21x10PN (21x10PN.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 0.0882 0.0337 0.011 0.698 0.546 8.252 0.079 2.430 30.030 0.08 49112. 0.6202 0.44 0.0220 0.0562 0.0866 0.0340 0.011 0.704 0.537 8.325 0.079 2.388 29.252 0.08 49142. 0.5989 0.88 0.0441 0.1094 0.0850 0.0342 0.011 0.709 0.527 8.391 0.080 2.343 28.475 0.08 49174. 0.5775 1.31 0.0661 0.1596 0.0832 0.0345 0.011 0.714 0.516 8.447 0.081 2.295 27.702 0.08 49209. 0.5560 1.75 0.0881 0.2069 0.0814 0.0347 0.011 0.718 0.504 8.494 0.081 2.243 26.933 0.08 49246. 0.5345 2.19 0.1101 0.2513 0.0794 0.0348 0.011 0.721 0.492 8.529 0.081 2.189 26.170 0.08 49285. 0.5129 2.63 0.1322 0.2928 0.0773 0.0349 0.011 0.723 0.479 8.549 0.082 2.130 25.413 0.08 49328. 0.4914 3.07 0.1542 0.3315 0.0750 0.0349 0.011 0.723 0.465 8.553 0.082 2.069 24.661 0.08 49372. 0.4699 3.50 0.1762 0.3674 0.0726 0.0348 0.011 0.722 0.450 8.539 0.082 2.003 23.916 0.08 49420. 0.4484 3.94 0.1983 0.4006 0.0701 0.0347 0.011 0.719 0.435 8.505 0.081 1.933 23.177 0.08 49471. 0.4269 4.38 0.2203 0.4310 0.0675 0.0345 0.011 0.714 0.418 8.450 0.081 1.860 22.443 0.08 49525. 0.4055 4.82 0.2423 0.4587 0.0647 0.0342 0.011 0.708 0.401 8.372 0.080 1.783 21.713 0.08 49581. 0.3841 5.26 0.2643 0.4836 0.0617 0.0337 0.011 0.699 0.383 8.271 0.079 1.702 20.985 0.08 49641. 0.3627 5.69 0.2864 0.5058 0.0587 0.0332 0.011 0.689 0.364 8.146 0.078 1.618 20.258 0.08 49703. 0.3414 6.13 0.3084 0.5250 0.0556 0.0326 0.011 0.676 0.344 7.997 0.076 1.532 19.528 0.08 49769. 0.3202 6.57 0.3304 0.5414 0.0523 0.0319 0.010 0.661 0.324 7.824 0.075 1.442 18.793 0.08 49838. 0.2990 7.01 0.3524 0.5546 0.0490 0.0311 0.010 0.645 0.303 7.626 0.073 1.350 18.048 0.08 49910. 0.2778 7.45 0.3745 0.5644 0.0455 0.0302 0.010 0.626 0.282 7.402 0.071 1.255 17.289 0.08 49986. 0.2566 7.89 0.3965 0.5707 0.0420 0.0292 0.010 0.605 0.260 7.153 0.068 1.158 16.510 0.08 50064. 0.2354 8.32 0.4185 0.5730 0.0384 0.0281 0.009 0.581 0.238 6.877 0.066 1.059 15.703 0.08 50146. 0.2141 8.76 0.4406 0.5707 0.0348 0.0268 0.009 0.556 0.215 6.575 0.063 0.958 14.858 0.08 50232. 0.1927 9.20 0.4626 0.5631 0.0310 0.0255 0.008 0.528 0.192 6.246 0.060 0.855 13.963 0.08 50320. 0.1711 9.64 0.4846 0.5493 0.0272 0.0240 0.008 0.498 0.169 5.890 0.056 0.751 13.001 0.08 50412. 0.1493 10.08 0.5066 0.5278 0.0234 0.0225 0.007 0.465 0.145 5.507 0.053 0.645 11.948 0.08 50508. 0.1272 10.51 0.5287 0.4965 0.0195 0.0208 0.007 0.431 0.121 5.097 0.049 0.538 10.772 0.08 50606. 0.1047 10.95 0.5507 0.4525 0.0156 0.0190 0.006 0.394 0.097 4.661 0.045 0.431 9.424 0.08 50709. 0.0820 11.39 0.5727 0.3911 0.0117 0.0171 0.006 0.355 0.073 4.200 0.040 0.323 7.833 0.08 50814. 0.0589 11.83 0.5948 0.3051 0.0078 0.0152 0.005 0.314 0.048 3.714 0.035 0.214 5.884 0.08 50923. 0.0361 12.27 0.6168 0.1817 0.0039 0.0131 0.004 0.271 0.024 3.205 0.031 0.106 3.379 0.08 51035. 0.0146 12.70 0.6388 -0.0035 -0.0001 0.0109 0.004 0.226 0.000 2.673 0.026 -0.002 -0.063 0.09 51148. 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 0.0886 0.0305 0.080 2.529 2.197 59.832 0.286 9.772 16.655 0.17 98222. 0.6898 0.88 0.0221 0.0625 0.0871 0.0308 0.081 2.556 2.159 60.473 0.289 9.603 16.194 0.17 98282. 0.6648 1.76 0.0442 0.1214 0.0855 0.0311 0.082 2.580 2.118 61.058 0.292 9.423 15.737 0.17 98347. 0.6400 2.64 0.0664 0.1769 0.0837 0.0314 0.083 2.602 2.075 61.573 0.294 9.230 15.285 0.17 98416. 0.6152 3.52 0.0885 0.2290 0.0818 0.0316 0.083 2.620 2.029 62.005 0.296 9.023 14.840 0.17 98491. 0.5906 4.40 0.1106 0.2777 0.0798 0.0318 0.084 2.634 1.979 62.338 0.298 8.804 14.401 0.17 98571. 0.5661 5.28 0.1327 0.3233 0.0777 0.0319 0.084 2.644 1.927 62.556 0.299 8.569 13.969 0.17 98656. 0.5418 6.16 0.1549 0.3657 0.0755 0.0320 0.084 2.647 1.871 62.642 0.299 8.320 13.544 0.17 98746. 0.5176 7.04 0.1770 0.4051 0.0731 0.0319 0.084 2.645 1.811 62.579 0.299 8.056 13.127 0.17 98843. 0.4936 7.92 0.1991 0.4415 0.0705 0.0318 0.084 2.635 1.748 62.352 0.298 7.776 12.717 0.17 98945. 0.4698 8.80 0.2212 0.4750 0.0678 0.0316 0.083 2.618 1.682 61.947 0.296 7.480 12.313 0.17 99053. 0.4462 9.68 0.2433 0.5056 0.0650 0.0313 0.082 2.593 1.612 61.355 0.293 7.170 11.916 0.17 99167. 0.4227 10.56 0.2655 0.5334 0.0621 0.0309 0.081 2.560 1.539 60.569 0.289 6.845 11.524 0.17 99287. 0.3995 11.44 0.2876 0.5585 0.0590 0.0304 0.080 2.518 1.463 59.584 0.284 6.508 11.137 0.17 99413. 0.3764 12.32 0.3097 0.5807 0.0558 0.0298 0.078 2.468 1.384 58.397 0.279 6.158 10.753 0.17 99546. 0.3535 13.20 0.3318 0.6000 0.0526 0.0291 0.076 2.409 1.303 57.003 0.272 5.797 10.371 0.17 99685. 0.3308 14.08 0.3540 0.6164 0.0492 0.0283 0.074 2.341 1.220 55.397 0.265 5.426 9.987 0.17 99830. 0.3082 14.96 0.3761 0.6296 0.0457 0.0273 0.072 2.264 1.134 53.576 0.256 5.045 9.601 0.17 99982. 0.2857 15.84 0.3982 0.6394 0.0422 0.0263 0.069 2.178 1.046 51.535 0.246 4.654 9.209 0.17 100141. 0.2632 16.72 0.4203 0.6455 0.0386 0.0251 0.066 2.082 0.957 49.271 0.235 4.256 8.808 0.17 100306. 0.2407 17.60 0.4424 0.6473 0.0349 0.0239 0.063 1.977 0.865 46.780 0.223 3.849 8.391 0.17 100478. 0.2181 18.48 0.4646 0.6442 0.0312 0.0225 0.059 1.862 0.773 44.060 0.210 3.436 7.953 0.17 100656. 0.1953 19.36 0.4867 0.6350 0.0274 0.0210 0.055 1.737 0.678 41.110 0.196 3.017 7.483 0.17 100842. 0.1722 20.24 0.5088 0.6183 0.0235 0.0193 0.051 1.603 0.583 37.930 0.181 2.592 6.969 0.17 101034. 0.1487 21.12 0.5309 0.5916 0.0196 0.0176 0.046 1.459 0.486 34.522 0.165 2.163 6.390 0.17 101233. 0.1245 22.00 0.5531 0.5512 0.0157 0.0158 0.041 1.305 0.389 30.889 0.147 1.731 5.716 0.17 101439. 0.0996 22.88 0.5752 0.4908 0.0118 0.0138 0.036 1.143 0.292 27.039 0.129 1.298 4.894 0.17 101652. 0.0739 23.76 0.5973 0.3990 0.0078 0.0117 0.031 0.971 0.194 22.982 0.110 0.864 3.832 0.17 101872. 0.0472 24.64 0.6194 0.2533 0.0039 0.0096 0.025 0.792 0.097 18.730 0.089 0.431 2.346 0.17 102098. 0.0204 25.52 0.6415 -0.0017 0.0000 0.0073 0.019 0.603 0.000 14.261 0.068 -0.002 -0.015 0.17 102320. 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 0.0891 0.0293 0.260 5.471 4.973 194.199 0.618 22.118 11.614 0.25 147328. 0.7236 1.32 0.0222 0.0654 0.0876 0.0297 0.263 5.535 4.887 196.454 0.625 21.737 11.283 0.25 147418. 0.6969 2.65 0.0443 0.1271 0.0860 0.0300 0.266 5.593 4.795 198.519 0.632 21.330 10.956 0.25 147516. 0.6704 3.97 0.0665 0.1850 0.0842 0.0303 0.269 5.645 4.697 200.348 0.638 20.894 10.634 0.25 147621. 0.6440 5.29 0.0887 0.2393 0.0823 0.0305 0.271 5.688 4.593 201.890 0.643 20.428 10.318 0.25 147733. 0.6178 6.61 0.1109 0.2901 0.0803 0.0307 0.272 5.722 4.481 203.094 0.646 19.931 10.007 0.25 147853. 0.5919 7.94 0.1330 0.3376 0.0782 0.0308 0.273 5.745 4.362 203.903 0.649 19.402 9.703 0.25 147982. 0.5662 9.26 0.1552 0.3817 0.0759 0.0309 0.274 5.755 4.235 204.260 0.650 18.839 9.405 0.25 148118. 0.5408 10.58 0.1774 0.4227 0.0735 0.0308 0.274 5.750 4.101 204.105 0.650 18.240 9.113 0.25 148263. 0.5156 11.90 0.1995 0.4607 0.0710 0.0307 0.273 5.730 3.958 203.383 0.647 17.606 8.827 0.25 148417. 0.4907 13.23 0.2217 0.4956 0.0683 0.0305 0.271 5.693 3.808 202.048 0.643 16.936 8.548 0.25 148580. 0.4660 14.55 0.2439 0.5277 0.0654 0.0302 0.268 5.637 3.650 200.068 0.637 16.233 8.274 0.25 148752. 0.4416 15.87 0.2661 0.5570 0.0625 0.0298 0.265 5.562 3.484 197.418 0.628 15.498 8.005 0.25 148933. 0.4175 17.20 0.2882 0.5835 0.0594 0.0293 0.260 5.468 3.312 194.081 0.618 14.733 7.741 0.25 149123. 0.3936 18.52 0.3104 0.6073 0.0562 0.0287 0.255 5.354 3.134 190.041 0.605 13.941 7.480 0.25 149323. 0.3700 19.84 0.3326 0.6282 0.0529 0.0280 0.248 5.220 2.950 185.282 0.590 13.123 7.222 0.25 149533. 0.3466 21.16 0.3547 0.6463 0.0495 0.0272 0.241 5.065 2.761 179.788 0.572 12.281 6.966 0.25 149752. 0.3234 22.49 0.3769 0.6613 0.0460 0.0262 0.233 4.889 2.567 173.544 0.552 11.417 6.708 0.25 149981. 0.3003 23.81 0.3991 0.6731 0.0425 0.0252 0.223 4.692 2.368 166.536 0.530 10.533 6.449 0.25 150220. 0.2773 25.13 0.4212 0.6815 0.0388 0.0240 0.213 4.473 2.165 158.752 0.505 9.629 6.185 0.25 150468. 0.2543 26.45 0.4434 0.6858 0.0351 0.0227 0.201 4.231 1.958 150.178 0.478 8.709 5.913 0.25 150727. 0.2312 27.78 0.4656 0.6854 0.0313 0.0213 0.189 3.967 1.747 140.808 0.448 7.773 5.629 0.25 150997. 0.2079 29.10 0.4878 0.6794 0.0275 0.0197 0.175 3.681 1.534 130.636 0.416 6.823 5.326 0.25 151276. 0.1843 30.42 0.5099 0.6661 0.0236 0.0181 0.160 3.371 1.318 119.662 0.381 5.861 4.995 0.25 151566. 0.1602 31.74 0.5321 0.6432 0.0197 0.0163 0.145 3.040 1.099 107.894 0.343 4.890 4.621 0.25 151866. 0.1354 33.07 0.5543 0.6065 0.0158 0.0144 0.128 2.686 0.879 95.346 0.303 3.912 4.184 0.25 152176. 0.1096 34.39 0.5764 0.5490 0.0118 0.0124 0.110 2.311 0.659 82.042 0.261 2.930 3.642 0.25 152497. 0.0826 35.71 0.5986 0.4572 0.0079 0.0103 0.091 1.916 0.438 68.019 0.217 1.948 2.920 0.25 152827. 0.0540 37.04 0.6208 0.3009 0.0039 0.0081 0.072 1.502 0.218 53.319 0.170 0.969 1.853 0.25 153167. 0.0242 38.36 0.6430 -0.0063 -0.0001 0.0057 0.051 1.065 -0.003 37.808 0.120 -0.014 -0.037 0.26 153496. 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 0.0898 0.0289 0.607 9.562 8.908 452.515 1.080 39.623 8.929 0.33 196427. 0.7446 1.77 0.0222 0.0671 0.0883 0.0292 0.614 9.678 8.755 458.008 1.093 38.944 8.671 0.33 196548. 0.7169 3.53 0.0444 0.1303 0.0866 0.0295 0.621 9.784 8.592 463.045 1.105 38.217 8.416 0.33 196679. 0.6893 5.30 0.0666 0.1897 0.0849 0.0298 0.627 9.879 8.417 467.510 1.116 37.439 8.166 0.33 196820. 0.6620 7.06 0.0888 0.2453 0.0830 0.0300 0.632 9.959 8.230 471.286 1.125 36.607 7.921 0.33 196970. 0.6349 8.83 0.1110 0.2973 0.0810 0.0302 0.636 10.021 8.030 474.246 1.132 35.720 7.680 0.33 197131. 0.6081 10.60 0.1332 0.3459 0.0788 0.0304 0.639 10.064 7.818 476.254 1.137 34.773 7.445 0.33 197303. 0.5817 12.36 0.1554 0.3911 0.0766 0.0304 0.640 10.083 7.591 477.169 1.139 33.765 7.216 0.33 197486. 0.5555 14.13 0.1776 0.4331 0.0741 0.0304 0.639 10.076 7.350 476.851 1.138 32.694 6.991 0.33 197681. 0.5296 15.90 0.1998 0.4719 0.0715 0.0303 0.637 10.041 7.095 475.165 1.134 31.559 6.773 0.33 197887. 0.5041 17.66 0.2220 0.5078 0.0688 0.0301 0.633 9.974 6.825 471.998 1.127 30.359 6.559 0.33 198105. 0.4788 19.43 0.2442 0.5409 0.0660 0.0298 0.627 9.874 6.542 467.269 1.116 29.099 6.350 0.33 198335. 0.4538 21.19 0.2664 0.5711 0.0630 0.0294 0.618 9.740 6.246 460.920 1.100 27.782 6.146 0.33 198577. 0.4292 22.96 0.2886 0.5985 0.0599 0.0289 0.607 9.570 5.938 452.909 1.081 26.411 5.946 0.33 198832. 0.4049 24.73 0.3108 0.6233 0.0567 0.0283 0.594 9.365 5.618 443.193 1.058 24.990 5.750 0.33 199100. 0.3808 26.49 0.3330 0.6453 0.0533 0.0275 0.579 9.123 5.288 431.736 1.031 23.523 5.556 0.34 199380. 0.3570 28.26 0.3552 0.6645 0.0499 0.0267 0.561 8.843 4.949 418.500 0.999 22.014 5.364 0.34 199673. 0.3334 30.02 0.3774 0.6808 0.0464 0.0257 0.541 8.525 4.601 403.446 0.963 20.464 5.172 0.34 199980. 0.3100 31.79 0.3996 0.6941 0.0428 0.0246 0.518 8.168 4.244 386.541 0.923 18.878 4.980 0.34 200299. 0.2867 33.56 0.4219 0.7040 0.0391 0.0234 0.493 7.771 3.880 367.751 0.878 17.257 4.785 0.34 200632. 0.2634 35.32 0.4441 0.7101 0.0354 0.0221 0.465 7.333 3.509 347.050 0.829 15.606 4.585 0.34 200979. 0.2400 37.09 0.4663 0.7118 0.0316 0.0207 0.435 6.855 3.131 324.417 0.774 13.927 4.378 0.34 201339. 0.2164 38.85 0.4885 0.7081 0.0277 0.0191 0.402 6.336 2.748 299.841 0.716 12.223 4.157 0.34 201712. 0.1925 40.62 0.5107 0.6975 0.0238 0.0174 0.367 5.775 2.360 273.323 0.653 10.498 3.917 0.34 202100. 0.1681 42.39 0.5329 0.6776 0.0199 0.0156 0.328 5.174 1.969 244.878 0.585 8.756 3.646 0.34 202501. 0.1429 44.15 0.5551 0.6442 0.0159 0.0137 0.288 4.533 1.574 214.544 0.512 7.002 3.328 0.34 202916. 0.1167 45.92 0.5773 0.5899 0.0119 0.0116 0.245 3.854 1.178 182.380 0.435 5.241 2.930 0.34 203345. 0.0889 47.69 0.5995 0.4996 0.0079 0.0095 0.199 3.137 0.782 148.476 0.354 3.480 2.390 0.34 203787. 0.0591 49.45 0.6217 0.3376 0.0039 0.0072 0.151 2.386 0.388 112.935 0.270 1.725 1.557 0.34 204242. 0.0271 51.22 0.6439 -0.0136 -0.0001 0.0048 0.101 1.590 -0.010 75.263 0.180 -0.045 -0.061 0.34 204669. 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 0.0907 0.0287 1.180 14.871 14.055 879.699 1.680 62.518 7.247 0.42 245517. 0.7591 2.21 0.0222 0.0681 0.0892 0.0291 1.194 15.056 13.816 890.667 1.701 61.456 7.036 0.42 245669. 0.7307 4.42 0.0444 0.1323 0.0875 0.0294 1.208 15.226 13.560 900.727 1.720 60.315 6.828 0.42 245833. 0.7026 6.63 0.0666 0.1925 0.0857 0.0297 1.220 15.377 13.286 909.644 1.737 59.094 6.624 0.42 246010. 0.6747 8.84 0.0889 0.2489 0.0838 0.0299 1.230 15.505 12.992 917.187 1.752 57.788 6.425 0.42 246199. 0.6471 11.04 0.1111 0.3016 0.0818 0.0301 1.238 15.605 12.678 923.105 1.763 56.393 6.230 0.42 246402. 0.6198 13.25 0.1333 0.3509 0.0797 0.0303 1.243 15.673 12.344 927.127 1.771 54.905 6.039 0.42 246617. 0.5928 15.46 0.1555 0.3968 0.0774 0.0303 1.246 15.704 11.987 928.976 1.774 53.320 5.853 0.42 246847. 0.5662 17.67 0.1777 0.4394 0.0749 0.0303 1.245 15.694 11.608 928.370 1.773 51.634 5.671 0.42 247091. 0.5399 19.88 0.1999 0.4789 0.0723 0.0302 1.241 15.637 11.206 925.041 1.767 49.846 5.495 0.42 247350. 0.5140 22.09 0.2222 0.5154 0.0696 0.0300 1.232 15.531 10.782 918.764 1.755 47.957 5.323 0.42 247624. 0.4883 24.30 0.2444 0.5491 0.0667 0.0297 1.219 15.373 10.335 909.376 1.737 45.970 5.155 0.42 247912. 0.4630 26.51 0.2666 0.5800 0.0637 0.0293 1.203 15.159 9.868 896.761 1.713 43.893 4.991 0.42 248216. 0.4381 28.72 0.2888 0.6082 0.0605 0.0288 1.181 14.890 9.382 880.832 1.682 41.730 4.831 0.42 248536. 0.4134 30.93 0.3110 0.6337 0.0573 0.0281 1.155 14.563 8.878 861.510 1.645 39.488 4.674 0.42 248872. 0.3891 33.13 0.3332 0.6565 0.0539 0.0274 1.125 14.178 8.357 838.718 1.602 37.174 4.520 0.42 249223. 0.3651 35.34 0.3555 0.6766 0.0505 0.0265 1.089 13.733 7.822 812.384 1.552 34.791 4.367 0.42 249591. 0.3413 37.55 0.3777 0.6940 0.0469 0.0255 1.049 13.227 7.272 782.432 1.494 32.344 4.215 0.42 249975. 0.3176 39.76 0.3999 0.7083 0.0433 0.0244 1.004 12.658 6.709 748.795 1.430 29.840 4.064 0.42 250375. 0.2941 41.97 0.4221 0.7195 0.0396 0.0232 0.954 12.026 6.133 711.407 1.359 27.282 3.910 0.42 250792. 0.2706 44.18 0.4443 0.7271 0.0358 0.0219 0.899 11.330 5.547 670.214 1.280 24.674 3.754 0.42 251226. 0.2471 46.39 0.4665 0.7305 0.0320 0.0204 0.838 10.568 4.951 625.177 1.194 22.022 3.592 0.42 251677. 0.2233 48.60 0.4888 0.7288 0.0280 0.0188 0.773 9.742 4.346 576.271 1.101 19.331 3.421 0.42 252145. 0.1992 50.81 0.5110 0.7205 0.0241 0.0171 0.702 8.849 3.733 523.499 1.000 16.606 3.235 0.42 252630. 0.1746 53.02 0.5332 0.7032 0.0201 0.0152 0.626 7.893 3.115 466.894 0.892 13.854 3.026 0.42 253133. 0.1492 55.22 0.5554 0.6730 0.0161 0.0133 0.545 6.872 2.491 406.528 0.776 11.082 2.780 0.42 253652. 0.1226 57.43 0.5776 0.6221 0.0120 0.0112 0.459 5.790 1.866 342.521 0.654 8.300 2.471 0.42 254189. 0.0943 59.64 0.5998 0.5348 0.0080 0.0090 0.369 4.650 1.240 275.051 0.525 5.517 2.045 0.42 254743. 0.0636 61.85 0.6220 0.3713 0.0040 0.0067 0.274 3.454 0.617 204.329 0.390 2.744 1.369 0.42 255311. 0.0300 64.06 0.6443 -0.0133 -0.0001 0.0042 0.173 2.184 -0.013 129.168 0.247 -0.060 -0.047 0.43 255837. 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 0.0918 0.0288 2.047 21.507 20.488 1526.752 2.430 91.132 6.087 0.50 294594. 0.7698 2.67 0.0224 0.0692 0.0903 0.0292 2.074 21.782 20.141 1546.266 2.461 89.585 5.908 0.50 294779. 0.7408 5.34 0.0448 0.1343 0.0886 0.0295 2.098 22.034 19.767 1564.130 2.489 87.923 5.732 0.50 294979. 0.7121 8.02 0.0672 0.1954 0.0868 0.0298 2.119 22.257 19.366 1579.927 2.515 86.140 5.560 0.50 295194. 0.6836 10.69 0.0896 0.2526 0.0849 0.0301 2.137 22.444 18.937 1593.239 2.536 84.231 5.391 0.50 295425. 0.6555 13.36 0.1120 0.3061 0.0828 0.0303 2.150 22.590 18.478 1603.608 2.552 82.189 5.226 0.50 295671. 0.6277 16.03 0.1344 0.3560 0.0806 0.0304 2.160 22.688 17.987 1610.559 2.563 80.008 5.066 0.50 295935. 0.6003 18.70 0.1568 0.4025 0.0783 0.0305 2.164 22.731 17.464 1613.587 2.568 77.681 4.909 0.50 296215. 0.5732 21.38 0.1792 0.4458 0.0758 0.0305 2.162 22.711 16.908 1612.184 2.566 75.205 4.757 0.50 296512. 0.5465 24.05 0.2015 0.4859 0.0731 0.0303 2.154 22.622 16.316 1605.872 2.556 72.576 4.609 0.50 296828. 0.5201 26.72 0.2239 0.5230 0.0703 0.0301 2.138 22.458 15.692 1594.245 2.537 69.796 4.464 0.50 297162. 0.4941 29.39 0.2463 0.5572 0.0674 0.0298 2.115 22.216 15.034 1577.019 2.510 66.871 4.324 0.50 297514. 0.4685 32.06 0.2687 0.5886 0.0643 0.0294 2.084 21.891 14.346 1553.989 2.473 63.811 4.187 0.50 297884. 0.4431 34.74 0.2911 0.6173 0.0611 0.0288 2.045 21.483 13.630 1525.003 2.427 60.625 4.054 0.50 298274. 0.4182 37.41 0.3135 0.6434 0.0578 0.0281 1.998 20.989 12.887 1489.922 2.371 57.321 3.923 0.50 298683. 0.3935 40.08 0.3359 0.6668 0.0543 0.0274 1.943 20.407 12.120 1448.615 2.306 53.909 3.795 0.50 299112. 0.3691 42.75 0.3583 0.6875 0.0508 0.0265 1.879 19.735 11.330 1400.951 2.230 50.396 3.668 0.50 299560. 0.3450 45.42 0.3807 0.7055 0.0471 0.0254 1.806 18.972 10.519 1346.799 2.143 46.790 3.543 0.50 300028. 0.3210 48.10 0.4031 0.7205 0.0434 0.0243 1.725 18.117 9.689 1286.039 2.047 43.097 3.417 0.50 300516. 0.2972 50.77 0.4255 0.7324 0.0396 0.0230 1.634 17.166 8.841 1218.557 1.939 39.325 3.291 0.50 301024. 0.2734 53.44 0.4479 0.7408 0.0358 0.0216 1.534 16.119 7.977 1144.261 1.821 35.480 3.162 0.50 301553. 0.2495 56.11 0.4703 0.7449 0.0318 0.0201 1.426 14.976 7.098 1063.082 1.692 31.570 3.028 0.51 302103. 0.2254 58.78 0.4927 0.7440 0.0278 0.0184 1.307 13.735 6.206 974.984 1.552 27.603 2.887 0.51 302673. 0.2009 61.46 0.5151 0.7364 0.0238 0.0166 1.180 12.396 5.303 879.979 1.401 23.586 2.733 0.51 303264. 0.1759 64.13 0.5375 0.7195 0.0197 0.0147 1.043 10.962 4.391 778.136 1.238 19.530 2.559 0.51 303876. 0.1498 66.80 0.5599 0.6889 0.0156 0.0126 0.898 9.433 3.473 669.600 1.066 15.447 2.352 0.51 304509. 0.1225 69.47 0.5822 0.6356 0.0114 0.0105 0.744 7.813 2.552 554.609 0.883 11.350 2.087 0.51 305163. 0.0931 72.14 0.6046 0.5397 0.0073 0.0082 0.581 6.107 1.631 433.504 0.690 7.254 1.706 0.51 305837. 0.0609 74.82 0.6270 0.3463 0.0032 0.0058 0.411 4.320 0.714 306.645 0.488 3.175 1.056 0.51 306528. 0.0249 77.49 0.6494 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 0.0932 0.0292 3.291 29.631 28.309 2454.028 3.348 125.919 5.232 0.58 343653. 0.7779 3.09 0.0222 0.0689 0.0917 0.0296 3.333 30.012 27.838 2485.552 3.391 123.825 5.080 0.58 343869. 0.7489 6.19 0.0445 0.1338 0.0900 0.0299 3.372 30.360 27.332 2514.393 3.430 121.572 4.930 0.58 344103. 0.7202 9.28 0.0667 0.1947 0.0882 0.0302 3.406 30.668 26.788 2539.885 3.465 119.154 4.784 0.58 344353. 0.6918 12.38 0.0889 0.2518 0.0863 0.0305 3.435 30.928 26.206 2561.367 3.494 116.563 4.641 0.58 344621. 0.6638 15.47 0.1112 0.3053 0.0842 0.0307 3.457 31.130 25.582 2578.131 3.517 113.789 4.501 0.58 344908. 0.6360 18.57 0.1334 0.3553 0.0820 0.0308 3.472 31.266 24.916 2589.413 3.532 110.825 4.364 0.58 345214. 0.6087 21.66 0.1556 0.4019 0.0797 0.0309 3.479 31.327 24.204 2594.416 3.539 107.661 4.232 0.58 345540. 0.5817 24.76 0.1779 0.4453 0.0772 0.0308 3.476 31.302 23.447 2592.345 3.536 104.292 4.102 0.58 345885. 0.5550 27.85 0.2001 0.4856 0.0746 0.0307 3.463 31.182 22.642 2582.429 3.523 100.713 3.977 0.58 346252. 0.5287 30.95 0.2223 0.5230 0.0718 0.0305 3.438 30.960 21.791 2564.017 3.498 96.925 3.855 0.58 346638. 0.5028 34.04 0.2446 0.5576 0.0688 0.0302 3.402 30.629 20.894 2536.631 3.460 92.938 3.736 0.58 347046. 0.4772 37.14 0.2668 0.5895 0.0657 0.0297 3.352 30.186 19.955 2499.953 3.410 88.762 3.621 0.59 347476. 0.4519 40.23 0.2890 0.6187 0.0625 0.0292 3.291 29.628 18.977 2453.737 3.347 84.411 3.508 0.59 347927. 0.4270 43.33 0.3113 0.6454 0.0591 0.0285 3.215 28.952 17.963 2397.775 3.271 79.897 3.398 0.59 348400. 0.4024 46.42 0.3335 0.6695 0.0557 0.0277 3.127 28.156 16.914 2331.865 3.181 75.233 3.290 0.59 348896. 0.3781 49.52 0.3557 0.6911 0.0521 0.0268 3.025 27.238 15.834 2255.807 3.077 70.429 3.184 0.59 349414. 0.3540 52.61 0.3779 0.7101 0.0485 0.0258 2.909 26.195 14.724 2169.403 2.959 65.495 3.079 0.59 349955. 0.3301 55.71 0.4002 0.7263 0.0447 0.0247 2.779 25.024 13.588 2072.466 2.827 60.440 2.974 0.59 350519. 0.3063 58.80 0.4224 0.7395 0.0409 0.0234 2.635 23.724 12.427 1964.817 2.680 55.275 2.869 0.59 351106. 0.2826 61.90 0.4446 0.7495 0.0370 0.0220 2.476 22.293 11.243 1846.305 2.519 50.008 2.762 0.59 351716. 0.2588 64.99 0.4669 0.7556 0.0331 0.0204 2.302 20.730 10.038 1716.817 2.342 44.650 2.652 0.59 352350. 0.2348 68.09 0.4891 0.7571 0.0290 0.0188 2.114 19.033 8.815 1576.289 2.150 39.209 2.536 0.59 353008. 0.2104 71.18 0.5113 0.7526 0.0249 0.0169 1.911 17.203 7.576 1424.725 1.944 33.699 2.412 0.59 353689. 0.1855 74.28 0.5336 0.7400 0.0208 0.0150 1.693 15.241 6.324 1262.214 1.722 28.131 2.273 0.59 354395. 0.1597 77.37 0.5558 0.7153 0.0167 0.0130 1.460 13.149 5.063 1088.967 1.486 22.521 2.109 0.59 355124. 0.1326 80.47 0.5780 0.6710 0.0125 0.0108 1.214 10.932 3.796 905.328 1.235 16.887 1.902 0.59 355877. 0.1036 83.56 0.6003 0.5903 0.0083 0.0085 0.955 8.595 2.529 711.812 0.971 11.249 1.612 0.59 356654. 0.0716 86.66 0.6225 0.4284 0.0042 0.0061 0.683 6.146 1.266 509.029 0.694 5.630 1.128 0.59 357452. 0.0355 89.75 0.6447 -0.0101 -0.0001 0.0035 0.393 3.535 -0.017 292.748 0.399 -0.074 -0.026 0.60 358169. 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 0.0949 0.0298 5.011 39.479 37.660 3736.640 4.460 167.511 4.571 0.67 392689. 0.7838 3.54 0.0223 0.0689 0.0934 0.0302 5.076 39.991 37.044 3785.128 4.518 164.771 4.439 0.67 392939. 0.7549 7.08 0.0445 0.1338 0.0917 0.0305 5.135 40.459 36.379 3829.404 4.571 161.816 4.309 0.67 393208. 0.7262 10.62 0.0668 0.1948 0.0899 0.0308 5.188 40.871 35.665 3868.431 4.618 158.638 4.182 0.67 393497. 0.6978 14.17 0.0890 0.2520 0.0880 0.0311 5.232 41.217 34.898 3901.191 4.657 155.225 4.057 0.67 393807. 0.6697 17.71 0.1113 0.3055 0.0859 0.0313 5.266 41.486 34.075 3926.591 4.687 151.567 3.936 0.67 394138. 0.6420 21.25 0.1336 0.3556 0.0837 0.0314 5.288 41.664 33.195 3943.465 4.707 147.650 3.818 0.67 394491. 0.6146 24.79 0.1558 0.4024 0.0813 0.0315 5.298 41.739 32.254 3950.608 4.716 143.465 3.703 0.67 394866. 0.5876 28.33 0.1781 0.4460 0.0788 0.0315 5.293 41.699 31.251 3946.795 4.711 139.003 3.591 0.67 395265. 0.5610 31.87 0.2003 0.4866 0.0761 0.0313 5.271 41.531 30.184 3930.855 4.692 134.256 3.483 0.67 395686. 0.5346 35.41 0.2226 0.5243 0.0732 0.0311 5.232 41.223 29.053 3901.776 4.657 129.228 3.377 0.67 396132. 0.5086 38.95 0.2449 0.5593 0.0702 0.0308 5.175 40.770 27.862 3858.830 4.606 123.929 3.275 0.67 396602. 0.4830 42.50 0.2671 0.5915 0.0671 0.0303 5.098 40.164 26.613 3801.528 4.538 118.374 3.175 0.67 397097. 0.4577 46.04 0.2894 0.6212 0.0638 0.0297 5.001 39.403 25.311 3729.509 4.452 112.582 3.078 0.67 397616. 0.4327 49.58 0.3116 0.6484 0.0604 0.0290 4.885 38.484 23.959 3642.485 4.348 106.570 2.983 0.67 398161. 0.4080 53.12 0.3339 0.6731 0.0569 0.0282 4.747 37.403 22.562 3540.160 4.226 100.354 2.891 0.67 398730. 0.3836 56.66 0.3562 0.6953 0.0532 0.0273 4.589 36.157 21.121 3422.252 4.085 93.948 2.799 0.67 399326. 0.3595 60.20 0.3784 0.7150 0.0495 0.0262 4.410 34.744 19.642 3288.473 3.925 87.368 2.709 0.67 399948. 0.3355 63.74 0.4007 0.7320 0.0457 0.0250 4.209 33.160 18.126 3138.539 3.746 80.624 2.619 0.67 400595. 0.3116 67.28 0.4229 0.7462 0.0418 0.0237 3.986 31.402 16.576 2972.196 3.548 73.731 2.530 0.67 401269. 0.2878 70.83 0.4452 0.7571 0.0378 0.0222 3.740 29.469 14.995 2789.217 3.329 66.699 2.438 0.67 401970. 0.2638 74.37 0.4674 0.7645 0.0337 0.0206 3.472 27.358 13.387 2589.435 3.091 59.543 2.345 0.67 402698. 0.2397 77.91 0.4897 0.7673 0.0296 0.0189 3.182 25.069 11.753 2372.752 2.832 52.276 2.247 0.67 403453. 0.2152 81.45 0.5120 0.7645 0.0255 0.0170 2.869 22.601 10.097 2139.176 2.553 44.912 2.141 0.68 404234. 0.1901 84.99 0.5342 0.7537 0.0212 0.0151 2.533 19.956 8.424 1888.851 2.255 37.470 2.023 0.68 405043. 0.1640 88.53 0.5565 0.7312 0.0170 0.0129 2.175 17.138 6.738 1622.096 1.936 29.970 1.884 0.68 405880. 0.1366 92.07 0.5787 0.6894 0.0127 0.0107 1.796 14.152 5.044 1339.461 1.599 22.435 1.708 0.68 406743. 0.1072 95.61 0.6010 0.6111 0.0084 0.0083 1.397 11.007 3.348 1041.772 1.244 14.893 1.458 0.68 407633. 0.0745 99.16 0.6233 0.4478 0.0042 0.0058 0.979 7.713 1.658 730.025 0.871 7.374 1.030 0.68 408547. 0.0371 102.70 0.6455 -0.0476 -0.0002 0.0031 0.524 4.132 -0.091 391.093 0.467 -0.405 -0.106 0.68 409242. 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 0.0971 0.0309 7.415 51.929 48.736 5529.471 5.867 216.778 3.998 0.75 441693. 0.7798 4.02 0.0224 0.0685 0.0955 0.0313 7.499 52.516 47.954 5591.951 5.933 213.298 3.890 0.75 441978. 0.7526 8.03 0.0449 0.1332 0.0938 0.0316 7.575 53.050 47.106 5648.790 5.994 209.528 3.782 0.75 442287. 0.7254 12.05 0.0673 0.1941 0.0920 0.0319 7.642 53.517 46.191 5698.530 6.046 205.458 3.677 0.75 442618. 0.6982 16.06 0.0897 0.2515 0.0900 0.0321 7.697 53.904 45.205 5739.689 6.090 201.073 3.572 0.75 442974. 0.6711 20.08 0.1122 0.3054 0.0879 0.0323 7.739 54.194 44.145 5770.638 6.123 196.357 3.470 0.75 443353. 0.6441 24.09 0.1346 0.3558 0.0857 0.0324 7.764 54.373 43.007 5789.641 6.143 191.295 3.369 0.75 443759. 0.6174 28.11 0.1570 0.4030 0.0832 0.0324 7.771 54.421 41.788 5794.820 6.148 185.872 3.271 0.75 444190. 0.5908 32.12 0.1795 0.4470 0.0806 0.0324 7.757 54.322 40.485 5784.274 6.137 180.076 3.175 0.75 444647. 0.5644 36.14 0.2019 0.4881 0.0779 0.0322 7.719 54.058 39.096 5756.154 6.107 173.900 3.081 0.75 445131. 0.5382 40.15 0.2243 0.5262 0.0749 0.0320 7.656 53.614 37.623 5708.850 6.057 167.347 2.989 0.75 445643. 0.5123 44.17 0.2468 0.5615 0.0718 0.0316 7.565 52.978 36.068 5641.123 5.985 160.430 2.900 0.75 446182. 0.4866 48.18 0.2692 0.5942 0.0686 0.0311 7.446 52.142 34.436 5552.146 5.891 153.172 2.813 0.75 446750. 0.4613 52.20 0.2916 0.6244 0.0652 0.0305 7.297 51.101 32.733 5441.277 5.773 145.597 2.729 0.75 447345. 0.4362 56.21 0.3141 0.6520 0.0617 0.0297 7.118 49.849 30.964 5307.989 5.632 137.728 2.646 0.75 447969. 0.4114 60.23 0.3365 0.6772 0.0580 0.0288 6.909 48.383 29.134 5151.827 5.466 129.587 2.565 0.75 448622. 0.3868 64.24 0.3589 0.7000 0.0543 0.0278 6.668 46.697 27.247 4972.366 5.276 121.195 2.485 0.75 449304. 0.3625 68.26 0.3814 0.7202 0.0504 0.0267 6.396 44.790 25.308 4769.244 5.060 112.570 2.407 0.76 450016. 0.3383 72.27 0.4038 0.7378 0.0465 0.0254 6.091 42.657 23.320 4542.092 4.819 103.728 2.329 0.76 450758. 0.3142 76.29 0.4262 0.7526 0.0424 0.0240 5.754 40.295 21.287 4290.596 4.552 94.687 2.250 0.76 451529. 0.2901 80.30 0.4487 0.7642 0.0383 0.0225 5.384 37.702 19.214 4014.520 4.260 85.462 2.171 0.76 452331. 0.2659 84.32 0.4711 0.7721 0.0341 0.0208 4.980 34.877 17.102 3713.743 3.940 76.071 2.089 0.76 453163. 0.2414 88.33 0.4936 0.7754 0.0298 0.0190 4.544 31.821 14.958 3388.304 3.595 66.532 2.002 0.76 454026. 0.2164 92.35 0.5160 0.7726 0.0255 0.0170 4.075 28.536 12.784 3038.490 3.224 56.864 1.908 0.76 454920. 0.1907 96.37 0.5384 0.7613 0.0211 0.0149 3.574 25.027 10.587 2664.875 2.828 47.092 1.802 0.76 455844. 0.1638 100.38 0.5609 0.7367 0.0167 0.0127 3.042 21.304 8.373 2268.427 2.407 37.242 1.674 0.76 456800. 0.1354 104.40 0.5833 0.6896 0.0122 0.0104 2.482 17.380 6.148 1850.582 1.964 27.347 1.507 0.76 457786. 0.1044 108.41 0.6057 0.5982 0.0078 0.0079 1.895 13.273 3.922 1413.302 1.500 17.443 1.259 0.76 458802. 0.0696 112.43 0.6282 0.3967 0.0034 0.0054 1.286 9.004 1.701 958.753 1.017 7.568 0.805 0.76 459843. 0.0293 116.44 0.6506 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 0.0997 0.0348 11.446 72.140 61.767 8534.961 8.150 274.740 3.282 0.83 490649. 0.7208 4.46 0.0224 0.0629 0.0981 0.0350 11.494 72.447 60.819 8571.350 8.185 270.524 3.218 0.83 490970. 0.7013 8.91 0.0448 0.1232 0.0965 0.0351 11.531 72.679 59.787 8598.825 8.211 265.931 3.154 0.83 491316. 0.6813 13.37 0.0672 0.1810 0.0947 0.0352 11.554 72.824 58.666 8615.917 8.228 260.946 3.088 0.83 491688. 0.6609 17.83 0.0896 0.2362 0.0927 0.0352 11.561 72.868 57.453 8621.099 8.233 255.549 3.023 0.83 492087. 0.6402 22.28 0.1120 0.2888 0.0906 0.0351 11.550 72.797 56.142 8612.708 8.225 249.718 2.957 0.83 492513. 0.6190 26.74 0.1345 0.3388 0.0883 0.0350 11.518 72.596 54.729 8588.915 8.202 243.436 2.890 0.83 492968. 0.5974 31.20 0.1569 0.3861 0.0859 0.0349 11.463 72.247 53.211 8547.712 8.162 236.683 2.824 0.83 493452. 0.5755 35.65 0.1793 0.4309 0.0832 0.0346 11.381 71.734 51.584 8486.926 8.104 229.445 2.757 0.83 493965. 0.5532 40.11 0.2017 0.4730 0.0804 0.0343 11.270 71.036 49.845 8404.363 8.026 221.710 2.690 0.83 494509. 0.5307 44.56 0.2241 0.5125 0.0774 0.0339 11.128 70.137 47.995 8298.080 7.924 213.481 2.623 0.84 495082. 0.5078 49.02 0.2465 0.5495 0.0743 0.0333 10.952 69.026 46.038 8166.582 7.799 204.777 2.557 0.84 495686. 0.4848 53.48 0.2689 0.5839 0.0710 0.0327 10.740 67.693 43.980 8008.836 7.648 195.625 2.491 0.84 496321. 0.4615 57.93 0.2913 0.6159 0.0675 0.0319 10.492 66.131 41.830 7824.022 7.471 186.059 2.425 0.84 496987. 0.4382 62.39 0.3137 0.6453 0.0639 0.0311 10.207 64.333 39.593 7611.342 7.268 176.108 2.359 0.84 497685. 0.4148 66.85 0.3361 0.6723 0.0601 0.0301 9.883 62.292 37.276 7369.920 7.038 165.802 2.294 0.84 498415. 0.3913 71.30 0.3586 0.6966 0.0563 0.0290 9.521 60.010 34.884 7099.907 6.780 155.165 2.229 0.84 499177. 0.3678 75.76 0.3810 0.7181 0.0523 0.0278 9.121 57.490 32.424 6801.759 6.495 144.220 2.162 0.84 499971. 0.3440 80.22 0.4034 0.7367 0.0482 0.0264 8.681 54.717 29.899 6473.646 6.182 132.991 2.095 0.84 500798. 0.3201 84.67 0.4258 0.7518 0.0441 0.0250 8.203 51.703 27.315 6117.105 5.841 121.499 2.025 0.84 501657. 0.2958 89.13 0.4482 0.7629 0.0398 0.0234 7.687 48.452 24.677 5732.483 5.474 109.762 1.952 0.84 502550. 0.2710 93.59 0.4706 0.7696 0.0355 0.0217 7.130 44.941 21.989 5317.092 5.077 97.806 1.876 0.84 503477. 0.2458 98.04 0.4930 0.7705 0.0311 0.0199 6.534 41.182 19.256 4872.342 4.653 85.652 1.793 0.84 504437. 0.2198 102.50 0.5154 0.7637 0.0266 0.0180 5.900 37.186 16.485 4399.593 4.201 73.326 1.700 0.84 505430. 0.1928 106.96 0.5378 0.7459 0.0221 0.0159 5.231 32.972 13.681 3901.012 3.725 60.854 1.591 0.85 506458. 0.1644 111.41 0.5602 0.7114 0.0175 0.0138 4.532 28.564 10.852 3379.446 3.227 48.272 1.457 0.85 507520. 0.1341 115.87 0.5827 0.6500 0.0129 0.0116 3.806 23.990 8.008 2838.356 2.710 35.618 1.280 0.85 508615. 0.1012 120.32 0.6051 0.5408 0.0083 0.0093 3.060 19.288 5.158 2281.948 2.179 22.942 1.025 0.85 509744. 0.0651 124.78 0.6275 0.3348 0.0037 0.0070 2.299 14.493 2.314 1714.638 1.637 10.290 0.612 0.85 510900. 0.0260 129.24 0.6499 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 0.1015 0.0434 18.981 108.758 76.147 14154.142 12.287 338.704 2.440 0.92 539610. 0.5950 4.90 0.0224 0.0517 0.1002 0.0434 18.976 108.731 75.128 14150.572 12.284 334.169 2.408 0.92 539956. 0.5832 9.79 0.0448 0.1020 0.0987 0.0433 18.938 108.511 73.997 14121.957 12.260 329.140 2.377 0.92 540332. 0.5712 14.69 0.0671 0.1510 0.0970 0.0431 18.863 108.082 72.749 14066.077 12.211 323.588 2.346 0.92 540738. 0.5591 19.58 0.0895 0.1988 0.0952 0.0429 18.749 107.430 71.376 13981.241 12.137 317.480 2.316 0.92 541175. 0.5466 24.48 0.1119 0.2452 0.0932 0.0425 18.595 106.547 69.872 13866.285 12.038 310.789 2.286 0.92 541644. 0.5338 29.37 0.1343 0.2904 0.0910 0.0421 18.399 105.425 68.230 13720.363 11.911 303.488 2.256 0.92 542145. 0.5206 34.27 0.1566 0.3343 0.0886 0.0415 18.161 104.060 66.446 13542.690 11.757 295.553 2.225 0.92 542679. 0.5069 39.16 0.1790 0.3768 0.0860 0.0409 17.879 102.446 64.516 13332.581 11.574 286.965 2.195 0.92 543247. 0.4926 44.06 0.2014 0.4179 0.0833 0.0401 17.553 100.576 62.435 13089.279 11.363 277.712 2.164 0.92 543848. 0.4777 48.95 0.2238 0.4574 0.0803 0.0393 17.182 98.448 60.206 12812.252 11.123 267.798 2.131 0.92 544483. 0.4621 53.85 0.2462 0.4953 0.0771 0.0383 16.764 96.058 57.833 12501.236 10.853 257.241 2.098 0.92 545152. 0.4459 58.74 0.2685 0.5316 0.0738 0.0373 16.302 93.410 55.324 12156.639 10.553 246.081 2.064 0.92 545856. 0.4290 63.64 0.2909 0.5660 0.0703 0.0361 15.796 90.506 52.689 11778.779 10.225 234.360 2.029 0.92 546594. 0.4115 68.53 0.3133 0.5986 0.0666 0.0348 15.245 87.349 49.937 11367.870 9.869 222.121 1.992 0.92 547366. 0.3934 73.43 0.3357 0.6292 0.0628 0.0335 14.650 83.940 47.078 10924.147 9.483 209.404 1.955 0.92 548174. 0.3747 78.32 0.3580 0.6577 0.0588 0.0320 14.011 80.278 44.121 10447.642 9.070 196.248 1.915 0.92 549017. 0.3555 83.22 0.3804 0.6837 0.0548 0.0305 13.330 76.376 41.072 9939.845 8.629 182.686 1.874 0.92 549895. 0.3356 88.11 0.4028 0.7061 0.0506 0.0289 12.624 72.333 37.937 9413.566 8.172 168.743 1.828 0.92 550808. 0.3146 93.01 0.4252 0.7246 0.0463 0.0272 11.885 68.099 34.724 8862.587 7.694 154.453 1.777 0.92 551758. 0.2926 97.90 0.4476 0.7370 0.0419 0.0255 11.136 63.808 31.437 8304.202 7.209 139.834 1.717 0.93 552743. 0.2690 102.80 0.4699 0.7358 0.0374 0.0239 10.458 59.925 28.073 7798.758 6.770 124.871 1.633 0.93 553765. 0.2417 107.69 0.4923 0.7259 0.0329 0.0223 9.752 55.880 24.651 7272.354 6.313 109.646 1.537 0.93 554823. 0.2133 112.59 0.5147 0.7048 0.0282 0.0206 9.021 51.689 21.177 6726.899 5.840 94.197 1.428 0.93 555917. 0.1836 117.48 0.5371 0.6691 0.0236 0.0189 8.270 47.387 17.664 6167.028 5.354 78.568 1.299 0.93 557048. 0.1526 122.38 0.5594 0.6139 0.0188 0.0172 7.507 43.012 14.121 5597.730 4.859 62.811 1.144 0.93 558216. 0.1201 127.27 0.5818 0.5321 0.0141 0.0154 6.739 38.611 10.565 5024.950 4.362 46.994 0.954 0.93 559420. 0.0866 132.17 0.6042 0.4137 0.0094 0.0137 5.974 34.228 7.013 4454.570 3.867 31.193 0.714 0.93 560661. 0.0528 137.06 0.6266 0.2440 0.0046 0.0119 5.218 29.899 3.483 3891.199 3.378 15.495 0.406 0.93 561936. 0.0212 141.96 0.6490 -0.0052 -0.0001 0.0101 4.437 25.423 -0.060 3308.672 2.872 -0.269 -0.008 0.94 563180. 0.0000