390 lines
69 KiB
Plaintext
390 lines
69 KiB
Plaintext
20.5x10.5WPN (205x105WPN.dat)
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v2022-0915
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Simulation Date: 09/22/2022
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AIRFOIL AERO DATA GENERATED USING: POLAR DIAGRAMS
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====== PERFORMANCE DATA (versus advance ratio and MPH) ======
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DEFINITIONS:
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J=V/nD (advance ratio)
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Ct=T/(rho * n**2 * D**4) (thrust coef.)
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Cp=P/(rho * n**3 * D**5) (power coef.)
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Pe=Ct*J/Cp (efficiency)
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V (model speed in MPH)
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Mach (at prop tip)
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Reyn (at 75% of span)
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FOM (Figure of Merit)
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PROP RPM = 1000
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V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
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(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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PROP RPM = 2000
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V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
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(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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PROP RPM = 3000
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V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
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(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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PROP RPM = 4000
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V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
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(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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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
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PROP RPM = 5000
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V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
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(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
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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
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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
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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
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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
|
|
|
|
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