18x8W (18x8W.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 0.0859 0.0346 0.005 0.332 0.287 3.928 0.038 1.278 33.165 0.07 38449. 0.5794 0.36 0.0209 0.0505 0.0842 0.0348 0.005 0.334 0.282 3.948 0.038 1.253 32.348 0.07 38471. 0.5596 0.71 0.0418 0.0985 0.0824 0.0350 0.005 0.335 0.276 3.965 0.038 1.226 31.532 0.07 38495. 0.5396 1.07 0.0627 0.1440 0.0805 0.0351 0.005 0.336 0.269 3.977 0.038 1.198 30.716 0.07 38521. 0.5196 1.43 0.0836 0.1869 0.0785 0.0351 0.005 0.337 0.263 3.984 0.038 1.168 29.902 0.07 38548. 0.4995 1.78 0.1045 0.2273 0.0764 0.0351 0.005 0.337 0.256 3.985 0.038 1.137 29.090 0.07 38577. 0.4794 2.14 0.1255 0.2651 0.0742 0.0351 0.005 0.336 0.248 3.980 0.038 1.104 28.280 0.07 38607. 0.4592 2.49 0.1464 0.3005 0.0719 0.0350 0.005 0.335 0.240 3.969 0.038 1.069 27.471 0.07 38640. 0.4391 2.85 0.1673 0.3333 0.0694 0.0348 0.005 0.334 0.232 3.951 0.038 1.033 26.663 0.07 38674. 0.4189 3.21 0.1882 0.3636 0.0669 0.0346 0.005 0.332 0.224 3.925 0.037 0.995 25.855 0.07 38710. 0.3987 3.56 0.2091 0.3913 0.0642 0.0343 0.005 0.329 0.215 3.891 0.037 0.956 25.046 0.07 38748. 0.3785 3.92 0.2300 0.4165 0.0615 0.0340 0.005 0.325 0.206 3.850 0.037 0.915 24.235 0.07 38788. 0.3583 4.28 0.2509 0.4391 0.0586 0.0335 0.005 0.321 0.196 3.800 0.036 0.873 23.418 0.07 38830. 0.3381 4.63 0.2718 0.4589 0.0557 0.0330 0.005 0.316 0.186 3.742 0.036 0.829 22.595 0.07 38874. 0.3180 4.99 0.2927 0.4760 0.0527 0.0324 0.005 0.311 0.176 3.675 0.035 0.784 21.761 0.07 38920. 0.2979 5.35 0.3136 0.4902 0.0496 0.0317 0.005 0.304 0.166 3.599 0.034 0.738 20.914 0.07 38968. 0.2777 5.70 0.3346 0.5012 0.0464 0.0310 0.005 0.297 0.155 3.513 0.034 0.691 20.049 0.07 39018. 0.2575 6.06 0.3555 0.5090 0.0432 0.0301 0.005 0.289 0.144 3.418 0.033 0.642 19.161 0.07 39070. 0.2373 6.42 0.3764 0.5131 0.0398 0.0292 0.004 0.280 0.133 3.313 0.032 0.593 18.243 0.07 39125. 0.2171 6.77 0.3973 0.5132 0.0364 0.0282 0.004 0.270 0.122 3.198 0.031 0.542 17.287 0.07 39182. 0.1967 7.13 0.4182 0.5089 0.0330 0.0271 0.004 0.260 0.110 3.072 0.029 0.491 16.283 0.07 39241. 0.1763 7.48 0.4391 0.4993 0.0295 0.0259 0.004 0.248 0.099 2.937 0.028 0.438 15.218 0.07 39302. 0.1557 7.84 0.4600 0.4837 0.0259 0.0246 0.004 0.236 0.087 2.790 0.027 0.385 14.073 0.07 39366. 0.1350 8.20 0.4809 0.4609 0.0223 0.0232 0.004 0.223 0.074 2.633 0.025 0.331 12.825 0.07 39432. 0.1141 8.55 0.5018 0.4291 0.0186 0.0217 0.003 0.208 0.062 2.466 0.024 0.277 11.444 0.07 39500. 0.0930 8.91 0.5227 0.3861 0.0149 0.0202 0.003 0.193 0.050 2.288 0.022 0.222 9.884 0.07 39570. 0.0719 9.27 0.5436 0.3284 0.0112 0.0185 0.003 0.177 0.037 2.100 0.020 0.166 8.084 0.07 39643. 0.0510 9.62 0.5646 0.2510 0.0075 0.0168 0.003 0.161 0.025 1.901 0.018 0.111 5.949 0.07 39718. 0.0306 9.98 0.5855 0.1457 0.0037 0.0149 0.002 0.143 0.012 1.693 0.016 0.055 3.331 0.07 39795. 0.0121 10.34 0.6064 -0.0015 0.0000 0.0130 0.002 0.125 0.000 1.475 0.014 0.000 -0.033 0.07 39870. 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 0.0863 0.0309 0.038 1.184 1.155 28.014 0.134 5.136 18.694 0.14 76897. 0.6548 0.72 0.0210 0.0572 0.0846 0.0311 0.038 1.192 1.132 28.206 0.135 5.035 18.204 0.14 76942. 0.6314 1.43 0.0420 0.1112 0.0828 0.0313 0.038 1.199 1.108 28.367 0.135 4.929 17.718 0.14 76990. 0.6080 2.15 0.0630 0.1623 0.0809 0.0314 0.038 1.204 1.083 28.491 0.136 4.816 17.236 0.14 77042. 0.5846 2.86 0.0840 0.2105 0.0789 0.0315 0.038 1.208 1.056 28.574 0.136 4.697 16.760 0.14 77096. 0.5614 3.58 0.1050 0.2557 0.0768 0.0315 0.038 1.209 1.028 28.612 0.137 4.571 16.289 0.14 77154. 0.5383 4.30 0.1260 0.2981 0.0746 0.0315 0.038 1.209 0.998 28.599 0.137 4.438 15.824 0.14 77216. 0.5152 5.01 0.1470 0.3376 0.0722 0.0315 0.038 1.206 0.966 28.531 0.136 4.299 15.364 0.14 77281. 0.4923 5.73 0.1681 0.3744 0.0698 0.0313 0.038 1.200 0.934 28.405 0.136 4.153 14.908 0.14 77350. 0.4696 6.45 0.1891 0.4085 0.0672 0.0311 0.038 1.192 0.899 28.216 0.135 4.001 14.458 0.14 77422. 0.4470 7.16 0.2101 0.4399 0.0646 0.0308 0.037 1.182 0.864 27.963 0.134 3.842 14.011 0.14 77499. 0.4245 7.88 0.2311 0.4685 0.0618 0.0305 0.037 1.168 0.827 27.643 0.132 3.678 13.568 0.14 77579. 0.4022 8.59 0.2521 0.4945 0.0589 0.0300 0.037 1.152 0.789 27.252 0.130 3.508 13.126 0.14 77664. 0.3800 9.31 0.2731 0.5177 0.0560 0.0295 0.036 1.132 0.749 26.789 0.128 3.332 12.685 0.14 77753. 0.3579 10.03 0.2941 0.5381 0.0530 0.0289 0.035 1.109 0.709 26.249 0.125 3.152 12.244 0.14 77845. 0.3360 10.74 0.3151 0.5557 0.0498 0.0283 0.034 1.083 0.667 25.632 0.122 2.966 11.800 0.14 77942. 0.3141 11.46 0.3361 0.5702 0.0466 0.0275 0.033 1.054 0.624 24.935 0.119 2.776 11.351 0.14 78044. 0.2923 12.17 0.3571 0.5814 0.0434 0.0266 0.032 1.021 0.580 24.154 0.115 2.581 10.894 0.14 78149. 0.2705 12.89 0.3781 0.5892 0.0400 0.0257 0.031 0.984 0.535 23.289 0.111 2.381 10.426 0.14 78259. 0.2487 13.61 0.3991 0.5931 0.0366 0.0246 0.030 0.944 0.490 22.337 0.107 2.178 9.943 0.14 78374. 0.2268 14.32 0.4201 0.5926 0.0331 0.0235 0.029 0.900 0.443 21.296 0.102 1.971 9.438 0.14 78493. 0.2048 15.04 0.4411 0.5869 0.0296 0.0222 0.027 0.852 0.396 20.166 0.096 1.761 8.903 0.14 78616. 0.1826 15.75 0.4621 0.5752 0.0260 0.0209 0.025 0.801 0.348 18.945 0.090 1.547 8.327 0.14 78745. 0.1601 16.47 0.4832 0.5558 0.0224 0.0194 0.024 0.745 0.299 17.632 0.084 1.331 7.697 0.14 78878. 0.1372 17.19 0.5042 0.5266 0.0187 0.0179 0.022 0.686 0.250 16.228 0.077 1.112 6.989 0.14 79015. 0.1139 17.90 0.5252 0.4845 0.0150 0.0162 0.020 0.623 0.201 14.733 0.070 0.892 6.173 0.14 79157. 0.0901 18.62 0.5462 0.4242 0.0113 0.0145 0.018 0.556 0.151 13.150 0.063 0.670 5.197 0.14 79304. 0.0658 19.34 0.5672 0.3371 0.0075 0.0127 0.015 0.485 0.101 11.479 0.055 0.448 3.977 0.15 79455. 0.0411 20.05 0.5882 0.2076 0.0038 0.0107 0.013 0.411 0.051 9.725 0.046 0.225 2.361 0.15 79609. 0.0173 20.77 0.6092 0.0014 0.0000 0.0087 0.011 0.333 0.000 7.873 0.038 0.001 0.015 0.15 79754. 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 0.0867 0.0294 0.121 2.537 2.611 90.064 0.287 11.612 13.147 0.21 115343. 0.6924 1.08 0.0211 0.0604 0.0850 0.0296 0.122 2.557 2.560 90.755 0.289 11.385 12.792 0.21 115410. 0.6672 2.15 0.0421 0.1175 0.0832 0.0298 0.122 2.573 2.506 91.339 0.291 11.144 12.442 0.21 115483. 0.6420 3.23 0.0632 0.1714 0.0813 0.0300 0.123 2.586 2.448 91.799 0.292 10.889 12.096 0.21 115561. 0.6170 4.31 0.0843 0.2221 0.0793 0.0301 0.124 2.595 2.388 92.118 0.293 10.620 11.756 0.21 115643. 0.5921 5.39 0.1053 0.2697 0.0772 0.0301 0.124 2.600 2.323 92.280 0.294 10.335 11.420 0.21 115731. 0.5675 6.46 0.1264 0.3143 0.0749 0.0301 0.124 2.600 2.256 92.267 0.294 10.035 11.090 0.21 115823. 0.5430 7.54 0.1475 0.3559 0.0726 0.0301 0.123 2.594 2.185 92.065 0.293 9.719 10.765 0.21 115922. 0.5187 8.62 0.1685 0.3947 0.0701 0.0299 0.123 2.582 2.111 91.660 0.292 9.389 10.445 0.21 116026. 0.4947 9.70 0.1896 0.4306 0.0675 0.0297 0.122 2.565 2.033 91.041 0.290 9.045 10.130 0.21 116135. 0.4709 10.77 0.2107 0.4638 0.0649 0.0295 0.121 2.541 1.953 90.197 0.287 8.686 9.820 0.21 116251. 0.4473 11.85 0.2318 0.4942 0.0621 0.0291 0.120 2.511 1.869 89.119 0.284 8.314 9.513 0.21 116372. 0.4240 12.93 0.2528 0.5219 0.0592 0.0287 0.118 2.474 1.783 87.797 0.279 7.929 9.209 0.21 116499. 0.4008 14.01 0.2739 0.5469 0.0562 0.0282 0.116 2.429 1.693 86.220 0.274 7.531 8.907 0.22 116633. 0.3778 15.08 0.2950 0.5691 0.0532 0.0276 0.113 2.377 1.601 84.380 0.269 7.122 8.607 0.22 116773. 0.3550 16.16 0.3160 0.5885 0.0500 0.0269 0.110 2.318 1.507 82.268 0.262 6.701 8.306 0.22 116919. 0.3324 17.24 0.3371 0.6049 0.0468 0.0261 0.107 2.250 1.410 79.875 0.254 6.270 8.004 0.22 117072. 0.3098 18.32 0.3582 0.6182 0.0435 0.0252 0.104 2.175 1.310 77.192 0.246 5.828 7.699 0.22 117231. 0.2873 19.39 0.3792 0.6281 0.0401 0.0242 0.100 2.091 1.209 74.213 0.236 5.377 7.388 0.22 117397. 0.2648 20.47 0.4003 0.6343 0.0367 0.0232 0.095 1.998 1.105 70.931 0.226 4.917 7.068 0.22 117570. 0.2422 21.55 0.4214 0.6362 0.0332 0.0220 0.090 1.897 1.000 67.338 0.214 4.448 6.735 0.22 117750. 0.2196 22.62 0.4424 0.6332 0.0297 0.0207 0.085 1.787 0.893 63.431 0.202 3.971 6.384 0.22 117936. 0.1966 23.70 0.4635 0.6242 0.0260 0.0193 0.079 1.668 0.784 59.207 0.188 3.488 6.007 0.22 118130. 0.1734 24.78 0.4846 0.6077 0.0224 0.0179 0.073 1.540 0.674 54.663 0.174 2.999 5.594 0.22 118330. 0.1497 25.86 0.5056 0.5812 0.0187 0.0163 0.067 1.403 0.563 49.800 0.159 2.504 5.127 0.22 118537. 0.1254 26.93 0.5267 0.5412 0.0150 0.0146 0.060 1.257 0.451 44.620 0.142 2.005 4.583 0.22 118752. 0.1003 28.01 0.5478 0.4813 0.0112 0.0128 0.052 1.102 0.338 39.130 0.125 1.504 3.919 0.22 118973. 0.0743 29.09 0.5689 0.3905 0.0075 0.0109 0.045 0.939 0.225 33.338 0.106 1.001 3.062 0.22 119200. 0.0474 30.17 0.5899 0.2465 0.0037 0.0089 0.037 0.768 0.112 27.253 0.087 0.498 1.864 0.22 119433. 0.0203 31.24 0.6110 -0.0072 -0.0001 0.0068 0.028 0.586 -0.002 20.789 0.066 -0.011 -0.053 0.22 119639. 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 0.0872 0.0287 0.279 4.401 4.669 208.273 0.497 20.768 10.168 0.29 153785. 0.7162 1.44 0.0211 0.0624 0.0855 0.0289 0.282 4.437 4.578 209.972 0.501 20.364 9.890 0.29 153876. 0.6898 2.88 0.0422 0.1213 0.0837 0.0291 0.284 4.467 4.482 211.414 0.505 19.934 9.615 0.29 153973. 0.6635 4.32 0.0633 0.1768 0.0818 0.0293 0.285 4.491 4.379 212.557 0.507 19.478 9.345 0.29 154077. 0.6374 5.76 0.0844 0.2291 0.0798 0.0294 0.286 4.508 4.271 213.362 0.509 18.996 9.079 0.29 154187. 0.6116 7.19 0.1055 0.2781 0.0776 0.0295 0.287 4.517 4.156 213.786 0.510 18.487 8.818 0.29 154304. 0.5860 8.63 0.1266 0.3240 0.0754 0.0295 0.287 4.518 4.036 213.790 0.510 17.951 8.562 0.29 154428. 0.5607 10.07 0.1477 0.3670 0.0730 0.0294 0.286 4.508 3.909 213.335 0.509 17.387 8.311 0.29 154560. 0.5356 11.51 0.1688 0.4069 0.0705 0.0293 0.285 4.488 3.776 212.392 0.507 16.796 8.064 0.29 154699. 0.5108 12.95 0.1899 0.4440 0.0680 0.0291 0.283 4.457 3.638 210.931 0.504 16.180 7.822 0.29 154846. 0.4863 14.39 0.2110 0.4784 0.0653 0.0288 0.280 4.415 3.493 208.926 0.499 15.538 7.584 0.29 155000. 0.4620 15.83 0.2321 0.5099 0.0625 0.0284 0.277 4.360 3.344 206.354 0.493 14.872 7.349 0.29 155163. 0.4381 17.27 0.2532 0.5388 0.0596 0.0280 0.272 4.294 3.189 203.189 0.485 14.183 7.118 0.29 155334. 0.4143 18.70 0.2743 0.5649 0.0566 0.0275 0.267 4.214 3.029 199.409 0.476 13.471 6.889 0.29 155512. 0.3908 20.14 0.2954 0.5883 0.0535 0.0269 0.261 4.120 2.864 194.991 0.466 12.739 6.662 0.29 155700. 0.3675 21.58 0.3165 0.6089 0.0503 0.0262 0.255 4.013 2.695 189.913 0.453 11.986 6.435 0.29 155895. 0.3444 23.02 0.3376 0.6266 0.0471 0.0254 0.247 3.891 2.521 184.154 0.440 11.213 6.209 0.29 156100. 0.3214 24.46 0.3587 0.6414 0.0438 0.0245 0.238 3.755 2.343 177.694 0.424 10.422 5.981 0.29 156313. 0.2984 25.90 0.3798 0.6528 0.0404 0.0235 0.229 3.603 2.162 170.514 0.407 9.614 5.750 0.29 156535. 0.2756 27.34 0.4010 0.6607 0.0369 0.0224 0.218 3.436 1.976 162.598 0.388 8.790 5.513 0.29 156767. 0.2526 28.78 0.4221 0.6645 0.0334 0.0212 0.206 3.253 1.788 153.930 0.367 7.951 5.267 0.29 157007. 0.2296 30.22 0.4432 0.6635 0.0298 0.0199 0.194 3.053 1.596 144.501 0.345 7.098 5.009 0.29 157256. 0.2063 31.65 0.4643 0.6568 0.0262 0.0185 0.180 2.838 1.401 134.300 0.321 6.233 4.733 0.29 157515. 0.1826 33.09 0.4854 0.6426 0.0225 0.0170 0.165 2.606 1.204 123.325 0.294 5.357 4.430 0.29 157783. 0.1585 34.53 0.5065 0.6187 0.0188 0.0154 0.150 2.358 1.005 111.575 0.266 4.472 4.087 0.29 158060. 0.1336 35.97 0.5276 0.5811 0.0150 0.0137 0.133 2.093 0.805 99.059 0.236 3.580 3.685 0.29 158347. 0.1078 37.41 0.5487 0.5229 0.0113 0.0118 0.115 1.813 0.603 85.791 0.205 2.682 3.188 0.29 158643. 0.0807 38.85 0.5698 0.4312 0.0075 0.0099 0.096 1.517 0.401 71.790 0.171 1.783 2.532 0.29 158947. 0.0523 40.29 0.5909 0.2785 0.0037 0.0079 0.077 1.206 0.198 57.080 0.136 0.883 1.577 0.29 159258. 0.0229 41.73 0.6120 -0.0150 -0.0001 0.0057 0.055 0.874 -0.007 41.356 0.099 -0.033 -0.082 0.29 159514. 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 0.0879 0.0284 0.539 6.795 7.350 401.965 0.768 32.695 8.294 0.36 192222. 0.7330 1.80 0.0211 0.0637 0.0862 0.0286 0.544 6.853 7.208 405.369 0.774 32.060 8.065 0.36 192336. 0.7058 3.60 0.0423 0.1238 0.0844 0.0288 0.547 6.901 7.056 408.260 0.780 31.385 7.839 0.36 192458. 0.6788 5.40 0.0634 0.1804 0.0824 0.0290 0.551 6.940 6.895 410.559 0.784 30.669 7.617 0.36 192588. 0.6520 7.20 0.0845 0.2337 0.0804 0.0291 0.553 6.968 6.725 412.184 0.787 29.912 7.400 0.36 192727. 0.6256 9.00 0.1056 0.2837 0.0783 0.0291 0.554 6.982 6.545 413.053 0.789 29.111 7.187 0.36 192874. 0.5993 10.80 0.1268 0.3305 0.0760 0.0291 0.554 6.983 6.355 413.085 0.789 28.268 6.978 0.36 193030. 0.5734 12.60 0.1479 0.3743 0.0736 0.0291 0.553 6.968 6.156 412.206 0.787 27.380 6.773 0.36 193196. 0.5478 14.41 0.1690 0.4151 0.0711 0.0290 0.550 6.937 5.947 410.353 0.784 26.451 6.573 0.36 193370. 0.5225 16.21 0.1902 0.4530 0.0685 0.0287 0.546 6.888 5.728 407.470 0.778 25.480 6.377 0.36 193554. 0.4975 18.01 0.2113 0.4882 0.0658 0.0285 0.541 6.821 5.501 403.504 0.771 24.470 6.184 0.36 193748. 0.4728 19.81 0.2324 0.5205 0.0630 0.0281 0.534 6.735 5.265 398.408 0.761 23.421 5.994 0.36 193952. 0.4484 21.61 0.2535 0.5502 0.0600 0.0277 0.526 6.629 5.021 392.133 0.749 22.335 5.808 0.36 194166. 0.4243 23.41 0.2747 0.5772 0.0570 0.0271 0.516 6.502 4.769 384.634 0.735 21.215 5.624 0.36 194391. 0.4004 25.21 0.2958 0.6015 0.0539 0.0265 0.504 6.354 4.510 375.864 0.718 20.060 5.442 0.36 194626. 0.3768 27.01 0.3169 0.6230 0.0507 0.0258 0.491 6.183 4.243 365.781 0.699 18.874 5.262 0.36 194871. 0.3533 28.81 0.3380 0.6418 0.0475 0.0250 0.475 5.990 3.970 354.342 0.677 17.657 5.081 0.36 195128. 0.3300 30.61 0.3592 0.6576 0.0441 0.0241 0.458 5.773 3.689 341.508 0.652 16.411 4.900 0.36 195395. 0.3068 32.41 0.3803 0.6703 0.0407 0.0231 0.439 5.532 3.403 327.241 0.625 15.138 4.717 0.36 195674. 0.2837 34.21 0.4014 0.6795 0.0372 0.0220 0.418 5.266 3.111 311.509 0.595 13.839 4.530 0.36 195964. 0.2605 36.01 0.4226 0.6848 0.0336 0.0208 0.395 4.975 2.814 294.282 0.562 12.517 4.337 0.36 196265. 0.2372 37.81 0.4437 0.6855 0.0300 0.0194 0.370 4.658 2.512 275.538 0.526 11.173 4.135 0.36 196577. 0.2136 39.62 0.4648 0.6805 0.0264 0.0180 0.342 4.315 2.205 255.260 0.488 9.809 3.919 0.36 196902. 0.1897 41.42 0.4859 0.6685 0.0227 0.0165 0.313 3.946 1.895 233.440 0.446 8.428 3.682 0.36 197238. 0.1652 43.22 0.5071 0.6468 0.0189 0.0148 0.282 3.551 1.581 210.081 0.401 7.033 3.414 0.36 197585. 0.1399 45.02 0.5282 0.6115 0.0151 0.0131 0.248 3.131 1.265 185.197 0.354 5.627 3.098 0.36 197944. 0.1136 46.82 0.5493 0.5552 0.0113 0.0112 0.213 2.685 0.947 158.816 0.303 4.213 2.705 0.36 198315. 0.0858 48.62 0.5705 0.4638 0.0075 0.0092 0.176 2.214 0.628 130.982 0.250 2.795 2.176 0.36 198696. 0.0562 50.42 0.5916 0.3051 0.0037 0.0072 0.136 1.720 0.310 101.736 0.194 1.377 1.380 0.36 199086. 0.0250 52.22 0.6127 -0.0264 -0.0002 0.0050 0.094 1.186 -0.018 70.178 0.134 -0.079 -0.115 0.36 199369. 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 0.0887 0.0283 0.928 9.752 10.683 692.293 1.102 47.516 6.999 0.43 230652. 0.7457 2.16 0.0212 0.0645 0.0870 0.0285 0.936 9.837 10.476 698.293 1.111 46.597 6.805 0.43 230790. 0.7179 4.33 0.0423 0.1254 0.0852 0.0287 0.943 9.909 10.256 703.390 1.119 45.620 6.614 0.43 230937. 0.6904 6.49 0.0635 0.1828 0.0832 0.0289 0.949 9.966 10.023 707.439 1.126 44.582 6.426 0.43 231094. 0.6632 8.65 0.0846 0.2368 0.0812 0.0290 0.953 10.006 9.776 710.300 1.130 43.484 6.243 0.43 231262. 0.6363 10.82 0.1058 0.2875 0.0790 0.0291 0.955 10.028 9.515 711.828 1.133 42.322 6.063 0.43 231439. 0.6096 12.98 0.1269 0.3350 0.0767 0.0291 0.955 10.028 9.240 711.880 1.133 41.097 5.887 0.43 231628. 0.5833 15.14 0.1481 0.3794 0.0743 0.0290 0.953 10.006 8.950 710.323 1.131 39.809 5.715 0.43 231827. 0.5573 17.31 0.1692 0.4208 0.0718 0.0289 0.948 9.960 8.646 707.049 1.125 38.459 5.547 0.43 232038. 0.5317 19.47 0.1904 0.4593 0.0692 0.0287 0.941 9.889 8.329 701.958 1.117 37.048 5.382 0.43 232260. 0.5063 21.63 0.2115 0.4951 0.0664 0.0284 0.932 9.790 7.999 694.959 1.106 35.580 5.221 0.43 232493. 0.4813 23.80 0.2327 0.5281 0.0636 0.0280 0.920 9.663 7.656 685.966 1.092 34.055 5.062 0.43 232739. 0.4566 25.96 0.2538 0.5584 0.0606 0.0276 0.905 9.507 7.301 674.896 1.074 32.476 4.907 0.43 232997. 0.4322 28.12 0.2750 0.5861 0.0576 0.0270 0.887 9.321 6.935 661.671 1.053 30.847 4.754 0.43 233268. 0.4081 30.28 0.2961 0.6111 0.0544 0.0264 0.867 9.103 6.557 646.209 1.028 29.168 4.603 0.43 233550. 0.3842 32.45 0.3173 0.6334 0.0512 0.0257 0.843 8.853 6.169 628.435 1.000 27.442 4.453 0.43 233846. 0.3605 34.61 0.3384 0.6530 0.0479 0.0248 0.816 8.569 5.771 608.276 0.968 25.671 4.304 0.43 234155. 0.3370 36.77 0.3596 0.6697 0.0445 0.0239 0.785 8.250 5.364 585.662 0.932 23.859 4.154 0.43 234477. 0.3136 38.94 0.3807 0.6834 0.0411 0.0229 0.752 7.896 4.947 560.528 0.892 22.006 4.003 0.43 234813. 0.2903 41.10 0.4019 0.6937 0.0376 0.0218 0.715 7.506 4.523 532.817 0.848 20.117 3.850 0.43 235161. 0.2669 43.26 0.4230 0.7002 0.0340 0.0205 0.674 7.078 4.090 502.478 0.800 18.192 3.692 0.43 235524. 0.2434 45.43 0.4442 0.7023 0.0303 0.0192 0.630 6.613 3.650 469.470 0.747 16.236 3.527 0.43 235900. 0.2196 47.59 0.4653 0.6990 0.0266 0.0177 0.582 6.110 3.204 433.765 0.690 14.252 3.350 0.43 236290. 0.1955 49.75 0.4865 0.6887 0.0229 0.0161 0.530 5.569 2.752 395.350 0.629 12.242 3.158 0.43 236694. 0.1708 51.92 0.5076 0.6690 0.0191 0.0145 0.475 4.990 2.296 354.227 0.564 10.211 2.940 0.43 237113. 0.1452 54.08 0.5288 0.6358 0.0152 0.0127 0.416 4.373 1.836 310.424 0.494 8.164 2.682 0.43 237545. 0.1184 56.24 0.5499 0.5815 0.0114 0.0108 0.354 3.719 1.373 263.992 0.420 6.106 2.359 0.43 237990. 0.0901 58.41 0.5711 0.4908 0.0075 0.0088 0.288 3.029 0.909 215.007 0.342 4.042 1.917 0.44 238449. 0.0596 60.57 0.5922 0.3274 0.0037 0.0067 0.219 2.304 0.445 163.542 0.260 1.977 1.233 0.44 238917. 0.0268 62.73 0.6134 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 0.0897 0.0284 1.479 13.320 14.703 1103.111 1.505 65.399 6.046 0.50 269073. 0.7557 2.53 0.0212 0.0652 0.0880 0.0286 1.492 13.437 14.420 1112.826 1.518 64.139 5.877 0.50 269236. 0.7275 5.06 0.0424 0.1267 0.0861 0.0288 1.503 13.536 14.118 1121.063 1.529 62.797 5.712 0.50 269409. 0.6996 7.59 0.0636 0.1847 0.0842 0.0290 1.512 13.615 13.798 1127.586 1.538 61.372 5.550 0.50 269594. 0.6720 10.12 0.0848 0.2392 0.0821 0.0291 1.518 13.671 13.458 1132.170 1.544 59.862 5.392 0.50 269791. 0.6448 12.65 0.1060 0.2904 0.0799 0.0292 1.521 13.700 13.099 1134.575 1.548 58.264 5.237 0.50 269999. 0.6178 15.18 0.1272 0.3384 0.0776 0.0292 1.521 13.700 12.720 1134.574 1.548 56.578 5.085 0.50 270221. 0.5912 17.71 0.1484 0.3833 0.0752 0.0291 1.518 13.668 12.321 1131.949 1.544 54.804 4.937 0.50 270455. 0.5649 20.24 0.1696 0.4252 0.0726 0.0290 1.511 13.602 11.903 1126.523 1.537 52.944 4.792 0.50 270703. 0.5390 22.77 0.1908 0.4642 0.0699 0.0287 1.499 13.501 11.466 1118.132 1.525 51.000 4.651 0.50 270964. 0.5134 25.30 0.2120 0.5005 0.0672 0.0285 1.484 13.362 11.010 1106.633 1.510 48.974 4.513 0.50 271239. 0.4881 27.83 0.2332 0.5340 0.0643 0.0281 1.464 13.184 10.538 1091.890 1.490 46.871 4.377 0.50 271527. 0.4632 30.36 0.2544 0.5649 0.0613 0.0276 1.440 12.965 10.048 1073.770 1.465 44.694 4.244 0.50 271830. 0.4386 32.89 0.2756 0.5931 0.0582 0.0271 1.411 12.704 9.543 1052.142 1.435 42.445 4.114 0.50 272148. 0.4142 35.42 0.2968 0.6187 0.0550 0.0264 1.377 12.399 9.022 1026.882 1.401 40.128 3.985 0.50 272480. 0.3902 37.95 0.3180 0.6417 0.0518 0.0257 1.338 12.049 8.486 997.868 1.361 37.746 3.857 0.50 272827. 0.3663 40.48 0.3392 0.6619 0.0484 0.0248 1.294 11.652 7.936 964.981 1.316 35.302 3.730 0.50 273190. 0.3426 43.01 0.3604 0.6794 0.0450 0.0239 1.245 11.207 7.374 928.109 1.266 32.799 3.604 0.50 273568. 0.3190 45.54 0.3816 0.6939 0.0415 0.0228 1.190 10.712 6.799 887.152 1.210 30.241 3.476 0.50 273961. 0.2955 48.07 0.4028 0.7051 0.0379 0.0216 1.129 10.167 6.212 842.013 1.149 27.631 3.346 0.50 274371. 0.2719 50.60 0.4240 0.7127 0.0343 0.0204 1.063 9.571 5.615 792.613 1.081 24.974 3.213 0.50 274796. 0.2482 53.13 0.4452 0.7159 0.0305 0.0190 0.991 8.922 5.007 738.887 1.008 22.272 3.074 0.50 275237. 0.2242 55.66 0.4664 0.7138 0.0268 0.0175 0.913 8.220 4.391 680.789 0.929 19.531 2.925 0.51 275695. 0.1998 58.18 0.4876 0.7049 0.0230 0.0159 0.829 7.466 3.767 618.298 0.843 16.755 2.763 0.51 276169. 0.1748 60.71 0.5088 0.6866 0.0191 0.0142 0.739 6.658 3.136 551.423 0.752 13.950 2.580 0.51 276659. 0.1489 63.24 0.5300 0.6548 0.0153 0.0123 0.644 5.798 2.500 480.207 0.655 11.122 2.362 0.51 277165. 0.1217 65.77 0.5512 0.6014 0.0114 0.0104 0.543 4.887 1.861 404.737 0.552 8.278 2.086 0.51 277688. 0.0928 68.30 0.5725 0.5096 0.0074 0.0084 0.436 3.926 1.220 325.141 0.444 5.427 1.702 0.51 278225. 0.0613 70.83 0.5937 0.3376 0.0035 0.0062 0.324 2.916 0.579 241.531 0.329 2.575 1.087 0.51 278772. 0.0270 73.36 0.6149 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 0.0909 0.0286 2.229 17.562 19.462 1662.193 1.984 86.566 5.311 0.57 307484. 0.7637 2.89 0.0212 0.0653 0.0892 0.0289 2.249 17.717 19.090 1676.922 2.002 84.912 5.163 0.57 307670. 0.7354 5.77 0.0423 0.1270 0.0873 0.0291 2.266 17.849 18.694 1689.386 2.017 83.150 5.019 0.57 307869. 0.7074 8.66 0.0635 0.1852 0.0853 0.0293 2.279 17.953 18.273 1699.227 2.028 81.278 4.878 0.57 308081. 0.6797 11.55 0.0847 0.2399 0.0833 0.0294 2.288 18.025 17.827 1706.103 2.037 79.294 4.739 0.57 308307. 0.6523 14.43 0.1058 0.2913 0.0811 0.0294 2.293 18.063 17.354 1709.659 2.041 77.193 4.604 0.57 308547. 0.6252 17.32 0.1270 0.3396 0.0787 0.0294 2.293 18.062 16.856 1709.537 2.041 74.974 4.472 0.57 308801. 0.5985 20.21 0.1482 0.3847 0.0763 0.0294 2.287 18.018 16.330 1705.419 2.036 72.638 4.343 0.57 309070. 0.5721 23.09 0.1694 0.4270 0.0737 0.0292 2.276 17.930 15.779 1697.027 2.026 70.187 4.217 0.57 309353. 0.5461 25.98 0.1905 0.4663 0.0710 0.0290 2.258 17.793 15.203 1684.118 2.010 67.624 4.095 0.57 309652. 0.5204 28.87 0.2117 0.5030 0.0682 0.0287 2.235 17.607 14.603 1666.479 1.989 64.953 3.974 0.57 309967. 0.4951 31.75 0.2329 0.5369 0.0653 0.0283 2.205 17.368 13.979 1643.909 1.962 62.179 3.857 0.57 310298. 0.4701 34.64 0.2540 0.5682 0.0623 0.0278 2.167 17.076 13.333 1616.211 1.929 59.306 3.742 0.57 310644. 0.4454 37.53 0.2752 0.5970 0.0592 0.0273 2.123 16.727 12.666 1583.195 1.890 56.338 3.629 0.57 311008. 0.4210 40.41 0.2964 0.6231 0.0559 0.0266 2.071 16.320 11.978 1544.674 1.844 53.279 3.517 0.57 311388. 0.3968 43.30 0.3175 0.6467 0.0526 0.0258 2.012 15.853 11.271 1500.467 1.791 50.133 3.407 0.57 311785. 0.3729 46.19 0.3387 0.6677 0.0493 0.0250 1.945 15.324 10.545 1450.396 1.731 46.906 3.298 0.57 312199. 0.3491 49.07 0.3599 0.6860 0.0458 0.0240 1.870 14.731 9.802 1394.301 1.664 43.600 3.189 0.57 312631. 0.3254 51.96 0.3810 0.7014 0.0422 0.0229 1.786 14.073 9.042 1332.023 1.590 40.221 3.079 0.58 313080. 0.3018 54.85 0.4022 0.7136 0.0386 0.0218 1.694 13.348 8.267 1263.422 1.508 36.773 2.968 0.58 313548. 0.2782 57.73 0.4234 0.7223 0.0349 0.0205 1.594 12.556 7.478 1188.378 1.419 33.260 2.854 0.58 314033. 0.2544 60.62 0.4445 0.7269 0.0312 0.0191 1.484 11.694 6.675 1106.793 1.321 29.689 2.735 0.58 314537. 0.2304 63.51 0.4657 0.7265 0.0274 0.0175 1.366 10.762 5.860 1018.597 1.216 26.065 2.609 0.58 315059. 0.2059 66.39 0.4869 0.7195 0.0235 0.0159 1.239 9.760 5.035 923.757 1.103 22.394 2.472 0.58 315600. 0.1808 69.28 0.5081 0.7037 0.0196 0.0142 1.103 8.688 4.200 822.283 0.982 18.683 2.317 0.58 316159. 0.1548 72.17 0.5292 0.6749 0.0157 0.0123 0.958 7.546 3.359 714.239 0.853 14.941 2.133 0.58 316736. 0.1274 75.05 0.5504 0.6253 0.0117 0.0103 0.804 6.337 2.513 599.753 0.716 11.177 1.900 0.58 317332. 0.0982 77.94 0.5716 0.5384 0.0078 0.0083 0.642 5.061 1.664 479.017 0.572 7.402 1.576 0.58 317945. 0.0663 80.83 0.5927 0.3720 0.0038 0.0061 0.472 3.721 0.815 352.215 0.420 3.626 1.050 0.58 318569. 0.0309 83.71 0.6139 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 0.0923 0.0291 3.223 22.569 25.025 2403.185 2.550 111.310 4.723 0.64 345880. 0.7702 3.25 0.0212 0.0654 0.0906 0.0293 3.251 22.770 24.551 2424.552 2.573 109.204 4.593 0.64 346091. 0.7418 6.50 0.0424 0.1272 0.0887 0.0295 3.276 22.939 24.046 2442.565 2.592 106.956 4.465 0.64 346317. 0.7138 9.75 0.0635 0.1855 0.0868 0.0297 3.295 23.072 23.508 2456.713 2.607 104.566 4.340 0.64 346557. 0.6860 13.00 0.0847 0.2403 0.0846 0.0298 3.308 23.164 22.938 2466.488 2.617 102.028 4.218 0.64 346813. 0.6586 16.24 0.1059 0.2919 0.0824 0.0299 3.314 23.210 22.334 2471.379 2.622 99.340 4.099 0.64 347085. 0.6314 19.49 0.1271 0.3403 0.0801 0.0299 3.313 23.205 21.695 2470.872 2.622 96.499 3.982 0.64 347373. 0.6047 22.74 0.1482 0.3857 0.0776 0.0298 3.305 23.145 21.022 2464.493 2.615 93.505 3.869 0.64 347677. 0.5782 25.99 0.1694 0.4282 0.0750 0.0297 3.288 23.026 20.315 2451.833 2.601 90.361 3.758 0.64 347999. 0.5522 29.24 0.1906 0.4679 0.0722 0.0294 3.262 22.845 19.575 2432.553 2.581 87.071 3.650 0.64 348337. 0.5264 32.49 0.2118 0.5048 0.0694 0.0291 3.227 22.599 18.804 2406.347 2.553 83.641 3.544 0.64 348693. 0.5010 35.74 0.2330 0.5391 0.0664 0.0287 3.182 22.285 18.003 2372.929 2.518 80.077 3.441 0.64 349067. 0.4760 38.99 0.2541 0.5709 0.0634 0.0282 3.127 21.901 17.173 2332.025 2.474 76.384 3.340 0.64 349460. 0.4512 42.24 0.2753 0.6001 0.0602 0.0276 3.062 21.444 16.315 2283.366 2.423 72.568 3.241 0.65 349870. 0.4267 45.48 0.2965 0.6267 0.0569 0.0269 2.986 20.912 15.430 2226.688 2.363 68.634 3.143 0.65 350300. 0.4025 48.73 0.3177 0.6509 0.0536 0.0262 2.899 20.302 14.521 2161.734 2.294 64.588 3.047 0.65 350749. 0.3785 51.98 0.3388 0.6725 0.0501 0.0253 2.800 19.612 13.587 2088.257 2.216 60.435 2.951 0.65 351217. 0.3546 55.23 0.3600 0.6915 0.0466 0.0243 2.690 18.839 12.631 2006.020 2.128 56.181 2.856 0.65 351704. 0.3309 58.48 0.3812 0.7076 0.0430 0.0232 2.568 17.983 11.653 1914.804 2.032 51.831 2.760 0.65 352212. 0.3071 61.73 0.4024 0.7208 0.0393 0.0220 2.433 17.040 10.655 1814.412 1.925 47.392 2.663 0.65 352739. 0.2834 64.98 0.4236 0.7305 0.0356 0.0206 2.286 16.009 9.638 1704.665 1.809 42.869 2.564 0.65 353287. 0.2595 68.23 0.4447 0.7362 0.0318 0.0192 2.126 14.889 8.604 1585.423 1.682 38.269 2.461 0.65 353855. 0.2354 71.48 0.4659 0.7371 0.0279 0.0176 1.953 13.679 7.554 1456.588 1.545 33.600 2.352 0.65 354444. 0.2107 74.72 0.4871 0.7316 0.0240 0.0159 1.768 12.379 6.490 1318.112 1.399 28.869 2.233 0.65 355053. 0.1855 77.97 0.5083 0.7176 0.0200 0.0142 1.569 10.988 5.415 1170.008 1.241 24.087 2.099 0.65 355683. 0.1592 81.22 0.5294 0.6909 0.0160 0.0122 1.358 9.508 4.331 1012.373 1.074 19.262 1.940 0.65 356334. 0.1316 84.47 0.5506 0.6436 0.0120 0.0102 1.134 7.939 3.239 845.393 0.897 14.409 1.738 0.65 357005. 0.1020 87.72 0.5718 0.5589 0.0079 0.0081 0.898 6.286 2.145 669.349 0.710 9.540 1.453 0.65 357695. 0.0694 90.97 0.5930 0.3918 0.0039 0.0059 0.650 4.550 1.049 484.516 0.514 4.668 0.982 0.65 358399. 0.0328 94.22 0.6142 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 0.0941 0.0297 4.523 28.505 31.482 3372.471 3.220 140.032 4.234 0.71 384256. 0.7744 3.60 0.0211 0.0650 0.0924 0.0300 4.561 28.749 30.895 3401.325 3.248 137.423 4.120 0.71 384492. 0.7465 7.20 0.0422 0.1265 0.0905 0.0302 4.594 28.954 30.269 3425.623 3.271 134.634 4.008 0.71 384745. 0.7188 10.80 0.0634 0.1846 0.0885 0.0304 4.619 29.115 29.601 3444.619 3.289 131.665 3.898 0.71 385014. 0.6913 14.40 0.0845 0.2393 0.0864 0.0305 4.637 29.224 28.891 3457.583 3.302 128.509 3.790 0.71 385300. 0.6641 18.00 0.1056 0.2908 0.0841 0.0305 4.645 29.277 28.139 3463.758 3.308 125.162 3.685 0.71 385603. 0.6372 21.60 0.1267 0.3392 0.0817 0.0305 4.643 29.265 27.343 3462.392 3.306 121.621 3.582 0.71 385925. 0.6106 25.20 0.1479 0.3847 0.0792 0.0305 4.630 29.184 26.503 3452.774 3.297 117.886 3.482 0.71 386265. 0.5843 28.81 0.1690 0.4273 0.0766 0.0303 4.605 29.028 25.620 3434.308 3.280 113.959 3.384 0.72 386623. 0.5583 32.41 0.1901 0.4671 0.0738 0.0300 4.568 28.793 24.696 3406.516 3.253 109.847 3.288 0.72 387001. 0.5327 36.01 0.2112 0.5043 0.0709 0.0297 4.518 28.475 23.731 3368.982 3.217 105.557 3.195 0.72 387397. 0.5074 39.61 0.2324 0.5389 0.0679 0.0293 4.454 28.073 22.728 3321.324 3.172 101.096 3.104 0.72 387814. 0.4824 43.21 0.2535 0.5710 0.0648 0.0288 4.376 27.581 21.689 3263.174 3.116 96.472 3.015 0.72 388251. 0.4577 46.81 0.2746 0.6007 0.0616 0.0282 4.283 26.998 20.614 3194.176 3.050 91.691 2.927 0.72 388708. 0.4332 50.41 0.2957 0.6279 0.0583 0.0275 4.176 26.320 19.506 3113.977 2.974 86.761 2.841 0.72 389186. 0.4090 54.01 0.3169 0.6526 0.0549 0.0267 4.053 25.545 18.365 3022.226 2.886 81.689 2.756 0.72 389684. 0.3850 57.61 0.3380 0.6749 0.0514 0.0257 3.914 24.669 17.195 2918.587 2.787 76.482 2.672 0.72 390204. 0.3612 61.21 0.3591 0.6946 0.0478 0.0247 3.759 23.689 15.995 2802.737 2.676 71.146 2.588 0.72 390746. 0.3375 64.81 0.3802 0.7117 0.0441 0.0236 3.586 22.604 14.768 2674.379 2.554 65.688 2.505 0.72 391309. 0.3138 68.41 0.4014 0.7258 0.0404 0.0223 3.397 21.412 13.515 2533.244 2.419 60.117 2.420 0.72 391894. 0.2900 72.01 0.4225 0.7366 0.0366 0.0210 3.190 20.109 12.239 2379.086 2.272 54.439 2.333 0.72 392502. 0.2661 75.61 0.4436 0.7437 0.0327 0.0195 2.966 18.694 10.940 2211.720 2.112 48.662 2.244 0.72 393132. 0.2419 79.22 0.4647 0.7462 0.0288 0.0179 2.724 17.167 9.621 2031.033 1.939 42.796 2.149 0.72 393784. 0.2173 82.82 0.4859 0.7427 0.0248 0.0162 2.463 15.527 8.285 1837.006 1.754 36.851 2.046 0.72 394459. 0.1919 86.42 0.5070 0.7310 0.0207 0.0144 2.185 13.775 6.933 1629.723 1.556 30.837 1.929 0.72 395157. 0.1656 90.02 0.5281 0.7072 0.0166 0.0124 1.890 11.913 5.569 1409.413 1.346 24.769 1.792 0.72 395878. 0.1379 93.62 0.5492 0.6638 0.0125 0.0104 1.578 9.944 4.195 1176.467 1.123 18.660 1.617 0.72 396621. 0.1080 97.22 0.5703 0.5846 0.0084 0.0082 1.249 7.873 2.817 931.458 0.889 12.528 1.372 0.73 397385. 0.0750 100.82 0.5915 0.4266 0.0043 0.0060 0.905 5.705 1.437 675.020 0.645 6.390 0.965 0.73 398164. 0.0377 104.42 0.6126 0.0116 0.0001 0.0035 0.537 3.385 0.022 400.483 0.382 0.100 0.025 0.73 398743. 0.0001 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 0.0962 0.0313 6.328 36.260 38.951 4718.940 4.097 173.255 3.744 0.79 422606. 0.7617 3.97 0.0212 0.0636 0.0945 0.0314 6.363 36.461 38.238 4745.181 4.119 170.082 3.655 0.79 422869. 0.7368 7.93 0.0423 0.1241 0.0926 0.0316 6.391 36.619 37.473 4765.690 4.137 166.681 3.566 0.79 423151. 0.7117 11.90 0.0635 0.1815 0.0906 0.0317 6.410 36.726 36.657 4779.603 4.149 163.051 3.479 0.79 423450. 0.6866 15.87 0.0846 0.2360 0.0884 0.0317 6.418 36.775 35.788 4786.042 4.155 159.185 3.392 0.79 423769. 0.6614 19.84 0.1058 0.2875 0.0861 0.0317 6.416 36.760 34.864 4784.076 4.153 155.077 3.305 0.79 424107. 0.6362 23.80 0.1270 0.3361 0.0837 0.0316 6.400 36.673 33.886 4772.721 4.143 150.724 3.220 0.79 424465. 0.6111 27.77 0.1481 0.3818 0.0812 0.0315 6.371 36.506 32.852 4751.011 4.124 146.124 3.136 0.79 424843. 0.5860 31.74 0.1693 0.4249 0.0785 0.0313 6.327 36.253 31.763 4718.104 4.096 141.282 3.053 0.79 425242. 0.5610 35.71 0.1904 0.4652 0.0756 0.0310 6.267 35.909 30.621 4673.271 4.057 136.203 2.972 0.79 425662. 0.5361 39.67 0.2116 0.5029 0.0727 0.0306 6.190 35.468 29.429 4615.883 4.007 130.898 2.892 0.79 426103. 0.5114 43.64 0.2327 0.5381 0.0696 0.0301 6.095 34.926 28.187 4545.353 3.946 125.377 2.813 0.79 426566. 0.4868 47.61 0.2539 0.5708 0.0665 0.0296 5.982 34.278 26.900 4461.095 3.873 119.649 2.735 0.79 427051. 0.4624 51.58 0.2751 0.6010 0.0632 0.0289 5.850 33.521 25.568 4362.520 3.787 113.724 2.658 0.79 427559. 0.4382 55.54 0.2962 0.6288 0.0598 0.0282 5.698 32.649 24.193 4249.042 3.689 107.612 2.583 0.79 428089. 0.4141 59.51 0.3174 0.6542 0.0563 0.0273 5.525 31.658 22.779 4120.102 3.577 101.319 2.508 0.79 428642. 0.3901 63.48 0.3385 0.6771 0.0527 0.0263 5.331 30.545 21.326 3975.262 3.451 94.857 2.433 0.79 429219. 0.3663 67.44 0.3597 0.6975 0.0490 0.0253 5.115 29.306 19.836 3814.007 3.311 88.232 2.359 0.79 429819. 0.3425 71.41 0.3809 0.7152 0.0452 0.0241 4.876 27.938 18.312 3635.988 3.156 81.454 2.284 0.79 430443. 0.3187 75.38 0.4020 0.7299 0.0414 0.0228 4.614 26.440 16.756 3440.942 2.987 74.531 2.209 0.79 431091. 0.2947 79.35 0.4232 0.7413 0.0375 0.0214 4.330 24.809 15.169 3228.774 2.803 67.474 2.131 0.79 431763. 0.2706 83.31 0.4443 0.7486 0.0335 0.0199 4.022 23.048 13.555 2999.490 2.604 60.291 2.050 0.79 432460. 0.2460 87.28 0.4655 0.7510 0.0294 0.0182 3.692 21.156 11.914 2753.245 2.390 52.994 1.963 0.79 433182. 0.2208 91.25 0.4867 0.7468 0.0253 0.0165 3.340 19.136 10.251 2490.392 2.162 45.594 1.867 0.79 433928. 0.1948 95.22 0.5078 0.7334 0.0212 0.0147 2.966 16.993 8.567 2211.467 1.920 38.106 1.757 0.80 434700. 0.1676 99.18 0.5290 0.7064 0.0170 0.0127 2.571 14.732 6.867 1917.260 1.664 30.545 1.625 0.80 435496. 0.1388 103.15 0.5501 0.6572 0.0127 0.0107 2.157 12.362 5.155 1608.834 1.397 22.929 1.453 0.80 436316. 0.1076 107.12 0.5713 0.5683 0.0085 0.0085 1.727 9.893 3.435 1287.520 1.118 15.279 1.210 0.80 437160. 0.0731 111.08 0.5925 0.3961 0.0042 0.0063 1.280 7.336 1.712 954.724 0.829 7.615 0.813 0.80 438020. 0.0347 115.05 0.6136 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 0.0987 0.0354 9.289 48.791 47.534 6927.083 5.512 211.430 3.112 0.86 460922. 0.6995 4.33 0.0212 0.0582 0.0969 0.0353 9.279 48.735 46.689 6919.121 5.506 207.673 3.061 0.86 461212. 0.6817 8.67 0.0424 0.1143 0.0950 0.0352 9.257 48.620 45.780 6902.853 5.493 203.631 3.008 0.86 461523. 0.6635 13.00 0.0636 0.1685 0.0930 0.0351 9.223 48.442 44.806 6877.490 5.473 199.297 2.955 0.86 461855. 0.6448 17.34 0.0848 0.2205 0.0908 0.0349 9.176 48.193 43.764 6842.192 5.445 194.664 2.901 0.86 462207. 0.6256 21.67 0.1060 0.2705 0.0885 0.0347 9.114 47.869 42.654 6796.162 5.408 189.727 2.847 0.86 462581. 0.6061 26.01 0.1272 0.3183 0.0861 0.0344 9.037 47.463 41.474 6738.549 5.362 184.478 2.792 0.86 462977. 0.5861 30.34 0.1483 0.3639 0.0835 0.0340 8.943 46.970 40.224 6668.514 5.307 178.918 2.736 0.86 463395. 0.5656 34.68 0.1695 0.4074 0.0808 0.0336 8.831 46.384 38.906 6585.307 5.240 173.052 2.680 0.86 463836. 0.5449 39.01 0.1907 0.4486 0.0779 0.0331 8.701 45.701 37.520 6488.295 5.163 166.889 2.623 0.86 464301. 0.5237 43.35 0.2119 0.4875 0.0749 0.0325 8.552 44.916 36.070 6376.875 5.075 160.440 2.566 0.86 464788. 0.5023 47.68 0.2331 0.5242 0.0717 0.0319 8.382 44.025 34.559 6250.370 4.974 153.718 2.508 0.86 465299. 0.4806 52.02 0.2543 0.5586 0.0685 0.0312 8.191 43.022 32.989 6108.079 4.861 146.735 2.450 0.86 465835. 0.4587 56.35 0.2755 0.5907 0.0651 0.0304 7.978 41.904 31.363 5949.255 4.734 139.502 2.391 0.86 466395. 0.4365 60.69 0.2967 0.6204 0.0616 0.0295 7.742 40.664 29.684 5773.212 4.594 132.033 2.332 0.86 466979. 0.4142 65.02 0.3179 0.6478 0.0580 0.0285 7.482 39.297 27.953 5579.220 4.440 124.337 2.273 0.86 467589. 0.3917 69.36 0.3391 0.6726 0.0543 0.0274 7.197 37.802 26.175 5366.885 4.271 116.428 2.212 0.86 468223. 0.3689 73.69 0.3603 0.6943 0.0505 0.0262 6.892 36.200 24.351 5139.449 4.090 108.314 2.149 0.86 468884. 0.3457 78.03 0.3815 0.7125 0.0467 0.0250 6.565 34.482 22.484 4895.532 3.896 100.007 2.083 0.86 469570. 0.3220 82.36 0.4026 0.7262 0.0427 0.0237 6.222 32.679 20.574 4639.563 3.692 91.515 2.011 0.86 470282. 0.2974 86.69 0.4238 0.7355 0.0387 0.0223 5.854 30.749 18.627 4365.532 3.474 82.851 1.935 0.86 471021. 0.2723 91.03 0.4450 0.7396 0.0345 0.0208 5.462 28.690 16.643 4073.305 3.241 74.029 1.853 0.87 471786. 0.2465 95.36 0.4662 0.7370 0.0304 0.0192 5.047 26.509 14.627 3763.634 2.995 65.063 1.763 0.87 472578. 0.2198 99.70 0.4874 0.7256 0.0261 0.0175 4.610 24.214 12.582 3437.717 2.736 55.966 1.660 0.87 473397. 0.1920 104.03 0.5086 0.7021 0.0218 0.0158 4.153 21.816 10.512 3097.250 2.465 46.758 1.539 0.87 474243. 0.1627 108.37 0.5298 0.6613 0.0175 0.0140 3.680 19.327 8.421 2743.948 2.184 37.458 1.392 0.87 475115. 0.1317 112.70 0.5510 0.5946 0.0131 0.0121 3.192 16.764 6.315 2380.058 1.894 28.090 1.203 0.87 476014. 0.0986 117.04 0.5722 0.4868 0.0087 0.0102 2.693 14.144 4.200 2008.015 1.598 18.682 0.949 0.87 476939. 0.0634 121.37 0.5934 0.3083 0.0043 0.0083 2.186 11.482 2.082 1630.166 1.297 9.261 0.579 0.87 477880. 0.0273 125.71 0.6146 -0.0223 -0.0002 0.0062 1.642 8.623 -0.109 1224.250 0.974 -0.485 -0.040 0.87 478481. 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 0.1003 0.0428 14.285 69.258 56.731 10652.268 7.825 252.338 2.416 0.93 499247. 0.5931 4.72 0.0213 0.0494 0.0987 0.0426 14.223 68.959 55.816 10606.190 7.791 248.270 2.387 0.93 499560. 0.5813 9.44 0.0426 0.0976 0.0970 0.0423 14.135 68.533 54.817 10540.809 7.743 243.828 2.359 0.93 499896. 0.5693 14.16 0.0639 0.1447 0.0950 0.0420 14.021 67.978 53.733 10455.355 7.680 239.004 2.331 0.93 500255. 0.5570 18.88 0.0852 0.1907 0.0930 0.0415 13.879 67.288 52.560 10349.268 7.602 233.786 2.303 0.93 500639. 0.5444 23.60 0.1065 0.2355 0.0907 0.0410 13.708 66.462 51.296 10222.140 7.509 228.163 2.276 0.93 501047. 0.5314 28.32 0.1278 0.2792 0.0883 0.0404 13.509 65.497 49.939 10073.744 7.400 222.128 2.248 0.93 501481. 0.5180 33.04 0.1491 0.3217 0.0858 0.0398 13.282 64.393 48.489 9904.024 7.275 215.678 2.221 0.93 501940. 0.5041 37.76 0.1704 0.3629 0.0830 0.0390 13.026 63.153 46.947 9713.252 7.135 208.821 2.192 0.93 502424. 0.4897 42.48 0.1917 0.4029 0.0802 0.0381 12.742 61.779 45.317 9501.949 6.980 201.570 2.163 0.93 502935. 0.4747 47.20 0.2130 0.4414 0.0771 0.0372 12.432 60.275 43.602 9270.613 6.810 193.940 2.133 0.93 503471. 0.4592 51.92 0.2343 0.4785 0.0739 0.0362 12.095 58.642 41.805 9019.497 6.625 185.950 2.102 0.93 504034. 0.4431 56.64 0.2556 0.5141 0.0706 0.0351 11.732 56.881 39.932 8748.602 6.426 177.616 2.070 0.93 504624. 0.4265 61.36 0.2769 0.5480 0.0672 0.0340 11.342 54.990 37.984 8457.818 6.213 168.953 2.037 0.93 505241. 0.4092 66.08 0.2982 0.5801 0.0636 0.0327 10.926 52.971 35.966 8147.214 5.985 159.979 2.002 0.93 505884. 0.3914 70.80 0.3195 0.6103 0.0599 0.0314 10.483 50.823 33.883 7816.856 5.742 150.713 1.966 0.93 506555. 0.3731 75.53 0.3408 0.6384 0.0561 0.0300 10.013 48.545 31.738 7466.453 5.485 141.172 1.928 0.93 507254. 0.3541 80.25 0.3621 0.6642 0.0522 0.0285 9.515 46.134 29.535 7095.592 5.212 131.373 1.888 0.93 507981. 0.3345 84.97 0.3834 0.6856 0.0482 0.0270 9.013 43.697 27.275 6720.795 4.937 121.320 1.841 0.94 508735. 0.3134 89.69 0.4047 0.7018 0.0442 0.0255 8.506 41.238 24.961 6342.600 4.659 111.029 1.785 0.94 509518. 0.2907 94.41 0.4260 0.7044 0.0400 0.0242 8.073 39.140 22.589 6019.905 4.422 100.478 1.702 0.94 510330. 0.2637 99.13 0.4473 0.6989 0.0357 0.0228 7.629 36.990 20.172 5689.208 4.179 89.727 1.608 0.94 511170. 0.2355 103.85 0.4686 0.6840 0.0313 0.0215 7.172 34.771 17.716 5347.904 3.928 78.801 1.503 0.94 512039. 0.2062 108.57 0.4899 0.6576 0.0269 0.0201 6.703 32.498 15.226 4998.308 3.672 67.724 1.382 0.94 512937. 0.1757 113.29 0.5112 0.6166 0.0225 0.0186 6.226 30.184 12.708 4642.418 3.410 56.524 1.242 0.94 513864. 0.1443 118.01 0.5325 0.5571 0.0180 0.0172 5.745 27.852 10.170 4283.837 3.147 45.238 1.077 0.94 514820. 0.1119 122.73 0.5539 0.4741 0.0135 0.0158 5.263 25.516 7.624 3924.550 2.883 33.910 0.881 0.94 515805. 0.0793 127.45 0.5752 0.3609 0.0090 0.0143 4.783 23.191 5.080 3566.856 2.620 22.595 0.646 0.94 516817. 0.0475 132.17 0.5965 0.2087 0.0045 0.0129 4.307 20.882 2.551 3211.750 2.359 11.346 0.360 0.94 517850. 0.0188 136.89 0.6178 0.0000 0.0000 0.0114 3.805 18.447 0.000 2837.306 2.084 0.002 0.000 0.95 518780. 0.0000