22x10E (22x10E.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 0.0771 0.0269 0.011 0.702 0.576 8.305 0.079 2.561 31.441 0.09 44336. 0.6363 0.43 0.0206 0.0577 0.0757 0.0271 0.011 0.707 0.565 8.369 0.080 2.514 30.630 0.09 44360. 0.6142 0.86 0.0412 0.1123 0.0742 0.0272 0.011 0.712 0.554 8.424 0.080 2.464 29.823 0.09 44385. 0.5920 1.29 0.0618 0.1639 0.0726 0.0274 0.011 0.716 0.542 8.471 0.081 2.411 29.020 0.09 44412. 0.5698 1.72 0.0825 0.2126 0.0709 0.0275 0.011 0.719 0.529 8.506 0.081 2.354 28.224 0.09 44441. 0.5477 2.15 0.1031 0.2583 0.0691 0.0276 0.011 0.721 0.516 8.529 0.081 2.295 27.433 0.09 44472. 0.5255 2.58 0.1237 0.3011 0.0672 0.0276 0.011 0.722 0.502 8.538 0.082 2.231 26.650 0.09 44505. 0.5034 3.01 0.1443 0.3410 0.0652 0.0276 0.011 0.721 0.487 8.532 0.081 2.165 25.872 0.09 44540. 0.4814 3.44 0.1649 0.3781 0.0631 0.0275 0.011 0.719 0.471 8.509 0.081 2.094 25.100 0.09 44578. 0.4594 3.87 0.1855 0.4123 0.0608 0.0274 0.011 0.716 0.454 8.467 0.081 2.020 24.333 0.09 44617. 0.4374 4.29 0.2061 0.4437 0.0585 0.0272 0.011 0.710 0.437 8.404 0.080 1.942 23.569 0.09 44659. 0.4154 4.72 0.2268 0.4723 0.0560 0.0269 0.011 0.703 0.418 8.319 0.079 1.861 22.807 0.09 44703. 0.3934 5.15 0.2474 0.4981 0.0535 0.0266 0.011 0.694 0.399 8.211 0.078 1.775 22.045 0.09 44749. 0.3714 5.58 0.2680 0.5208 0.0508 0.0261 0.011 0.683 0.379 8.080 0.077 1.686 21.280 0.09 44798. 0.3494 6.01 0.2886 0.5406 0.0480 0.0256 0.011 0.670 0.358 7.926 0.076 1.594 20.508 0.09 44849. 0.3274 6.44 0.3092 0.5571 0.0451 0.0251 0.010 0.655 0.337 7.748 0.074 1.499 19.725 0.09 44903. 0.3054 6.87 0.3298 0.5702 0.0422 0.0244 0.010 0.638 0.315 7.547 0.072 1.401 18.928 0.09 44959. 0.2833 7.30 0.3504 0.5796 0.0392 0.0237 0.010 0.619 0.292 7.322 0.070 1.300 18.109 0.09 45017. 0.2611 7.73 0.3711 0.5850 0.0361 0.0229 0.009 0.598 0.269 7.073 0.068 1.197 17.262 0.09 45078. 0.2389 8.16 0.3917 0.5859 0.0329 0.0220 0.009 0.575 0.246 6.801 0.065 1.092 16.379 0.09 45142. 0.2165 8.59 0.4123 0.5818 0.0297 0.0210 0.009 0.550 0.222 6.505 0.062 0.986 15.449 0.09 45208. 0.1940 9.02 0.4329 0.5717 0.0264 0.0200 0.008 0.523 0.197 6.187 0.059 0.877 14.459 0.09 45277. 0.1713 9.45 0.4535 0.5547 0.0231 0.0189 0.008 0.494 0.173 5.845 0.056 0.768 13.392 0.09 45349. 0.1484 9.88 0.4741 0.5294 0.0198 0.0177 0.007 0.463 0.148 5.482 0.052 0.657 12.224 0.09 45423. 0.1253 10.31 0.4947 0.4937 0.0164 0.0165 0.007 0.431 0.123 5.097 0.049 0.546 10.925 0.09 45499. 0.1021 10.74 0.5154 0.4449 0.0131 0.0152 0.006 0.397 0.098 4.693 0.045 0.435 9.452 0.09 45579. 0.0788 11.17 0.5360 0.3790 0.0098 0.0138 0.006 0.361 0.073 4.270 0.041 0.324 7.743 0.09 45661. 0.0558 11.60 0.5566 0.2900 0.0065 0.0124 0.005 0.324 0.048 3.831 0.037 0.214 5.705 0.09 45746. 0.0334 12.03 0.5772 0.1685 0.0032 0.0109 0.005 0.285 0.024 3.378 0.032 0.106 3.197 0.09 45833. 0.0132 12.45 0.5978 -0.0018 0.0000 0.0094 0.004 0.246 0.000 2.910 0.028 -0.001 -0.033 0.09 45922. 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 0.0775 0.0249 0.083 2.601 2.313 61.558 0.294 10.289 17.045 0.17 88670. 0.6914 0.87 0.0209 0.0632 0.0760 0.0251 0.083 2.626 2.271 62.128 0.297 10.099 16.576 0.17 88718. 0.6662 1.74 0.0417 0.1228 0.0745 0.0253 0.084 2.647 2.225 62.634 0.299 9.897 16.113 0.17 88770. 0.6410 2.61 0.0626 0.1790 0.0729 0.0255 0.085 2.665 2.177 63.061 0.301 9.681 15.655 0.17 88825. 0.6160 3.48 0.0835 0.2318 0.0712 0.0256 0.085 2.679 2.125 63.397 0.303 9.453 15.204 0.17 88884. 0.5911 4.35 0.1043 0.2813 0.0693 0.0257 0.085 2.689 2.071 63.629 0.304 9.210 14.759 0.17 88947. 0.5664 5.22 0.1252 0.3276 0.0674 0.0258 0.085 2.694 2.013 63.744 0.304 8.953 14.322 0.17 89015. 0.5419 6.09 0.1461 0.3707 0.0654 0.0258 0.085 2.693 1.952 63.728 0.304 8.681 13.891 0.17 89086. 0.5176 6.96 0.1670 0.4107 0.0632 0.0257 0.085 2.686 1.887 63.566 0.304 8.394 13.466 0.17 89162. 0.4934 7.83 0.1878 0.4476 0.0609 0.0256 0.085 2.673 1.819 63.244 0.302 8.092 13.048 0.17 89242. 0.4694 8.70 0.2087 0.4816 0.0585 0.0254 0.084 2.652 1.748 62.745 0.300 7.774 12.635 0.17 89327. 0.4455 9.56 0.2296 0.5127 0.0560 0.0251 0.083 2.623 1.673 62.057 0.296 7.441 12.226 0.17 89417. 0.4218 10.43 0.2504 0.5408 0.0534 0.0247 0.082 2.585 1.594 61.173 0.292 7.092 11.822 0.18 89512. 0.3981 11.30 0.2713 0.5659 0.0507 0.0243 0.081 2.539 1.513 60.089 0.287 6.729 11.419 0.18 89611. 0.3746 12.17 0.2922 0.5880 0.0478 0.0238 0.079 2.485 1.428 58.803 0.281 6.353 11.017 0.18 89716. 0.3512 13.04 0.3130 0.6069 0.0449 0.0232 0.077 2.422 1.341 57.312 0.274 5.965 10.613 0.18 89825. 0.3278 13.91 0.3339 0.6224 0.0419 0.0225 0.075 2.350 1.251 55.615 0.266 5.566 10.205 0.18 89940. 0.3044 14.78 0.3548 0.6344 0.0388 0.0217 0.072 2.270 1.159 53.709 0.256 5.156 9.789 0.18 90060. 0.2811 15.65 0.3756 0.6424 0.0357 0.0209 0.069 2.180 1.065 51.595 0.246 4.737 9.362 0.18 90184. 0.2577 16.52 0.3965 0.6460 0.0324 0.0199 0.066 2.082 0.969 49.273 0.235 4.309 8.918 0.18 90315. 0.2341 17.39 0.4174 0.6445 0.0292 0.0189 0.063 1.975 0.871 46.745 0.223 3.875 8.453 0.18 90450. 0.2104 18.26 0.4382 0.6371 0.0259 0.0178 0.059 1.860 0.772 44.012 0.210 3.435 7.958 0.18 90591. 0.1865 19.13 0.4591 0.6224 0.0225 0.0166 0.055 1.736 0.672 41.081 0.196 2.990 7.422 0.18 90737. 0.1623 20.00 0.4800 0.5988 0.0191 0.0153 0.051 1.604 0.571 37.956 0.181 2.542 6.829 0.18 90888. 0.1377 20.87 0.5009 0.5634 0.0158 0.0140 0.046 1.464 0.470 34.647 0.165 2.093 6.159 0.18 91045. 0.1127 21.74 0.5217 0.5125 0.0124 0.0126 0.042 1.317 0.369 31.166 0.149 1.643 5.377 0.18 91208. 0.0872 22.61 0.5426 0.4394 0.0090 0.0111 0.037 1.163 0.269 27.525 0.131 1.197 4.434 0.18 91376. 0.0613 23.48 0.5635 0.3336 0.0057 0.0096 0.032 1.003 0.170 23.744 0.113 0.755 3.241 0.18 91549. 0.0356 24.35 0.5843 0.1751 0.0024 0.0080 0.027 0.838 0.072 19.841 0.095 0.319 1.640 0.18 91728. 0.0117 25.22 0.6052 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 0.0779 0.0241 0.270 5.676 5.235 201.450 0.641 23.284 11.786 0.26 133002. 0.7192 1.29 0.0207 0.0650 0.0765 0.0244 0.273 5.732 5.139 203.446 0.648 22.860 11.458 0.26 133073. 0.6928 2.59 0.0414 0.1263 0.0750 0.0246 0.275 5.782 5.038 205.223 0.653 22.408 11.134 0.26 133150. 0.6665 3.88 0.0621 0.1840 0.0734 0.0248 0.277 5.825 4.929 206.738 0.658 21.926 10.815 0.26 133232. 0.6404 5.17 0.0828 0.2382 0.0717 0.0249 0.279 5.859 4.814 207.949 0.662 21.415 10.501 0.26 133320. 0.6145 6.47 0.1035 0.2890 0.0698 0.0250 0.280 5.883 4.693 208.810 0.665 20.873 10.193 0.26 133414. 0.5889 7.76 0.1242 0.3365 0.0679 0.0251 0.281 5.896 4.564 209.276 0.666 20.299 9.891 0.26 133514. 0.5635 9.05 0.1449 0.3808 0.0659 0.0251 0.281 5.897 4.427 209.302 0.666 19.692 9.594 0.26 133620. 0.5384 10.35 0.1656 0.4220 0.0638 0.0250 0.280 5.884 4.283 208.838 0.665 19.052 9.303 0.26 133733. 0.5135 11.64 0.1863 0.4602 0.0615 0.0249 0.279 5.856 4.132 207.835 0.662 18.378 9.017 0.26 133852. 0.4888 12.94 0.2070 0.4954 0.0591 0.0247 0.277 5.811 3.972 206.236 0.656 17.668 8.736 0.26 133978. 0.4644 14.23 0.2277 0.5277 0.0566 0.0244 0.274 5.747 3.805 203.999 0.649 16.923 8.459 0.26 134112. 0.4401 15.52 0.2484 0.5571 0.0540 0.0241 0.270 5.666 3.630 201.096 0.640 16.144 8.186 0.26 134252. 0.4160 16.82 0.2691 0.5836 0.0513 0.0237 0.265 5.565 3.447 197.513 0.629 15.334 7.917 0.26 134399. 0.3920 18.11 0.2898 0.6072 0.0485 0.0231 0.259 5.444 3.259 193.239 0.615 14.494 7.649 0.26 134554. 0.3682 19.40 0.3105 0.6278 0.0456 0.0225 0.252 5.304 3.064 188.264 0.599 13.627 7.381 0.26 134716. 0.3446 20.70 0.3311 0.6453 0.0426 0.0219 0.245 5.144 2.863 182.582 0.581 12.734 7.112 0.26 134886. 0.3210 21.99 0.3518 0.6594 0.0395 0.0211 0.236 4.964 2.657 176.186 0.561 11.818 6.840 0.26 135063. 0.2974 23.28 0.3725 0.6699 0.0364 0.0202 0.227 4.764 2.446 169.074 0.538 10.881 6.563 0.26 135248. 0.2738 24.58 0.3932 0.6763 0.0332 0.0193 0.216 4.543 2.232 161.245 0.513 9.926 6.277 0.26 135440. 0.2501 25.87 0.4139 0.6782 0.0300 0.0183 0.205 4.302 2.013 152.704 0.486 8.954 5.979 0.26 135640. 0.2263 27.16 0.4346 0.6746 0.0267 0.0172 0.192 4.042 1.792 143.458 0.457 7.969 5.664 0.26 135849. 0.2022 28.46 0.4553 0.6644 0.0233 0.0160 0.179 3.762 1.568 133.522 0.425 6.973 5.325 0.26 136065. 0.1778 29.75 0.4760 0.6460 0.0200 0.0147 0.165 3.463 1.342 122.916 0.391 5.970 4.953 0.26 136289. 0.1530 31.05 0.4967 0.6168 0.0166 0.0134 0.150 3.146 1.116 111.667 0.355 4.963 4.532 0.27 136521. 0.1277 32.34 0.5174 0.5730 0.0132 0.0120 0.134 2.812 0.889 99.814 0.318 3.956 4.042 0.27 136761. 0.1017 33.63 0.5381 0.5081 0.0099 0.0105 0.117 2.462 0.664 87.402 0.278 2.954 3.446 0.27 137009. 0.0749 34.93 0.5588 0.4110 0.0066 0.0089 0.100 2.099 0.441 74.491 0.237 1.961 2.684 0.27 137265. 0.0475 36.22 0.5795 0.2600 0.0033 0.0073 0.082 1.723 0.221 61.146 0.195 0.982 1.637 0.27 137529. 0.0205 37.51 0.6002 0.0057 0.0001 0.0057 0.064 1.334 0.004 47.355 0.151 0.016 0.035 0.27 137793. 0.0001 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 0.0785 0.0238 0.632 9.960 9.378 471.346 1.125 41.713 9.024 0.35 177328. 0.7371 1.73 0.0207 0.0664 0.0771 0.0241 0.639 10.063 9.208 476.212 1.137 40.955 8.770 0.35 177424. 0.7098 3.45 0.0415 0.1290 0.0756 0.0243 0.644 10.154 9.026 480.552 1.147 40.147 8.519 0.35 177527. 0.6826 5.18 0.0622 0.1879 0.0739 0.0245 0.649 10.233 8.832 484.256 1.156 39.286 8.273 0.35 177637. 0.6557 6.91 0.0829 0.2432 0.0722 0.0246 0.653 10.295 8.627 487.223 1.163 38.371 8.031 0.35 177755. 0.6291 8.64 0.1036 0.2951 0.0704 0.0247 0.656 10.340 8.408 489.344 1.168 37.401 7.794 0.35 177881. 0.6028 10.36 0.1244 0.3435 0.0685 0.0248 0.658 10.365 8.177 490.508 1.171 36.373 7.562 0.35 178015. 0.5767 12.09 0.1451 0.3887 0.0664 0.0248 0.658 10.367 7.933 490.604 1.171 35.286 7.334 0.35 178157. 0.5510 13.82 0.1658 0.4308 0.0643 0.0247 0.656 10.344 7.675 489.515 1.169 34.139 7.112 0.35 178308. 0.5255 15.54 0.1865 0.4698 0.0620 0.0246 0.653 10.293 7.403 487.117 1.163 32.931 6.894 0.35 178468. 0.5003 17.27 0.2073 0.5058 0.0596 0.0244 0.648 10.212 7.117 483.278 1.154 31.658 6.680 0.35 178637. 0.4753 19.00 0.2280 0.5389 0.0571 0.0241 0.641 10.098 6.817 477.887 1.141 30.322 6.470 0.35 178815. 0.4506 20.73 0.2487 0.5691 0.0544 0.0238 0.631 9.950 6.503 470.879 1.124 28.925 6.264 0.35 179003. 0.4260 22.45 0.2694 0.5965 0.0517 0.0234 0.620 9.767 6.176 462.216 1.103 27.471 6.061 0.35 179200. 0.4017 24.18 0.2902 0.6211 0.0489 0.0228 0.606 9.548 5.837 451.871 1.079 25.964 5.859 0.35 179407. 0.3776 25.91 0.3109 0.6427 0.0459 0.0222 0.590 9.294 5.487 439.820 1.050 24.407 5.659 0.35 179624. 0.3535 27.63 0.3316 0.6612 0.0429 0.0215 0.571 9.003 5.127 426.042 1.017 22.804 5.458 0.35 179851. 0.3296 29.36 0.3523 0.6765 0.0398 0.0207 0.551 8.675 4.757 410.525 0.980 21.160 5.256 0.35 180088. 0.3058 31.09 0.3731 0.6883 0.0367 0.0199 0.527 8.310 4.379 393.260 0.939 19.478 5.051 0.35 180335. 0.2819 32.82 0.3938 0.6962 0.0334 0.0189 0.502 7.908 3.993 374.246 0.893 17.762 4.840 0.35 180593. 0.2579 34.54 0.4145 0.6997 0.0301 0.0179 0.474 7.470 3.601 353.493 0.844 16.017 4.620 0.35 180861. 0.2339 36.27 0.4352 0.6979 0.0268 0.0167 0.444 6.995 3.203 331.020 0.790 14.248 4.389 0.35 181139. 0.2095 38.00 0.4560 0.6897 0.0235 0.0155 0.412 6.484 2.801 306.861 0.733 12.461 4.141 0.35 181428. 0.1848 39.72 0.4767 0.6735 0.0201 0.0142 0.377 5.939 2.397 281.067 0.671 10.660 3.867 0.35 181728. 0.1597 41.45 0.4974 0.6465 0.0167 0.0128 0.340 5.361 1.990 253.707 0.606 8.852 3.558 0.35 182038. 0.1339 43.18 0.5181 0.6047 0.0133 0.0114 0.302 4.752 1.584 224.871 0.537 7.045 3.195 0.35 182359. 0.1072 44.91 0.5389 0.5410 0.0099 0.0098 0.261 4.114 1.180 194.678 0.465 5.247 2.748 0.35 182691. 0.0796 46.63 0.5596 0.4425 0.0065 0.0082 0.219 3.450 0.779 163.272 0.390 3.465 2.164 0.35 183033. 0.0510 48.36 0.5803 0.2826 0.0032 0.0066 0.175 2.764 0.384 130.817 0.312 1.710 1.333 0.35 183386. 0.0220 50.09 0.6010 -0.0059 0.0000 0.0049 0.130 2.054 -0.006 97.192 0.232 -0.025 -0.027 0.36 183734. 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 0.0793 0.0238 1.232 15.526 14.799 918.476 1.754 65.828 7.308 0.44 221648. 0.7499 2.16 0.0207 0.0672 0.0779 0.0240 1.245 15.690 14.532 928.176 1.773 64.639 7.101 0.44 221768. 0.7220 4.32 0.0414 0.1305 0.0763 0.0242 1.256 15.837 14.247 936.822 1.789 63.370 6.898 0.44 221897. 0.6944 6.47 0.0621 0.1901 0.0747 0.0244 1.266 15.961 13.943 944.201 1.803 62.019 6.698 0.44 222035. 0.6670 8.63 0.0829 0.2460 0.0730 0.0246 1.274 16.061 13.620 950.110 1.815 60.581 6.502 0.44 222183. 0.6400 10.79 0.1036 0.2984 0.0711 0.0247 1.280 16.133 13.277 954.333 1.823 59.056 6.310 0.44 222341. 0.6132 12.95 0.1243 0.3475 0.0692 0.0247 1.283 16.172 12.914 956.652 1.827 57.440 6.123 0.44 222509. 0.5868 15.10 0.1450 0.3933 0.0671 0.0248 1.283 16.175 12.529 956.839 1.827 55.730 5.939 0.44 222687. 0.5607 17.26 0.1657 0.4359 0.0650 0.0247 1.280 16.138 12.123 954.667 1.823 53.925 5.760 0.44 222876. 0.5349 19.42 0.1864 0.4754 0.0627 0.0246 1.274 16.057 11.696 949.891 1.814 52.022 5.585 0.44 223077. 0.5094 21.58 0.2071 0.5120 0.0603 0.0244 1.264 15.928 11.245 942.249 1.800 50.018 5.413 0.44 223288. 0.4841 23.73 0.2278 0.5457 0.0577 0.0241 1.249 15.747 10.772 931.514 1.779 47.913 5.245 0.44 223512. 0.4591 25.89 0.2486 0.5766 0.0551 0.0237 1.230 15.511 10.277 917.554 1.752 45.711 5.080 0.44 223747. 0.4344 28.05 0.2693 0.6047 0.0523 0.0233 1.207 15.219 9.761 900.291 1.719 43.419 4.918 0.44 223994. 0.4098 30.21 0.2900 0.6300 0.0494 0.0228 1.180 14.870 9.227 879.667 1.680 41.041 4.758 0.44 224253. 0.3854 32.36 0.3107 0.6524 0.0465 0.0221 1.147 14.464 8.675 855.636 1.634 38.585 4.598 0.44 224524. 0.3612 34.52 0.3314 0.6719 0.0434 0.0214 1.111 14.000 8.106 828.159 1.582 36.056 4.440 0.44 224808. 0.3371 36.68 0.3521 0.6882 0.0403 0.0206 1.069 13.476 7.523 797.206 1.523 33.460 4.280 0.44 225105. 0.3131 38.84 0.3728 0.7012 0.0371 0.0197 1.023 12.894 6.925 762.761 1.457 30.804 4.118 0.44 225414. 0.2890 40.99 0.3935 0.7104 0.0338 0.0188 0.972 12.253 6.316 724.821 1.384 28.095 3.953 0.44 225736. 0.2649 43.15 0.4143 0.7153 0.0305 0.0177 0.916 11.553 5.697 683.404 1.305 25.340 3.781 0.44 226071. 0.2407 45.31 0.4350 0.7152 0.0272 0.0165 0.856 10.794 5.069 638.552 1.220 22.546 3.600 0.44 226418. 0.2162 47.47 0.4557 0.7089 0.0238 0.0153 0.792 9.979 4.434 590.328 1.127 19.721 3.407 0.44 226779. 0.1913 49.63 0.4764 0.6948 0.0203 0.0139 0.723 9.109 3.794 538.834 1.029 16.876 3.194 0.44 227154. 0.1659 51.78 0.4971 0.6703 0.0169 0.0125 0.649 8.185 3.152 484.208 0.925 14.020 2.953 0.44 227541. 0.1398 53.94 0.5178 0.6310 0.0134 0.0110 0.572 7.212 2.510 426.633 0.815 11.165 2.669 0.44 227942. 0.1128 56.10 0.5385 0.5697 0.0100 0.0095 0.491 6.193 1.871 366.344 0.700 8.322 2.316 0.44 228357. 0.0845 58.26 0.5593 0.4723 0.0066 0.0079 0.407 5.133 1.238 303.632 0.580 5.507 1.849 0.44 228785. 0.0549 60.41 0.5800 0.3090 0.0033 0.0062 0.320 4.037 0.614 238.829 0.456 2.733 1.167 0.44 229225. 0.0244 62.57 0.6007 -0.0018 0.0000 0.0044 0.230 2.902 -0.003 171.665 0.328 -0.011 -0.007 0.44 229659. 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 0.0803 0.0239 2.141 22.490 21.580 1596.494 2.541 95.990 6.131 0.52 265958. 0.7596 2.59 0.0207 0.0676 0.0789 0.0242 2.164 22.731 21.194 1613.576 2.568 94.269 5.957 0.52 266103. 0.7315 5.18 0.0414 0.1314 0.0773 0.0244 2.184 22.945 20.780 1628.782 2.592 92.430 5.787 0.52 266259. 0.7036 7.77 0.0622 0.1914 0.0757 0.0246 2.202 23.127 20.339 1641.740 2.613 90.470 5.619 0.52 266426. 0.6759 10.36 0.0829 0.2477 0.0739 0.0247 2.215 23.273 19.870 1652.080 2.629 88.384 5.455 0.52 266604. 0.6486 12.95 0.1036 0.3006 0.0721 0.0248 2.225 23.376 19.372 1659.422 2.641 86.168 5.295 0.52 266794. 0.6216 15.54 0.1243 0.3500 0.0701 0.0249 2.231 23.432 18.844 1663.382 2.647 83.818 5.138 0.52 266997. 0.5949 18.13 0.1450 0.3962 0.0680 0.0249 2.231 23.435 18.285 1663.563 2.648 81.332 4.985 0.52 267212. 0.5686 20.72 0.1657 0.4392 0.0658 0.0248 2.226 23.378 17.694 1659.560 2.641 78.705 4.836 0.52 267440. 0.5426 23.31 0.1865 0.4792 0.0635 0.0247 2.214 23.257 17.071 1650.947 2.628 75.934 4.690 0.52 267681. 0.5168 25.90 0.2072 0.5163 0.0611 0.0245 2.196 23.064 16.415 1637.263 2.606 73.015 4.547 0.52 267936. 0.4914 28.49 0.2279 0.5505 0.0585 0.0242 2.170 22.794 15.725 1618.102 2.575 69.946 4.408 0.52 268206. 0.4662 31.08 0.2486 0.5819 0.0558 0.0239 2.137 22.444 15.003 1593.220 2.536 66.735 4.271 0.53 268489. 0.4413 33.67 0.2693 0.6106 0.0530 0.0234 2.095 22.011 14.251 1562.479 2.487 63.390 4.137 0.53 268786. 0.4165 36.26 0.2900 0.6365 0.0501 0.0228 2.046 21.494 13.471 1525.779 2.428 59.919 4.005 0.53 269098. 0.3920 38.84 0.3108 0.6596 0.0471 0.0222 1.989 20.892 12.665 1483.038 2.360 56.333 3.873 0.53 269425. 0.3676 41.43 0.3315 0.6798 0.0440 0.0215 1.923 20.204 11.834 1434.188 2.283 52.638 3.743 0.53 269766. 0.3434 44.02 0.3522 0.6970 0.0409 0.0206 1.850 19.429 10.982 1379.181 2.195 48.846 3.611 0.53 270123. 0.3192 46.61 0.3729 0.7109 0.0376 0.0197 1.767 18.567 10.109 1317.986 2.098 44.964 3.479 0.53 270495. 0.2950 49.20 0.3936 0.7212 0.0343 0.0187 1.677 17.617 9.218 1250.600 1.990 41.004 3.343 0.53 270882. 0.2707 51.79 0.4143 0.7273 0.0309 0.0176 1.578 16.581 8.313 1177.056 1.873 36.975 3.203 0.53 271284. 0.2463 54.38 0.4351 0.7286 0.0275 0.0164 1.472 15.460 7.394 1097.427 1.747 32.889 3.056 0.53 271702. 0.2216 56.97 0.4558 0.7239 0.0241 0.0151 1.357 14.254 6.465 1011.828 1.610 28.757 2.898 0.53 272136. 0.1965 59.56 0.4765 0.7115 0.0206 0.0138 1.234 12.966 5.529 920.441 1.465 24.595 2.725 0.53 272586. 0.1709 62.15 0.4972 0.6888 0.0171 0.0123 1.104 11.601 4.590 823.510 1.311 20.416 2.528 0.53 273051. 0.1445 64.74 0.5179 0.6515 0.0136 0.0108 0.967 10.162 3.651 721.365 1.148 16.238 2.295 0.53 273533. 0.1170 67.33 0.5386 0.5917 0.0101 0.0092 0.824 8.655 2.716 614.427 0.978 12.079 2.005 0.53 274031. 0.0881 69.92 0.5594 0.4944 0.0067 0.0075 0.675 7.089 1.789 503.216 0.801 7.959 1.613 0.53 274544. 0.0575 72.51 0.5801 0.3256 0.0033 0.0058 0.521 5.470 0.877 388.329 0.618 3.900 1.024 0.53 275073. 0.0256 75.10 0.6008 -0.0158 -0.0001 0.0040 0.361 3.788 -0.028 268.901 0.428 -0.127 -0.048 0.53 275585. 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 0.0816 0.0242 3.445 31.022 29.836 2569.216 3.505 132.712 5.267 0.61 310255. 0.7674 3.02 0.0207 0.0677 0.0801 0.0245 3.482 31.356 29.308 2596.839 3.543 130.361 5.119 0.61 310425. 0.7391 6.03 0.0414 0.1315 0.0786 0.0247 3.515 31.652 28.742 2621.381 3.576 127.846 4.973 0.61 310608. 0.7111 9.05 0.0620 0.1915 0.0769 0.0249 3.543 31.904 28.139 2642.235 3.604 125.162 4.830 0.61 310803. 0.6834 12.06 0.0827 0.2480 0.0752 0.0251 3.566 32.104 27.496 2658.804 3.627 122.304 4.691 0.61 311012. 0.6560 15.08 0.1034 0.3010 0.0733 0.0252 3.581 32.245 26.813 2670.473 3.643 119.265 4.554 0.61 311235. 0.6290 18.09 0.1241 0.3506 0.0713 0.0252 3.589 32.319 26.088 2676.619 3.651 116.040 4.421 0.61 311472. 0.6022 21.11 0.1447 0.3970 0.0692 0.0252 3.589 32.319 25.320 2676.594 3.651 112.624 4.291 0.61 311724. 0.5758 24.12 0.1654 0.4403 0.0670 0.0252 3.580 32.236 24.508 2669.758 3.642 109.013 4.164 0.61 311991. 0.5498 27.14 0.1861 0.4806 0.0647 0.0250 3.561 32.063 23.651 2655.431 3.622 105.201 4.040 0.61 312273. 0.5240 30.15 0.2068 0.5180 0.0622 0.0248 3.531 31.791 22.748 2632.876 3.592 101.184 3.919 0.61 312571. 0.4985 33.17 0.2274 0.5526 0.0596 0.0245 3.489 31.411 21.798 2601.413 3.549 96.958 3.801 0.61 312886. 0.4733 36.18 0.2481 0.5845 0.0569 0.0241 3.434 30.919 20.803 2560.635 3.493 92.533 3.685 0.61 313216. 0.4483 39.20 0.2688 0.6137 0.0540 0.0237 3.366 30.311 19.766 2510.312 3.425 87.919 3.571 0.61 313564. 0.4235 42.21 0.2895 0.6402 0.0511 0.0231 3.286 29.586 18.689 2450.288 3.343 83.130 3.460 0.61 313928. 0.3989 45.23 0.3101 0.6640 0.0480 0.0224 3.192 28.743 17.576 2380.436 3.247 78.177 3.349 0.61 314309. 0.3745 48.24 0.3308 0.6850 0.0449 0.0217 3.085 27.780 16.429 2300.651 3.139 73.074 3.239 0.61 314707. 0.3501 51.26 0.3515 0.7030 0.0417 0.0208 2.965 26.695 15.250 2210.857 3.016 67.833 3.129 0.61 315123. 0.3259 54.27 0.3722 0.7179 0.0384 0.0199 2.831 25.490 14.044 2111.010 2.880 62.466 3.017 0.62 315556. 0.3016 57.29 0.3928 0.7293 0.0350 0.0189 2.684 24.163 12.812 2001.108 2.730 56.988 2.904 0.62 316007. 0.2772 60.30 0.4135 0.7368 0.0316 0.0177 2.523 22.715 11.559 1881.201 2.566 51.413 2.787 0.62 316476. 0.2527 63.32 0.4342 0.7395 0.0281 0.0165 2.349 21.148 10.287 1751.407 2.389 45.757 2.664 0.62 316962. 0.2279 66.33 0.4549 0.7365 0.0246 0.0152 2.162 19.463 9.001 1611.916 2.199 40.036 2.533 0.62 317467. 0.2027 69.35 0.4755 0.7262 0.0211 0.0138 1.962 17.665 7.705 1463.017 1.996 34.270 2.389 0.62 317990. 0.1768 72.36 0.4962 0.7059 0.0175 0.0123 1.750 15.759 6.403 1305.109 1.780 28.479 2.225 0.62 318532. 0.1502 75.38 0.5169 0.6713 0.0139 0.0107 1.527 13.750 5.100 1138.720 1.553 22.686 2.032 0.62 319092. 0.1224 78.39 0.5376 0.6147 0.0104 0.0091 1.293 11.646 3.803 964.533 1.316 16.918 1.789 0.62 319671. 0.0930 81.41 0.5582 0.5204 0.0069 0.0074 1.051 9.459 2.518 783.398 1.069 11.202 1.458 0.62 320268. 0.0617 84.42 0.5789 0.3525 0.0034 0.0056 0.800 7.200 1.252 596.293 0.813 5.569 0.952 0.62 320883. 0.0284 87.44 0.5996 -0.0010 0.0000 0.0038 0.539 4.857 -0.002 402.210 0.549 -0.010 -0.002 0.62 321484. 0.0000 PROP RPM = 8000 V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM (mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - - 0.00 0.0000 0.0000 0.0832 0.0247 5.253 41.389 39.732 3917.427 4.676 176.726 4.600 0.70 354534. 0.7734 3.44 0.0207 0.0675 0.0817 0.0250 5.310 41.834 39.038 3959.533 4.726 173.642 4.472 0.70 354730. 0.7452 6.89 0.0413 0.1312 0.0802 0.0252 5.360 42.228 38.295 3996.856 4.771 170.336 4.346 0.70 354940. 0.7173 10.33 0.0620 0.1912 0.0785 0.0254 5.402 42.562 37.501 4028.434 4.809 166.803 4.222 0.70 355166. 0.6896 13.77 0.0826 0.2476 0.0767 0.0256 5.436 42.825 36.654 4053.342 4.838 163.035 4.102 0.70 355406. 0.6623 17.21 0.1033 0.3006 0.0748 0.0257 5.459 43.008 35.752 4070.637 4.859 159.023 3.984 0.70 355663. 0.6353 20.66 0.1239 0.3503 0.0728 0.0258 5.471 43.100 34.793 4079.356 4.869 154.760 3.869 0.70 355935. 0.6086 24.10 0.1446 0.3969 0.0707 0.0258 5.469 43.091 33.777 4078.522 4.868 150.239 3.756 0.70 356225. 0.5823 27.54 0.1653 0.4403 0.0684 0.0257 5.454 42.971 32.701 4067.140 4.855 145.454 3.647 0.70 356532. 0.5562 30.99 0.1859 0.4809 0.0661 0.0255 5.423 42.728 31.565 4044.194 4.827 140.400 3.540 0.70 356856. 0.5305 34.43 0.2066 0.5186 0.0636 0.0253 5.376 42.352 30.366 4008.578 4.785 135.069 3.436 0.70 357199. 0.5050 37.87 0.2272 0.5536 0.0609 0.0250 5.309 41.830 29.104 3959.228 4.726 129.456 3.334 0.70 357559. 0.4797 41.31 0.2479 0.5859 0.0581 0.0246 5.224 41.157 27.781 3895.485 4.650 123.571 3.235 0.70 357939. 0.4547 44.76 0.2685 0.6155 0.0553 0.0241 5.119 40.328 26.401 3817.003 4.556 117.431 3.137 0.70 358337. 0.4299 48.20 0.2892 0.6426 0.0523 0.0235 4.993 39.341 24.967 3723.557 4.445 111.052 3.041 0.70 358755. 0.4053 51.64 0.3099 0.6670 0.0491 0.0228 4.848 38.193 23.483 3614.958 4.315 104.451 2.946 0.70 359192. 0.3808 55.08 0.3305 0.6888 0.0459 0.0220 4.682 36.884 21.953 3491.070 4.167 97.645 2.852 0.70 359648. 0.3564 58.53 0.3512 0.7076 0.0427 0.0212 4.495 35.413 20.380 3351.781 4.001 90.651 2.758 0.70 360124. 0.3321 61.97 0.3718 0.7234 0.0393 0.0202 4.287 33.778 18.769 3197.038 3.816 83.486 2.663 0.70 360620. 0.3077 65.41 0.3925 0.7359 0.0358 0.0191 4.059 31.980 17.124 3026.844 3.613 76.169 2.566 0.70 361135. 0.2832 68.86 0.4131 0.7445 0.0323 0.0179 3.810 30.019 15.449 2841.286 3.392 68.718 2.466 0.70 361672. 0.2585 72.30 0.4338 0.7485 0.0288 0.0167 3.541 27.898 13.749 2640.543 3.152 61.156 2.362 0.70 362228. 0.2336 75.74 0.4544 0.7471 0.0252 0.0153 3.252 25.620 12.029 2424.937 2.895 53.504 2.250 0.71 362805. 0.2081 79.18 0.4751 0.7384 0.0215 0.0139 2.943 23.190 10.294 2194.942 2.620 45.788 2.127 0.71 363403. 0.1820 82.63 0.4958 0.7200 0.0179 0.0123 2.617 20.615 8.551 1951.231 2.329 38.036 1.988 0.71 364022. 0.1550 86.07 0.5164 0.6874 0.0142 0.0107 2.273 17.905 6.807 1694.703 2.023 30.278 1.822 0.71 364661. 0.1268 89.51 0.5371 0.6326 0.0106 0.0090 1.913 15.072 5.070 1426.520 1.703 22.550 1.612 0.71 365322. 0.0968 92.96 0.5577 0.5389 0.0070 0.0073 1.540 12.130 3.348 1148.144 1.370 14.891 1.322 0.71 366004. 0.0645 96.40 0.5784 0.3673 0.0035 0.0054 1.155 9.100 1.650 861.283 1.028 7.340 0.869 0.71 366706. 0.0298 99.84 0.5990 -0.0124 -0.0001 0.0036 0.756 5.957 -0.035 563.828 0.673 -0.156 -0.028 0.71 367382. 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 0.0852 0.0259 7.840 54.905 51.503 5846.342 6.203 229.084 3.996 0.79 398788. 0.7648 3.86 0.0206 0.0660 0.0837 0.0261 7.903 55.345 50.625 5893.193 6.253 225.181 3.896 0.79 399010. 0.7394 7.73 0.0412 0.1287 0.0822 0.0263 7.958 55.728 49.682 5933.936 6.296 220.986 3.798 0.79 399249. 0.7139 11.59 0.0618 0.1880 0.0805 0.0265 8.002 56.041 48.672 5967.314 6.332 216.492 3.699 0.79 399504. 0.6884 15.46 0.0824 0.2441 0.0787 0.0266 8.035 56.274 47.592 5992.060 6.358 211.688 3.602 0.79 399777. 0.6628 19.32 0.1030 0.2970 0.0768 0.0266 8.055 56.412 46.439 6006.824 6.373 206.561 3.507 0.79 400067. 0.6373 23.19 0.1237 0.3468 0.0748 0.0267 8.060 56.444 45.212 6010.200 6.377 201.104 3.412 0.79 400376. 0.6119 27.05 0.1443 0.3936 0.0726 0.0266 8.047 56.355 43.909 6000.738 6.367 195.305 3.319 0.79 400704. 0.5866 30.91 0.1649 0.4374 0.0703 0.0265 8.015 56.132 42.527 5976.938 6.342 189.159 3.227 0.79 401051. 0.5613 34.78 0.1855 0.4783 0.0679 0.0263 7.962 55.759 41.065 5937.213 6.300 182.658 3.137 0.79 401418. 0.5362 38.64 0.2061 0.5165 0.0654 0.0261 7.885 55.220 39.521 5879.870 6.239 175.791 3.049 0.79 401805. 0.5112 42.51 0.2267 0.5519 0.0627 0.0257 7.782 54.500 37.894 5803.156 6.157 168.553 2.962 0.79 402213. 0.4863 46.37 0.2473 0.5848 0.0598 0.0253 7.652 53.586 36.185 5705.875 6.054 160.953 2.876 0.79 402641. 0.4615 50.24 0.2679 0.6150 0.0569 0.0248 7.493 52.473 34.400 5587.326 5.928 153.012 2.793 0.79 403091. 0.4368 54.10 0.2885 0.6427 0.0538 0.0242 7.305 51.157 32.543 5447.248 5.780 144.753 2.710 0.79 403562. 0.4123 57.96 0.3091 0.6678 0.0506 0.0234 7.088 49.636 30.620 5285.267 5.608 136.198 2.628 0.79 404054. 0.3878 61.83 0.3298 0.6901 0.0474 0.0226 6.841 47.906 28.635 5101.103 5.412 127.370 2.546 0.79 404568. 0.3634 65.69 0.3504 0.7097 0.0440 0.0217 6.564 45.968 26.594 4894.746 5.193 118.290 2.464 0.79 405104. 0.3389 69.56 0.3710 0.7262 0.0405 0.0207 6.258 43.823 24.501 4666.332 4.951 108.981 2.382 0.79 405662. 0.3144 73.42 0.3916 0.7393 0.0370 0.0196 5.922 41.473 22.362 4416.093 4.686 99.467 2.297 0.79 406242. 0.2897 77.29 0.4122 0.7484 0.0334 0.0184 5.558 38.922 20.183 4144.461 4.397 89.773 2.209 0.79 406845. 0.2647 81.15 0.4328 0.7527 0.0297 0.0171 5.166 36.177 17.969 3852.146 4.087 79.925 2.116 0.79 407470. 0.2392 85.02 0.4534 0.7510 0.0260 0.0157 4.747 33.246 15.727 3540.054 3.756 69.952 2.015 0.79 408118. 0.2131 88.88 0.4740 0.7414 0.0223 0.0142 4.304 30.141 13.464 3209.422 3.405 59.887 1.903 0.79 408789. 0.1862 92.74 0.4946 0.7210 0.0185 0.0127 3.838 26.877 11.188 2861.863 3.037 49.765 1.773 0.80 409483. 0.1582 96.61 0.5152 0.6847 0.0147 0.0111 3.352 23.473 8.909 2499.381 2.652 39.627 1.617 0.80 410201. 0.1287 100.47 0.5359 0.6241 0.0110 0.0094 2.849 19.951 6.636 2124.427 2.254 29.517 1.417 0.80 410942. 0.0973 104.34 0.5565 0.5224 0.0072 0.0077 2.333 16.340 4.381 1739.867 1.846 19.487 1.142 0.80 411707. 0.0638 108.20 0.5771 0.3438 0.0036 0.0060 1.809 12.668 2.156 1348.904 1.431 9.588 0.725 0.80 412493. 0.0284 112.07 0.5977 -0.0126 -0.0001 0.0042 1.272 8.906 -0.054 948.354 1.006 -0.238 -0.026 0.80 413255. 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 0.0876 0.0302 12.513 78.866 65.361 9330.792 8.910 290.724 3.177 0.87 443008. 0.6851 4.32 0.0207 0.0591 0.0861 0.0302 12.509 78.843 64.287 9328.073 8.908 285.947 3.126 0.87 443259. 0.6685 8.63 0.0414 0.1163 0.0846 0.0301 12.492 78.734 63.126 9315.176 8.895 280.785 3.074 0.87 443529. 0.6513 12.95 0.0622 0.1715 0.0829 0.0300 12.459 78.529 61.877 9290.885 8.872 275.229 3.021 0.87 443818. 0.6338 17.26 0.0829 0.2246 0.0811 0.0299 12.410 78.217 60.535 9253.966 8.837 269.260 2.967 0.87 444126. 0.6157 21.58 0.1036 0.2755 0.0792 0.0298 12.342 77.787 59.097 9203.111 8.788 262.864 2.913 0.87 444454. 0.5972 25.90 0.1243 0.3244 0.0771 0.0295 12.253 77.228 57.560 9137.012 8.725 256.027 2.857 0.87 444804. 0.5782 30.21 0.1450 0.3710 0.0749 0.0293 12.142 76.529 55.921 9054.307 8.646 248.738 2.801 0.87 445175. 0.5587 34.53 0.1657 0.4154 0.0726 0.0290 12.007 75.677 54.179 8953.535 8.550 240.987 2.745 0.87 445568. 0.5388 38.84 0.1865 0.4576 0.0701 0.0286 11.845 74.660 52.330 8833.132 8.435 232.765 2.687 0.87 445983. 0.5184 43.16 0.2072 0.4974 0.0675 0.0281 11.655 73.461 50.373 8691.263 8.300 224.060 2.629 0.87 446421. 0.4976 47.48 0.2279 0.5349 0.0647 0.0276 11.433 72.063 48.306 8525.919 8.142 214.863 2.570 0.87 446882. 0.4764 51.79 0.2486 0.5699 0.0618 0.0270 11.178 70.455 46.130 8335.642 7.960 205.186 2.510 0.88 447366. 0.4547 56.11 0.2693 0.6025 0.0587 0.0263 10.889 68.629 43.852 8119.658 7.754 195.056 2.450 0.88 447874. 0.4327 60.42 0.2900 0.6327 0.0556 0.0255 10.564 66.581 41.480 7877.298 7.522 184.501 2.388 0.88 448406. 0.4103 64.74 0.3108 0.6598 0.0523 0.0246 10.209 64.345 39.018 7612.780 7.270 173.551 2.325 0.88 448961. 0.3873 69.06 0.3315 0.6833 0.0489 0.0237 9.830 61.954 36.474 7329.887 7.000 162.234 2.257 0.88 449541. 0.3635 73.37 0.3522 0.7028 0.0453 0.0227 9.425 59.402 33.853 7027.942 6.711 150.579 2.185 0.88 450145. 0.3390 77.69 0.3729 0.7175 0.0417 0.0217 8.997 56.706 31.164 6709.037 6.407 138.616 2.107 0.88 450774. 0.3137 82.00 0.3936 0.7270 0.0381 0.0206 8.546 53.866 28.412 6372.939 6.086 126.377 2.022 0.88 451427. 0.2875 86.32 0.4143 0.7309 0.0343 0.0194 8.064 50.827 25.607 6013.487 5.742 113.900 1.931 0.88 452106. 0.2607 90.64 0.4351 0.7281 0.0305 0.0182 7.554 47.611 22.757 5632.993 5.379 101.221 1.832 0.88 452809. 0.2331 94.95 0.4558 0.7167 0.0266 0.0169 7.020 44.244 19.869 5234.552 4.999 88.379 1.722 0.88 453538. 0.2047 99.27 0.4765 0.6942 0.0227 0.0156 6.465 40.750 16.956 4821.209 4.604 75.419 1.595 0.88 454292. 0.1752 103.58 0.4972 0.6571 0.0188 0.0142 5.896 37.159 14.026 4396.400 4.198 62.388 1.447 0.88 455072. 0.1445 107.90 0.5179 0.6004 0.0149 0.0128 5.316 33.507 11.094 3964.261 3.786 49.346 1.269 0.88 455878. 0.1128 112.22 0.5386 0.5167 0.0109 0.0114 4.733 29.830 8.173 3529.215 3.370 36.353 1.050 0.89 456711. 0.0801 116.53 0.5594 0.3951 0.0071 0.0100 4.152 26.167 5.278 3095.840 2.956 23.478 0.773 0.89 457569. 0.0474 120.85 0.5801 0.2185 0.0033 0.0086 3.578 22.554 2.427 2668.401 2.548 10.794 0.412 0.89 458451. 0.0171 125.16 0.6008 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 0.0883 0.0380 20.955 120.071 79.801 15626.360 13.566 354.955 2.316 0.96 487270. 0.5519 4.91 0.0214 0.0493 0.0870 0.0379 20.909 119.807 78.630 15592.014 13.536 349.748 2.287 0.96 487550. 0.5410 9.82 0.0429 0.0973 0.0856 0.0377 20.825 119.323 77.341 15529.098 13.481 344.014 2.259 0.96 487852. 0.5299 14.74 0.0643 0.1441 0.0841 0.0375 20.699 118.600 75.928 15434.908 13.399 337.728 2.231 0.96 488178. 0.5185 19.65 0.0857 0.1898 0.0823 0.0372 20.527 117.618 74.383 15307.202 13.288 330.857 2.204 0.96 488528. 0.5070 24.56 0.1072 0.2344 0.0805 0.0368 20.309 116.365 72.701 15144.111 13.147 323.372 2.177 0.96 488903. 0.4952 29.47 0.1286 0.2779 0.0785 0.0363 20.041 114.830 70.874 14944.264 12.973 315.249 2.151 0.96 489304. 0.4830 34.38 0.1500 0.3203 0.0763 0.0357 19.722 113.004 68.900 14706.650 12.767 306.466 2.125 0.96 489731. 0.4704 39.30 0.1715 0.3616 0.0739 0.0351 19.352 110.883 66.773 14430.636 12.527 297.008 2.099 0.96 490185. 0.4574 44.21 0.1929 0.4016 0.0714 0.0343 18.929 108.460 64.490 14115.320 12.254 286.853 2.072 0.96 490666. 0.4439 49.12 0.2143 0.4404 0.0687 0.0334 18.454 105.738 62.049 13761.070 11.946 275.993 2.045 0.96 491175. 0.4297 54.03 0.2358 0.4778 0.0658 0.0325 17.926 102.715 59.447 13367.624 11.605 264.420 2.017 0.96 491712. 0.4148 58.94 0.2572 0.5136 0.0628 0.0314 17.347 99.397 56.691 12935.805 11.230 252.160 1.988 0.96 492277. 0.3992 63.86 0.2786 0.5478 0.0595 0.0303 16.719 95.797 53.790 12467.370 10.823 239.258 1.957 0.96 492870. 0.3828 68.77 0.3001 0.5801 0.0562 0.0291 16.044 91.929 50.756 11963.905 10.386 225.762 1.924 0.96 493492. 0.3656 73.68 0.3215 0.6103 0.0527 0.0278 15.323 87.801 47.598 11426.620 9.920 211.718 1.889 0.96 494142. 0.3477 78.59 0.3429 0.6370 0.0491 0.0264 14.583 83.559 44.326 10874.556 9.440 197.164 1.849 0.97 494820. 0.3283 83.50 0.3644 0.6580 0.0453 0.0251 13.856 79.395 40.948 10332.664 8.970 182.138 1.797 0.97 495527. 0.3068 88.41 0.3858 0.6717 0.0415 0.0238 13.153 75.363 37.475 9807.954 8.514 166.690 1.733 0.97 496263. 0.2830 93.33 0.4072 0.6700 0.0375 0.0228 12.594 72.160 33.908 9391.055 8.153 150.823 1.638 0.97 497029. 0.2543 98.24 0.4287 0.6570 0.0335 0.0219 12.069 69.156 30.272 9000.182 7.813 134.650 1.526 0.97 497823. 0.2239 103.15 0.4501 0.6340 0.0294 0.0209 11.534 66.090 26.587 8601.202 7.467 118.260 1.402 0.97 498646. 0.1928 108.06 0.4715 0.5994 0.0253 0.0199 10.995 63.002 22.871 8199.321 7.118 101.730 1.265 0.97 499500. 0.1614 112.97 0.4930 0.5514 0.0212 0.0189 10.459 59.930 19.143 7799.513 6.771 85.149 1.113 0.97 500383. 0.1299 117.89 0.5144 0.4881 0.0171 0.0180 9.934 56.921 15.426 7407.835 6.431 68.617 0.945 0.97 501296. 0.0989 122.80 0.5358 0.4082 0.0130 0.0171 9.422 53.989 11.747 7026.297 6.100 52.249 0.758 0.97 502240. 0.0693 127.71 0.5573 0.3101 0.0090 0.0162 8.928 51.157 8.131 6657.710 5.780 36.165 0.554 0.97 503216. 0.0421 132.62 0.5787 0.1925 0.0051 0.0153 8.453 48.432 4.602 6303.040 5.472 20.468 0.331 0.98 504226. 0.0189 137.53 0.6001 0.0528 0.0013 0.0145 7.978 45.714 1.150 5949.406 5.165 5.114 0.088 0.98 505288. 0.0025 142.45 0.6216