20.5x10.5WPN (205x105WPN.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 0.0966 0.0383 0.011 0.704 0.544 8.327 0.080 2.420 29.631 0.08 47571. 0.6255 0.45 0.0231 0.0568 0.0950 0.0387 0.011 0.711 0.535 8.406 0.080 2.379 28.858 0.08 47602. 0.6041 0.90 0.0463 0.1107 0.0933 0.0390 0.011 0.717 0.525 8.479 0.081 2.335 28.086 0.08 47637. 0.5825 1.35 0.0694 0.1615 0.0914 0.0393 0.011 0.722 0.515 8.542 0.082 2.289 27.320 0.08 47674. 0.5609 1.80 0.0926 0.2093 0.0894 0.0396 0.012 0.726 0.503 8.595 0.082 2.239 26.559 0.08 47713. 0.5393 2.25 0.1157 0.2542 0.0873 0.0397 0.012 0.730 0.491 8.635 0.082 2.185 25.804 0.08 47756. 0.5177 2.70 0.1389 0.2962 0.0850 0.0399 0.012 0.732 0.478 8.660 0.083 2.128 25.056 0.08 47801. 0.4960 3.15 0.1620 0.3353 0.0826 0.0399 0.012 0.733 0.465 8.667 0.083 2.067 24.316 0.08 47849. 0.4744 3.59 0.1852 0.3717 0.0800 0.0398 0.012 0.732 0.450 8.655 0.083 2.002 23.584 0.08 47901. 0.4528 4.04 0.2083 0.4053 0.0772 0.0397 0.012 0.729 0.435 8.622 0.082 1.933 22.858 0.08 47955. 0.4313 4.49 0.2315 0.4361 0.0743 0.0394 0.011 0.724 0.418 8.565 0.082 1.860 22.139 0.08 48012. 0.4097 4.94 0.2546 0.4643 0.0712 0.0391 0.011 0.717 0.401 8.485 0.081 1.783 21.426 0.08 48073. 0.3883 5.39 0.2778 0.4897 0.0680 0.0386 0.011 0.708 0.383 8.380 0.080 1.702 20.716 0.08 48137. 0.3668 5.84 0.3009 0.5124 0.0647 0.0380 0.011 0.697 0.364 8.249 0.079 1.619 20.007 0.08 48204. 0.3454 6.29 0.3241 0.5322 0.0612 0.0373 0.011 0.684 0.344 8.093 0.077 1.532 19.297 0.08 48275. 0.3241 6.74 0.3472 0.5491 0.0576 0.0364 0.011 0.669 0.324 7.912 0.076 1.442 18.583 0.08 48349. 0.3028 7.19 0.3704 0.5630 0.0539 0.0355 0.010 0.651 0.303 7.705 0.074 1.349 17.861 0.08 48426. 0.2816 7.64 0.3935 0.5735 0.0501 0.0344 0.010 0.631 0.282 7.471 0.071 1.255 17.125 0.08 48507. 0.2603 8.09 0.4167 0.5805 0.0462 0.0332 0.010 0.609 0.260 7.210 0.069 1.157 16.370 0.08 48591. 0.2390 8.54 0.4398 0.5834 0.0423 0.0319 0.009 0.585 0.238 6.923 0.066 1.058 15.588 0.08 48679. 0.2176 8.99 0.4629 0.5819 0.0382 0.0304 0.009 0.559 0.215 6.608 0.063 0.957 14.770 0.08 48770. 0.1961 9.44 0.4861 0.5751 0.0341 0.0288 0.008 0.530 0.192 6.265 0.060 0.854 13.903 0.08 48865. 0.1744 9.89 0.5092 0.5621 0.0299 0.0271 0.008 0.498 0.169 5.895 0.056 0.750 12.969 0.08 48964. 0.1524 10.34 0.5324 0.5412 0.0257 0.0253 0.007 0.465 0.145 5.498 0.053 0.644 11.945 0.08 49066. 0.1301 10.78 0.5555 0.5105 0.0215 0.0234 0.007 0.429 0.121 5.073 0.048 0.537 10.797 0.08 49171. 0.1074 11.23 0.5787 0.4667 0.0172 0.0213 0.006 0.391 0.097 4.622 0.044 0.430 9.477 0.08 49281. 0.0843 11.68 0.6018 0.4050 0.0128 0.0191 0.006 0.350 0.072 4.144 0.040 0.321 7.907 0.08 49393. 0.0608 12.13 0.6250 0.3174 0.0085 0.0168 0.005 0.308 0.048 3.642 0.035 0.213 5.967 0.08 49510. 0.0374 12.58 0.6481 0.1897 0.0042 0.0143 0.004 0.263 0.024 3.117 0.030 0.105 3.440 0.08 49630. 0.0151 13.03 0.6713 -0.0064 -0.0001 0.0118 0.003 0.217 -0.001 2.566 0.025 -0.003 -0.112 0.08 49750. 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 0.0971 0.0349 0.081 2.564 2.187 60.677 0.290 9.727 16.348 0.16 95139. 0.6920 0.90 0.0233 0.0629 0.0955 0.0353 0.082 2.594 2.150 61.372 0.293 9.565 15.892 0.16 95203. 0.6671 1.81 0.0465 0.1222 0.0938 0.0357 0.083 2.621 2.111 62.012 0.296 9.390 15.441 0.16 95272. 0.6422 2.71 0.0698 0.1781 0.0919 0.0360 0.084 2.645 2.069 62.580 0.299 9.203 14.996 0.16 95347. 0.6174 3.61 0.0930 0.2305 0.0899 0.0363 0.085 2.665 2.024 63.061 0.301 9.002 14.557 0.16 95426. 0.5928 4.51 0.1163 0.2795 0.0878 0.0365 0.085 2.681 1.976 63.437 0.303 8.787 14.125 0.16 95512. 0.5683 5.42 0.1395 0.3254 0.0855 0.0366 0.085 2.692 1.924 63.692 0.304 8.558 13.701 0.16 95603. 0.5439 6.32 0.1628 0.3680 0.0830 0.0367 0.086 2.697 1.869 63.806 0.305 8.312 13.284 0.16 95700. 0.5198 7.22 0.1860 0.4077 0.0804 0.0367 0.086 2.695 1.810 63.761 0.304 8.051 12.875 0.16 95803. 0.4958 8.13 0.2093 0.4443 0.0776 0.0366 0.085 2.685 1.747 63.539 0.303 7.773 12.474 0.16 95913. 0.4720 9.03 0.2325 0.4781 0.0747 0.0363 0.085 2.668 1.681 63.126 0.301 7.478 12.080 0.16 96029. 0.4483 9.93 0.2558 0.5091 0.0716 0.0360 0.084 2.642 1.612 62.514 0.298 7.168 11.693 0.16 96151. 0.4249 10.83 0.2790 0.5373 0.0683 0.0355 0.083 2.607 1.539 61.696 0.295 6.844 11.312 0.16 96280. 0.4016 11.74 0.3023 0.5627 0.0650 0.0349 0.081 2.564 1.463 60.668 0.290 6.506 10.936 0.16 96416. 0.3786 12.64 0.3255 0.5854 0.0615 0.0342 0.080 2.511 1.384 59.426 0.284 6.156 10.564 0.16 96558. 0.3557 13.54 0.3488 0.6052 0.0579 0.0334 0.078 2.450 1.303 57.968 0.277 5.795 10.193 0.16 96707. 0.3330 14.45 0.3721 0.6221 0.0542 0.0324 0.075 2.379 1.219 56.290 0.269 5.422 9.823 0.16 96863. 0.3104 15.35 0.3953 0.6359 0.0503 0.0313 0.073 2.299 1.133 54.388 0.260 5.040 9.450 0.16 97026. 0.2879 16.25 0.4186 0.6463 0.0464 0.0301 0.070 2.209 1.045 52.260 0.250 4.649 9.072 0.16 97196. 0.2655 17.15 0.4418 0.6531 0.0424 0.0287 0.067 2.109 0.955 49.901 0.238 4.250 8.685 0.16 97373. 0.2430 18.06 0.4651 0.6557 0.0384 0.0272 0.063 1.999 0.864 47.309 0.226 3.843 8.283 0.16 97557. 0.2204 18.96 0.4883 0.6534 0.0342 0.0256 0.060 1.880 0.771 44.482 0.212 3.429 7.861 0.16 97749. 0.1976 19.86 0.5116 0.6451 0.0301 0.0238 0.056 1.750 0.677 41.420 0.198 3.009 7.408 0.16 97947. 0.1744 20.77 0.5348 0.6293 0.0258 0.0219 0.051 1.611 0.581 38.123 0.182 2.584 6.912 0.16 98153. 0.1508 21.67 0.5581 0.6035 0.0215 0.0199 0.046 1.462 0.485 34.594 0.165 2.155 6.353 0.17 98366. 0.1266 22.57 0.5813 0.5638 0.0172 0.0177 0.041 1.303 0.387 30.837 0.147 1.723 5.698 0.17 98587. 0.1015 23.47 0.6046 0.5038 0.0129 0.0155 0.036 1.135 0.290 26.859 0.128 1.290 4.896 0.17 98814. 0.0754 24.38 0.6278 0.4113 0.0085 0.0130 0.030 0.958 0.192 22.673 0.108 0.856 3.849 0.17 99049. 0.0483 25.28 0.6511 0.2617 0.0042 0.0105 0.025 0.773 0.095 18.289 0.087 0.424 2.362 0.17 99290. 0.0209 26.18 0.6743 -0.0092 -0.0001 0.0079 0.018 0.577 -0.002 13.663 0.065 -0.011 -0.080 0.17 99527. 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 0.0977 0.0336 0.265 5.561 4.948 197.386 0.628 22.009 11.370 0.24 142703. 0.7239 1.36 0.0233 0.0657 0.0961 0.0341 0.268 5.630 4.866 199.826 0.636 21.643 11.045 0.24 142799. 0.6973 2.71 0.0466 0.1276 0.0943 0.0344 0.271 5.693 4.777 202.076 0.643 21.250 10.723 0.24 142904. 0.6708 4.07 0.0699 0.1858 0.0924 0.0348 0.274 5.750 4.682 204.083 0.650 20.827 10.406 0.24 143016. 0.6445 5.43 0.0932 0.2403 0.0904 0.0351 0.276 5.798 4.581 205.793 0.655 20.374 10.096 0.24 143136. 0.6184 6.79 0.1165 0.2913 0.0883 0.0353 0.278 5.836 4.471 207.147 0.659 19.889 9.791 0.24 143265. 0.5926 8.14 0.1398 0.3389 0.0860 0.0355 0.279 5.863 4.355 208.083 0.662 19.370 9.492 0.24 143402. 0.5670 9.50 0.1631 0.3832 0.0835 0.0356 0.280 5.875 4.230 208.537 0.664 18.815 9.200 0.24 143549. 0.5416 10.86 0.1864 0.4243 0.0809 0.0355 0.280 5.873 4.097 208.445 0.664 18.223 8.915 0.24 143704. 0.5165 12.21 0.2097 0.4625 0.0781 0.0354 0.279 5.853 3.956 207.746 0.661 17.594 8.636 0.24 143869. 0.4916 13.57 0.2330 0.4976 0.0751 0.0352 0.277 5.815 3.806 206.391 0.657 16.928 8.364 0.24 144044. 0.4670 14.93 0.2563 0.5300 0.0720 0.0348 0.274 5.757 3.648 204.347 0.650 16.226 8.097 0.24 144229. 0.4427 16.29 0.2797 0.5595 0.0688 0.0344 0.270 5.680 3.483 201.592 0.642 15.492 7.836 0.24 144423. 0.4186 17.64 0.3030 0.5863 0.0654 0.0338 0.266 5.582 3.311 198.111 0.631 14.727 7.580 0.25 144627. 0.3948 19.00 0.3263 0.6104 0.0618 0.0331 0.260 5.463 3.133 193.892 0.617 13.934 7.328 0.25 144842. 0.3712 20.36 0.3496 0.6318 0.0582 0.0322 0.253 5.323 2.948 188.922 0.601 13.114 7.079 0.25 145067. 0.3479 21.72 0.3729 0.6503 0.0545 0.0312 0.246 5.161 2.759 183.187 0.583 12.271 6.831 0.25 145302. 0.3247 23.07 0.3962 0.6659 0.0506 0.0301 0.237 4.978 2.564 176.676 0.562 11.405 6.583 0.25 145547. 0.3017 24.43 0.4195 0.6783 0.0467 0.0289 0.227 4.772 2.365 169.375 0.539 10.519 6.333 0.25 145803. 0.2788 25.79 0.4428 0.6872 0.0427 0.0275 0.216 4.544 2.162 161.274 0.513 9.615 6.079 0.25 146070. 0.2558 27.14 0.4661 0.6923 0.0386 0.0260 0.204 4.293 1.954 152.364 0.485 8.693 5.818 0.25 146348. 0.2328 28.50 0.4894 0.6928 0.0344 0.0243 0.191 4.019 1.744 142.636 0.454 7.755 5.544 0.25 146636. 0.2096 29.86 0.5127 0.6876 0.0302 0.0225 0.177 3.722 1.530 132.090 0.420 6.805 5.253 0.25 146935. 0.1860 31.22 0.5360 0.6753 0.0259 0.0206 0.162 3.401 1.314 120.726 0.384 5.843 4.935 0.25 147245. 0.1619 32.57 0.5593 0.6534 0.0216 0.0185 0.146 3.058 1.095 108.553 0.346 4.871 4.576 0.25 147566. 0.1371 33.93 0.5826 0.6178 0.0173 0.0163 0.128 2.693 0.875 95.589 0.304 3.893 4.153 0.25 147898. 0.1112 35.29 0.6059 0.5612 0.0129 0.0140 0.110 2.306 0.655 81.860 0.261 2.912 3.628 0.25 148241. 0.0840 36.64 0.6292 0.4693 0.0086 0.0115 0.090 1.899 0.434 67.406 0.215 1.931 2.921 0.25 148595. 0.0551 38.00 0.6525 0.3100 0.0042 0.0089 0.070 1.473 0.214 52.267 0.166 0.954 1.861 0.25 148958. 0.0247 39.36 0.6758 -0.0166 -0.0002 0.0062 0.049 1.019 -0.008 36.183 0.115 -0.034 -0.096 0.25 149305. 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 0.0984 0.0331 0.618 9.730 8.859 460.476 1.099 39.407 8.727 0.33 190259. 0.7435 1.81 0.0234 0.0674 0.0968 0.0335 0.625 9.856 8.713 466.415 1.113 38.755 8.473 0.33 190389. 0.7159 3.63 0.0467 0.1308 0.0950 0.0339 0.633 9.972 8.555 471.899 1.127 38.053 8.223 0.33 190528. 0.6884 5.44 0.0701 0.1903 0.0931 0.0343 0.639 10.075 8.386 476.796 1.138 37.300 7.977 0.33 190679. 0.6612 7.26 0.0934 0.2461 0.0911 0.0346 0.645 10.163 8.204 480.979 1.148 36.491 7.736 0.33 190840. 0.6342 9.07 0.1168 0.2982 0.0889 0.0348 0.649 10.234 8.009 484.303 1.156 35.623 7.501 0.33 191013. 0.6076 10.88 0.1401 0.3469 0.0866 0.0350 0.653 10.283 7.800 486.618 1.162 34.695 7.270 0.33 191197. 0.5812 12.70 0.1635 0.3922 0.0841 0.0351 0.654 10.307 7.577 487.768 1.164 33.702 7.046 0.33 191394. 0.5551 14.51 0.1869 0.4342 0.0815 0.0351 0.654 10.303 7.339 487.598 1.164 32.643 6.827 0.33 191603. 0.5293 16.32 0.2102 0.4732 0.0787 0.0350 0.652 10.269 7.085 485.963 1.160 31.516 6.613 0.33 191824. 0.5038 18.14 0.2336 0.5093 0.0757 0.0347 0.647 10.201 6.817 482.740 1.152 30.322 6.405 0.33 192058. 0.4787 19.95 0.2569 0.5425 0.0726 0.0344 0.641 10.097 6.534 477.848 1.141 29.064 6.202 0.33 192306. 0.4538 21.77 0.2803 0.5729 0.0693 0.0339 0.632 9.957 6.238 471.235 1.125 27.746 6.004 0.33 192566. 0.4292 23.58 0.3036 0.6006 0.0658 0.0333 0.621 9.781 5.929 462.863 1.105 26.374 5.810 0.33 192840. 0.4050 25.39 0.3270 0.6256 0.0623 0.0326 0.607 9.566 5.609 452.700 1.081 24.951 5.620 0.33 193128. 0.3810 27.21 0.3504 0.6480 0.0586 0.0317 0.591 9.313 5.279 440.715 1.052 23.480 5.433 0.33 193429. 0.3573 29.02 0.3737 0.6676 0.0548 0.0307 0.572 9.020 4.939 426.876 1.019 21.967 5.247 0.33 193744. 0.3338 30.83 0.3971 0.6843 0.0510 0.0296 0.551 8.688 4.589 411.152 0.982 20.413 5.063 0.33 194073. 0.3104 32.65 0.4204 0.6981 0.0470 0.0283 0.528 8.315 4.232 393.514 0.939 18.823 4.878 0.33 194417. 0.2872 34.46 0.4438 0.7086 0.0429 0.0269 0.501 7.901 3.867 373.933 0.893 17.198 4.690 0.33 194774. 0.2640 36.28 0.4672 0.7153 0.0388 0.0253 0.473 7.446 3.495 352.386 0.841 15.544 4.498 0.33 195146. 0.2407 38.09 0.4905 0.7177 0.0346 0.0237 0.441 6.949 3.116 328.858 0.785 13.861 4.298 0.33 195532. 0.2172 39.90 0.5139 0.7148 0.0303 0.0218 0.407 6.410 2.733 303.342 0.724 12.155 4.086 0.33 195933. 0.1933 41.72 0.5372 0.7050 0.0260 0.0198 0.370 5.829 2.344 275.843 0.659 10.428 3.855 0.33 196348. 0.1689 43.53 0.5606 0.6859 0.0217 0.0177 0.330 5.206 1.953 246.382 0.588 8.685 3.594 0.33 196778. 0.1438 45.34 0.5839 0.6534 0.0173 0.0155 0.288 4.543 1.558 215.004 0.513 6.930 3.287 0.33 197223. 0.1174 47.16 0.6073 0.5996 0.0129 0.0131 0.244 3.841 1.162 181.774 0.434 5.170 2.900 0.33 197682. 0.0895 48.97 0.6307 0.5086 0.0085 0.0106 0.197 3.102 0.767 146.788 0.350 3.410 2.369 0.33 198155. 0.0594 50.79 0.6540 0.3416 0.0041 0.0079 0.148 2.327 0.373 110.147 0.263 1.657 1.534 0.33 198642. 0.0268 52.60 0.6774 -0.0486 -0.0004 0.0051 0.095 1.489 -0.033 70.490 0.168 -0.146 -0.211 0.33 199067. 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 0.0993 0.0330 1.201 15.140 13.969 895.638 1.711 62.133 7.074 0.41 237805. 0.7568 2.27 0.0233 0.0682 0.0976 0.0334 1.217 15.341 13.740 907.482 1.733 61.114 6.867 0.41 237968. 0.7286 4.53 0.0467 0.1324 0.0959 0.0338 1.232 15.525 13.493 918.419 1.754 60.017 6.664 0.41 238143. 0.7006 6.80 0.0700 0.1927 0.0940 0.0342 1.245 15.691 13.228 928.195 1.773 58.837 6.464 0.41 238332. 0.6729 9.07 0.0934 0.2491 0.0920 0.0345 1.256 15.832 12.943 936.549 1.789 57.571 6.268 0.41 238534. 0.6455 11.33 0.1167 0.3019 0.0898 0.0347 1.265 15.944 12.637 943.199 1.801 56.212 6.077 0.41 238751. 0.6184 13.60 0.1401 0.3512 0.0875 0.0349 1.271 16.023 12.310 947.851 1.810 54.755 5.891 0.41 238982. 0.5916 15.86 0.1634 0.3971 0.0850 0.0350 1.274 16.063 11.960 950.192 1.815 53.197 5.709 0.41 239229. 0.5651 18.13 0.1868 0.4397 0.0823 0.0350 1.274 16.058 11.586 949.916 1.814 51.534 5.532 0.41 239491. 0.5390 20.40 0.2101 0.4793 0.0795 0.0349 1.270 16.004 11.188 946.733 1.808 49.764 5.360 0.41 239768. 0.5132 22.66 0.2335 0.5159 0.0765 0.0346 1.261 15.897 10.766 940.400 1.796 47.887 5.193 0.41 240062. 0.4877 24.93 0.2568 0.5497 0.0734 0.0343 1.248 15.734 10.321 930.752 1.778 45.909 5.030 0.41 240372. 0.4625 27.20 0.2802 0.5808 0.0700 0.0338 1.231 15.513 9.855 917.682 1.753 43.836 4.871 0.41 240698. 0.4377 29.46 0.3035 0.6092 0.0666 0.0332 1.208 15.233 9.370 901.118 1.721 41.676 4.716 0.41 241042. 0.4132 31.73 0.3269 0.6349 0.0630 0.0324 1.181 14.893 8.866 880.996 1.683 39.434 4.564 0.41 241402. 0.3890 34.00 0.3502 0.6581 0.0593 0.0316 1.150 14.491 8.345 857.254 1.637 37.119 4.415 0.41 241779. 0.3651 36.26 0.3736 0.6785 0.0555 0.0306 1.113 14.028 7.809 829.830 1.585 34.734 4.268 0.41 242173. 0.3414 38.53 0.3969 0.6963 0.0516 0.0294 1.071 13.501 7.259 798.665 1.525 32.286 4.122 0.41 242585. 0.3179 40.80 0.4203 0.7112 0.0476 0.0281 1.024 12.910 6.695 763.698 1.459 29.780 3.976 0.41 243014. 0.2945 43.06 0.4436 0.7229 0.0435 0.0267 0.972 12.254 6.120 724.875 1.384 27.221 3.829 0.41 243461. 0.2711 45.33 0.4670 0.7311 0.0393 0.0251 0.915 11.531 5.533 682.151 1.303 24.612 3.679 0.41 243926. 0.2477 47.59 0.4903 0.7352 0.0351 0.0234 0.852 10.743 4.937 635.493 1.214 21.960 3.524 0.41 244409. 0.2241 49.86 0.5137 0.7344 0.0308 0.0215 0.784 9.887 4.332 584.887 1.117 19.270 3.360 0.41 244910. 0.2001 52.13 0.5370 0.7271 0.0264 0.0195 0.711 8.965 3.720 530.345 1.013 16.547 3.181 0.41 245430. 0.1756 54.39 0.5604 0.7110 0.0220 0.0174 0.633 7.977 3.102 471.908 0.901 13.797 2.981 0.41 245967. 0.1503 56.66 0.5837 0.6820 0.0176 0.0151 0.549 6.925 2.480 409.661 0.782 11.030 2.746 0.41 246523. 0.1237 58.93 0.6071 0.6325 0.0132 0.0127 0.461 5.811 1.855 343.736 0.656 8.253 2.448 0.41 247097. 0.0955 61.19 0.6304 0.5461 0.0088 0.0101 0.368 4.637 1.231 274.321 0.524 5.476 2.036 0.41 247688. 0.0647 63.46 0.6538 0.3814 0.0043 0.0074 0.270 3.408 0.609 201.621 0.385 2.711 1.371 0.42 248296. 0.0306 65.73 0.6771 -0.0284 -0.0002 0.0045 0.165 2.086 -0.027 123.390 0.236 -0.119 -0.099 0.42 248843. 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 0.1004 0.0331 2.085 21.898 20.342 1554.460 2.474 90.482 5.936 0.49 285337. 0.7663 2.72 0.0234 0.0688 0.0988 0.0336 2.113 22.193 20.012 1575.391 2.507 89.014 5.762 0.49 285534. 0.7377 5.45 0.0468 0.1335 0.0970 0.0340 2.139 22.465 19.656 1594.710 2.538 87.429 5.591 0.49 285746. 0.7094 8.17 0.0701 0.1942 0.0951 0.0344 2.162 22.708 19.273 1611.966 2.566 85.724 5.423 0.49 285974. 0.6814 10.89 0.0935 0.2512 0.0931 0.0347 2.181 22.915 18.860 1626.696 2.589 83.891 5.259 0.49 286218. 0.6537 13.62 0.1169 0.3044 0.0909 0.0349 2.197 23.080 18.418 1638.411 2.608 81.922 5.099 0.49 286480. 0.6263 16.34 0.1403 0.3541 0.0886 0.0351 2.208 23.195 17.943 1646.578 2.621 79.810 4.943 0.49 286760. 0.5992 19.06 0.1637 0.4004 0.0860 0.0352 2.214 23.253 17.434 1650.656 2.627 77.548 4.791 0.49 287057. 0.5725 21.79 0.1871 0.4435 0.0834 0.0352 2.213 23.245 16.891 1650.103 2.626 75.132 4.643 0.49 287374. 0.5462 24.51 0.2104 0.4835 0.0805 0.0350 2.205 23.165 16.312 1644.402 2.617 72.557 4.499 0.49 287709. 0.5201 27.24 0.2338 0.5206 0.0775 0.0348 2.190 23.006 15.698 1633.127 2.599 69.826 4.360 0.49 288064. 0.4944 29.96 0.2572 0.5548 0.0743 0.0344 2.167 22.764 15.051 1615.980 2.572 66.946 4.224 0.49 288438. 0.4691 32.68 0.2806 0.5864 0.0709 0.0339 2.136 22.438 14.372 1592.780 2.535 63.925 4.093 0.49 288832. 0.4441 35.41 0.3040 0.6153 0.0674 0.0333 2.097 22.024 13.664 1563.397 2.488 60.776 3.964 0.49 289246. 0.4194 38.13 0.3274 0.6416 0.0638 0.0326 2.049 21.521 12.929 1527.722 2.431 57.507 3.838 0.49 289680. 0.3950 40.85 0.3507 0.6654 0.0601 0.0317 1.992 20.928 12.169 1485.651 2.364 54.129 3.715 0.49 290135. 0.3710 43.58 0.3741 0.6866 0.0562 0.0306 1.927 20.244 11.387 1437.079 2.287 50.650 3.594 0.49 290610. 0.3471 46.30 0.3975 0.7051 0.0522 0.0294 1.853 19.467 10.584 1381.900 2.199 47.077 3.474 0.49 291107. 0.3235 49.02 0.4209 0.7209 0.0482 0.0281 1.770 18.595 9.761 1320.012 2.101 43.419 3.354 0.49 291624. 0.3000 51.75 0.4443 0.7336 0.0440 0.0267 1.678 17.627 8.921 1251.322 1.992 39.682 3.234 0.49 292163. 0.2765 54.47 0.4677 0.7430 0.0398 0.0251 1.577 16.563 8.065 1175.751 1.871 35.874 3.111 0.49 292723. 0.2529 57.19 0.4910 0.7484 0.0355 0.0233 1.466 15.401 7.194 1093.244 1.740 32.000 2.985 0.49 293305. 0.2292 59.92 0.5144 0.7491 0.0311 0.0214 1.346 14.140 6.311 1003.776 1.598 28.071 2.852 0.49 293909. 0.2050 62.64 0.5378 0.7436 0.0267 0.0193 1.217 12.782 5.417 907.368 1.444 24.093 2.708 0.49 294534. 0.1804 65.36 0.5612 0.7296 0.0223 0.0171 1.078 11.327 4.514 804.096 1.280 20.076 2.546 0.50 295181. 0.1548 68.09 0.5846 0.7031 0.0178 0.0148 0.931 9.778 3.604 694.109 1.105 16.033 2.355 0.50 295850. 0.1280 70.81 0.6079 0.6562 0.0133 0.0123 0.775 8.137 2.692 577.646 0.919 11.975 2.114 0.50 296541. 0.0993 73.54 0.6313 0.5720 0.0088 0.0097 0.610 6.410 1.780 455.044 0.724 7.918 1.774 0.50 297253. 0.0678 76.26 0.6547 0.4045 0.0043 0.0070 0.438 4.602 0.871 326.660 0.520 3.876 1.210 0.50 297984. 0.0323 78.98 0.6781 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 0.1018 0.0335 3.349 30.156 28.072 2497.489 3.407 124.863 5.098 0.57 332850. 0.7731 3.18 0.0234 0.0689 0.1002 0.0340 3.395 30.567 27.623 2531.515 3.453 122.866 4.949 0.57 333081. 0.7445 6.35 0.0468 0.1338 0.0984 0.0344 3.437 30.946 27.138 2562.895 3.496 120.709 4.803 0.57 333330. 0.7161 9.53 0.0701 0.1947 0.0965 0.0348 3.474 31.284 26.615 2590.893 3.534 118.383 4.659 0.57 333598. 0.6880 12.71 0.0935 0.2517 0.0945 0.0351 3.506 31.572 26.052 2614.759 3.567 115.879 4.519 0.57 333885. 0.6602 15.88 0.1169 0.3051 0.0923 0.0353 3.532 31.801 25.447 2633.697 3.593 113.187 4.382 0.57 334192. 0.6328 19.06 0.1403 0.3550 0.0899 0.0355 3.549 31.960 24.797 2646.856 3.611 110.295 4.249 0.57 334520. 0.6056 22.24 0.1636 0.4016 0.0874 0.0356 3.558 32.038 24.100 2653.356 3.620 107.195 4.120 0.57 334870. 0.5789 25.41 0.1870 0.4449 0.0847 0.0356 3.557 32.026 23.354 2652.316 3.618 103.880 3.994 0.57 335241. 0.5524 28.59 0.2104 0.4852 0.0818 0.0355 3.544 31.912 22.559 2642.902 3.605 100.344 3.872 0.57 335634. 0.5263 31.77 0.2338 0.5226 0.0787 0.0352 3.519 31.689 21.715 2624.417 3.580 96.590 3.753 0.57 336049. 0.5006 34.94 0.2571 0.5573 0.0755 0.0348 3.482 31.350 20.824 2596.379 3.542 92.626 3.638 0.57 336488. 0.4752 38.12 0.2805 0.5892 0.0721 0.0343 3.431 30.893 19.889 2558.488 3.490 88.467 3.526 0.57 336949. 0.4501 41.30 0.3039 0.6186 0.0686 0.0337 3.367 30.314 18.914 2510.553 3.425 84.128 3.417 0.57 337434. 0.4254 44.47 0.3273 0.6455 0.0649 0.0329 3.289 29.612 17.901 2452.395 3.346 79.622 3.311 0.57 337942. 0.4009 47.65 0.3506 0.6698 0.0611 0.0320 3.197 28.784 16.853 2383.866 3.252 74.963 3.207 0.57 338474. 0.3768 50.83 0.3740 0.6917 0.0572 0.0309 3.091 27.830 15.774 2304.797 3.144 70.162 3.104 0.57 339031. 0.3529 54.00 0.3974 0.7109 0.0532 0.0297 2.970 26.746 14.665 2215.023 3.022 65.231 3.003 0.57 339611. 0.3292 57.18 0.4208 0.7275 0.0491 0.0284 2.835 25.531 13.530 2114.393 2.884 60.181 2.902 0.57 340216. 0.3056 60.36 0.4441 0.7412 0.0449 0.0269 2.686 24.183 12.370 2002.755 2.732 55.020 2.801 0.57 340846. 0.2820 63.53 0.4675 0.7517 0.0406 0.0252 2.521 22.700 11.187 1879.987 2.565 49.759 2.699 0.58 341500. 0.2584 66.71 0.4909 0.7585 0.0362 0.0234 2.341 21.082 9.984 1746.001 2.382 44.408 2.594 0.58 342180. 0.2346 69.88 0.5143 0.7607 0.0318 0.0215 2.147 19.329 8.763 1600.761 2.184 38.977 2.483 0.58 342885. 0.2104 73.06 0.5377 0.7571 0.0273 0.0194 1.937 17.439 7.526 1444.293 1.970 33.477 2.364 0.58 343615. 0.1856 76.24 0.5610 0.7454 0.0228 0.0171 1.712 15.416 6.278 1276.722 1.742 27.923 2.230 0.58 344370. 0.1599 79.41 0.5844 0.7218 0.0182 0.0147 1.473 13.261 5.020 1098.285 1.498 22.330 2.073 0.58 345151. 0.1330 82.59 0.6078 0.6786 0.0136 0.0122 1.219 10.980 3.758 909.369 1.241 16.715 1.874 0.58 345957. 0.1040 85.77 0.6312 0.5990 0.0090 0.0095 0.953 8.579 2.495 710.518 0.969 11.100 1.593 0.58 346788. 0.0720 88.94 0.6545 0.4357 0.0045 0.0067 0.674 6.065 1.237 502.318 0.685 5.504 1.117 0.58 347640. 0.0356 92.12 0.6779 -0.0508 -0.0003 0.0037 0.367 3.304 -0.076 273.630 0.373 -0.338 -0.126 0.58 348312. 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 0.1035 0.0342 5.095 40.140 37.282 3799.270 4.535 165.831 4.451 0.65 380338. 0.7779 3.64 0.0234 0.0689 0.1019 0.0346 5.165 40.693 36.697 3851.589 4.597 163.227 4.321 0.65 380604. 0.7493 7.27 0.0468 0.1337 0.1001 0.0351 5.230 41.202 36.063 3899.760 4.655 160.406 4.194 0.65 380892. 0.7209 10.91 0.0702 0.1946 0.0982 0.0354 5.287 41.655 35.377 3942.650 4.706 157.359 4.070 0.65 381201. 0.6929 14.54 0.0936 0.2517 0.0962 0.0358 5.336 42.040 34.638 3979.104 4.750 154.071 3.948 0.65 381532. 0.6651 18.18 0.1170 0.3052 0.0940 0.0360 5.375 42.345 33.842 4007.904 4.784 150.529 3.830 0.65 381887. 0.6377 21.81 0.1404 0.3552 0.0916 0.0362 5.401 42.554 32.985 4027.737 4.808 146.719 3.715 0.65 382265. 0.6106 25.45 0.1639 0.4019 0.0890 0.0363 5.414 42.655 32.065 4037.256 4.819 142.627 3.602 0.65 382668. 0.5839 29.08 0.1873 0.4454 0.0863 0.0363 5.411 42.632 31.080 4035.114 4.817 138.245 3.494 0.65 383096. 0.5575 32.72 0.2107 0.4860 0.0834 0.0361 5.391 42.473 30.028 4020.033 4.799 133.564 3.388 0.65 383549. 0.5314 36.35 0.2341 0.5236 0.0803 0.0359 5.352 42.165 28.909 3990.933 4.764 128.588 3.286 0.65 384028. 0.5056 39.99 0.2575 0.5586 0.0770 0.0355 5.293 41.702 27.727 3947.080 4.711 123.328 3.186 0.65 384533. 0.4802 43.62 0.2809 0.5909 0.0735 0.0350 5.214 41.078 26.485 3888.026 4.641 117.804 3.090 0.65 385065. 0.4551 47.26 0.3043 0.6207 0.0699 0.0343 5.114 40.291 25.188 3813.492 4.552 112.035 2.996 0.65 385623. 0.4303 50.90 0.3277 0.6480 0.0662 0.0335 4.993 39.337 23.840 3723.241 4.444 106.042 2.904 0.65 386208. 0.4059 54.53 0.3511 0.6729 0.0623 0.0325 4.851 38.215 22.446 3617.045 4.318 99.841 2.815 0.65 386820. 0.3817 58.17 0.3745 0.6953 0.0583 0.0314 4.686 36.922 21.009 3494.672 4.171 93.450 2.727 0.66 387460. 0.3577 61.80 0.3979 0.7153 0.0542 0.0302 4.500 35.456 19.533 3355.886 4.006 86.882 2.640 0.66 388127. 0.3340 65.44 0.4213 0.7326 0.0500 0.0288 4.292 33.814 18.020 3200.464 3.820 80.152 2.554 0.66 388822. 0.3103 69.07 0.4448 0.7472 0.0457 0.0272 4.061 31.994 16.473 3028.196 3.615 73.274 2.467 0.66 389546. 0.2866 72.71 0.4682 0.7586 0.0414 0.0255 3.807 29.994 14.896 2838.900 3.389 66.259 2.380 0.66 390297. 0.2629 76.34 0.4916 0.7665 0.0369 0.0237 3.530 27.813 13.292 2632.448 3.142 59.122 2.290 0.66 391078. 0.2390 79.98 0.5150 0.7700 0.0324 0.0217 3.230 25.450 11.663 2408.784 2.875 51.876 2.196 0.66 391887. 0.2147 83.61 0.5384 0.7679 0.0278 0.0195 2.907 22.905 10.013 2167.957 2.588 44.537 2.095 0.66 392724. 0.1897 87.25 0.5618 0.7580 0.0232 0.0172 2.562 20.181 8.346 1910.156 2.280 37.123 1.982 0.66 393591. 0.1639 90.88 0.5852 0.7366 0.0185 0.0147 2.194 17.282 6.667 1635.754 1.953 29.655 1.849 0.66 394486. 0.1366 94.52 0.6086 0.6959 0.0138 0.0121 1.804 14.214 4.981 1345.346 1.606 22.156 1.679 0.66 395411. 0.1073 98.15 0.6320 0.6184 0.0091 0.0093 1.394 10.986 3.295 1039.778 1.241 14.655 1.437 0.66 396363. 0.0747 101.79 0.6554 0.4537 0.0045 0.0065 0.965 7.606 1.614 719.949 0.859 7.178 1.017 0.66 397340. 0.0370 105.43 0.6788 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 0.1056 0.0352 7.472 52.325 48.145 5571.632 5.912 214.151 3.919 0.73 427791. 0.7784 4.10 0.0235 0.0685 0.1040 0.0356 7.571 53.019 47.408 5645.501 5.990 210.869 3.809 0.73 428094. 0.7506 8.21 0.0470 0.1331 0.1022 0.0361 7.662 53.660 46.605 5713.726 6.062 207.301 3.700 0.73 428422. 0.7229 12.31 0.0704 0.1938 0.1003 0.0365 7.744 54.231 45.736 5774.554 6.127 203.434 3.592 0.73 428774. 0.6954 16.41 0.0939 0.2509 0.0983 0.0368 7.813 54.716 44.795 5826.208 6.182 199.247 3.487 0.73 429152. 0.6681 20.51 0.1174 0.3044 0.0960 0.0370 7.868 55.097 43.778 5866.810 6.225 194.723 3.385 0.73 429557. 0.6410 24.62 0.1409 0.3544 0.0936 0.0372 7.904 55.356 42.681 5894.357 6.254 189.844 3.284 0.73 429989. 0.6141 28.72 0.1644 0.4012 0.0910 0.0373 7.921 55.473 41.500 5906.759 6.267 184.592 3.187 0.73 430448. 0.5876 32.82 0.1879 0.4449 0.0883 0.0373 7.915 55.427 40.232 5901.928 6.262 178.954 3.092 0.73 430936. 0.5613 36.93 0.2113 0.4856 0.0853 0.0371 7.882 55.202 38.876 5877.905 6.237 172.921 3.000 0.73 431453. 0.5354 41.03 0.2348 0.5235 0.0821 0.0368 7.822 54.780 37.432 5833.029 6.189 166.496 2.911 0.73 431998. 0.5097 45.13 0.2583 0.5588 0.0788 0.0364 7.733 54.152 35.902 5766.183 6.118 159.693 2.824 0.73 432574. 0.4843 49.23 0.2818 0.5914 0.0752 0.0358 7.613 53.312 34.294 5676.747 6.023 152.540 2.740 0.73 433179. 0.4593 53.34 0.3053 0.6216 0.0715 0.0351 7.462 52.257 32.613 5564.338 5.904 145.063 2.658 0.74 433814. 0.4345 57.44 0.3288 0.6494 0.0677 0.0343 7.280 50.983 30.865 5428.668 5.760 137.289 2.579 0.74 434480. 0.4101 61.54 0.3522 0.6748 0.0637 0.0333 7.066 49.487 29.056 5269.451 5.591 129.241 2.501 0.74 435176. 0.3859 65.64 0.3757 0.6978 0.0596 0.0321 6.821 47.768 27.190 5086.354 5.397 120.941 2.425 0.74 435903. 0.3619 69.75 0.3992 0.7184 0.0554 0.0308 6.543 45.821 25.272 4879.055 5.177 112.408 2.349 0.74 436661. 0.3380 73.85 0.4227 0.7364 0.0511 0.0293 6.232 43.644 23.305 4647.242 4.931 103.660 2.275 0.74 437451. 0.3143 77.95 0.4462 0.7518 0.0467 0.0277 5.888 41.234 21.294 4390.635 4.659 94.715 2.200 0.74 438272. 0.2905 82.06 0.4697 0.7641 0.0422 0.0259 5.510 38.589 19.242 4109.012 4.360 85.590 2.124 0.74 439125. 0.2667 86.16 0.4931 0.7729 0.0376 0.0240 5.099 35.708 17.154 3802.241 4.034 76.302 2.046 0.74 440011. 0.2426 90.26 0.5166 0.7775 0.0330 0.0219 4.654 32.591 15.034 3470.336 3.682 66.870 1.965 0.74 440928. 0.2181 94.36 0.5401 0.7765 0.0283 0.0197 4.175 29.240 12.885 3113.506 3.304 57.313 1.877 0.74 441878. 0.1929 98.47 0.5636 0.7678 0.0235 0.0173 3.664 25.659 10.714 2732.233 2.899 47.655 1.779 0.74 442860. 0.1666 102.57 0.5871 0.7471 0.0187 0.0147 3.121 21.857 8.526 2327.364 2.469 37.922 1.662 0.74 443875. 0.1389 106.67 0.6106 0.7064 0.0139 0.0120 2.548 17.845 6.328 1900.163 2.016 28.146 1.510 0.75 444922. 0.1088 110.78 0.6340 0.6262 0.0091 0.0092 1.948 13.640 4.129 1452.371 1.541 18.365 1.289 0.75 446000. 0.0750 114.88 0.6575 0.4486 0.0042 0.0062 1.322 9.258 1.936 985.844 1.046 8.611 0.891 0.75 447106. 0.0355 118.98 0.6810 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 0.1081 0.0383 11.153 70.295 60.865 8316.673 7.942 270.730 3.319 0.81 475193. 0.7412 4.54 0.0234 0.0646 0.1066 0.0386 11.240 70.841 59.976 8381.318 8.004 266.772 3.246 0.81 475533. 0.7195 9.07 0.0467 0.1262 0.1048 0.0388 11.316 71.325 59.004 8438.598 8.058 262.450 3.171 0.81 475899. 0.6973 13.61 0.0701 0.1848 0.1030 0.0391 11.381 71.731 57.946 8486.592 8.104 257.744 3.097 0.81 476293. 0.6748 18.15 0.0935 0.2405 0.1009 0.0392 11.430 72.040 56.796 8523.179 8.139 252.630 3.022 0.81 476716. 0.6520 22.69 0.1169 0.2932 0.0987 0.0393 11.460 72.233 55.549 8546.044 8.161 247.082 2.948 0.81 477168. 0.6289 27.22 0.1402 0.3430 0.0963 0.0394 11.469 72.290 54.199 8552.738 8.167 241.076 2.874 0.81 477650. 0.6057 31.76 0.1636 0.3900 0.0937 0.0393 11.453 72.188 52.741 8540.694 8.156 234.591 2.801 0.81 478164. 0.5822 36.30 0.1870 0.4342 0.0909 0.0392 11.408 71.905 51.171 8507.233 8.124 227.608 2.728 0.81 478708. 0.5586 40.84 0.2104 0.4756 0.0879 0.0389 11.331 71.419 49.486 8449.761 8.069 220.115 2.656 0.81 479284. 0.5349 45.37 0.2337 0.5143 0.0847 0.0385 11.219 70.711 47.687 8365.917 7.989 212.114 2.585 0.82 479893. 0.5110 49.91 0.2571 0.5504 0.0813 0.0380 11.069 69.765 45.778 8253.982 7.882 203.622 2.516 0.82 480534. 0.4872 54.45 0.2805 0.5841 0.0778 0.0373 10.880 68.572 43.766 8112.864 7.747 194.672 2.447 0.82 481207. 0.4633 58.99 0.3039 0.6153 0.0740 0.0366 10.650 67.126 41.659 7941.822 7.584 185.300 2.379 0.82 481914. 0.4395 63.52 0.3272 0.6440 0.0701 0.0356 10.380 65.422 39.465 7740.213 7.391 175.542 2.313 0.82 482654. 0.4158 68.06 0.3506 0.6704 0.0661 0.0346 10.068 63.454 37.192 7507.410 7.169 165.428 2.247 0.82 483427. 0.3922 72.60 0.3740 0.6945 0.0619 0.0333 9.713 61.220 34.844 7243.015 6.917 154.987 2.182 0.82 484234. 0.3687 77.14 0.3973 0.7159 0.0576 0.0320 9.317 58.725 32.429 6947.857 6.635 144.244 2.117 0.82 485075. 0.3451 81.67 0.4207 0.7346 0.0532 0.0305 8.880 55.968 29.951 6621.633 6.323 133.220 2.052 0.82 485950. 0.3214 86.21 0.4441 0.7503 0.0487 0.0288 8.399 52.937 27.414 6263.085 5.981 121.937 1.985 0.82 486860. 0.2975 90.75 0.4675 0.7629 0.0441 0.0270 7.874 49.629 24.824 5871.754 5.607 110.416 1.918 0.82 487805. 0.2735 95.29 0.4908 0.7715 0.0394 0.0251 7.307 46.053 22.185 5448.580 5.203 98.679 1.847 0.82 488784. 0.2490 99.82 0.5142 0.7752 0.0347 0.0230 6.697 42.211 19.503 4994.046 4.769 86.749 1.771 0.82 489799. 0.2239 104.36 0.5376 0.7723 0.0298 0.0208 6.047 38.114 16.783 4509.393 4.306 74.649 1.688 0.82 490848. 0.1979 108.90 0.5610 0.7602 0.0249 0.0184 5.359 33.779 14.030 3996.440 3.816 62.406 1.592 0.83 491933. 0.1707 113.44 0.5843 0.7341 0.0200 0.0159 4.637 29.223 11.253 3457.483 3.302 50.052 1.476 0.83 493054. 0.1417 117.97 0.6077 0.6853 0.0150 0.0133 3.883 24.473 8.459 2895.467 2.765 37.625 1.325 0.83 494209. 0.1103 122.51 0.6311 0.5957 0.0101 0.0107 3.103 19.560 5.659 2314.200 2.210 25.170 1.109 0.83 495399. 0.0755 127.05 0.6544 0.4209 0.0051 0.0079 2.303 14.518 2.862 1717.668 1.640 12.731 0.756 0.83 496620. 0.0366 131.58 0.6778 0.0008 0.0000 0.0050 1.451 9.143 0.003 1081.734 1.033 0.015 0.001 0.83 497741. 0.0000