21.5x10WPN (215x10WPN.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 0.0847 0.0318 0.012 0.743 0.579 8.796 0.084 2.575 29.845 0.09 46061. 0.6191 0.44 0.0216 0.0562 0.0832 0.0321 0.012 0.750 0.569 8.876 0.085 2.530 29.062 0.09 46088. 0.5976 0.88 0.0433 0.1094 0.0816 0.0323 0.012 0.756 0.558 8.949 0.085 2.482 28.280 0.09 46117. 0.5760 1.32 0.0649 0.1596 0.0800 0.0325 0.012 0.762 0.546 9.012 0.086 2.430 27.501 0.09 46148. 0.5543 1.76 0.0866 0.2068 0.0781 0.0327 0.012 0.766 0.534 9.064 0.087 2.376 26.729 0.09 46182. 0.5326 2.21 0.1082 0.2510 0.0762 0.0329 0.012 0.769 0.521 9.102 0.087 2.317 25.962 0.09 46217. 0.5109 2.65 0.1299 0.2924 0.0742 0.0330 0.012 0.771 0.507 9.125 0.087 2.255 25.201 0.09 46256. 0.4893 3.09 0.1515 0.3310 0.0720 0.0330 0.012 0.772 0.492 9.131 0.087 2.189 24.448 0.09 46296. 0.4676 3.53 0.1732 0.3667 0.0697 0.0329 0.012 0.771 0.476 9.118 0.087 2.119 23.701 0.09 46339. 0.4461 3.97 0.1948 0.3996 0.0673 0.0328 0.012 0.768 0.460 9.083 0.087 2.045 22.960 0.09 46385. 0.4245 4.41 0.2165 0.4298 0.0647 0.0326 0.012 0.763 0.442 9.026 0.086 1.967 22.225 0.09 46434. 0.4030 4.85 0.2381 0.4572 0.0620 0.0323 0.012 0.756 0.424 8.945 0.085 1.885 21.493 0.09 46485. 0.3816 5.29 0.2598 0.4819 0.0592 0.0319 0.012 0.747 0.405 8.839 0.084 1.800 20.765 0.09 46539. 0.3602 5.73 0.2814 0.5038 0.0563 0.0314 0.012 0.736 0.385 8.709 0.083 1.711 20.037 0.09 46596. 0.3389 6.18 0.3031 0.5228 0.0533 0.0309 0.011 0.723 0.364 8.553 0.082 1.619 19.307 0.09 46655. 0.3176 6.62 0.3247 0.5388 0.0501 0.0302 0.011 0.707 0.343 8.370 0.080 1.524 18.572 0.09 46718. 0.2965 7.06 0.3464 0.5517 0.0469 0.0295 0.011 0.690 0.321 8.161 0.078 1.427 17.828 0.09 46783. 0.2753 7.50 0.3680 0.5612 0.0436 0.0286 0.011 0.670 0.298 7.925 0.076 1.327 17.070 0.09 46852. 0.2542 7.94 0.3897 0.5671 0.0403 0.0277 0.010 0.648 0.275 7.662 0.073 1.224 16.292 0.09 46923. 0.2330 8.38 0.4113 0.5691 0.0368 0.0266 0.010 0.623 0.252 7.371 0.070 1.119 15.487 0.09 46997. 0.2118 8.82 0.4330 0.5665 0.0333 0.0255 0.009 0.596 0.228 7.051 0.067 1.013 14.645 0.09 47075. 0.1905 9.26 0.4546 0.5586 0.0297 0.0242 0.009 0.567 0.203 6.702 0.064 0.904 13.753 0.09 47155. 0.1691 9.71 0.4762 0.5444 0.0261 0.0228 0.008 0.535 0.178 6.325 0.060 0.794 12.796 0.09 47239. 0.1474 10.15 0.4979 0.5226 0.0224 0.0214 0.008 0.500 0.153 5.919 0.057 0.682 11.750 0.09 47325. 0.1254 10.59 0.5195 0.4912 0.0187 0.0198 0.007 0.464 0.128 5.485 0.052 0.569 10.582 0.09 47415. 0.1032 11.03 0.5412 0.4471 0.0150 0.0181 0.007 0.424 0.102 5.022 0.048 0.455 9.247 0.09 47508. 0.0807 11.47 0.5628 0.3859 0.0112 0.0164 0.006 0.383 0.077 4.531 0.043 0.341 7.674 0.09 47604. 0.0579 11.91 0.5845 0.3003 0.0074 0.0145 0.005 0.339 0.051 4.015 0.038 0.226 5.752 0.09 47703. 0.0354 12.35 0.6061 0.1782 0.0037 0.0125 0.005 0.294 0.025 3.473 0.033 0.112 3.291 0.09 47805. 0.0142 12.79 0.6278 -0.0046 -0.0001 0.0105 0.004 0.246 -0.001 2.905 0.028 -0.002 -0.081 0.09 47908. 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 0.0851 0.0287 0.085 2.690 2.328 63.645 0.304 10.354 16.589 0.17 92120. 0.6901 0.89 0.0217 0.0626 0.0837 0.0290 0.086 2.719 2.287 64.349 0.307 10.174 16.123 0.17 92174. 0.6649 1.77 0.0435 0.1217 0.0821 0.0293 0.087 2.747 2.244 64.992 0.310 9.982 15.662 0.17 92232. 0.6397 2.66 0.0652 0.1772 0.0804 0.0296 0.088 2.771 2.198 65.560 0.313 9.777 15.206 0.17 92295. 0.6147 3.54 0.0870 0.2293 0.0786 0.0298 0.089 2.791 2.149 66.037 0.315 9.557 14.757 0.17 92363. 0.5898 4.43 0.1087 0.2780 0.0767 0.0300 0.089 2.806 2.096 66.406 0.317 9.322 14.315 0.17 92435. 0.5651 5.32 0.1304 0.3235 0.0746 0.0301 0.089 2.817 2.040 66.651 0.318 9.073 13.881 0.17 92512. 0.5405 6.20 0.1522 0.3658 0.0724 0.0301 0.090 2.821 1.980 66.754 0.319 8.807 13.454 0.17 92594. 0.5162 7.09 0.1739 0.4050 0.0701 0.0301 0.089 2.819 1.917 66.698 0.318 8.526 13.034 0.17 92681. 0.4920 7.97 0.1957 0.4413 0.0677 0.0300 0.089 2.809 1.850 66.469 0.317 8.228 12.622 0.17 92773. 0.4681 8.86 0.2174 0.4746 0.0651 0.0298 0.089 2.791 1.779 66.051 0.315 7.914 12.217 0.17 92871. 0.4443 9.75 0.2391 0.5050 0.0624 0.0295 0.088 2.765 1.705 65.435 0.312 7.584 11.819 0.17 92974. 0.4208 10.63 0.2609 0.5326 0.0595 0.0292 0.087 2.731 1.628 64.613 0.309 7.240 11.426 0.17 93083. 0.3975 11.52 0.2826 0.5574 0.0566 0.0287 0.085 2.687 1.547 63.582 0.304 6.883 11.038 0.17 93197. 0.3744 12.40 0.3044 0.5793 0.0536 0.0281 0.084 2.634 1.464 62.335 0.298 6.512 10.653 0.17 93317. 0.3515 13.29 0.3261 0.5984 0.0504 0.0275 0.082 2.572 1.378 60.867 0.291 6.130 10.270 0.17 93443. 0.3287 14.18 0.3478 0.6144 0.0472 0.0267 0.079 2.501 1.290 59.175 0.283 5.737 9.886 0.17 93575. 0.3061 15.06 0.3696 0.6273 0.0439 0.0258 0.077 2.420 1.199 57.252 0.273 5.334 9.500 0.17 93713. 0.2836 15.95 0.3913 0.6368 0.0405 0.0249 0.074 2.328 1.106 55.096 0.263 4.921 9.108 0.17 93857. 0.2612 16.83 0.4130 0.6425 0.0370 0.0238 0.071 2.227 1.012 52.701 0.252 4.499 8.706 0.17 94007. 0.2387 17.72 0.4348 0.6440 0.0335 0.0226 0.067 2.116 0.915 50.064 0.239 4.070 8.289 0.17 94163. 0.2162 18.61 0.4565 0.6404 0.0299 0.0213 0.063 1.994 0.817 47.182 0.225 3.633 7.851 0.17 94325. 0.1935 19.49 0.4783 0.6309 0.0262 0.0199 0.059 1.862 0.717 44.055 0.210 3.189 7.382 0.17 94493. 0.1705 20.38 0.5000 0.6137 0.0225 0.0184 0.055 1.719 0.616 40.682 0.194 2.741 6.870 0.17 94668. 0.1470 21.26 0.5217 0.5867 0.0188 0.0167 0.050 1.566 0.514 37.064 0.177 2.287 6.293 0.17 94849. 0.1230 22.15 0.5435 0.5459 0.0151 0.0150 0.045 1.403 0.412 33.206 0.159 1.831 5.622 0.17 95036. 0.0983 23.04 0.5652 0.4853 0.0113 0.0131 0.039 1.230 0.308 29.114 0.139 1.372 4.806 0.17 95230. 0.0728 23.92 0.5870 0.3937 0.0075 0.0112 0.033 1.048 0.205 24.798 0.118 0.913 3.754 0.17 95429. 0.0464 24.81 0.6087 0.2488 0.0037 0.0091 0.027 0.857 0.102 20.269 0.097 0.455 2.288 0.17 95635. 0.0199 25.69 0.6304 -0.0037 0.0000 0.0070 0.021 0.655 -0.001 15.492 0.074 -0.005 -0.033 0.17 95839. 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 0.0857 0.0276 0.277 5.816 5.270 206.443 0.657 23.442 11.579 0.26 138174. 0.7248 1.33 0.0218 0.0657 0.0842 0.0279 0.280 5.886 5.179 208.918 0.665 23.037 11.244 0.26 138256. 0.6977 2.66 0.0436 0.1275 0.0826 0.0282 0.283 5.950 5.082 211.189 0.672 22.603 10.914 0.26 138344. 0.6708 4.00 0.0654 0.1855 0.0809 0.0285 0.286 6.007 4.977 213.200 0.679 22.139 10.589 0.26 138439. 0.6441 5.33 0.0871 0.2399 0.0791 0.0287 0.288 6.055 4.866 214.900 0.684 21.643 10.270 0.26 138541. 0.6177 6.66 0.1089 0.2907 0.0772 0.0289 0.290 6.092 4.747 216.230 0.688 21.113 9.956 0.26 138649. 0.5915 7.99 0.1307 0.3381 0.0751 0.0290 0.291 6.118 4.620 217.134 0.691 20.548 9.650 0.26 138765. 0.5655 9.32 0.1525 0.3822 0.0729 0.0291 0.292 6.129 4.485 217.551 0.692 19.947 9.350 0.26 138889. 0.5399 10.66 0.1743 0.4231 0.0706 0.0291 0.292 6.126 4.341 217.424 0.692 19.310 9.056 0.26 139020. 0.5145 11.99 0.1961 0.4609 0.0681 0.0290 0.291 6.105 4.190 216.696 0.690 18.635 8.769 0.26 139160. 0.4894 13.32 0.2179 0.4957 0.0655 0.0288 0.289 6.066 4.030 215.318 0.685 17.924 8.489 0.26 139307. 0.4646 14.65 0.2397 0.5276 0.0628 0.0285 0.286 6.008 3.862 213.256 0.679 17.177 8.214 0.26 139462. 0.4401 15.98 0.2614 0.5567 0.0599 0.0281 0.282 5.930 3.687 210.484 0.670 16.398 7.944 0.26 139626. 0.4159 17.32 0.2832 0.5829 0.0570 0.0277 0.278 5.832 3.504 206.982 0.659 15.587 7.679 0.26 139799. 0.3920 18.65 0.3050 0.6064 0.0539 0.0271 0.272 5.712 3.316 202.734 0.645 14.748 7.418 0.26 139980. 0.3683 19.98 0.3268 0.6271 0.0507 0.0264 0.265 5.571 3.121 197.721 0.629 13.881 7.159 0.26 140170. 0.3448 21.31 0.3486 0.6448 0.0475 0.0257 0.257 5.407 2.920 191.926 0.611 12.990 6.902 0.26 140368. 0.3216 22.64 0.3704 0.6596 0.0441 0.0248 0.249 5.222 2.715 185.331 0.590 12.076 6.644 0.26 140576. 0.2985 23.98 0.3922 0.6711 0.0407 0.0238 0.239 5.013 2.505 177.922 0.566 11.140 6.385 0.26 140793. 0.2755 25.31 0.4140 0.6790 0.0372 0.0227 0.228 4.781 2.290 169.682 0.540 10.184 6.120 0.26 141019. 0.2525 26.64 0.4357 0.6830 0.0337 0.0215 0.215 4.525 2.071 160.601 0.511 9.211 5.848 0.26 141254. 0.2295 27.97 0.4575 0.6823 0.0300 0.0201 0.202 4.245 1.848 150.668 0.480 8.221 5.564 0.26 141498. 0.2062 29.30 0.4793 0.6758 0.0264 0.0187 0.188 3.941 1.622 139.878 0.445 7.216 5.261 0.26 141752. 0.1827 30.64 0.5011 0.6621 0.0227 0.0171 0.172 3.613 1.394 128.231 0.408 6.199 4.930 0.26 142015. 0.1587 31.97 0.5229 0.6387 0.0189 0.0155 0.155 3.261 1.163 115.734 0.368 5.172 4.557 0.26 142288. 0.1340 33.30 0.5447 0.6016 0.0151 0.0137 0.137 2.885 0.930 102.400 0.326 4.138 4.121 0.26 142570. 0.1084 34.63 0.5665 0.5437 0.0113 0.0118 0.118 2.486 0.697 88.253 0.281 3.100 3.581 0.26 142861. 0.0815 35.96 0.5883 0.4517 0.0075 0.0098 0.098 2.066 0.463 73.328 0.233 2.060 2.865 0.26 143162. 0.0532 37.29 0.6100 0.2959 0.0037 0.0077 0.077 1.625 0.230 57.664 0.184 1.024 1.810 0.26 143472. 0.0237 38.63 0.6318 -0.0091 -0.0001 0.0055 0.055 1.157 -0.005 41.056 0.131 -0.022 -0.053 0.26 143773. 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 0.0864 0.0271 0.645 10.165 9.445 481.072 1.148 42.013 8.905 0.34 184222. 0.7463 1.78 0.0218 0.0674 0.0849 0.0275 0.653 10.293 9.283 487.100 1.163 41.292 8.644 0.34 184332. 0.7181 3.56 0.0436 0.1308 0.0833 0.0278 0.661 10.410 9.109 492.635 1.176 40.518 8.387 0.34 184450. 0.6902 5.34 0.0655 0.1903 0.0816 0.0281 0.667 10.513 8.923 497.546 1.188 39.689 8.134 0.34 184577. 0.6625 7.11 0.0873 0.2460 0.0798 0.0283 0.673 10.601 8.723 501.703 1.198 38.802 7.887 0.34 184714. 0.6351 8.89 0.1091 0.2980 0.0778 0.0285 0.677 10.670 8.511 504.970 1.206 37.855 7.644 0.34 184859. 0.6081 10.67 0.1309 0.3465 0.0758 0.0286 0.680 10.718 8.283 507.207 1.211 36.845 7.407 0.34 185015. 0.5813 12.45 0.1527 0.3917 0.0735 0.0287 0.682 10.740 8.042 508.267 1.213 35.770 7.176 0.34 185180. 0.5549 14.23 0.1746 0.4336 0.0712 0.0287 0.681 10.735 7.785 508.013 1.213 34.628 6.951 0.34 185356. 0.5288 16.01 0.1964 0.4723 0.0687 0.0286 0.679 10.699 7.514 506.306 1.209 33.420 6.731 0.34 185543. 0.5031 17.79 0.2182 0.5081 0.0661 0.0284 0.675 10.629 7.227 503.029 1.201 32.145 6.516 0.34 185740. 0.4777 19.56 0.2400 0.5409 0.0633 0.0281 0.668 10.525 6.926 498.093 1.189 30.807 6.307 0.34 185949. 0.4526 21.34 0.2618 0.5710 0.0605 0.0277 0.659 10.384 6.612 491.440 1.173 29.409 6.102 0.34 186168. 0.4278 23.12 0.2836 0.5982 0.0575 0.0273 0.648 10.207 6.285 483.020 1.153 27.955 5.902 0.34 186399. 0.4034 24.90 0.3055 0.6227 0.0544 0.0267 0.634 9.990 5.946 472.790 1.129 26.449 5.705 0.34 186642. 0.3793 26.68 0.3273 0.6445 0.0512 0.0260 0.618 9.735 5.597 460.707 1.100 24.895 5.510 0.34 186896. 0.3554 28.46 0.3491 0.6634 0.0479 0.0252 0.599 9.440 5.237 446.728 1.066 23.296 5.318 0.34 187162. 0.3318 30.24 0.3709 0.6794 0.0445 0.0243 0.578 9.103 4.869 430.811 1.028 21.655 5.126 0.34 187440. 0.3084 32.01 0.3927 0.6924 0.0411 0.0233 0.554 8.725 4.491 412.918 0.986 19.976 4.933 0.34 187730. 0.2850 33.79 0.4146 0.7019 0.0375 0.0222 0.527 8.305 4.105 393.013 0.938 18.261 4.738 0.34 188032. 0.2618 35.57 0.4364 0.7077 0.0340 0.0209 0.498 7.841 3.713 371.064 0.886 16.513 4.538 0.34 188346. 0.2384 37.35 0.4582 0.7090 0.0303 0.0196 0.465 7.333 3.313 347.051 0.829 14.737 4.330 0.35 188673. 0.2149 39.13 0.4800 0.7049 0.0266 0.0181 0.430 6.782 2.908 320.961 0.766 12.934 4.109 0.35 189013. 0.1911 40.91 0.5018 0.6938 0.0228 0.0165 0.393 6.187 2.498 292.791 0.699 11.109 3.869 0.35 189365. 0.1667 42.69 0.5237 0.6734 0.0191 0.0148 0.352 5.548 2.083 262.559 0.627 9.266 3.599 0.35 189729. 0.1416 44.46 0.5455 0.6396 0.0152 0.0130 0.309 4.866 1.666 230.299 0.550 7.410 3.281 0.35 190107. 0.1155 46.24 0.5673 0.5848 0.0114 0.0111 0.263 4.143 1.247 196.070 0.468 5.546 2.884 0.35 190497. 0.0878 48.02 0.5891 0.4941 0.0076 0.0090 0.215 3.380 0.828 159.958 0.382 3.681 2.347 0.35 190899. 0.0582 49.80 0.6109 0.3323 0.0037 0.0069 0.164 2.579 0.410 122.057 0.291 1.822 1.522 0.35 191312. 0.0266 51.58 0.6328 -0.0181 -0.0001 0.0046 0.109 1.725 -0.014 81.618 0.195 -0.064 -0.080 0.35 191705. 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 0.0873 0.0270 1.255 15.818 14.912 935.753 1.787 66.330 7.228 0.43 230261. 0.7611 2.22 0.0218 0.0684 0.0858 0.0274 1.271 16.022 14.658 947.793 1.810 65.201 7.015 0.43 230399. 0.7323 4.45 0.0437 0.1327 0.0842 0.0277 1.286 16.209 14.386 958.847 1.831 63.987 6.805 0.43 230547. 0.7037 6.67 0.0655 0.1931 0.0825 0.0280 1.299 16.375 14.093 968.654 1.850 62.686 6.599 0.43 230707. 0.6755 8.90 0.0873 0.2496 0.0807 0.0282 1.310 16.515 13.780 976.957 1.866 61.293 6.398 0.43 230878. 0.6475 11.12 0.1092 0.3023 0.0787 0.0284 1.319 16.625 13.445 983.487 1.878 59.804 6.201 0.43 231061. 0.6200 13.35 0.1310 0.3516 0.0766 0.0285 1.325 16.701 13.088 987.958 1.887 58.216 6.009 0.43 231257. 0.5927 15.57 0.1528 0.3974 0.0744 0.0286 1.328 16.737 12.708 990.086 1.891 56.524 5.822 0.43 231465. 0.5659 17.80 0.1747 0.4400 0.0720 0.0286 1.327 16.729 12.304 989.592 1.890 54.727 5.639 0.43 231686. 0.5393 20.02 0.1965 0.4794 0.0695 0.0285 1.323 16.671 11.876 986.205 1.884 52.823 5.462 0.43 231920. 0.5132 22.24 0.2183 0.5158 0.0669 0.0283 1.314 16.561 11.424 979.687 1.871 50.814 5.289 0.43 232168. 0.4874 24.47 0.2401 0.5493 0.0641 0.0280 1.301 16.395 10.949 969.864 1.852 48.703 5.121 0.43 232429. 0.4620 26.69 0.2620 0.5800 0.0612 0.0276 1.283 16.171 10.453 956.613 1.827 46.497 4.956 0.43 232705. 0.4369 28.92 0.2838 0.6080 0.0582 0.0271 1.260 15.888 9.937 939.843 1.795 44.202 4.796 0.43 232994. 0.4122 31.14 0.3056 0.6333 0.0550 0.0266 1.233 15.543 9.403 919.465 1.756 41.825 4.638 0.43 233299. 0.3878 33.37 0.3275 0.6559 0.0518 0.0259 1.201 15.136 8.851 895.395 1.710 39.371 4.484 0.43 233617. 0.3637 35.59 0.3493 0.6757 0.0485 0.0251 1.163 14.665 8.284 867.548 1.657 36.845 4.331 0.43 233951. 0.3399 37.82 0.3711 0.6928 0.0451 0.0241 1.121 14.129 7.701 835.843 1.596 34.254 4.179 0.43 234299. 0.3162 40.04 0.3930 0.7069 0.0416 0.0231 1.073 13.527 7.105 800.201 1.528 31.601 4.027 0.43 234662. 0.2927 42.26 0.4148 0.7177 0.0380 0.0220 1.020 12.857 6.495 760.552 1.453 28.892 3.874 0.43 235041. 0.2692 44.49 0.4366 0.7250 0.0344 0.0207 0.961 12.118 5.875 716.835 1.369 26.130 3.717 0.43 235435. 0.2457 46.71 0.4585 0.7280 0.0307 0.0193 0.897 11.309 5.243 669.008 1.278 23.322 3.555 0.43 235845. 0.2219 48.94 0.4803 0.7259 0.0269 0.0178 0.827 10.431 4.603 617.042 1.178 20.473 3.383 0.43 236270. 0.1979 51.16 0.5021 0.7172 0.0231 0.0162 0.752 9.482 3.954 560.938 1.071 17.589 3.197 0.43 236711. 0.1734 53.39 0.5240 0.6995 0.0193 0.0145 0.671 8.464 3.299 500.725 0.956 14.675 2.989 0.43 237167. 0.1480 55.61 0.5458 0.6687 0.0154 0.0126 0.585 7.378 2.640 436.474 0.834 11.741 2.743 0.43 237639. 0.1215 57.84 0.5676 0.6174 0.0116 0.0106 0.494 6.226 1.977 368.304 0.703 8.794 2.435 0.43 238127. 0.0934 60.06 0.5894 0.5296 0.0077 0.0086 0.397 5.010 1.314 296.384 0.566 5.846 2.011 0.43 238631. 0.0629 62.28 0.6113 0.3661 0.0038 0.0064 0.296 3.734 0.653 220.908 0.422 2.905 1.341 0.43 239149. 0.0295 64.51 0.6331 -0.0179 -0.0001 0.0040 0.188 2.368 -0.020 140.105 0.268 -0.087 -0.063 0.44 239632. 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 0.0884 0.0272 2.180 22.903 21.755 1625.798 2.588 96.767 6.069 0.51 276286. 0.7719 2.69 0.0220 0.0693 0.0869 0.0275 2.209 23.204 21.386 1647.188 2.622 95.127 5.889 0.51 276454. 0.7426 5.37 0.0439 0.1345 0.0853 0.0279 2.235 23.480 20.989 1666.797 2.653 93.361 5.712 0.51 276635. 0.7135 8.06 0.0659 0.1956 0.0836 0.0282 2.258 23.725 20.563 1684.158 2.680 91.465 5.538 0.51 276829. 0.6847 10.74 0.0879 0.2528 0.0817 0.0284 2.278 23.931 20.106 1698.808 2.704 89.433 5.368 0.51 277037. 0.6563 13.43 0.1098 0.3063 0.0797 0.0286 2.293 24.093 19.617 1710.257 2.722 87.257 5.203 0.51 277260. 0.6283 16.12 0.1318 0.3562 0.0776 0.0287 2.304 24.202 19.095 1717.999 2.734 84.933 5.041 0.51 277498. 0.6006 18.80 0.1538 0.4026 0.0753 0.0288 2.309 24.251 18.538 1721.526 2.740 82.455 4.884 0.51 277751. 0.5734 21.49 0.1757 0.4457 0.0729 0.0288 2.307 24.234 17.945 1720.330 2.738 79.821 4.731 0.51 278020. 0.5465 24.17 0.1977 0.4857 0.0704 0.0287 2.298 24.144 17.317 1713.937 2.728 77.027 4.583 0.51 278305. 0.5200 26.86 0.2197 0.5226 0.0677 0.0285 2.282 23.975 16.654 1701.918 2.709 74.076 4.438 0.51 278606. 0.4939 29.54 0.2416 0.5567 0.0649 0.0282 2.258 23.722 15.956 1683.966 2.680 70.974 4.298 0.51 278924. 0.4681 32.23 0.2636 0.5879 0.0619 0.0277 2.226 23.383 15.227 1659.872 2.642 67.731 4.161 0.51 279259. 0.4427 34.92 0.2856 0.6165 0.0588 0.0272 2.185 22.954 14.469 1629.470 2.593 64.356 4.027 0.51 279612. 0.4177 37.60 0.3075 0.6424 0.0556 0.0266 2.136 22.435 13.682 1592.611 2.535 60.860 3.897 0.51 279982. 0.3930 40.29 0.3295 0.6656 0.0523 0.0259 2.077 21.823 12.871 1549.149 2.466 57.249 3.768 0.51 280369. 0.3686 42.97 0.3515 0.6861 0.0489 0.0251 2.010 21.116 12.035 1498.934 2.386 53.534 3.642 0.52 280774. 0.3445 45.66 0.3734 0.7039 0.0454 0.0241 1.934 20.311 11.178 1441.823 2.295 49.720 3.516 0.52 281198. 0.3206 48.35 0.3954 0.7187 0.0419 0.0230 1.847 19.407 10.300 1377.677 2.193 45.815 3.391 0.52 281639. 0.2967 51.03 0.4174 0.7304 0.0382 0.0218 1.752 18.403 9.404 1306.375 2.079 41.827 3.265 0.52 282100. 0.2730 53.72 0.4393 0.7386 0.0345 0.0205 1.647 17.296 8.490 1227.810 1.954 37.762 3.136 0.52 282578. 0.2492 56.40 0.4613 0.7426 0.0307 0.0191 1.531 16.086 7.560 1141.908 1.817 33.629 3.003 0.52 283076. 0.2251 59.09 0.4833 0.7415 0.0269 0.0175 1.406 14.772 6.617 1048.625 1.669 29.434 2.862 0.52 283592. 0.2008 61.78 0.5052 0.7338 0.0230 0.0158 1.271 13.354 5.663 947.968 1.509 25.188 2.709 0.52 284128. 0.1758 64.46 0.5272 0.7170 0.0191 0.0140 1.126 11.833 4.699 839.998 1.337 20.900 2.537 0.52 284682. 0.1500 67.15 0.5492 0.6867 0.0152 0.0121 0.972 10.211 3.728 724.854 1.154 16.581 2.333 0.52 285256. 0.1228 69.83 0.5711 0.6343 0.0112 0.0101 0.808 8.491 2.753 602.760 0.959 12.246 2.072 0.52 285848. 0.0937 72.52 0.5931 0.5409 0.0072 0.0079 0.636 6.678 1.778 474.040 0.754 7.910 1.701 0.52 286460. 0.0619 75.20 0.6151 0.3556 0.0033 0.0057 0.455 4.776 0.806 339.015 0.540 3.586 1.079 0.52 287087. 0.0264 77.89 0.6370 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 0.0899 0.0276 3.510 31.607 30.091 2617.635 3.571 133.846 5.214 0.60 322294. 0.7799 3.12 0.0219 0.0692 0.0884 0.0279 3.557 32.025 29.591 2652.270 3.618 131.622 5.060 0.60 322490. 0.7506 6.23 0.0437 0.1342 0.0868 0.0283 3.599 32.408 29.052 2683.998 3.661 129.224 4.910 0.60 322701. 0.7215 9.35 0.0656 0.1952 0.0850 0.0286 3.637 32.747 28.473 2712.068 3.700 126.647 4.762 0.60 322928. 0.6928 12.47 0.0874 0.2524 0.0832 0.0288 3.669 33.033 27.851 2735.739 3.732 123.881 4.618 0.60 323172. 0.6644 15.59 0.1093 0.3059 0.0812 0.0290 3.693 33.256 27.185 2754.222 3.757 120.917 4.477 0.60 323432. 0.6364 18.70 0.1311 0.3558 0.0790 0.0291 3.710 33.407 26.472 2766.711 3.774 117.747 4.340 0.60 323709. 0.6088 21.82 0.1530 0.4024 0.0768 0.0292 3.718 33.476 25.712 2772.392 3.782 114.365 4.206 0.60 324004. 0.5816 24.94 0.1748 0.4457 0.0744 0.0292 3.715 33.452 24.903 2770.465 3.779 110.766 4.077 0.60 324317. 0.5547 28.05 0.1967 0.4860 0.0718 0.0291 3.701 33.328 24.044 2760.160 3.765 106.947 3.951 0.60 324649. 0.5283 31.17 0.2185 0.5232 0.0691 0.0289 3.675 33.094 23.136 2740.794 3.739 102.910 3.829 0.60 325000. 0.5022 34.29 0.2404 0.5577 0.0662 0.0285 3.637 32.745 22.181 2711.864 3.699 98.663 3.710 0.60 325370. 0.4764 37.41 0.2622 0.5894 0.0633 0.0281 3.585 32.276 21.182 2673.030 3.647 94.219 3.594 0.60 325760. 0.4511 40.52 0.2841 0.6185 0.0601 0.0276 3.519 31.684 20.142 2624.041 3.580 89.592 3.482 0.60 326169. 0.4260 43.64 0.3059 0.6450 0.0569 0.0270 3.439 30.967 19.064 2564.663 3.499 84.795 3.371 0.60 326599. 0.4014 46.76 0.3278 0.6690 0.0536 0.0263 3.345 30.122 17.950 2494.680 3.403 79.840 3.264 0.60 327049. 0.3770 49.88 0.3496 0.6903 0.0502 0.0254 3.237 29.147 16.803 2413.862 3.293 74.738 3.157 0.60 327519. 0.3529 52.99 0.3715 0.7091 0.0467 0.0244 3.114 28.037 15.625 2321.990 3.168 69.499 3.052 0.60 328010. 0.3290 56.11 0.3933 0.7250 0.0431 0.0234 2.976 26.792 14.419 2218.843 3.027 64.134 2.947 0.60 328522. 0.3052 59.23 0.4152 0.7380 0.0394 0.0222 2.822 25.408 13.186 2104.225 2.871 58.652 2.842 0.60 329055. 0.2814 62.34 0.4370 0.7477 0.0356 0.0208 2.652 23.883 11.929 1977.969 2.698 53.062 2.736 0.60 329610. 0.2576 65.46 0.4589 0.7535 0.0318 0.0194 2.467 22.217 10.651 1839.948 2.510 47.376 2.626 0.60 330186. 0.2336 68.58 0.4808 0.7547 0.0279 0.0178 2.266 20.407 9.353 1690.091 2.306 41.603 2.510 0.60 330784. 0.2093 71.70 0.5026 0.7498 0.0240 0.0161 2.050 18.455 8.039 1528.395 2.085 35.755 2.386 0.61 331404. 0.1844 74.81 0.5245 0.7367 0.0200 0.0143 1.817 16.360 6.710 1354.947 1.848 29.847 2.246 0.61 332045. 0.1587 77.93 0.5463 0.7115 0.0160 0.0123 1.569 14.127 5.372 1169.949 1.596 23.894 2.083 0.61 332708. 0.1316 81.05 0.5682 0.6665 0.0120 0.0103 1.306 11.758 4.027 973.742 1.328 17.913 1.876 0.61 333394. 0.1026 84.16 0.5900 0.5852 0.0080 0.0081 1.028 9.259 2.681 766.822 1.046 11.926 1.586 0.61 334100. 0.0708 87.28 0.6119 0.4225 0.0040 0.0058 0.737 6.638 1.338 549.750 0.750 5.953 1.104 0.61 334827. 0.0348 90.40 0.6337 -0.0220 -0.0001 0.0033 0.423 3.811 -0.039 315.588 0.431 -0.172 -0.056 0.61 335478. 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 0.0916 0.0282 5.359 42.220 40.086 3996.115 4.770 178.303 4.550 0.68 368277. 0.7855 3.57 0.0219 0.0691 0.0902 0.0286 5.430 42.783 39.432 4049.383 4.834 175.393 4.417 0.68 368504. 0.7562 7.13 0.0438 0.1340 0.0885 0.0289 5.496 43.298 38.725 4098.084 4.892 172.250 4.286 0.68 368748. 0.7272 10.70 0.0656 0.1951 0.0868 0.0292 5.553 43.751 37.964 4141.051 4.943 168.863 4.158 0.68 369010. 0.6986 14.27 0.0875 0.2523 0.0849 0.0295 5.602 44.132 37.145 4177.114 4.986 165.220 4.033 0.68 369291. 0.6703 17.83 0.1094 0.3058 0.0829 0.0297 5.639 44.428 36.266 4205.068 5.019 161.309 3.912 0.68 369592. 0.6423 21.40 0.1313 0.3559 0.0808 0.0298 5.664 44.624 35.323 4223.665 5.042 157.119 3.793 0.68 369912. 0.6147 24.97 0.1532 0.4026 0.0785 0.0298 5.675 44.709 34.317 4231.663 5.051 152.641 3.678 0.68 370253. 0.5875 28.54 0.1750 0.4462 0.0760 0.0298 5.670 44.668 33.244 4227.830 5.047 147.868 3.566 0.68 370614. 0.5607 32.10 0.1969 0.4867 0.0734 0.0297 5.647 44.490 32.104 4210.995 5.027 142.797 3.458 0.68 370997. 0.5342 35.67 0.2188 0.5243 0.0706 0.0295 5.606 44.164 30.897 4180.116 4.990 137.429 3.353 0.68 371402. 0.5081 39.24 0.2407 0.5591 0.0677 0.0292 5.544 43.681 29.626 4134.417 4.935 131.777 3.250 0.68 371828. 0.4824 42.80 0.2626 0.5912 0.0647 0.0287 5.463 43.037 28.295 4073.396 4.862 125.857 3.151 0.69 372277. 0.4570 46.37 0.2844 0.6208 0.0615 0.0282 5.360 42.226 26.908 3996.686 4.771 119.688 3.054 0.69 372749. 0.4319 49.94 0.3063 0.6478 0.0582 0.0275 5.235 41.247 25.470 3903.960 4.660 113.289 2.959 0.69 373243. 0.4072 53.50 0.3282 0.6724 0.0548 0.0268 5.089 40.094 23.983 3794.904 4.530 106.676 2.866 0.69 373761. 0.3828 57.07 0.3501 0.6944 0.0513 0.0259 4.920 38.766 22.451 3669.194 4.380 99.864 2.775 0.69 374302. 0.3586 60.64 0.3720 0.7139 0.0477 0.0249 4.729 37.259 20.878 3526.510 4.209 92.867 2.685 0.69 374866. 0.3346 64.21 0.3938 0.7307 0.0440 0.0237 4.515 35.568 19.267 3366.525 4.018 85.699 2.596 0.69 375455. 0.3107 67.77 0.4157 0.7446 0.0403 0.0225 4.276 33.692 17.620 3188.946 3.807 78.372 2.506 0.69 376068. 0.2868 71.34 0.4376 0.7553 0.0364 0.0211 4.014 31.627 15.939 2993.515 3.573 70.899 2.415 0.69 376705. 0.2629 74.91 0.4595 0.7624 0.0325 0.0196 3.728 29.372 14.230 2780.042 3.318 63.293 2.322 0.69 377366. 0.2388 78.47 0.4814 0.7650 0.0286 0.0180 3.417 26.925 12.493 2548.427 3.042 55.570 2.224 0.69 378052. 0.2143 82.04 0.5032 0.7618 0.0245 0.0162 3.083 24.286 10.734 2298.669 2.744 47.744 2.118 0.69 378763. 0.1892 85.61 0.5251 0.7506 0.0205 0.0143 2.723 21.457 8.956 2030.908 2.424 39.835 2.000 0.69 379499. 0.1632 89.17 0.5470 0.7277 0.0164 0.0123 2.341 18.441 7.163 1745.457 2.083 31.862 1.861 0.69 380260. 0.1358 92.74 0.5689 0.6853 0.0123 0.0102 1.935 15.244 5.362 1442.868 1.722 23.851 1.686 0.69 381046. 0.1064 96.31 0.5908 0.6063 0.0081 0.0079 1.507 11.875 3.559 1123.966 1.342 15.828 1.436 0.69 381856. 0.0739 99.88 0.6126 0.4423 0.0040 0.0056 1.059 8.343 1.759 789.703 0.943 7.823 1.010 0.70 382688. 0.0365 103.44 0.6345 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 0.0939 0.0295 7.977 55.865 51.970 5948.592 6.312 231.164 3.963 0.77 414225. 0.7789 4.04 0.0220 0.0683 0.0924 0.0298 8.067 56.493 51.141 6015.456 6.383 227.473 3.856 0.77 414485. 0.7519 8.08 0.0440 0.1328 0.0908 0.0301 8.149 57.067 50.241 6076.492 6.447 223.470 3.750 0.77 414765. 0.7248 12.12 0.0661 0.1937 0.0890 0.0304 8.220 57.569 49.268 6130.022 6.504 219.142 3.645 0.77 415066. 0.6977 16.16 0.0881 0.2509 0.0871 0.0306 8.280 57.985 48.217 6174.278 6.551 214.470 3.542 0.77 415389. 0.6706 20.20 0.1101 0.3046 0.0851 0.0307 8.324 58.296 47.086 6207.439 6.586 209.438 3.441 0.77 415733. 0.6437 24.24 0.1321 0.3549 0.0829 0.0308 8.351 58.485 45.870 6227.548 6.608 204.030 3.341 0.77 416101. 0.6169 28.27 0.1542 0.4020 0.0805 0.0309 8.358 58.533 44.567 6232.672 6.613 198.233 3.243 0.77 416492. 0.5904 32.31 0.1762 0.4459 0.0780 0.0308 8.342 58.423 43.175 6220.884 6.601 192.040 3.148 0.77 416907. 0.5640 36.35 0.1982 0.4868 0.0753 0.0307 8.301 58.136 41.692 6190.328 6.568 185.447 3.055 0.77 417346. 0.5378 40.39 0.2202 0.5249 0.0725 0.0304 8.233 57.657 40.120 6139.320 6.514 178.454 2.964 0.77 417810. 0.5119 44.43 0.2423 0.5601 0.0695 0.0300 8.135 56.973 38.462 6066.562 6.437 171.079 2.876 0.77 418299. 0.4863 48.47 0.2643 0.5927 0.0663 0.0296 8.007 56.077 36.723 5971.151 6.336 163.344 2.789 0.77 418813. 0.4609 52.51 0.2863 0.6228 0.0631 0.0290 7.848 54.963 34.909 5852.473 6.210 155.276 2.705 0.77 419353. 0.4359 56.55 0.3083 0.6504 0.0597 0.0283 7.657 53.625 33.026 5709.983 6.058 146.901 2.623 0.77 419919. 0.4111 60.59 0.3303 0.6755 0.0561 0.0275 7.434 52.058 31.079 5543.184 5.882 138.240 2.543 0.77 420511. 0.3866 64.63 0.3524 0.6981 0.0525 0.0265 7.177 50.259 29.072 5351.618 5.678 129.314 2.464 0.77 421130. 0.3623 68.67 0.3744 0.7182 0.0488 0.0254 6.886 48.224 27.011 5134.921 5.448 120.143 2.386 0.77 421776. 0.3381 72.71 0.3964 0.7357 0.0450 0.0242 6.561 45.949 24.897 4892.706 5.191 110.744 2.308 0.77 422448. 0.3140 76.74 0.4184 0.7502 0.0411 0.0229 6.202 43.432 22.737 4624.660 4.907 101.133 2.230 0.78 423148. 0.2899 80.78 0.4405 0.7616 0.0371 0.0215 5.807 40.670 20.532 4330.587 4.595 91.327 2.150 0.78 423876. 0.2657 84.82 0.4625 0.7691 0.0330 0.0199 5.378 37.663 18.288 4010.417 4.255 81.344 2.068 0.78 424631. 0.2412 88.86 0.4845 0.7719 0.0289 0.0182 4.914 34.413 16.008 3664.322 3.888 71.201 1.981 0.78 425414. 0.2162 92.90 0.5065 0.7684 0.0247 0.0163 4.416 30.923 13.696 3292.752 3.494 60.921 1.887 0.78 426225. 0.1904 96.94 0.5286 0.7560 0.0205 0.0143 3.884 27.202 11.359 2896.469 3.073 50.527 1.779 0.78 427064. 0.1635 100.98 0.5506 0.7299 0.0163 0.0123 3.321 23.259 9.003 2476.611 2.628 40.046 1.649 0.78 427931. 0.1349 105.02 0.5726 0.6809 0.0120 0.0101 2.729 19.110 6.635 2034.799 2.159 29.510 1.479 0.78 428827. 0.1039 109.06 0.5946 0.5875 0.0077 0.0078 2.110 14.774 4.262 1573.157 1.669 18.958 1.229 0.78 429750. 0.0692 113.10 0.6166 0.3892 0.0034 0.0054 1.467 10.273 1.893 1093.867 1.161 8.421 0.785 0.78 430697. 0.0295 117.14 0.6387 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 0.0965 0.0341 12.658 79.783 65.981 9439.240 9.014 293.482 3.170 0.85 460125. 0.7022 4.48 0.0220 0.0612 0.0951 0.0342 12.689 79.977 64.979 9462.198 9.036 289.025 3.115 0.85 460417. 0.6846 8.96 0.0440 0.1201 0.0935 0.0342 12.708 80.095 63.885 9476.156 9.049 284.162 3.058 0.85 460731. 0.6664 13.44 0.0659 0.1767 0.0917 0.0342 12.712 80.123 62.697 9479.528 9.052 278.877 3.000 0.85 461069. 0.6477 17.91 0.0879 0.2310 0.0899 0.0342 12.700 80.048 61.408 9470.635 9.044 273.144 2.941 0.85 461432. 0.6284 22.39 0.1099 0.2829 0.0878 0.0341 12.670 79.854 60.014 9447.662 9.022 266.943 2.881 0.85 461819. 0.6086 26.87 0.1319 0.3323 0.0856 0.0340 12.617 79.524 58.510 9408.597 8.985 260.253 2.821 0.85 462232. 0.5883 31.35 0.1538 0.3793 0.0832 0.0338 12.540 79.040 56.893 9351.341 8.930 253.058 2.759 0.85 462670. 0.5675 35.83 0.1758 0.4238 0.0807 0.0335 12.436 78.384 55.159 9273.723 8.856 245.346 2.698 0.85 463136. 0.5463 40.31 0.1978 0.4658 0.0780 0.0331 12.302 77.537 53.307 9173.507 8.760 237.109 2.636 0.86 463628. 0.5247 44.79 0.2198 0.5053 0.0751 0.0327 12.134 76.480 51.337 9048.490 8.641 228.348 2.573 0.86 464148. 0.5027 49.27 0.2418 0.5423 0.0721 0.0321 11.931 75.199 49.254 8896.964 8.496 219.080 2.511 0.86 464696. 0.4805 53.74 0.2637 0.5769 0.0689 0.0315 11.691 73.686 47.063 8717.876 8.325 209.335 2.449 0.86 465271. 0.4580 58.22 0.2857 0.6091 0.0655 0.0307 11.413 71.933 44.773 8510.520 8.127 199.150 2.386 0.86 465875. 0.4354 62.70 0.3077 0.6388 0.0620 0.0299 11.096 69.935 42.392 8274.155 7.901 188.558 2.324 0.86 466508. 0.4125 67.18 0.3297 0.6660 0.0584 0.0289 10.739 67.685 39.926 8007.984 7.647 177.591 2.261 0.86 467169. 0.3896 71.66 0.3516 0.6905 0.0547 0.0279 10.345 65.201 37.382 7714.076 7.366 166.273 2.198 0.86 467859. 0.3664 76.14 0.3736 0.7118 0.0509 0.0267 9.916 62.497 34.764 7394.188 7.061 154.630 2.132 0.86 468579. 0.3428 80.62 0.3956 0.7294 0.0469 0.0255 9.454 59.587 32.078 7049.835 6.732 142.682 2.064 0.86 469329. 0.3187 85.10 0.4176 0.7428 0.0429 0.0241 8.960 56.471 29.328 6681.223 6.380 130.452 1.991 0.86 470108. 0.2940 89.57 0.4396 0.7519 0.0388 0.0227 8.425 53.104 26.521 6282.796 6.000 117.965 1.915 0.86 470917. 0.2688 94.05 0.4615 0.7558 0.0346 0.0211 7.852 49.487 23.661 5854.951 5.591 105.244 1.833 0.86 471757. 0.2431 98.53 0.4835 0.7532 0.0304 0.0195 7.240 45.630 20.753 5398.512 5.155 92.310 1.744 0.86 472627. 0.2166 103.01 0.5055 0.7419 0.0260 0.0177 6.591 41.544 17.803 4915.160 4.694 79.189 1.643 0.86 473528. 0.1890 107.49 0.5275 0.7186 0.0217 0.0159 5.910 37.252 14.817 4407.409 4.209 65.908 1.525 0.87 474459. 0.1600 111.97 0.5494 0.6775 0.0173 0.0140 5.202 32.786 11.803 3878.950 3.704 52.501 1.380 0.87 475422. 0.1293 116.45 0.5714 0.6092 0.0128 0.0120 4.470 28.174 8.770 3333.268 3.183 39.010 1.193 0.87 476415. 0.0964 120.93 0.5934 0.4964 0.0084 0.0100 3.721 23.454 5.729 2774.897 2.650 25.482 0.936 0.87 477438. 0.0611 125.40 0.6154 0.3037 0.0039 0.0080 2.961 18.664 2.690 2208.168 2.109 11.964 0.553 0.87 478489. 0.0247 129.88 0.6374