16x10 (16x10.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 0.1071 0.0489 0.004 0.260 0.224 3.075 0.029 0.995 33.013 0.06 30442. 0.5727 0.41 0.0271 0.0580 0.1057 0.0495 0.004 0.263 0.221 3.115 0.030 0.982 32.151 0.06 30466. 0.5540 0.82 0.0543 0.1128 0.1042 0.0501 0.004 0.267 0.218 3.154 0.030 0.968 31.287 0.06 30492. 0.5352 1.23 0.0814 0.1646 0.1025 0.0507 0.004 0.270 0.214 3.190 0.030 0.952 30.426 0.06 30520. 0.5162 1.65 0.1086 0.2133 0.1006 0.0512 0.004 0.272 0.210 3.223 0.031 0.935 29.570 0.06 30551. 0.4971 2.06 0.1357 0.2589 0.0986 0.0517 0.004 0.275 0.206 3.251 0.031 0.916 28.721 0.06 30585. 0.4779 2.47 0.1629 0.3016 0.0964 0.0520 0.004 0.277 0.201 3.274 0.031 0.895 27.879 0.06 30621. 0.4587 2.88 0.1900 0.3414 0.0940 0.0523 0.004 0.278 0.196 3.291 0.031 0.873 27.047 0.06 30660. 0.4394 3.29 0.2172 0.3783 0.0914 0.0525 0.004 0.279 0.191 3.301 0.032 0.849 26.225 0.06 30702. 0.4202 3.70 0.2443 0.4124 0.0886 0.0525 0.004 0.279 0.185 3.302 0.032 0.823 25.412 0.06 30746. 0.4009 4.11 0.2715 0.4437 0.0856 0.0524 0.004 0.278 0.179 3.295 0.031 0.795 24.608 0.06 30794. 0.3815 4.52 0.2986 0.4723 0.0824 0.0521 0.004 0.277 0.172 3.277 0.031 0.765 23.811 0.06 30845. 0.3622 4.94 0.3258 0.4981 0.0789 0.0516 0.004 0.275 0.165 3.248 0.031 0.733 23.021 0.06 30899. 0.3428 5.35 0.3529 0.5212 0.0753 0.0510 0.004 0.271 0.157 3.208 0.031 0.699 22.234 0.06 30955. 0.3233 5.76 0.3800 0.5414 0.0714 0.0501 0.004 0.267 0.149 3.155 0.030 0.664 21.447 0.06 31015. 0.3038 6.17 0.4072 0.5587 0.0674 0.0491 0.004 0.261 0.141 3.091 0.030 0.626 20.658 0.06 31078. 0.2842 6.58 0.4343 0.5730 0.0632 0.0479 0.004 0.255 0.132 3.014 0.029 0.587 19.861 0.06 31144. 0.2646 6.99 0.4615 0.5840 0.0588 0.0465 0.004 0.247 0.123 2.926 0.028 0.547 19.051 0.06 31213. 0.2449 7.40 0.4886 0.5914 0.0544 0.0449 0.004 0.239 0.114 2.827 0.027 0.505 18.220 0.06 31286. 0.2252 7.81 0.5158 0.5948 0.0498 0.0432 0.004 0.230 0.104 2.716 0.026 0.462 17.361 0.06 31361. 0.2053 8.23 0.5429 0.5936 0.0451 0.0412 0.003 0.219 0.094 2.594 0.025 0.419 16.461 0.06 31439. 0.1852 8.64 0.5701 0.5872 0.0403 0.0391 0.003 0.208 0.084 2.460 0.023 0.374 15.507 0.06 31521. 0.1649 9.05 0.5972 0.5744 0.0354 0.0368 0.003 0.196 0.074 2.316 0.022 0.329 14.480 0.06 31606. 0.1444 9.46 0.6244 0.5537 0.0305 0.0343 0.003 0.183 0.064 2.160 0.021 0.283 13.352 0.06 31694. 0.1235 9.87 0.6515 0.5231 0.0254 0.0317 0.003 0.169 0.053 1.994 0.019 0.236 12.087 0.06 31785. 0.1022 10.28 0.6787 0.4791 0.0204 0.0289 0.002 0.154 0.043 1.817 0.017 0.189 10.629 0.06 31879. 0.0804 10.69 0.7058 0.4169 0.0153 0.0259 0.002 0.138 0.032 1.630 0.016 0.142 8.893 0.07 31976. 0.0583 11.11 0.7329 0.3283 0.0102 0.0228 0.002 0.121 0.021 1.433 0.014 0.095 6.743 0.07 32076. 0.0361 11.52 0.7601 0.1989 0.0051 0.0195 0.002 0.104 0.011 1.227 0.012 0.047 3.939 0.07 32180. 0.0149 11.93 0.7872 0.0011 0.0000 0.0161 0.001 0.086 0.000 1.012 0.010 0.000 0.022 0.07 32285. 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 0.1076 0.0439 0.030 0.934 0.899 22.097 0.106 3.999 18.457 0.13 60883. 0.6418 0.83 0.0273 0.0651 0.1062 0.0446 0.030 0.949 0.887 22.452 0.107 3.947 17.927 0.13 60931. 0.6193 1.66 0.0546 0.1263 0.1047 0.0453 0.031 0.963 0.874 22.793 0.109 3.890 17.401 0.13 60983. 0.5967 2.48 0.0820 0.1838 0.1030 0.0459 0.031 0.977 0.860 23.114 0.110 3.826 16.881 0.13 61041. 0.5742 3.31 0.1093 0.2376 0.1011 0.0465 0.031 0.989 0.845 23.408 0.112 3.757 16.367 0.13 61103. 0.5517 4.14 0.1366 0.2878 0.0991 0.0470 0.032 1.000 0.828 23.667 0.113 3.682 15.862 0.13 61171. 0.5292 4.97 0.1639 0.3346 0.0969 0.0474 0.032 1.009 0.809 23.885 0.114 3.599 15.367 0.13 61244. 0.5069 5.79 0.1912 0.3781 0.0945 0.0478 0.032 1.016 0.789 24.051 0.115 3.510 14.881 0.13 61323. 0.4848 6.62 0.2186 0.4183 0.0919 0.0480 0.032 1.021 0.767 24.160 0.115 3.413 14.406 0.13 61407. 0.4628 7.45 0.2459 0.4554 0.0890 0.0481 0.032 1.023 0.744 24.201 0.116 3.309 13.941 0.13 61498. 0.4410 8.28 0.2732 0.4895 0.0860 0.0480 0.032 1.021 0.719 24.167 0.115 3.196 13.487 0.13 61594. 0.4193 9.11 0.3005 0.5206 0.0828 0.0478 0.032 1.016 0.692 24.050 0.115 3.076 13.042 0.13 61697. 0.3977 9.93 0.3278 0.5490 0.0793 0.0474 0.032 1.008 0.663 23.841 0.114 2.947 12.605 0.13 61805. 0.3763 10.76 0.3551 0.5745 0.0756 0.0468 0.032 0.995 0.632 23.534 0.112 2.810 12.176 0.13 61920. 0.3549 11.59 0.3825 0.5972 0.0717 0.0459 0.031 0.977 0.599 23.126 0.110 2.666 11.753 0.13 62041. 0.3337 12.42 0.4098 0.6171 0.0677 0.0449 0.030 0.956 0.565 22.618 0.108 2.514 11.335 0.13 62168. 0.3125 13.25 0.4371 0.6340 0.0634 0.0437 0.030 0.930 0.530 22.008 0.105 2.357 10.918 0.13 62302. 0.2914 14.07 0.4644 0.6479 0.0590 0.0423 0.029 0.900 0.493 21.300 0.102 2.194 10.501 0.13 62442. 0.2704 14.90 0.4917 0.6584 0.0545 0.0407 0.027 0.866 0.455 20.494 0.098 2.026 10.079 0.13 62588. 0.2494 15.73 0.5191 0.6653 0.0499 0.0389 0.026 0.828 0.417 19.589 0.094 1.854 9.649 0.13 62741. 0.2284 16.56 0.5464 0.6681 0.0451 0.0369 0.025 0.786 0.377 18.587 0.089 1.678 9.204 0.13 62899. 0.2073 17.38 0.5737 0.6659 0.0403 0.0347 0.023 0.739 0.337 17.489 0.084 1.498 8.737 0.13 63064. 0.1860 18.21 0.6010 0.6577 0.0354 0.0324 0.022 0.689 0.296 16.293 0.078 1.316 8.238 0.13 63236. 0.1643 19.04 0.6283 0.6420 0.0305 0.0298 0.020 0.634 0.254 15.002 0.072 1.132 7.691 0.13 63414. 0.1423 19.87 0.6557 0.6162 0.0254 0.0271 0.018 0.575 0.212 13.617 0.065 0.945 7.075 0.13 63598. 0.1196 20.70 0.6830 0.5765 0.0204 0.0241 0.016 0.513 0.170 12.140 0.058 0.756 6.354 0.13 63788. 0.0961 21.52 0.7103 0.5161 0.0153 0.0210 0.014 0.447 0.127 10.573 0.050 0.567 5.469 0.13 63985. 0.0716 22.35 0.7376 0.4227 0.0102 0.0177 0.012 0.377 0.085 8.922 0.043 0.377 4.313 0.13 64188. 0.0461 23.18 0.7649 0.2711 0.0051 0.0143 0.010 0.304 0.042 7.191 0.034 0.188 2.667 0.13 64397. 0.0201 24.01 0.7922 -0.0006 0.0000 0.0107 0.007 0.228 0.000 5.385 0.026 0.000 -0.006 0.13 64608. 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 0.1080 0.0419 0.096 2.007 2.030 71.228 0.227 9.032 12.930 0.19 91323. 0.6757 1.25 0.0274 0.0685 0.1066 0.0427 0.097 2.042 2.004 72.472 0.231 8.914 12.543 0.19 91395. 0.6512 2.49 0.0548 0.1328 0.1051 0.0434 0.099 2.076 1.975 73.672 0.235 8.785 12.160 0.19 91474. 0.6267 3.74 0.0822 0.1930 0.1034 0.0440 0.100 2.108 1.943 74.806 0.238 8.643 11.782 0.19 91560. 0.6023 4.98 0.1096 0.2492 0.1015 0.0446 0.102 2.137 1.908 75.848 0.241 8.488 11.411 0.19 91654. 0.5781 6.23 0.1370 0.3016 0.0995 0.0452 0.103 2.163 1.870 76.774 0.244 8.318 11.048 0.19 91756. 0.5540 7.47 0.1644 0.3502 0.0973 0.0457 0.104 2.185 1.828 77.556 0.247 8.132 10.693 0.19 91866. 0.5302 8.72 0.1918 0.3954 0.0949 0.0460 0.105 2.202 1.783 78.168 0.249 7.931 10.346 0.19 91985. 0.5067 9.96 0.2192 0.4371 0.0922 0.0463 0.105 2.214 1.734 78.579 0.250 7.713 10.009 0.19 92112. 0.4833 11.21 0.2466 0.4756 0.0894 0.0464 0.106 2.219 1.681 78.761 0.251 7.477 9.680 0.19 92249. 0.4603 12.45 0.2740 0.5110 0.0864 0.0463 0.106 2.217 1.624 78.684 0.250 7.223 9.361 0.19 92394. 0.4374 13.70 0.3014 0.5434 0.0831 0.0461 0.105 2.207 1.563 78.320 0.249 6.950 9.049 0.19 92549. 0.4148 14.94 0.3288 0.5730 0.0796 0.0457 0.104 2.187 1.497 77.641 0.247 6.659 8.746 0.19 92713. 0.3924 16.19 0.3562 0.5997 0.0759 0.0451 0.103 2.159 1.427 76.625 0.244 6.349 8.449 0.19 92886. 0.3702 17.43 0.3836 0.6236 0.0720 0.0443 0.101 2.120 1.354 75.261 0.240 6.022 8.159 0.19 93068. 0.3481 18.68 0.4109 0.6448 0.0679 0.0433 0.099 2.072 1.277 73.547 0.234 5.679 7.874 0.19 93260. 0.3263 19.92 0.4383 0.6632 0.0637 0.0421 0.096 2.014 1.197 71.485 0.228 5.322 7.592 0.19 93462. 0.3046 21.17 0.4657 0.6786 0.0592 0.0407 0.093 1.946 1.114 69.078 0.220 4.953 7.312 0.19 93673. 0.2830 22.42 0.4931 0.6909 0.0547 0.0390 0.089 1.869 1.028 66.328 0.211 4.573 7.031 0.19 93893. 0.2615 23.66 0.5205 0.6999 0.0500 0.0372 0.085 1.782 0.941 63.236 0.201 4.184 6.747 0.19 94123. 0.2400 24.91 0.5479 0.7049 0.0453 0.0352 0.080 1.685 0.851 59.805 0.190 3.786 6.456 0.19 94362. 0.2184 26.15 0.5753 0.7053 0.0404 0.0330 0.075 1.579 0.760 56.034 0.178 3.381 6.152 0.19 94611. 0.1967 27.40 0.6027 0.7002 0.0355 0.0306 0.070 1.463 0.667 51.926 0.165 2.969 5.830 0.19 94870. 0.1747 28.64 0.6301 0.6879 0.0305 0.0279 0.064 1.338 0.574 47.483 0.151 2.551 5.479 0.19 95138. 0.1522 29.89 0.6575 0.6660 0.0255 0.0251 0.057 1.203 0.479 42.709 0.136 2.129 5.083 0.19 95416. 0.1290 31.13 0.6849 0.6304 0.0204 0.0221 0.050 1.060 0.383 37.613 0.120 1.704 4.619 0.19 95703. 0.1048 32.38 0.7123 0.5735 0.0153 0.0190 0.043 0.907 0.287 32.206 0.103 1.276 4.041 0.20 96000. 0.0794 33.62 0.7397 0.4810 0.0101 0.0156 0.036 0.747 0.191 26.503 0.084 0.848 3.263 0.20 96306. 0.0523 34.87 0.7671 0.3199 0.0050 0.0121 0.028 0.578 0.095 20.524 0.065 0.421 2.093 0.20 96620. 0.0236 36.11 0.7945 -0.0045 0.0000 0.0084 0.019 0.402 -0.001 14.275 0.045 -0.004 -0.028 0.20 96937. 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 0.1085 0.0409 0.221 3.481 3.624 164.747 0.393 16.121 9.978 0.25 121760. 0.6966 1.66 0.0274 0.0705 0.1071 0.0417 0.225 3.545 3.578 167.773 0.401 15.914 9.672 0.25 121856. 0.6709 3.32 0.0548 0.1365 0.1055 0.0424 0.229 3.607 3.526 170.697 0.408 15.685 9.370 0.25 121962. 0.6453 4.99 0.0823 0.1983 0.1038 0.0431 0.233 3.665 3.470 173.463 0.414 15.434 9.073 0.25 122077. 0.6198 6.65 0.1097 0.2559 0.1020 0.0437 0.236 3.719 3.408 176.014 0.420 15.159 8.782 0.25 122202. 0.5945 8.31 0.1371 0.3096 0.1000 0.0443 0.239 3.767 3.340 178.287 0.426 14.857 8.497 0.25 122339. 0.5695 9.97 0.1645 0.3594 0.0977 0.0448 0.242 3.808 3.266 180.218 0.430 14.528 8.220 0.25 122486. 0.5448 11.63 0.1920 0.4055 0.0953 0.0451 0.244 3.840 3.186 181.740 0.434 14.170 7.950 0.25 122645. 0.5204 13.30 0.2194 0.4481 0.0927 0.0454 0.245 3.862 3.098 182.783 0.436 13.781 7.688 0.25 122815. 0.4963 14.96 0.2468 0.4875 0.0899 0.0455 0.246 3.873 3.004 183.277 0.438 13.361 7.434 0.25 122997. 0.4725 16.62 0.2742 0.5237 0.0868 0.0455 0.246 3.870 2.902 183.150 0.437 12.908 7.187 0.25 123192. 0.4490 18.28 0.3017 0.5568 0.0836 0.0453 0.245 3.853 2.793 182.333 0.435 12.423 6.947 0.26 123398. 0.4258 19.94 0.3291 0.5871 0.0801 0.0449 0.242 3.820 2.676 180.760 0.432 11.903 6.715 0.26 123617. 0.4028 21.61 0.3565 0.6146 0.0764 0.0443 0.239 3.769 2.552 178.378 0.426 11.350 6.488 0.26 123849. 0.3801 23.27 0.3839 0.6393 0.0724 0.0435 0.235 3.701 2.420 175.157 0.418 10.766 6.267 0.26 124093. 0.3576 24.93 0.4114 0.6614 0.0683 0.0425 0.229 3.615 2.283 171.091 0.408 10.153 6.051 0.26 124350. 0.3353 26.59 0.4388 0.6807 0.0640 0.0413 0.223 3.512 2.139 166.186 0.397 9.516 5.839 0.26 124619. 0.3132 28.25 0.4662 0.6973 0.0596 0.0398 0.215 3.390 1.991 160.446 0.383 8.857 5.629 0.26 124901. 0.2913 29.92 0.4936 0.7108 0.0550 0.0382 0.206 3.252 1.839 153.878 0.367 8.179 5.420 0.26 125195. 0.2695 31.58 0.5210 0.7211 0.0503 0.0364 0.196 3.095 1.682 146.483 0.350 7.483 5.209 0.26 125502. 0.2478 33.24 0.5485 0.7278 0.0456 0.0343 0.185 2.922 1.523 138.264 0.330 6.772 4.995 0.26 125822. 0.2260 34.90 0.5759 0.7302 0.0407 0.0321 0.173 2.731 1.360 129.223 0.308 6.048 4.772 0.26 126155. 0.2041 36.56 0.6033 0.7274 0.0357 0.0296 0.160 2.522 1.194 119.364 0.285 5.312 4.538 0.26 126501. 0.1819 38.23 0.6307 0.7179 0.0307 0.0270 0.146 2.297 1.027 108.693 0.259 4.566 4.284 0.26 126859. 0.1592 39.89 0.6582 0.6992 0.0256 0.0241 0.130 2.054 0.857 97.223 0.232 3.812 3.999 0.26 127230. 0.1358 41.55 0.6856 0.6673 0.0205 0.0211 0.114 1.795 0.686 84.970 0.203 3.053 3.664 0.26 127613. 0.1113 43.21 0.7130 0.6146 0.0154 0.0179 0.097 1.521 0.515 71.963 0.172 2.290 3.244 0.26 128010. 0.0854 44.87 0.7404 0.5254 0.0103 0.0145 0.078 1.231 0.343 58.238 0.139 1.525 2.671 0.26 128418. 0.0574 46.54 0.7679 0.3622 0.0051 0.0109 0.059 0.927 0.172 43.847 0.105 0.763 1.776 0.26 128839. 0.0270 48.20 0.7953 0.0033 0.0000 0.0071 0.039 0.608 0.001 28.793 0.069 0.004 0.016 0.26 129260. 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 0.1090 0.0404 0.426 5.367 5.690 317.468 0.606 25.308 8.129 0.32 152195. 0.7111 2.10 0.0277 0.0724 0.1076 0.0411 0.434 5.470 5.617 323.564 0.618 24.984 7.874 0.32 152316. 0.6844 4.20 0.0554 0.1402 0.1060 0.0419 0.442 5.569 5.536 329.459 0.629 24.626 7.622 0.32 152449. 0.6577 6.29 0.0831 0.2035 0.1043 0.0426 0.449 5.664 5.448 335.036 0.640 24.231 7.375 0.32 152595. 0.6313 8.39 0.1108 0.2624 0.1025 0.0433 0.456 5.751 5.350 340.179 0.650 23.797 7.133 0.32 152754. 0.6051 10.49 0.1385 0.3172 0.1004 0.0438 0.462 5.828 5.243 344.762 0.658 23.321 6.898 0.32 152927. 0.5792 12.59 0.1661 0.3680 0.0982 0.0443 0.468 5.894 5.126 348.651 0.666 22.801 6.669 0.32 153114. 0.5537 14.68 0.1938 0.4150 0.0957 0.0447 0.472 5.945 4.998 351.710 0.672 22.233 6.446 0.32 153315. 0.5285 16.78 0.2215 0.4584 0.0931 0.0450 0.474 5.981 4.860 353.796 0.676 21.617 6.230 0.32 153531. 0.5037 18.88 0.2492 0.4984 0.0902 0.0451 0.476 5.997 4.710 354.765 0.678 20.949 6.022 0.32 153763. 0.4792 20.98 0.2769 0.5352 0.0871 0.0451 0.475 5.992 4.548 354.474 0.677 20.229 5.819 0.32 154010. 0.4551 23.08 0.3046 0.5689 0.0838 0.0449 0.473 5.964 4.374 352.779 0.674 19.456 5.624 0.32 154273. 0.4313 25.17 0.3323 0.5997 0.0802 0.0444 0.469 5.909 4.188 349.550 0.668 18.627 5.434 0.32 154552. 0.4078 27.27 0.3600 0.6277 0.0764 0.0438 0.462 5.827 3.990 344.679 0.658 17.746 5.250 0.32 154846. 0.3846 29.37 0.3877 0.6529 0.0724 0.0430 0.453 5.716 3.780 338.111 0.646 16.814 5.071 0.32 155156. 0.3616 31.47 0.4154 0.6755 0.0682 0.0419 0.442 5.576 3.561 329.838 0.630 15.839 4.897 0.32 155483. 0.3389 33.56 0.4430 0.6953 0.0638 0.0407 0.429 5.407 3.333 319.868 0.611 14.823 4.726 0.32 155825. 0.3164 35.66 0.4707 0.7124 0.0593 0.0392 0.413 5.210 3.097 308.214 0.589 13.773 4.557 0.32 156184. 0.2941 37.76 0.4984 0.7266 0.0547 0.0375 0.395 4.985 2.854 294.884 0.563 12.693 4.389 0.32 156559. 0.2719 39.86 0.5261 0.7375 0.0499 0.0356 0.375 4.731 2.605 279.882 0.535 11.585 4.221 0.32 156950. 0.2498 41.96 0.5538 0.7449 0.0450 0.0335 0.353 4.449 2.350 263.214 0.503 10.454 4.050 0.32 157357. 0.2277 44.05 0.5815 0.7480 0.0400 0.0311 0.328 4.140 2.091 244.882 0.468 9.301 3.873 0.32 157780. 0.2054 46.15 0.6092 0.7458 0.0350 0.0286 0.302 3.802 1.828 224.896 0.430 8.130 3.686 0.32 158220. 0.1828 48.25 0.6369 0.7369 0.0299 0.0258 0.273 3.436 1.561 203.270 0.388 6.944 3.484 0.32 158675. 0.1596 50.35 0.6646 0.7184 0.0247 0.0229 0.241 3.043 1.292 180.031 0.344 5.746 3.255 0.32 159147. 0.1357 52.44 0.6923 0.6856 0.0195 0.0197 0.208 2.624 1.021 155.219 0.296 4.539 2.982 0.32 159636. 0.1105 54.54 0.7199 0.6295 0.0143 0.0164 0.173 2.179 0.748 128.894 0.246 3.328 2.633 0.33 160140. 0.0835 56.64 0.7476 0.5298 0.0091 0.0129 0.136 1.710 0.476 101.141 0.193 2.116 2.133 0.33 160660. 0.0540 58.74 0.7753 0.3313 0.0039 0.0092 0.097 1.218 0.204 72.063 0.138 0.909 1.286 0.33 161194. 0.0213 60.83 0.8030 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 0.1096 0.0401 0.731 7.678 8.239 545.072 0.868 36.649 6.856 0.38 182625. 0.7217 2.50 0.0275 0.0727 0.1082 0.0409 0.745 7.829 8.137 555.751 0.885 36.191 6.641 0.38 182769. 0.6947 5.00 0.0550 0.1408 0.1067 0.0417 0.759 7.975 8.023 566.090 0.901 35.685 6.428 0.38 182928. 0.6677 7.50 0.0824 0.2044 0.1050 0.0424 0.772 8.113 7.897 575.890 0.917 35.126 6.220 0.38 183101. 0.6410 9.99 0.1099 0.2636 0.1032 0.0430 0.784 8.240 7.759 584.948 0.931 34.510 6.016 0.38 183290. 0.6145 12.49 0.1374 0.3186 0.1012 0.0436 0.795 8.354 7.607 593.047 0.944 33.834 5.818 0.38 183496. 0.5884 14.99 0.1649 0.3697 0.0990 0.0441 0.805 8.452 7.440 599.963 0.955 33.095 5.625 0.38 183718. 0.5627 17.49 0.1924 0.4169 0.0965 0.0445 0.812 8.529 7.259 605.457 0.964 32.288 5.438 0.38 183958. 0.5373 19.99 0.2199 0.4606 0.0939 0.0448 0.817 8.583 7.062 609.287 0.970 31.411 5.257 0.38 184215. 0.5123 22.49 0.2473 0.5010 0.0911 0.0450 0.820 8.610 6.848 611.208 0.973 30.461 5.082 0.38 184490. 0.4877 24.98 0.2748 0.5381 0.0880 0.0450 0.819 8.607 6.618 610.970 0.972 29.435 4.913 0.38 184784. 0.4635 27.48 0.3023 0.5722 0.0847 0.0448 0.816 8.570 6.370 608.332 0.968 28.332 4.749 0.38 185096. 0.4396 29.98 0.3298 0.6034 0.0812 0.0444 0.809 8.495 6.104 603.066 0.960 27.151 4.591 0.38 185426. 0.4160 32.48 0.3573 0.6319 0.0774 0.0438 0.798 8.382 5.821 594.981 0.947 25.893 4.438 0.38 185776. 0.3927 34.98 0.3848 0.6577 0.0734 0.0430 0.783 8.226 5.522 583.970 0.929 24.562 4.289 0.38 186144. 0.3696 37.48 0.4122 0.6809 0.0693 0.0419 0.764 8.030 5.208 570.012 0.907 23.167 4.144 0.38 186531. 0.3469 39.97 0.4397 0.7015 0.0649 0.0407 0.742 7.792 4.882 553.119 0.880 21.714 4.003 0.38 186937. 0.3244 42.47 0.4672 0.7195 0.0604 0.0392 0.715 7.513 4.544 533.312 0.849 20.210 3.864 0.38 187362. 0.3021 44.97 0.4947 0.7347 0.0558 0.0376 0.685 7.193 4.195 510.608 0.813 18.661 3.727 0.39 187806. 0.2799 47.47 0.5222 0.7470 0.0511 0.0357 0.650 6.832 3.838 485.014 0.772 17.073 3.589 0.39 188270. 0.2579 49.97 0.5497 0.7559 0.0462 0.0336 0.612 6.431 3.473 456.537 0.727 15.449 3.451 0.39 188752. 0.2358 52.47 0.5771 0.7610 0.0412 0.0313 0.570 5.990 3.101 425.185 0.677 13.795 3.308 0.39 189254. 0.2137 54.97 0.6046 0.7613 0.0362 0.0288 0.524 5.508 2.723 390.970 0.622 12.114 3.160 0.39 189774. 0.1912 57.46 0.6321 0.7556 0.0311 0.0260 0.475 4.986 2.340 353.915 0.563 10.410 2.999 0.39 190314. 0.1683 59.96 0.6596 0.7416 0.0260 0.0231 0.421 4.424 1.953 314.060 0.500 8.688 2.821 0.39 190873. 0.1446 62.46 0.6871 0.7151 0.0208 0.0200 0.364 3.824 1.563 271.471 0.432 6.953 2.612 0.39 191451. 0.1197 64.96 0.7146 0.6686 0.0156 0.0166 0.303 3.187 1.171 226.243 0.360 5.209 2.348 0.39 192048. 0.0932 67.46 0.7420 0.5850 0.0104 0.0131 0.239 2.515 0.779 178.512 0.284 3.463 1.978 0.39 192664. 0.0640 69.96 0.7695 0.4194 0.0052 0.0095 0.172 1.810 0.387 128.453 0.204 1.723 1.368 0.39 193297. 0.0312 72.45 0.7970 -0.0060 0.0000 0.0056 0.102 1.070 -0.003 75.981 0.121 -0.014 -0.019 0.39 193921. 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 0.1103 0.0401 1.159 10.438 11.289 864.453 1.179 50.212 5.923 0.44 213049. 0.7298 2.93 0.0276 0.0737 0.1090 0.0409 1.183 10.649 11.150 881.896 1.203 49.594 5.734 0.44 213219. 0.7022 5.86 0.0553 0.1426 0.1074 0.0416 1.205 10.853 10.996 898.790 1.226 48.908 5.549 0.44 213405. 0.6748 8.79 0.0829 0.2069 0.1058 0.0424 1.227 11.046 10.825 914.807 1.248 48.149 5.367 0.44 213609. 0.6476 11.73 0.1106 0.2668 0.1039 0.0431 1.247 11.225 10.636 929.610 1.268 47.311 5.190 0.44 213832. 0.6207 14.66 0.1382 0.3224 0.1019 0.0437 1.264 11.384 10.429 942.844 1.286 46.388 5.017 0.44 214074. 0.5942 17.59 0.1658 0.3739 0.0997 0.0442 1.280 11.521 10.201 954.133 1.302 45.376 4.850 0.44 214336. 0.5680 20.52 0.1935 0.4217 0.0973 0.0446 1.292 11.629 9.953 963.089 1.314 44.270 4.687 0.45 214619. 0.5423 23.45 0.2211 0.4658 0.0946 0.0449 1.300 11.704 9.682 969.314 1.322 43.065 4.530 0.45 214922. 0.5170 26.38 0.2488 0.5065 0.0917 0.0451 1.304 11.741 9.388 972.401 1.327 41.758 4.379 0.45 215246. 0.4920 29.32 0.2764 0.5440 0.0886 0.0450 1.303 11.736 9.070 971.949 1.326 40.345 4.233 0.45 215593. 0.4675 32.25 0.3040 0.5784 0.0853 0.0448 1.298 11.683 8.728 967.560 1.320 38.823 4.092 0.45 215961. 0.4433 35.18 0.3317 0.6100 0.0817 0.0444 1.286 11.578 8.362 958.865 1.308 37.192 3.955 0.45 216351. 0.4194 38.11 0.3593 0.6388 0.0779 0.0438 1.268 11.417 7.971 945.554 1.290 35.453 3.823 0.45 216763. 0.3959 41.04 0.3870 0.6649 0.0738 0.0430 1.244 11.199 7.557 927.463 1.265 33.614 3.696 0.45 217198. 0.3726 43.97 0.4146 0.6885 0.0696 0.0419 1.213 10.922 7.123 904.558 1.234 31.683 3.572 0.45 217654. 0.3496 46.90 0.4422 0.7096 0.0652 0.0406 1.176 10.588 6.671 876.864 1.196 29.673 3.451 0.45 218133. 0.3269 49.84 0.4699 0.7280 0.0606 0.0391 1.132 10.196 6.203 844.417 1.152 27.593 3.332 0.45 218635. 0.3044 52.77 0.4975 0.7437 0.0559 0.0374 1.083 9.747 5.722 807.242 1.101 25.450 3.215 0.45 219159. 0.2820 55.70 0.5252 0.7565 0.0511 0.0355 1.026 9.241 5.228 765.355 1.044 23.253 3.098 0.45 219705. 0.2598 58.63 0.5528 0.7660 0.0461 0.0333 0.964 8.679 4.723 718.767 0.981 21.006 2.980 0.45 220274. 0.2375 61.56 0.5804 0.7717 0.0411 0.0309 0.895 8.060 4.208 667.488 0.911 18.718 2.859 0.45 220866. 0.2151 64.49 0.6081 0.7728 0.0360 0.0283 0.820 7.384 3.685 611.544 0.834 16.392 2.733 0.45 221480. 0.1924 67.43 0.6357 0.7678 0.0308 0.0255 0.739 6.653 3.155 550.973 0.752 14.035 2.598 0.45 222117. 0.1692 70.36 0.6634 0.7544 0.0256 0.0225 0.652 5.866 2.620 485.846 0.663 11.653 2.446 0.45 222776. 0.1452 73.29 0.6910 0.7282 0.0203 0.0193 0.558 5.026 2.080 416.274 0.568 9.252 2.266 0.45 223457. 0.1199 76.22 0.7186 0.6808 0.0150 0.0159 0.459 4.135 1.538 342.423 0.467 6.841 2.037 0.46 224161. 0.0927 79.15 0.7463 0.5924 0.0097 0.0123 0.355 3.194 0.996 264.524 0.361 4.429 1.707 0.46 224887. 0.0625 82.08 0.7739 0.4063 0.0044 0.0085 0.245 2.208 0.455 182.876 0.249 2.025 1.129 0.46 225633. 0.0279 85.01 0.8016 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 0.1112 0.0402 1.735 13.673 14.857 1294.140 1.545 66.084 5.207 0.51 243467. 0.7360 3.33 0.0275 0.0737 0.1098 0.0410 1.771 13.954 14.680 1320.714 1.576 65.296 5.041 0.51 243660. 0.7084 6.67 0.0550 0.1426 0.1083 0.0418 1.806 14.226 14.483 1346.482 1.607 64.418 4.879 0.51 243872. 0.6809 10.00 0.0825 0.2069 0.1067 0.0426 1.838 14.484 14.264 1370.939 1.636 63.445 4.719 0.51 244105. 0.6536 13.34 0.1100 0.2668 0.1049 0.0433 1.869 14.724 14.021 1393.578 1.663 62.367 4.564 0.51 244358. 0.6267 16.67 0.1375 0.3225 0.1029 0.0439 1.896 14.938 13.754 1413.864 1.688 61.178 4.412 0.51 244634. 0.6001 20.01 0.1650 0.3741 0.1007 0.0444 1.919 15.121 13.460 1431.230 1.708 59.872 4.266 0.51 244932. 0.5739 23.34 0.1926 0.4220 0.0983 0.0449 1.938 15.268 13.139 1445.093 1.725 58.441 4.124 0.51 245253. 0.5482 26.67 0.2201 0.4662 0.0957 0.0452 1.951 15.371 12.788 1454.858 1.737 56.880 3.987 0.51 245598. 0.5228 30.01 0.2476 0.5071 0.0928 0.0453 1.958 15.424 12.406 1459.917 1.743 55.184 3.854 0.51 245967. 0.4979 33.34 0.2751 0.5448 0.0897 0.0453 1.957 15.422 11.994 1459.669 1.742 53.348 3.727 0.51 246360. 0.4733 36.68 0.3026 0.5795 0.0864 0.0451 1.949 15.357 11.549 1453.522 1.735 51.369 3.604 0.51 246779. 0.4491 40.01 0.3301 0.6113 0.0828 0.0447 1.932 15.224 11.072 1440.923 1.720 49.246 3.485 0.51 247222. 0.4253 43.35 0.3576 0.6405 0.0790 0.0441 1.906 15.018 10.562 1421.401 1.697 46.980 3.370 0.51 247690. 0.4017 46.68 0.3851 0.6670 0.0750 0.0433 1.870 14.735 10.023 1394.689 1.665 44.580 3.259 0.51 248184. 0.3784 50.01 0.4126 0.6911 0.0707 0.0422 1.825 14.376 9.456 1360.724 1.624 42.059 3.152 0.51 248702. 0.3554 53.35 0.4401 0.7127 0.0663 0.0410 1.770 13.941 8.865 1319.546 1.575 39.431 3.047 0.51 249246. 0.3327 56.68 0.4676 0.7317 0.0617 0.0395 1.705 13.431 8.253 1271.209 1.517 36.709 2.945 0.51 249816. 0.3102 60.02 0.4951 0.7482 0.0570 0.0377 1.630 12.845 7.622 1215.758 1.451 33.904 2.844 0.51 250410. 0.2879 63.35 0.5226 0.7619 0.0522 0.0358 1.546 12.184 6.975 1153.219 1.377 31.025 2.743 0.51 251030. 0.2657 66.68 0.5502 0.7725 0.0472 0.0336 1.453 11.449 6.313 1083.614 1.293 28.081 2.643 0.52 251676. 0.2435 70.02 0.5777 0.7796 0.0422 0.0313 1.350 10.639 5.639 1006.958 1.202 25.080 2.540 0.52 252346. 0.2212 73.35 0.6052 0.7824 0.0371 0.0287 1.238 9.755 4.953 923.286 1.102 22.029 2.433 0.52 253043. 0.1986 76.69 0.6327 0.7796 0.0318 0.0258 1.117 8.797 4.257 832.652 0.994 18.936 2.319 0.52 253764. 0.1755 80.02 0.6602 0.7692 0.0266 0.0228 0.986 7.767 3.554 735.156 0.878 15.808 2.193 0.52 254512. 0.1516 83.36 0.6877 0.7473 0.0213 0.0196 0.846 6.666 2.845 630.955 0.753 12.654 2.045 0.52 255284. 0.1265 86.69 0.7152 0.7064 0.0160 0.0161 0.698 5.497 2.132 520.284 0.621 9.484 1.859 0.52 256082. 0.0995 90.02 0.7427 0.6294 0.0106 0.0125 0.541 4.263 1.419 403.480 0.482 6.310 1.595 0.52 256904. 0.0697 93.36 0.7702 0.4671 0.0053 0.0087 0.377 2.969 0.707 280.977 0.335 3.145 1.141 0.52 257750. 0.0352 96.69 0.7977 -0.0054 0.0000 0.0047 0.204 1.610 -0.004 152.381 0.182 -0.019 -0.013 0.52 258574. 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 0.1121 0.0404 2.487 17.419 18.968 1854.783 1.968 84.369 4.638 0.57 273878. 0.7408 3.75 0.0275 0.0739 0.1108 0.0413 2.540 17.785 18.749 1893.774 2.009 83.395 4.490 0.57 274095. 0.7131 7.51 0.0550 0.1430 0.1094 0.0421 2.590 18.140 18.504 1931.603 2.049 82.307 4.345 0.57 274334. 0.6855 11.26 0.0826 0.2075 0.1078 0.0429 2.639 18.478 18.231 1967.542 2.088 81.093 4.203 0.57 274596. 0.6581 15.01 0.1101 0.2675 0.1060 0.0436 2.683 18.791 17.928 2000.830 2.123 79.746 4.064 0.57 274882. 0.6311 18.77 0.1376 0.3233 0.1040 0.0443 2.723 19.071 17.593 2030.678 2.155 78.254 3.930 0.57 275192. 0.6044 22.52 0.1651 0.3751 0.1018 0.0448 2.757 19.311 17.223 2056.259 2.182 76.609 3.799 0.57 275529. 0.5782 26.27 0.1927 0.4231 0.0994 0.0453 2.785 19.503 16.817 2076.716 2.203 74.802 3.673 0.57 275891. 0.5524 30.03 0.2202 0.4675 0.0968 0.0456 2.804 19.639 16.373 2091.181 2.219 72.826 3.551 0.57 276281. 0.5270 33.78 0.2477 0.5085 0.0939 0.0458 2.815 19.710 15.889 2098.775 2.227 70.675 3.434 0.57 276698. 0.5020 37.53 0.2752 0.5464 0.0908 0.0458 2.814 19.709 15.365 2098.617 2.227 68.342 3.321 0.57 277142. 0.4774 41.29 0.3028 0.5813 0.0875 0.0456 2.803 19.627 14.798 2089.863 2.217 65.824 3.212 0.57 277614. 0.4531 45.04 0.3303 0.6134 0.0839 0.0452 2.778 19.456 14.190 2071.708 2.198 63.118 3.107 0.57 278115. 0.4292 48.79 0.3578 0.6429 0.0800 0.0445 2.740 19.191 13.540 2043.475 2.168 60.226 3.005 0.57 278644. 0.4056 52.55 0.3853 0.6698 0.0760 0.0437 2.688 18.828 12.851 2004.768 2.127 57.160 2.907 0.58 279201. 0.3822 56.30 0.4129 0.6942 0.0717 0.0426 2.622 18.365 12.126 1955.499 2.075 53.936 2.813 0.58 279786. 0.3592 60.05 0.4404 0.7162 0.0672 0.0413 2.542 17.804 11.370 1895.730 2.011 50.573 2.720 0.58 280400. 0.3364 63.81 0.4679 0.7357 0.0626 0.0398 2.448 17.144 10.586 1825.547 1.937 47.087 2.630 0.58 281042. 0.3138 67.56 0.4954 0.7528 0.0578 0.0380 2.340 16.388 9.778 1745.024 1.852 43.494 2.542 0.58 281713. 0.2915 71.31 0.5230 0.7671 0.0529 0.0361 2.218 15.535 8.949 1654.208 1.755 39.804 2.454 0.58 282412. 0.2692 75.07 0.5505 0.7785 0.0479 0.0339 2.083 14.586 8.100 1553.132 1.648 36.029 2.366 0.58 283140. 0.2469 78.82 0.5780 0.7864 0.0428 0.0314 1.934 13.541 7.235 1441.824 1.530 32.180 2.276 0.58 283896. 0.2245 82.57 0.6055 0.7903 0.0376 0.0288 1.771 12.400 6.355 1320.334 1.401 28.266 2.183 0.58 284681. 0.2018 86.33 0.6331 0.7887 0.0323 0.0259 1.594 11.164 5.462 1188.742 1.261 24.296 2.084 0.58 285495. 0.1786 90.08 0.6606 0.7799 0.0270 0.0228 1.404 9.835 4.559 1047.194 1.111 20.280 1.975 0.58 286337. 0.1546 93.83 0.6881 0.7599 0.0216 0.0195 1.201 8.414 3.649 895.916 0.951 16.230 1.847 0.58 287207. 0.1294 97.59 0.7156 0.7214 0.0162 0.0160 0.986 6.905 2.734 735.250 0.780 12.159 1.686 0.59 288106. 0.1022 101.34 0.7432 0.6472 0.0107 0.0123 0.759 5.313 1.817 565.685 0.600 8.081 1.457 0.59 289033. 0.0720 105.09 0.7707 0.4862 0.0053 0.0085 0.520 3.643 0.902 387.860 0.412 4.014 1.055 0.59 289985. 0.0368 108.85 0.7982 -0.0141 -0.0001 0.0044 0.269 1.887 -0.013 200.934 0.213 -0.058 -0.030 0.59 290902. 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 0.1132 0.0408 3.447 21.723 23.649 2570.075 2.454 105.192 4.174 0.63 304279. 0.7443 4.17 0.0275 0.0739 0.1120 0.0417 3.521 22.190 23.388 2625.377 2.507 104.029 4.041 0.63 304520. 0.7166 8.35 0.0551 0.1430 0.1106 0.0426 3.593 22.645 23.094 2679.135 2.558 102.721 3.910 0.63 304786. 0.6890 12.52 0.0826 0.2075 0.1090 0.0434 3.661 23.077 22.764 2730.274 2.607 101.256 3.782 0.63 305077. 0.6617 16.69 0.1102 0.2676 0.1072 0.0441 3.725 23.478 22.397 2777.701 2.653 99.620 3.657 0.64 305396. 0.6347 20.86 0.1377 0.3234 0.1053 0.0448 3.782 23.838 21.988 2820.273 2.693 97.800 3.536 0.64 305742. 0.6081 25.04 0.1652 0.3753 0.1031 0.0454 3.831 24.146 21.535 2856.796 2.728 95.786 3.419 0.64 306117. 0.5819 29.21 0.1928 0.4233 0.1007 0.0459 3.870 24.394 21.035 2886.062 2.756 93.566 3.306 0.64 306521. 0.5560 33.38 0.2203 0.4678 0.0981 0.0462 3.898 24.569 20.488 2906.844 2.776 91.130 3.197 0.64 306956. 0.5307 37.55 0.2479 0.5090 0.0952 0.0464 3.913 24.663 19.890 2917.902 2.786 88.470 3.092 0.64 307421. 0.5057 41.73 0.2754 0.5471 0.0921 0.0464 3.913 24.664 19.240 2918.019 2.787 85.579 2.991 0.64 307917. 0.4811 45.90 0.3029 0.5822 0.0888 0.0462 3.897 24.562 18.537 2906.006 2.775 82.451 2.893 0.64 308444. 0.4568 50.07 0.3305 0.6145 0.0851 0.0458 3.863 24.349 17.780 2880.745 2.751 79.084 2.799 0.64 309002. 0.4329 54.24 0.3580 0.6442 0.0813 0.0452 3.810 24.015 16.970 2841.297 2.713 75.482 2.709 0.64 309592. 0.4092 58.42 0.3856 0.6714 0.0771 0.0443 3.738 23.557 16.110 2787.098 2.661 71.656 2.622 0.64 310213. 0.3859 62.59 0.4131 0.6962 0.0728 0.0432 3.645 22.973 15.204 2718.029 2.596 67.629 2.537 0.64 310866. 0.3628 66.76 0.4406 0.7186 0.0683 0.0419 3.533 22.265 14.259 2634.187 2.515 63.425 2.455 0.64 311550. 0.3400 70.93 0.4682 0.7386 0.0636 0.0403 3.400 21.432 13.279 2535.713 2.421 59.063 2.375 0.64 312266. 0.3174 75.11 0.4957 0.7562 0.0587 0.0385 3.249 20.477 12.267 2422.722 2.314 54.564 2.297 0.64 313013. 0.2950 79.28 0.5232 0.7711 0.0538 0.0365 3.078 19.400 11.228 2295.298 2.192 49.942 2.219 0.64 313792. 0.2726 83.45 0.5508 0.7832 0.0487 0.0342 2.888 18.202 10.164 2153.493 2.056 45.211 2.141 0.64 314603. 0.2503 87.63 0.5783 0.7920 0.0435 0.0317 2.678 16.882 9.079 1997.352 1.907 40.385 2.062 0.65 315445. 0.2278 91.80 0.6059 0.7969 0.0382 0.0290 2.450 15.442 7.976 1826.948 1.745 35.475 1.980 0.65 316319. 0.2051 95.97 0.6334 0.7966 0.0328 0.0261 2.202 13.882 6.856 1642.398 1.568 30.493 1.893 0.65 317225. 0.1818 100.14 0.6609 0.7892 0.0274 0.0229 1.936 12.204 5.722 1443.899 1.379 25.453 1.798 0.65 318162. 0.1577 104.32 0.6885 0.7711 0.0219 0.0196 1.652 10.411 4.579 1231.770 1.176 20.367 1.686 0.65 319131. 0.1323 108.49 0.7160 0.7350 0.0164 0.0160 1.350 8.507 3.429 1006.492 0.961 15.253 1.545 0.65 320131. 0.1049 112.66 0.7436 0.6635 0.0109 0.0122 1.031 6.498 2.277 768.750 0.734 10.128 1.343 0.65 321162. 0.0743 116.83 0.7711 0.5043 0.0054 0.0083 0.697 4.391 1.128 519.451 0.496 5.016 0.985 0.65 322222. 0.0383 121.01 0.7986 -0.0237 -0.0001 0.0041 0.345 2.172 -0.025 256.985 0.245 -0.112 -0.045 0.65 323227. 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 0.1145 0.0416 4.675 26.787 28.932 3486.122 3.026 128.690 3.764 0.70 334668. 0.7425 4.60 0.0276 0.0736 0.1133 0.0425 4.774 27.353 28.630 3559.842 3.090 127.344 3.648 0.70 334934. 0.7158 9.21 0.0552 0.1426 0.1119 0.0434 4.870 27.905 28.287 3631.645 3.153 125.818 3.533 0.70 335227. 0.6891 13.81 0.0829 0.2070 0.1104 0.0442 4.962 28.431 27.899 3700.108 3.212 124.096 3.420 0.70 335549. 0.6625 18.41 0.1105 0.2671 0.1087 0.0449 5.047 28.920 27.464 3763.767 3.267 122.159 3.310 0.70 335901. 0.6361 23.02 0.1381 0.3231 0.1067 0.0456 5.124 29.360 26.976 3821.060 3.317 119.991 3.202 0.70 336284. 0.6099 27.62 0.1657 0.3751 0.1046 0.0462 5.190 29.739 26.434 3870.353 3.360 117.576 3.098 0.70 336700. 0.5841 32.22 0.1933 0.4233 0.1022 0.0467 5.243 30.044 25.832 3909.954 3.394 114.901 2.997 0.70 337148. 0.5585 36.82 0.2209 0.4680 0.0996 0.0470 5.281 30.260 25.169 3938.129 3.419 111.953 2.899 0.70 337630. 0.5333 41.43 0.2486 0.5093 0.0967 0.0472 5.301 30.375 24.443 3953.131 3.432 108.721 2.804 0.70 338145. 0.5085 46.03 0.2762 0.5476 0.0936 0.0472 5.301 30.376 23.650 3953.200 3.432 105.196 2.713 0.70 338695. 0.4839 50.63 0.3038 0.5829 0.0902 0.0470 5.279 30.249 22.791 3936.633 3.417 101.372 2.626 0.70 339280. 0.4597 55.24 0.3314 0.6154 0.0865 0.0466 5.232 29.981 21.863 3901.836 3.387 97.247 2.541 0.70 339899. 0.4358 59.84 0.3590 0.6454 0.0826 0.0459 5.160 29.563 20.869 3847.456 3.340 92.824 2.460 0.70 340553. 0.4122 64.44 0.3867 0.6729 0.0784 0.0450 5.059 28.989 19.811 3772.734 3.275 88.121 2.382 0.70 341242. 0.3888 69.05 0.4143 0.6980 0.0740 0.0439 4.932 28.258 18.697 3677.517 3.193 83.163 2.306 0.70 341966. 0.3657 73.65 0.4419 0.7208 0.0694 0.0425 4.777 27.370 17.532 3561.971 3.092 77.981 2.232 0.71 342724. 0.3428 78.25 0.4695 0.7412 0.0646 0.0409 4.595 26.327 16.322 3426.308 2.974 72.602 2.161 0.71 343518. 0.3201 82.85 0.4971 0.7593 0.0596 0.0391 4.386 25.132 15.074 3270.714 2.839 67.048 2.090 0.71 344346. 0.2976 87.46 0.5247 0.7748 0.0546 0.0370 4.151 23.784 13.791 3095.332 2.687 61.340 2.021 0.71 345209. 0.2752 92.06 0.5524 0.7875 0.0494 0.0346 3.889 22.285 12.477 2900.243 2.518 55.496 1.951 0.71 346107. 0.2528 96.66 0.5800 0.7970 0.0441 0.0321 3.601 20.635 11.135 2685.530 2.331 49.530 1.881 0.71 347040. 0.2302 101.27 0.6076 0.8026 0.0387 0.0293 3.287 18.835 9.770 2451.295 2.128 43.458 1.808 0.71 348008. 0.2072 105.87 0.6352 0.8032 0.0332 0.0262 2.947 16.887 8.385 2197.706 1.908 37.296 1.730 0.71 349010. 0.1838 110.47 0.6628 0.7967 0.0276 0.0230 2.582 14.792 6.982 1925.076 1.671 31.058 1.645 0.71 350047. 0.1594 115.08 0.6905 0.7796 0.0220 0.0195 2.191 12.555 5.567 1633.919 1.418 24.762 1.545 0.71 351119. 0.1337 119.68 0.7181 0.7441 0.0164 0.0158 1.777 10.181 4.143 1325.031 1.150 18.428 1.418 0.72 352226. 0.1059 124.28 0.7457 0.6715 0.0107 0.0119 1.340 7.681 2.716 999.580 0.868 12.081 1.232 0.72 353366. 0.0745 128.88 0.7733 0.5023 0.0051 0.0079 0.884 5.065 1.292 659.123 0.572 5.747 0.889 0.72 354538. 0.0371 133.49 0.8009 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 0.1158 0.0437 6.367 33.444 34.840 4748.243 3.779 154.970 3.328 0.76 365045. 0.7204 5.01 0.0275 0.0710 0.1147 0.0445 6.487 34.071 34.506 4837.166 3.849 153.481 3.236 0.76 365332. 0.6970 10.01 0.0551 0.1380 0.1135 0.0453 6.602 34.675 34.122 4922.947 3.918 151.776 3.144 0.76 365650. 0.6735 15.02 0.0826 0.2010 0.1120 0.0460 6.710 35.245 33.685 5003.837 3.982 149.832 3.053 0.76 366000. 0.6499 20.02 0.1101 0.2602 0.1104 0.0467 6.810 35.767 33.190 5078.040 4.041 147.628 2.964 0.76 366383. 0.6263 25.03 0.1376 0.3157 0.1085 0.0473 6.898 36.230 32.630 5143.681 4.093 145.139 2.877 0.76 366800. 0.6028 30.03 0.1652 0.3676 0.1064 0.0478 6.972 36.618 32.002 5198.824 4.137 142.346 2.792 0.76 367252. 0.5792 35.04 0.1927 0.4160 0.1041 0.0482 7.029 36.919 31.302 5241.479 4.171 139.230 2.709 0.76 367740. 0.5558 40.04 0.2202 0.4612 0.1015 0.0485 7.067 37.117 30.525 5269.636 4.193 135.776 2.627 0.76 368265. 0.5323 45.05 0.2478 0.5032 0.0987 0.0486 7.082 37.198 29.669 5281.220 4.203 131.970 2.548 0.76 368827. 0.5090 50.05 0.2753 0.5422 0.0955 0.0485 7.073 37.149 28.732 5274.142 4.197 127.800 2.471 0.76 369426. 0.4857 55.06 0.3028 0.5783 0.0921 0.0483 7.035 36.952 27.711 5246.296 4.175 123.260 2.396 0.77 370063. 0.4625 60.06 0.3303 0.6116 0.0885 0.0478 6.967 36.596 26.607 5195.658 4.135 118.347 2.323 0.77 370738. 0.4394 65.07 0.3579 0.6423 0.0845 0.0471 6.867 36.066 25.419 5120.395 4.075 113.064 2.252 0.77 371451. 0.4163 70.07 0.3854 0.6705 0.0803 0.0462 6.731 35.354 24.152 5019.295 3.994 107.430 2.183 0.77 372202. 0.3934 75.08 0.4129 0.6962 0.0759 0.0450 6.560 34.456 22.815 4891.920 3.893 101.479 2.115 0.77 372990. 0.3705 80.08 0.4405 0.7197 0.0712 0.0436 6.354 33.374 21.414 4738.249 3.771 95.248 2.050 0.77 373816. 0.3479 85.09 0.4680 0.7407 0.0664 0.0419 6.113 32.107 19.957 4558.353 3.627 88.769 1.986 0.77 374679. 0.3253 90.09 0.4955 0.7595 0.0614 0.0400 5.837 30.655 18.451 4352.287 3.463 82.072 1.923 0.77 375580. 0.3029 95.10 0.5230 0.7758 0.0562 0.0379 5.525 29.020 16.902 4120.112 3.279 75.181 1.861 0.77 376519. 0.2805 100.10 0.5506 0.7893 0.0509 0.0355 5.179 27.202 15.315 3861.932 3.073 68.119 1.799 0.77 377495. 0.2581 105.11 0.5781 0.7998 0.0455 0.0329 4.798 25.202 13.693 3577.962 2.847 60.905 1.736 0.77 378509. 0.2355 110.11 0.6056 0.8066 0.0400 0.0301 4.383 23.022 12.040 3268.523 2.601 53.556 1.671 0.78 379561. 0.2126 115.12 0.6332 0.8084 0.0345 0.0270 3.935 20.667 10.362 2934.136 2.335 46.090 1.602 0.78 380650. 0.1891 120.12 0.6607 0.8033 0.0288 0.0237 3.454 18.141 8.662 2575.577 2.050 38.527 1.525 0.78 381776. 0.1646 125.13 0.6882 0.7874 0.0231 0.0202 2.942 15.454 6.944 2194.015 1.746 30.885 1.435 0.78 382940. 0.1387 130.13 0.7157 0.7531 0.0173 0.0165 2.402 12.616 5.213 1791.112 1.425 23.188 1.320 0.78 384141. 0.1105 135.14 0.7433 0.6823 0.0116 0.0126 1.836 9.643 3.476 1369.112 1.090 15.463 1.152 0.78 385379. 0.0787 140.15 0.7708 0.5211 0.0058 0.0086 1.248 6.557 1.741 930.894 0.741 7.742 0.848 0.78 386651. 0.0410 145.15 0.7983 -0.0008 0.0000 0.0044 0.638 3.350 -0.001 475.551 0.378 -0.006 -0.001 0.79 387869. 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 0.1172 0.0484 8.970 43.488 41.377 6688.700 4.913 184.044 2.806 0.83 395406. 0.6619 5.43 0.0275 0.0652 0.1162 0.0491 9.103 44.132 41.022 6787.813 4.986 182.464 2.741 0.83 395715. 0.6438 10.85 0.0551 0.1274 0.1151 0.0498 9.226 44.732 40.609 6879.982 5.054 180.630 2.677 0.83 396058. 0.6257 16.28 0.0826 0.1866 0.1137 0.0504 9.337 45.270 40.133 6962.754 5.115 178.511 2.614 0.83 396436. 0.6074 21.70 0.1102 0.2429 0.1122 0.0509 9.433 45.732 39.586 7033.899 5.167 176.077 2.553 0.83 396850. 0.5890 27.13 0.1377 0.2964 0.1104 0.0513 9.509 46.105 38.960 7091.223 5.209 173.295 2.492 0.83 397302. 0.5704 32.55 0.1653 0.3471 0.1084 0.0516 9.565 46.374 38.251 7132.626 5.239 170.139 2.432 0.83 397794. 0.5517 37.98 0.1928 0.3952 0.1061 0.0518 9.596 46.527 37.452 7156.029 5.257 166.584 2.374 0.83 398325. 0.5327 43.41 0.2204 0.4407 0.1036 0.0518 9.601 46.548 36.558 7159.404 5.259 162.608 2.316 0.83 398896. 0.5135 48.83 0.2479 0.4836 0.1008 0.0517 9.576 46.427 35.565 7140.770 5.245 158.193 2.259 0.83 399508. 0.4941 54.26 0.2755 0.5239 0.0977 0.0513 9.519 46.150 34.470 7098.139 5.214 153.325 2.203 0.83 400162. 0.4743 59.68 0.3030 0.5617 0.0943 0.0508 9.427 45.704 33.272 7029.528 5.164 147.994 2.147 0.83 400856. 0.4541 65.11 0.3305 0.5970 0.0906 0.0502 9.297 45.076 31.969 6932.949 5.093 142.199 2.091 0.83 401592. 0.4337 70.53 0.3581 0.6298 0.0866 0.0492 9.128 44.254 30.563 6806.559 5.000 135.942 2.037 0.83 402369. 0.4129 75.96 0.3856 0.6601 0.0823 0.0481 8.917 43.231 29.058 6649.117 4.884 129.248 1.982 0.83 403187. 0.3918 81.39 0.4132 0.6880 0.0778 0.0467 8.663 42.003 27.463 6460.279 4.745 122.157 1.928 0.83 404046. 0.3706 86.81 0.4407 0.7134 0.0731 0.0451 8.368 40.572 25.790 6240.176 4.584 114.714 1.875 0.83 404946. 0.3491 92.24 0.4683 0.7364 0.0681 0.0433 8.031 38.938 24.047 5988.938 4.399 106.962 1.821 0.83 405886. 0.3275 97.66 0.4958 0.7569 0.0630 0.0413 7.653 37.102 22.243 5706.510 4.192 98.937 1.768 0.84 406867. 0.3058 103.09 0.5234 0.7748 0.0578 0.0390 7.232 35.063 20.384 5392.835 3.961 90.669 1.714 0.84 407888. 0.2839 108.51 0.5509 0.7895 0.0523 0.0365 6.772 32.831 18.477 5049.619 3.709 82.184 1.660 0.84 408950. 0.2616 113.94 0.5785 0.8003 0.0468 0.0338 6.273 30.415 16.525 4678.005 3.436 73.504 1.602 0.84 410053. 0.2389 119.37 0.6060 0.8064 0.0412 0.0309 5.737 27.815 14.535 4278.085 3.143 64.652 1.541 0.84 411196. 0.2155 124.79 0.6336 0.8065 0.0354 0.0278 5.162 25.027 12.512 3849.312 2.828 55.652 1.474 0.84 412379. 0.1912 130.22 0.6611 0.7980 0.0296 0.0246 4.551 22.066 10.460 3393.815 2.493 46.525 1.398 0.84 413603. 0.1658 135.64 0.6886 0.7760 0.0238 0.0211 3.908 18.948 8.385 2914.333 2.141 37.295 1.305 0.84 414867. 0.1386 141.07 0.7162 0.7311 0.0178 0.0175 3.238 15.698 6.293 2414.429 1.774 27.989 1.182 0.85 416171. 0.1087 146.49 0.7437 0.6431 0.0119 0.0137 2.546 12.343 4.191 1898.394 1.394 18.641 1.001 0.85 417515. 0.0752 151.92 0.7713 0.4601 0.0059 0.0099 1.839 8.916 2.089 1371.299 1.007 9.290 0.691 0.85 418895. 0.0366 157.34 0.7988 -0.0077 -0.0001 0.0060 1.117 5.415 -0.020 832.835 0.612 -0.091 -0.011 0.85 420229. 0.0000 PROP RPM = 14000 V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM (mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - - 0.00 0.0000 0.0000 0.1178 0.0557 12.903 58.091 48.211 9621.995 6.563 214.441 2.273 0.89 425791. 0.5787 5.86 0.0276 0.0572 0.1169 0.0565 13.074 58.857 47.867 9748.946 6.650 212.912 2.227 0.89 426118. 0.5650 11.71 0.0552 0.1121 0.1159 0.0571 13.228 59.552 47.462 9864.009 6.728 211.109 2.182 0.89 426482. 0.5514 17.57 0.0828 0.1648 0.1148 0.0577 13.359 60.143 46.984 9961.940 6.795 208.985 2.139 0.89 426883. 0.5377 23.43 0.1105 0.2154 0.1134 0.0581 13.462 60.606 46.424 10038.602 6.847 206.496 2.098 0.89 427325. 0.5241 29.29 0.1381 0.2642 0.1118 0.0584 13.530 60.914 45.772 10089.564 6.882 203.595 2.058 0.89 427809. 0.5105 35.14 0.1657 0.3111 0.1100 0.0586 13.559 61.044 45.018 10111.057 6.897 200.239 2.019 0.89 428337. 0.4969 41.00 0.1933 0.3564 0.1079 0.0585 13.545 60.978 44.152 10100.160 6.889 196.388 1.983 0.89 428909. 0.4832 46.86 0.2209 0.4000 0.1055 0.0582 13.484 60.704 43.168 10054.852 6.858 192.012 1.947 0.89 429525. 0.4692 52.71 0.2485 0.4420 0.1027 0.0578 13.375 60.215 42.060 9973.791 6.803 187.084 1.913 0.89 430188. 0.4549 58.57 0.2761 0.4824 0.0997 0.0571 13.217 59.504 40.824 9856.060 6.723 181.585 1.879 0.89 430896. 0.4402 64.43 0.3037 0.5211 0.0964 0.0562 13.009 58.568 39.457 9700.936 6.617 175.504 1.845 0.89 431649. 0.4250 70.29 0.3314 0.5580 0.0927 0.0551 12.750 57.401 37.957 9507.741 6.485 168.834 1.811 0.89 432448. 0.4091 76.14 0.3590 0.5930 0.0887 0.0537 12.439 56.001 36.327 9275.777 6.327 161.583 1.776 0.89 433292. 0.3926 82.00 0.3866 0.6260 0.0845 0.0522 12.076 54.365 34.572 9004.807 6.142 153.776 1.741 0.90 434181. 0.3755 87.86 0.4142 0.6570 0.0799 0.0504 11.661 52.498 32.703 8695.530 5.931 145.462 1.706 0.90 435115. 0.3577 93.72 0.4418 0.6859 0.0751 0.0484 11.197 50.408 30.733 8349.363 5.695 136.699 1.670 0.90 436092. 0.3394 99.57 0.4694 0.7125 0.0700 0.0461 10.685 48.103 28.674 7967.530 5.435 127.540 1.632 0.90 437114. 0.3205 105.43 0.4970 0.7368 0.0648 0.0437 10.126 45.587 26.537 7550.846 5.150 118.035 1.594 0.90 438179. 0.3011 111.29 0.5246 0.7584 0.0594 0.0411 9.521 42.863 24.331 7099.612 4.843 108.223 1.554 0.90 439288. 0.2812 117.14 0.5523 0.7767 0.0539 0.0383 8.873 39.945 22.063 6616.430 4.513 98.138 1.512 0.90 440441. 0.2605 123.00 0.5799 0.7901 0.0482 0.0354 8.195 36.894 19.740 6111.054 4.168 87.805 1.465 0.90 441637. 0.2387 128.86 0.6075 0.7939 0.0424 0.0325 7.515 33.833 17.363 5603.955 3.822 77.232 1.405 0.90 442877. 0.2148 134.72 0.6351 0.7869 0.0365 0.0295 6.820 30.706 14.940 5085.954 3.469 66.455 1.332 0.91 444160. 0.1889 140.57 0.6627 0.7675 0.0305 0.0263 6.096 27.445 12.482 4545.831 3.101 55.518 1.245 0.91 445486. 0.1614 146.43 0.6903 0.7296 0.0244 0.0231 5.349 24.081 9.994 3988.621 2.721 44.454 1.137 0.91 446856. 0.1318 152.29 0.7179 0.6629 0.0183 0.0198 4.587 20.651 7.488 3420.530 2.333 33.305 0.993 0.91 448268. 0.0996 158.14 0.7455 0.5491 0.0121 0.0165 3.820 17.197 4.973 2848.463 1.943 22.122 0.792 0.91 449722. 0.0648 164.00 0.7732 0.3529 0.0060 0.0132 3.057 13.761 2.466 2279.244 1.555 10.969 0.491 0.92 451217. 0.0283 169.86 0.8008 -0.0065 -0.0001 0.0099 2.294 10.329 -0.033 1710.916 1.167 -0.147 -0.009 0.92 452695. 0.0000