390 lines
69 KiB
Plaintext
390 lines
69 KiB
Plaintext
21.5x10WPN (215x10WPN.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 0.0847 0.0318 0.012 0.743 0.579 8.796 0.084 2.575 29.845 0.09 46061. 0.6191
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0.44 0.0216 0.0562 0.0832 0.0321 0.012 0.750 0.569 8.876 0.085 2.530 29.062 0.09 46088. 0.5976
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0.88 0.0433 0.1094 0.0816 0.0323 0.012 0.756 0.558 8.949 0.085 2.482 28.280 0.09 46117. 0.5760
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1.32 0.0649 0.1596 0.0800 0.0325 0.012 0.762 0.546 9.012 0.086 2.430 27.501 0.09 46148. 0.5543
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1.76 0.0866 0.2068 0.0781 0.0327 0.012 0.766 0.534 9.064 0.087 2.376 26.729 0.09 46182. 0.5326
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2.21 0.1082 0.2510 0.0762 0.0329 0.012 0.769 0.521 9.102 0.087 2.317 25.962 0.09 46217. 0.5109
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2.65 0.1299 0.2924 0.0742 0.0330 0.012 0.771 0.507 9.125 0.087 2.255 25.201 0.09 46256. 0.4893
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3.09 0.1515 0.3310 0.0720 0.0330 0.012 0.772 0.492 9.131 0.087 2.189 24.448 0.09 46296. 0.4676
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3.53 0.1732 0.3667 0.0697 0.0329 0.012 0.771 0.476 9.118 0.087 2.119 23.701 0.09 46339. 0.4461
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3.97 0.1948 0.3996 0.0673 0.0328 0.012 0.768 0.460 9.083 0.087 2.045 22.960 0.09 46385. 0.4245
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4.41 0.2165 0.4298 0.0647 0.0326 0.012 0.763 0.442 9.026 0.086 1.967 22.225 0.09 46434. 0.4030
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4.85 0.2381 0.4572 0.0620 0.0323 0.012 0.756 0.424 8.945 0.085 1.885 21.493 0.09 46485. 0.3816
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5.29 0.2598 0.4819 0.0592 0.0319 0.012 0.747 0.405 8.839 0.084 1.800 20.765 0.09 46539. 0.3602
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5.73 0.2814 0.5038 0.0563 0.0314 0.012 0.736 0.385 8.709 0.083 1.711 20.037 0.09 46596. 0.3389
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6.18 0.3031 0.5228 0.0533 0.0309 0.011 0.723 0.364 8.553 0.082 1.619 19.307 0.09 46655. 0.3176
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6.62 0.3247 0.5388 0.0501 0.0302 0.011 0.707 0.343 8.370 0.080 1.524 18.572 0.09 46718. 0.2965
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7.06 0.3464 0.5517 0.0469 0.0295 0.011 0.690 0.321 8.161 0.078 1.427 17.828 0.09 46783. 0.2753
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7.50 0.3680 0.5612 0.0436 0.0286 0.011 0.670 0.298 7.925 0.076 1.327 17.070 0.09 46852. 0.2542
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7.94 0.3897 0.5671 0.0403 0.0277 0.010 0.648 0.275 7.662 0.073 1.224 16.292 0.09 46923. 0.2330
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8.38 0.4113 0.5691 0.0368 0.0266 0.010 0.623 0.252 7.371 0.070 1.119 15.487 0.09 46997. 0.2118
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8.82 0.4330 0.5665 0.0333 0.0255 0.009 0.596 0.228 7.051 0.067 1.013 14.645 0.09 47075. 0.1905
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9.26 0.4546 0.5586 0.0297 0.0242 0.009 0.567 0.203 6.702 0.064 0.904 13.753 0.09 47155. 0.1691
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9.71 0.4762 0.5444 0.0261 0.0228 0.008 0.535 0.178 6.325 0.060 0.794 12.796 0.09 47239. 0.1474
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10.15 0.4979 0.5226 0.0224 0.0214 0.008 0.500 0.153 5.919 0.057 0.682 11.750 0.09 47325. 0.1254
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10.59 0.5195 0.4912 0.0187 0.0198 0.007 0.464 0.128 5.485 0.052 0.569 10.582 0.09 47415. 0.1032
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11.03 0.5412 0.4471 0.0150 0.0181 0.007 0.424 0.102 5.022 0.048 0.455 9.247 0.09 47508. 0.0807
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11.47 0.5628 0.3859 0.0112 0.0164 0.006 0.383 0.077 4.531 0.043 0.341 7.674 0.09 47604. 0.0579
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11.91 0.5845 0.3003 0.0074 0.0145 0.005 0.339 0.051 4.015 0.038 0.226 5.752 0.09 47703. 0.0354
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12.35 0.6061 0.1782 0.0037 0.0125 0.005 0.294 0.025 3.473 0.033 0.112 3.291 0.09 47805. 0.0142
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12.79 0.6278 -0.0046 -0.0001 0.0105 0.004 0.246 -0.001 2.905 0.028 -0.002 -0.081 0.09 47908. 0.0000
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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 0.0851 0.0287 0.085 2.690 2.328 63.645 0.304 10.354 16.589 0.17 92120. 0.6901
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0.89 0.0217 0.0626 0.0837 0.0290 0.086 2.719 2.287 64.349 0.307 10.174 16.123 0.17 92174. 0.6649
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1.77 0.0435 0.1217 0.0821 0.0293 0.087 2.747 2.244 64.992 0.310 9.982 15.662 0.17 92232. 0.6397
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2.66 0.0652 0.1772 0.0804 0.0296 0.088 2.771 2.198 65.560 0.313 9.777 15.206 0.17 92295. 0.6147
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3.54 0.0870 0.2293 0.0786 0.0298 0.089 2.791 2.149 66.037 0.315 9.557 14.757 0.17 92363. 0.5898
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4.43 0.1087 0.2780 0.0767 0.0300 0.089 2.806 2.096 66.406 0.317 9.322 14.315 0.17 92435. 0.5651
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5.32 0.1304 0.3235 0.0746 0.0301 0.089 2.817 2.040 66.651 0.318 9.073 13.881 0.17 92512. 0.5405
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6.20 0.1522 0.3658 0.0724 0.0301 0.090 2.821 1.980 66.754 0.319 8.807 13.454 0.17 92594. 0.5162
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7.09 0.1739 0.4050 0.0701 0.0301 0.089 2.819 1.917 66.698 0.318 8.526 13.034 0.17 92681. 0.4920
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7.97 0.1957 0.4413 0.0677 0.0300 0.089 2.809 1.850 66.469 0.317 8.228 12.622 0.17 92773. 0.4681
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8.86 0.2174 0.4746 0.0651 0.0298 0.089 2.791 1.779 66.051 0.315 7.914 12.217 0.17 92871. 0.4443
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9.75 0.2391 0.5050 0.0624 0.0295 0.088 2.765 1.705 65.435 0.312 7.584 11.819 0.17 92974. 0.4208
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10.63 0.2609 0.5326 0.0595 0.0292 0.087 2.731 1.628 64.613 0.309 7.240 11.426 0.17 93083. 0.3975
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11.52 0.2826 0.5574 0.0566 0.0287 0.085 2.687 1.547 63.582 0.304 6.883 11.038 0.17 93197. 0.3744
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12.40 0.3044 0.5793 0.0536 0.0281 0.084 2.634 1.464 62.335 0.298 6.512 10.653 0.17 93317. 0.3515
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13.29 0.3261 0.5984 0.0504 0.0275 0.082 2.572 1.378 60.867 0.291 6.130 10.270 0.17 93443. 0.3287
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14.18 0.3478 0.6144 0.0472 0.0267 0.079 2.501 1.290 59.175 0.283 5.737 9.886 0.17 93575. 0.3061
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15.06 0.3696 0.6273 0.0439 0.0258 0.077 2.420 1.199 57.252 0.273 5.334 9.500 0.17 93713. 0.2836
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15.95 0.3913 0.6368 0.0405 0.0249 0.074 2.328 1.106 55.096 0.263 4.921 9.108 0.17 93857. 0.2612
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16.83 0.4130 0.6425 0.0370 0.0238 0.071 2.227 1.012 52.701 0.252 4.499 8.706 0.17 94007. 0.2387
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17.72 0.4348 0.6440 0.0335 0.0226 0.067 2.116 0.915 50.064 0.239 4.070 8.289 0.17 94163. 0.2162
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18.61 0.4565 0.6404 0.0299 0.0213 0.063 1.994 0.817 47.182 0.225 3.633 7.851 0.17 94325. 0.1935
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19.49 0.4783 0.6309 0.0262 0.0199 0.059 1.862 0.717 44.055 0.210 3.189 7.382 0.17 94493. 0.1705
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20.38 0.5000 0.6137 0.0225 0.0184 0.055 1.719 0.616 40.682 0.194 2.741 6.870 0.17 94668. 0.1470
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21.26 0.5217 0.5867 0.0188 0.0167 0.050 1.566 0.514 37.064 0.177 2.287 6.293 0.17 94849. 0.1230
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22.15 0.5435 0.5459 0.0151 0.0150 0.045 1.403 0.412 33.206 0.159 1.831 5.622 0.17 95036. 0.0983
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23.04 0.5652 0.4853 0.0113 0.0131 0.039 1.230 0.308 29.114 0.139 1.372 4.806 0.17 95230. 0.0728
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23.92 0.5870 0.3937 0.0075 0.0112 0.033 1.048 0.205 24.798 0.118 0.913 3.754 0.17 95429. 0.0464
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24.81 0.6087 0.2488 0.0037 0.0091 0.027 0.857 0.102 20.269 0.097 0.455 2.288 0.17 95635. 0.0199
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25.69 0.6304 -0.0037 0.0000 0.0070 0.021 0.655 -0.001 15.492 0.074 -0.005 -0.033 0.17 95839. 0.0000
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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 0.0857 0.0276 0.277 5.816 5.270 206.443 0.657 23.442 11.579 0.26 138174. 0.7248
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1.33 0.0218 0.0657 0.0842 0.0279 0.280 5.886 5.179 208.918 0.665 23.037 11.244 0.26 138256. 0.6977
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2.66 0.0436 0.1275 0.0826 0.0282 0.283 5.950 5.082 211.189 0.672 22.603 10.914 0.26 138344. 0.6708
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4.00 0.0654 0.1855 0.0809 0.0285 0.286 6.007 4.977 213.200 0.679 22.139 10.589 0.26 138439. 0.6441
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5.33 0.0871 0.2399 0.0791 0.0287 0.288 6.055 4.866 214.900 0.684 21.643 10.270 0.26 138541. 0.6177
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6.66 0.1089 0.2907 0.0772 0.0289 0.290 6.092 4.747 216.230 0.688 21.113 9.956 0.26 138649. 0.5915
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7.99 0.1307 0.3381 0.0751 0.0290 0.291 6.118 4.620 217.134 0.691 20.548 9.650 0.26 138765. 0.5655
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9.32 0.1525 0.3822 0.0729 0.0291 0.292 6.129 4.485 217.551 0.692 19.947 9.350 0.26 138889. 0.5399
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10.66 0.1743 0.4231 0.0706 0.0291 0.292 6.126 4.341 217.424 0.692 19.310 9.056 0.26 139020. 0.5145
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11.99 0.1961 0.4609 0.0681 0.0290 0.291 6.105 4.190 216.696 0.690 18.635 8.769 0.26 139160. 0.4894
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13.32 0.2179 0.4957 0.0655 0.0288 0.289 6.066 4.030 215.318 0.685 17.924 8.489 0.26 139307. 0.4646
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14.65 0.2397 0.5276 0.0628 0.0285 0.286 6.008 3.862 213.256 0.679 17.177 8.214 0.26 139462. 0.4401
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15.98 0.2614 0.5567 0.0599 0.0281 0.282 5.930 3.687 210.484 0.670 16.398 7.944 0.26 139626. 0.4159
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17.32 0.2832 0.5829 0.0570 0.0277 0.278 5.832 3.504 206.982 0.659 15.587 7.679 0.26 139799. 0.3920
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18.65 0.3050 0.6064 0.0539 0.0271 0.272 5.712 3.316 202.734 0.645 14.748 7.418 0.26 139980. 0.3683
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19.98 0.3268 0.6271 0.0507 0.0264 0.265 5.571 3.121 197.721 0.629 13.881 7.159 0.26 140170. 0.3448
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21.31 0.3486 0.6448 0.0475 0.0257 0.257 5.407 2.920 191.926 0.611 12.990 6.902 0.26 140368. 0.3216
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22.64 0.3704 0.6596 0.0441 0.0248 0.249 5.222 2.715 185.331 0.590 12.076 6.644 0.26 140576. 0.2985
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23.98 0.3922 0.6711 0.0407 0.0238 0.239 5.013 2.505 177.922 0.566 11.140 6.385 0.26 140793. 0.2755
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25.31 0.4140 0.6790 0.0372 0.0227 0.228 4.781 2.290 169.682 0.540 10.184 6.120 0.26 141019. 0.2525
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26.64 0.4357 0.6830 0.0337 0.0215 0.215 4.525 2.071 160.601 0.511 9.211 5.848 0.26 141254. 0.2295
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27.97 0.4575 0.6823 0.0300 0.0201 0.202 4.245 1.848 150.668 0.480 8.221 5.564 0.26 141498. 0.2062
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29.30 0.4793 0.6758 0.0264 0.0187 0.188 3.941 1.622 139.878 0.445 7.216 5.261 0.26 141752. 0.1827
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30.64 0.5011 0.6621 0.0227 0.0171 0.172 3.613 1.394 128.231 0.408 6.199 4.930 0.26 142015. 0.1587
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31.97 0.5229 0.6387 0.0189 0.0155 0.155 3.261 1.163 115.734 0.368 5.172 4.557 0.26 142288. 0.1340
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33.30 0.5447 0.6016 0.0151 0.0137 0.137 2.885 0.930 102.400 0.326 4.138 4.121 0.26 142570. 0.1084
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34.63 0.5665 0.5437 0.0113 0.0118 0.118 2.486 0.697 88.253 0.281 3.100 3.581 0.26 142861. 0.0815
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35.96 0.5883 0.4517 0.0075 0.0098 0.098 2.066 0.463 73.328 0.233 2.060 2.865 0.26 143162. 0.0532
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37.29 0.6100 0.2959 0.0037 0.0077 0.077 1.625 0.230 57.664 0.184 1.024 1.810 0.26 143472. 0.0237
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38.63 0.6318 -0.0091 -0.0001 0.0055 0.055 1.157 -0.005 41.056 0.131 -0.022 -0.053 0.26 143773. 0.0000
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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 0.0864 0.0271 0.645 10.165 9.445 481.072 1.148 42.013 8.905 0.34 184222. 0.7463
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1.78 0.0218 0.0674 0.0849 0.0275 0.653 10.293 9.283 487.100 1.163 41.292 8.644 0.34 184332. 0.7181
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3.56 0.0436 0.1308 0.0833 0.0278 0.661 10.410 9.109 492.635 1.176 40.518 8.387 0.34 184450. 0.6902
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5.34 0.0655 0.1903 0.0816 0.0281 0.667 10.513 8.923 497.546 1.188 39.689 8.134 0.34 184577. 0.6625
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7.11 0.0873 0.2460 0.0798 0.0283 0.673 10.601 8.723 501.703 1.198 38.802 7.887 0.34 184714. 0.6351
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8.89 0.1091 0.2980 0.0778 0.0285 0.677 10.670 8.511 504.970 1.206 37.855 7.644 0.34 184859. 0.6081
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10.67 0.1309 0.3465 0.0758 0.0286 0.680 10.718 8.283 507.207 1.211 36.845 7.407 0.34 185015. 0.5813
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12.45 0.1527 0.3917 0.0735 0.0287 0.682 10.740 8.042 508.267 1.213 35.770 7.176 0.34 185180. 0.5549
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14.23 0.1746 0.4336 0.0712 0.0287 0.681 10.735 7.785 508.013 1.213 34.628 6.951 0.34 185356. 0.5288
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16.01 0.1964 0.4723 0.0687 0.0286 0.679 10.699 7.514 506.306 1.209 33.420 6.731 0.34 185543. 0.5031
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17.79 0.2182 0.5081 0.0661 0.0284 0.675 10.629 7.227 503.029 1.201 32.145 6.516 0.34 185740. 0.4777
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19.56 0.2400 0.5409 0.0633 0.0281 0.668 10.525 6.926 498.093 1.189 30.807 6.307 0.34 185949. 0.4526
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21.34 0.2618 0.5710 0.0605 0.0277 0.659 10.384 6.612 491.440 1.173 29.409 6.102 0.34 186168. 0.4278
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23.12 0.2836 0.5982 0.0575 0.0273 0.648 10.207 6.285 483.020 1.153 27.955 5.902 0.34 186399. 0.4034
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24.90 0.3055 0.6227 0.0544 0.0267 0.634 9.990 5.946 472.790 1.129 26.449 5.705 0.34 186642. 0.3793
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26.68 0.3273 0.6445 0.0512 0.0260 0.618 9.735 5.597 460.707 1.100 24.895 5.510 0.34 186896. 0.3554
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28.46 0.3491 0.6634 0.0479 0.0252 0.599 9.440 5.237 446.728 1.066 23.296 5.318 0.34 187162. 0.3318
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30.24 0.3709 0.6794 0.0445 0.0243 0.578 9.103 4.869 430.811 1.028 21.655 5.126 0.34 187440. 0.3084
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32.01 0.3927 0.6924 0.0411 0.0233 0.554 8.725 4.491 412.918 0.986 19.976 4.933 0.34 187730. 0.2850
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33.79 0.4146 0.7019 0.0375 0.0222 0.527 8.305 4.105 393.013 0.938 18.261 4.738 0.34 188032. 0.2618
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35.57 0.4364 0.7077 0.0340 0.0209 0.498 7.841 3.713 371.064 0.886 16.513 4.538 0.34 188346. 0.2384
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37.35 0.4582 0.7090 0.0303 0.0196 0.465 7.333 3.313 347.051 0.829 14.737 4.330 0.35 188673. 0.2149
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39.13 0.4800 0.7049 0.0266 0.0181 0.430 6.782 2.908 320.961 0.766 12.934 4.109 0.35 189013. 0.1911
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40.91 0.5018 0.6938 0.0228 0.0165 0.393 6.187 2.498 292.791 0.699 11.109 3.869 0.35 189365. 0.1667
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42.69 0.5237 0.6734 0.0191 0.0148 0.352 5.548 2.083 262.559 0.627 9.266 3.599 0.35 189729. 0.1416
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44.46 0.5455 0.6396 0.0152 0.0130 0.309 4.866 1.666 230.299 0.550 7.410 3.281 0.35 190107. 0.1155
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46.24 0.5673 0.5848 0.0114 0.0111 0.263 4.143 1.247 196.070 0.468 5.546 2.884 0.35 190497. 0.0878
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48.02 0.5891 0.4941 0.0076 0.0090 0.215 3.380 0.828 159.958 0.382 3.681 2.347 0.35 190899. 0.0582
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49.80 0.6109 0.3323 0.0037 0.0069 0.164 2.579 0.410 122.057 0.291 1.822 1.522 0.35 191312. 0.0266
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51.58 0.6328 -0.0181 -0.0001 0.0046 0.109 1.725 -0.014 81.618 0.195 -0.064 -0.080 0.35 191705. 0.0000
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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 0.0873 0.0270 1.255 15.818 14.912 935.753 1.787 66.330 7.228 0.43 230261. 0.7611
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2.22 0.0218 0.0684 0.0858 0.0274 1.271 16.022 14.658 947.793 1.810 65.201 7.015 0.43 230399. 0.7323
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4.45 0.0437 0.1327 0.0842 0.0277 1.286 16.209 14.386 958.847 1.831 63.987 6.805 0.43 230547. 0.7037
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6.67 0.0655 0.1931 0.0825 0.0280 1.299 16.375 14.093 968.654 1.850 62.686 6.599 0.43 230707. 0.6755
|
|
8.90 0.0873 0.2496 0.0807 0.0282 1.310 16.515 13.780 976.957 1.866 61.293 6.398 0.43 230878. 0.6475
|
|
11.12 0.1092 0.3023 0.0787 0.0284 1.319 16.625 13.445 983.487 1.878 59.804 6.201 0.43 231061. 0.6200
|
|
13.35 0.1310 0.3516 0.0766 0.0285 1.325 16.701 13.088 987.958 1.887 58.216 6.009 0.43 231257. 0.5927
|
|
15.57 0.1528 0.3974 0.0744 0.0286 1.328 16.737 12.708 990.086 1.891 56.524 5.822 0.43 231465. 0.5659
|
|
17.80 0.1747 0.4400 0.0720 0.0286 1.327 16.729 12.304 989.592 1.890 54.727 5.639 0.43 231686. 0.5393
|
|
20.02 0.1965 0.4794 0.0695 0.0285 1.323 16.671 11.876 986.205 1.884 52.823 5.462 0.43 231920. 0.5132
|
|
22.24 0.2183 0.5158 0.0669 0.0283 1.314 16.561 11.424 979.687 1.871 50.814 5.289 0.43 232168. 0.4874
|
|
24.47 0.2401 0.5493 0.0641 0.0280 1.301 16.395 10.949 969.864 1.852 48.703 5.121 0.43 232429. 0.4620
|
|
26.69 0.2620 0.5800 0.0612 0.0276 1.283 16.171 10.453 956.613 1.827 46.497 4.956 0.43 232705. 0.4369
|
|
28.92 0.2838 0.6080 0.0582 0.0271 1.260 15.888 9.937 939.843 1.795 44.202 4.796 0.43 232994. 0.4122
|
|
31.14 0.3056 0.6333 0.0550 0.0266 1.233 15.543 9.403 919.465 1.756 41.825 4.638 0.43 233299. 0.3878
|
|
33.37 0.3275 0.6559 0.0518 0.0259 1.201 15.136 8.851 895.395 1.710 39.371 4.484 0.43 233617. 0.3637
|
|
35.59 0.3493 0.6757 0.0485 0.0251 1.163 14.665 8.284 867.548 1.657 36.845 4.331 0.43 233951. 0.3399
|
|
37.82 0.3711 0.6928 0.0451 0.0241 1.121 14.129 7.701 835.843 1.596 34.254 4.179 0.43 234299. 0.3162
|
|
40.04 0.3930 0.7069 0.0416 0.0231 1.073 13.527 7.105 800.201 1.528 31.601 4.027 0.43 234662. 0.2927
|
|
42.26 0.4148 0.7177 0.0380 0.0220 1.020 12.857 6.495 760.552 1.453 28.892 3.874 0.43 235041. 0.2692
|
|
44.49 0.4366 0.7250 0.0344 0.0207 0.961 12.118 5.875 716.835 1.369 26.130 3.717 0.43 235435. 0.2457
|
|
46.71 0.4585 0.7280 0.0307 0.0193 0.897 11.309 5.243 669.008 1.278 23.322 3.555 0.43 235845. 0.2219
|
|
48.94 0.4803 0.7259 0.0269 0.0178 0.827 10.431 4.603 617.042 1.178 20.473 3.383 0.43 236270. 0.1979
|
|
51.16 0.5021 0.7172 0.0231 0.0162 0.752 9.482 3.954 560.938 1.071 17.589 3.197 0.43 236711. 0.1734
|
|
53.39 0.5240 0.6995 0.0193 0.0145 0.671 8.464 3.299 500.725 0.956 14.675 2.989 0.43 237167. 0.1480
|
|
55.61 0.5458 0.6687 0.0154 0.0126 0.585 7.378 2.640 436.474 0.834 11.741 2.743 0.43 237639. 0.1215
|
|
57.84 0.5676 0.6174 0.0116 0.0106 0.494 6.226 1.977 368.304 0.703 8.794 2.435 0.43 238127. 0.0934
|
|
60.06 0.5894 0.5296 0.0077 0.0086 0.397 5.010 1.314 296.384 0.566 5.846 2.011 0.43 238631. 0.0629
|
|
62.28 0.6113 0.3661 0.0038 0.0064 0.296 3.734 0.653 220.908 0.422 2.905 1.341 0.43 239149. 0.0295
|
|
64.51 0.6331 -0.0179 -0.0001 0.0040 0.188 2.368 -0.020 140.105 0.268 -0.087 -0.063 0.44 239632. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 6000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.0884 0.0272 2.180 22.903 21.755 1625.798 2.588 96.767 6.069 0.51 276286. 0.7719
|
|
2.69 0.0220 0.0693 0.0869 0.0275 2.209 23.204 21.386 1647.188 2.622 95.127 5.889 0.51 276454. 0.7426
|
|
5.37 0.0439 0.1345 0.0853 0.0279 2.235 23.480 20.989 1666.797 2.653 93.361 5.712 0.51 276635. 0.7135
|
|
8.06 0.0659 0.1956 0.0836 0.0282 2.258 23.725 20.563 1684.158 2.680 91.465 5.538 0.51 276829. 0.6847
|
|
10.74 0.0879 0.2528 0.0817 0.0284 2.278 23.931 20.106 1698.808 2.704 89.433 5.368 0.51 277037. 0.6563
|
|
13.43 0.1098 0.3063 0.0797 0.0286 2.293 24.093 19.617 1710.257 2.722 87.257 5.203 0.51 277260. 0.6283
|
|
16.12 0.1318 0.3562 0.0776 0.0287 2.304 24.202 19.095 1717.999 2.734 84.933 5.041 0.51 277498. 0.6006
|
|
18.80 0.1538 0.4026 0.0753 0.0288 2.309 24.251 18.538 1721.526 2.740 82.455 4.884 0.51 277751. 0.5734
|
|
21.49 0.1757 0.4457 0.0729 0.0288 2.307 24.234 17.945 1720.330 2.738 79.821 4.731 0.51 278020. 0.5465
|
|
24.17 0.1977 0.4857 0.0704 0.0287 2.298 24.144 17.317 1713.937 2.728 77.027 4.583 0.51 278305. 0.5200
|
|
26.86 0.2197 0.5226 0.0677 0.0285 2.282 23.975 16.654 1701.918 2.709 74.076 4.438 0.51 278606. 0.4939
|
|
29.54 0.2416 0.5567 0.0649 0.0282 2.258 23.722 15.956 1683.966 2.680 70.974 4.298 0.51 278924. 0.4681
|
|
32.23 0.2636 0.5879 0.0619 0.0277 2.226 23.383 15.227 1659.872 2.642 67.731 4.161 0.51 279259. 0.4427
|
|
34.92 0.2856 0.6165 0.0588 0.0272 2.185 22.954 14.469 1629.470 2.593 64.356 4.027 0.51 279612. 0.4177
|
|
37.60 0.3075 0.6424 0.0556 0.0266 2.136 22.435 13.682 1592.611 2.535 60.860 3.897 0.51 279982. 0.3930
|
|
40.29 0.3295 0.6656 0.0523 0.0259 2.077 21.823 12.871 1549.149 2.466 57.249 3.768 0.51 280369. 0.3686
|
|
42.97 0.3515 0.6861 0.0489 0.0251 2.010 21.116 12.035 1498.934 2.386 53.534 3.642 0.52 280774. 0.3445
|
|
45.66 0.3734 0.7039 0.0454 0.0241 1.934 20.311 11.178 1441.823 2.295 49.720 3.516 0.52 281198. 0.3206
|
|
48.35 0.3954 0.7187 0.0419 0.0230 1.847 19.407 10.300 1377.677 2.193 45.815 3.391 0.52 281639. 0.2967
|
|
51.03 0.4174 0.7304 0.0382 0.0218 1.752 18.403 9.404 1306.375 2.079 41.827 3.265 0.52 282100. 0.2730
|
|
53.72 0.4393 0.7386 0.0345 0.0205 1.647 17.296 8.490 1227.810 1.954 37.762 3.136 0.52 282578. 0.2492
|
|
56.40 0.4613 0.7426 0.0307 0.0191 1.531 16.086 7.560 1141.908 1.817 33.629 3.003 0.52 283076. 0.2251
|
|
59.09 0.4833 0.7415 0.0269 0.0175 1.406 14.772 6.617 1048.625 1.669 29.434 2.862 0.52 283592. 0.2008
|
|
61.78 0.5052 0.7338 0.0230 0.0158 1.271 13.354 5.663 947.968 1.509 25.188 2.709 0.52 284128. 0.1758
|
|
64.46 0.5272 0.7170 0.0191 0.0140 1.126 11.833 4.699 839.998 1.337 20.900 2.537 0.52 284682. 0.1500
|
|
67.15 0.5492 0.6867 0.0152 0.0121 0.972 10.211 3.728 724.854 1.154 16.581 2.333 0.52 285256. 0.1228
|
|
69.83 0.5711 0.6343 0.0112 0.0101 0.808 8.491 2.753 602.760 0.959 12.246 2.072 0.52 285848. 0.0937
|
|
72.52 0.5931 0.5409 0.0072 0.0079 0.636 6.678 1.778 474.040 0.754 7.910 1.701 0.52 286460. 0.0619
|
|
75.20 0.6151 0.3556 0.0033 0.0057 0.455 4.776 0.806 339.015 0.540 3.586 1.079 0.52 287087. 0.0264
|
|
77.89 0.6370
|
|
|
|
|
|
|
|
PROP RPM = 7000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.0899 0.0276 3.510 31.607 30.091 2617.635 3.571 133.846 5.214 0.60 322294. 0.7799
|
|
3.12 0.0219 0.0692 0.0884 0.0279 3.557 32.025 29.591 2652.270 3.618 131.622 5.060 0.60 322490. 0.7506
|
|
6.23 0.0437 0.1342 0.0868 0.0283 3.599 32.408 29.052 2683.998 3.661 129.224 4.910 0.60 322701. 0.7215
|
|
9.35 0.0656 0.1952 0.0850 0.0286 3.637 32.747 28.473 2712.068 3.700 126.647 4.762 0.60 322928. 0.6928
|
|
12.47 0.0874 0.2524 0.0832 0.0288 3.669 33.033 27.851 2735.739 3.732 123.881 4.618 0.60 323172. 0.6644
|
|
15.59 0.1093 0.3059 0.0812 0.0290 3.693 33.256 27.185 2754.222 3.757 120.917 4.477 0.60 323432. 0.6364
|
|
18.70 0.1311 0.3558 0.0790 0.0291 3.710 33.407 26.472 2766.711 3.774 117.747 4.340 0.60 323709. 0.6088
|
|
21.82 0.1530 0.4024 0.0768 0.0292 3.718 33.476 25.712 2772.392 3.782 114.365 4.206 0.60 324004. 0.5816
|
|
24.94 0.1748 0.4457 0.0744 0.0292 3.715 33.452 24.903 2770.465 3.779 110.766 4.077 0.60 324317. 0.5547
|
|
28.05 0.1967 0.4860 0.0718 0.0291 3.701 33.328 24.044 2760.160 3.765 106.947 3.951 0.60 324649. 0.5283
|
|
31.17 0.2185 0.5232 0.0691 0.0289 3.675 33.094 23.136 2740.794 3.739 102.910 3.829 0.60 325000. 0.5022
|
|
34.29 0.2404 0.5577 0.0662 0.0285 3.637 32.745 22.181 2711.864 3.699 98.663 3.710 0.60 325370. 0.4764
|
|
37.41 0.2622 0.5894 0.0633 0.0281 3.585 32.276 21.182 2673.030 3.647 94.219 3.594 0.60 325760. 0.4511
|
|
40.52 0.2841 0.6185 0.0601 0.0276 3.519 31.684 20.142 2624.041 3.580 89.592 3.482 0.60 326169. 0.4260
|
|
43.64 0.3059 0.6450 0.0569 0.0270 3.439 30.967 19.064 2564.663 3.499 84.795 3.371 0.60 326599. 0.4014
|
|
46.76 0.3278 0.6690 0.0536 0.0263 3.345 30.122 17.950 2494.680 3.403 79.840 3.264 0.60 327049. 0.3770
|
|
49.88 0.3496 0.6903 0.0502 0.0254 3.237 29.147 16.803 2413.862 3.293 74.738 3.157 0.60 327519. 0.3529
|
|
52.99 0.3715 0.7091 0.0467 0.0244 3.114 28.037 15.625 2321.990 3.168 69.499 3.052 0.60 328010. 0.3290
|
|
56.11 0.3933 0.7250 0.0431 0.0234 2.976 26.792 14.419 2218.843 3.027 64.134 2.947 0.60 328522. 0.3052
|
|
59.23 0.4152 0.7380 0.0394 0.0222 2.822 25.408 13.186 2104.225 2.871 58.652 2.842 0.60 329055. 0.2814
|
|
62.34 0.4370 0.7477 0.0356 0.0208 2.652 23.883 11.929 1977.969 2.698 53.062 2.736 0.60 329610. 0.2576
|
|
65.46 0.4589 0.7535 0.0318 0.0194 2.467 22.217 10.651 1839.948 2.510 47.376 2.626 0.60 330186. 0.2336
|
|
68.58 0.4808 0.7547 0.0279 0.0178 2.266 20.407 9.353 1690.091 2.306 41.603 2.510 0.60 330784. 0.2093
|
|
71.70 0.5026 0.7498 0.0240 0.0161 2.050 18.455 8.039 1528.395 2.085 35.755 2.386 0.61 331404. 0.1844
|
|
74.81 0.5245 0.7367 0.0200 0.0143 1.817 16.360 6.710 1354.947 1.848 29.847 2.246 0.61 332045. 0.1587
|
|
77.93 0.5463 0.7115 0.0160 0.0123 1.569 14.127 5.372 1169.949 1.596 23.894 2.083 0.61 332708. 0.1316
|
|
81.05 0.5682 0.6665 0.0120 0.0103 1.306 11.758 4.027 973.742 1.328 17.913 1.876 0.61 333394. 0.1026
|
|
84.16 0.5900 0.5852 0.0080 0.0081 1.028 9.259 2.681 766.822 1.046 11.926 1.586 0.61 334100. 0.0708
|
|
87.28 0.6119 0.4225 0.0040 0.0058 0.737 6.638 1.338 549.750 0.750 5.953 1.104 0.61 334827. 0.0348
|
|
90.40 0.6337 -0.0220 -0.0001 0.0033 0.423 3.811 -0.039 315.588 0.431 -0.172 -0.056 0.61 335478. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 8000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.0916 0.0282 5.359 42.220 40.086 3996.115 4.770 178.303 4.550 0.68 368277. 0.7855
|
|
3.57 0.0219 0.0691 0.0902 0.0286 5.430 42.783 39.432 4049.383 4.834 175.393 4.417 0.68 368504. 0.7562
|
|
7.13 0.0438 0.1340 0.0885 0.0289 5.496 43.298 38.725 4098.084 4.892 172.250 4.286 0.68 368748. 0.7272
|
|
10.70 0.0656 0.1951 0.0868 0.0292 5.553 43.751 37.964 4141.051 4.943 168.863 4.158 0.68 369010. 0.6986
|
|
14.27 0.0875 0.2523 0.0849 0.0295 5.602 44.132 37.145 4177.114 4.986 165.220 4.033 0.68 369291. 0.6703
|
|
17.83 0.1094 0.3058 0.0829 0.0297 5.639 44.428 36.266 4205.068 5.019 161.309 3.912 0.68 369592. 0.6423
|
|
21.40 0.1313 0.3559 0.0808 0.0298 5.664 44.624 35.323 4223.665 5.042 157.119 3.793 0.68 369912. 0.6147
|
|
24.97 0.1532 0.4026 0.0785 0.0298 5.675 44.709 34.317 4231.663 5.051 152.641 3.678 0.68 370253. 0.5875
|
|
28.54 0.1750 0.4462 0.0760 0.0298 5.670 44.668 33.244 4227.830 5.047 147.868 3.566 0.68 370614. 0.5607
|
|
32.10 0.1969 0.4867 0.0734 0.0297 5.647 44.490 32.104 4210.995 5.027 142.797 3.458 0.68 370997. 0.5342
|
|
35.67 0.2188 0.5243 0.0706 0.0295 5.606 44.164 30.897 4180.116 4.990 137.429 3.353 0.68 371402. 0.5081
|
|
39.24 0.2407 0.5591 0.0677 0.0292 5.544 43.681 29.626 4134.417 4.935 131.777 3.250 0.68 371828. 0.4824
|
|
42.80 0.2626 0.5912 0.0647 0.0287 5.463 43.037 28.295 4073.396 4.862 125.857 3.151 0.69 372277. 0.4570
|
|
46.37 0.2844 0.6208 0.0615 0.0282 5.360 42.226 26.908 3996.686 4.771 119.688 3.054 0.69 372749. 0.4319
|
|
49.94 0.3063 0.6478 0.0582 0.0275 5.235 41.247 25.470 3903.960 4.660 113.289 2.959 0.69 373243. 0.4072
|
|
53.50 0.3282 0.6724 0.0548 0.0268 5.089 40.094 23.983 3794.904 4.530 106.676 2.866 0.69 373761. 0.3828
|
|
57.07 0.3501 0.6944 0.0513 0.0259 4.920 38.766 22.451 3669.194 4.380 99.864 2.775 0.69 374302. 0.3586
|
|
60.64 0.3720 0.7139 0.0477 0.0249 4.729 37.259 20.878 3526.510 4.209 92.867 2.685 0.69 374866. 0.3346
|
|
64.21 0.3938 0.7307 0.0440 0.0237 4.515 35.568 19.267 3366.525 4.018 85.699 2.596 0.69 375455. 0.3107
|
|
67.77 0.4157 0.7446 0.0403 0.0225 4.276 33.692 17.620 3188.946 3.807 78.372 2.506 0.69 376068. 0.2868
|
|
71.34 0.4376 0.7553 0.0364 0.0211 4.014 31.627 15.939 2993.515 3.573 70.899 2.415 0.69 376705. 0.2629
|
|
74.91 0.4595 0.7624 0.0325 0.0196 3.728 29.372 14.230 2780.042 3.318 63.293 2.322 0.69 377366. 0.2388
|
|
78.47 0.4814 0.7650 0.0286 0.0180 3.417 26.925 12.493 2548.427 3.042 55.570 2.224 0.69 378052. 0.2143
|
|
82.04 0.5032 0.7618 0.0245 0.0162 3.083 24.286 10.734 2298.669 2.744 47.744 2.118 0.69 378763. 0.1892
|
|
85.61 0.5251 0.7506 0.0205 0.0143 2.723 21.457 8.956 2030.908 2.424 39.835 2.000 0.69 379499. 0.1632
|
|
89.17 0.5470 0.7277 0.0164 0.0123 2.341 18.441 7.163 1745.457 2.083 31.862 1.861 0.69 380260. 0.1358
|
|
92.74 0.5689 0.6853 0.0123 0.0102 1.935 15.244 5.362 1442.868 1.722 23.851 1.686 0.69 381046. 0.1064
|
|
96.31 0.5908 0.6063 0.0081 0.0079 1.507 11.875 3.559 1123.966 1.342 15.828 1.436 0.69 381856. 0.0739
|
|
99.88 0.6126 0.4423 0.0040 0.0056 1.059 8.343 1.759 789.703 0.943 7.823 1.010 0.70 382688. 0.0365
|
|
103.44 0.6345
|
|
|
|
|
|
|
|
PROP RPM = 9000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.0939 0.0295 7.977 55.865 51.970 5948.592 6.312 231.164 3.963 0.77 414225. 0.7789
|
|
4.04 0.0220 0.0683 0.0924 0.0298 8.067 56.493 51.141 6015.456 6.383 227.473 3.856 0.77 414485. 0.7519
|
|
8.08 0.0440 0.1328 0.0908 0.0301 8.149 57.067 50.241 6076.492 6.447 223.470 3.750 0.77 414765. 0.7248
|
|
12.12 0.0661 0.1937 0.0890 0.0304 8.220 57.569 49.268 6130.022 6.504 219.142 3.645 0.77 415066. 0.6977
|
|
16.16 0.0881 0.2509 0.0871 0.0306 8.280 57.985 48.217 6174.278 6.551 214.470 3.542 0.77 415389. 0.6706
|
|
20.20 0.1101 0.3046 0.0851 0.0307 8.324 58.296 47.086 6207.439 6.586 209.438 3.441 0.77 415733. 0.6437
|
|
24.24 0.1321 0.3549 0.0829 0.0308 8.351 58.485 45.870 6227.548 6.608 204.030 3.341 0.77 416101. 0.6169
|
|
28.27 0.1542 0.4020 0.0805 0.0309 8.358 58.533 44.567 6232.672 6.613 198.233 3.243 0.77 416492. 0.5904
|
|
32.31 0.1762 0.4459 0.0780 0.0308 8.342 58.423 43.175 6220.884 6.601 192.040 3.148 0.77 416907. 0.5640
|
|
36.35 0.1982 0.4868 0.0753 0.0307 8.301 58.136 41.692 6190.328 6.568 185.447 3.055 0.77 417346. 0.5378
|
|
40.39 0.2202 0.5249 0.0725 0.0304 8.233 57.657 40.120 6139.320 6.514 178.454 2.964 0.77 417810. 0.5119
|
|
44.43 0.2423 0.5601 0.0695 0.0300 8.135 56.973 38.462 6066.562 6.437 171.079 2.876 0.77 418299. 0.4863
|
|
48.47 0.2643 0.5927 0.0663 0.0296 8.007 56.077 36.723 5971.151 6.336 163.344 2.789 0.77 418813. 0.4609
|
|
52.51 0.2863 0.6228 0.0631 0.0290 7.848 54.963 34.909 5852.473 6.210 155.276 2.705 0.77 419353. 0.4359
|
|
56.55 0.3083 0.6504 0.0597 0.0283 7.657 53.625 33.026 5709.983 6.058 146.901 2.623 0.77 419919. 0.4111
|
|
60.59 0.3303 0.6755 0.0561 0.0275 7.434 52.058 31.079 5543.184 5.882 138.240 2.543 0.77 420511. 0.3866
|
|
64.63 0.3524 0.6981 0.0525 0.0265 7.177 50.259 29.072 5351.618 5.678 129.314 2.464 0.77 421130. 0.3623
|
|
68.67 0.3744 0.7182 0.0488 0.0254 6.886 48.224 27.011 5134.921 5.448 120.143 2.386 0.77 421776. 0.3381
|
|
72.71 0.3964 0.7357 0.0450 0.0242 6.561 45.949 24.897 4892.706 5.191 110.744 2.308 0.77 422448. 0.3140
|
|
76.74 0.4184 0.7502 0.0411 0.0229 6.202 43.432 22.737 4624.660 4.907 101.133 2.230 0.78 423148. 0.2899
|
|
80.78 0.4405 0.7616 0.0371 0.0215 5.807 40.670 20.532 4330.587 4.595 91.327 2.150 0.78 423876. 0.2657
|
|
84.82 0.4625 0.7691 0.0330 0.0199 5.378 37.663 18.288 4010.417 4.255 81.344 2.068 0.78 424631. 0.2412
|
|
88.86 0.4845 0.7719 0.0289 0.0182 4.914 34.413 16.008 3664.322 3.888 71.201 1.981 0.78 425414. 0.2162
|
|
92.90 0.5065 0.7684 0.0247 0.0163 4.416 30.923 13.696 3292.752 3.494 60.921 1.887 0.78 426225. 0.1904
|
|
96.94 0.5286 0.7560 0.0205 0.0143 3.884 27.202 11.359 2896.469 3.073 50.527 1.779 0.78 427064. 0.1635
|
|
100.98 0.5506 0.7299 0.0163 0.0123 3.321 23.259 9.003 2476.611 2.628 40.046 1.649 0.78 427931. 0.1349
|
|
105.02 0.5726 0.6809 0.0120 0.0101 2.729 19.110 6.635 2034.799 2.159 29.510 1.479 0.78 428827. 0.1039
|
|
109.06 0.5946 0.5875 0.0077 0.0078 2.110 14.774 4.262 1573.157 1.669 18.958 1.229 0.78 429750. 0.0692
|
|
113.10 0.6166 0.3892 0.0034 0.0054 1.467 10.273 1.893 1093.867 1.161 8.421 0.785 0.78 430697. 0.0295
|
|
117.14 0.6387
|
|
|
|
|
|
|
|
PROP RPM = 10000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.0965 0.0341 12.658 79.783 65.981 9439.240 9.014 293.482 3.170 0.85 460125. 0.7022
|
|
4.48 0.0220 0.0612 0.0951 0.0342 12.689 79.977 64.979 9462.198 9.036 289.025 3.115 0.85 460417. 0.6846
|
|
8.96 0.0440 0.1201 0.0935 0.0342 12.708 80.095 63.885 9476.156 9.049 284.162 3.058 0.85 460731. 0.6664
|
|
13.44 0.0659 0.1767 0.0917 0.0342 12.712 80.123 62.697 9479.528 9.052 278.877 3.000 0.85 461069. 0.6477
|
|
17.91 0.0879 0.2310 0.0899 0.0342 12.700 80.048 61.408 9470.635 9.044 273.144 2.941 0.85 461432. 0.6284
|
|
22.39 0.1099 0.2829 0.0878 0.0341 12.670 79.854 60.014 9447.662 9.022 266.943 2.881 0.85 461819. 0.6086
|
|
26.87 0.1319 0.3323 0.0856 0.0340 12.617 79.524 58.510 9408.597 8.985 260.253 2.821 0.85 462232. 0.5883
|
|
31.35 0.1538 0.3793 0.0832 0.0338 12.540 79.040 56.893 9351.341 8.930 253.058 2.759 0.85 462670. 0.5675
|
|
35.83 0.1758 0.4238 0.0807 0.0335 12.436 78.384 55.159 9273.723 8.856 245.346 2.698 0.85 463136. 0.5463
|
|
40.31 0.1978 0.4658 0.0780 0.0331 12.302 77.537 53.307 9173.507 8.760 237.109 2.636 0.86 463628. 0.5247
|
|
44.79 0.2198 0.5053 0.0751 0.0327 12.134 76.480 51.337 9048.490 8.641 228.348 2.573 0.86 464148. 0.5027
|
|
49.27 0.2418 0.5423 0.0721 0.0321 11.931 75.199 49.254 8896.964 8.496 219.080 2.511 0.86 464696. 0.4805
|
|
53.74 0.2637 0.5769 0.0689 0.0315 11.691 73.686 47.063 8717.876 8.325 209.335 2.449 0.86 465271. 0.4580
|
|
58.22 0.2857 0.6091 0.0655 0.0307 11.413 71.933 44.773 8510.520 8.127 199.150 2.386 0.86 465875. 0.4354
|
|
62.70 0.3077 0.6388 0.0620 0.0299 11.096 69.935 42.392 8274.155 7.901 188.558 2.324 0.86 466508. 0.4125
|
|
67.18 0.3297 0.6660 0.0584 0.0289 10.739 67.685 39.926 8007.984 7.647 177.591 2.261 0.86 467169. 0.3896
|
|
71.66 0.3516 0.6905 0.0547 0.0279 10.345 65.201 37.382 7714.076 7.366 166.273 2.198 0.86 467859. 0.3664
|
|
76.14 0.3736 0.7118 0.0509 0.0267 9.916 62.497 34.764 7394.188 7.061 154.630 2.132 0.86 468579. 0.3428
|
|
80.62 0.3956 0.7294 0.0469 0.0255 9.454 59.587 32.078 7049.835 6.732 142.682 2.064 0.86 469329. 0.3187
|
|
85.10 0.4176 0.7428 0.0429 0.0241 8.960 56.471 29.328 6681.223 6.380 130.452 1.991 0.86 470108. 0.2940
|
|
89.57 0.4396 0.7519 0.0388 0.0227 8.425 53.104 26.521 6282.796 6.000 117.965 1.915 0.86 470917. 0.2688
|
|
94.05 0.4615 0.7558 0.0346 0.0211 7.852 49.487 23.661 5854.951 5.591 105.244 1.833 0.86 471757. 0.2431
|
|
98.53 0.4835 0.7532 0.0304 0.0195 7.240 45.630 20.753 5398.512 5.155 92.310 1.744 0.86 472627. 0.2166
|
|
103.01 0.5055 0.7419 0.0260 0.0177 6.591 41.544 17.803 4915.160 4.694 79.189 1.643 0.86 473528. 0.1890
|
|
107.49 0.5275 0.7186 0.0217 0.0159 5.910 37.252 14.817 4407.409 4.209 65.908 1.525 0.87 474459. 0.1600
|
|
111.97 0.5494 0.6775 0.0173 0.0140 5.202 32.786 11.803 3878.950 3.704 52.501 1.380 0.87 475422. 0.1293
|
|
116.45 0.5714 0.6092 0.0128 0.0120 4.470 28.174 8.770 3333.268 3.183 39.010 1.193 0.87 476415. 0.0964
|
|
120.93 0.5934 0.4964 0.0084 0.0100 3.721 23.454 5.729 2774.897 2.650 25.482 0.936 0.87 477438. 0.0611
|
|
125.40 0.6154 0.3037 0.0039 0.0080 2.961 18.664 2.690 2208.168 2.109 11.964 0.553 0.87 478489. 0.0247
|
|
129.88 0.6374
|
|
|
|
|
|
|