18.1x12 (181x12.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 0.1078 0.0475 0.007 0.468 0.369 5.533 0.053 1.639 30.215 0.07 37985. 0.5947 0.48 0.0282 0.0622 0.1065 0.0482 0.008 0.475 0.364 5.624 0.054 1.621 29.385 0.07 38015. 0.5750 0.97 0.0564 0.1209 0.1051 0.0490 0.008 0.483 0.360 5.713 0.055 1.600 28.554 0.07 38049. 0.5551 1.45 0.0846 0.1762 0.1036 0.0497 0.008 0.490 0.354 5.798 0.055 1.577 27.727 0.07 38085. 0.5351 1.93 0.1127 0.2279 0.1020 0.0504 0.008 0.497 0.349 5.878 0.056 1.551 26.906 0.07 38125. 0.5151 2.42 0.1409 0.2763 0.1001 0.0510 0.008 0.503 0.342 5.951 0.057 1.523 26.095 0.07 38169. 0.4950 2.90 0.1691 0.3214 0.0981 0.0516 0.008 0.508 0.335 6.014 0.057 1.492 25.294 0.07 38217. 0.4749 3.38 0.1973 0.3633 0.0958 0.0520 0.008 0.513 0.328 6.066 0.058 1.458 24.505 0.07 38268. 0.4548 3.86 0.2255 0.4020 0.0934 0.0524 0.008 0.516 0.319 6.104 0.058 1.420 23.729 0.07 38324. 0.4347 4.35 0.2537 0.4377 0.0907 0.0525 0.008 0.518 0.310 6.126 0.058 1.380 22.966 0.07 38383. 0.4146 4.83 0.2818 0.4705 0.0877 0.0526 0.008 0.518 0.300 6.127 0.059 1.335 22.216 0.07 38447. 0.3946 5.31 0.3100 0.5004 0.0846 0.0524 0.008 0.516 0.289 6.107 0.058 1.286 21.479 0.07 38514. 0.3745 5.80 0.3382 0.5274 0.0811 0.0520 0.008 0.512 0.277 6.062 0.058 1.234 20.754 0.07 38586. 0.3543 6.28 0.3664 0.5517 0.0774 0.0514 0.008 0.506 0.265 5.991 0.057 1.177 20.038 0.07 38662. 0.3342 6.76 0.3946 0.5731 0.0734 0.0506 0.008 0.498 0.251 5.894 0.056 1.117 19.329 0.07 38743. 0.3141 7.25 0.4228 0.5917 0.0693 0.0495 0.008 0.488 0.237 5.772 0.055 1.054 18.624 0.07 38828. 0.2939 7.73 0.4510 0.6072 0.0650 0.0483 0.008 0.475 0.222 5.625 0.054 0.988 17.918 0.07 38917. 0.2738 8.21 0.4791 0.6195 0.0605 0.0468 0.007 0.461 0.207 5.454 0.052 0.920 17.206 0.07 39010. 0.2537 8.70 0.5073 0.6283 0.0559 0.0451 0.007 0.444 0.191 5.259 0.050 0.850 16.481 0.07 39107. 0.2336 9.18 0.5355 0.6332 0.0511 0.0432 0.007 0.426 0.175 5.040 0.048 0.778 15.735 0.07 39209. 0.2133 9.66 0.5637 0.6336 0.0463 0.0412 0.006 0.406 0.158 4.798 0.046 0.704 14.959 0.07 39315. 0.1929 10.14 0.5919 0.6289 0.0413 0.0389 0.006 0.383 0.141 4.532 0.043 0.628 14.140 0.07 39425. 0.1723 10.63 0.6201 0.6178 0.0363 0.0364 0.006 0.359 0.124 4.243 0.041 0.552 13.259 0.07 39540. 0.1514 11.11 0.6482 0.5988 0.0312 0.0337 0.005 0.332 0.107 3.932 0.038 0.474 12.293 0.07 39658. 0.1301 11.59 0.6764 0.5695 0.0260 0.0309 0.005 0.304 0.089 3.599 0.034 0.395 11.205 0.07 39781. 0.1083 12.08 0.7046 0.5264 0.0208 0.0278 0.004 0.274 0.071 3.244 0.031 0.316 9.941 0.07 39908. 0.0859 12.56 0.7328 0.4634 0.0156 0.0246 0.004 0.242 0.053 2.869 0.027 0.237 8.416 0.07 40040. 0.0630 13.04 0.7610 0.3708 0.0103 0.0212 0.003 0.209 0.035 2.475 0.024 0.157 6.485 0.07 40175. 0.0395 13.53 0.7892 0.2298 0.0052 0.0177 0.003 0.174 0.018 2.064 0.020 0.078 3.876 0.07 40315. 0.0167 14.01 0.8174 0.0005 0.0000 0.0140 0.002 0.138 0.000 1.637 0.016 0.000 0.008 0.07 40456. 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 0.1082 0.0432 0.054 1.701 1.481 40.246 0.192 6.586 16.687 0.14 75969. 0.6583 0.97 0.0284 0.0690 0.1070 0.0440 0.055 1.734 1.464 41.023 0.196 6.512 16.186 0.14 76030. 0.6349 1.94 0.0567 0.1337 0.1056 0.0448 0.056 1.766 1.445 41.787 0.200 6.429 15.688 0.14 76097. 0.6114 2.92 0.0851 0.1943 0.1041 0.0456 0.057 1.797 1.425 42.524 0.203 6.337 15.195 0.14 76171. 0.5880 3.89 0.1134 0.2508 0.1025 0.0463 0.058 1.827 1.402 43.219 0.206 6.235 14.710 0.14 76252. 0.5646 4.86 0.1418 0.3033 0.1006 0.0470 0.059 1.853 1.376 43.858 0.209 6.122 14.234 0.14 76340. 0.5414 5.83 0.1702 0.3521 0.0986 0.0476 0.060 1.877 1.348 44.422 0.212 5.998 13.768 0.14 76436. 0.5183 6.81 0.1985 0.3972 0.0963 0.0481 0.060 1.897 1.318 44.894 0.214 5.861 13.313 0.14 76540. 0.4954 7.78 0.2269 0.4388 0.0938 0.0485 0.061 1.912 1.284 45.253 0.216 5.711 12.869 0.14 76652. 0.4727 8.75 0.2552 0.4771 0.0911 0.0488 0.061 1.922 1.247 45.478 0.217 5.547 12.437 0.14 76772. 0.4502 9.72 0.2836 0.5121 0.0882 0.0488 0.061 1.925 1.207 45.542 0.217 5.367 12.016 0.14 76900. 0.4279 10.69 0.3120 0.5442 0.0850 0.0487 0.061 1.920 1.162 45.422 0.217 5.170 11.607 0.14 77037. 0.4057 11.67 0.3403 0.5733 0.0815 0.0484 0.060 1.906 1.115 45.100 0.215 4.958 11.209 0.14 77183. 0.3836 12.64 0.3687 0.5996 0.0777 0.0478 0.060 1.883 1.063 44.565 0.213 4.729 10.821 0.14 77337. 0.3617 13.61 0.3970 0.6231 0.0737 0.0470 0.059 1.852 1.009 43.817 0.209 4.487 10.442 0.14 77500. 0.3400 14.58 0.4254 0.6438 0.0695 0.0460 0.057 1.811 0.952 42.856 0.205 4.232 10.070 0.14 77671. 0.3184 15.56 0.4538 0.6617 0.0652 0.0447 0.056 1.762 0.892 41.687 0.199 3.967 9.703 0.15 77851. 0.2970 16.53 0.4821 0.6766 0.0607 0.0432 0.054 1.704 0.830 40.310 0.192 3.691 9.338 0.15 78039. 0.2758 17.50 0.5105 0.6883 0.0560 0.0415 0.052 1.637 0.766 38.730 0.185 3.407 8.971 0.15 78236. 0.2546 18.47 0.5388 0.6964 0.0512 0.0396 0.050 1.561 0.701 36.948 0.176 3.116 8.600 0.15 78442. 0.2334 19.44 0.5672 0.7006 0.0463 0.0375 0.047 1.478 0.634 34.964 0.167 2.818 8.219 0.15 78656. 0.2121 20.42 0.5956 0.7001 0.0413 0.0351 0.044 1.385 0.565 32.780 0.157 2.515 7.822 0.15 78879. 0.1907 21.39 0.6239 0.6939 0.0363 0.0326 0.041 1.285 0.496 30.399 0.145 2.206 7.400 0.15 79111. 0.1689 22.36 0.6523 0.6803 0.0311 0.0298 0.037 1.176 0.426 27.823 0.133 1.893 6.940 0.15 79351. 0.1468 23.33 0.6806 0.6568 0.0259 0.0269 0.034 1.059 0.355 25.057 0.120 1.578 6.421 0.15 79600. 0.1240 24.30 0.7090 0.6193 0.0207 0.0237 0.030 0.934 0.283 22.107 0.106 1.260 5.812 0.15 79857. 0.1003 25.28 0.7374 0.5604 0.0155 0.0204 0.025 0.802 0.212 18.983 0.091 0.941 5.057 0.15 80123. 0.0754 26.25 0.7657 0.4662 0.0102 0.0168 0.021 0.663 0.140 15.699 0.075 0.624 4.051 0.15 80397. 0.0492 27.22 0.7941 0.3057 0.0051 0.0132 0.016 0.519 0.069 12.270 0.059 0.308 2.562 0.15 80679. 0.0219 28.19 0.8224 -0.0078 -0.0001 0.0093 0.012 0.367 -0.001 8.691 0.041 -0.005 -0.063 0.15 80958. 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 0.1086 0.0415 0.175 3.679 3.344 130.564 0.416 14.875 11.618 0.22 113951. 0.6887 1.46 0.0284 0.0721 0.1074 0.0423 0.179 3.755 3.307 133.269 0.424 14.709 11.255 0.22 114042. 0.6635 2.92 0.0568 0.1396 0.1061 0.0432 0.182 3.830 3.265 135.934 0.433 14.525 10.896 0.22 114143. 0.6383 4.38 0.0853 0.2026 0.1046 0.0440 0.186 3.902 3.219 138.512 0.441 14.319 10.541 0.22 114254. 0.6131 5.85 0.1137 0.2613 0.1029 0.0448 0.189 3.971 3.168 140.953 0.449 14.091 10.194 0.22 114376. 0.5882 7.31 0.1421 0.3157 0.1011 0.0455 0.192 4.035 3.111 143.201 0.456 13.838 9.854 0.22 114509. 0.5634 8.77 0.1705 0.3661 0.0990 0.0461 0.195 4.091 3.048 145.199 0.462 13.559 9.522 0.22 114654. 0.5390 10.23 0.1990 0.4126 0.0968 0.0467 0.197 4.138 2.979 146.882 0.468 13.251 9.200 0.22 114810. 0.5148 11.69 0.2274 0.4555 0.0943 0.0471 0.199 4.175 2.903 148.183 0.472 12.914 8.886 0.22 114979. 0.4909 13.15 0.2558 0.4949 0.0916 0.0473 0.200 4.199 2.820 149.023 0.474 12.543 8.583 0.22 115160. 0.4672 14.62 0.2842 0.5311 0.0886 0.0474 0.200 4.207 2.729 149.317 0.475 12.137 8.288 0.22 115353. 0.4438 16.08 0.3127 0.5641 0.0854 0.0473 0.200 4.197 2.629 148.980 0.474 11.693 8.003 0.22 115560. 0.4207 17.54 0.3411 0.5942 0.0819 0.0470 0.198 4.168 2.521 147.947 0.471 11.212 7.728 0.22 115779. 0.3977 19.00 0.3695 0.6215 0.0781 0.0464 0.196 4.119 2.405 146.187 0.465 10.696 7.461 0.22 116011. 0.3750 20.46 0.3979 0.6460 0.0741 0.0457 0.193 4.048 2.281 143.689 0.457 10.147 7.201 0.22 116256. 0.3526 21.92 0.4264 0.6678 0.0699 0.0446 0.188 3.957 2.152 140.459 0.447 9.571 6.948 0.22 116514. 0.3304 23.39 0.4548 0.6869 0.0655 0.0434 0.183 3.846 2.017 136.504 0.435 8.969 6.700 0.22 116785. 0.3085 24.85 0.4832 0.7032 0.0610 0.0419 0.177 3.714 1.876 131.835 0.420 8.346 6.456 0.22 117069. 0.2867 26.31 0.5116 0.7165 0.0563 0.0402 0.170 3.563 1.732 126.456 0.403 7.704 6.212 0.22 117366. 0.2650 27.77 0.5401 0.7265 0.0515 0.0382 0.161 3.391 1.584 120.372 0.383 7.045 5.968 0.22 117676. 0.2435 29.23 0.5685 0.7329 0.0465 0.0361 0.152 3.200 1.432 113.589 0.362 6.371 5.719 0.22 117999. 0.2219 30.69 0.5969 0.7350 0.0415 0.0337 0.142 2.990 1.278 106.109 0.338 5.684 5.462 0.22 118335. 0.2002 32.16 0.6253 0.7318 0.0364 0.0311 0.131 2.759 1.121 97.941 0.312 4.986 5.191 0.22 118684. 0.1782 33.62 0.6538 0.7218 0.0313 0.0283 0.119 2.510 0.962 89.094 0.284 4.279 4.898 0.22 119046. 0.1557 35.08 0.6822 0.7025 0.0260 0.0253 0.107 2.242 0.802 79.583 0.253 3.565 4.568 0.22 119420. 0.1326 36.54 0.7106 0.6699 0.0208 0.0221 0.093 1.956 0.640 69.433 0.221 2.847 4.182 0.22 119808. 0.1085 38.00 0.7390 0.6161 0.0155 0.0186 0.079 1.653 0.478 58.678 0.187 2.128 3.698 0.22 120208. 0.0829 39.46 0.7675 0.5254 0.0103 0.0150 0.064 1.334 0.317 47.365 0.151 1.411 3.037 0.22 120621. 0.0554 40.92 0.7959 0.3596 0.0051 0.0113 0.048 1.002 0.157 35.550 0.113 0.699 2.004 0.22 121045. 0.0258 42.39 0.8243 -0.0086 -0.0001 0.0074 0.031 0.653 -0.002 23.179 0.074 -0.010 -0.046 0.22 121460. 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 0.1091 0.0407 0.407 6.411 5.972 303.377 0.724 26.562 8.928 0.29 151929. 0.7073 1.95 0.0285 0.0740 0.1079 0.0415 0.416 6.549 5.906 309.944 0.740 26.271 8.643 0.29 152051. 0.6810 3.90 0.0569 0.1431 0.1066 0.0424 0.424 6.686 5.833 316.425 0.755 25.946 8.361 0.29 152186. 0.6547 5.86 0.0854 0.2075 0.1051 0.0433 0.433 6.819 5.752 322.702 0.770 25.584 8.084 0.29 152335. 0.6285 7.81 0.1139 0.2674 0.1034 0.0441 0.441 6.945 5.661 328.655 0.785 25.180 7.813 0.29 152498. 0.6026 9.76 0.1423 0.3229 0.1016 0.0448 0.448 7.061 5.561 334.151 0.798 24.733 7.548 0.29 152676. 0.5770 11.71 0.1708 0.3742 0.0996 0.0454 0.455 7.164 5.449 339.048 0.809 24.238 7.290 0.29 152869. 0.5517 13.66 0.1993 0.4216 0.0973 0.0460 0.460 7.252 5.327 343.192 0.819 23.693 7.040 0.29 153078. 0.5267 15.61 0.2277 0.4653 0.0949 0.0464 0.465 7.320 5.192 346.419 0.827 23.092 6.797 0.29 153303. 0.5021 17.57 0.2562 0.5054 0.0922 0.0467 0.467 7.365 5.043 348.540 0.832 22.432 6.563 0.29 153546. 0.4778 19.52 0.2847 0.5421 0.0892 0.0468 0.468 7.382 4.880 349.350 0.834 21.708 6.336 0.29 153805. 0.4538 21.47 0.3131 0.5758 0.0859 0.0467 0.468 7.367 4.702 348.643 0.832 20.916 6.118 0.29 154081. 0.4301 23.42 0.3416 0.6065 0.0824 0.0464 0.464 7.317 4.509 346.264 0.827 20.057 5.907 0.29 154374. 0.4066 25.37 0.3701 0.6344 0.0786 0.0459 0.459 7.229 4.302 342.128 0.817 19.135 5.703 0.29 154685. 0.3835 27.32 0.3985 0.6596 0.0746 0.0451 0.451 7.104 4.081 336.214 0.803 18.154 5.506 0.29 155013. 0.3606 29.28 0.4270 0.6821 0.0703 0.0440 0.441 6.942 3.850 328.531 0.784 17.123 5.315 0.29 155358. 0.3381 31.23 0.4555 0.7020 0.0659 0.0428 0.428 6.743 3.608 319.096 0.762 16.047 5.128 0.29 155720. 0.3158 33.18 0.4839 0.7193 0.0613 0.0413 0.413 6.507 3.357 307.930 0.735 14.932 4.945 0.29 156100. 0.2937 35.13 0.5124 0.7336 0.0566 0.0395 0.396 6.235 3.099 295.046 0.704 13.783 4.763 0.29 156498. 0.2718 37.08 0.5409 0.7449 0.0518 0.0376 0.376 5.926 2.833 280.456 0.670 12.603 4.582 0.29 156912. 0.2500 39.03 0.5693 0.7528 0.0468 0.0354 0.354 5.582 2.562 264.169 0.631 11.396 4.399 0.29 157344. 0.2283 40.99 0.5978 0.7566 0.0418 0.0330 0.330 5.202 2.286 246.195 0.588 10.167 4.211 0.29 157793. 0.2064 42.94 0.6263 0.7556 0.0366 0.0304 0.304 4.787 2.005 226.550 0.541 8.918 4.014 0.29 158260. 0.1842 44.89 0.6547 0.7481 0.0314 0.0275 0.275 4.337 1.720 205.259 0.490 7.652 3.802 0.29 158744. 0.1617 46.84 0.6832 0.7320 0.0262 0.0244 0.245 3.853 1.433 182.361 0.435 6.375 3.565 0.29 159245. 0.1384 48.79 0.7117 0.7031 0.0209 0.0212 0.212 3.337 1.144 157.912 0.377 5.090 3.287 0.29 159763. 0.1140 50.74 0.7401 0.6536 0.0156 0.0177 0.177 2.789 0.855 131.997 0.315 3.803 2.938 0.30 160299. 0.0881 52.70 0.7686 0.5669 0.0104 0.0140 0.140 2.213 0.567 104.733 0.250 2.520 2.454 0.30 160851. 0.0599 54.65 0.7971 0.3996 0.0051 0.0102 0.102 1.611 0.280 76.255 0.182 1.247 1.668 0.30 161417. 0.0286 56.60 0.8255 -0.0133 -0.0001 0.0062 0.062 0.979 -0.005 46.343 0.111 -0.024 -0.054 0.30 161962. 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 0.1097 0.0403 0.787 9.921 9.381 586.870 1.121 41.725 7.250 0.36 189903. 0.7198 2.44 0.0285 0.0751 0.1085 0.0412 0.805 10.142 9.280 599.983 1.146 41.279 7.016 0.36 190055. 0.6928 4.88 0.0569 0.1452 0.1072 0.0421 0.822 10.361 9.168 612.938 1.171 40.778 6.784 0.36 190224. 0.6659 7.32 0.0854 0.2104 0.1057 0.0429 0.839 10.574 9.042 625.502 1.195 40.219 6.557 0.36 190410. 0.6391 9.76 0.1139 0.2711 0.1041 0.0437 0.855 10.775 8.902 637.430 1.217 39.595 6.334 0.36 190614. 0.6127 12.20 0.1424 0.3272 0.1023 0.0445 0.870 10.962 8.746 648.463 1.238 38.902 6.117 0.36 190836. 0.5865 14.64 0.1708 0.3791 0.1003 0.0452 0.883 11.128 8.573 658.314 1.257 38.134 5.907 0.36 191078. 0.5607 17.08 0.1993 0.4271 0.0980 0.0458 0.894 11.270 8.382 666.681 1.273 37.284 5.703 0.36 191340. 0.5352 19.52 0.2278 0.4712 0.0956 0.0462 0.903 11.381 8.172 673.232 1.286 36.348 5.505 0.36 191623. 0.5102 21.96 0.2563 0.5117 0.0929 0.0465 0.909 11.454 7.940 677.600 1.294 35.317 5.315 0.36 191926. 0.4855 24.40 0.2847 0.5489 0.0899 0.0466 0.911 11.485 7.686 679.377 1.298 34.186 5.131 0.36 192250. 0.4611 26.84 0.3132 0.5830 0.0866 0.0465 0.909 11.464 7.407 678.156 1.295 32.947 4.954 0.36 192596. 0.4371 29.28 0.3417 0.6141 0.0831 0.0462 0.903 11.387 7.104 673.621 1.287 31.600 4.784 0.36 192963. 0.4133 31.72 0.3702 0.6424 0.0793 0.0457 0.893 11.252 6.779 665.602 1.271 30.153 4.620 0.36 193352. 0.3899 34.16 0.3986 0.6682 0.0752 0.0449 0.877 11.056 6.433 654.051 1.249 28.614 4.461 0.36 193763. 0.3668 36.60 0.4271 0.6913 0.0710 0.0439 0.857 10.802 6.069 638.982 1.220 26.994 4.308 0.36 194195. 0.3440 39.04 0.4556 0.7118 0.0665 0.0426 0.832 10.488 5.689 620.434 1.185 25.303 4.159 0.36 194649. 0.3215 41.48 0.4841 0.7298 0.0619 0.0411 0.803 10.116 5.294 598.441 1.143 23.549 4.013 0.36 195125. 0.2993 43.92 0.5125 0.7450 0.0572 0.0393 0.768 9.687 4.888 573.035 1.094 21.741 3.869 0.36 195622. 0.2773 46.36 0.5410 0.7573 0.0523 0.0373 0.730 9.200 4.470 544.235 1.039 19.885 3.726 0.36 196141. 0.2554 48.80 0.5695 0.7663 0.0473 0.0351 0.687 8.656 4.044 512.061 0.978 17.986 3.582 0.36 196681. 0.2335 51.24 0.5980 0.7716 0.0422 0.0327 0.639 8.056 3.609 476.533 0.910 16.051 3.435 0.37 197243. 0.2115 53.69 0.6264 0.7723 0.0370 0.0300 0.587 7.399 3.167 437.682 0.836 14.085 3.282 0.37 197827. 0.1893 56.13 0.6549 0.7671 0.0318 0.0271 0.530 6.687 2.719 395.556 0.755 12.093 3.118 0.37 198432. 0.1666 58.57 0.6834 0.7537 0.0265 0.0240 0.470 5.920 2.267 350.232 0.669 10.082 2.936 0.37 199059. 0.1433 61.01 0.7118 0.7282 0.0212 0.0207 0.405 5.102 1.812 301.823 0.576 8.059 2.723 0.37 199708. 0.1188 63.45 0.7403 0.6830 0.0159 0.0172 0.336 4.235 1.356 250.498 0.478 6.032 2.456 0.37 200377. 0.0927 65.89 0.7688 0.6014 0.0105 0.0135 0.263 3.322 0.902 196.487 0.375 4.012 2.082 0.37 201068. 0.0641 68.33 0.7973 0.4377 0.0053 0.0096 0.188 2.368 0.451 140.062 0.267 2.007 1.461 0.37 201777. 0.0318 70.77 0.8257 0.0013 0.0000 0.0055 0.108 1.365 0.001 80.764 0.154 0.003 0.004 0.37 202456. 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 0.1104 0.0402 1.356 14.245 13.594 1011.238 1.609 60.466 6.097 0.43 227870. 0.7288 2.93 0.0285 0.0758 0.1093 0.0411 1.387 14.573 13.453 1034.476 1.646 59.838 5.898 0.43 228054. 0.7013 5.87 0.0570 0.1466 0.1080 0.0420 1.418 14.896 13.294 1057.459 1.683 59.130 5.702 0.43 228256. 0.6740 8.80 0.0856 0.2125 0.1065 0.0429 1.448 15.211 13.115 1079.771 1.719 58.337 5.509 0.43 228480. 0.6468 11.73 0.1141 0.2737 0.1049 0.0437 1.476 15.510 12.916 1100.978 1.752 57.450 5.321 0.43 228726. 0.6199 14.67 0.1426 0.3303 0.1031 0.0445 1.503 15.786 12.693 1120.608 1.784 56.460 5.138 0.43 228994. 0.5934 17.60 0.1711 0.3827 0.1011 0.0452 1.526 16.033 12.446 1138.161 1.811 55.359 4.960 0.43 229285. 0.5672 20.53 0.1996 0.4309 0.0988 0.0458 1.546 16.244 12.172 1153.094 1.835 54.139 4.788 0.43 229601. 0.5415 23.47 0.2282 0.4754 0.0964 0.0463 1.562 16.409 11.869 1164.827 1.854 52.792 4.622 0.43 229941. 0.5161 26.40 0.2567 0.5163 0.0937 0.0466 1.573 16.520 11.535 1172.708 1.866 51.306 4.461 0.43 230306. 0.4912 29.33 0.2852 0.5538 0.0907 0.0467 1.577 16.567 11.167 1176.024 1.872 49.671 4.307 0.43 230697. 0.4666 32.26 0.3137 0.5882 0.0874 0.0466 1.574 16.539 10.764 1174.055 1.869 47.878 4.158 0.43 231114. 0.4423 35.20 0.3423 0.6196 0.0839 0.0463 1.564 16.429 10.325 1166.239 1.856 45.927 4.016 0.43 231557. 0.4183 38.13 0.3708 0.6484 0.0800 0.0458 1.545 16.232 9.853 1152.270 1.834 43.828 3.879 0.43 232026. 0.3947 41.06 0.3993 0.6745 0.0759 0.0450 1.518 15.947 9.351 1132.058 1.802 41.593 3.746 0.43 232520. 0.3714 44.00 0.4278 0.6980 0.0716 0.0439 1.483 15.575 8.821 1105.634 1.760 39.238 3.619 0.43 233041. 0.3484 46.93 0.4563 0.7191 0.0672 0.0426 1.439 15.116 8.269 1073.062 1.708 36.779 3.495 0.44 233588. 0.3258 49.86 0.4849 0.7376 0.0625 0.0411 1.387 14.572 7.695 1034.411 1.646 34.227 3.374 0.44 234161. 0.3034 52.80 0.5134 0.7535 0.0577 0.0393 1.327 13.942 7.103 989.734 1.575 31.596 3.255 0.44 234760. 0.2813 55.73 0.5419 0.7665 0.0528 0.0373 1.259 13.229 6.496 939.069 1.495 28.893 3.137 0.44 235385. 0.2592 58.66 0.5704 0.7765 0.0477 0.0350 1.183 12.431 5.874 882.451 1.404 26.129 3.019 0.44 236037. 0.2372 61.60 0.5989 0.7829 0.0426 0.0326 1.100 11.550 5.241 819.917 1.305 23.311 2.899 0.44 236714. 0.2152 64.53 0.6275 0.7848 0.0373 0.0298 1.008 10.587 4.597 751.521 1.196 20.447 2.774 0.44 237417. 0.1928 67.46 0.6560 0.7812 0.0320 0.0269 0.908 9.542 3.944 677.349 1.078 17.545 2.641 0.44 238146. 0.1701 70.40 0.6845 0.7697 0.0267 0.0237 0.801 8.418 3.286 597.538 0.951 14.615 2.494 0.44 238901. 0.1466 73.33 0.7130 0.7466 0.0213 0.0203 0.687 7.217 2.623 512.291 0.815 11.667 2.322 0.44 239681. 0.1219 76.26 0.7415 0.7041 0.0159 0.0168 0.566 5.943 1.959 421.909 0.671 8.714 2.106 0.44 240488. 0.0956 79.19 0.7701 0.6250 0.0105 0.0130 0.438 4.604 1.297 326.801 0.520 5.770 1.800 0.44 241319. 0.0665 82.13 0.7986 0.4599 0.0052 0.0090 0.305 3.204 0.641 227.454 0.362 2.849 1.277 0.44 242172. 0.0331 85.06 0.8271 -0.0270 -0.0002 0.0049 0.164 1.725 -0.020 122.434 0.195 -0.087 -0.072 0.45 242960. 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 0.1112 0.0403 2.158 19.434 18.641 1609.468 2.196 82.915 5.253 0.50 265830. 0.7353 3.45 0.0287 0.0768 0.1101 0.0412 2.210 19.895 18.453 1647.675 2.248 82.080 5.080 0.50 266045. 0.7074 6.90 0.0575 0.1484 0.1088 0.0422 2.260 20.352 18.241 1685.506 2.299 81.135 4.909 0.50 266284. 0.6796 10.35 0.0862 0.2150 0.1074 0.0431 2.310 20.796 18.001 1722.253 2.349 80.069 4.741 0.50 266548. 0.6520 13.80 0.1150 0.2768 0.1058 0.0439 2.356 21.217 17.732 1757.191 2.397 78.870 4.577 0.50 266837. 0.6248 17.25 0.1437 0.3340 0.1040 0.0448 2.400 21.608 17.429 1789.526 2.441 77.526 4.418 0.50 267154. 0.5979 20.69 0.1725 0.3868 0.1020 0.0455 2.439 21.957 17.092 1818.411 2.481 76.026 4.263 0.50 267498. 0.5714 24.14 0.2012 0.4355 0.0997 0.0461 2.471 22.253 16.717 1842.945 2.514 74.356 4.114 0.50 267872. 0.5453 27.59 0.2300 0.4803 0.0973 0.0466 2.497 22.485 16.301 1862.156 2.540 72.505 3.970 0.50 268274. 0.5197 31.04 0.2587 0.5215 0.0945 0.0469 2.514 22.640 15.840 1874.965 2.558 70.458 3.832 0.50 268707. 0.4944 34.49 0.2875 0.5593 0.0915 0.0470 2.521 22.703 15.333 1880.190 2.565 68.199 3.699 0.50 269170. 0.4695 37.94 0.3162 0.5939 0.0882 0.0469 2.517 22.660 14.774 1876.646 2.560 65.717 3.571 0.51 269664. 0.4450 41.39 0.3450 0.6257 0.0845 0.0466 2.499 22.500 14.166 1863.419 2.542 63.011 3.448 0.51 270188. 0.4207 44.84 0.3737 0.6546 0.0806 0.0460 2.468 22.218 13.511 1840.023 2.510 60.095 3.330 0.51 270743. 0.3968 48.29 0.4024 0.6810 0.0764 0.0452 2.422 21.811 12.812 1806.329 2.464 56.989 3.217 0.51 271330. 0.3733 51.74 0.4312 0.7049 0.0721 0.0441 2.363 21.280 12.076 1762.400 2.404 53.716 3.108 0.51 271947. 0.3501 55.18 0.4599 0.7263 0.0675 0.0427 2.291 20.628 11.307 1708.354 2.331 50.295 3.002 0.51 272595. 0.3273 58.63 0.4887 0.7452 0.0627 0.0411 2.205 19.854 10.509 1644.309 2.243 46.746 2.899 0.51 273274. 0.3047 62.08 0.5174 0.7614 0.0578 0.0393 2.106 18.961 9.686 1570.358 2.142 43.085 2.798 0.51 273983. 0.2823 65.53 0.5462 0.7749 0.0528 0.0372 1.994 17.950 8.841 1486.568 2.028 39.324 2.697 0.51 274724. 0.2600 68.98 0.5749 0.7854 0.0476 0.0348 1.868 16.820 7.976 1392.996 1.900 35.478 2.597 0.51 275495. 0.2378 72.43 0.6037 0.7922 0.0423 0.0323 1.730 15.573 7.094 1289.711 1.759 31.556 2.495 0.51 276297. 0.2154 75.88 0.6324 0.7947 0.0370 0.0294 1.578 14.210 6.199 1176.810 1.605 27.571 2.389 0.51 277129. 0.1928 79.33 0.6612 0.7915 0.0316 0.0264 1.414 12.732 5.291 1054.446 1.438 23.534 2.276 0.51 277993. 0.1697 82.78 0.6899 0.7803 0.0261 0.0231 1.238 11.143 4.375 922.859 1.259 19.459 2.150 0.51 278886. 0.1458 86.23 0.7187 0.7568 0.0206 0.0196 1.049 9.447 3.453 782.411 1.067 15.361 2.002 0.52 279811. 0.1206 89.67 0.7474 0.7122 0.0151 0.0158 0.850 7.651 2.531 633.634 0.864 11.257 1.812 0.52 280765. 0.0934 93.12 0.7762 0.6254 0.0096 0.0119 0.640 5.763 1.612 477.244 0.651 7.169 1.532 0.52 281748. 0.0630 96.57 0.8049 0.4285 0.0042 0.0079 0.421 3.792 0.701 314.026 0.428 3.117 1.012 0.52 282755. 0.0275 100.02 0.8336 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 0.1122 0.0405 3.243 25.550 24.557 2418.282 2.887 109.228 4.606 0.57 303781. 0.7399 3.93 0.0287 0.0767 0.1111 0.0415 3.322 26.170 24.323 2476.963 2.957 108.187 4.454 0.57 304026. 0.7121 7.86 0.0573 0.1483 0.1099 0.0425 3.400 26.785 24.056 2535.160 3.026 107.003 4.304 0.57 304297. 0.6843 11.79 0.0860 0.2148 0.1085 0.0434 3.476 27.383 23.754 2591.803 3.094 105.659 4.157 0.57 304597. 0.6568 15.72 0.1146 0.2766 0.1070 0.0443 3.548 27.953 23.413 2645.756 3.158 104.140 4.014 0.57 304927. 0.6296 19.65 0.1433 0.3337 0.1052 0.0452 3.615 28.482 23.028 2695.794 3.218 102.428 3.874 0.57 305288. 0.6027 23.58 0.1719 0.3865 0.1032 0.0459 3.675 28.955 22.596 2740.617 3.271 100.507 3.740 0.58 305680. 0.5763 27.51 0.2006 0.4352 0.1010 0.0466 3.726 29.359 22.114 2778.848 3.317 98.362 3.609 0.58 306106. 0.5502 31.43 0.2292 0.4801 0.0986 0.0471 3.767 29.678 21.577 2809.012 3.353 95.974 3.484 0.58 306564. 0.5246 35.36 0.2579 0.5214 0.0958 0.0474 3.794 29.894 20.981 2829.497 3.377 93.325 3.363 0.58 307058. 0.4994 39.29 0.2866 0.5594 0.0928 0.0476 3.807 29.990 20.323 2838.520 3.388 90.395 3.247 0.58 307585. 0.4746 43.22 0.3152 0.5942 0.0895 0.0475 3.801 29.945 19.597 2834.292 3.383 87.167 3.136 0.58 308148. 0.4501 47.15 0.3439 0.6262 0.0859 0.0472 3.775 29.745 18.804 2815.386 3.361 83.641 3.029 0.58 308746. 0.4259 51.08 0.3725 0.6555 0.0820 0.0466 3.729 29.382 17.948 2781.014 3.320 79.831 2.927 0.58 309379. 0.4020 55.01 0.4012 0.6822 0.0778 0.0458 3.662 28.853 17.033 2730.956 3.260 75.764 2.829 0.58 310047. 0.3785 58.94 0.4298 0.7065 0.0734 0.0447 3.574 28.160 16.068 2665.305 3.181 71.470 2.734 0.58 310750. 0.3553 62.87 0.4585 0.7284 0.0688 0.0433 3.466 27.303 15.058 2584.257 3.085 66.977 2.643 0.58 311488. 0.3325 66.80 0.4871 0.7479 0.0640 0.0417 3.336 26.287 14.009 2488.008 2.970 62.311 2.554 0.58 312261. 0.3099 70.73 0.5158 0.7648 0.0590 0.0398 3.187 25.111 12.926 2376.720 2.837 57.493 2.467 0.58 313069. 0.2875 74.66 0.5445 0.7792 0.0540 0.0377 3.018 23.777 11.812 2250.508 2.686 52.541 2.381 0.58 313911. 0.2652 78.59 0.5731 0.7906 0.0488 0.0353 2.829 22.287 10.673 2109.470 2.518 47.471 2.295 0.58 314789. 0.2430 82.52 0.6018 0.7987 0.0434 0.0327 2.620 20.642 9.510 1953.709 2.332 42.300 2.208 0.58 315701. 0.2207 86.44 0.6304 0.8027 0.0380 0.0299 2.392 18.842 8.328 1783.368 2.129 37.042 2.118 0.59 316648. 0.1981 90.37 0.6591 0.8014 0.0326 0.0268 2.144 16.890 7.130 1598.671 1.908 31.712 2.023 0.59 317630. 0.1751 94.30 0.6877 0.7928 0.0270 0.0235 1.877 14.791 5.919 1399.967 1.671 26.328 1.918 0.59 318647. 0.1513 98.23 0.7164 0.7731 0.0215 0.0199 1.593 12.549 4.701 1187.785 1.418 20.910 1.795 0.59 319697. 0.1262 102.16 0.7450 0.7342 0.0159 0.0161 1.291 10.173 3.480 962.898 1.149 15.480 1.639 0.59 320782. 0.0991 106.09 0.7737 0.6573 0.0103 0.0122 0.974 7.674 2.263 726.371 0.867 10.067 1.413 0.59 321900. 0.0689 110.02 0.8024 0.4819 0.0048 0.0080 0.643 5.065 1.056 479.419 0.572 4.697 0.999 0.59 323047. 0.0333 113.95 0.8310 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 0.1133 0.0410 4.670 32.702 31.382 3482.118 3.695 139.586 4.088 0.65 341720. 0.7423 4.41 0.0286 0.0764 0.1123 0.0420 4.785 33.508 31.104 3567.937 3.786 138.351 3.954 0.65 341994. 0.7149 8.81 0.0571 0.1476 0.1111 0.0430 4.899 34.310 30.786 3653.343 3.876 136.935 3.822 0.65 342298. 0.6875 13.22 0.0857 0.2139 0.1098 0.0440 5.011 35.093 30.422 3736.743 3.965 135.316 3.693 0.65 342633. 0.6603 17.62 0.1142 0.2755 0.1083 0.0449 5.118 35.842 30.007 3816.459 4.049 133.470 3.566 0.65 343003. 0.6333 22.03 0.1428 0.3325 0.1066 0.0458 5.217 36.539 29.536 3890.674 4.128 131.377 3.443 0.65 343407. 0.6066 26.43 0.1713 0.3852 0.1047 0.0466 5.307 37.166 29.005 3957.429 4.199 129.012 3.324 0.65 343847. 0.5804 30.84 0.1999 0.4339 0.1025 0.0472 5.384 37.703 28.407 4014.678 4.260 126.355 3.209 0.65 344324. 0.5545 35.24 0.2285 0.4788 0.1001 0.0478 5.445 38.131 27.739 4060.240 4.308 123.384 3.099 0.65 344839. 0.5291 39.65 0.2570 0.5201 0.0974 0.0481 5.487 38.427 26.995 4091.766 4.341 120.074 2.992 0.65 345392. 0.5040 44.05 0.2856 0.5582 0.0945 0.0483 5.507 38.568 26.169 4106.698 4.357 116.399 2.890 0.65 345984. 0.4793 48.46 0.3141 0.5932 0.0912 0.0483 5.501 38.528 25.256 4102.444 4.353 112.338 2.792 0.65 346615. 0.4549 52.86 0.3427 0.6254 0.0875 0.0480 5.467 38.287 24.255 4076.873 4.326 107.886 2.698 0.65 347286. 0.4308 57.27 0.3712 0.6549 0.0836 0.0474 5.403 37.836 23.171 4028.765 4.275 103.062 2.609 0.65 347996. 0.4071 61.67 0.3998 0.6820 0.0794 0.0466 5.307 37.169 22.010 3957.756 4.199 97.900 2.522 0.65 348745. 0.3836 66.08 0.4284 0.7067 0.0750 0.0455 5.182 36.288 20.782 3863.981 4.100 92.438 2.439 0.65 349534. 0.3605 70.48 0.4569 0.7290 0.0704 0.0441 5.026 35.197 19.495 3747.750 3.976 86.713 2.359 0.65 350361. 0.3377 74.89 0.4855 0.7491 0.0655 0.0425 4.840 33.897 18.156 3609.396 3.830 80.758 2.282 0.65 351228. 0.3152 79.29 0.5140 0.7667 0.0605 0.0406 4.625 32.393 16.772 3449.184 3.660 74.602 2.206 0.65 352133. 0.2928 83.70 0.5426 0.7818 0.0554 0.0384 4.382 30.685 15.348 3267.314 3.467 68.269 2.131 0.66 353077. 0.2706 88.11 0.5711 0.7942 0.0501 0.0361 4.109 28.775 13.890 3063.945 3.251 61.781 2.056 0.66 354060. 0.2484 92.51 0.5997 0.8034 0.0448 0.0334 3.807 26.664 12.401 2839.236 3.013 55.158 1.981 0.66 355081. 0.2261 96.92 0.6283 0.8089 0.0393 0.0305 3.478 24.356 10.885 2593.389 2.752 48.418 1.904 0.66 356142. 0.2036 101.32 0.6568 0.8095 0.0337 0.0274 3.120 21.851 9.348 2326.721 2.469 41.581 1.822 0.66 357241. 0.1806 105.73 0.6854 0.8033 0.0281 0.0240 2.735 19.156 7.794 2039.706 2.164 34.669 1.733 0.66 358378. 0.1569 110.13 0.7139 0.7871 0.0225 0.0204 2.324 16.276 6.229 1733.082 1.839 27.707 1.630 0.66 359554. 0.1319 114.54 0.7425 0.7537 0.0168 0.0166 1.888 13.222 4.659 1407.926 1.494 20.723 1.501 0.66 360768. 0.1050 118.94 0.7710 0.6862 0.0112 0.0125 1.429 10.009 3.092 1065.734 1.131 13.755 1.316 0.67 362018. 0.0750 123.35 0.7996 0.5322 0.0055 0.0083 0.950 6.652 1.537 708.313 0.752 6.836 0.984 0.67 363302. 0.0396 127.75 0.8282 -0.0289 -0.0001 0.0039 0.440 3.083 -0.037 328.301 0.348 -0.166 -0.052 0.67 364432. 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 0.1145 0.0422 6.591 41.543 39.154 4915.042 4.694 174.155 3.613 0.72 379647. 0.7329 4.90 0.0286 0.0752 0.1136 0.0432 6.748 42.530 38.840 5031.758 4.805 172.759 3.501 0.72 379950. 0.7073 9.80 0.0572 0.1456 0.1125 0.0442 6.903 43.511 38.475 5147.866 4.916 171.138 3.390 0.72 380286. 0.6817 14.70 0.0857 0.2114 0.1113 0.0451 7.055 44.469 38.054 5261.179 5.024 169.264 3.281 0.72 380659. 0.6561 19.59 0.1143 0.2726 0.1098 0.0461 7.200 45.384 37.569 5369.407 5.127 167.105 3.174 0.72 381069. 0.6306 24.49 0.1429 0.3295 0.1082 0.0469 7.335 46.234 37.012 5470.057 5.224 164.628 3.069 0.72 381518. 0.6053 29.39 0.1715 0.3823 0.1064 0.0477 7.457 46.999 36.377 5560.492 5.310 161.804 2.967 0.72 382008. 0.5802 34.29 0.2001 0.4312 0.1042 0.0484 7.561 47.653 35.657 5637.904 5.384 158.603 2.869 0.72 382540. 0.5553 39.19 0.2286 0.4764 0.1019 0.0489 7.643 48.172 34.846 5699.355 5.442 154.994 2.773 0.72 383114. 0.5307 44.09 0.2572 0.5181 0.0992 0.0493 7.700 48.530 33.936 5741.620 5.483 150.947 2.681 0.72 383732. 0.5063 48.99 0.2858 0.5566 0.0962 0.0494 7.726 48.695 32.920 5761.156 5.501 146.429 2.592 0.72 384393. 0.4821 53.88 0.3144 0.5920 0.0929 0.0494 7.717 48.636 31.792 5754.261 5.495 141.411 2.506 0.72 385098. 0.4581 58.78 0.3430 0.6245 0.0893 0.0490 7.668 48.328 30.550 5717.805 5.460 135.888 2.423 0.72 385847. 0.4342 63.68 0.3715 0.6544 0.0854 0.0485 7.577 47.754 29.200 5649.863 5.395 129.881 2.344 0.72 386639. 0.4106 68.58 0.4001 0.6819 0.0811 0.0476 7.442 46.908 27.750 5549.721 5.300 123.433 2.268 0.72 387476. 0.3873 73.48 0.4287 0.7070 0.0766 0.0465 7.265 45.789 26.213 5417.401 5.173 116.594 2.195 0.72 388356. 0.3643 78.38 0.4573 0.7298 0.0719 0.0451 7.045 44.402 24.598 5253.244 5.016 109.412 2.124 0.73 389280. 0.3415 83.28 0.4859 0.7503 0.0670 0.0434 6.782 42.749 22.916 5057.672 4.830 101.931 2.055 0.73 390246. 0.3189 88.17 0.5144 0.7685 0.0619 0.0414 6.479 40.834 21.175 4831.128 4.613 94.188 1.988 0.73 391256. 0.2966 93.07 0.5430 0.7843 0.0567 0.0392 6.134 38.660 19.383 4573.942 4.368 86.215 1.922 0.73 392309. 0.2743 97.97 0.5716 0.7974 0.0513 0.0368 5.748 36.229 17.545 4286.371 4.093 78.039 1.857 0.73 393405. 0.2521 102.87 0.6002 0.8075 0.0458 0.0340 5.322 33.544 15.667 3968.657 3.790 69.687 1.791 0.73 394544. 0.2298 107.77 0.6288 0.8140 0.0402 0.0311 4.856 30.606 13.755 3621.088 3.458 61.182 1.723 0.73 395726. 0.2071 112.67 0.6573 0.8158 0.0345 0.0278 4.350 27.420 11.814 3244.117 3.098 52.548 1.652 0.73 396950. 0.1840 117.57 0.6859 0.8112 0.0288 0.0243 3.807 23.992 9.850 2838.521 2.711 43.814 1.574 0.73 398218. 0.1601 122.47 0.7145 0.7968 0.0230 0.0206 3.226 20.332 7.871 2405.512 2.297 35.011 1.484 0.74 399527. 0.1350 127.36 0.7431 0.7655 0.0172 0.0167 2.611 16.456 5.885 1946.897 1.859 26.175 1.371 0.74 400879. 0.1078 132.26 0.7717 0.7002 0.0114 0.0126 1.965 12.385 3.901 1465.248 1.399 17.351 1.208 0.74 402271. 0.0773 137.16 0.8002 0.5462 0.0056 0.0083 1.292 8.146 1.930 963.749 0.920 8.585 0.908 0.74 403700. 0.0409 142.06 0.8288 -0.0532 -0.0002 0.0037 0.575 3.624 -0.081 428.767 0.409 -0.359 -0.085 0.74 404880. 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 0.1157 0.0455 9.469 54.257 47.884 7061.143 6.130 212.990 3.076 0.79 417560. 0.6900 5.39 0.0286 0.0707 0.1149 0.0465 9.667 55.391 47.550 7208.731 6.258 211.503 2.992 0.79 417890. 0.6688 10.78 0.0572 0.1375 0.1139 0.0474 9.862 56.505 47.157 7353.766 6.384 209.754 2.909 0.79 418258. 0.6475 16.17 0.0858 0.2004 0.1128 0.0483 10.048 57.575 46.695 7492.978 6.505 207.700 2.827 0.79 418665. 0.6262 21.56 0.1144 0.2596 0.1115 0.0491 10.223 58.575 46.155 7623.095 6.618 205.297 2.746 0.79 419115. 0.6048 26.95 0.1430 0.3152 0.1100 0.0499 10.381 59.479 45.526 7740.740 6.720 202.500 2.668 0.79 419609. 0.5835 32.34 0.1715 0.3674 0.1082 0.0505 10.517 60.261 44.799 7842.517 6.808 199.267 2.591 0.79 420148. 0.5622 37.73 0.2001 0.4162 0.1062 0.0511 10.628 60.894 43.964 7924.953 6.880 195.554 2.516 0.79 420734. 0.5409 43.12 0.2287 0.4619 0.1039 0.0515 10.707 61.352 43.013 7984.521 6.932 191.322 2.443 0.79 421368. 0.5195 48.51 0.2573 0.5046 0.1013 0.0517 10.752 61.605 41.936 8017.491 6.960 186.530 2.372 0.79 422050. 0.4980 53.91 0.2859 0.5443 0.0984 0.0517 10.755 61.622 40.722 8019.721 6.962 181.133 2.303 0.79 422780. 0.4765 59.30 0.3145 0.5811 0.0951 0.0515 10.711 61.370 39.365 7986.909 6.934 175.097 2.236 0.79 423559. 0.4547 64.69 0.3431 0.6153 0.0915 0.0510 10.615 60.820 37.862 7915.317 6.871 168.410 2.170 0.79 424387. 0.4328 70.08 0.3717 0.6468 0.0875 0.0503 10.464 59.955 36.218 7802.720 6.774 161.099 2.105 0.80 425263. 0.4108 75.47 0.4003 0.6758 0.0832 0.0493 10.257 58.770 34.446 7648.447 6.640 153.217 2.043 0.80 426188. 0.3887 80.86 0.4289 0.7024 0.0787 0.0480 9.994 57.265 32.560 7452.659 6.470 144.828 1.982 0.80 427161. 0.3666 86.25 0.4575 0.7267 0.0739 0.0465 9.677 55.445 30.574 7215.779 6.264 135.992 1.922 0.80 428182. 0.3445 91.64 0.4860 0.7485 0.0689 0.0447 9.304 53.312 28.500 6938.237 6.023 126.767 1.863 0.80 429250. 0.3224 97.03 0.5146 0.7679 0.0637 0.0427 8.878 50.870 26.349 6620.308 5.747 117.200 1.805 0.80 430365. 0.3004 102.42 0.5432 0.7848 0.0583 0.0404 8.398 48.117 24.131 6262.090 5.436 107.334 1.748 0.80 431528. 0.2783 107.81 0.5718 0.7990 0.0528 0.0378 7.863 45.055 21.854 5863.632 5.090 97.206 1.690 0.80 432738. 0.2562 113.20 0.6004 0.8100 0.0472 0.0350 7.276 41.689 19.525 5425.584 4.710 86.846 1.632 0.80 433994. 0.2338 118.59 0.6290 0.8173 0.0414 0.0319 6.636 38.021 17.151 4948.141 4.296 76.286 1.572 0.81 435298. 0.2111 123.98 0.6576 0.8198 0.0356 0.0286 5.944 34.056 14.738 4432.091 3.848 65.555 1.508 0.81 436648. 0.1877 129.37 0.6862 0.8153 0.0297 0.0250 5.202 29.808 12.295 3879.321 3.368 54.688 1.438 0.81 438046. 0.1634 134.76 0.7148 0.7999 0.0238 0.0212 4.416 25.301 9.829 3292.772 2.859 43.721 1.354 0.81 439489. 0.1376 140.15 0.7434 0.7655 0.0178 0.0172 3.589 20.565 7.352 2676.398 2.323 32.701 1.246 0.81 440978. 0.1095 145.54 0.7720 0.6930 0.0118 0.0131 2.730 15.640 4.874 2035.485 1.767 21.679 1.086 0.81 442512. 0.0777 150.94 0.8005 0.5252 0.0058 0.0089 1.846 10.575 2.408 1376.281 1.195 10.713 0.794 0.81 444086. 0.0399 156.33 0.8291 -0.0484 -0.0003 0.0044 0.914 5.236 -0.106 681.450 0.592 -0.472 -0.071 0.82 445401. 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 0.1166 0.0525 14.194 74.555 57.435 10584.831 8.423 255.469 2.461 0.86 455466. 0.6047 5.95 0.0289 0.0627 0.1159 0.0535 14.447 75.879 57.100 10772.882 8.573 253.980 2.404 0.86 455825. 0.5889 11.90 0.0579 0.1225 0.1151 0.0544 14.690 77.158 56.700 10954.392 8.717 252.202 2.348 0.86 456226. 0.5731 17.85 0.0868 0.1794 0.1141 0.0552 14.917 78.347 56.222 11123.297 8.852 250.075 2.293 0.86 456673. 0.5573 23.80 0.1157 0.2336 0.1130 0.0560 15.118 79.405 55.651 11273.408 8.971 247.533 2.239 0.86 457167. 0.5415 29.75 0.1446 0.2853 0.1116 0.0566 15.286 80.286 54.971 11398.538 9.071 244.510 2.187 0.86 457711. 0.5257 35.70 0.1736 0.3346 0.1100 0.0571 15.411 80.946 54.167 11492.294 9.145 240.935 2.138 0.86 458307. 0.5101 41.65 0.2025 0.3816 0.1081 0.0573 15.489 81.354 53.226 11550.226 9.191 236.748 2.090 0.86 458957. 0.4943 47.60 0.2314 0.4265 0.1058 0.0574 15.513 81.482 52.134 11568.389 9.206 231.891 2.044 0.86 459661. 0.4784 53.54 0.2603 0.4693 0.1033 0.0573 15.479 81.304 50.878 11543.024 9.186 226.305 1.999 0.86 460421. 0.4623 59.49 0.2893 0.5100 0.1004 0.0569 15.382 80.791 49.446 11470.272 9.128 219.934 1.955 0.87 461235. 0.4457 65.44 0.3182 0.5485 0.0971 0.0563 15.215 79.917 47.826 11346.089 9.029 212.728 1.912 0.87 462105. 0.4286 71.39 0.3471 0.5849 0.0934 0.0554 14.975 78.656 46.014 11167.114 8.887 204.671 1.869 0.87 463031. 0.4110 77.34 0.3760 0.6193 0.0894 0.0543 14.660 77.000 44.019 10931.980 8.699 195.794 1.826 0.87 464011. 0.3928 83.29 0.4050 0.6514 0.0850 0.0528 14.271 74.955 41.854 10641.635 8.468 186.168 1.784 0.87 465045. 0.3741 89.24 0.4339 0.6813 0.0803 0.0511 13.810 72.536 39.541 10298.262 8.195 175.878 1.742 0.87 466133. 0.3550 95.19 0.4628 0.7090 0.0753 0.0492 13.282 69.760 37.097 9904.076 7.881 165.007 1.699 0.87 467275. 0.3354 101.14 0.4917 0.7342 0.0701 0.0470 12.687 66.636 34.539 9460.588 7.528 153.627 1.656 0.87 468469. 0.3155 107.09 0.5207 0.7569 0.0647 0.0445 12.027 63.172 31.880 8968.730 7.137 141.804 1.612 0.87 469716. 0.2951 113.04 0.5496 0.7770 0.0592 0.0418 11.303 59.366 29.134 8428.481 6.707 129.589 1.568 0.87 471016. 0.2743 118.99 0.5785 0.7941 0.0534 0.0389 10.513 55.218 26.310 7839.503 6.238 117.029 1.522 0.88 472368. 0.2531 124.94 0.6074 0.8072 0.0475 0.0358 9.666 50.767 23.418 7207.668 5.736 104.162 1.474 0.88 473772. 0.2312 130.89 0.6364 0.8144 0.0415 0.0325 8.770 46.066 20.464 6540.120 5.204 91.026 1.419 0.88 475228. 0.2081 136.84 0.6653 0.8118 0.0354 0.0290 7.847 41.215 17.457 5851.479 4.656 77.650 1.353 0.88 476735. 0.1833 142.79 0.6942 0.7980 0.0293 0.0254 6.875 36.109 14.410 5126.598 4.080 64.094 1.275 0.88 478294. 0.1569 148.74 0.7231 0.7667 0.0230 0.0217 5.863 30.794 11.333 4371.999 3.479 50.410 1.176 0.88 479905. 0.1283 154.68 0.7521 0.7049 0.0167 0.0179 4.823 25.334 8.243 3596.804 2.862 36.663 1.039 0.89 481566. 0.0967 160.63 0.7810 0.5857 0.0105 0.0140 3.770 19.802 5.156 2811.385 2.237 22.932 0.832 0.89 483276. 0.0612 166.58 0.8099 0.3416 0.0042 0.0101 2.717 14.271 2.089 2026.048 1.612 9.294 0.468 0.89 485025. 0.0219 172.53 0.8388 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 0.1151 0.0600 20.602 99.888 66.525 15363.271 11.285 295.902 1.964 0.93 493482. 0.5193 6.49 0.0291 0.0548 0.1145 0.0609 20.914 101.396 66.198 15595.241 11.456 294.450 1.925 0.93 493867. 0.5078 12.98 0.0582 0.1073 0.1139 0.0618 21.221 102.887 65.812 15824.596 11.624 292.730 1.886 0.93 494297. 0.4961 19.47 0.0874 0.1577 0.1131 0.0626 21.516 104.316 65.350 16044.415 11.786 290.677 1.847 0.93 494775. 0.4841 25.96 0.1165 0.2058 0.1121 0.0634 21.788 105.634 64.798 16247.071 11.934 288.222 1.809 0.93 495305. 0.4721 32.45 0.1456 0.2519 0.1110 0.0641 22.025 106.785 64.138 16424.113 12.065 285.285 1.771 0.93 495889. 0.4599 38.93 0.1747 0.2960 0.1096 0.0647 22.216 107.711 63.351 16566.576 12.169 281.784 1.734 0.93 496529. 0.4475 45.42 0.2039 0.3383 0.1080 0.0651 22.348 108.352 62.417 16665.139 12.242 277.629 1.699 0.94 497228. 0.4351 51.91 0.2330 0.3788 0.1061 0.0652 22.409 108.645 61.315 16710.141 12.275 272.730 1.664 0.94 497987. 0.4225 58.40 0.2621 0.4176 0.1038 0.0652 22.383 108.523 60.024 16691.371 12.261 266.988 1.631 0.94 498808. 0.4097 64.89 0.2912 0.4549 0.1012 0.0648 22.258 107.914 58.520 16597.807 12.192 260.298 1.599 0.94 499690. 0.3966 71.38 0.3203 0.4909 0.0982 0.0641 22.016 106.741 56.780 16417.268 12.059 252.556 1.569 0.94 500636. 0.3832 77.87 0.3495 0.5256 0.0948 0.0630 21.646 104.947 54.791 16141.458 11.857 243.708 1.540 0.94 501644. 0.3694 84.36 0.3786 0.5591 0.0909 0.0616 21.144 102.515 52.556 15767.334 11.582 233.769 1.512 0.94 502715. 0.3553 90.85 0.4077 0.5915 0.0867 0.0597 20.514 99.460 50.091 15297.409 11.237 222.807 1.485 0.94 503848. 0.3408 97.34 0.4368 0.6227 0.0820 0.0575 19.764 95.824 47.419 14738.172 10.826 210.920 1.459 0.94 505041. 0.3258 103.82 0.4660 0.6526 0.0771 0.0550 18.906 91.662 44.563 14098.050 10.356 198.216 1.434 0.94 506295. 0.3103 110.31 0.4951 0.6808 0.0719 0.0523 17.950 87.027 41.546 13385.199 9.832 184.796 1.408 0.94 507609. 0.2942 116.80 0.5242 0.7073 0.0664 0.0492 16.905 81.960 38.387 12605.932 9.260 170.747 1.381 0.95 508980. 0.2774 123.29 0.5533 0.7315 0.0607 0.0459 15.776 76.487 35.104 11764.166 8.642 156.141 1.353 0.95 510410. 0.2600 129.78 0.5824 0.7533 0.0549 0.0424 14.568 70.631 31.711 10863.442 7.980 141.049 1.324 0.95 511898. 0.2417 136.27 0.6116 0.7719 0.0488 0.0387 13.286 64.413 28.224 9907.085 7.277 125.539 1.292 0.95 513442. 0.2225 142.76 0.6407 0.7835 0.0426 0.0349 11.977 58.070 24.652 8931.511 6.561 109.653 1.252 0.95 515044. 0.2015 149.25 0.6698 0.7750 0.0363 0.0314 10.778 52.255 20.989 8037.041 5.904 93.360 1.185 0.95 516701. 0.1759 155.74 0.6989 0.7429 0.0299 0.0281 9.647 46.773 17.259 7193.929 5.284 76.768 1.088 0.96 518414. 0.1465 162.23 0.7281 0.6860 0.0233 0.0248 8.510 41.261 13.497 6346.150 4.662 60.033 0.965 0.96 520184. 0.1149 168.72 0.7572 0.5929 0.0168 0.0215 7.384 35.798 9.731 5505.999 4.044 43.283 0.802 0.96 522008. 0.0811 175.20 0.7863 0.4459 0.0104 0.0183 6.285 30.471 5.998 4686.656 3.443 26.680 0.580 0.96 523886. 0.0461 181.69 0.8154 0.2166 0.0040 0.0152 5.224 25.328 2.335 3895.521 2.861 10.388 0.272 0.96 525811. 0.0135 188.18 0.8445