17x10WE (17x10WE.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 0.0448 0.005 0.318 0.282 3.762 0.036 1.253 33.973 0.07 33489. 0.6243 0.40 0.0252 0.0588 0.1055 0.0453 0.005 0.321 0.278 3.801 0.036 1.235 33.118 0.07 33514. 0.6040 0.81 0.0505 0.1146 0.1038 0.0457 0.005 0.324 0.273 3.838 0.037 1.214 32.265 0.07 33542. 0.5836 1.21 0.0757 0.1673 0.1019 0.0461 0.005 0.327 0.268 3.871 0.037 1.193 31.415 0.07 33571. 0.5631 1.62 0.1009 0.2171 0.0999 0.0464 0.005 0.330 0.263 3.899 0.037 1.169 30.571 0.07 33603. 0.5425 2.02 0.1261 0.2640 0.0977 0.0467 0.005 0.331 0.257 3.922 0.037 1.144 29.735 0.07 33637. 0.5219 2.43 0.1514 0.3079 0.0954 0.0469 0.005 0.333 0.251 3.938 0.038 1.116 28.907 0.07 33673. 0.5013 2.83 0.1766 0.3491 0.0929 0.0470 0.005 0.334 0.244 3.946 0.038 1.087 28.089 0.07 33712. 0.4807 3.24 0.2018 0.3875 0.0902 0.0470 0.005 0.334 0.237 3.946 0.038 1.056 27.281 0.07 33754. 0.4601 3.64 0.2271 0.4231 0.0873 0.0469 0.005 0.333 0.230 3.936 0.038 1.022 26.481 0.07 33798. 0.4394 4.05 0.2523 0.4561 0.0843 0.0466 0.005 0.331 0.222 3.915 0.037 0.986 25.691 0.07 33845. 0.4188 4.45 0.2775 0.4864 0.0810 0.0462 0.005 0.328 0.213 3.882 0.037 0.948 24.907 0.07 33895. 0.3981 4.86 0.3028 0.5140 0.0776 0.0457 0.005 0.324 0.204 3.837 0.037 0.908 24.127 0.07 33948. 0.3773 5.26 0.3280 0.5389 0.0739 0.0450 0.005 0.319 0.194 3.777 0.036 0.865 23.348 0.07 34003. 0.3564 5.67 0.3532 0.5609 0.0701 0.0441 0.005 0.313 0.184 3.704 0.035 0.820 22.565 0.07 34062. 0.3353 6.07 0.3784 0.5799 0.0660 0.0431 0.005 0.306 0.174 3.617 0.035 0.772 21.774 0.07 34123. 0.3141 6.48 0.4037 0.5956 0.0618 0.0419 0.005 0.297 0.163 3.517 0.034 0.723 20.968 0.07 34187. 0.2927 6.88 0.4289 0.6079 0.0574 0.0405 0.005 0.288 0.151 3.403 0.032 0.672 20.140 0.07 34254. 0.2710 7.29 0.4541 0.6162 0.0530 0.0390 0.004 0.277 0.139 3.277 0.031 0.620 19.281 0.07 34324. 0.2491 7.69 0.4794 0.6200 0.0484 0.0374 0.004 0.265 0.127 3.139 0.030 0.566 18.381 0.07 34396. 0.2269 8.10 0.5046 0.6188 0.0437 0.0356 0.004 0.253 0.115 2.989 0.029 0.511 17.426 0.07 34472. 0.2044 8.50 0.5298 0.6115 0.0389 0.0337 0.004 0.239 0.102 2.828 0.027 0.455 16.401 0.07 34550. 0.1816 8.91 0.5551 0.5970 0.0340 0.0316 0.004 0.224 0.089 2.655 0.025 0.398 15.284 0.07 34632. 0.1583 9.31 0.5803 0.5736 0.0291 0.0294 0.003 0.209 0.077 2.472 0.024 0.341 14.046 0.07 34716. 0.1345 9.72 0.6055 0.5389 0.0242 0.0271 0.003 0.193 0.064 2.279 0.022 0.283 12.648 0.07 34803. 0.1104 10.12 0.6307 0.4897 0.0192 0.0247 0.003 0.176 0.051 2.077 0.020 0.225 11.033 0.07 34893. 0.0859 10.53 0.6560 0.4209 0.0143 0.0222 0.003 0.158 0.038 1.867 0.018 0.167 9.119 0.07 34987. 0.0612 10.93 0.6812 0.3249 0.0094 0.0196 0.002 0.139 0.025 1.650 0.016 0.110 6.777 0.07 35083. 0.0368 11.34 0.7064 0.1889 0.0045 0.0170 0.002 0.121 0.012 1.427 0.014 0.053 3.801 0.07 35181. 0.0144 11.74 0.7317 -0.0096 -0.0002 0.0143 0.002 0.101 0.000 1.199 0.011 -0.002 -0.187 0.07 35282. 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 0.1075 0.0417 0.038 1.183 1.131 27.983 0.134 5.032 18.335 0.13 66978. 0.6751 0.81 0.0253 0.0636 0.1059 0.0422 0.038 1.197 1.114 28.327 0.135 4.957 17.843 0.13 67028. 0.6520 1.63 0.0506 0.1236 0.1042 0.0427 0.038 1.211 1.096 28.650 0.137 4.876 17.353 0.13 67083. 0.6289 2.44 0.0759 0.1803 0.1023 0.0431 0.039 1.223 1.076 28.943 0.138 4.788 16.869 0.13 67142. 0.6059 3.25 0.1013 0.2336 0.1003 0.0435 0.039 1.234 1.055 29.200 0.139 4.694 16.391 0.13 67205. 0.5829 4.06 0.1266 0.2836 0.0981 0.0438 0.039 1.243 1.032 29.411 0.140 4.592 15.920 0.13 67274. 0.5599 4.88 0.1519 0.3304 0.0958 0.0440 0.040 1.250 1.008 29.570 0.141 4.482 15.458 0.13 67347. 0.5372 5.69 0.1772 0.3741 0.0933 0.0442 0.040 1.254 0.981 29.666 0.142 4.365 15.003 0.13 67426. 0.5145 6.50 0.2025 0.4149 0.0906 0.0442 0.040 1.255 0.953 29.692 0.142 4.239 14.558 0.13 67510. 0.4920 7.31 0.2278 0.4527 0.0877 0.0441 0.040 1.253 0.923 29.637 0.142 4.104 14.121 0.13 67599. 0.4695 8.13 0.2531 0.4878 0.0846 0.0439 0.040 1.246 0.890 29.494 0.141 3.960 13.692 0.13 67694. 0.4472 8.94 0.2784 0.5201 0.0813 0.0435 0.039 1.236 0.856 29.252 0.140 3.807 13.271 0.13 67794. 0.4250 9.75 0.3038 0.5496 0.0779 0.0430 0.039 1.222 0.819 28.905 0.138 3.644 12.857 0.14 67900. 0.4029 10.56 0.3291 0.5764 0.0742 0.0423 0.038 1.202 0.781 28.444 0.136 3.472 12.447 0.14 68011. 0.3807 11.38 0.3544 0.6005 0.0703 0.0415 0.037 1.178 0.740 27.865 0.133 3.290 12.040 0.14 68129. 0.3584 12.19 0.3797 0.6217 0.0662 0.0404 0.036 1.148 0.697 27.170 0.130 3.100 11.634 0.14 68252. 0.3362 13.00 0.4050 0.6398 0.0620 0.0392 0.035 1.114 0.652 26.360 0.126 2.902 11.225 0.14 68381. 0.3138 13.81 0.4303 0.6547 0.0576 0.0379 0.034 1.075 0.606 25.440 0.121 2.697 10.810 0.14 68515. 0.2914 14.63 0.4556 0.6659 0.0531 0.0363 0.033 1.032 0.559 24.411 0.117 2.486 10.384 0.14 68656. 0.2687 15.44 0.4809 0.6731 0.0485 0.0347 0.031 0.984 0.510 23.276 0.111 2.270 9.944 0.14 68802. 0.2459 16.25 0.5063 0.6755 0.0438 0.0328 0.030 0.931 0.461 22.038 0.105 2.049 9.481 0.14 68954. 0.2228 17.06 0.5316 0.6724 0.0390 0.0308 0.028 0.875 0.410 20.700 0.099 1.824 8.987 0.14 69112. 0.1993 17.88 0.5569 0.6624 0.0341 0.0287 0.026 0.814 0.359 19.265 0.092 1.597 8.452 0.14 69276. 0.1753 18.69 0.5822 0.6439 0.0292 0.0264 0.024 0.750 0.307 17.738 0.085 1.367 7.858 0.14 69445. 0.1508 19.50 0.6075 0.6141 0.0243 0.0240 0.022 0.681 0.255 16.123 0.077 1.136 7.183 0.14 69621. 0.1256 20.32 0.6328 0.5692 0.0193 0.0215 0.019 0.610 0.203 14.428 0.069 0.904 6.391 0.14 69802. 0.0997 21.13 0.6581 0.5026 0.0144 0.0188 0.017 0.535 0.151 12.660 0.060 0.674 5.426 0.14 69989. 0.0731 21.94 0.6834 0.4033 0.0095 0.0161 0.015 0.458 0.100 10.830 0.052 0.445 4.193 0.14 70182. 0.0459 22.75 0.7088 0.2508 0.0047 0.0133 0.012 0.378 0.050 8.949 0.043 0.221 2.514 0.14 70381. 0.0194 23.57 0.7341 0.0008 0.0000 0.0105 0.009 0.297 0.000 7.025 0.034 0.001 0.007 0.14 70582. 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 0.1079 0.0404 0.123 2.578 2.554 91.519 0.291 11.360 12.658 0.20 100464. 0.7002 1.22 0.0254 0.0659 0.1063 0.0409 0.124 2.613 2.516 92.732 0.295 11.192 12.307 0.20 100540. 0.6758 2.44 0.0508 0.1281 0.1045 0.0414 0.126 2.645 2.475 93.871 0.299 11.009 11.959 0.20 100622. 0.6513 3.67 0.0761 0.1867 0.1027 0.0419 0.127 2.674 2.431 94.910 0.302 10.812 11.616 0.20 100711. 0.6269 4.89 0.1015 0.2417 0.1006 0.0423 0.129 2.700 2.383 95.825 0.305 10.599 11.279 0.20 100807. 0.6027 6.11 0.1269 0.2933 0.0985 0.0426 0.130 2.721 2.331 96.587 0.307 10.369 10.947 0.20 100910. 0.5786 7.33 0.1523 0.3415 0.0961 0.0429 0.130 2.738 2.276 97.167 0.309 10.122 10.623 0.20 101021. 0.5547 8.55 0.1776 0.3865 0.0936 0.0430 0.131 2.748 2.216 97.536 0.310 9.857 10.305 0.20 101139. 0.5310 9.78 0.2030 0.4284 0.0909 0.0431 0.131 2.751 2.152 97.660 0.311 9.572 9.995 0.20 101266. 0.5075 11.00 0.2284 0.4673 0.0880 0.0430 0.131 2.747 2.083 97.510 0.310 9.267 9.691 0.20 101400. 0.4842 12.22 0.2538 0.5033 0.0849 0.0428 0.130 2.734 2.010 97.053 0.309 8.942 9.395 0.20 101543. 0.4611 13.44 0.2792 0.5366 0.0816 0.0425 0.129 2.712 1.932 96.260 0.306 8.595 9.105 0.20 101694. 0.4382 14.66 0.3045 0.5671 0.0781 0.0419 0.128 2.679 1.850 95.102 0.303 8.227 8.821 0.20 101854. 0.4153 15.89 0.3299 0.5949 0.0744 0.0413 0.125 2.636 1.762 93.549 0.298 7.836 8.542 0.20 102022. 0.3925 17.11 0.3553 0.6200 0.0705 0.0404 0.123 2.580 1.669 91.588 0.292 7.425 8.266 0.20 102199. 0.3697 18.33 0.3807 0.6423 0.0664 0.0394 0.120 2.514 1.572 89.221 0.284 6.993 7.993 0.20 102384. 0.3469 19.55 0.4060 0.6617 0.0621 0.0381 0.116 2.436 1.471 86.459 0.275 6.545 7.719 0.20 102579. 0.3241 20.78 0.4314 0.6779 0.0577 0.0367 0.112 2.347 1.367 83.308 0.265 6.081 7.444 0.20 102782. 0.3013 22.00 0.4568 0.6908 0.0532 0.0352 0.107 2.248 1.260 79.777 0.254 5.604 7.163 0.20 102993. 0.2783 23.22 0.4822 0.6997 0.0486 0.0335 0.102 2.138 1.150 75.875 0.242 5.115 6.874 0.20 103214. 0.2552 24.44 0.5076 0.7042 0.0438 0.0316 0.096 2.018 1.038 71.609 0.228 4.615 6.572 0.20 103443. 0.2318 25.66 0.5329 0.7034 0.0390 0.0295 0.090 1.887 0.923 66.990 0.213 4.108 6.252 0.20 103681. 0.2080 26.89 0.5583 0.6962 0.0341 0.0274 0.083 1.748 0.808 62.029 0.197 3.593 5.906 0.20 103927. 0.1838 28.11 0.5837 0.6806 0.0292 0.0250 0.076 1.599 0.691 56.742 0.181 3.073 5.523 0.21 104183. 0.1589 29.33 0.6091 0.6540 0.0242 0.0226 0.069 1.441 0.574 51.148 0.163 2.551 5.087 0.21 104447. 0.1334 30.55 0.6344 0.6121 0.0193 0.0200 0.061 1.275 0.456 45.269 0.144 2.029 4.570 0.21 104721. 0.1069 31.77 0.6598 0.5476 0.0143 0.0173 0.052 1.103 0.339 39.135 0.125 1.509 3.932 0.21 105003. 0.0793 33.00 0.6852 0.4474 0.0094 0.0145 0.044 0.924 0.224 32.783 0.104 0.994 3.093 0.21 105294. 0.0506 34.22 0.7106 0.2846 0.0046 0.0116 0.035 0.740 0.110 26.254 0.084 0.488 1.897 0.21 105594. 0.0218 35.44 0.7360 -0.0061 -0.0001 0.0086 0.026 0.551 -0.002 19.565 0.062 -0.008 -0.039 0.21 105895. 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 0.1083 0.0397 0.286 4.511 4.559 213.461 0.510 20.280 9.688 0.27 133948. 0.7161 1.65 0.0257 0.0681 0.1067 0.0403 0.290 4.574 4.491 216.447 0.517 19.978 9.412 0.27 134050. 0.6905 3.30 0.0514 0.1322 0.1049 0.0408 0.294 4.633 4.418 219.252 0.523 19.649 9.139 0.27 134162. 0.6649 4.95 0.0771 0.1924 0.1031 0.0413 0.297 4.687 4.338 221.813 0.530 19.293 8.870 0.27 134282. 0.6395 6.60 0.1028 0.2489 0.1010 0.0417 0.300 4.735 4.251 224.068 0.535 18.909 8.605 0.27 134412. 0.6142 8.25 0.1285 0.3018 0.0988 0.0420 0.303 4.774 4.158 225.946 0.539 18.494 8.347 0.27 134552. 0.5891 9.90 0.1542 0.3512 0.0964 0.0423 0.305 4.805 4.057 227.376 0.543 18.047 8.093 0.27 134703. 0.5643 11.55 0.1799 0.3972 0.0938 0.0425 0.306 4.824 3.949 228.280 0.545 17.566 7.847 0.27 134864. 0.5398 13.20 0.2056 0.4401 0.0911 0.0425 0.307 4.830 3.833 228.580 0.546 17.049 7.606 0.27 135035. 0.5155 14.85 0.2312 0.4798 0.0881 0.0425 0.306 4.822 3.709 228.196 0.545 16.496 7.371 0.27 135218. 0.4914 16.50 0.2569 0.5166 0.0849 0.0423 0.304 4.798 3.576 227.051 0.542 15.904 7.143 0.27 135413. 0.4675 18.15 0.2826 0.5505 0.0816 0.0419 0.302 4.756 3.434 225.071 0.537 15.273 6.920 0.27 135618. 0.4439 19.80 0.3083 0.5817 0.0780 0.0413 0.298 4.695 3.283 222.181 0.530 14.603 6.702 0.27 135836. 0.4204 21.45 0.3340 0.6101 0.0742 0.0406 0.293 4.613 3.123 218.310 0.521 13.891 6.489 0.27 136065. 0.3969 23.10 0.3597 0.6357 0.0702 0.0397 0.286 4.510 2.954 213.429 0.510 13.141 6.279 0.27 136306. 0.3736 24.75 0.3854 0.6586 0.0660 0.0386 0.278 4.386 2.778 207.549 0.495 12.356 6.071 0.27 136559. 0.3503 26.40 0.4111 0.6785 0.0616 0.0373 0.269 4.241 2.595 200.689 0.479 11.540 5.864 0.27 136823. 0.3270 28.05 0.4368 0.6954 0.0571 0.0359 0.259 4.075 2.405 192.869 0.460 10.697 5.656 0.27 137100. 0.3036 29.69 0.4625 0.7088 0.0525 0.0343 0.247 3.890 2.210 184.108 0.440 9.830 5.444 0.27 137388. 0.2802 31.34 0.4882 0.7183 0.0478 0.0325 0.234 3.686 2.010 174.425 0.416 8.941 5.227 0.27 137689. 0.2565 32.99 0.5139 0.7233 0.0429 0.0305 0.220 3.462 1.806 163.842 0.391 8.035 5.001 0.27 138001. 0.2327 34.64 0.5396 0.7230 0.0380 0.0284 0.204 3.220 1.599 152.385 0.364 7.114 4.760 0.27 138325. 0.2084 36.29 0.5653 0.7159 0.0330 0.0261 0.188 2.960 1.390 140.084 0.334 6.181 4.499 0.27 138662. 0.1836 37.94 0.5910 0.7001 0.0280 0.0236 0.170 2.683 1.178 126.979 0.303 5.241 4.209 0.27 139010. 0.1581 39.59 0.6167 0.6723 0.0230 0.0211 0.152 2.390 0.966 113.120 0.270 4.297 3.873 0.27 139371. 0.1318 41.24 0.6424 0.6274 0.0179 0.0183 0.132 2.083 0.754 98.571 0.235 3.354 3.470 0.27 139744. 0.1043 42.89 0.6680 0.5557 0.0129 0.0155 0.112 1.763 0.543 83.411 0.199 2.417 2.955 0.27 140128. 0.0754 44.54 0.6937 0.4389 0.0080 0.0126 0.091 1.431 0.336 67.737 0.162 1.493 2.247 0.28 140525. 0.0451 46.19 0.7194 0.2344 0.0031 0.0096 0.069 1.092 0.132 51.659 0.123 0.586 1.158 0.28 140933. 0.0146 47.84 0.7451 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 0.1089 0.0394 0.555 6.993 7.161 413.693 0.790 31.850 7.851 0.34 167427. 0.7272 2.04 0.0254 0.0682 0.1073 0.0400 0.563 7.093 7.056 419.583 0.801 31.384 7.627 0.34 167554. 0.7013 4.08 0.0508 0.1325 0.1056 0.0405 0.570 7.187 6.942 425.128 0.812 30.877 7.406 0.34 167692. 0.6755 6.12 0.0763 0.1929 0.1037 0.0410 0.577 7.272 6.819 430.209 0.822 30.329 7.189 0.34 167841. 0.6498 8.16 0.1017 0.2495 0.1017 0.0414 0.583 7.348 6.685 434.701 0.830 29.737 6.976 0.34 168002. 0.6244 10.20 0.1271 0.3026 0.0995 0.0418 0.588 7.412 6.542 438.474 0.837 29.098 6.767 0.34 168175. 0.5991 12.24 0.1525 0.3522 0.0971 0.0421 0.592 7.461 6.387 441.388 0.843 28.409 6.563 0.34 168360. 0.5742 14.28 0.1779 0.3984 0.0946 0.0422 0.594 7.494 6.220 443.297 0.847 27.667 6.364 0.34 168559. 0.5495 16.32 0.2033 0.4415 0.0919 0.0423 0.595 7.506 6.041 444.050 0.848 26.872 6.171 0.34 168770. 0.5250 18.36 0.2288 0.4815 0.0889 0.0423 0.595 7.497 5.850 443.494 0.847 26.019 5.983 0.34 168996. 0.5009 20.40 0.2542 0.5186 0.0858 0.0421 0.592 7.463 5.645 441.481 0.843 25.108 5.799 0.34 169235. 0.4770 22.44 0.2796 0.5530 0.0825 0.0417 0.587 7.402 5.426 437.865 0.836 24.137 5.621 0.34 169488. 0.4533 24.48 0.3050 0.5846 0.0790 0.0412 0.580 7.311 5.194 432.505 0.826 23.104 5.447 0.34 169755. 0.4297 26.52 0.3304 0.6135 0.0752 0.0405 0.570 7.189 4.948 425.259 0.812 22.008 5.277 0.34 170037. 0.4063 28.56 0.3558 0.6398 0.0713 0.0396 0.558 7.033 4.688 416.054 0.795 20.851 5.110 0.34 170333. 0.3830 30.60 0.3813 0.6635 0.0671 0.0386 0.543 6.845 4.415 404.901 0.773 19.639 4.946 0.34 170644. 0.3598 32.64 0.4067 0.6844 0.0628 0.0373 0.525 6.624 4.132 391.835 0.748 18.379 4.783 0.34 170969. 0.3366 34.68 0.4321 0.7024 0.0584 0.0359 0.505 6.371 3.839 376.892 0.720 17.076 4.620 0.34 171309. 0.3134 36.72 0.4575 0.7172 0.0538 0.0343 0.483 6.087 3.537 360.107 0.688 15.734 4.455 0.34 171663. 0.2901 38.76 0.4829 0.7285 0.0491 0.0325 0.458 5.773 3.228 341.517 0.652 14.359 4.287 0.34 172032. 0.2667 40.80 0.5084 0.7357 0.0443 0.0306 0.431 5.429 2.913 321.161 0.613 12.955 4.113 0.34 172415. 0.2430 42.84 0.5338 0.7381 0.0394 0.0285 0.401 5.056 2.592 299.084 0.571 11.527 3.930 0.34 172813. 0.2190 44.88 0.5592 0.7345 0.0345 0.0262 0.369 4.655 2.266 275.345 0.526 10.081 3.733 0.34 173226. 0.1946 46.92 0.5846 0.7233 0.0295 0.0238 0.335 4.226 1.938 250.014 0.477 8.622 3.516 0.34 173653. 0.1695 48.96 0.6100 0.7016 0.0245 0.0213 0.299 3.773 1.609 223.184 0.426 7.155 3.269 0.34 174095. 0.1435 51.00 0.6354 0.6651 0.0194 0.0186 0.261 3.296 1.279 194.969 0.372 5.688 2.975 0.34 174552. 0.1164 53.04 0.6609 0.6057 0.0145 0.0158 0.222 2.798 0.951 165.514 0.316 4.228 2.605 0.34 175024. 0.0879 55.08 0.6863 0.5078 0.0095 0.0129 0.181 2.282 0.626 135.000 0.258 2.784 2.103 0.34 175511. 0.0576 57.12 0.7117 0.3366 0.0047 0.0099 0.139 1.752 0.307 103.636 0.198 1.366 1.344 0.34 176011. 0.0258 59.16 0.7371 -0.0098 -0.0001 0.0068 0.096 1.208 -0.006 71.433 0.136 -0.026 -0.038 0.35 176509. 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 0.1096 0.0393 0.957 10.050 10.375 713.390 1.135 46.149 6.597 0.40 200902. 0.7355 2.45 0.0254 0.0688 0.1080 0.0399 0.971 10.196 10.225 723.765 1.152 45.479 6.408 0.40 201055. 0.7093 4.90 0.0508 0.1335 0.1062 0.0404 0.984 10.333 10.061 733.537 1.167 44.752 6.221 0.40 201220. 0.6831 7.34 0.0762 0.1944 0.1044 0.0409 0.996 10.460 9.884 742.496 1.182 43.964 6.038 0.40 201399. 0.6571 9.79 0.1017 0.2514 0.1023 0.0414 1.006 10.571 9.692 750.429 1.194 43.111 5.858 0.40 201593. 0.6313 12.24 0.1271 0.3049 0.1002 0.0417 1.015 10.665 9.485 757.102 1.205 42.190 5.682 0.40 201801. 0.6058 14.69 0.1525 0.3548 0.0978 0.0420 1.022 10.738 9.262 762.274 1.213 41.196 5.511 0.40 202024. 0.5806 17.13 0.1779 0.4014 0.0953 0.0422 1.027 10.786 9.021 765.686 1.219 40.127 5.344 0.40 202262. 0.5556 19.58 0.2033 0.4448 0.0925 0.0423 1.029 10.806 8.763 767.075 1.221 38.977 5.181 0.40 202517. 0.5310 22.03 0.2287 0.4852 0.0896 0.0422 1.027 10.793 8.486 766.172 1.219 37.746 5.024 0.40 202788. 0.5066 24.48 0.2542 0.5226 0.0865 0.0421 1.023 10.744 8.190 762.716 1.214 36.428 4.870 0.40 203075. 0.4825 26.93 0.2796 0.5573 0.0831 0.0417 1.014 10.656 7.874 756.451 1.204 35.023 4.721 0.41 203379. 0.4586 29.37 0.3050 0.5893 0.0796 0.0412 1.002 10.525 7.538 747.131 1.189 33.528 4.576 0.41 203701. 0.4349 31.82 0.3304 0.6186 0.0758 0.0405 0.985 10.347 7.181 734.506 1.169 31.941 4.434 0.41 204040. 0.4114 34.27 0.3558 0.6454 0.0718 0.0396 0.963 10.121 6.804 718.440 1.143 30.266 4.296 0.41 204395. 0.3879 36.72 0.3812 0.6695 0.0677 0.0385 0.937 9.846 6.410 698.949 1.112 28.510 4.159 0.41 204769. 0.3645 39.16 0.4066 0.6910 0.0633 0.0373 0.907 9.524 5.999 676.092 1.076 26.683 4.025 0.41 205159. 0.3412 41.61 0.4321 0.7096 0.0589 0.0358 0.872 9.156 5.574 649.932 1.034 24.793 3.890 0.41 205567. 0.3179 44.06 0.4575 0.7252 0.0542 0.0342 0.832 8.741 5.137 620.528 0.988 22.847 3.754 0.41 205993. 0.2946 46.51 0.4829 0.7374 0.0495 0.0324 0.788 8.282 4.688 587.945 0.936 20.852 3.617 0.41 206435. 0.2711 48.95 0.5083 0.7456 0.0447 0.0304 0.741 7.780 4.230 552.249 0.879 18.816 3.474 0.41 206896. 0.2474 51.40 0.5337 0.7493 0.0397 0.0283 0.689 7.234 3.764 513.523 0.817 16.744 3.325 0.41 207374. 0.2233 53.85 0.5591 0.7471 0.0348 0.0260 0.633 6.647 3.292 471.866 0.751 14.645 3.165 0.41 207869. 0.1988 56.30 0.5846 0.7376 0.0297 0.0236 0.573 6.021 2.816 427.404 0.680 12.526 2.989 0.41 208382. 0.1736 58.75 0.6100 0.7180 0.0247 0.0210 0.510 5.357 2.338 380.297 0.605 10.397 2.788 0.41 208913. 0.1476 61.19 0.6354 0.6838 0.0196 0.0182 0.444 4.659 1.859 330.749 0.526 8.268 2.549 0.41 209462. 0.1203 63.64 0.6608 0.6270 0.0146 0.0154 0.374 3.931 1.382 279.016 0.444 6.149 2.247 0.41 210028. 0.0915 66.09 0.6862 0.5312 0.0096 0.0124 0.302 3.175 0.911 225.417 0.359 4.053 1.834 0.41 210612. 0.0606 68.54 0.7116 0.3588 0.0047 0.0094 0.228 2.399 0.448 170.323 0.271 1.995 1.194 0.41 211212. 0.0277 70.98 0.7371 -0.0078 -0.0001 0.0063 0.153 1.602 -0.006 113.722 0.181 -0.028 -0.025 0.41 211808. 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 0.1104 0.0394 1.523 13.712 14.227 1135.597 1.549 63.280 5.682 0.47 234370. 0.7419 2.89 0.0257 0.0698 0.1088 0.0400 1.546 13.917 14.020 1152.567 1.572 62.362 5.517 0.47 234550. 0.7151 5.77 0.0514 0.1355 0.1070 0.0406 1.567 14.110 13.796 1168.542 1.594 61.362 5.355 0.47 234747. 0.6885 8.66 0.0771 0.1972 0.1051 0.0411 1.587 14.286 13.552 1183.174 1.614 60.278 5.195 0.47 234959. 0.6620 11.54 0.1027 0.2550 0.1031 0.0415 1.604 14.442 13.287 1196.102 1.632 59.101 5.039 0.47 235188. 0.6358 14.43 0.1284 0.3091 0.1009 0.0419 1.619 14.573 13.001 1206.939 1.646 57.828 4.886 0.47 235435. 0.6098 17.32 0.1541 0.3596 0.0985 0.0422 1.630 14.674 12.692 1215.278 1.658 56.453 4.737 0.47 235699. 0.5842 20.20 0.1798 0.4067 0.0959 0.0424 1.637 14.739 12.359 1220.690 1.665 54.971 4.592 0.47 235982. 0.5588 23.09 0.2055 0.4506 0.0931 0.0425 1.640 14.764 12.000 1222.734 1.668 53.376 4.451 0.47 236285. 0.5338 25.97 0.2312 0.4913 0.0901 0.0424 1.637 14.743 11.615 1220.964 1.666 51.663 4.315 0.47 236607. 0.5090 28.86 0.2569 0.5292 0.0869 0.0422 1.629 14.670 11.203 1214.945 1.657 49.830 4.182 0.47 236949. 0.4846 31.75 0.2825 0.5642 0.0835 0.0418 1.615 14.541 10.763 1204.254 1.643 47.872 4.054 0.47 237311. 0.4603 34.63 0.3082 0.5965 0.0799 0.0413 1.594 14.350 10.294 1188.477 1.621 45.787 3.929 0.47 237693. 0.4363 37.52 0.3339 0.6261 0.0760 0.0405 1.565 14.094 9.796 1167.209 1.592 43.572 3.807 0.47 238096. 0.4124 40.41 0.3596 0.6532 0.0719 0.0396 1.529 13.768 9.270 1140.253 1.556 41.233 3.687 0.47 238519. 0.3886 43.29 0.3853 0.6776 0.0676 0.0385 1.485 13.374 8.719 1107.647 1.511 38.783 3.570 0.47 238963. 0.3650 46.18 0.4110 0.6994 0.0632 0.0371 1.434 12.914 8.146 1069.490 1.459 36.233 3.455 0.47 239428. 0.3413 49.06 0.4367 0.7183 0.0586 0.0356 1.376 12.387 7.553 1025.890 1.400 33.596 3.339 0.48 239913. 0.3177 51.95 0.4623 0.7341 0.0539 0.0339 1.310 11.796 6.943 976.945 1.333 30.881 3.223 0.48 240419. 0.2940 54.84 0.4880 0.7465 0.0490 0.0320 1.237 11.142 6.317 922.760 1.259 28.099 3.105 0.48 240946. 0.2702 57.72 0.5137 0.7549 0.0441 0.0300 1.158 10.426 5.679 863.456 1.178 25.259 2.983 0.48 241493. 0.2461 60.61 0.5394 0.7585 0.0390 0.0277 1.072 9.650 5.030 799.171 1.090 22.372 2.855 0.48 242062. 0.2216 63.49 0.5651 0.7561 0.0339 0.0253 0.979 8.815 4.372 730.080 0.996 19.448 2.716 0.48 242651. 0.1966 66.38 0.5908 0.7459 0.0288 0.0228 0.880 7.926 3.710 656.407 0.895 16.500 2.563 0.48 243261. 0.1709 69.27 0.6165 0.7248 0.0236 0.0201 0.776 6.984 3.044 578.434 0.789 13.540 2.387 0.48 243893. 0.1442 72.15 0.6422 0.6874 0.0185 0.0172 0.666 5.995 2.379 496.524 0.677 10.582 2.173 0.48 244545. 0.1160 75.04 0.6678 0.6236 0.0133 0.0143 0.551 4.964 1.718 411.134 0.561 7.643 1.896 0.48 245219. 0.0860 77.92 0.6935 0.5118 0.0083 0.0112 0.433 3.898 1.066 322.826 0.440 4.743 1.498 0.48 245913. 0.0535 80.81 0.7192 0.2955 0.0033 0.0081 0.311 2.804 0.427 232.229 0.317 1.900 0.834 0.48 246626. 0.0189 83.70 0.7449 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 0.1113 0.0397 2.288 18.024 18.744 1705.960 2.036 83.375 4.984 0.54 267830. 0.7469 3.26 0.0254 0.0692 0.1098 0.0403 2.322 18.294 18.480 1731.528 2.067 82.197 4.841 0.54 268034. 0.7203 6.52 0.0508 0.1343 0.1080 0.0408 2.354 18.549 18.191 1755.628 2.096 80.914 4.700 0.54 268256. 0.6939 9.78 0.0761 0.1955 0.1062 0.0414 2.384 18.782 17.878 1777.743 2.122 79.521 4.561 0.54 268496. 0.6676 13.04 0.1015 0.2529 0.1042 0.0418 2.410 18.989 17.538 1797.344 2.145 78.009 4.426 0.54 268754. 0.6416 16.30 0.1269 0.3067 0.1020 0.0422 2.432 19.164 17.170 1813.868 2.165 76.373 4.294 0.54 269033. 0.6159 19.55 0.1523 0.3570 0.0996 0.0425 2.450 19.300 16.772 1826.718 2.180 74.604 4.165 0.54 269331. 0.5904 22.81 0.1777 0.4040 0.0971 0.0427 2.461 19.390 16.344 1835.265 2.191 72.696 4.039 0.54 269650. 0.5653 26.07 0.2030 0.4478 0.0943 0.0428 2.466 19.428 15.882 1838.863 2.195 70.643 3.917 0.54 269991. 0.5404 29.33 0.2284 0.4885 0.0914 0.0427 2.463 19.407 15.386 1836.860 2.193 68.437 3.799 0.54 270353. 0.5159 32.59 0.2538 0.5264 0.0882 0.0425 2.452 19.320 14.855 1828.614 2.183 66.075 3.685 0.54 270738. 0.4916 35.85 0.2792 0.5616 0.0849 0.0422 2.432 19.160 14.288 1813.503 2.165 63.552 3.573 0.54 271145. 0.4676 39.11 0.3046 0.5942 0.0813 0.0417 2.402 18.922 13.684 1790.925 2.138 60.864 3.465 0.54 271574. 0.4438 42.37 0.3299 0.6241 0.0775 0.0409 2.361 18.598 13.041 1760.273 2.101 58.008 3.360 0.54 272027. 0.4201 45.63 0.3553 0.6516 0.0734 0.0400 2.308 18.185 12.362 1721.181 2.055 54.988 3.258 0.54 272502. 0.3965 48.89 0.3807 0.6766 0.0692 0.0389 2.244 17.683 11.650 1673.656 1.998 51.819 3.157 0.54 273001. 0.3730 52.14 0.4061 0.6991 0.0648 0.0376 2.170 17.093 10.908 1617.843 1.931 48.518 3.058 0.54 273522. 0.3496 55.40 0.4315 0.7188 0.0602 0.0361 2.084 16.417 10.139 1553.897 1.855 45.100 2.960 0.54 274066. 0.3262 58.66 0.4568 0.7357 0.0555 0.0345 1.987 15.657 9.347 1481.971 1.769 41.577 2.861 0.54 274634. 0.3028 61.92 0.4822 0.7495 0.0507 0.0326 1.880 14.815 8.535 1402.216 1.674 37.964 2.761 0.54 275224. 0.2792 65.18 0.5076 0.7595 0.0458 0.0306 1.763 13.891 7.705 1314.803 1.569 34.273 2.658 0.54 275838. 0.2554 68.44 0.5330 0.7653 0.0407 0.0284 1.636 12.889 6.861 1219.927 1.456 30.516 2.551 0.55 276474. 0.2313 71.70 0.5583 0.7658 0.0357 0.0260 1.499 11.810 6.004 1117.836 1.334 26.708 2.436 0.55 277134. 0.2067 74.96 0.5837 0.7594 0.0305 0.0235 1.353 10.659 5.140 1008.834 1.204 22.862 2.311 0.55 277818. 0.1814 78.22 0.6091 0.7435 0.0254 0.0208 1.198 9.438 4.271 893.313 1.066 18.996 2.168 0.55 278524. 0.1551 81.48 0.6345 0.7139 0.0202 0.0180 1.035 8.154 3.401 771.773 0.921 15.127 1.999 0.55 279255. 0.1276 84.73 0.6599 0.6623 0.0151 0.0150 0.865 6.813 2.535 644.844 0.770 11.275 1.783 0.55 280008. 0.0983 87.99 0.6852 0.5720 0.0100 0.0119 0.688 5.423 1.678 513.309 0.613 7.464 1.483 0.55 280785. 0.0665 91.25 0.7106 0.4013 0.0050 0.0088 0.507 3.995 0.836 378.096 0.451 3.719 1.003 0.55 281584. 0.0318 94.51 0.7360 0.0071 0.0001 0.0056 0.321 2.527 0.009 239.199 0.286 0.040 0.017 0.55 282377. 0.0001 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 0.1125 0.0401 3.291 23.044 23.967 2453.771 2.604 106.604 4.430 0.61 301279. 0.7508 3.67 0.0254 0.0692 0.1109 0.0407 3.341 23.395 23.634 2491.065 2.643 105.124 4.303 0.61 301509. 0.7242 7.34 0.0508 0.1344 0.1092 0.0413 3.388 23.725 23.271 2526.222 2.680 103.509 4.178 0.61 301760. 0.6977 11.00 0.0762 0.1956 0.1074 0.0418 3.431 24.028 22.876 2558.485 2.715 101.751 4.055 0.61 302031. 0.6714 14.67 0.1016 0.2531 0.1053 0.0423 3.469 24.296 22.446 2587.081 2.745 99.840 3.935 0.61 302323. 0.6454 18.34 0.1269 0.3070 0.1032 0.0427 3.502 24.523 21.980 2611.182 2.771 97.768 3.818 0.61 302638. 0.6196 22.01 0.1523 0.3573 0.1008 0.0430 3.527 24.699 21.476 2629.920 2.790 95.525 3.704 0.61 302975. 0.5942 25.67 0.1777 0.4044 0.0982 0.0432 3.543 24.816 20.931 2642.378 2.804 93.101 3.593 0.61 303336. 0.5690 29.34 0.2031 0.4483 0.0955 0.0433 3.551 24.865 20.344 2647.618 2.809 90.489 3.485 0.61 303720. 0.5442 33.01 0.2285 0.4892 0.0925 0.0432 3.547 24.837 19.712 2644.691 2.806 87.681 3.381 0.61 304130. 0.5196 36.68 0.2539 0.5273 0.0893 0.0430 3.530 24.724 19.035 2632.659 2.793 84.669 3.280 0.61 304564. 0.4953 40.35 0.2793 0.5627 0.0859 0.0426 3.501 24.517 18.311 2610.629 2.770 81.449 3.181 0.61 305024. 0.4713 44.01 0.3047 0.5955 0.0823 0.0421 3.457 24.208 17.539 2577.720 2.735 78.015 3.086 0.61 305509. 0.4474 47.68 0.3301 0.6258 0.0785 0.0414 3.397 23.789 16.718 2533.060 2.688 74.363 2.994 0.61 306020. 0.4237 51.35 0.3554 0.6536 0.0744 0.0405 3.320 23.254 15.849 2476.090 2.627 70.498 2.903 0.61 306556. 0.4001 55.02 0.3808 0.6789 0.0701 0.0393 3.228 22.603 14.937 2406.817 2.554 66.440 2.815 0.61 307119. 0.3766 58.68 0.4062 0.7018 0.0656 0.0380 3.118 21.839 13.986 2325.449 2.467 62.209 2.728 0.61 307707. 0.3531 62.35 0.4316 0.7221 0.0610 0.0365 2.993 20.964 13.000 2232.221 2.368 57.825 2.642 0.61 308321. 0.3297 66.02 0.4570 0.7395 0.0562 0.0348 2.853 19.979 11.984 2127.357 2.257 53.306 2.555 0.61 308961. 0.3062 69.69 0.4824 0.7539 0.0513 0.0329 2.697 18.887 10.942 2011.086 2.134 48.668 2.468 0.61 309627. 0.2826 73.36 0.5078 0.7648 0.0463 0.0308 2.526 17.690 9.876 1883.658 1.999 43.928 2.378 0.61 310318. 0.2587 77.02 0.5332 0.7714 0.0413 0.0285 2.341 16.391 8.791 1745.366 1.852 39.103 2.285 0.61 311036. 0.2345 80.69 0.5586 0.7729 0.0361 0.0261 2.141 14.994 7.691 1596.565 1.694 34.210 2.185 0.61 311780. 0.2098 84.36 0.5839 0.7677 0.0309 0.0235 1.928 13.502 6.580 1437.708 1.525 29.267 2.076 0.62 312550. 0.1843 88.03 0.6093 0.7532 0.0256 0.0207 1.702 11.921 5.462 1269.368 1.347 24.296 1.952 0.62 313346. 0.1579 91.69 0.6347 0.7251 0.0204 0.0178 1.465 10.258 4.344 1092.275 1.159 19.321 1.804 0.62 314169. 0.1301 95.36 0.6601 0.6750 0.0152 0.0148 1.217 8.521 3.230 907.355 0.963 14.367 1.615 0.62 315017. 0.1005 99.03 0.6855 0.5855 0.0100 0.0117 0.960 6.722 2.128 715.762 0.759 9.466 1.349 0.62 315892. 0.0681 102.70 0.7109 0.4115 0.0049 0.0085 0.696 4.873 1.045 518.858 0.551 4.650 0.914 0.62 316792. 0.0323 106.37 0.7363 -0.0140 -0.0001 0.0052 0.424 2.969 -0.021 316.180 0.335 -0.093 -0.030 0.62 317674. 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 0.1138 0.0407 4.578 28.855 29.942 3413.945 3.260 133.183 3.978 0.67 334715. 0.7535 4.07 0.0254 0.0690 0.1123 0.0413 4.649 29.299 29.536 3466.450 3.310 131.377 3.865 0.67 334972. 0.7271 8.15 0.0507 0.1340 0.1106 0.0419 4.715 29.718 29.092 3515.979 3.358 129.401 3.753 0.67 335251. 0.7007 12.22 0.0761 0.1951 0.1087 0.0424 4.776 30.102 28.607 3561.439 3.401 127.245 3.643 0.67 335553. 0.6746 16.29 0.1015 0.2525 0.1067 0.0429 4.830 30.443 28.079 3601.737 3.439 124.897 3.536 0.67 335879. 0.6486 20.36 0.1269 0.3063 0.1046 0.0433 4.876 30.730 27.505 3635.708 3.472 122.344 3.431 0.67 336230. 0.6230 24.44 0.1522 0.3567 0.1022 0.0436 4.911 30.953 26.883 3662.113 3.497 119.574 3.330 0.67 336605. 0.5976 28.51 0.1776 0.4038 0.0996 0.0438 4.935 31.102 26.209 3679.677 3.514 116.577 3.231 0.67 337008. 0.5725 32.58 0.2030 0.4477 0.0969 0.0439 4.944 31.164 25.481 3687.078 3.521 113.340 3.135 0.67 337437. 0.5477 36.65 0.2284 0.4888 0.0939 0.0439 4.939 31.130 24.698 3682.990 3.517 109.855 3.042 0.67 337893. 0.5233 40.73 0.2537 0.5270 0.0907 0.0437 4.916 30.987 23.856 3666.101 3.501 106.113 2.951 0.67 338377. 0.4990 44.80 0.2791 0.5625 0.0873 0.0433 4.875 30.725 22.955 3635.156 3.471 102.106 2.864 0.67 338889. 0.4750 48.87 0.3045 0.5955 0.0836 0.0427 4.813 30.335 21.994 3588.938 3.427 97.828 2.780 0.68 339430. 0.4512 52.94 0.3298 0.6261 0.0797 0.0420 4.729 29.805 20.970 3526.232 3.367 93.275 2.697 0.68 339999. 0.4276 57.02 0.3552 0.6542 0.0756 0.0410 4.621 29.128 19.885 3446.215 3.291 88.450 2.617 0.68 340596. 0.4040 61.09 0.3806 0.6799 0.0713 0.0399 4.491 28.305 18.745 3348.864 3.198 83.378 2.539 0.68 341222. 0.3805 65.16 0.4060 0.7033 0.0667 0.0385 4.338 27.339 17.555 3234.483 3.089 78.086 2.462 0.68 341877. 0.3571 69.24 0.4313 0.7240 0.0620 0.0370 4.162 26.231 16.321 3103.412 2.964 72.598 2.385 0.68 342561. 0.3336 73.31 0.4567 0.7421 0.0572 0.0352 3.964 24.985 15.049 2955.976 2.823 66.936 2.309 0.68 343272. 0.3101 77.38 0.4821 0.7572 0.0522 0.0333 3.745 23.603 13.742 2792.513 2.667 61.123 2.232 0.68 344013. 0.2864 81.45 0.5075 0.7688 0.0472 0.0311 3.505 22.089 12.405 2613.374 2.496 55.179 2.153 0.68 344782. 0.2625 85.53 0.5328 0.7764 0.0420 0.0288 3.244 20.446 11.044 2418.982 2.310 49.124 2.071 0.68 345580. 0.2382 89.60 0.5582 0.7791 0.0367 0.0263 2.963 18.678 9.663 2209.831 2.110 42.981 1.983 0.68 346407. 0.2134 93.67 0.5836 0.7752 0.0314 0.0237 2.664 16.791 8.268 1986.561 1.897 36.774 1.888 0.68 347262. 0.1879 97.74 0.6089 0.7623 0.0261 0.0208 2.347 14.791 6.863 1749.976 1.671 30.529 1.779 0.68 348147. 0.1613 101.82 0.6343 0.7360 0.0207 0.0179 2.013 12.688 5.457 1501.113 1.433 24.274 1.649 0.69 349060. 0.1334 105.89 0.6597 0.6882 0.0154 0.0148 1.665 10.492 4.057 1241.308 1.185 18.045 1.482 0.69 350002. 0.1034 109.96 0.6851 0.6006 0.0102 0.0116 1.304 8.218 2.671 972.250 0.928 11.880 1.246 0.69 350974. 0.0705 114.03 0.7104 0.4263 0.0050 0.0083 0.933 5.882 1.308 695.968 0.665 5.820 0.853 0.69 351972. 0.0338 118.11 0.7358 -0.0200 -0.0001 0.0049 0.552 3.479 -0.035 411.657 0.393 -0.156 -0.039 0.69 352947. 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 0.1154 0.0417 6.244 35.776 36.731 4656.046 4.042 163.378 3.578 0.74 368134. 0.7507 4.51 0.0255 0.0688 0.1139 0.0423 6.335 36.296 36.245 4723.693 4.101 161.216 3.480 0.74 368420. 0.7253 9.02 0.0511 0.1338 0.1122 0.0428 6.420 36.788 35.710 4787.655 4.156 158.840 3.383 0.74 368731. 0.6998 13.53 0.0766 0.1950 0.1103 0.0434 6.499 37.240 35.125 4846.478 4.207 156.237 3.287 0.74 369067. 0.6744 18.04 0.1022 0.2525 0.1083 0.0438 6.569 37.641 34.485 4898.658 4.253 153.390 3.193 0.74 369430. 0.6491 22.55 0.1277 0.3065 0.1061 0.0442 6.628 37.978 33.787 4942.559 4.291 150.284 3.101 0.74 369821. 0.6239 27.06 0.1533 0.3571 0.1038 0.0445 6.674 38.238 33.027 4976.447 4.320 146.903 3.010 0.74 370241. 0.5988 31.57 0.1788 0.4044 0.1012 0.0447 6.703 38.408 32.201 4998.471 4.339 143.232 2.922 0.74 370690. 0.5740 36.08 0.2043 0.4486 0.0984 0.0448 6.714 38.471 31.308 5006.726 4.346 139.257 2.836 0.74 371169. 0.5494 40.59 0.2299 0.4899 0.0953 0.0447 6.704 38.414 30.343 4999.269 4.340 134.965 2.753 0.74 371678. 0.5249 45.10 0.2554 0.5283 0.0921 0.0445 6.670 38.221 29.305 4974.183 4.318 130.347 2.672 0.74 372219. 0.5007 49.61 0.2810 0.5641 0.0886 0.0441 6.611 37.878 28.191 4929.617 4.279 125.393 2.594 0.74 372791. 0.4767 54.12 0.3065 0.5974 0.0848 0.0435 6.522 37.373 27.000 4863.795 4.222 120.095 2.518 0.74 373395. 0.4529 58.63 0.3321 0.6282 0.0808 0.0427 6.403 36.690 25.730 4774.985 4.145 114.447 2.444 0.74 374030. 0.4292 63.14 0.3576 0.6566 0.0766 0.0417 6.252 35.823 24.383 4662.066 4.047 108.456 2.372 0.74 374697. 0.4055 67.65 0.3831 0.6827 0.0721 0.0405 6.068 34.770 22.966 4525.050 3.928 102.152 2.302 0.75 375396. 0.3819 72.16 0.4087 0.7064 0.0675 0.0391 5.853 33.535 21.486 4364.378 3.789 95.570 2.233 0.75 376127. 0.3583 76.67 0.4342 0.7275 0.0627 0.0374 5.606 32.123 19.951 4180.546 3.629 88.740 2.165 0.75 376890. 0.3347 81.18 0.4598 0.7460 0.0577 0.0356 5.329 30.536 18.366 3974.046 3.450 81.692 2.096 0.75 377684. 0.3110 85.69 0.4853 0.7615 0.0526 0.0335 5.023 28.779 16.738 3745.401 3.251 74.452 2.027 0.75 378510. 0.2871 90.20 0.5109 0.7735 0.0474 0.0313 4.687 26.857 15.073 3495.195 3.034 67.046 1.956 0.75 379368. 0.2629 94.71 0.5364 0.7814 0.0420 0.0288 4.324 24.774 13.377 3224.129 2.799 59.501 1.882 0.75 380258. 0.2383 99.22 0.5619 0.7840 0.0366 0.0262 3.933 22.537 11.656 2933.092 2.546 51.846 1.802 0.75 381179. 0.2130 103.73 0.5875 0.7797 0.0312 0.0235 3.518 20.156 9.917 2623.214 2.277 44.110 1.715 0.75 382133. 0.1869 108.24 0.6130 0.7656 0.0257 0.0205 3.079 17.642 8.167 2295.969 1.993 36.326 1.613 0.75 383118. 0.1596 112.75 0.6386 0.7363 0.0202 0.0175 2.619 15.009 6.415 1953.255 1.696 28.533 1.490 0.75 384136. 0.1306 117.26 0.6641 0.6817 0.0147 0.0143 2.142 12.275 4.671 1597.478 1.387 20.775 1.326 0.76 385186. 0.0992 121.77 0.6897 0.5790 0.0093 0.0110 1.652 9.464 2.945 1231.618 1.069 13.100 1.085 0.76 386268. 0.0644 126.28 0.7152 0.3655 0.0039 0.0077 1.152 6.601 1.250 859.096 0.746 5.562 0.660 0.76 387378. 0.0256 130.79 0.7407 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 0.1172 0.0444 8.630 45.328 44.393 6435.376 5.121 197.460 3.129 0.81 401532. 0.7216 4.92 0.0255 0.0659 0.1157 0.0448 8.723 45.815 43.831 6504.614 5.176 194.960 3.056 0.81 401844. 0.7005 9.83 0.0511 0.1286 0.1141 0.0453 8.809 46.266 43.210 6568.561 5.227 192.199 2.984 0.81 402184. 0.6790 14.75 0.0766 0.1883 0.1123 0.0457 8.885 46.667 42.527 6625.548 5.272 189.160 2.911 0.81 402553. 0.6572 19.67 0.1021 0.2448 0.1103 0.0460 8.950 47.008 41.776 6673.882 5.311 185.821 2.839 0.81 402951. 0.6353 24.59 0.1276 0.2983 0.1081 0.0463 9.000 47.274 40.954 6711.663 5.341 182.163 2.768 0.81 403379. 0.6131 29.50 0.1532 0.3488 0.1057 0.0464 9.034 47.451 40.055 6736.872 5.361 178.165 2.697 0.81 403839. 0.5908 34.42 0.1787 0.3964 0.1031 0.0465 9.048 47.525 39.076 6747.321 5.369 173.808 2.627 0.81 404331. 0.5684 39.34 0.2042 0.4411 0.1003 0.0465 9.039 47.479 38.011 6740.743 5.364 169.075 2.558 0.81 404857. 0.5459 44.25 0.2297 0.4830 0.0973 0.0463 9.005 47.296 36.859 6714.776 5.343 163.949 2.490 0.81 405415. 0.5233 49.17 0.2553 0.5223 0.0940 0.0460 8.941 46.960 35.615 6667.070 5.305 158.416 2.423 0.81 406008. 0.5005 54.09 0.2808 0.5590 0.0905 0.0455 8.844 46.454 34.278 6595.281 5.248 152.467 2.357 0.81 406635. 0.4778 59.01 0.3063 0.5931 0.0867 0.0448 8.713 45.763 32.844 6497.117 5.170 146.091 2.293 0.81 407297. 0.4549 63.92 0.3319 0.6248 0.0827 0.0439 8.543 44.869 31.313 6370.186 5.069 139.280 2.230 0.81 407993. 0.4319 68.84 0.3574 0.6541 0.0784 0.0428 8.331 43.759 29.686 6212.702 4.944 132.042 2.167 0.81 408724. 0.4088 73.76 0.3829 0.6809 0.0738 0.0415 8.079 42.433 27.970 6024.355 4.794 124.412 2.106 0.81 409490. 0.3855 78.67 0.4084 0.7053 0.0691 0.0400 7.786 40.896 26.176 5806.105 4.620 116.432 2.045 0.81 410290. 0.3622 83.59 0.4340 0.7270 0.0642 0.0383 7.454 39.152 24.312 5558.613 4.423 108.141 1.984 0.81 411124. 0.3386 88.51 0.4595 0.7458 0.0591 0.0364 7.084 37.208 22.386 5282.527 4.204 99.574 1.922 0.82 411993. 0.3148 93.42 0.4850 0.7615 0.0539 0.0343 6.676 35.065 20.406 4978.339 3.962 90.765 1.859 0.82 412896. 0.2907 98.34 0.5106 0.7734 0.0485 0.0320 6.232 32.731 18.378 4646.993 3.698 81.747 1.794 0.82 413834. 0.2662 103.26 0.5361 0.7806 0.0431 0.0296 5.753 30.218 16.311 4290.210 3.414 72.550 1.724 0.82 414805. 0.2411 108.18 0.5616 0.7818 0.0375 0.0269 5.243 27.538 14.211 3909.684 3.111 63.209 1.649 0.82 415812. 0.2151 113.09 0.5871 0.7749 0.0319 0.0242 4.704 24.707 12.087 3507.757 2.791 53.761 1.563 0.82 416853. 0.1881 118.01 0.6127 0.7560 0.0263 0.0213 4.140 21.746 9.947 3087.415 2.457 44.245 1.461 0.82 417928. 0.1595 122.93 0.6382 0.7192 0.0206 0.0183 3.556 18.680 7.803 2652.038 2.110 34.709 1.335 0.82 419039. 0.1291 127.84 0.6637 0.6530 0.0150 0.0152 2.958 15.536 5.666 2205.772 1.755 25.204 1.165 0.82 420184. 0.0960 132.76 0.6892 0.5344 0.0094 0.0121 2.351 12.351 3.550 1753.466 1.395 15.790 0.918 0.83 421363. 0.0599 137.68 0.7148 0.3092 0.0039 0.0090 1.744 9.159 1.469 1300.370 1.035 6.532 0.512 0.83 422574. 0.0215 142.60 0.7403 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 0.1189 0.0504 12.478 60.497 52.879 9304.835 6.835 235.204 2.578 0.87 434911. 0.6488 5.28 0.0253 0.0587 0.1175 0.0507 12.542 60.810 52.260 9352.932 6.870 232.451 2.534 0.87 435246. 0.6342 10.56 0.0506 0.1153 0.1160 0.0509 12.593 61.057 51.571 9390.817 6.898 229.388 2.491 0.87 435611. 0.6192 15.84 0.0759 0.1700 0.1143 0.0510 12.628 61.225 50.808 9416.664 6.917 225.992 2.447 0.87 436007. 0.6038 21.12 0.1012 0.2226 0.1124 0.0511 12.644 61.303 49.964 9428.678 6.926 222.238 2.404 0.87 436435. 0.5881 26.40 0.1265 0.2731 0.1103 0.0511 12.639 61.279 49.033 9425.060 6.923 218.101 2.360 0.87 436896. 0.5720 31.69 0.1518 0.3217 0.1080 0.0510 12.611 61.142 48.012 9403.946 6.908 213.556 2.316 0.88 437390. 0.5554 36.97 0.1772 0.3681 0.1055 0.0508 12.556 60.878 46.893 9363.358 6.878 208.580 2.272 0.88 437920. 0.5385 42.25 0.2025 0.4125 0.1027 0.0504 12.473 60.474 45.673 9301.225 6.832 203.151 2.227 0.88 438485. 0.5210 47.53 0.2278 0.4548 0.0997 0.0500 12.358 59.916 44.346 9215.355 6.769 197.250 2.183 0.88 439086. 0.5031 52.81 0.2531 0.4949 0.0965 0.0493 12.208 59.188 42.909 9103.446 6.687 190.859 2.138 0.88 439724. 0.4848 58.09 0.2784 0.5330 0.0930 0.0486 12.020 58.276 41.358 8963.121 6.584 183.962 2.093 0.88 440398. 0.4659 63.37 0.3037 0.5689 0.0893 0.0477 11.790 57.162 39.692 8791.771 6.458 176.548 2.048 0.88 441110. 0.4466 68.65 0.3290 0.6026 0.0853 0.0465 11.515 55.831 37.906 8587.085 6.308 168.607 2.002 0.88 441858. 0.4267 73.93 0.3543 0.6341 0.0810 0.0452 11.193 54.270 36.003 8346.977 6.131 160.141 1.956 0.88 442643. 0.4064 79.21 0.3796 0.6633 0.0765 0.0438 10.824 52.476 33.990 8071.122 5.929 151.190 1.910 0.88 443465. 0.3855 84.49 0.4049 0.6902 0.0717 0.0421 10.407 50.455 31.880 7760.174 5.700 141.804 1.863 0.88 444324. 0.3642 89.77 0.4302 0.7141 0.0668 0.0402 9.950 48.242 29.683 7419.928 5.450 132.029 1.814 0.88 445219. 0.3422 95.06 0.4555 0.7344 0.0616 0.0382 9.459 45.859 27.407 7053.334 5.181 121.907 1.762 0.88 446150. 0.3194 100.34 0.4808 0.7503 0.0564 0.0361 8.937 43.328 25.062 6664.035 4.895 111.475 1.706 0.88 447118. 0.2956 105.62 0.5061 0.7601 0.0510 0.0339 8.394 40.696 22.655 6259.252 4.598 100.768 1.642 0.89 448122. 0.2705 110.90 0.5315 0.7640 0.0454 0.0316 7.817 37.901 20.197 5829.349 4.282 89.835 1.571 0.89 449162. 0.2445 116.18 0.5568 0.7602 0.0398 0.0292 7.211 34.964 17.697 5377.579 3.950 78.716 1.493 0.89 450239. 0.2174 121.46 0.5821 0.7464 0.0341 0.0266 6.580 31.904 15.165 4907.007 3.604 67.454 1.402 0.89 451352. 0.1890 126.74 0.6074 0.7187 0.0284 0.0240 5.931 28.754 12.612 4422.537 3.249 56.098 1.293 0.89 452502. 0.1590 132.02 0.6327 0.6713 0.0226 0.0213 5.270 25.552 10.050 3930.012 2.887 44.704 1.160 0.89 453688. 0.1273 137.30 0.6580 0.5957 0.0169 0.0186 4.606 22.333 7.495 3434.923 2.523 33.336 0.990 0.89 454911. 0.0938 142.58 0.6833 0.4778 0.0112 0.0160 3.948 19.140 4.961 2943.782 2.162 22.067 0.764 0.89 456170. 0.0589 147.86 0.7086 0.2947 0.0056 0.0134 3.303 16.015 2.469 2463.121 1.809 10.980 0.455 0.90 457464. 0.0247 153.15 0.7339 0.0029 0.0000 0.0108 2.669 12.939 0.019 1990.089 1.462 0.083 0.004 0.90 458768. 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 0.1189 0.0585 18.072 81.359 61.304 13476.058 9.192 272.682 2.063 0.94 468362. 0.5592 5.84 0.0260 0.0521 0.1177 0.0588 18.161 81.760 60.678 13542.516 9.237 269.895 2.032 0.94 468723. 0.5480 11.69 0.0520 0.1026 0.1163 0.0590 18.222 82.035 59.967 13588.048 9.268 266.733 2.002 0.94 469118. 0.5366 17.53 0.0780 0.1515 0.1147 0.0591 18.249 82.159 59.163 13608.511 9.282 263.158 1.972 0.94 469550. 0.5250 23.37 0.1040 0.1991 0.1130 0.0590 18.238 82.108 58.257 13600.105 9.277 259.128 1.943 0.94 470019. 0.5133 29.22 0.1300 0.2453 0.1110 0.0589 18.184 81.863 57.240 13559.487 9.249 254.604 1.915 0.94 470527. 0.5015 35.06 0.1560 0.2901 0.1088 0.0585 18.082 81.406 56.104 13483.763 9.197 249.549 1.887 0.94 471076. 0.4893 40.90 0.1820 0.3336 0.1064 0.0580 17.930 80.722 54.840 13370.513 9.120 243.926 1.860 0.94 471665. 0.4769 46.75 0.2080 0.3758 0.1036 0.0574 17.725 79.799 53.441 13217.621 9.016 237.704 1.834 0.94 472296. 0.4641 52.59 0.2340 0.4168 0.1007 0.0565 17.464 78.622 51.899 13022.680 8.883 230.847 1.808 0.94 472970. 0.4508 58.44 0.2600 0.4563 0.0974 0.0555 17.145 77.187 50.211 12784.959 8.721 223.339 1.781 0.94 473686. 0.4369 64.28 0.2860 0.4945 0.0938 0.0543 16.767 75.484 48.372 12502.831 8.528 215.160 1.755 0.95 474445. 0.4225 70.12 0.3120 0.5312 0.0899 0.0528 16.327 73.503 46.379 12174.801 8.304 206.294 1.728 0.95 475247. 0.4073 75.97 0.3380 0.5662 0.0858 0.0512 15.823 71.237 44.229 11799.480 8.048 196.731 1.700 0.95 476092. 0.3914 81.81 0.3640 0.5995 0.0813 0.0494 15.256 68.684 41.926 11376.645 7.760 186.486 1.672 0.95 476979. 0.3747 87.65 0.3901 0.6309 0.0766 0.0473 14.629 65.858 39.484 10908.499 7.441 175.623 1.642 0.95 477908. 0.3571 93.50 0.4161 0.6601 0.0716 0.0451 13.944 62.774 36.918 10397.672 7.092 164.211 1.610 0.95 478879. 0.3387 99.34 0.4421 0.6866 0.0664 0.0428 13.211 59.478 34.242 9851.728 6.720 152.310 1.577 0.95 479892. 0.3193 105.18 0.4681 0.7081 0.0610 0.0403 12.464 56.114 31.467 9294.536 6.340 139.964 1.536 0.95 480946. 0.2982 111.03 0.4941 0.7239 0.0555 0.0379 11.699 52.667 28.604 8723.623 5.950 127.231 1.487 0.95 482041. 0.2753 116.87 0.5201 0.7256 0.0498 0.0357 11.018 49.603 25.654 8216.104 5.604 114.111 1.416 0.95 483177. 0.2483 122.71 0.5461 0.7155 0.0439 0.0335 10.354 46.614 22.641 7721.045 5.266 100.706 1.330 0.96 484354. 0.2191 128.56 0.5721 0.6937 0.0380 0.0313 9.676 43.563 19.582 7215.675 4.922 87.103 1.231 0.96 485572. 0.1886 134.40 0.5981 0.6573 0.0320 0.0291 8.994 40.492 16.496 6706.978 4.575 73.374 1.116 0.96 486830. 0.1568 140.24 0.6241 0.6027 0.0260 0.0269 8.316 37.437 13.401 6200.986 4.230 59.608 0.980 0.96 488130. 0.1242 146.09 0.6501 0.5255 0.0200 0.0248 7.651 34.443 10.321 5705.008 3.891 45.906 0.821 0.96 489472. 0.0912 151.93 0.6761 0.4209 0.0141 0.0227 7.009 31.554 7.281 5226.438 3.565 32.388 0.632 0.96 490855. 0.0590 157.78 0.7021 0.2839 0.0084 0.0207 6.396 28.797 4.316 4769.860 3.253 19.196 0.410 0.96 492281. 0.0295 163.62 0.7281 0.1083 0.0028 0.0188 5.813 26.169 1.443 4334.572 2.957 6.416 0.151 0.97 493757. 0.0063 169.46 0.7541