.24 84964. 0.3407 19.05 0.3354 0.6240 0.0457 0.0246 0.096 1.513 1.179 71.612 0.171 5.246 7.470 0.24 85077. 0.3174 20.24 0.3563 0.6371 0.0425 0.0237 0.093 1.463 1.096 69.242 0.165 4.874 7.178 0.24 85196. 0.2939 21.44 0.3773 0.6463 0.0391 0.0228 0.089 1.407 1.010 66.595 0.159 4.492 6.878 0.24 85319. 0.2704 22.63 0.3982 0.6513 0.0357 0.0218 0.085 1.346 0.922 63.677 0.152 4.100 6.566 0.24 85448. 0.2466 23.82 0.4192 0.6514 0.0322 0.0207 0.081 1.278 0.832 60.491 0.144 3.701 6.239 0.24 85581. 0.2226 25.01 0.4401 0.6458 0.0287 0.0196 0.076 1.205 0.741 57.045 0.136 3.295 5.891 0.24 85720. 0.1983 26.20 0.4611 0.6333 0.0251 0.0183 0.072 1.127 0.648 53.344 0.127 2.884 5.514 0.24 85864. 0.1737 27.39 0.4821 0.6121 0.0215 0.0169 0.066 1.044 0.555 49.397 0.118 2.470 5.098 0.24 86014. 0.1486 28.58 0.5030 0.5800 0.0179 0.0155 0.061 0.955 0.461 45.217 0.108 2.052 4.629 0.24 86169. 0.1230 29.77 0.5240 0.5331 0.0142 0.0140 0.055 0.863 0.368 40.818 0.097 1.635 4.084 0.24 86329. 0.0969 30.96 0.5449 0.4657 0.0106 0.0124 0.049 0.765 0.274 36.218 0.086 1.219 3.431 0.24 86495. 0.0703 32.15 0.5659 0.3686 0.0070 0.0108 0.042 0.664 0.181 31.443 0.075 0.806 2.615 0.24 86666. 0.0435 33.34 0.5869 0.2248 0.0035 0.0091 0.036 0.560 0.090 26.519 0.063 0.400 1.538 0.24 86842. 0.0180 34.54 0.6078 0.0003 0.0000 0.0074 0.029 0.453 0.000 21.456 0.051 0.000 0.002 0.24 87019. 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 0.0820 0.0263 0.201 2.534 3.306 149.896 0.286 14.705 10.003 0.30 104778. 0.7115 1.49 0.0210 0.0636 0.0806 0.0266 0.203 2.559 3.249 151.374 0.289 14.452 9.735 0.30 104837. 0.6864 2.98 0.0420 0.1238 0.0790 0.0268 0.205 2.581 3.188 152.710 0.292 14.182 9.470 0.30 104900. 0.6614 4.47 0.0630 0.1805 0.0774 0.0270 0.206 2.601 3.123 153.872 0.294 13.893 9.207 0.30 104969. 0.6365 5.96 0.0840 0.2339 0.0757 0.0272 0.208 2.617 3.054 154.825 0.296 13.586 8.948 0.30 105041. 0.6117 7.45 0.1049 0.2840 0.0739 0.0273 0.209 2.629 2.981 155.535 0.297 13.258 8.692 0.30 105119. 0.5871 8.94 0.1259 0.3310 0.0720 0.0274 0.209 2.637 2.903 155.967 0.298 12.911 8.441 0.30 105203. 0.5626 10.43 0.1469 0.3748 0.0699 0.0274 0.209 2.639 2.820 156.085 0.298 12.542 8.194 0.30 105291. 0.5382 11.93 0.1679 0.4157 0.0677 0.0274 0.209 2.635 2.732 155.852 0.298 12.152 7.951 0.30 105385. 0.5141 13.42 0.1889 0.4536 0.0654 0.0273 0.208 2.624 2.639 155.234 0.296 11.739 7.711 0.30 105485. 0.4900 14.91 0.2099 0.4885 0.0630 0.0271 0.207 2.607 2.541 154.198 0.294 11.304 7.476 0.30 105590. 0.4662 16.40 0.2309 0.5207 0.0605 0.0268 0.205 2.581 2.439 152.711 0.292 10.847 7.243 0.30 105701. 0.4425 17.89 0.2519 0.5500 0.0578 0.0265 0.202 2.548 2.331 150.744 0.288 10.367 7.013 0.30 105819. 0.4188 19.38 0.2729 0.5764 0.0550 0.0260 0.199 2.506 2.218 148.271 0.283 9.866 6.785 0.30 105942. 0.3953 20.87 0.2938 0.6000 0.0521 0.0255 0.195 2.456 2.100 145.266 0.277 9.342 6.558 0.30 106072. 0.3718 22.36 0.3148 0.6205 0.0490 0.0249 0.190 2.395 1.978 141.704 0.271 8.796 6.330 0.30 106207. 0.3482 23.85 0.3358 0.6379 0.0459 0.0242 0.184 2.325 1.850 137.566 0.263 8.230 6.100 0.30 106349. 0.3246 25.34 0.3568 0.6519 0.0426 0.0233 0.178 2.246 1.719 132.862 0.254 7.645 5.867 0.30 106498. 0.3009 26.83 0.3778 0.6621 0.0393 0.0224 0.171 2.157 1.584 127.602 0.244 7.044 5.629 0.30 106652. 0.2771 28.32 0.3988 0.6682 0.0358 0.0214 0.163 2.059 1.445 121.799 0.233 6.428 5.382 0.30 106813. 0.2531 29.81 0.4198 0.6696 0.0323 0.0203 0.155 1.952 1.304 115.460 0.221 5.801 5.123 0.30 106981. 0.2289 31.30 0.4408 0.6653 0.0288 0.0191 0.146 1.836 1.161 108.598 0.207 5.163 4.848 0.30 107155. 0.2043 32.80 0.4618 0.6542 0.0252 0.0178 0.136 1.711 1.016 101.225 0.193 4.517 4.550 0.30 107336. 0.1794 34.29 0.4827 0.6346 0.0215 0.0164 0.125 1.578 0.869 93.359 0.178 3.865 4.222 0.30 107524. 0.1539 35.78 0.5037 0.6038 0.0179 0.0149 0.114 1.437 0.722 85.024 0.162 3.210 3.850 0.30 107718. 0.1279 37.27 0.5247 0.5581 0.0142 0.0134 0.102 1.289 0.574 76.249 0.146 2.554 3.416 0.30 107918. 0.1012 38.76 0.5457 0.4910 0.0106 0.0118 0.090 1.134 0.427 67.075 0.128 1.901 2.890 0.30 108126. 0.0739 40.25 0.5667 0.3919 0.0070 0.0101 0.077 0.973 0.282 57.549 0.110 1.253 2.221 0.30 108340. 0.0461 41.74 0.5877 0.2409 0.0034 0.0084 0.064 0.807 0.139 47.728 0.091 0.616 1.316 0.30 108561. 0.0192 43.23 0.6087 -0.0056 -0.0001 0.0066 0.050 0.636 -0.002 37.617 0.072 -0.011 -0.030 0.30 108782. 0.0000 PROP RPM = 6000 V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM (mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - - 0.00 0.0000 0.0000 0.0824 0.0261 0.344 3.617 4.786 256.771 0.409 21.290 8.455 0.36 125730. 0.7236 1.81 0.0213 0.0653 0.0810 0.0264 0.348 3.654 4.703 259.409 0.413 20.921 8.224 0.36 125801. 0.6977 3.62 0.0425 0.1270 0.0794 0.0266 0.351 3.688 4.614 261.792 0.417 20.525 7.995 0.36 125879. 0.6718 5.44 0.0638 0.1851 0.0778 0.0268 0.354 3.717 4.519 263.860 0.420 20.102 7.769 0.36 125962. 0.6461 7.25 0.0850 0.2397 0.0761 0.0270 0.356 3.741 4.418 265.552 0.423 19.652 7.546 0.36 126051. 0.6205 9.06 0.1063 0.2910 0.0742 0.0271 0.358 3.758 4.310 266.805 0.425 19.171 7.327 0.36 126147. 0.5950 10.87 0.1275 0.3389 0.0722 0.0272 0.359 3.769 4.195 267.553 0.426 18.660 7.112 0.36 126248. 0.5698 12.68 0.1488 0.3836 0.0701 0.0272 0.359 3.772 4.073 267.732 0.426 18.118 6.901 0.36 126357. 0.5448 14.49 0.1701 0.4253 0.0679 0.0272 0.358 3.765 3.944 267.276 0.425 17.543 6.693 0.36 126472. 0.5200 16.31 0.1913 0.4639 0.0656 0.0270 0.357 3.749 3.807 266.121 0.424 16.935 6.489 0.36 126594. 0.4953 18.12 0.2126 0.4995 0.0631 0.0268 0.354 3.722 3.663 264.206 0.420 16.294 6.289 0.36 126723. 0.4709 19.93 0.2338 0.5322 0.0605 0.0266 0.351 3.683 3.512 261.474 0.416 15.620 6.092 0.36 126859. 0.4465 21.74 0.2551 0.5620 0.0577 0.0262 0.346 3.633 3.353 257.872 0.410 14.912 5.897 0.36 127003. 0.4224 23.55 0.2763 0.5889 0.0549 0.0257 0.340 3.569 3.186 253.351 0.403 14.171 5.704 0.36 127154. 0.3983 25.36 0.2976 0.6129 0.0519 0.0252 0.332 3.492 3.012 247.867 0.394 13.398 5.512 0.36 127313. 0.3742 27.18 0.3189 0.6338 0.0487 0.0245 0.324 3.400 2.831 241.369 0.384 12.592 5.320 0.36 127480. 0.3501 28.99 0.3401 0.6515 0.0455 0.0238 0.314 3.294 2.643 233.834 0.372 11.756 5.127 0.36 127654. 0.3260 30.80 0.3614 0.6657 0.0422 0.0229 0.302 3.174 2.449 225.281 0.359 10.893 4.931 0.36 127836. 0.3018 32.61 0.3826 0.6762 0.0387 0.0219 0.289 3.039 2.250 215.730 0.343 10.006 4.730 0.36 128026. 0.2775 34.42 0.4039 0.6823 0.0352 0.0208 0.275 2.891 2.046 205.198 0.327 9.099 4.522 0.36 128224. 0.2530 36.23 0.4251 0.6836 0.0316 0.0197 0.260 2.729 1.838 193.704 0.308 8.175 4.303 0.36 128430. 0.2282 38.05 0.4464 0.6789 0.0280 0.0184 0.243 2.554 1.627 181.266 0.288 7.236 4.071 0.36 128643. 0.2031 39.86 0.4677 0.6670 0.0243 0.0171 0.225 2.365 1.413 167.913 0.267 6.286 3.817 0.36 128865. 0.1775 41.67 0.4889 0.6458 0.0206 0.0156 0.206 2.165 1.198 153.679 0.245 5.328 3.535 0.36 129096. 0.1514 43.48 0.5102 0.6123 0.0169 0.0141 0.186 1.953 0.982 138.609 0.221 4.367 3.212 0.36 129334. 0.1245 45.29 0.5314 0.5616 0.0132 0.0125 0.165 1.729 0.766 122.765 0.195 3.405 2.829 0.36 129581. 0.0968 47.10 0.5527 0.4856 0.0095 0.0108 0.142 1.496 0.551 106.222 0.169 2.450 2.352 0.36 129836. 0.0683 48.92 0.5739 0.3695 0.0058 0.0091 0.119 1.255 0.338 89.077 0.142 1.505 1.723 0.36 130099. 0.0392 50.73 0.5952 0.1831 0.0022 0.0073 0.096 1.006 0.130 71.431 0.114 0.577 0.823 0.36 130369. 0.0116 52.54 0.6165 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 0.0829 0.0260 0.545 4.905 6.557 406.229 0.554 29.165 7.321 0.42 146679. 0.7333 2.09 0.0210 0.0652 0.0815 0.0263 0.550 4.956 6.445 410.442 0.560 28.667 7.122 0.42 146762. 0.7073 4.18 0.0420 0.1268 0.0800 0.0265 0.556 5.002 6.325 414.256 0.565 28.134 6.925 0.42 146851. 0.6813 6.27 0.0630 0.1849 0.0784 0.0267 0.560 5.042 6.197 417.575 0.570 27.565 6.731 0.42 146947. 0.6555 8.36 0.0840 0.2396 0.0767 0.0269 0.564 5.075 6.061 420.306 0.573 26.958 6.540 0.42 147050. 0.6299 10.44 0.1050 0.2909 0.0748 0.0270 0.566 5.100 5.915 422.350 0.576 26.312 6.353 0.42 147160. 0.6044 12.53 0.1260 0.3389 0.0729 0.0271 0.568 5.115 5.761 423.607 0.578 25.625 6.168 0.42 147277. 0.5792 14.62 0.1471 0.3838 0.0708 0.0271 0.569 5.119 5.597 423.974 0.578 24.895 5.988 0.42 147402. 0.5541 16.71 0.1681 0.4256 0.0686 0.0271 0.568 5.112 5.423 423.350 0.578 24.122 5.810 0.42 147534. 0.5293 18.80 0.1891 0.4645 0.0663 0.0270 0.565 5.091 5.239 421.634 0.575 23.305 5.636 0.42 147674. 0.5047 20.89 0.2101 0.5005 0.0638 0.0268 0.562 5.056 5.046 418.733 0.571 22.443 5.465 0.42 147822. 0.4802 22.98 0.2311 0.5336 0.0612 0.0265 0.556 5.006 4.842 414.556 0.566 21.536 5.297 0.42 147979. 0.4560 25.07 0.2521 0.5639 0.0585 0.0262 0.549 4.939 4.628 409.017 0.558 20.584 5.132 0.42 148144. 0.4318 27.15 0.2731 0.5914 0.0557 0.0257 0.539 4.855 4.404 402.043 0.548 19.588 4.968 0.42 148317. 0.4078 29.24 0.2941 0.6161 0.0527 0.0252 0.528 4.752 4.170 393.560 0.537 18.548 4.806 0.42 148499. 0.3839 31.33 0.3151 0.6379 0.0497 0.0245 0.514 4.631 3.926 383.496 0.523 17.464 4.644 0.42 148690. 0.3599 33.42 0.3361 0.6566 0.0465 0.0238 0.499 4.489 3.673 371.797 0.507 16.339 4.481 0.42 148889. 0.3360 35.51 0.3571 0.6720 0.0432 0.0229 0.481 4.329 3.412 358.484 0.489 15.176 4.317 0.42 149098. 0.3119 37.60 0.3781 0.6839 0.0398 0.0220 0.461 4.149 3.143 343.589 0.469 13.981 4.149 0.42 149315. 0.2878 39.69 0.3991 0.6919 0.0363 0.0209 0.439 3.950 2.868 327.141 0.446 12.758 3.977 0.42 149541. 0.2635 41.78 0.4202 0.6953 0.0327 0.0198 0.415 3.733 2.588 309.165 0.422 11.511 3.797 0.42 149777. 0.2389 43.87 0.4412 0.6934 0.0291 0.0185 0.388 3.498 2.303 289.692 0.395 10.243 3.606 0.42 150021. 0.2140 45.95 0.4622 0.6848 0.0255 0.0172 0.360 3.245 2.014 268.759 0.367 8.959 3.399 0.42 150275. 0.1887 48.04 0.4832 0.6680 0.0218 0.0158 0.330 2.975 1.723 246.417 0.336 7.664 3.172 0.42 150538. 0.1628 50.13 0.5042 0.6401 0.0181 0.0143 0.299 2.689 1.430 222.734 0.304 6.362 2.913 0.42 150810. 0.1363 52.22 0.5252 0.5971 0.0144 0.0127 0.265 2.388 1.137 197.797 0.270 5.059 2.608 0.42 151092. 0.1088 54.31 0.5462 0.5317 0.0107 0.0110 0.230 2.073 0.846 171.719 0.234 3.761 2.233 0.42 151383. 0.0803 56.40 0.5672 0.4315 0.0070 0.0093 0.194 1.746 0.557 144.640 0.197 2.476 1.745 0.42 151684. 0.0509 58.49 0.5882 0.2711 0.0034 0.0075 0.157 1.409 0.272 116.725 0.159 1.210 1.057 0.42 151993. 0.0216 60.58 0.6092 -0.0112 -0.0001 0.0056 0.118 1.062 -0.008 87.940 0.120 -0.036 -0.042 0.42 152300. 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 0.0836 0.0260 0.813 6.409 8.629 606.609 0.724 38.382 6.452 0.48 167625. 0.7414 2.38 0.0210 0.0656 0.0822 0.0263 0.822 6.476 8.483 612.990 0.732 37.731 6.277 0.48 167720. 0.7151 4.77 0.0420 0.1276 0.0806 0.0265 0.830 6.537 8.326 618.765 0.739 37.034 6.103 0.48 167823. 0.6889 7.15 0.0629 0.1860 0.0790 0.0267 0.837 6.591 8.158 623.791 0.745 36.289 5.932 0.48 167933. 0.6628 9.54 0.0839 0.2410 0.0773 0.0269 0.842 6.634 7.980 627.926 0.750 35.494 5.764 0.48 168050. 0.6369 11.92 0.1049 0.2926 0.0754 0.0270 0.846 6.667 7.789 631.021 0.753 34.647 5.599 0.48 168176. 0.6113 14.31 0.1259 0.3410 0.0735 0.0271 0.849 6.687 7.587 632.924 0.755 33.746 5.437 0.48 168310. 0.5858 16.69 0.1469 0.3862 0.0714 0.0272 0.850 6.693 7.372 633.480 0.756 32.789 5.278 0.48 168452. 0.5606 19.08 0.1679 0.4284 0.0692 0.0271 0.848 6.683 7.144 632.537 0.755 31.775 5.123 0.48 168604. 0.5356 21.46 0.1888 0.4676 0.0669 0.0270 0.845 6.656 6.903 629.943 0.752 30.703 4.970 0.48 168764. 0.5108 23.84 0.2098 0.5039 0.0644 0.0268 0.839 6.609 6.648 625.555 0.747 29.572 4.820 0.48 168934. 0.4862 26.23 0.2308 0.5374 0.0618 0.0265 0.830 6.542 6.381 619.236 0.739 28.381 4.674 0.48 169113. 0.4618 28.61 0.2518 0.5681 0.0591 0.0262 0.819 6.454 6.100 610.860 0.729 27.131 4.529 0.48 169301. 0.4376 31.00 0.2728 0.5961 0.0562 0.0257 0.805 6.342 5.805 600.312 0.717 25.822 4.386 0.48 169499. 0.4134 33.38 0.2938 0.6212 0.0532 0.0252 0.788 6.207 5.498 587.484 0.701 24.456 4.245 0.48 169707. 0.3894 35.77 0.3147 0.6435 0.0501 0.0245 0.767 6.046 5.178 572.264 0.683 23.032 4.104 0.48 169925. 0.3653 38.15 0.3357 0.6628 0.0469 0.0238 0.744 5.859 4.846 554.571 0.662 21.553 3.963 0.48 170153. 0.3412 40.54 0.3567 0.6790 0.0436 0.0229 0.717 5.646 4.502 534.431 0.638 20.024 3.821 0.48 170391. 0.3171 42.92 0.3777 0.6917 0.0402 0.0219 0.686 5.408 4.149 511.895 0.611 18.453 3.676 0.48 170639. 0.2929 45.30 0.3987 0.7005 0.0367 0.0209 0.653 5.145 3.787 487.002 0.581 16.845 3.527 0.48 170897. 0.2685 47.69 0.4197 0.7049 0.0331 0.0197 0.617 4.858 3.418 459.792 0.549 15.204 3.372 0.48 171166. 0.2439 50.07 0.4406 0.7041 0.0295 0.0184 0.577 4.546 3.043 430.310 0.514 13.536 3.208 0.48 171445. 0.2189 52.46 0.4616 0.6970 0.0258 0.0171 0.535 4.211 2.663 398.614 0.476 11.847 3.031 0.48 171735. 0.1935 54.84 0.4826 0.6816 0.0221 0.0156 0.489 3.854 2.280 364.780 0.435 10.142 2.835 0.48 172035. 0.1675 57.23 0.5036 0.6555 0.0184 0.0141 0.441 3.475 1.895 328.909 0.393 8.428 2.613 0.48 172345. 0.1407 59.61 0.5246 0.6144 0.0146 0.0125 0.390 3.076 1.509 291.133 0.348 6.713 2.351 0.48 172667. 0.1130 62.00 0.5456 0.5511 0.0109 0.0108 0.337 2.658 1.125 251.622 0.300 5.004 2.028 0.48 172999. 0.0841 64.38 0.5665 0.4525 0.0072 0.0090 0.282 2.225 0.744 210.590 0.251 3.311 1.603 0.48 173342. 0.0541 66.76 0.5875 0.2917 0.0036 0.0072 0.226 1.778 0.370 168.286 0.201 1.645 0.997 0.48 173694. 0.0237 69.15 0.6085 0.0010 0.0000 0.0053 0.167 1.317 0.001 124.696 0.149 0.004 0.003 0.48 174046. 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 0.0843 0.0261 1.163 8.144 11.017 867.180 0.920 49.005 5.763 0.54 188568. 0.7482 2.68 0.0210 0.0659 0.0829 0.0264 1.175 8.231 10.832 876.404 0.930 48.179 5.606 0.54 188675. 0.7217 5.36 0.0420 0.1282 0.0814 0.0266 1.186 8.309 10.633 884.748 0.939 47.294 5.451 0.54 188791. 0.6953 8.05 0.0629 0.1869 0.0797 0.0269 1.196 8.377 10.420 892.004 0.946 46.348 5.298 0.54 188915. 0.6690 10.73 0.0839 0.2422 0.0780 0.0270 1.204 8.433 10.193 897.963 0.953 45.338 5.148 0.54 189048. 0.6430 13.41 0.1049 0.2941 0.0761 0.0272 1.210 8.475 9.951 902.411 0.957 44.260 5.001 0.54 189190. 0.6171 16.09 0.1259 0.3427 0.0742 0.0272 1.214 8.500 9.693 905.128 0.960 43.113 4.857 0.54 189341. 0.5915 18.78 0.1469 0.3882 0.0721 0.0273 1.215 8.508 9.419 905.891 0.961 41.895 4.716 0.54 189502. 0.5662 21.46 0.1679 0.4306 0.0699 0.0272 1.213 8.494 9.128 904.478 0.960 40.603 4.578 0.54 189673. 0.5410 24.14 0.1888 0.4701 0.0675 0.0271 1.208 8.459 8.821 900.671 0.956 39.236 4.442 0.54 189854. 0.5161 26.82 0.2098 0.5068 0.0650 0.0269 1.199 8.398 8.497 894.264 0.949 37.793 4.309 0.54 190045. 0.4914 29.51 0.2308 0.5406 0.0624 0.0266 1.187 8.312 8.155 885.056 0.939 36.273 4.179 0.54 190247. 0.4669 32.19 0.2518 0.5717 0.0597 0.0263 1.171 8.197 7.796 872.868 0.926 34.678 4.051 0.54 190459. 0.4425 34.87 0.2728 0.6000 0.0568 0.0258 1.150 8.053 7.421 857.532 0.910 33.007 3.925 0.54 190683. 0.4182 37.55 0.2938 0.6256 0.0538 0.0253 1.125 7.878 7.028 838.896 0.890 31.262 3.800 0.54 190917. 0.3941 40.24 0.3147 0.6484 0.0507 0.0246 1.095 7.671 6.619 816.797 0.867 29.443 3.676 0.54 191163. 0.3699 42.92 0.3357 0.6682 0.0474 0.0238 1.061 7.430 6.194 791.118 0.839 27.553 3.551 0.54 191419. 0.3458 45.60 0.3567 0.6849 0.0440 0.0229 1.022 7.155 5.755 761.892 0.808 25.599 3.426 0.54 191687. 0.3215 48.28 0.3777 0.6983 0.0406 0.0220 0.978 6.848 5.304 729.191 0.774 23.591 3.299 0.54 191967. 0.2972 50.97 0.3987 0.7079 0.0370 0.0209 0.929 6.509 4.841 693.076 0.735 21.534 3.168 0.54 192258. 0.2727 53.65 0.4196 0.7132 0.0334 0.0197 0.876 6.138 4.370 653.601 0.693 19.436 3.032 0.54 192560. 0.2480 56.33 0.4406 0.7133 0.0298 0.0184 0.819 5.737 3.890 610.833 0.648 17.303 2.889 0.54 192874. 0.2229 59.01 0.4616 0.7072 0.0261 0.0170 0.757 5.305 3.404 564.856 0.599 15.143 2.734 0.54 193200. 0.1973 61.69 0.4826 0.6931 0.0223 0.0155 0.692 4.844 2.914 515.780 0.547 12.962 2.563 0.54 193538. 0.1711 64.38 0.5036 0.6683 0.0185 0.0140 0.622 4.355 2.421 463.751 0.492 10.769 2.368 0.54 193888. 0.1441 67.06 0.5246 0.6285 0.0148 0.0123 0.548 3.841 1.928 408.962 0.434 8.574 2.138 0.54 194250. 0.1161 69.74 0.5455 0.5663 0.0110 0.0106 0.472 3.303 1.436 351.661 0.373 6.388 1.852 0.54 194623. 0.0868 72.42 0.5665 0.4679 0.0073 0.0088 0.392 2.744 0.949 292.160 0.310 4.222 1.474 0.54 195009. 0.0562 75.11 0.5875 0.3040 0.0036 0.0069 0.310 2.168 0.470 230.822 0.245 2.090 0.923 0.54 195405. 0.0248 77.79 0.6085 -0.0023 0.0000 0.0050 0.225 1.574 -0.002 167.584 0.178 -0.011 -0.007 0.55 195799. 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 0.0852 0.0263 1.607 10.130 13.741 1198.483 1.144 61.118 5.200 0.59 209506. 0.7540 2.98 0.0210 0.0661 0.0837 0.0266 1.624 10.239 13.511 1211.338 1.157 60.097 5.059 0.60 209626. 0.7274 5.96 0.0420 0.1285 0.0822 0.0268 1.640 10.337 13.265 1222.954 1.168 59.001 4.920 0.60 209755. 0.7009 8.94 0.0629 0.1874 0.0806 0.0271 1.654 10.422 13.001 1233.037 1.177 57.828 4.782 0.60 209894. 0.6745 11.92 0.0839 0.2428 0.0788 0.0272 1.665 10.492 12.719 1241.304 1.185 56.575 4.648 0.60 210042. 0.6484 14.90 0.1049 0.2949 0.0770 0.0274 1.673 10.544 12.418 1247.448 1.191 55.237 4.515 0.60 210200. 0.6224 17.88 0.1259 0.3437 0.0750 0.0275 1.678 10.575 12.098 1251.165 1.195 53.813 4.386 0.60 210369. 0.5967 20.86 0.1468 0.3894 0.0729 0.0275 1.679 10.583 11.758 1252.143 1.196 52.298 4.259 0.60 210548. 0.5713 23.84 0.1678 0.4321 0.0706 0.0274 1.676 10.566 11.396 1250.072 1.194 50.691 4.135 0.60 210738. 0.5460 26.81 0.1888 0.4718 0.0683 0.0273 1.669 10.520 11.014 1244.652 1.189 48.990 4.014 0.60 210940. 0.5210 29.79 0.2098 0.5087 0.0658 0.0271 1.657 10.444 10.610 1235.592 1.180 47.193 3.895 0.60 211153. 0.4963 32.77 0.2307 0.5429 0.0631 0.0268 1.640 10.334 10.184 1222.618 1.168 45.300 3.778 0.60 211378. 0.4717 35.75 0.2517 0.5743 0.0604 0.0265 1.617 10.189 9.737 1205.474 1.151 43.312 3.664 0.60 211615. 0.4472 38.73 0.2727 0.6030 0.0575 0.0260 1.588 10.007 9.269 1183.935 1.131 41.229 3.551 0.60 211863. 0.4229 41.71 0.2937 0.6290 0.0544 0.0254 1.553 9.786 8.780 1157.786 1.106 39.052 3.440 0.60 212124. 0.3987 44.69 0.3146 0.6522 0.0513 0.0247 1.511 9.524 8.270 1126.807 1.076 36.783 3.329 0.60 212397. 0.3745 47.67 0.3356 0.6725 0.0480 0.0239 1.463 9.220 7.739 1090.826 1.042 34.425 3.218 0.60 212683. 0.3502 50.65 0.3566 0.6898 0.0446 0.0230 1.408 8.874 7.191 1049.891 1.003 31.986 3.107 0.60 212981. 0.3259 53.63 0.3776 0.7038 0.0411 0.0220 1.347 8.487 6.627 1004.100 0.959 29.478 2.994 0.60 213292. 0.3015 56.61 0.3985 0.7142 0.0375 0.0209 1.279 8.060 6.050 953.538 0.911 26.910 2.878 0.60 213616. 0.2769 59.59 0.4195 0.7203 0.0338 0.0197 1.205 7.593 5.461 898.284 0.858 24.289 2.757 0.60 213952. 0.2520 62.57 0.4405 0.7214 0.0301 0.0184 1.124 7.087 4.861 838.429 0.801 21.624 2.630 0.60 214301. 0.2268 65.55 0.4615 0.7163 0.0264 0.0170 1.038 6.543 4.254 774.091 0.739 18.924 2.493 0.60 214663. 0.2011 68.53 0.4824 0.7034 0.0226 0.0155 0.946 5.962 3.642 705.425 0.674 16.198 2.341 0.60 215039. 0.1748 71.51 0.5034 0.6800 0.0188 0.0139 0.848 5.347 3.025 632.635 0.604 13.457 2.169 0.60 215427. 0.1476 74.49 0.5244 0.6416 0.0149 0.0122 0.746 4.699 2.408 555.991 0.531 10.713 1.965 0.60 215829. 0.1193 77.46 0.5454 0.5806 0.0111 0.0104 0.638 4.022 1.794 475.842 0.454 7.979 1.710 0.60 216244. 0.0896 80.44 0.5663 0.4827 0.0073 0.0086 0.527 3.319 1.185 392.624 0.375 5.270 1.369 0.60 216672. 0.0583 83.42 0.5873 0.3164 0.0036 0.0067 0.411 2.594 0.585 306.849 0.293 2.603 0.865 0.61 217113. 0.0259 86.40 0.6083 -0.0045 0.0000 0.0048 0.293 1.846 -0.006 218.381 0.209 -0.025 -0.012 0.61 217549. 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 0.0862 0.0266 2.163 12.393 16.822 1612.910 1.400 74.826 4.731 0.65 230439. 0.7590 3.28 0.0210 0.0661 0.0847 0.0269 2.186 12.527 16.544 1630.307 1.415 73.588 4.603 0.65 230571. 0.7323 6.55 0.0419 0.1286 0.0832 0.0271 2.207 12.648 16.245 1646.006 1.429 72.259 4.477 0.65 230714. 0.7058 9.83 0.0629 0.1875 0.0816 0.0274 2.226 12.752 15.925 1659.609 1.441 70.834 4.352 0.65 230867. 0.6794 13.10 0.0839 0.2430 0.0798 0.0275 2.240 12.838 15.582 1670.725 1.450 69.311 4.230 0.65 231031. 0.6532 16.38 0.1048 0.2951 0.0779 0.0277 2.252 12.901 15.217 1678.944 1.458 67.683 4.111 0.65 231206. 0.6273 19.65 0.1258 0.3441 0.0759 0.0278 2.258 12.938 14.826 1683.848 1.462 65.948 3.994 0.66 231392. 0.6015 22.93 0.1467 0.3899 0.0738 0.0278 2.260 12.947 14.411 1685.017 1.463 64.101 3.879 0.66 231590. 0.5761 26.20 0.1677 0.4328 0.0716 0.0277 2.256 12.924 13.970 1682.033 1.460 62.141 3.767 0.66 231800. 0.5508 29.48 0.1887 0.4727 0.0692 0.0276 2.246 12.867 13.504 1674.487 1.454 60.064 3.658 0.66 232022. 0.5258 32.76 0.2096 0.5099 0.0666 0.0274 2.229 12.770 13.010 1661.988 1.443 57.869 3.551 0.66 232258. 0.5010 36.03 0.2306 0.5443 0.0640 0.0271 2.205 12.634 12.490 1644.166 1.427 55.556 3.446 0.66 232506. 0.4763 39.31 0.2516 0.5760 0.0612 0.0267 2.173 12.453 11.943 1620.680 1.407 53.124 3.343 0.66 232767. 0.4519 42.58 0.2725 0.6050 0.0582 0.0262 2.134 12.227 11.370 1591.223 1.381 50.575 3.241 0.66 233041. 0.4275 45.86 0.2935 0.6314 0.0552 0.0256 2.086 11.952 10.771 1555.509 1.350 47.911 3.141 0.66 233328. 0.4032 49.13 0.3145 0.6551 0.0520 0.0249 2.029 11.628 10.147 1513.245 1.314 45.133 3.041 0.66 233629. 0.3790 52.41 0.3354 0.6759 0.0487 0.0241 1.964 11.251 9.497 1464.198 1.271 42.244 2.942 0.66 233944. 0.3547 55.68 0.3564 0.6938 0.0452 0.0232 1.889 10.822 8.826 1408.423 1.223 39.256 2.842 0.66 234272. 0.3303 58.96 0.3773 0.7085 0.0417 0.0222 1.805 10.343 8.134 1346.057 1.169 36.182 2.741 0.66 234615. 0.3058 62.23 0.3983 0.7195 0.0380 0.0211 1.713 9.814 7.426 1277.215 1.109 33.032 2.637 0.66 234971. 0.2811 65.51 0.4193 0.7265 0.0343 0.0198 1.612 9.236 6.703 1202.007 1.043 29.817 2.530 0.66 235341. 0.2562 68.79 0.4402 0.7285 0.0306 0.0185 1.503 8.610 5.968 1120.558 0.973 26.548 2.416 0.66 235725. 0.2309 72.06 0.4612 0.7245 0.0268 0.0170 1.385 7.938 5.224 1033.028 0.897 23.234 2.293 0.66 236124. 0.2050 75.34 0.4822 0.7129 0.0229 0.0155 1.260 7.220 4.471 939.626 0.816 19.888 2.158 0.66 236536. 0.1785 78.61 0.5031 0.6908 0.0190 0.0139 1.127 6.459 3.715 840.631 0.730 16.523 2.004 0.66 236964. 0.1511 81.89 0.5241 0.6538 0.0151 0.0121 0.988 5.658 2.957 736.412 0.639 13.153 1.821 0.66 237405. 0.1225 85.16 0.5450 0.5943 0.0113 0.0103 0.841 4.821 2.202 627.439 0.545 9.795 1.592 0.66 237862. 0.0924 88.44 0.5660 0.4972 0.0074 0.0085 0.690 3.952 1.454 514.312 0.446 6.468 1.282 0.67 238332. 0.0605 91.71 0.5870 0.3290 0.0037 0.0066 0.533 3.056 0.717 397.740 0.345 3.191 0.818 0.67 238817. 0.0271 94.99 0.6079 -0.0062 0.0000 0.0046 0.372 2.132 -0.009 277.507 0.241 -0.040 -0.015 0.67 239295. 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 0.0874 0.0270 2.852 14.978 20.293 2126.476 1.692 90.265 4.328 0.71 251365. 0.7628 3.57 0.0209 0.0659 0.0859 0.0273 2.882 15.138 19.962 2149.201 1.710 88.791 4.213 0.71 251510. 0.7363 7.14 0.0419 0.1283 0.0844 0.0276 2.910 15.283 19.606 2169.735 1.727 87.206 4.098 0.71 251667. 0.7099 10.71 0.0628 0.1872 0.0827 0.0278 2.934 15.408 19.223 2187.525 1.741 85.505 3.986 0.71 251834. 0.6836 14.28 0.0838 0.2426 0.0810 0.0280 2.953 15.510 18.814 2202.029 1.752 83.683 3.875 0.71 252014. 0.6575 17.85 0.1047 0.2948 0.0791 0.0281 2.967 15.585 18.376 2212.684 1.761 81.735 3.767 0.71 252205. 0.6316 21.42 0.1257 0.3438 0.0771 0.0282 2.976 15.629 17.908 2218.921 1.766 79.655 3.661 0.71 252409. 0.6060 24.99 0.1466 0.3897 0.0749 0.0282 2.977 15.638 17.410 2220.174 1.767 77.440 3.557 0.71 252626. 0.5805 28.56 0.1676 0.4327 0.0727 0.0281 2.972 15.608 16.881 2215.895 1.763 75.086 3.455 0.72 252856. 0.5553 32.13 0.1885 0.4728 0.0702 0.0280 2.958 15.535 16.320 2205.540 1.755 72.590 3.356 0.72 253100. 0.5304 35.70 0.2095 0.5101 0.0677 0.0278 2.935 15.415 15.726 2188.595 1.742 69.950 3.259 0.72 253357. 0.5056 39.27 0.2304 0.5448 0.0650 0.0275 2.903 15.246 15.100 2164.577 1.723 67.166 3.164 0.72 253629. 0.4810 42.84 0.2514 0.5768 0.0622 0.0271 2.860 15.024 14.442 2133.033 1.697 64.237 3.071 0.72 253914. 0.4565 46.41 0.2723 0.6062 0.0592 0.0266 2.808 14.746 13.751 2093.561 1.666 61.165 2.979 0.72 254214. 0.4322 49.98 0.2932 0.6330 0.0561 0.0260 2.743 14.410 13.029 2045.792 1.628 57.953 2.889 0.72 254528. 0.4079 53.56 0.3142 0.6571 0.0528 0.0253 2.668 14.012 12.276 1989.346 1.583 54.602 2.799 0.72 254857. 0.3836 57.13 0.3351 0.6785 0.0495 0.0244 2.580 13.551 11.492 1923.911 1.531 51.115 2.709 0.72 255201. 0.3593 60.70 0.3561 0.6970 0.0460 0.0235 2.480 13.027 10.681 1849.550 1.472 47.507 2.619 0.72 255560. 0.3348 64.27 0.3770 0.7123 0.0424 0.0224 2.369 12.442 9.846 1766.446 1.406 43.794 2.528 0.72 255933. 0.3103 67.84 0.3980 0.7241 0.0387 0.0213 2.246 11.796 8.990 1674.757 1.333 39.987 2.435 0.72 256322. 0.2856 71.41 0.4189 0.7319 0.0349 0.0200 2.112 11.091 8.116 1574.635 1.253 36.101 2.338 0.72 256726. 0.2605 74.98 0.4399 0.7349 0.0311 0.0186 1.966 10.328 7.227 1466.264 1.167 32.147 2.236 0.72 257145. 0.2351 78.55 0.4608 0.7320 0.0272 0.0171 1.810 9.508 6.326 1349.876 1.074 28.139 2.126 0.72 257580. 0.2091 82.12 0.4818 0.7215 0.0233 0.0156 1.644 8.634 5.416 1225.785 0.975 24.090 2.004 0.72 258030. 0.1824 85.69 0.5027 0.7006 0.0194 0.0139 1.468 7.709 4.500 1094.411 0.871 20.017 1.865 0.72 258495. 0.1548 89.26 0.5237 0.6649 0.0154 0.0121 1.282 6.736 3.583 956.301 0.761 15.936 1.699 0.72 258977. 0.1258 92.83 0.5446 0.6064 0.0115 0.0103 1.089 5.721 2.668 812.173 0.646 11.868 1.490 0.72 259474. 0.0952 96.40 0.5655 0.5093 0.0076 0.0084 0.889 4.669 1.762 662.928 0.528 7.835 1.205 0.73 259987. 0.0626 99.97 0.5865 0.3388 0.0037 0.0065 0.683 3.590 0.869 509.635 0.406 3.864 0.773 0.73 260515. 0.0282 103.54 0.6074 -0.0073 -0.0001 0.0045 0.472 2.480 -0.013 352.043 0.280 -0.056 -0.016 0.73 261035. 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 0.0887 0.0278 3.737 18.119 24.191 2786.784 2.047 107.601 3.937 0.77 272282. 0.7575 3.86 0.0209 0.0650 0.0873 0.0281 3.770 18.280 23.803 2811.531 2.065 105.876 3.840 0.77 272440. 0.7329 7.73 0.0418 0.1268 0.0858 0.0283 3.800 18.424 23.385 2833.709 2.082 104.017 3.743 0.77 272610. 0.7081 11.59 0.0628 0.1853 0.0841 0.0285 3.825 18.547 22.936 2852.659 2.095 102.019 3.647 0.77 272793. 0.6832 15.45 0.0837 0.2406 0.0824 0.0286 3.846 18.645 22.454 2867.719 2.107 99.874 3.551 0.77 272988. 0.6583 19.31 0.1046 0.2927 0.0805 0.0287 3.860 18.713 21.937 2878.194 2.114 97.577 3.457 0.77 273197. 0.6334 23.18 0.1255 0.3418 0.0784 0.0288 3.867 18.747 21.385 2883.365 2.118 95.121 3.364 0.77 273419. 0.6085 27.04 0.1464 0.3879 0.0763 0.0288 3.865 18.741 20.796 2882.486 2.117 92.501 3.272 0.77 273655. 0.5837 30.90 0.1673 0.4311 0.0740 0.0287 3.855 18.691 20.169 2874.813 2.112 89.712 3.182 0.77 273905. 0.5590 34.76 0.1883 0.4715 0.0715 0.0286 3.835 18.592 19.504 2859.602 2.101 86.753 3.094 0.77 274170. 0.5344 38.63 0.2092 0.5091 0.0689 0.0283 3.803 18.440 18.799 2836.134 2.083 83.619 3.006 0.78 274450. 0.5099 42.49 0.2301 0.5441 0.0662 0.0280 3.760 18.229 18.055 2803.707 2.059 80.311 2.921 0.78 274745. 0.4855 46.35 0.2510 0.5765 0.0633 0.0276 3.703 17.956 17.273 2761.682 2.029 76.828 2.837 0.78 275055. 0.4612 50.22 0.2719 0.6062 0.0603 0.0271 3.633 17.616 16.451 2709.462 1.990 73.173 2.754 0.78 275380. 0.4369 54.08 0.2929 0.6335 0.0572 0.0264 3.549 17.207 15.591 2646.536 1.944 69.348 2.672 0.78 275722. 0.4127 57.94 0.3138 0.6581 0.0539 0.0257 3.450 16.725 14.693 2572.396 1.890 65.355 2.591 0.78 276078. 0.3885 61.80 0.3347 0.6799 0.0505 0.0248 3.335 16.168 13.758 2486.655 1.827 61.198 2.510 0.78 276451. 0.3641 65.67 0.3556 0.6990 0.0469 0.0239 3.204 15.535 12.791 2389.424 1.755 56.893 2.428 0.78 276840. 0.3397 69.53 0.3765 0.7148 0.0433 0.0228 3.059 14.830 11.794 2280.993 1.676 52.460 2.345 0.78 277245. 0.3151 73.39 0.3974 0.7272 0.0395 0.0216 2.899 14.054 10.772 2161.651 1.588 47.914 2.260 0.78 277666. 0.2902 77.25 0.4184 0.7355 0.0357 0.0203 2.725 13.210 9.728 2031.706 1.492 43.270 2.172 0.78 278104. 0.2650 81.12 0.4393 0.7389 0.0318 0.0189 2.537 12.298 8.665 1891.503 1.389 38.542 2.078 0.78 278558. 0.2393 84.98 0.4602 0.7362 0.0278 0.0174 2.335 11.323 7.587 1741.485 1.279 33.747 1.976 0.78 279028. 0.2129 88.84 0.4811 0.7254 0.0238 0.0158 2.122 10.287 6.497 1582.241 1.162 28.901 1.863 0.78 279515. 0.1857 92.70 0.5020 0.7038 0.0198 0.0141 1.897 9.197 5.401 1414.502 1.039 24.022 1.732 0.78 280019. 0.1574 96.57 0.5229 0.6664 0.0158 0.0124 1.662 8.057 4.301 1239.207 0.910 19.131 1.574 0.78 280540. 0.1277 100.43 0.5439 0.6051 0.0118 0.0106 1.418 6.876 3.204 1057.527 0.777 14.252 1.374 0.79 281078. 0.0962 104.29 0.5648 0.5039 0.0078 0.0087 1.168 5.662 2.116 870.875 0.640 9.412 1.102 0.79 281632. 0.0627 108.16 0.5857 0.3296 0.0038 0.0068 0.913 4.427 1.044 680.865 0.500 4.642 0.695 0.79 282203. 0.0278 112.02 0.6066 -0.0069 -0.0001 0.0049 0.653 3.168 -0.015 487.199 0.358 -0.067 -0.014 0.79 282766. 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 0.0903 0.0299 5.022 22.607 28.556 3744.583 2.554 127.016 3.459 0.83 293187. 0.7230 4.16 0.0209 0.0618 0.0889 0.0301 5.043 22.705 28.109 3760.825 2.565 125.030 3.390 0.83 293359. 0.7031 8.31 0.0418 0.1210 0.0874 0.0302 5.061 22.783 27.627 3773.704 2.574 122.883 3.321 0.83 293543. 0.6827 12.47 0.0627 0.1777 0.0857 0.0303 5.072 22.836 27.107 3782.545 2.580 120.570 3.250 0.83 293741. 0.6620 16.63 0.0836 0.2318 0.0840 0.0303 5.078 22.861 26.547 3786.636 2.583 118.081 3.180 0.83 293953. 0.6409 20.79 0.1045 0.2833 0.0821 0.0303 5.076 22.853 25.946 3785.228 2.582 115.409 3.109 0.83 294179. 0.6195 24.94 0.1254 0.3322 0.0800 0.0302 5.066 22.806 25.303 3777.512 2.577 112.546 3.038 0.83 294420. 0.5978 29.10 0.1463 0.3785 0.0778 0.0301 5.046 22.717 24.615 3762.701 2.567 109.485 2.967 0.83 294676. 0.5758 33.26 0.1672 0.4223 0.0755 0.0299 5.015 22.579 23.881 3739.975 2.551 106.222 2.896 0.83 294947. 0.5536 37.41 0.1881 0.4634 0.0731 0.0297 4.973 22.389 23.101 3708.519 2.530 102.751 2.825 0.83 295234. 0.5312 41.57 0.2090 0.5020 0.0704 0.0293 4.918 22.142 22.273 3667.522 2.502 99.072 2.755 0.83 295537. 0.5085 45.73 0.2300 0.5381 0.0677 0.0289 4.849 21.832 21.399 3616.192 2.467 95.181 2.684 0.84 295856. 0.4857 49.89 0.2509 0.5716 0.0648 0.0284 4.766 21.455 20.477 3553.753 2.424 91.081 2.613 0.84 296192. 0.4626 54.04 0.2718 0.6025 0.0617 0.0278 4.666 21.007 19.508 3479.465 2.373 86.773 2.543 0.84 296544. 0.4394 58.20 0.2927 0.6308 0.0585 0.0271 4.550 20.484 18.494 3392.957 2.314 82.261 2.472 0.84 296912. 0.4159 62.36 0.3136 0.6562 0.0551 0.0263 4.418 19.889 17.434 3294.420 2.247 77.546 2.400 0.84 297298. 0.3920 66.52 0.3345 0.6786 0.0516 0.0255 4.268 19.214 16.329 3182.559 2.171 72.634 2.327 0.84 297701. 0.3679 70.67 0.3554 0.6978 0.0480 0.0245 4.101 18.462 15.185 3057.941 2.086 67.542 2.252 0.84 298121. 0.3433 74.83 0.3763 0.7134 0.0443 0.0234 3.917 17.635 14.005 2920.929 1.992 62.294 2.175 0.84 298558. 0.3184 78.99 0.3972 0.7251 0.0405 0.0222 3.716 16.731 12.794 2771.245 1.890 56.908 2.094 0.84 299012. 0.2930 83.14 0.4181 0.7322 0.0365 0.0209 3.499 15.754 11.557 2609.488 1.780 51.404 2.009 0.84 299484. 0.2671 87.30 0.4390 0.7336 0.0326 0.0195 3.267 14.710 10.296 2436.451 1.662 45.797 1.917 0.84 299974. 0.2406 91.46 0.4599 0.7279 0.0285 0.0180 3.021 13.602 9.017 2252.919 1.537 40.108 1.815 0.84 300481. 0.2132 95.62 0.4808 0.7128 0.0244 0.0165 2.763 12.437 7.723 2060.016 1.405 34.354 1.701 0.84 301005. 0.1849 99.77 0.5017 0.6851 0.0203 0.0149 2.493 11.224 6.420 1859.146 1.268 28.558 1.566 0.84 301548. 0.1553 103.93 0.5226 0.6398 0.0162 0.0132 2.215 9.972 5.114 1651.795 1.127 22.745 1.404 0.84 302109. 0.1242 108.09 0.5435 0.5687 0.0120 0.0115 1.931 8.693 3.810 1439.800 0.982 16.945 1.200 0.85 302688. 0.0916 112.24 0.5644 0.4582 0.0080 0.0098 1.643 7.397 2.516 1225.244 0.836 11.189 0.931 0.85 303285. 0.0578 116.40 0.5853 0.2839 0.0039 0.0081 1.355 6.100 1.239 1010.337 0.689 5.513 0.556 0.85 303899. 0.0242 120.56 0.6062 -0.0061 -0.0001 0.0064 1.065 4.794 -0.020 794.114 0.542 -0.090 -0.012 0.85 304508. 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 0.0918 0.0342 7.046 29.605 33.320 5253.873 3.345 148.209 2.877 0.89 314087. 0.6495 4.47 0.0210 0.0556 0.0904 0.0341 7.038 29.571 32.820 5247.907 3.341 145.985 2.837 0.89 314272. 0.6357 8.94 0.0420 0.1096 0.0889 0.0340 7.022 29.504 32.277 5236.060 3.333 143.568 2.796 0.89 314471. 0.6214 13.41 0.0629 0.1619 0.0873 0.0339 6.997 29.401 31.688 5217.725 3.322 140.950 2.755 0.89 314685. 0.6066 17.88 0.0839 0.2126 0.0855 0.0338 6.963 29.257 31.052 5192.257 3.305 138.121 2.713 0.89 314914. 0.5913 22.35 0.1049 0.2615 0.0837 0.0335 6.918 29.070 30.366 5159.035 3.284 135.070 2.670 0.89 315159. 0.5755 26.82 0.1259 0.3087 0.0816 0.0333 6.863 28.836 29.628 5117.401 3.258 131.787 2.626 0.89 315419. 0.5592 31.29 0.1468 0.3541 0.0794 0.0329 6.795 28.550 28.837 5066.698 3.226 128.267 2.581 0.89 315696. 0.5423 35.76 0.1678 0.3975 0.0771 0.0326 6.713 28.209 27.990 5006.255 3.187 124.501 2.536 0.89 315990. 0.5248 40.22 0.1888 0.4390 0.0746 0.0321 6.618 27.809 27.087 4935.245 3.142 120.483 2.489 0.89 316301. 0.5068 44.69 0.2098 0.4784 0.0720 0.0316 6.508 27.346 26.127 4853.082 3.090 116.212 2.442 0.89 316630. 0.4882 49.16 0.2307 0.5158 0.0692 0.0309 6.382 26.816 25.109 4759.020 3.030 111.687 2.393 0.89 316975. 0.4691 53.63 0.2517 0.5510 0.0662 0.0303 6.239 26.215 24.035 4652.306 2.962 106.907 2.343 0.90 317339. 0.4494 58.10 0.2727 0.5838 0.0631 0.0295 6.078 25.538 22.903 4532.220 2.885 101.875 2.292 0.90 317720. 0.4291 62.57 0.2937 0.6143 0.0598 0.0286 5.898 24.783 21.717 4398.094 2.800 96.595 2.240 0.90 318120. 0.4083 67.04 0.3146 0.6421 0.0564 0.0276 5.701 23.954 20.475 4251.024 2.706 91.072 2.185 0.90 318538. 0.3867 71.51 0.3356 0.6661 0.0528 0.0266 5.491 23.072 19.179 4094.477 2.607 85.309 2.125 0.90 318973. 0.3640 75.98 0.3566 0.6865 0.0491 0.0255 5.264 22.118 17.835 3925.193 2.499 79.330 2.061 0.90 319428. 0.3405 80.45 0.3776 0.7021 0.0453 0.0244 5.025 21.116 16.448 3747.489 2.386 73.162 1.991 0.90 319900. 0.3158 84.92 0.3986 0.7110 0.0414 0.0232 4.785 20.104 15.023 3567.845 2.271 66.823 1.910 0.90 320392. 0.2896 89.39 0.4195 0.7136 0.0374 0.0220 4.531 19.039 13.566 3378.896 2.151 60.340 1.821 0.90 320902. 0.2624 93.86 0.4405 0.7091 0.0333 0.0207 4.264 17.917 12.081 3179.767 2.024 53.736 1.723 0.90 321430. 0.2343 98.33 0.4615 0.6956 0.0291 0.0193 3.986 16.747 10.574 2972.045 1.892 47.034 1.614 0.90 321978. 0.2053 102.80 0.4825 0.6710 0.0249 0.0179 3.697 15.536 9.051 2757.213 1.755 40.258 1.489 0.90 322545. 0.1752 107.27 0.5034 0.6319 0.0207 0.0165 3.403 14.298 7.517 2537.416 1.615 33.437 1.344 0.90 323131. 0.1441 111.73 0.5244 0.5739 0.0165 0.0151 3.105 13.046 5.981 2315.222 1.474 26.602 1.172 0.90 323736. 0.1121 116.20 0.5454 0.4912 0.0123 0.0136 2.806 11.792 4.449 2092.777 1.332 19.789 0.964 0.91 324360. 0.0796 120.67 0.5664 0.3757 0.0081 0.0122 2.511 10.553 2.932 1872.733 1.192 13.044 0.710 0.91 325004. 0.0476 125.14 0.5873 0.2163 0.0040 0.0108 2.223 9.340 1.441 1657.507 1.055 6.409 0.394 0.91 325667. 0.0185 129.61 0.6083 -0.0055 -0.0001 0.0094 1.934 8.127 -0.031 1442.222 0.918 -0.137 -0.010 0.91 326332. 0.0000 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 0.0921 0.0397 9.941 39.160 38.052 7412.901 4.424 169.256 2.328 0.95 335012. 0.5618 4.88 0.0215 0.0492 0.0909 0.0396 9.924 39.094 37.529 7400.416 4.417 166.931 2.300 0.95 335210. 0.5512 9.76 0.0429 0.0972 0.0895 0.0395 9.891 38.964 36.953 7375.787 4.402 164.368 2.272 0.95 335425. 0.5404 14.64 0.0644 0.1441 0.0879 0.0393 9.840 38.763 36.320 7337.801 4.379 161.553 2.245 0.95 335657. 0.5293 19.52 0.0859 0.1898 0.0863 0.0390 9.770 38.486 35.628 7285.393 4.348 158.471 2.218 0.95 335906. 0.5179 24.40 0.1073 0.2344 0.0844 0.0387 9.679 38.129 34.871 7217.716 4.308 155.107 2.191 0.95 336173. 0.5062 29.28 0.1288 0.2778 0.0824 0.0382 9.567 37.687 34.048 7134.085 4.258 151.446 2.165 0.95 336459. 0.4941 34.16 0.1503 0.3201 0.0803 0.0377 9.433 37.158 33.156 7034.016 4.198 147.478 2.138 0.95 336764. 0.4816 39.03 0.1718 0.3612 0.0779 0.0371 9.276 36.541 32.193 6917.127 4.128 143.194 2.111 0.95 337088. 0.4685 43.91 0.1932 0.4011 0.0754 0.0363 9.096 35.833 31.157 6783.088 4.048 138.587 2.083 0.95 337431. 0.4549 48.79 0.2147 0.4396 0.0728 0.0355 8.893 35.033 30.048 6631.629 3.958 133.652 2.055 0.95 337794. 0.4407 53.67 0.2362 0.4767 0.0699 0.0346 8.666 34.139 28.864 6462.490 3.857 128.388 2.026 0.95 338178. 0.4258 58.55 0.2576 0.5122 0.0668 0.0336 8.416 33.152 27.607 6275.581 3.745 122.796 1.995 0.96 338581. 0.4101 63.43 0.2791 0.5459 0.0636 0.0325 8.141 32.071 26.278 6070.919 3.623 116.883 1.963 0.96 339005. 0.3937 68.31 0.3006 0.5778 0.0602 0.0313 7.843 30.896 24.878 5848.557 3.491 110.655 1.929 0.96 339449. 0.3764 73.19 0.3220 0.6074 0.0567 0.0300 7.521 29.627 23.408 5608.304 3.347 104.120 1.893 0.96 339914. 0.3583 78.07 0.3435 0.6335 0.0530 0.0287 7.187 28.313 21.872 5359.604 3.199 97.289 1.851 0.96 340398. 0.3386 82.95 0.3650 0.6547 0.0491 0.0274 6.850 26.986 20.277 5108.373 3.049 90.192 1.800 0.96 340904. 0.3171 87.83 0.3864 0.6710 0.0451 0.0260 6.502 25.615 18.630 4848.909 2.894 82.868 1.743 0.96 341430. 0.2942 92.71 0.4079 0.6765 0.0410 0.0247 6.188 24.378 16.935 4614.650 2.754 75.329 1.665 0.96 341977. 0.2680 97.59 0.4294 0.6686 0.0368 0.0236 5.915 23.300 15.198 4410.654 2.632 67.601 1.563 0.96 342544. 0.2383 102.47 0.4509 0.6516 0.0325 0.0225 5.632 22.186 13.431 4199.879 2.507 59.741 1.450 0.96 343133. 0.2079 107.35 0.4723 0.6233 0.0282 0.0214 5.346 21.060 11.642 3986.632 2.379 51.784 1.325 0.96 343742. 0.1768 112.22 0.4938 0.5821 0.0238 0.0202 5.059 19.929 9.840 3772.521 2.252 43.770 1.183 0.96 344373. 0.1452 117.10 0.5153 0.5257 0.0195 0.0191 4.774 18.804 8.036 3559.633 2.124 35.744 1.024 0.96 345025. 0.1135 121.98 0.5367 0.4518 0.0151 0.0180 4.493 17.699 6.241 3350.419 2.000 27.759 0.845 0.97 345698. 0.0826 126.86 0.5582 0.3581 0.0108 0.0169 4.221 16.627 4.468 3147.554 1.879 19.873 0.644 0.97 346394. 0.0532 131.74 0.5797 0.2424 0.0066 0.0158 3.959 15.596 2.731 2952.310 1.762 12.149 0.420 0.97 347112. 0.0271 136.62 0.6011 0.1022 0.0025 0.0148 3.706 14.599 1.040 2763.626 1.649 4.626 0.171 0.97 347856. 0.0068 141.50 0.6226