20x10E (20x10E.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 0.0824 0.0303 0.008 0.491 0.420 5.814 0.056 1.869 32.782 0.08 36690. 0.6235 0.42 0.0222 0.0588 0.0810 0.0306 0.008 0.496 0.413 5.869 0.056 1.838 31.929 0.08 36711. 0.6021 0.84 0.0444 0.1145 0.0795 0.0308 0.008 0.500 0.406 5.919 0.057 1.804 31.079 0.08 36734. 0.5807 1.26 0.0666 0.1671 0.0779 0.0311 0.008 0.504 0.397 5.962 0.057 1.768 30.235 0.08 36759. 0.5592 1.68 0.0887 0.2166 0.0762 0.0312 0.008 0.507 0.389 5.998 0.057 1.729 29.397 0.08 36786. 0.5377 2.10 0.1109 0.2631 0.0744 0.0314 0.008 0.509 0.380 6.026 0.058 1.688 28.566 0.08 36814. 0.5163 2.52 0.1331 0.3066 0.0725 0.0315 0.008 0.511 0.370 6.043 0.058 1.644 27.743 0.08 36845. 0.4949 2.94 0.1553 0.3472 0.0704 0.0315 0.008 0.511 0.359 6.049 0.058 1.598 26.928 0.08 36877. 0.4735 3.36 0.1775 0.3849 0.0683 0.0315 0.008 0.511 0.348 6.043 0.058 1.548 26.121 0.08 36912. 0.4521 3.78 0.1997 0.4198 0.0659 0.0314 0.008 0.509 0.336 6.023 0.058 1.496 25.322 0.08 36949. 0.4308 4.20 0.2218 0.4518 0.0635 0.0312 0.008 0.506 0.324 5.988 0.057 1.440 24.528 0.08 36988. 0.4095 4.62 0.2440 0.4810 0.0609 0.0309 0.008 0.502 0.311 5.936 0.057 1.382 23.738 0.08 37030. 0.3882 5.04 0.2662 0.5073 0.0582 0.0305 0.008 0.496 0.297 5.866 0.056 1.320 22.951 0.08 37074. 0.3668 5.46 0.2884 0.5307 0.0554 0.0301 0.008 0.488 0.282 5.778 0.055 1.256 22.162 0.08 37120. 0.3455 5.88 0.3106 0.5511 0.0524 0.0295 0.008 0.479 0.267 5.671 0.054 1.188 21.369 0.08 37168. 0.3241 6.30 0.3328 0.5683 0.0493 0.0289 0.007 0.469 0.251 5.545 0.053 1.118 20.568 0.08 37219. 0.3026 6.72 0.3550 0.5821 0.0461 0.0281 0.007 0.456 0.235 5.401 0.052 1.046 19.752 0.08 37272. 0.2810 7.14 0.3771 0.5923 0.0428 0.0273 0.007 0.443 0.218 5.238 0.050 0.972 18.915 0.08 37328. 0.2594 7.56 0.3993 0.5985 0.0395 0.0263 0.007 0.427 0.201 5.058 0.048 0.895 18.050 0.08 37386. 0.2376 7.98 0.4215 0.6002 0.0360 0.0253 0.007 0.411 0.184 4.859 0.046 0.817 17.149 0.08 37447. 0.2156 8.40 0.4437 0.5968 0.0325 0.0242 0.006 0.392 0.166 4.643 0.044 0.738 16.199 0.08 37510. 0.1935 8.82 0.4659 0.5874 0.0290 0.0230 0.006 0.373 0.148 4.410 0.042 0.657 15.186 0.08 37576. 0.1712 9.24 0.4881 0.5711 0.0253 0.0217 0.006 0.352 0.129 4.160 0.040 0.575 14.093 0.08 37644. 0.1486 9.66 0.5102 0.5462 0.0217 0.0203 0.005 0.329 0.111 3.894 0.037 0.492 12.893 0.08 37715. 0.1258 10.08 0.5324 0.5108 0.0180 0.0188 0.005 0.305 0.092 3.613 0.034 0.409 11.555 0.08 37788. 0.1028 10.50 0.5546 0.4619 0.0144 0.0173 0.004 0.280 0.073 3.317 0.032 0.326 10.032 0.08 37864. 0.0797 10.92 0.5768 0.3954 0.0107 0.0157 0.004 0.254 0.055 3.008 0.029 0.244 8.255 0.08 37943. 0.0567 11.34 0.5990 0.3047 0.0071 0.0140 0.004 0.227 0.036 2.688 0.026 0.161 6.126 0.08 38024. 0.0342 11.76 0.6212 0.1797 0.0036 0.0123 0.003 0.199 0.018 2.358 0.023 0.081 3.485 0.08 38107. 0.0138 12.18 0.6434 0.0031 0.0001 0.0105 0.003 0.171 0.000 2.020 0.019 0.001 0.059 0.08 38192. 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 0.0828 0.0280 0.058 1.817 1.688 42.995 0.205 7.507 17.805 0.16 73378. 0.6786 0.84 0.0223 0.0641 0.0814 0.0283 0.058 1.838 1.659 43.480 0.208 7.381 17.310 0.16 73421. 0.6542 1.69 0.0446 0.1246 0.0799 0.0286 0.059 1.856 1.629 43.926 0.210 7.246 16.820 0.16 73468. 0.6298 2.53 0.0669 0.1815 0.0783 0.0289 0.059 1.873 1.596 44.320 0.212 7.100 16.337 0.16 73518. 0.6056 3.38 0.0892 0.2349 0.0766 0.0291 0.060 1.887 1.561 44.655 0.213 6.945 15.860 0.16 73571. 0.5814 4.22 0.1115 0.2849 0.0747 0.0292 0.060 1.898 1.524 44.918 0.214 6.779 15.390 0.16 73629. 0.5574 5.07 0.1338 0.3317 0.0728 0.0294 0.060 1.906 1.484 45.100 0.215 6.603 14.929 0.16 73691. 0.5336 5.91 0.1561 0.3752 0.0707 0.0294 0.061 1.910 1.442 45.188 0.216 6.415 14.476 0.16 73757. 0.5100 6.76 0.1784 0.4156 0.0685 0.0294 0.061 1.909 1.397 45.173 0.216 6.215 14.030 0.16 73827. 0.4866 7.60 0.2007 0.4530 0.0662 0.0293 0.060 1.904 1.350 45.043 0.215 6.004 13.592 0.16 73901. 0.4633 8.45 0.2230 0.4874 0.0637 0.0292 0.060 1.893 1.300 44.786 0.214 5.781 13.162 0.16 73980. 0.4402 9.29 0.2453 0.5188 0.0611 0.0289 0.060 1.876 1.247 44.391 0.212 5.545 12.737 0.16 74064. 0.4172 10.14 0.2676 0.5474 0.0584 0.0285 0.059 1.853 1.191 43.845 0.209 5.296 12.318 0.16 74152. 0.3944 10.98 0.2899 0.5730 0.0555 0.0281 0.058 1.823 1.132 43.142 0.206 5.036 11.903 0.16 74245. 0.3716 11.83 0.3122 0.5956 0.0525 0.0275 0.057 1.787 1.071 42.280 0.202 4.764 11.490 0.16 74343. 0.3489 12.67 0.3345 0.6152 0.0494 0.0269 0.055 1.744 1.008 41.258 0.197 4.482 11.077 0.16 74446. 0.3262 13.51 0.3568 0.6316 0.0462 0.0261 0.054 1.694 0.942 40.078 0.191 4.190 10.660 0.16 74554. 0.3035 14.36 0.3791 0.6445 0.0429 0.0252 0.052 1.637 0.874 38.740 0.185 3.890 10.238 0.16 74666. 0.2809 15.20 0.4014 0.6536 0.0395 0.0242 0.050 1.574 0.805 37.244 0.178 3.582 9.806 0.16 74784. 0.2582 16.05 0.4237 0.6585 0.0360 0.0232 0.048 1.504 0.734 35.594 0.170 3.267 9.360 0.16 74906. 0.2353 16.89 0.4460 0.6585 0.0325 0.0220 0.045 1.428 0.662 33.789 0.161 2.946 8.892 0.16 75034. 0.2123 17.74 0.4683 0.6529 0.0289 0.0207 0.043 1.345 0.589 31.834 0.152 2.621 8.396 0.16 75166. 0.1891 18.58 0.4906 0.6404 0.0253 0.0194 0.040 1.257 0.515 29.733 0.142 2.292 7.861 0.16 75304. 0.1656 19.43 0.5129 0.6193 0.0216 0.0179 0.037 1.162 0.441 27.491 0.131 1.960 7.272 0.16 75447. 0.1416 20.27 0.5352 0.5872 0.0179 0.0163 0.034 1.061 0.366 25.115 0.120 1.627 6.608 0.16 75595. 0.1173 21.12 0.5575 0.5403 0.0143 0.0147 0.030 0.956 0.291 22.614 0.108 1.294 5.837 0.16 75748. 0.0924 21.96 0.5798 0.4727 0.0106 0.0130 0.027 0.845 0.217 19.999 0.095 0.963 4.910 0.16 75907. 0.0670 22.81 0.6021 0.3745 0.0070 0.0113 0.023 0.730 0.143 17.283 0.083 0.635 3.746 0.16 76070. 0.0415 23.65 0.6244 0.2277 0.0034 0.0094 0.019 0.612 0.070 14.483 0.069 0.312 2.196 0.16 76239. 0.0171 24.49 0.6467 -0.0050 -0.0001 0.0076 0.016 0.490 -0.001 11.605 0.055 -0.005 -0.047 0.16 76409. 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 0.0831 0.0271 0.188 3.956 3.816 140.398 0.447 16.971 12.326 0.24 110064. 0.7064 1.28 0.0226 0.0673 0.0817 0.0274 0.191 4.004 3.751 142.127 0.452 16.684 11.971 0.24 110130. 0.6802 2.56 0.0451 0.1306 0.0802 0.0277 0.193 4.049 3.682 143.717 0.457 16.376 11.619 0.24 110201. 0.6541 3.84 0.0677 0.1900 0.0786 0.0280 0.195 4.089 3.607 145.131 0.462 16.045 11.273 0.24 110277. 0.6281 5.13 0.0902 0.2457 0.0769 0.0282 0.196 4.123 3.527 146.333 0.466 15.690 10.933 0.24 110359. 0.6024 6.41 0.1128 0.2978 0.0750 0.0284 0.198 4.150 3.442 147.286 0.469 15.311 10.600 0.24 110447. 0.5770 7.69 0.1353 0.3464 0.0730 0.0285 0.198 4.168 3.351 147.951 0.471 14.906 10.274 0.24 110541. 0.5518 8.97 0.1579 0.3915 0.0709 0.0286 0.199 4.178 3.254 148.287 0.472 14.476 9.954 0.24 110641. 0.5268 10.25 0.1805 0.4334 0.0687 0.0286 0.199 4.177 3.152 148.257 0.472 14.018 9.642 0.24 110748. 0.5022 11.53 0.2030 0.4721 0.0663 0.0285 0.198 4.165 3.043 147.818 0.471 13.533 9.336 0.24 110862. 0.4778 12.82 0.2256 0.5077 0.0638 0.0283 0.197 4.140 2.927 146.931 0.468 13.020 9.036 0.24 110983. 0.4536 14.10 0.2481 0.5403 0.0611 0.0281 0.195 4.101 2.805 145.551 0.463 12.479 8.742 0.24 111111. 0.4296 15.38 0.2707 0.5700 0.0583 0.0277 0.193 4.047 2.677 143.636 0.457 11.908 8.454 0.24 111246. 0.4058 16.66 0.2932 0.5967 0.0554 0.0272 0.189 3.977 2.542 141.163 0.449 11.308 8.169 0.24 111389. 0.3821 17.94 0.3158 0.6204 0.0523 0.0266 0.185 3.892 2.402 138.125 0.440 10.683 7.887 0.24 111539. 0.3586 19.22 0.3384 0.6411 0.0492 0.0259 0.180 3.790 2.256 134.521 0.428 10.035 7.607 0.24 111696. 0.3352 20.51 0.3609 0.6586 0.0459 0.0251 0.175 3.673 2.105 130.352 0.415 9.364 7.326 0.24 111861. 0.3118 21.79 0.3835 0.6726 0.0425 0.0242 0.168 3.539 1.950 125.618 0.400 8.675 7.042 0.24 112033. 0.2885 23.07 0.4060 0.6829 0.0390 0.0232 0.161 3.390 1.791 120.324 0.383 7.968 6.753 0.24 112213. 0.2651 24.35 0.4286 0.6891 0.0355 0.0221 0.154 3.225 1.629 114.473 0.364 7.246 6.455 0.24 112400. 0.2417 25.63 0.4511 0.6904 0.0319 0.0208 0.145 3.045 1.464 108.074 0.344 6.511 6.143 0.24 112596. 0.2181 26.91 0.4737 0.6859 0.0282 0.0195 0.136 2.849 1.296 101.138 0.322 5.766 5.813 0.24 112799. 0.1942 28.20 0.4963 0.6744 0.0246 0.0181 0.126 2.639 1.127 93.680 0.298 5.012 5.456 0.24 113010. 0.1699 29.48 0.5188 0.6540 0.0208 0.0165 0.115 2.415 0.956 85.720 0.273 4.254 5.060 0.24 113229. 0.1452 30.76 0.5414 0.6215 0.0171 0.0149 0.104 2.177 0.785 77.286 0.246 3.493 4.609 0.24 113456. 0.1198 32.04 0.5639 0.5724 0.0134 0.0132 0.092 1.927 0.615 68.412 0.218 2.734 4.075 0.24 113690. 0.0937 33.32 0.5865 0.4986 0.0097 0.0114 0.079 1.666 0.445 59.140 0.188 1.979 3.413 0.24 113933. 0.0668 34.60 0.6090 0.3855 0.0060 0.0096 0.066 1.395 0.277 49.524 0.158 1.234 2.541 0.24 114184. 0.0393 35.89 0.6316 0.2032 0.0025 0.0076 0.053 1.116 0.113 39.621 0.126 0.502 1.292 0.24 114442. 0.0127 37.17 0.6542 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 0.0837 0.0267 0.439 6.923 6.825 327.652 0.782 30.357 9.448 0.32 146747. 0.7241 1.69 0.0223 0.0680 0.0823 0.0270 0.445 7.012 6.711 331.826 0.792 29.852 9.174 0.32 146834. 0.6972 3.38 0.0447 0.1321 0.0808 0.0273 0.450 7.093 6.589 335.675 0.801 29.309 8.904 0.32 146927. 0.6705 5.07 0.0670 0.1922 0.0792 0.0276 0.455 7.166 6.458 339.112 0.810 28.726 8.638 0.32 147028. 0.6440 6.77 0.0893 0.2485 0.0774 0.0278 0.459 7.228 6.318 342.055 0.817 28.102 8.378 0.32 147136. 0.6178 8.46 0.1116 0.3012 0.0756 0.0280 0.462 7.278 6.168 344.414 0.822 27.436 8.123 0.32 147252. 0.5919 10.15 0.1340 0.3503 0.0736 0.0282 0.464 7.313 6.008 346.099 0.826 26.724 7.874 0.32 147376. 0.5662 11.84 0.1563 0.3961 0.0716 0.0282 0.465 7.333 5.838 347.017 0.828 25.967 7.630 0.32 147508. 0.5409 13.53 0.1786 0.4386 0.0693 0.0282 0.465 7.334 5.657 347.074 0.829 25.162 7.393 0.32 147649. 0.5159 15.22 0.2010 0.4779 0.0670 0.0282 0.464 7.315 5.465 346.177 0.826 24.310 7.161 0.32 147799. 0.4911 16.92 0.2233 0.5142 0.0645 0.0280 0.462 7.274 5.263 344.230 0.822 23.408 6.934 0.32 147958. 0.4667 18.61 0.2456 0.5475 0.0619 0.0278 0.457 7.208 5.048 341.131 0.814 22.455 6.712 0.32 148126. 0.4425 20.30 0.2679 0.5780 0.0591 0.0274 0.452 7.116 4.823 336.777 0.804 21.451 6.495 0.32 148304. 0.4185 21.99 0.2903 0.6056 0.0562 0.0269 0.444 6.996 4.586 331.104 0.790 20.397 6.282 0.32 148491. 0.3946 23.68 0.3126 0.6303 0.0532 0.0264 0.435 6.848 4.338 324.093 0.774 19.296 6.071 0.32 148687. 0.3710 25.37 0.3349 0.6522 0.0500 0.0257 0.423 6.672 4.081 315.738 0.754 18.154 5.863 0.32 148894. 0.3475 27.07 0.3573 0.6710 0.0468 0.0249 0.410 6.467 3.816 306.036 0.731 16.973 5.655 0.32 149110. 0.3241 28.76 0.3796 0.6867 0.0434 0.0240 0.396 6.233 3.543 294.992 0.704 15.757 5.447 0.32 149336. 0.3008 30.45 0.4019 0.6989 0.0400 0.0230 0.379 5.972 3.262 282.608 0.675 14.510 5.236 0.32 149572. 0.2774 32.14 0.4242 0.7072 0.0365 0.0219 0.361 5.682 2.976 268.897 0.642 13.236 5.019 0.32 149818. 0.2540 33.83 0.4466 0.7112 0.0329 0.0207 0.340 5.364 2.684 253.872 0.606 11.939 4.795 0.32 150074. 0.2305 35.52 0.4689 0.7101 0.0293 0.0193 0.319 5.020 2.388 237.559 0.567 10.622 4.559 0.32 150340. 0.2067 37.21 0.4912 0.7026 0.0256 0.0179 0.295 4.649 2.089 219.990 0.525 9.290 4.306 0.32 150616. 0.1826 38.91 0.5136 0.6871 0.0219 0.0164 0.270 4.252 1.787 201.212 0.480 7.949 4.028 0.32 150903. 0.1580 40.60 0.5359 0.6609 0.0182 0.0148 0.243 3.831 1.484 181.282 0.433 6.602 3.713 0.32 151200. 0.1327 42.29 0.5582 0.6199 0.0145 0.0130 0.215 3.387 1.182 160.280 0.383 5.256 3.344 0.32 151507. 0.1066 43.98 0.5805 0.5568 0.0108 0.0113 0.185 2.922 0.881 138.300 0.330 3.917 2.888 0.32 151825. 0.0795 45.67 0.6029 0.4583 0.0071 0.0094 0.155 2.440 0.583 115.462 0.276 2.592 2.289 0.32 152153. 0.0513 47.36 0.6252 0.2968 0.0036 0.0075 0.123 1.942 0.290 91.903 0.219 1.288 1.430 0.32 152490. 0.0226 49.06 0.6475 0.0025 0.0000 0.0055 0.091 1.430 0.002 67.654 0.162 0.008 0.012 0.32 152830. 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 0.0843 0.0265 0.853 10.758 10.748 636.388 1.215 47.805 7.660 0.40 183425. 0.7367 2.11 0.0223 0.0689 0.0829 0.0269 0.865 10.899 10.570 644.728 1.231 47.015 7.436 0.40 183534. 0.7093 4.23 0.0447 0.1338 0.0814 0.0272 0.875 11.029 10.379 652.421 1.246 46.165 7.216 0.40 183651. 0.6820 6.34 0.0670 0.1946 0.0798 0.0275 0.884 11.145 10.174 659.299 1.259 45.253 6.999 0.40 183777. 0.6550 8.46 0.0893 0.2517 0.0781 0.0277 0.892 11.245 9.954 665.195 1.270 44.275 6.787 0.40 183913. 0.6282 10.57 0.1116 0.3050 0.0762 0.0279 0.898 11.325 9.719 669.933 1.279 43.230 6.580 0.40 184058. 0.6018 12.69 0.1340 0.3547 0.0743 0.0281 0.903 11.382 9.468 673.331 1.286 42.114 6.378 0.40 184214. 0.5758 14.80 0.1563 0.4010 0.0722 0.0281 0.905 11.414 9.201 675.205 1.290 40.925 6.181 0.40 184380. 0.5500 16.92 0.1786 0.4441 0.0699 0.0281 0.906 11.417 8.917 675.369 1.290 39.661 5.988 0.40 184556. 0.5246 19.03 0.2010 0.4839 0.0676 0.0281 0.903 11.387 8.615 673.635 1.287 38.321 5.801 0.40 184744. 0.4995 21.14 0.2233 0.5208 0.0651 0.0279 0.898 11.323 8.296 669.815 1.279 36.903 5.618 0.40 184943. 0.4747 23.26 0.2456 0.5547 0.0624 0.0277 0.890 11.220 7.960 663.705 1.268 35.404 5.440 0.40 185154. 0.4502 25.37 0.2679 0.5857 0.0597 0.0273 0.879 11.074 7.604 655.100 1.251 33.824 5.265 0.40 185376. 0.4260 27.49 0.2903 0.6139 0.0567 0.0268 0.863 10.884 7.231 643.870 1.230 32.165 5.094 0.40 185610. 0.4019 29.60 0.3126 0.6393 0.0537 0.0262 0.845 10.649 6.842 629.970 1.203 30.432 4.926 0.40 185856. 0.3780 31.72 0.3349 0.6618 0.0505 0.0256 0.823 10.369 6.437 613.388 1.171 28.632 4.760 0.40 186115. 0.3543 33.83 0.3573 0.6815 0.0472 0.0248 0.797 10.043 6.019 594.119 1.135 26.771 4.595 0.40 186385. 0.3307 35.95 0.3796 0.6980 0.0438 0.0238 0.767 9.672 5.588 572.166 1.093 24.855 4.430 0.40 186668. 0.3072 38.06 0.4019 0.7113 0.0404 0.0228 0.734 9.256 5.146 547.539 1.046 22.889 4.263 0.40 186963. 0.2837 40.17 0.4242 0.7208 0.0368 0.0217 0.698 8.795 4.694 520.257 0.994 20.881 4.093 0.40 187271. 0.2602 42.29 0.4466 0.7262 0.0332 0.0204 0.658 8.289 4.234 490.350 0.937 18.835 3.917 0.40 187591. 0.2365 44.40 0.4689 0.7265 0.0296 0.0191 0.614 7.740 3.768 457.866 0.874 16.758 3.732 0.40 187924. 0.2125 46.52 0.4912 0.7208 0.0259 0.0176 0.567 7.148 3.295 422.871 0.808 14.658 3.535 0.40 188270. 0.1882 48.63 0.5136 0.7074 0.0221 0.0161 0.517 6.516 2.820 385.454 0.736 12.541 3.318 0.40 188628. 0.1634 50.75 0.5359 0.6835 0.0184 0.0144 0.464 5.845 2.342 345.737 0.660 10.417 3.072 0.40 188999. 0.1379 52.86 0.5582 0.6449 0.0146 0.0127 0.407 5.137 1.864 303.873 0.580 8.293 2.783 0.40 189383. 0.1115 54.98 0.5805 0.5841 0.0109 0.0108 0.349 4.396 1.390 260.055 0.497 6.181 2.424 0.40 189781. 0.0838 57.09 0.6029 0.4867 0.0072 0.0089 0.288 3.626 0.920 214.524 0.410 4.091 1.945 0.40 190191. 0.0547 59.20 0.6252 0.3216 0.0036 0.0070 0.225 2.832 0.458 167.557 0.320 2.036 1.239 0.40 190613. 0.0246 61.32 0.6475 0.0035 0.0000 0.0050 0.160 2.015 0.003 119.187 0.228 0.015 0.013 0.41 191036. 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 0.0851 0.0266 1.477 15.517 15.627 1101.501 1.753 69.510 6.435 0.48 220097. 0.7463 2.54 0.0223 0.0695 0.0837 0.0269 1.497 15.724 15.371 1116.232 1.777 68.372 6.246 0.48 220228. 0.7184 5.08 0.0447 0.1349 0.0822 0.0272 1.515 15.916 15.096 1129.822 1.798 67.146 6.060 0.48 220369. 0.6908 7.62 0.0670 0.1963 0.0806 0.0275 1.531 16.087 14.799 1141.972 1.818 65.828 5.878 0.48 220521. 0.6634 10.15 0.0894 0.2537 0.0789 0.0278 1.545 16.234 14.482 1152.385 1.834 64.414 5.700 0.48 220684. 0.6364 12.69 0.1117 0.3075 0.0770 0.0280 1.557 16.352 14.141 1160.751 1.847 62.901 5.526 0.48 220860. 0.6096 15.23 0.1340 0.3577 0.0751 0.0281 1.565 16.436 13.778 1166.750 1.857 61.284 5.356 0.48 221047. 0.5833 17.77 0.1564 0.4044 0.0729 0.0282 1.569 16.483 13.390 1170.055 1.862 59.560 5.191 0.48 221247. 0.5573 20.31 0.1787 0.4478 0.0707 0.0282 1.569 16.487 12.978 1170.337 1.863 57.727 5.030 0.48 221460. 0.5316 22.85 0.2011 0.4881 0.0683 0.0281 1.565 16.443 12.541 1167.266 1.858 55.781 4.873 0.48 221686. 0.5063 25.39 0.2234 0.5254 0.0658 0.0280 1.556 16.348 12.078 1160.513 1.847 53.721 4.720 0.48 221926. 0.4813 27.93 0.2457 0.5597 0.0631 0.0277 1.542 16.196 11.588 1149.720 1.830 51.544 4.572 0.48 222179. 0.4566 30.46 0.2681 0.5911 0.0603 0.0274 1.521 15.982 11.071 1134.524 1.806 49.246 4.426 0.48 222447. 0.4321 33.00 0.2904 0.6198 0.0574 0.0269 1.495 15.703 10.529 1114.689 1.774 46.832 4.284 0.48 222729. 0.4078 35.54 0.3128 0.6458 0.0543 0.0263 1.462 15.357 9.962 1090.130 1.735 44.309 4.145 0.48 223025. 0.3838 38.08 0.3351 0.6690 0.0511 0.0256 1.423 14.944 9.372 1060.825 1.688 41.688 4.007 0.48 223336. 0.3599 40.62 0.3574 0.6893 0.0477 0.0248 1.377 14.464 8.763 1026.766 1.634 38.977 3.871 0.48 223662. 0.3362 43.16 0.3798 0.7066 0.0443 0.0238 1.325 13.917 8.135 987.958 1.572 36.184 3.735 0.48 224002. 0.3125 45.70 0.4021 0.7207 0.0408 0.0228 1.266 13.304 7.491 944.418 1.503 33.319 3.598 0.48 224357. 0.2889 48.23 0.4245 0.7312 0.0372 0.0216 1.202 12.625 6.832 896.179 1.426 30.390 3.458 0.48 224727. 0.2652 50.77 0.4468 0.7377 0.0336 0.0203 1.131 11.880 6.161 843.296 1.342 27.406 3.314 0.48 225112. 0.2413 53.31 0.4691 0.7393 0.0299 0.0189 1.054 11.070 5.481 785.851 1.251 24.377 3.163 0.48 225512. 0.2173 55.85 0.4915 0.7350 0.0261 0.0175 0.971 10.199 4.792 723.963 1.152 21.313 3.002 0.48 225927. 0.1928 58.39 0.5138 0.7232 0.0223 0.0159 0.882 9.266 4.097 657.792 1.047 18.225 2.825 0.48 226358. 0.1678 60.93 0.5362 0.7012 0.0185 0.0142 0.788 8.277 3.400 587.553 0.935 15.125 2.625 0.48 226804. 0.1420 63.47 0.5585 0.6645 0.0147 0.0124 0.689 7.234 2.704 513.520 0.817 12.027 2.388 0.48 227266. 0.1152 66.01 0.5808 0.6053 0.0110 0.0105 0.585 6.143 2.011 436.040 0.694 8.945 2.092 0.48 227743. 0.0870 68.54 0.6032 0.5082 0.0072 0.0086 0.477 5.009 1.326 355.540 0.566 5.896 1.691 0.48 228236. 0.0571 71.08 0.6255 0.3379 0.0035 0.0066 0.365 3.839 0.651 272.520 0.434 2.898 1.084 0.49 228743. 0.0257 73.62 0.6479 -0.0096 -0.0001 0.0045 0.251 2.633 -0.012 186.891 0.297 -0.054 -0.030 0.49 229247. 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 0.0862 0.0268 2.364 21.286 21.524 1762.842 2.405 95.740 5.538 0.56 256760. 0.7538 2.96 0.0223 0.0697 0.0848 0.0271 2.396 21.574 21.177 1786.736 2.437 94.194 5.376 0.56 256913. 0.7258 5.91 0.0446 0.1352 0.0833 0.0275 2.426 21.840 20.802 1808.773 2.468 92.525 5.216 0.56 257078. 0.6980 8.87 0.0669 0.1968 0.0816 0.0278 2.452 22.078 20.398 1828.469 2.494 90.730 5.060 0.56 257256. 0.6705 11.83 0.0892 0.2544 0.0799 0.0280 2.475 22.282 19.965 1845.346 2.517 88.803 4.907 0.56 257447. 0.6433 14.78 0.1115 0.3084 0.0780 0.0282 2.493 22.446 19.500 1858.898 2.536 86.737 4.758 0.56 257652. 0.6164 17.74 0.1338 0.3588 0.0761 0.0284 2.506 22.563 19.004 1868.608 2.549 84.528 4.613 0.56 257871. 0.5899 20.70 0.1561 0.4057 0.0739 0.0285 2.513 22.627 18.474 1873.949 2.556 82.170 4.471 0.56 258105. 0.5638 23.66 0.1784 0.4494 0.0717 0.0285 2.514 22.633 17.909 1874.389 2.557 79.660 4.334 0.56 258354. 0.5381 26.61 0.2007 0.4900 0.0693 0.0284 2.507 22.572 17.310 1869.398 2.550 76.995 4.200 0.56 258618. 0.5126 29.57 0.2230 0.5276 0.0667 0.0282 2.492 22.440 16.675 1858.441 2.535 74.170 4.070 0.56 258898. 0.4876 32.53 0.2453 0.5622 0.0641 0.0280 2.469 22.229 16.003 1840.957 2.511 71.183 3.943 0.56 259194. 0.4628 35.48 0.2676 0.5941 0.0612 0.0276 2.436 21.932 15.294 1816.353 2.478 68.029 3.819 0.56 259507. 0.4382 38.44 0.2900 0.6233 0.0582 0.0271 2.393 21.544 14.549 1784.229 2.434 64.713 3.698 0.56 259836. 0.4139 41.40 0.3123 0.6497 0.0551 0.0265 2.339 21.063 13.769 1744.438 2.380 61.245 3.580 0.56 260181. 0.3897 44.35 0.3346 0.6735 0.0519 0.0258 2.276 20.490 12.958 1696.943 2.315 57.639 3.464 0.56 260544. 0.3658 47.31 0.3569 0.6945 0.0485 0.0249 2.202 19.823 12.119 1641.733 2.240 53.907 3.348 0.56 260923. 0.3420 50.27 0.3792 0.7126 0.0450 0.0240 2.117 19.064 11.255 1578.819 2.154 50.062 3.233 0.56 261320. 0.3182 53.23 0.4015 0.7275 0.0415 0.0229 2.023 18.211 10.368 1508.230 2.058 46.115 3.118 0.56 261734. 0.2945 56.18 0.4238 0.7390 0.0379 0.0217 1.918 17.267 9.460 1430.015 1.951 42.078 3.000 0.56 262165. 0.2708 59.14 0.4461 0.7466 0.0342 0.0204 1.803 16.232 8.535 1344.267 1.834 37.964 2.880 0.56 262613. 0.2468 62.10 0.4684 0.7496 0.0304 0.0190 1.678 15.107 7.596 1251.120 1.707 33.786 2.754 0.56 263079. 0.2227 65.05 0.4907 0.7470 0.0266 0.0175 1.543 13.895 6.645 1150.761 1.570 29.558 2.619 0.56 263563. 0.1981 68.01 0.5130 0.7371 0.0228 0.0158 1.399 12.599 5.687 1043.452 1.423 25.296 2.472 0.56 264064. 0.1730 70.97 0.5353 0.7173 0.0189 0.0141 1.247 11.224 4.725 929.534 1.268 21.015 2.305 0.56 264584. 0.1470 73.92 0.5576 0.6833 0.0151 0.0123 1.085 9.774 3.763 809.453 1.104 16.736 2.108 0.56 265121. 0.1200 76.88 0.5799 0.6272 0.0112 0.0104 0.917 8.256 2.805 683.770 0.933 12.477 1.861 0.56 265676. 0.0914 79.84 0.6022 0.5331 0.0074 0.0084 0.742 6.679 1.858 553.180 0.755 8.263 1.523 0.57 266249. 0.0609 82.79 0.6245 0.3642 0.0037 0.0064 0.561 5.053 0.926 418.495 0.571 4.118 1.003 0.57 266840. 0.0283 85.75 0.6468 0.0054 0.0000 0.0042 0.375 3.377 0.009 279.713 0.382 0.040 0.014 0.57 267428. 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 0.0874 0.0271 3.577 28.185 28.520 2667.741 3.184 126.857 4.849 0.63 293412. 0.7597 3.38 0.0223 0.0697 0.0860 0.0275 3.627 28.572 28.067 2704.346 3.228 124.841 4.707 0.63 293588. 0.7316 6.76 0.0446 0.1353 0.0845 0.0278 3.672 28.929 27.577 2738.085 3.268 122.661 4.568 0.63 293778. 0.7038 10.14 0.0669 0.1969 0.0829 0.0282 3.712 29.247 27.049 2768.211 3.304 120.313 4.432 0.63 293982. 0.6762 13.51 0.0892 0.2547 0.0811 0.0284 3.747 29.519 26.481 2793.982 3.335 117.786 4.299 0.63 294202. 0.6490 16.89 0.1115 0.3088 0.0793 0.0286 3.774 29.737 25.871 2814.630 3.360 115.074 4.169 0.64 294437. 0.6221 20.27 0.1338 0.3593 0.0773 0.0288 3.794 29.893 25.218 2829.363 3.377 112.169 4.043 0.64 294689. 0.5956 23.65 0.1561 0.4064 0.0751 0.0289 3.805 29.978 24.520 2837.361 3.387 109.066 3.920 0.64 294957. 0.5694 27.03 0.1784 0.4503 0.0729 0.0289 3.806 29.982 23.776 2837.821 3.387 105.757 3.800 0.64 295243. 0.5436 30.41 0.2007 0.4911 0.0704 0.0288 3.795 29.899 22.985 2829.932 3.378 102.239 3.684 0.64 295546. 0.5182 33.79 0.2230 0.5289 0.0679 0.0286 3.772 29.719 22.147 2812.881 3.358 98.508 3.571 0.64 295867. 0.4930 37.16 0.2453 0.5639 0.0651 0.0283 3.736 29.433 21.259 2785.823 3.325 94.559 3.461 0.64 296207. 0.4682 40.54 0.2676 0.5962 0.0623 0.0279 3.685 29.032 20.320 2747.856 3.280 90.385 3.354 0.64 296565. 0.4436 43.92 0.2899 0.6257 0.0592 0.0274 3.619 28.509 19.333 2698.346 3.221 85.992 3.250 0.64 296943. 0.4192 47.30 0.3122 0.6527 0.0561 0.0268 3.536 27.861 18.299 2637.052 3.148 81.395 3.147 0.64 297339. 0.3950 50.68 0.3345 0.6770 0.0528 0.0261 3.438 27.089 17.224 2563.921 3.060 76.611 3.047 0.64 297754. 0.3710 54.06 0.3568 0.6985 0.0494 0.0252 3.324 26.191 16.110 2478.947 2.959 71.657 2.948 0.64 298189. 0.3471 57.44 0.3791 0.7173 0.0458 0.0242 3.195 25.168 14.961 2382.150 2.843 66.548 2.849 0.64 298643. 0.3233 60.82 0.4014 0.7330 0.0422 0.0231 3.049 24.021 13.782 2273.580 2.714 61.302 2.749 0.64 299117. 0.2995 64.19 0.4237 0.7454 0.0385 0.0219 2.888 22.751 12.575 2153.323 2.570 55.934 2.649 0.64 299610. 0.2756 67.57 0.4460 0.7540 0.0348 0.0206 2.711 21.358 11.345 2021.519 2.413 50.461 2.545 0.64 300124. 0.2515 70.95 0.4683 0.7582 0.0309 0.0191 2.519 19.846 10.095 1878.376 2.242 44.901 2.438 0.64 300657. 0.2272 74.33 0.4906 0.7569 0.0271 0.0175 2.312 18.217 8.829 1724.187 2.058 39.272 2.323 0.64 301210. 0.2025 77.71 0.5129 0.7484 0.0231 0.0159 2.091 16.475 7.553 1559.352 1.861 33.595 2.197 0.64 301783. 0.1771 81.09 0.5352 0.7303 0.0192 0.0141 1.857 14.627 6.271 1384.403 1.653 27.893 2.055 0.64 302377. 0.1509 84.47 0.5575 0.6982 0.0153 0.0122 1.609 12.679 4.989 1200.023 1.432 22.190 1.886 0.64 302991. 0.1236 87.84 0.5798 0.6439 0.0114 0.0102 1.351 10.640 3.713 1007.081 1.202 16.514 1.672 0.65 303626. 0.0945 91.22 0.6021 0.5509 0.0075 0.0082 1.082 8.523 2.450 806.655 0.963 10.896 1.377 0.65 304281. 0.0632 94.60 0.6244 0.3785 0.0037 0.0061 0.805 6.339 1.207 600.007 0.716 5.370 0.913 0.65 304955. 0.0294 97.98 0.6467 -0.0085 -0.0001 0.0039 0.519 4.087 -0.017 386.793 0.462 -0.075 -0.020 0.65 305622. 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 0.0889 0.0277 5.202 36.430 36.725 3879.085 4.116 163.355 4.294 0.71 330049. 0.7635 3.80 0.0223 0.0694 0.0875 0.0281 5.273 36.924 36.155 3931.738 4.172 160.819 4.171 0.71 330248. 0.7358 7.59 0.0445 0.1348 0.0860 0.0284 5.338 37.381 35.537 3980.397 4.223 158.071 4.050 0.71 330462. 0.7082 11.39 0.0668 0.1962 0.0844 0.0287 5.396 37.790 34.870 4023.937 4.270 155.101 3.930 0.71 330693. 0.6809 15.18 0.0891 0.2539 0.0827 0.0290 5.446 38.141 34.150 4061.246 4.309 151.899 3.814 0.71 330942. 0.6539 18.98 0.1114 0.3079 0.0808 0.0292 5.486 38.421 33.376 4091.128 4.341 148.454 3.700 0.71 331208. 0.6272 22.78 0.1336 0.3584 0.0788 0.0294 5.515 38.621 32.544 4112.371 4.363 144.758 3.589 0.71 331492. 0.6008 26.57 0.1559 0.4056 0.0766 0.0295 5.530 38.728 31.655 4123.744 4.375 140.800 3.482 0.71 331796. 0.5747 30.37 0.1782 0.4496 0.0743 0.0295 5.530 38.730 30.705 4124.011 4.376 136.575 3.377 0.72 332118. 0.5490 34.17 0.2004 0.4906 0.0719 0.0294 5.514 38.617 29.693 4111.994 4.363 132.076 3.275 0.72 332461. 0.5236 37.96 0.2227 0.5286 0.0693 0.0292 5.480 38.378 28.619 4086.516 4.336 127.297 3.176 0.72 332824. 0.4985 41.76 0.2450 0.5639 0.0665 0.0289 5.426 38.001 27.480 4046.354 4.293 122.233 3.080 0.72 333207. 0.4738 45.55 0.2673 0.5965 0.0636 0.0285 5.351 37.474 26.276 3990.224 4.234 116.876 2.987 0.72 333612. 0.4492 49.35 0.2895 0.6265 0.0605 0.0280 5.253 36.787 25.007 3917.130 4.156 111.231 2.896 0.72 334037. 0.4248 53.15 0.3118 0.6539 0.0573 0.0273 5.132 35.938 23.677 3826.712 4.060 105.315 2.806 0.72 334484. 0.4006 56.94 0.3341 0.6787 0.0540 0.0266 4.987 34.925 22.292 3718.889 3.946 99.153 2.719 0.72 334952. 0.3766 60.74 0.3563 0.7009 0.0505 0.0257 4.819 33.750 20.856 3593.672 3.813 92.766 2.632 0.72 335442. 0.3527 64.54 0.3786 0.7204 0.0469 0.0247 4.628 32.411 19.374 3451.104 3.662 86.175 2.546 0.72 335953. 0.3288 68.33 0.4009 0.7369 0.0432 0.0235 4.414 30.910 17.851 3291.270 3.492 79.401 2.460 0.72 336487. 0.3049 72.13 0.4232 0.7503 0.0394 0.0222 4.176 29.248 16.292 3114.312 3.304 72.465 2.373 0.72 337042. 0.2810 75.92 0.4454 0.7600 0.0356 0.0209 3.916 27.427 14.701 2920.446 3.099 65.390 2.283 0.72 337619. 0.2568 79.72 0.4677 0.7653 0.0317 0.0194 3.634 25.451 13.084 2710.017 2.875 58.197 2.190 0.72 338219. 0.2324 83.52 0.4900 0.7654 0.0277 0.0177 3.330 23.324 11.446 2483.501 2.635 50.911 2.090 0.72 338841. 0.2075 87.31 0.5122 0.7585 0.0237 0.0160 3.006 21.051 9.793 2241.561 2.378 43.559 1.982 0.72 339485. 0.1819 91.11 0.5345 0.7421 0.0197 0.0142 2.662 18.642 8.131 1985.064 2.106 36.169 1.858 0.72 340152. 0.1554 94.91 0.5568 0.7118 0.0157 0.0123 2.300 16.108 6.469 1715.163 1.820 28.774 1.711 0.73 340842. 0.1277 98.70 0.5790 0.6591 0.0117 0.0102 1.922 13.461 4.814 1433.328 1.521 21.412 1.523 0.73 341555. 0.0981 102.50 0.6013 0.5669 0.0077 0.0082 1.531 10.719 3.175 1141.396 1.211 14.121 1.262 0.73 342290. 0.0659 106.29 0.6236 0.3921 0.0038 0.0060 1.129 7.903 1.561 841.541 0.893 6.945 0.842 0.73 343048. 0.0309 110.09 0.6459 -0.0121 -0.0001 0.0038 0.715 5.009 -0.030 533.339 0.566 -0.132 -0.025 0.73 343794. 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 0.0908 0.0293 7.546 47.562 46.284 5627.127 5.374 205.870 3.731 0.79 366665. 0.7446 4.21 0.0222 0.0671 0.0894 0.0296 7.621 48.037 45.591 5683.297 5.427 202.787 3.638 0.79 366887. 0.7208 8.42 0.0445 0.1309 0.0879 0.0299 7.690 48.467 44.836 5734.206 5.476 199.431 3.546 0.79 367127. 0.6967 12.63 0.0667 0.1913 0.0863 0.0301 7.749 48.841 44.018 5778.498 5.518 195.791 3.455 0.79 367385. 0.6725 16.84 0.0889 0.2484 0.0846 0.0303 7.798 49.148 43.132 5814.812 5.553 191.853 3.364 0.79 367662. 0.6483 21.05 0.1111 0.3022 0.0827 0.0304 7.834 49.375 42.177 5841.702 5.578 187.602 3.275 0.79 367960. 0.6239 25.26 0.1334 0.3528 0.0807 0.0305 7.855 49.511 41.148 5857.678 5.594 183.026 3.186 0.79 368277. 0.5996 29.47 0.1556 0.4003 0.0785 0.0305 7.860 49.540 40.044 5861.143 5.597 178.114 3.099 0.79 368616. 0.5753 33.68 0.1778 0.4448 0.0762 0.0305 7.846 49.450 38.861 5850.472 5.587 172.855 3.013 0.79 368976. 0.5510 37.89 0.2000 0.4864 0.0737 0.0303 7.810 49.226 37.600 5824.008 5.562 167.243 2.928 0.79 369359. 0.5268 42.10 0.2223 0.5251 0.0711 0.0301 7.751 48.854 36.257 5780.035 5.520 161.270 2.845 0.80 369763. 0.5026 46.31 0.2445 0.5610 0.0683 0.0298 7.666 48.319 34.831 5716.763 5.459 154.930 2.764 0.80 370191. 0.4785 50.52 0.2667 0.5943 0.0653 0.0293 7.553 47.605 33.321 5632.213 5.378 148.212 2.683 0.80 370642. 0.4544 54.73 0.2889 0.6249 0.0622 0.0288 7.409 46.696 31.727 5524.713 5.276 141.120 2.605 0.80 371116. 0.4304 58.93 0.3112 0.6530 0.0589 0.0281 7.233 45.589 30.053 5393.723 5.151 133.677 2.527 0.80 371613. 0.4065 63.14 0.3334 0.6784 0.0555 0.0273 7.025 44.281 28.307 5238.908 5.003 125.910 2.451 0.80 372134. 0.3825 67.35 0.3556 0.7012 0.0520 0.0264 6.786 42.770 26.495 5060.239 4.832 117.850 2.375 0.80 372679. 0.3586 71.56 0.3779 0.7213 0.0483 0.0253 6.514 41.058 24.623 4857.632 4.639 109.523 2.299 0.80 373248. 0.3347 75.77 0.4001 0.7384 0.0445 0.0241 6.211 39.144 22.697 4631.232 4.423 100.956 2.223 0.80 373841. 0.3107 79.98 0.4223 0.7522 0.0406 0.0228 5.876 37.034 20.723 4381.558 4.184 92.176 2.145 0.80 374458. 0.2865 84.19 0.4445 0.7621 0.0367 0.0214 5.511 34.732 18.707 4109.217 3.924 83.210 2.065 0.80 375099. 0.2620 88.40 0.4668 0.7675 0.0327 0.0199 5.116 32.246 16.656 3815.072 3.643 74.088 1.980 0.80 375764. 0.2371 92.61 0.4890 0.7669 0.0286 0.0182 4.694 29.586 14.577 3500.316 3.343 64.838 1.889 0.80 376454. 0.2116 96.82 0.5112 0.7586 0.0245 0.0165 4.246 26.764 12.477 3166.499 3.024 55.496 1.787 0.80 377169. 0.1852 101.03 0.5334 0.7394 0.0203 0.0147 3.776 23.797 10.363 2815.517 2.689 46.095 1.669 0.80 377909. 0.1577 105.24 0.5557 0.7044 0.0162 0.0128 3.285 20.706 8.246 2449.770 2.339 36.679 1.527 0.81 378673. 0.1286 109.45 0.5779 0.6444 0.0120 0.0108 2.779 17.514 6.136 2072.163 1.979 27.292 1.343 0.81 379463. 0.0976 113.66 0.6001 0.5420 0.0079 0.0088 2.261 14.251 4.044 1686.065 1.610 17.987 1.088 0.81 380278. 0.0642 117.87 0.6224 0.3587 0.0039 0.0067 1.737 10.948 1.982 1295.260 1.237 8.817 0.694 0.81 381116. 0.0287 122.08 0.6446 -0.0140 -0.0001 0.0047 1.206 7.600 -0.052 899.185 0.859 -0.230 -0.026 0.81 381946. 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 0.0928 0.0341 11.689 66.974 57.261 8716.244 7.567 254.697 2.980 0.87 403258. 0.6615 4.63 0.0222 0.0595 0.0915 0.0342 11.717 67.137 56.450 8737.453 7.585 251.089 2.930 0.87 403504. 0.6459 9.27 0.0445 0.1170 0.0901 0.0342 11.732 67.225 55.562 8748.799 7.595 247.139 2.881 0.87 403769. 0.6299 13.90 0.0667 0.1724 0.0885 0.0342 11.733 67.226 54.593 8748.939 7.595 242.828 2.830 0.87 404055. 0.6135 18.53 0.0889 0.2258 0.0868 0.0342 11.716 67.131 53.538 8736.588 7.584 238.138 2.779 0.87 404363. 0.5967 23.16 0.1112 0.2770 0.0849 0.0341 11.681 66.929 52.394 8710.378 7.562 233.048 2.728 0.87 404692. 0.5794 27.80 0.1334 0.3262 0.0829 0.0339 11.625 66.610 51.156 8668.859 7.526 227.543 2.677 0.87 405045. 0.5616 32.43 0.1557 0.3731 0.0808 0.0337 11.547 66.162 49.822 8610.550 7.475 221.606 2.624 0.87 405421. 0.5435 37.06 0.1779 0.4178 0.0784 0.0334 11.444 65.573 48.387 8533.872 7.408 215.224 2.572 0.87 405821. 0.5248 41.69 0.2001 0.4603 0.0759 0.0330 11.314 64.830 46.849 8437.219 7.324 208.385 2.519 0.87 406245. 0.5057 46.33 0.2224 0.5006 0.0733 0.0325 11.156 63.922 45.207 8318.979 7.222 201.081 2.465 0.87 406694. 0.4862 50.96 0.2446 0.5385 0.0704 0.0320 10.966 62.834 43.459 8177.393 7.099 193.304 2.410 0.88 407168. 0.4662 55.59 0.2668 0.5741 0.0674 0.0313 10.742 61.551 41.602 8010.435 6.954 185.044 2.356 0.88 407668. 0.4457 60.22 0.2891 0.6073 0.0642 0.0306 10.482 60.058 39.636 7816.124 6.785 176.299 2.300 0.88 408194. 0.4248 64.86 0.3113 0.6380 0.0609 0.0297 10.183 58.349 37.567 7593.681 6.592 167.099 2.244 0.88 408745. 0.4035 69.49 0.3335 0.6660 0.0574 0.0287 9.851 56.443 35.405 7345.705 6.377 157.479 2.186 0.88 409322. 0.3816 74.12 0.3558 0.6907 0.0537 0.0277 9.487 54.359 33.156 7074.390 6.141 147.476 2.126 0.88 409925. 0.3591 78.75 0.3780 0.7120 0.0500 0.0265 9.092 52.098 30.828 6780.127 5.886 137.123 2.062 0.88 410555. 0.3359 83.39 0.4003 0.7294 0.0461 0.0253 8.666 49.657 28.430 6462.504 5.610 126.456 1.995 0.88 411210. 0.3121 88.02 0.4225 0.7416 0.0421 0.0240 8.219 47.093 25.968 6128.800 5.321 115.505 1.922 0.88 411892. 0.2873 92.65 0.4447 0.7478 0.0380 0.0226 7.747 44.391 23.451 5777.241 5.015 104.308 1.841 0.88 412600. 0.2616 97.28 0.4670 0.7478 0.0339 0.0211 7.246 41.518 20.887 5403.255 4.691 92.906 1.753 0.88 413335. 0.2351 101.92 0.4892 0.7398 0.0296 0.0196 6.718 38.491 18.287 5009.331 4.349 81.339 1.656 0.88 414097. 0.2077 106.55 0.5114 0.7214 0.0254 0.0180 6.167 35.339 15.659 4599.103 3.993 69.651 1.544 0.88 414886. 0.1793 111.18 0.5337 0.6889 0.0211 0.0163 5.601 32.094 13.015 4176.796 3.626 57.890 1.413 0.89 415701. 0.1496 115.81 0.5559 0.6372 0.0168 0.0147 5.024 28.787 10.366 3746.373 3.252 46.108 1.255 0.89 416544. 0.1185 120.45 0.5781 0.5586 0.0125 0.0130 4.442 25.454 7.726 3312.681 2.876 34.366 1.058 0.89 417414. 0.0863 125.08 0.6004 0.4412 0.0083 0.0113 3.863 22.137 5.111 2880.990 2.501 22.733 0.805 0.89 418312. 0.0534 129.71 0.6226 0.2664 0.0041 0.0096 3.294 18.874 2.537 2456.315 2.132 11.284 0.468 0.89 419236. 0.0219 134.34 0.6448 0.0004 0.0000 0.0080 2.729 15.638 0.003 2035.142 1.767 0.013 0.001 0.89 420166. 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 0.0931 0.0415 18.485 97.090 68.375 13784.325 10.969 304.132 2.250 0.95 439899. 0.5458 5.22 0.0230 0.0507 0.0920 0.0416 18.516 97.252 67.525 13807.237 10.987 300.352 2.218 0.95 440169. 0.5348 10.44 0.0459 0.1001 0.0907 0.0416 18.515 97.246 66.576 13806.416 10.987 296.131 2.187 0.95 440463. 0.5236 15.65 0.0689 0.1480 0.0892 0.0415 18.477 97.048 65.521 13778.317 10.964 291.435 2.157 0.95 440782. 0.5122 20.87 0.0918 0.1946 0.0876 0.0413 18.399 96.636 64.350 13719.780 10.918 286.229 2.127 0.95 441126. 0.5007 26.09 0.1148 0.2400 0.0859 0.0411 18.276 95.990 63.057 13628.090 10.845 280.477 2.099 0.95 441498. 0.4889 31.31 0.1377 0.2842 0.0839 0.0407 18.105 95.095 61.634 13501.052 10.744 274.148 2.071 0.95 441897. 0.4769 36.52 0.1607 0.3271 0.0818 0.0402 17.885 93.939 60.076 13336.946 10.613 267.216 2.043 0.95 442324. 0.4646 41.74 0.1837 0.3689 0.0795 0.0396 17.614 92.514 58.376 13134.556 10.452 259.658 2.016 0.95 442780. 0.4519 46.96 0.2066 0.4094 0.0770 0.0389 17.290 90.812 56.532 12893.009 10.260 251.455 1.989 0.95 443266. 0.4387 52.18 0.2296 0.4487 0.0743 0.0380 16.913 88.831 54.540 12611.728 10.036 242.594 1.961 0.95 443781. 0.4250 57.39 0.2525 0.4865 0.0714 0.0370 16.482 86.568 52.397 12290.398 9.780 233.064 1.934 0.96 444327. 0.4107 62.61 0.2755 0.5229 0.0682 0.0359 15.996 84.019 50.101 11928.511 9.492 222.851 1.905 0.96 444902. 0.3956 67.83 0.2984 0.5576 0.0649 0.0347 15.457 81.185 47.655 11526.234 9.172 211.969 1.875 0.96 445509. 0.3798 73.05 0.3214 0.5905 0.0614 0.0334 14.866 78.080 45.068 11085.279 8.821 200.464 1.844 0.96 446145. 0.3632 78.26 0.3444 0.6214 0.0577 0.0320 14.225 74.716 42.354 10607.685 8.441 188.393 1.811 0.96 446812. 0.3458 83.48 0.3673 0.6488 0.0538 0.0305 13.560 71.222 39.523 10111.736 8.047 175.798 1.773 0.96 447510. 0.3270 88.70 0.3903 0.6721 0.0498 0.0289 12.874 67.620 36.585 9600.329 7.640 162.730 1.728 0.96 448237. 0.3067 93.92 0.4132 0.6903 0.0457 0.0274 12.173 63.935 33.553 9077.081 7.223 149.245 1.677 0.96 448996. 0.2849 99.13 0.4362 0.7007 0.0415 0.0258 11.482 60.310 30.438 8562.419 6.814 135.389 1.612 0.96 449784. 0.2610 104.35 0.4591 0.6941 0.0371 0.0245 10.920 57.356 27.240 8143.127 6.480 121.163 1.517 0.96 450604. 0.2323 109.57 0.4821 0.6766 0.0327 0.0233 10.359 54.407 23.987 7724.392 6.147 106.696 1.409 0.96 451454. 0.2024 114.79 0.5051 0.6472 0.0282 0.0220 9.789 51.413 20.698 7299.377 5.809 92.067 1.286 0.96 452335. 0.1717 120.00 0.5280 0.6038 0.0237 0.0207 9.217 48.412 17.392 6873.240 5.470 77.361 1.148 0.97 453247. 0.1404 125.22 0.5510 0.5438 0.0192 0.0194 8.652 45.443 14.090 6451.703 5.134 62.670 0.991 0.97 454190. 0.1091 130.44 0.5739 0.4643 0.0147 0.0182 8.101 42.549 10.814 6040.898 4.807 48.099 0.812 0.97 455165. 0.0783 135.66 0.5969 0.3628 0.0103 0.0170 7.569 39.756 7.591 5644.271 4.492 33.765 0.610 0.97 456172. 0.0493 140.87 0.6198 0.2367 0.0061 0.0159 7.060 37.080 4.448 5264.472 4.189 19.783 0.383 0.97 457214. 0.0237 146.09 0.6428 0.0826 0.0019 0.0148 6.567 34.494 1.393 4897.273 3.897 6.196 0.129 0.97 458298. 0.0045 151.31 0.6658