20x10PN (20x10PN.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 0.0897 0.0352 0.009 0.571 0.457 6.754 0.064 2.035 30.719 0.08 43830. 0.6096 0.43 0.0229 0.0569 0.0882 0.0355 0.009 0.577 0.450 6.821 0.065 2.001 29.917 0.08 43858. 0.5887 0.87 0.0458 0.1107 0.0866 0.0358 0.009 0.582 0.442 6.883 0.066 1.965 29.115 0.08 43887. 0.5678 1.30 0.0687 0.1615 0.0849 0.0361 0.009 0.586 0.433 6.938 0.066 1.927 28.316 0.08 43920. 0.5467 1.73 0.0916 0.2093 0.0831 0.0364 0.009 0.590 0.424 6.984 0.067 1.885 27.523 0.08 43954. 0.5257 2.17 0.1145 0.2542 0.0812 0.0366 0.009 0.593 0.414 7.021 0.067 1.841 26.736 0.08 43991. 0.5046 2.60 0.1374 0.2961 0.0791 0.0367 0.009 0.595 0.403 7.045 0.067 1.793 25.955 0.08 44031. 0.4835 3.04 0.1603 0.3351 0.0768 0.0367 0.009 0.596 0.392 7.057 0.067 1.743 25.181 0.08 44073. 0.4624 3.47 0.1832 0.3713 0.0745 0.0367 0.009 0.596 0.380 7.053 0.067 1.689 24.414 0.08 44119. 0.4413 3.90 0.2061 0.4047 0.0719 0.0366 0.009 0.594 0.367 7.032 0.067 1.631 23.654 0.08 44167. 0.4203 4.34 0.2290 0.4354 0.0692 0.0364 0.009 0.591 0.353 6.993 0.067 1.570 22.900 0.08 44217. 0.3992 4.77 0.2519 0.4633 0.0664 0.0361 0.009 0.586 0.339 6.934 0.066 1.506 22.151 0.08 44271. 0.3782 5.20 0.2748 0.4884 0.0634 0.0357 0.009 0.579 0.324 6.855 0.065 1.439 21.405 0.08 44328. 0.3572 5.64 0.2977 0.5106 0.0603 0.0352 0.009 0.571 0.308 6.755 0.065 1.369 20.661 0.08 44388. 0.3362 6.07 0.3206 0.5301 0.0571 0.0346 0.009 0.561 0.291 6.635 0.063 1.296 19.914 0.08 44450. 0.3153 6.51 0.3435 0.5465 0.0538 0.0338 0.009 0.549 0.274 6.494 0.062 1.220 19.163 0.08 44516. 0.2945 6.94 0.3664 0.5598 0.0504 0.0330 0.008 0.535 0.257 6.331 0.060 1.143 18.403 0.08 44585. 0.2736 7.37 0.3893 0.5698 0.0468 0.0320 0.008 0.519 0.239 6.146 0.059 1.063 17.629 0.08 44658. 0.2528 7.81 0.4122 0.5761 0.0432 0.0309 0.008 0.502 0.220 5.940 0.057 0.981 16.835 0.08 44733. 0.2319 8.24 0.4351 0.5785 0.0395 0.0297 0.008 0.483 0.202 5.711 0.055 0.897 16.013 0.08 44811. 0.2110 8.67 0.4580 0.5762 0.0358 0.0284 0.007 0.461 0.182 5.460 0.052 0.811 15.154 0.08 44893. 0.1899 9.11 0.4809 0.5687 0.0319 0.0270 0.007 0.438 0.163 5.186 0.050 0.724 14.244 0.08 44978. 0.1686 9.54 0.5038 0.5548 0.0280 0.0255 0.007 0.413 0.143 4.889 0.047 0.636 13.265 0.08 45066. 0.1472 9.97 0.5267 0.5332 0.0241 0.0238 0.006 0.386 0.123 4.570 0.044 0.547 12.195 0.08 45158. 0.1254 10.41 0.5496 0.5019 0.0201 0.0220 0.006 0.357 0.103 4.229 0.040 0.456 10.999 0.08 45253. 0.1033 10.84 0.5725 0.4576 0.0161 0.0201 0.005 0.327 0.082 3.866 0.037 0.365 9.628 0.08 45351. 0.0809 11.28 0.5953 0.3959 0.0121 0.0181 0.005 0.294 0.061 3.481 0.033 0.273 8.009 0.08 45452. 0.0583 11.71 0.6182 0.3093 0.0080 0.0160 0.004 0.260 0.041 3.076 0.029 0.182 6.024 0.08 45557. 0.0357 12.14 0.6411 0.1848 0.0040 0.0138 0.004 0.224 0.020 2.652 0.025 0.090 3.472 0.08 45664. 0.0145 12.58 0.6640 -0.0023 0.0000 0.0115 0.003 0.187 0.000 2.209 0.021 -0.001 -0.042 0.08 45772. 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 0.0902 0.0318 0.065 2.063 1.839 48.814 0.233 8.180 17.087 0.16 87659. 0.6798 0.87 0.0230 0.0634 0.0887 0.0322 0.066 2.088 1.809 49.407 0.236 8.046 16.606 0.16 87714. 0.6553 1.74 0.0460 0.1232 0.0871 0.0325 0.067 2.111 1.777 49.958 0.239 7.902 16.129 0.16 87774. 0.6307 2.61 0.0690 0.1794 0.0854 0.0328 0.068 2.132 1.742 50.453 0.241 7.747 15.658 0.16 87839. 0.6063 3.48 0.0920 0.2321 0.0836 0.0331 0.068 2.150 1.704 50.880 0.243 7.581 15.193 0.16 87908. 0.5819 4.36 0.1150 0.2814 0.0816 0.0333 0.069 2.165 1.664 51.227 0.245 7.403 14.736 0.16 87983. 0.5577 5.23 0.1380 0.3274 0.0795 0.0335 0.069 2.176 1.621 51.480 0.246 7.212 14.286 0.16 88063. 0.5337 6.10 0.1610 0.3701 0.0773 0.0336 0.069 2.182 1.576 51.622 0.246 7.009 13.845 0.16 88148. 0.5099 6.97 0.1840 0.4098 0.0749 0.0336 0.069 2.182 1.527 51.640 0.247 6.792 13.411 0.16 88239. 0.4862 7.84 0.2070 0.4464 0.0723 0.0335 0.069 2.177 1.475 51.518 0.246 6.561 12.986 0.16 88336. 0.4627 8.71 0.2300 0.4800 0.0696 0.0334 0.069 2.166 1.420 51.244 0.245 6.316 12.568 0.16 88439. 0.4394 9.58 0.2530 0.5108 0.0668 0.0331 0.068 2.147 1.362 50.808 0.243 6.057 12.157 0.16 88547. 0.4162 10.45 0.2760 0.5387 0.0638 0.0327 0.067 2.122 1.301 50.203 0.240 5.786 11.753 0.16 88661. 0.3933 11.33 0.2990 0.5637 0.0607 0.0322 0.066 2.089 1.237 49.426 0.236 5.503 11.354 0.16 88782. 0.3705 12.20 0.3220 0.5860 0.0574 0.0316 0.065 2.049 1.171 48.474 0.231 5.210 10.959 0.16 88908. 0.3480 13.07 0.3450 0.6053 0.0541 0.0308 0.063 2.001 1.103 47.343 0.226 4.906 10.566 0.16 89041. 0.3256 13.94 0.3680 0.6217 0.0506 0.0300 0.062 1.945 1.032 46.031 0.220 4.592 10.173 0.16 89180. 0.3033 14.81 0.3910 0.6349 0.0471 0.0290 0.060 1.882 0.960 44.534 0.213 4.270 9.778 0.16 89326. 0.2811 15.68 0.4140 0.6447 0.0434 0.0279 0.057 1.811 0.886 42.850 0.205 3.941 9.378 0.16 89478. 0.2590 16.55 0.4370 0.6508 0.0397 0.0267 0.055 1.732 0.810 40.976 0.196 3.604 8.968 0.16 89636. 0.2368 17.42 0.4600 0.6526 0.0359 0.0253 0.052 1.644 0.733 38.910 0.186 3.260 8.543 0.16 89801. 0.2146 18.30 0.4830 0.6494 0.0321 0.0239 0.049 1.549 0.654 36.650 0.175 2.910 8.097 0.16 89972. 0.1921 19.17 0.5060 0.6402 0.0282 0.0223 0.046 1.445 0.574 34.196 0.163 2.555 7.620 0.16 90150. 0.1694 20.04 0.5290 0.6235 0.0242 0.0205 0.042 1.333 0.494 31.547 0.151 2.196 7.098 0.16 90335. 0.1463 20.91 0.5520 0.5968 0.0202 0.0187 0.038 1.213 0.412 28.707 0.137 1.833 6.510 0.16 90526. 0.1226 21.78 0.5750 0.5563 0.0162 0.0167 0.034 1.085 0.330 25.679 0.123 1.467 5.827 0.16 90724. 0.0982 22.65 0.5980 0.4958 0.0121 0.0146 0.030 0.950 0.247 22.469 0.107 1.100 4.993 0.16 90928. 0.0729 23.52 0.6210 0.4039 0.0081 0.0124 0.026 0.807 0.165 19.086 0.091 0.733 3.917 0.16 91139. 0.0467 24.39 0.6440 0.2578 0.0040 0.0101 0.021 0.657 0.083 15.541 0.074 0.367 2.410 0.16 91356. 0.0203 25.26 0.6670 0.0016 0.0000 0.0077 0.016 0.499 0.000 11.818 0.056 0.002 0.014 0.16 91569. 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 0.0907 0.0305 0.212 4.454 4.160 158.102 0.503 18.504 11.935 0.24 131484. 0.7142 1.31 0.0231 0.0666 0.0892 0.0309 0.215 4.513 4.092 160.193 0.510 18.203 11.587 0.24 131567. 0.6877 2.62 0.0461 0.1292 0.0876 0.0313 0.217 4.568 4.019 162.138 0.516 17.878 11.244 0.24 131658. 0.6613 3.93 0.0692 0.1879 0.0859 0.0316 0.220 4.618 3.941 163.896 0.522 17.529 10.906 0.24 131755. 0.6352 5.24 0.0922 0.2429 0.0840 0.0319 0.222 4.661 3.857 165.424 0.527 17.154 10.574 0.24 131860. 0.6092 6.55 0.1153 0.2943 0.0821 0.0321 0.224 4.696 3.766 166.675 0.531 16.752 10.249 0.24 131973. 0.5835 7.86 0.1383 0.3422 0.0800 0.0323 0.225 4.722 3.669 167.602 0.533 16.321 9.930 0.24 132093. 0.5581 9.17 0.1614 0.3867 0.0777 0.0324 0.225 4.738 3.566 168.153 0.535 15.861 9.619 0.24 132222. 0.5329 10.48 0.1845 0.4280 0.0753 0.0325 0.226 4.741 3.455 168.275 0.536 15.370 9.314 0.24 132359. 0.5079 11.79 0.2075 0.4661 0.0727 0.0324 0.225 4.731 3.338 167.918 0.534 14.847 9.016 0.24 132505. 0.4833 13.10 0.2306 0.5012 0.0700 0.0322 0.224 4.706 3.213 167.035 0.532 14.293 8.726 0.24 132660. 0.4589 14.41 0.2536 0.5333 0.0672 0.0319 0.222 4.665 3.082 165.592 0.527 13.708 8.441 0.24 132823. 0.4347 15.72 0.2767 0.5626 0.0641 0.0315 0.219 4.608 2.944 163.568 0.521 13.093 8.163 0.24 132996. 0.4109 17.03 0.2998 0.5891 0.0610 0.0310 0.216 4.535 2.800 160.947 0.512 12.452 7.889 0.24 133177. 0.3873 18.34 0.3228 0.6128 0.0577 0.0304 0.212 4.444 2.650 157.717 0.502 11.786 7.621 0.24 133368. 0.3639 19.65 0.3459 0.6336 0.0544 0.0297 0.206 4.335 2.495 153.867 0.490 11.098 7.355 0.24 133568. 0.3408 20.96 0.3689 0.6516 0.0509 0.0288 0.200 4.209 2.335 149.386 0.476 10.388 7.091 0.24 133778. 0.3179 22.27 0.3920 0.6666 0.0473 0.0278 0.193 4.064 2.171 144.262 0.459 9.658 6.827 0.24 133997. 0.2951 23.58 0.4150 0.6783 0.0437 0.0267 0.186 3.902 2.003 138.487 0.441 8.911 6.561 0.24 134226. 0.2725 24.89 0.4381 0.6865 0.0399 0.0255 0.177 3.720 1.832 132.049 0.420 8.147 6.291 0.24 134465. 0.2498 26.20 0.4612 0.6908 0.0361 0.0241 0.168 3.520 1.657 124.941 0.398 7.368 6.014 0.24 134714. 0.2271 27.51 0.4842 0.6904 0.0322 0.0226 0.157 3.301 1.478 117.158 0.373 6.576 5.724 0.24 134972. 0.2042 28.82 0.5073 0.6842 0.0283 0.0210 0.146 3.062 1.298 108.696 0.346 5.772 5.415 0.24 135240. 0.1810 30.13 0.5303 0.6709 0.0243 0.0192 0.134 2.805 1.115 99.558 0.317 4.958 5.079 0.24 135518. 0.1573 31.44 0.5534 0.6478 0.0203 0.0173 0.120 2.529 0.930 89.750 0.286 4.137 4.700 0.24 135807. 0.1330 32.75 0.5765 0.6111 0.0162 0.0153 0.106 2.234 0.744 79.287 0.252 3.309 4.256 0.24 136105. 0.1077 34.06 0.5995 0.5535 0.0121 0.0132 0.091 1.921 0.557 68.191 0.217 2.479 3.706 0.24 136413. 0.0812 35.37 0.6226 0.4614 0.0081 0.0109 0.076 1.592 0.371 56.494 0.180 1.648 2.975 0.24 136731. 0.0531 36.68 0.6456 0.3045 0.0040 0.0085 0.059 1.246 0.185 44.235 0.141 0.821 1.893 0.24 137057. 0.0239 37.99 0.6687 -0.0046 0.0000 0.0060 0.042 0.882 -0.002 31.303 0.100 -0.008 -0.027 0.24 137370. 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 0.0913 0.0299 0.493 7.769 7.446 367.653 0.878 33.121 9.186 0.32 175304. 0.7354 1.75 0.0231 0.0684 0.0898 0.0303 0.500 7.877 7.326 372.758 0.890 32.585 8.914 0.32 175415. 0.7078 3.50 0.0462 0.1326 0.0882 0.0307 0.506 7.977 7.196 377.513 0.901 32.007 8.646 0.32 175536. 0.6804 5.25 0.0693 0.1929 0.0865 0.0311 0.512 8.068 7.056 381.817 0.912 31.385 8.382 0.32 175667. 0.6532 7.00 0.0924 0.2493 0.0846 0.0314 0.517 8.147 6.906 385.566 0.920 30.716 8.124 0.32 175808. 0.6263 8.75 0.1155 0.3019 0.0827 0.0316 0.521 8.212 6.744 388.651 0.928 29.999 7.871 0.32 175958. 0.5997 10.50 0.1386 0.3509 0.0805 0.0318 0.524 8.261 6.571 390.953 0.933 29.230 7.624 0.32 176120. 0.5734 12.25 0.1617 0.3964 0.0783 0.0319 0.526 8.291 6.387 392.348 0.937 28.407 7.383 0.32 176293. 0.5474 14.00 0.1848 0.4386 0.0759 0.0320 0.527 8.298 6.189 392.710 0.938 27.529 7.148 0.32 176476. 0.5217 15.75 0.2079 0.4777 0.0733 0.0319 0.526 8.281 5.979 391.914 0.936 26.594 6.919 0.32 176672. 0.4964 17.50 0.2310 0.5137 0.0706 0.0317 0.523 8.238 5.756 389.850 0.931 25.602 6.697 0.32 176879. 0.4713 19.25 0.2541 0.5467 0.0677 0.0314 0.518 8.166 5.520 386.434 0.923 24.554 6.479 0.32 177097. 0.4466 21.00 0.2772 0.5769 0.0646 0.0311 0.512 8.064 5.273 381.611 0.911 23.454 6.267 0.32 177328. 0.4222 22.75 0.3002 0.6043 0.0615 0.0305 0.503 7.931 5.015 375.343 0.896 22.305 6.060 0.32 177572. 0.3981 24.50 0.3233 0.6289 0.0582 0.0299 0.493 7.768 4.746 367.600 0.878 21.112 5.856 0.32 177827. 0.3743 26.25 0.3464 0.6508 0.0548 0.0292 0.481 7.572 4.469 358.355 0.856 19.877 5.656 0.32 178095. 0.3508 27.99 0.3695 0.6699 0.0513 0.0283 0.466 7.345 4.183 347.580 0.830 18.605 5.458 0.32 178376. 0.3275 29.74 0.3926 0.6861 0.0477 0.0273 0.450 7.084 3.889 335.248 0.800 17.297 5.261 0.32 178670. 0.3044 31.49 0.4157 0.6992 0.0440 0.0261 0.431 6.790 3.587 321.335 0.767 15.957 5.064 0.32 178976. 0.2814 33.24 0.4388 0.7089 0.0402 0.0249 0.410 6.462 3.280 305.815 0.730 14.588 4.864 0.32 179295. 0.2584 34.99 0.4619 0.7149 0.0364 0.0235 0.387 6.100 2.966 288.670 0.689 13.192 4.660 0.32 179628. 0.2354 36.74 0.4850 0.7164 0.0324 0.0220 0.362 5.703 2.646 269.885 0.644 11.772 4.448 0.32 179974. 0.2123 38.49 0.5081 0.7126 0.0285 0.0203 0.335 5.271 2.322 249.456 0.596 10.330 4.223 0.32 180333. 0.1888 40.24 0.5312 0.7019 0.0244 0.0185 0.305 4.805 1.994 227.384 0.543 8.871 3.978 0.32 180705. 0.1648 41.99 0.5543 0.6818 0.0204 0.0166 0.273 4.304 1.663 203.689 0.486 7.398 3.704 0.32 181090. 0.1401 43.74 0.5774 0.6483 0.0163 0.0145 0.239 3.770 1.330 178.404 0.426 5.915 3.381 0.32 181489. 0.1144 45.49 0.6005 0.5939 0.0122 0.0123 0.203 3.203 0.995 151.586 0.362 4.427 2.978 0.32 181901. 0.0872 47.24 0.6236 0.5033 0.0081 0.0100 0.165 2.606 0.661 123.314 0.294 2.939 2.430 0.32 182326. 0.0580 48.99 0.6467 0.3407 0.0040 0.0076 0.126 1.980 0.328 93.681 0.224 1.457 1.586 0.32 182763. 0.0266 50.74 0.6698 -0.0131 -0.0001 0.0051 0.084 1.316 -0.008 62.270 0.149 -0.036 -0.059 0.32 183169. 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 0.0921 0.0297 0.956 12.055 11.735 713.101 1.362 52.199 7.464 0.40 219116. 0.7502 2.19 0.0231 0.0695 0.0906 0.0301 0.970 12.227 11.547 723.323 1.381 51.362 7.241 0.40 219256. 0.7219 4.38 0.0462 0.1347 0.0890 0.0305 0.983 12.388 11.344 732.847 1.400 50.458 7.021 0.40 219408. 0.6938 6.57 0.0693 0.1959 0.0873 0.0309 0.994 12.534 11.125 741.471 1.416 49.484 6.805 0.40 219572. 0.6659 8.75 0.0924 0.2531 0.0854 0.0312 1.004 12.661 10.890 748.994 1.430 48.437 6.594 0.40 219749. 0.6384 10.94 0.1156 0.3065 0.0834 0.0315 1.013 12.766 10.637 755.193 1.442 47.311 6.388 0.40 219938. 0.6113 13.13 0.1387 0.3562 0.0813 0.0317 1.019 12.845 10.365 759.837 1.451 46.105 6.187 0.40 220141. 0.5844 15.32 0.1618 0.4024 0.0790 0.0318 1.023 12.893 10.075 762.677 1.457 44.813 5.992 0.40 220357. 0.5580 17.51 0.1849 0.4453 0.0766 0.0318 1.024 12.906 9.765 763.464 1.458 43.433 5.801 0.40 220588. 0.5318 19.70 0.2080 0.4849 0.0740 0.0317 1.022 12.880 9.434 761.949 1.455 41.963 5.616 0.40 220833. 0.5061 21.89 0.2311 0.5215 0.0713 0.0316 1.016 12.812 9.083 757.911 1.448 40.401 5.436 0.40 221093. 0.4806 24.07 0.2542 0.5552 0.0683 0.0313 1.007 12.698 8.712 751.184 1.435 38.752 5.260 0.40 221367. 0.4555 26.26 0.2773 0.5860 0.0653 0.0309 0.995 12.537 8.323 741.654 1.416 37.019 5.090 0.40 221657. 0.4308 28.45 0.3004 0.6141 0.0621 0.0304 0.978 12.328 7.916 729.249 1.393 35.210 4.923 0.40 221962. 0.4064 30.64 0.3235 0.6394 0.0588 0.0297 0.957 12.068 7.493 713.907 1.363 33.329 4.761 0.40 222282. 0.3823 32.83 0.3467 0.6621 0.0553 0.0290 0.933 11.758 7.055 695.575 1.328 31.383 4.601 0.40 222618. 0.3585 35.02 0.3698 0.6821 0.0518 0.0281 0.904 11.397 6.604 674.197 1.288 29.376 4.443 0.40 222970. 0.3350 37.20 0.3929 0.6992 0.0482 0.0271 0.871 10.983 6.141 649.720 1.241 27.314 4.287 0.40 223338. 0.3117 39.39 0.4160 0.7134 0.0444 0.0259 0.834 10.516 5.666 622.094 1.188 25.201 4.131 0.40 223722. 0.2885 41.58 0.4391 0.7244 0.0406 0.0246 0.793 9.995 5.180 591.272 1.129 23.041 3.974 0.40 224122. 0.2653 43.77 0.4622 0.7317 0.0368 0.0232 0.747 9.419 4.685 557.211 1.064 20.838 3.813 0.40 224538. 0.2422 45.96 0.4853 0.7349 0.0328 0.0217 0.697 8.788 4.181 519.889 0.993 18.598 3.648 0.40 224971. 0.2188 48.15 0.5084 0.7330 0.0288 0.0200 0.643 8.102 3.670 479.291 0.915 16.323 3.473 0.40 225421. 0.1952 50.34 0.5315 0.7246 0.0247 0.0181 0.584 7.361 3.152 435.425 0.832 14.021 3.284 0.40 225887. 0.1710 52.52 0.5547 0.7072 0.0206 0.0162 0.521 6.564 2.630 388.326 0.742 11.696 3.071 0.40 226370. 0.1461 54.71 0.5778 0.6768 0.0165 0.0141 0.453 5.715 2.103 338.063 0.646 9.355 2.822 0.40 226869. 0.1201 56.90 0.6009 0.6258 0.0124 0.0119 0.382 4.814 1.575 284.748 0.544 7.006 2.509 0.40 227385. 0.0924 59.09 0.6240 0.5383 0.0082 0.0095 0.306 3.863 1.047 228.541 0.436 4.657 2.078 0.40 227917. 0.0624 61.28 0.6471 0.3744 0.0041 0.0071 0.227 2.867 0.521 169.628 0.324 2.318 1.394 0.40 228463. 0.0295 63.47 0.6702 -0.0117 -0.0001 0.0045 0.144 1.809 -0.010 107.021 0.204 -0.044 -0.042 0.41 228963. 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 0.0930 0.0298 1.655 17.387 17.080 1234.235 1.964 75.971 6.277 0.48 262919. 0.7610 2.65 0.0234 0.0708 0.0916 0.0302 1.680 17.644 16.806 1252.520 1.993 74.755 6.086 0.48 263090. 0.7320 5.31 0.0467 0.1372 0.0899 0.0306 1.702 17.884 16.510 1269.540 2.021 73.438 5.899 0.48 263275. 0.7032 7.96 0.0701 0.1995 0.0882 0.0310 1.723 18.101 16.191 1284.924 2.045 72.017 5.715 0.48 263475. 0.6747 10.61 0.0934 0.2576 0.0863 0.0313 1.741 18.289 15.846 1298.307 2.066 70.485 5.536 0.48 263690. 0.6465 13.27 0.1168 0.3119 0.0843 0.0316 1.756 18.444 15.476 1309.283 2.084 68.837 5.361 0.48 263922. 0.6188 15.92 0.1401 0.3623 0.0821 0.0318 1.767 18.559 15.078 1317.432 2.097 67.066 5.191 0.48 264169. 0.5914 18.58 0.1635 0.4093 0.0798 0.0319 1.773 18.627 14.651 1322.307 2.105 65.168 5.026 0.48 264434. 0.5644 21.23 0.1868 0.4528 0.0773 0.0319 1.775 18.644 14.195 1323.451 2.106 63.138 4.865 0.48 264716. 0.5377 23.88 0.2102 0.4930 0.0747 0.0318 1.771 18.601 13.708 1320.422 2.102 60.971 4.709 0.48 265016. 0.5115 26.54 0.2335 0.5301 0.0719 0.0317 1.761 18.494 13.190 1312.821 2.089 58.669 4.557 0.48 265333. 0.4856 29.19 0.2569 0.5643 0.0689 0.0314 1.744 18.318 12.643 1300.350 2.070 56.234 4.410 0.48 265669. 0.4600 31.84 0.2802 0.5957 0.0657 0.0309 1.720 18.071 12.068 1282.818 2.042 53.676 4.267 0.48 266024. 0.4349 34.50 0.3036 0.6242 0.0625 0.0304 1.690 17.751 11.467 1260.094 2.006 51.004 4.127 0.48 266397. 0.4100 37.15 0.3269 0.6501 0.0591 0.0297 1.652 17.356 10.842 1232.074 1.961 48.226 3.991 0.48 266789. 0.3856 39.81 0.3503 0.6732 0.0555 0.0289 1.607 16.886 10.196 1198.661 1.908 45.351 3.858 0.48 267200. 0.3614 42.46 0.3736 0.6937 0.0519 0.0280 1.555 16.338 9.529 1159.761 1.846 42.386 3.727 0.48 267631. 0.3375 45.11 0.3970 0.7114 0.0482 0.0269 1.496 15.711 8.844 1115.276 1.775 39.340 3.597 0.48 268081. 0.3138 47.77 0.4203 0.7261 0.0444 0.0257 1.428 15.004 8.142 1065.116 1.695 36.217 3.467 0.48 268551. 0.2903 50.42 0.4437 0.7376 0.0404 0.0243 1.353 14.217 7.425 1009.199 1.606 33.026 3.337 0.48 269041. 0.2668 53.07 0.4670 0.7456 0.0365 0.0228 1.271 13.347 6.693 947.460 1.508 29.773 3.204 0.48 269550. 0.2432 55.73 0.4904 0.7493 0.0324 0.0212 1.180 12.395 5.949 879.851 1.400 26.463 3.067 0.48 270080. 0.2195 58.38 0.5138 0.7478 0.0283 0.0194 1.081 11.359 5.194 806.358 1.283 23.105 2.922 0.48 270630. 0.1954 61.03 0.5371 0.7395 0.0241 0.0175 0.975 10.241 4.430 727.004 1.157 19.705 2.764 0.48 271200. 0.1707 63.69 0.5605 0.7218 0.0199 0.0155 0.861 9.042 3.659 641.865 1.022 16.274 2.585 0.48 271791. 0.1451 66.34 0.5838 0.6900 0.0157 0.0133 0.739 7.763 2.882 551.083 0.877 12.820 2.372 0.48 272402. 0.1182 69.00 0.6072 0.6345 0.0115 0.0110 0.610 6.408 2.104 454.884 0.724 9.358 2.098 0.48 273033. 0.0893 71.65 0.6305 0.5344 0.0072 0.0085 0.474 4.981 1.326 353.579 0.563 5.899 1.701 0.49 273684. 0.0575 74.30 0.6539 0.3298 0.0030 0.0060 0.332 3.486 0.552 247.477 0.394 2.457 1.012 0.49 274349. 0.0221 76.96 0.6772 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 0.0943 0.0300 2.651 23.872 23.551 1977.067 2.697 104.754 5.403 0.56 306708. 0.7692 3.06 0.0231 0.0704 0.0928 0.0305 2.691 24.229 23.184 2006.618 2.737 103.122 5.240 0.56 306906. 0.7403 6.13 0.0462 0.1365 0.0912 0.0309 2.728 24.561 22.786 2034.139 2.775 101.354 5.081 0.56 307121. 0.7116 9.19 0.0693 0.1984 0.0895 0.0313 2.761 24.862 22.357 2059.047 2.809 99.442 4.925 0.56 307353. 0.6832 12.25 0.0924 0.2564 0.0876 0.0316 2.790 25.124 21.893 2080.759 2.839 97.380 4.772 0.56 307602. 0.6551 15.32 0.1155 0.3105 0.0856 0.0319 2.814 25.340 21.394 2098.650 2.863 95.159 4.624 0.56 307870. 0.6274 18.38 0.1386 0.3609 0.0835 0.0321 2.832 25.502 20.857 2112.056 2.881 92.772 4.479 0.56 308156. 0.6001 21.44 0.1618 0.4079 0.0812 0.0322 2.843 25.602 20.281 2120.281 2.892 90.212 4.339 0.56 308461. 0.5732 24.51 0.1849 0.4515 0.0787 0.0322 2.846 25.630 19.665 2122.617 2.896 87.471 4.202 0.56 308787. 0.5467 27.57 0.2080 0.4919 0.0761 0.0322 2.841 25.578 19.007 2118.360 2.890 84.545 4.070 0.56 309133. 0.5206 30.64 0.2311 0.5293 0.0733 0.0320 2.825 25.440 18.308 2106.874 2.874 81.433 3.941 0.56 309499. 0.4948 33.70 0.2542 0.5639 0.0703 0.0317 2.800 25.208 17.567 2087.674 2.848 78.140 3.817 0.56 309886. 0.4693 36.76 0.2773 0.5956 0.0672 0.0313 2.763 24.879 16.789 2060.440 2.811 74.675 3.696 0.56 310294. 0.4443 39.83 0.3004 0.6247 0.0639 0.0307 2.716 24.451 15.974 2024.962 2.762 71.053 3.578 0.56 310723. 0.4196 42.89 0.3235 0.6512 0.0605 0.0301 2.657 23.921 15.127 1981.084 2.703 67.284 3.463 0.56 311174. 0.3952 45.95 0.3466 0.6751 0.0570 0.0293 2.586 23.288 14.249 1928.659 2.631 63.382 3.351 0.56 311647. 0.3711 49.02 0.3697 0.6964 0.0534 0.0284 2.504 22.550 13.344 1867.544 2.548 59.355 3.241 0.56 312141. 0.3473 52.08 0.3928 0.7151 0.0497 0.0273 2.411 21.705 12.413 1797.593 2.452 55.215 3.132 0.56 312658. 0.3238 55.14 0.4159 0.7311 0.0459 0.0261 2.305 20.752 11.459 1718.666 2.345 50.969 3.024 0.56 313198. 0.3003 58.21 0.4390 0.7441 0.0420 0.0248 2.187 19.689 10.483 1630.634 2.224 46.628 2.916 0.56 313760. 0.2770 61.27 0.4622 0.7538 0.0380 0.0233 2.056 18.515 9.487 1533.387 2.092 42.199 2.806 0.56 314344. 0.2536 64.33 0.4853 0.7597 0.0339 0.0217 1.913 17.229 8.474 1426.848 1.946 37.691 2.694 0.56 314952. 0.2300 67.40 0.5084 0.7610 0.0298 0.0199 1.758 15.830 7.445 1310.981 1.788 33.114 2.576 0.56 315582. 0.2062 70.46 0.5315 0.7565 0.0256 0.0180 1.590 14.318 6.402 1185.806 1.618 28.478 2.449 0.56 316236. 0.1818 73.52 0.5546 0.7438 0.0214 0.0160 1.410 12.696 5.349 1051.421 1.434 23.793 2.308 0.56 316912. 0.1566 76.59 0.5777 0.7192 0.0172 0.0138 1.218 10.964 4.288 908.019 1.239 19.075 2.142 0.56 317612. 0.1301 79.65 0.6008 0.6754 0.0129 0.0115 1.014 9.127 3.223 755.917 1.031 14.337 1.934 0.57 318335. 0.1019 82.72 0.6239 0.5960 0.0086 0.0090 0.799 7.191 2.158 595.571 0.812 9.599 1.644 0.57 319080. 0.0708 85.78 0.6470 0.4376 0.0044 0.0065 0.573 5.162 1.097 427.524 0.583 4.879 1.164 0.57 319845. 0.0358 88.84 0.6701 0.0188 0.0001 0.0038 0.334 3.010 0.027 249.322 0.340 0.118 0.048 0.57 320553. 0.0002 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 0.0957 0.0305 4.019 31.663 31.244 2996.912 3.577 138.974 4.729 0.63 350480. 0.7755 3.51 0.0232 0.0706 0.0943 0.0309 4.080 32.147 30.767 3042.662 3.632 136.851 4.586 0.63 350709. 0.7464 7.02 0.0463 0.1369 0.0927 0.0314 4.137 32.596 30.248 3085.218 3.683 134.543 4.447 0.63 350956. 0.7175 10.53 0.0695 0.1990 0.0910 0.0318 4.189 33.003 29.686 3123.680 3.729 132.042 4.310 0.63 351223. 0.6890 14.04 0.0927 0.2571 0.0891 0.0321 4.234 33.356 29.077 3157.138 3.769 129.336 4.177 0.63 351511. 0.6609 17.55 0.1158 0.3114 0.0871 0.0324 4.271 33.647 28.421 3184.633 3.801 126.415 4.048 0.64 351819. 0.6331 21.06 0.1390 0.3621 0.0849 0.0326 4.298 33.863 27.714 3205.146 3.826 123.270 3.922 0.64 352150. 0.6057 24.57 0.1622 0.4093 0.0826 0.0327 4.315 33.995 26.954 3217.615 3.841 119.889 3.799 0.64 352502. 0.5787 28.08 0.1853 0.4531 0.0801 0.0328 4.319 34.030 26.139 3220.939 3.845 116.265 3.681 0.64 352878. 0.5521 31.59 0.2085 0.4938 0.0774 0.0327 4.310 33.957 25.268 3214.050 3.836 112.390 3.566 0.64 353276. 0.5259 35.10 0.2317 0.5315 0.0746 0.0325 4.286 33.766 24.340 3195.969 3.815 108.263 3.454 0.64 353699. 0.5000 38.61 0.2548 0.5664 0.0716 0.0322 4.246 33.449 23.357 3165.951 3.779 103.890 3.346 0.64 354145. 0.4744 42.12 0.2780 0.5985 0.0684 0.0318 4.189 33.001 22.322 3123.510 3.728 99.286 3.241 0.64 354615. 0.4493 45.63 0.3012 0.6280 0.0651 0.0312 4.115 32.418 21.238 3068.338 3.663 94.468 3.139 0.64 355110. 0.4245 49.14 0.3243 0.6550 0.0616 0.0305 4.023 31.698 20.111 3000.208 3.581 89.452 3.040 0.64 355629. 0.4000 52.65 0.3475 0.6794 0.0580 0.0297 3.914 30.839 18.942 2918.916 3.484 84.254 2.943 0.64 356174. 0.3758 56.16 0.3707 0.7013 0.0543 0.0287 3.787 29.839 17.736 2824.258 3.371 78.889 2.848 0.64 356743. 0.3519 59.67 0.3938 0.7206 0.0505 0.0276 3.642 28.696 16.495 2716.018 3.242 73.371 2.755 0.64 357338. 0.3282 63.18 0.4170 0.7372 0.0466 0.0264 3.479 27.406 15.223 2593.996 3.096 67.710 2.662 0.64 357959. 0.3047 66.69 0.4402 0.7510 0.0427 0.0250 3.296 25.969 13.921 2457.994 2.934 61.920 2.569 0.64 358606. 0.2812 70.20 0.4633 0.7616 0.0386 0.0235 3.095 24.383 12.592 2307.853 2.755 56.011 2.475 0.64 359278. 0.2577 73.71 0.4865 0.7686 0.0344 0.0218 2.874 22.646 11.240 2143.458 2.559 49.996 2.378 0.64 359977. 0.2339 77.22 0.5097 0.7711 0.0302 0.0200 2.635 20.758 9.866 1964.759 2.345 43.886 2.278 0.64 360702. 0.2099 80.73 0.5328 0.7678 0.0260 0.0180 2.376 18.720 8.475 1771.792 2.115 37.695 2.169 0.64 361453. 0.1853 84.24 0.5560 0.7567 0.0217 0.0159 2.098 16.532 7.068 1564.713 1.868 31.440 2.049 0.64 362231. 0.1598 87.75 0.5791 0.7338 0.0173 0.0137 1.802 14.198 5.651 1343.825 1.604 25.137 1.907 0.65 363035. 0.1330 91.26 0.6023 0.6915 0.0130 0.0113 1.488 11.724 4.228 1109.627 1.325 18.808 1.728 0.65 363865. 0.1043 94.77 0.6255 0.6126 0.0086 0.0088 1.157 9.116 2.805 862.839 1.030 12.477 1.475 0.65 364721. 0.0725 98.28 0.6486 0.4486 0.0043 0.0061 0.810 6.385 1.387 604.294 0.721 6.171 1.041 0.65 365599. 0.0360 101.79 0.6718 -0.0509 -0.0002 0.0033 0.432 3.407 -0.081 322.492 0.385 -0.361 -0.114 0.65 366238. 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 0.0975 0.0313 5.880 41.181 40.287 4384.948 4.653 179.195 4.167 0.71 394230. 0.7760 3.96 0.0232 0.0702 0.0961 0.0318 5.966 41.781 39.689 4448.871 4.720 176.539 4.046 0.71 394489. 0.7479 7.92 0.0464 0.1363 0.0945 0.0322 6.046 42.340 39.037 4508.394 4.784 173.636 3.927 0.71 394769. 0.7199 11.87 0.0697 0.1983 0.0928 0.0326 6.118 42.846 38.327 4562.229 4.841 170.477 3.810 0.71 395073. 0.6921 15.83 0.0929 0.2565 0.0909 0.0329 6.181 43.285 37.556 4609.051 4.890 167.048 3.696 0.71 395399. 0.6645 19.79 0.1161 0.3109 0.0889 0.0332 6.232 43.646 36.721 4647.435 4.931 163.333 3.584 0.71 395750. 0.6371 23.75 0.1393 0.3617 0.0867 0.0334 6.270 43.913 35.819 4675.861 4.961 159.321 3.474 0.71 396126. 0.6101 27.70 0.1625 0.4091 0.0844 0.0335 6.293 44.071 34.846 4692.722 4.979 154.997 3.368 0.71 396526. 0.5833 31.66 0.1858 0.4531 0.0818 0.0335 6.298 44.105 33.802 4696.350 4.983 150.350 3.265 0.72 396953. 0.5568 35.62 0.2090 0.4941 0.0791 0.0335 6.283 44.000 32.683 4685.098 4.971 145.372 3.164 0.72 397406. 0.5307 39.58 0.2322 0.5321 0.0762 0.0333 6.246 43.740 31.488 4657.456 4.942 140.060 3.067 0.72 397886. 0.5048 43.54 0.2554 0.5672 0.0732 0.0329 6.185 43.315 30.221 4612.233 4.894 134.423 2.972 0.72 398392. 0.4793 47.49 0.2786 0.5997 0.0699 0.0325 6.100 42.718 28.885 4548.646 4.826 128.480 2.880 0.72 398926. 0.4542 51.45 0.3018 0.6296 0.0665 0.0319 5.989 41.944 27.485 4466.222 4.739 122.252 2.791 0.72 399488. 0.4293 55.41 0.3251 0.6570 0.0630 0.0312 5.853 40.990 26.026 4364.638 4.631 115.763 2.705 0.72 400078. 0.4048 59.37 0.3483 0.6819 0.0594 0.0303 5.691 39.854 24.513 4243.631 4.503 109.035 2.620 0.72 400695. 0.3806 63.32 0.3715 0.7043 0.0556 0.0293 5.502 38.532 22.951 4102.926 4.353 102.086 2.537 0.72 401341. 0.3566 67.28 0.3947 0.7243 0.0517 0.0282 5.287 37.023 21.343 3942.248 4.183 94.934 2.456 0.72 402016. 0.3328 71.24 0.4179 0.7417 0.0477 0.0269 5.044 35.324 19.693 3761.309 3.991 87.595 2.375 0.72 402719. 0.3092 75.20 0.4412 0.7563 0.0436 0.0254 4.774 33.432 18.005 3559.836 3.777 80.084 2.294 0.72 403451. 0.2856 79.15 0.4644 0.7678 0.0394 0.0238 4.476 31.345 16.281 3337.594 3.541 72.417 2.213 0.72 404213. 0.2619 83.11 0.4876 0.7757 0.0352 0.0221 4.150 29.061 14.525 3094.427 3.283 64.607 2.129 0.72 405004. 0.2381 87.07 0.5108 0.7794 0.0308 0.0202 3.795 26.580 12.741 2830.271 3.003 56.672 2.042 0.72 405824. 0.2138 91.03 0.5340 0.7775 0.0265 0.0182 3.413 23.903 10.933 2545.213 2.701 48.630 1.948 0.72 406674. 0.1890 94.99 0.5573 0.7679 0.0220 0.0160 3.003 21.032 9.105 2239.536 2.376 40.500 1.844 0.73 407554. 0.1632 98.94 0.5805 0.7466 0.0176 0.0137 2.566 17.973 7.263 1913.790 2.031 32.305 1.721 0.73 408463. 0.1361 102.90 0.6037 0.7059 0.0131 0.0112 2.104 14.734 5.412 1568.880 1.665 24.074 1.565 0.73 409402. 0.1068 106.86 0.6269 0.6273 0.0086 0.0086 1.617 11.327 3.561 1206.113 1.280 15.839 1.339 0.73 410370. 0.0741 110.82 0.6501 0.4572 0.0042 0.0059 1.109 7.767 1.716 827.046 0.878 7.632 0.941 0.73 411362. 0.0362 114.77 0.6733 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 0.0339 8.725 54.990 50.826 6505.989 6.213 226.074 3.543 0.79 437947. 0.7411 4.40 0.0232 0.0668 0.0983 0.0342 8.812 55.543 50.108 6571.388 6.275 222.880 3.459 0.79 438237. 0.7183 8.81 0.0465 0.1303 0.0967 0.0345 8.891 56.038 49.318 6629.908 6.331 219.367 3.374 0.79 438551. 0.6952 13.21 0.0697 0.1905 0.0950 0.0348 8.958 56.461 48.453 6680.059 6.379 215.518 3.290 0.79 438891. 0.6719 17.61 0.0930 0.2476 0.0932 0.0350 9.012 56.802 47.508 6720.329 6.417 211.316 3.206 0.79 439258. 0.6484 22.01 0.1162 0.3015 0.0912 0.0351 9.051 57.045 46.480 6749.093 6.445 206.742 3.124 0.79 439651. 0.6248 26.42 0.1395 0.3523 0.0890 0.0352 9.071 57.176 45.364 6764.592 6.460 201.778 3.042 0.79 440073. 0.6010 30.82 0.1627 0.4000 0.0866 0.0352 9.072 57.179 44.156 6764.904 6.460 196.407 2.961 0.79 440523. 0.5772 35.22 0.1860 0.4448 0.0840 0.0351 9.049 57.036 42.854 6748.019 6.444 190.614 2.880 0.79 441002. 0.5532 39.63 0.2092 0.4867 0.0813 0.0350 9.001 56.730 41.454 6711.839 6.409 184.389 2.801 0.80 441510. 0.5292 44.03 0.2325 0.5257 0.0784 0.0347 8.924 56.245 39.957 6654.418 6.355 177.728 2.723 0.80 442049. 0.5051 48.43 0.2557 0.5620 0.0752 0.0342 8.816 55.566 38.364 6574.139 6.278 170.641 2.647 0.80 442617. 0.4810 52.84 0.2790 0.5956 0.0719 0.0337 8.676 54.685 36.680 6469.924 6.178 163.152 2.571 0.80 443216. 0.4569 57.24 0.3022 0.6266 0.0685 0.0330 8.503 53.596 34.913 6341.030 6.055 155.291 2.497 0.80 443845. 0.4329 61.64 0.3255 0.6551 0.0649 0.0322 8.297 52.293 33.068 6186.877 5.908 147.088 2.424 0.80 444506. 0.4090 66.04 0.3487 0.6811 0.0611 0.0313 8.055 50.771 31.154 6006.864 5.736 138.572 2.352 0.80 445198. 0.3852 70.45 0.3720 0.7046 0.0572 0.0302 7.778 49.026 29.174 5800.374 5.539 129.768 2.281 0.80 445921. 0.3615 74.85 0.3952 0.7255 0.0532 0.0290 7.465 47.052 27.136 5566.763 5.316 120.699 2.211 0.80 446675. 0.3379 79.25 0.4185 0.7438 0.0491 0.0276 7.115 44.844 25.042 5305.525 5.066 111.387 2.141 0.80 447462. 0.3143 83.66 0.4417 0.7593 0.0449 0.0261 6.727 42.400 22.898 5016.364 4.790 101.850 2.070 0.80 448281. 0.2907 88.06 0.4650 0.7716 0.0406 0.0245 6.301 39.717 20.708 4698.966 4.487 92.108 1.999 0.80 449131. 0.2669 92.46 0.4882 0.7804 0.0362 0.0227 5.837 36.792 18.476 4352.919 4.157 82.180 1.925 0.80 450015. 0.2428 96.86 0.5114 0.7846 0.0318 0.0207 5.335 33.627 16.206 3978.473 3.799 72.084 1.848 0.80 450931. 0.2182 101.27 0.5347 0.7828 0.0273 0.0186 4.796 30.229 13.904 3576.459 3.415 61.845 1.763 0.80 451880. 0.1929 105.67 0.5579 0.7726 0.0227 0.0164 4.222 26.608 11.575 3148.082 3.006 51.486 1.668 0.81 452861. 0.1665 110.07 0.5812 0.7493 0.0181 0.0140 3.614 22.779 9.226 2695.062 2.574 41.037 1.553 0.81 453875. 0.1384 114.48 0.6044 0.7039 0.0135 0.0116 2.977 18.762 6.864 2219.774 2.120 30.532 1.403 0.81 454922. 0.1078 118.88 0.6277 0.6164 0.0088 0.0090 2.314 14.582 4.499 1725.274 1.648 20.011 1.183 0.81 456001. 0.0736 123.28 0.6509 0.4316 0.0042 0.0063 1.629 10.269 2.139 1214.956 1.160 9.515 0.799 0.81 457106. 0.0343 127.69 0.6742