390 lines
69 KiB
Plaintext
390 lines
69 KiB
Plaintext
24x12E (24x12E.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 0.0825 0.0289 0.019 1.169 0.873 13.829 0.132 3.882 28.624 0.10 52921. 0.6538
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0.51 0.0223 0.0618 0.0811 0.0292 0.019 1.181 0.858 13.973 0.133 3.816 27.850 0.10 52952. 0.6307
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1.01 0.0446 0.1202 0.0797 0.0295 0.019 1.192 0.842 14.106 0.135 3.746 27.082 0.10 52986. 0.6076
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1.52 0.0668 0.1753 0.0781 0.0298 0.019 1.202 0.825 14.222 0.136 3.671 26.321 0.10 53022. 0.5846
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2.03 0.0891 0.2270 0.0763 0.0300 0.019 1.210 0.807 14.320 0.137 3.591 25.568 0.10 53060. 0.5616
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2.53 0.1114 0.2755 0.0745 0.0301 0.019 1.217 0.788 14.396 0.137 3.505 24.826 0.10 53102. 0.5388
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3.04 0.1337 0.3208 0.0726 0.0302 0.019 1.221 0.767 14.447 0.138 3.413 24.093 0.10 53146. 0.5160
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3.54 0.1559 0.3631 0.0705 0.0303 0.019 1.223 0.746 14.469 0.138 3.316 23.370 0.10 53194. 0.4933
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4.05 0.1782 0.4023 0.0683 0.0303 0.019 1.222 0.722 14.459 0.138 3.213 22.658 0.10 53244. 0.4708
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4.56 0.2005 0.4386 0.0660 0.0302 0.019 1.218 0.698 14.414 0.138 3.104 21.956 0.10 53298. 0.4484
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5.06 0.2228 0.4719 0.0635 0.0300 0.019 1.211 0.672 14.331 0.137 2.988 21.262 0.10 53355. 0.4261
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5.57 0.2450 0.5023 0.0609 0.0297 0.019 1.201 0.644 14.205 0.136 2.866 20.575 0.10 53415. 0.4038
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6.08 0.2673 0.5298 0.0582 0.0294 0.019 1.186 0.616 14.033 0.134 2.738 19.894 0.10 53478. 0.3816
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6.58 0.2896 0.5544 0.0554 0.0289 0.019 1.168 0.585 13.814 0.132 2.603 19.216 0.10 53545. 0.3594
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7.09 0.3119 0.5760 0.0524 0.0283 0.018 1.145 0.554 13.546 0.129 2.463 18.538 0.10 53616. 0.3372
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7.59 0.3341 0.5944 0.0493 0.0277 0.018 1.118 0.521 13.230 0.126 2.317 17.856 0.10 53690. 0.3150
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8.10 0.3564 0.6096 0.0461 0.0269 0.017 1.087 0.487 12.866 0.123 2.166 17.166 0.10 53767. 0.2928
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8.61 0.3787 0.6211 0.0428 0.0261 0.017 1.053 0.452 12.454 0.119 2.011 16.462 0.10 53848. 0.2706
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9.11 0.4010 0.6288 0.0394 0.0251 0.016 1.014 0.416 11.995 0.115 1.851 15.738 0.10 53933. 0.2482
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9.62 0.4232 0.6320 0.0359 0.0240 0.015 0.971 0.380 11.490 0.110 1.689 14.987 0.10 54021. 0.2258
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10.13 0.4455 0.6302 0.0324 0.0229 0.015 0.925 0.342 10.938 0.104 1.523 14.197 0.10 54113. 0.2031
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10.63 0.4678 0.6226 0.0288 0.0216 0.014 0.874 0.305 10.341 0.099 1.355 13.357 0.10 54208. 0.1802
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11.14 0.4901 0.6079 0.0252 0.0203 0.013 0.820 0.266 9.701 0.093 1.184 12.449 0.10 54307. 0.1571
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11.64 0.5123 0.5845 0.0215 0.0189 0.012 0.762 0.228 9.018 0.086 1.013 11.451 0.10 54410. 0.1336
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12.15 0.5346 0.5502 0.0179 0.0174 0.011 0.701 0.189 8.296 0.079 0.840 10.329 0.10 54517. 0.1098
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12.66 0.5569 0.5014 0.0142 0.0158 0.010 0.637 0.150 7.535 0.072 0.668 9.037 0.10 54627. 0.0856
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13.16 0.5792 0.4331 0.0105 0.0141 0.009 0.570 0.112 6.741 0.064 0.496 7.505 0.10 54741. 0.0613
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13.67 0.6014 0.3368 0.0069 0.0124 0.008 0.500 0.073 5.917 0.057 0.326 5.620 0.10 54859. 0.0372
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14.18 0.6237 0.1983 0.0034 0.0106 0.007 0.428 0.036 5.067 0.048 0.159 3.191 0.10 54980. 0.0147
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14.68 0.6460 -0.0092 -0.0001 0.0088 0.006 0.355 -0.001 4.194 0.040 -0.006 -0.144 0.10 55103. 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 0.0829 0.0271 0.139 4.375 3.508 103.522 0.494 15.603 15.369 0.19 105840. 0.7037
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1.01 0.0223 0.0664 0.0816 0.0274 0.141 4.428 3.449 104.777 0.500 15.341 14.930 0.19 105902. 0.6779
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2.03 0.0446 0.1290 0.0801 0.0277 0.142 4.477 3.386 105.932 0.506 15.060 14.497 0.19 105969. 0.6522
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3.04 0.0670 0.1878 0.0785 0.0280 0.143 4.520 3.318 106.961 0.511 14.758 14.070 0.19 106042. 0.6266
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4.06 0.0893 0.2429 0.0767 0.0282 0.145 4.557 3.246 107.839 0.515 14.436 13.651 0.19 106119. 0.6012
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5.07 0.1116 0.2944 0.0749 0.0284 0.146 4.587 3.168 108.540 0.518 14.092 13.239 0.19 106203. 0.5761
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6.09 0.1339 0.3426 0.0730 0.0285 0.146 4.608 3.086 109.035 0.521 13.725 12.836 0.19 106292. 0.5512
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7.10 0.1562 0.3874 0.0709 0.0286 0.147 4.619 2.998 109.296 0.522 13.334 12.441 0.19 106387. 0.5266
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8.12 0.1786 0.4289 0.0687 0.0286 0.147 4.619 2.905 109.295 0.522 12.920 12.054 0.19 106488. 0.5023
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9.13 0.2009 0.4674 0.0663 0.0285 0.146 4.607 2.806 109.004 0.520 12.480 11.675 0.19 106596. 0.4781
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10.15 0.2232 0.5028 0.0639 0.0284 0.145 4.581 2.701 108.394 0.518 12.016 11.304 0.19 106710. 0.4542
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11.16 0.2455 0.5353 0.0613 0.0281 0.144 4.540 2.591 107.434 0.513 11.526 10.940 0.19 106831. 0.4306
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12.18 0.2679 0.5648 0.0585 0.0278 0.142 4.484 2.475 106.092 0.507 11.010 10.582 0.19 106959. 0.4070
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13.19 0.2902 0.5915 0.0556 0.0273 0.140 4.410 2.353 104.351 0.498 10.468 10.229 0.19 107094. 0.3836
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14.20 0.3125 0.6152 0.0526 0.0267 0.137 4.319 2.226 102.205 0.488 9.902 9.880 0.19 107235. 0.3604
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15.22 0.3348 0.6360 0.0495 0.0261 0.134 4.211 2.094 99.652 0.476 9.315 9.532 0.19 107384. 0.3373
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16.23 0.3571 0.6536 0.0463 0.0253 0.130 4.086 1.958 96.694 0.462 8.709 9.184 0.19 107539. 0.3142
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17.25 0.3795 0.6679 0.0430 0.0244 0.125 3.944 1.818 93.331 0.446 8.085 8.833 0.19 107702. 0.2911
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18.26 0.4018 0.6786 0.0396 0.0234 0.120 3.785 1.674 89.565 0.428 7.444 8.476 0.19 107872. 0.2681
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19.28 0.4241 0.6852 0.0361 0.0223 0.115 3.609 1.527 85.399 0.408 6.790 8.108 0.19 108049. 0.2449
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20.29 0.4464 0.6873 0.0326 0.0211 0.108 3.416 1.377 80.839 0.386 6.124 7.726 0.19 108233. 0.2216
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21.31 0.4687 0.6839 0.0290 0.0199 0.102 3.207 1.225 75.891 0.362 5.449 7.321 0.19 108425. 0.1981
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22.32 0.4911 0.6738 0.0253 0.0185 0.095 2.982 1.071 70.565 0.337 4.765 6.886 0.19 108624. 0.1743
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23.34 0.5134 0.6555 0.0217 0.0170 0.087 2.742 0.916 64.876 0.310 4.077 6.407 0.19 108830. 0.1500
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24.35 0.5357 0.6263 0.0180 0.0154 0.079 2.487 0.761 58.842 0.281 3.385 5.866 0.19 109044. 0.1251
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25.37 0.5580 0.5821 0.0143 0.0137 0.070 2.218 0.606 52.485 0.251 2.694 5.235 0.19 109266. 0.0996
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26.38 0.5804 0.5163 0.0107 0.0120 0.061 1.937 0.451 45.834 0.219 2.007 4.465 0.19 109495. 0.0733
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27.39 0.6027 0.4173 0.0071 0.0102 0.052 1.645 0.298 38.925 0.186 1.326 3.475 0.19 109731. 0.0464
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28.41 0.6250 0.2624 0.0035 0.0083 0.043 1.344 0.148 31.798 0.152 0.657 2.107 0.19 109974. 0.0198
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29.42 0.6473 -0.0003 0.0000 0.0064 0.033 1.034 0.000 24.467 0.117 0.000 -0.002 0.19 110220. 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 0.0835 0.0264 0.457 9.601 7.943 340.777 1.085 35.332 10.573 0.29 158754. 0.7285
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1.54 0.0226 0.0693 0.0821 0.0268 0.463 9.726 7.809 345.222 1.099 34.736 10.260 0.29 158849. 0.7010
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3.08 0.0452 0.1344 0.0806 0.0271 0.468 9.842 7.665 349.318 1.112 34.095 9.953 0.29 158951. 0.6737
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4.62 0.0677 0.1954 0.0789 0.0274 0.473 9.945 7.511 352.974 1.124 33.407 9.651 0.29 159061. 0.6466
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6.16 0.0903 0.2526 0.0772 0.0276 0.478 10.033 7.345 356.098 1.133 32.670 9.355 0.29 159180. 0.6199
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7.70 0.1129 0.3060 0.0753 0.0278 0.481 10.103 7.168 358.596 1.141 31.881 9.066 0.29 159307. 0.5934
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9.24 0.1355 0.3557 0.0733 0.0279 0.483 10.153 6.978 360.367 1.147 31.040 8.783 0.29 159443. 0.5673
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10.78 0.1581 0.4020 0.0712 0.0280 0.485 10.180 6.777 361.312 1.150 30.144 8.507 0.29 159589. 0.5415
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12.32 0.1806 0.4448 0.0690 0.0280 0.485 10.180 6.563 361.328 1.150 29.192 8.238 0.29 159744. 0.5160
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13.86 0.2032 0.4845 0.0666 0.0279 0.483 10.152 6.336 360.314 1.147 28.182 7.976 0.29 159908. 0.4908
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15.40 0.2258 0.5210 0.0641 0.0278 0.480 10.091 6.096 358.164 1.140 27.114 7.720 0.29 160083. 0.4660
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16.94 0.2484 0.5546 0.0614 0.0275 0.476 9.995 5.842 354.768 1.129 25.986 7.469 0.29 160268. 0.4414
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18.48 0.2710 0.5851 0.0586 0.0271 0.469 9.861 5.575 350.014 1.114 24.796 7.224 0.29 160464. 0.4170
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20.02 0.2936 0.6128 0.0556 0.0267 0.461 9.687 5.294 343.843 1.094 23.548 6.983 0.29 160670. 0.3928
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21.55 0.3161 0.6375 0.0526 0.0261 0.451 9.473 5.001 336.235 1.070 22.245 6.746 0.29 160886. 0.3689
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23.09 0.3387 0.6593 0.0494 0.0254 0.439 9.218 4.697 327.185 1.041 20.893 6.512 0.29 161114. 0.3450
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24.63 0.3613 0.6780 0.0461 0.0245 0.425 8.922 4.383 316.690 1.008 19.497 6.278 0.29 161352. 0.3213
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26.17 0.3839 0.6934 0.0427 0.0236 0.409 8.586 4.060 304.753 0.970 18.060 6.043 0.29 161601. 0.2977
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27.71 0.4065 0.7052 0.0392 0.0226 0.391 8.209 3.729 291.379 0.927 16.587 5.805 0.29 161861. 0.2741
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29.25 0.4290 0.7131 0.0356 0.0214 0.371 7.792 3.391 276.580 0.880 15.082 5.561 0.29 162133. 0.2503
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30.79 0.4516 0.7164 0.0320 0.0202 0.349 7.336 3.047 260.375 0.829 13.552 5.307 0.29 162415. 0.2265
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32.33 0.4742 0.7143 0.0283 0.0188 0.326 6.840 2.698 242.790 0.773 11.999 5.040 0.29 162709. 0.2024
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33.87 0.4968 0.7055 0.0246 0.0174 0.300 6.307 2.345 223.865 0.713 10.430 4.751 0.29 163014. 0.1779
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35.41 0.5194 0.6880 0.0209 0.0158 0.273 5.738 1.990 203.652 0.648 8.851 4.432 0.29 163330. 0.1528
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36.95 0.5419 0.6588 0.0172 0.0141 0.244 5.134 1.634 182.220 0.580 7.267 4.067 0.29 163658. 0.1271
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38.49 0.5645 0.6129 0.0134 0.0124 0.214 4.498 1.279 159.659 0.508 5.687 3.632 0.29 163997. 0.1004
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40.03 0.5871 0.5414 0.0097 0.0105 0.182 3.834 0.926 136.079 0.433 4.117 3.085 0.29 164348. 0.0726
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41.57 0.6097 0.4274 0.0061 0.0087 0.150 3.145 0.577 111.615 0.355 2.567 2.345 0.29 164710. 0.0436
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43.11 0.6323 0.2331 0.0025 0.0067 0.116 2.435 0.235 86.420 0.275 1.045 1.233 0.29 165083. 0.0146
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44.65 0.6549
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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 0.0842 0.0262 1.074 16.930 14.245 801.198 1.913 63.362 8.064 0.38 211661. 0.7441
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2.03 0.0224 0.0697 0.0828 0.0266 1.089 17.156 14.009 811.916 1.938 62.313 7.826 0.38 211787. 0.7162
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4.07 0.0447 0.1353 0.0813 0.0269 1.102 17.365 13.755 821.814 1.962 61.183 7.592 0.38 211922. 0.6884
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6.10 0.0671 0.1968 0.0797 0.0272 1.114 17.553 13.483 830.676 1.983 59.971 7.362 0.38 212068. 0.6609
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8.13 0.0894 0.2544 0.0780 0.0274 1.124 17.714 13.191 838.287 2.001 58.672 7.137 0.38 212224. 0.6337
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10.16 0.1118 0.3082 0.0761 0.0276 1.132 17.843 12.878 844.421 2.016 57.283 6.917 0.38 212392. 0.6069
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12.20 0.1342 0.3584 0.0742 0.0278 1.138 17.937 12.545 848.848 2.026 55.800 6.703 0.38 212572. 0.5805
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14.23 0.1565 0.4051 0.0721 0.0278 1.142 17.989 12.190 851.329 2.032 54.220 6.494 0.38 212764. 0.5544
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16.26 0.1789 0.4485 0.0698 0.0278 1.142 17.995 11.812 851.626 2.033 52.541 6.291 0.38 212968. 0.5286
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18.30 0.2013 0.4887 0.0675 0.0278 1.139 17.950 11.412 849.497 2.028 50.761 6.093 0.38 213185. 0.5033
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20.33 0.2236 0.5258 0.0650 0.0276 1.133 17.849 10.989 844.700 2.017 48.877 5.900 0.38 213415. 0.4782
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22.36 0.2460 0.5600 0.0623 0.0274 1.122 17.686 10.541 836.975 1.998 46.887 5.712 0.38 213659. 0.4534
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24.39 0.2683 0.5913 0.0595 0.0270 1.108 17.455 10.069 826.055 1.972 44.788 5.529 0.38 213916. 0.4289
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26.43 0.2907 0.6197 0.0566 0.0265 1.089 17.153 9.574 811.775 1.938 42.585 5.349 0.38 214187. 0.4047
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28.46 0.3131 0.6454 0.0535 0.0260 1.065 16.779 9.057 794.078 1.896 40.284 5.173 0.38 214471. 0.3806
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30.49 0.3354 0.6683 0.0504 0.0253 1.037 16.333 8.519 772.944 1.845 37.894 4.999 0.38 214770. 0.3567
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32.53 0.3578 0.6883 0.0471 0.0245 1.004 15.813 7.964 748.367 1.787 35.424 4.827 0.38 215083. 0.3330
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34.56 0.3801 0.7052 0.0437 0.0236 0.966 15.221 7.392 720.347 1.720 32.881 4.655 0.38 215410. 0.3094
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36.59 0.4025 0.7188 0.0402 0.0225 0.924 14.557 6.806 688.895 1.645 30.272 4.481 0.38 215751. 0.2858
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38.62 0.4249 0.7288 0.0367 0.0214 0.877 13.820 6.207 654.034 1.561 27.607 4.304 0.38 216107. 0.2622
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40.66 0.4472 0.7347 0.0331 0.0201 0.826 13.012 5.596 615.802 1.470 24.893 4.122 0.38 216478. 0.2384
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42.69 0.4696 0.7357 0.0294 0.0188 0.770 12.134 4.977 574.260 1.371 22.138 3.931 0.39 216863. 0.2144
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44.72 0.4919 0.7307 0.0257 0.0173 0.710 11.188 4.351 529.492 1.264 19.353 3.727 0.39 217262. 0.1901
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46.76 0.5143 0.7181 0.0220 0.0157 0.646 10.177 3.720 481.616 1.150 16.547 3.503 0.39 217677. 0.1652
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48.79 0.5367 0.6952 0.0182 0.0141 0.578 9.103 3.087 430.785 1.028 13.730 3.250 0.39 218107. 0.1396
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50.82 0.5590 0.6575 0.0145 0.0123 0.506 7.970 2.454 377.199 0.900 10.916 2.951 0.39 218551. 0.1130
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52.85 0.5814 0.5973 0.0108 0.0105 0.431 6.785 1.825 321.109 0.767 8.118 2.578 0.39 219010. 0.0851
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54.89 0.6038 0.4995 0.0071 0.0086 0.352 5.554 1.203 262.825 0.627 5.350 2.076 0.39 219485. 0.0557
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56.92 0.6261 0.3300 0.0035 0.0066 0.272 4.283 0.591 202.704 0.484 2.629 1.322 0.39 219973. 0.0249
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58.95 0.6485 -0.0094 -0.0001 0.0046 0.189 2.973 -0.011 140.684 0.336 -0.050 -0.036 0.39 220459. 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 0.0852 0.0263 2.104 26.517 22.513 1568.630 2.996 100.138 6.510 0.48 264558. 0.7551
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2.54 0.0223 0.0703 0.0838 0.0266 2.132 26.879 22.144 1590.073 3.037 98.498 6.317 0.48 264715. 0.7267
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5.08 0.0447 0.1364 0.0823 0.0270 2.159 27.214 21.747 1609.875 3.075 96.731 6.127 0.48 264885. 0.6986
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7.62 0.0670 0.1984 0.0807 0.0273 2.183 27.514 21.320 1627.605 3.108 94.833 5.941 0.48 265068. 0.6707
|
|
10.16 0.0894 0.2565 0.0789 0.0275 2.203 27.771 20.862 1642.838 3.138 92.796 5.760 0.48 265264. 0.6432
|
|
12.70 0.1117 0.3108 0.0771 0.0277 2.220 27.979 20.372 1655.119 3.161 90.616 5.583 0.48 265475. 0.6161
|
|
15.24 0.1341 0.3614 0.0751 0.0279 2.231 28.129 19.849 1663.988 3.178 88.286 5.410 0.48 265700. 0.5893
|
|
17.78 0.1564 0.4085 0.0730 0.0279 2.238 28.213 19.290 1668.969 3.187 85.803 5.242 0.48 265941. 0.5629
|
|
20.32 0.1788 0.4524 0.0707 0.0280 2.239 28.223 18.696 1669.585 3.189 83.161 5.079 0.48 266197. 0.5369
|
|
22.85 0.2011 0.4930 0.0683 0.0279 2.233 28.152 18.066 1665.361 3.181 80.358 4.920 0.48 266469. 0.5113
|
|
25.39 0.2235 0.5306 0.0658 0.0277 2.220 27.991 17.399 1655.812 3.162 77.390 4.766 0.48 266757. 0.4860
|
|
27.93 0.2458 0.5652 0.0632 0.0275 2.200 27.731 16.693 1640.425 3.133 74.252 4.616 0.48 267062. 0.4611
|
|
30.47 0.2682 0.5970 0.0603 0.0271 2.171 27.363 15.949 1618.664 3.091 70.941 4.469 0.48 267384. 0.4364
|
|
33.01 0.2905 0.6261 0.0574 0.0266 2.132 26.881 15.167 1590.188 3.037 67.463 4.326 0.48 267723. 0.4119
|
|
35.55 0.3129 0.6524 0.0543 0.0260 2.085 26.284 14.350 1554.871 2.970 63.828 4.186 0.48 268079. 0.3877
|
|
38.09 0.3352 0.6760 0.0511 0.0253 2.029 25.571 13.501 1512.673 2.889 60.052 4.048 0.48 268453. 0.3637
|
|
40.63 0.3576 0.6968 0.0478 0.0245 1.963 24.741 12.623 1463.577 2.795 56.146 3.912 0.48 268845. 0.3398
|
|
43.17 0.3799 0.7146 0.0443 0.0236 1.888 23.795 11.718 1407.588 2.688 52.123 3.776 0.48 269254. 0.3160
|
|
45.71 0.4022 0.7293 0.0408 0.0225 1.803 22.732 10.790 1344.726 2.568 47.995 3.640 0.48 269681. 0.2923
|
|
48.25 0.4246 0.7406 0.0372 0.0213 1.710 21.554 9.842 1275.033 2.435 43.777 3.501 0.48 270126. 0.2685
|
|
50.79 0.4469 0.7478 0.0336 0.0201 1.607 20.262 8.876 1198.590 2.289 39.479 3.359 0.48 270589. 0.2446
|
|
53.33 0.4693 0.7505 0.0299 0.0187 1.496 18.857 7.895 1115.513 2.130 35.117 3.210 0.48 271070. 0.2205
|
|
55.87 0.4916 0.7474 0.0261 0.0172 1.376 17.344 6.903 1025.973 1.959 30.704 3.052 0.48 271570. 0.1960
|
|
58.41 0.5140 0.7370 0.0223 0.0156 1.247 15.725 5.903 930.200 1.777 26.257 2.878 0.48 272088. 0.1710
|
|
60.95 0.5363 0.7167 0.0185 0.0139 1.111 14.005 4.900 828.507 1.582 21.794 2.682 0.48 272624. 0.1452
|
|
63.49 0.5587 0.6820 0.0147 0.0121 0.967 12.193 3.897 721.292 1.378 17.333 2.450 0.48 273179. 0.1183
|
|
66.03 0.5810 0.6250 0.0110 0.0102 0.817 10.296 2.900 609.062 1.163 12.897 2.159 0.48 273753. 0.0899
|
|
68.56 0.6034 0.5296 0.0072 0.0082 0.660 8.324 1.913 492.438 0.940 8.509 1.762 0.48 274346. 0.0596
|
|
71.10 0.6257 0.3582 0.0036 0.0062 0.499 6.291 0.943 372.148 0.711 4.194 1.149 0.49 274956. 0.0273
|
|
73.64 0.6481 -0.0075 0.0000 0.0042 0.333 4.192 -0.013 247.995 0.474 -0.056 -0.023 0.49 275560. 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 0.0864 0.0266 3.675 38.608 32.893 2740.686 4.362 146.307 5.444 0.57 317439. 0.7633
|
|
3.05 0.0223 0.0705 0.0850 0.0269 3.726 39.144 32.362 2778.722 4.422 143.948 5.282 0.57 317629. 0.7347
|
|
6.09 0.0447 0.1368 0.0835 0.0273 3.773 39.639 31.790 2813.838 4.478 141.401 5.124 0.57 317834. 0.7064
|
|
9.14 0.0670 0.1991 0.0819 0.0276 3.816 40.081 31.173 2845.257 4.528 138.659 4.969 0.57 318054. 0.6783
|
|
12.18 0.0893 0.2573 0.0802 0.0278 3.852 40.461 30.511 2872.215 4.571 135.715 4.818 0.57 318291. 0.6507
|
|
15.23 0.1117 0.3118 0.0783 0.0280 3.881 40.767 29.802 2893.918 4.606 132.558 4.671 0.57 318545. 0.6234
|
|
18.27 0.1340 0.3627 0.0763 0.0282 3.902 40.987 29.042 2909.542 4.631 129.180 4.527 0.57 318817. 0.5965
|
|
21.32 0.1563 0.4101 0.0742 0.0283 3.913 41.110 28.232 2918.244 4.645 125.575 4.388 0.57 319107. 0.5700
|
|
24.37 0.1787 0.4542 0.0719 0.0283 3.915 41.123 27.369 2919.183 4.646 121.736 4.252 0.57 319416. 0.5439
|
|
27.41 0.2010 0.4952 0.0695 0.0282 3.904 41.015 26.452 2911.510 4.634 117.658 4.121 0.57 319743. 0.5182
|
|
30.46 0.2234 0.5332 0.0669 0.0280 3.881 40.773 25.480 2894.380 4.607 113.335 3.993 0.57 320090. 0.4928
|
|
33.50 0.2457 0.5682 0.0642 0.0278 3.845 40.386 24.452 2866.897 4.563 108.763 3.869 0.57 320458. 0.4677
|
|
36.55 0.2680 0.6005 0.0614 0.0274 3.793 39.840 23.367 2828.117 4.501 103.934 3.747 0.57 320845. 0.4429
|
|
39.59 0.2904 0.6300 0.0584 0.0269 3.725 39.125 22.225 2777.403 4.420 98.856 3.629 0.57 321253. 0.4183
|
|
42.64 0.3127 0.6569 0.0553 0.0263 3.640 38.240 21.031 2714.515 4.320 93.546 3.514 0.57 321682. 0.3940
|
|
45.69 0.3350 0.6811 0.0520 0.0256 3.539 37.181 19.789 2639.384 4.201 88.024 3.401 0.57 322131. 0.3699
|
|
48.73 0.3574 0.7026 0.0486 0.0247 3.422 35.950 18.505 2551.987 4.062 82.308 3.289 0.57 322602. 0.3459
|
|
51.78 0.3797 0.7213 0.0451 0.0238 3.289 34.546 17.181 2452.337 3.903 76.419 3.178 0.58 323094. 0.3220
|
|
54.82 0.4020 0.7369 0.0416 0.0227 3.139 32.970 15.821 2340.470 3.725 70.374 3.066 0.58 323607. 0.2982
|
|
57.87 0.4244 0.7492 0.0379 0.0215 2.972 31.224 14.432 2216.470 3.528 64.192 2.953 0.58 324141. 0.2743
|
|
60.92 0.4467 0.7578 0.0342 0.0202 2.790 29.308 13.015 2080.477 3.311 57.892 2.837 0.58 324697. 0.2503
|
|
63.96 0.4690 0.7618 0.0304 0.0187 2.592 27.226 11.577 1932.699 3.076 51.494 2.717 0.58 325275. 0.2260
|
|
67.01 0.4914 0.7604 0.0266 0.0172 2.378 24.983 10.122 1773.442 2.823 45.021 2.589 0.58 325875. 0.2013
|
|
70.05 0.5137 0.7520 0.0227 0.0155 2.150 22.583 8.654 1603.117 2.551 38.495 2.449 0.58 326496. 0.1761
|
|
73.10 0.5361 0.7339 0.0189 0.0138 1.907 20.036 7.181 1422.277 2.264 31.942 2.290 0.58 327140. 0.1500
|
|
76.14 0.5584 0.7018 0.0150 0.0119 1.652 17.350 5.709 1231.638 1.960 25.392 2.102 0.58 327806. 0.1228
|
|
79.19 0.5807 0.6475 0.0111 0.0100 1.384 14.539 4.244 1032.100 1.643 18.876 1.865 0.58 328494. 0.0939
|
|
82.24 0.6031 0.5540 0.0073 0.0080 1.106 11.619 2.795 824.785 1.313 12.430 1.537 0.58 329205. 0.0628
|
|
85.28 0.6254 0.3801 0.0036 0.0059 0.819 8.607 1.369 610.997 0.972 6.091 1.017 0.58 329936. 0.0291
|
|
88.33 0.6477 -0.0164 -0.0001 0.0038 0.523 5.494 -0.037 390.028 0.621 -0.162 -0.042 0.58 330654. 0.0000
|
|
|
|
|
|
|
|
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 0.0880 0.0271 5.951 53.583 45.595 4437.671 6.054 202.806 4.660 0.67 370300. 0.7693
|
|
3.54 0.0223 0.0703 0.0866 0.0275 6.034 54.335 44.877 4499.923 6.139 199.612 4.523 0.67 370522. 0.7408
|
|
7.09 0.0446 0.1364 0.0851 0.0278 6.112 55.028 44.100 4557.347 6.217 196.155 4.389 0.67 370762. 0.7126
|
|
10.63 0.0668 0.1985 0.0835 0.0281 6.180 55.648 43.261 4608.676 6.287 192.427 4.258 0.67 371021. 0.6847
|
|
14.18 0.0891 0.2567 0.0818 0.0284 6.239 56.179 42.359 4652.667 6.347 188.413 4.129 0.67 371298. 0.6571
|
|
17.72 0.1114 0.3111 0.0799 0.0286 6.287 56.606 41.390 4688.018 6.395 184.102 4.005 0.67 371596. 0.6299
|
|
21.27 0.1337 0.3620 0.0779 0.0288 6.321 56.912 40.351 4713.361 6.430 179.482 3.883 0.67 371914. 0.6030
|
|
24.81 0.1560 0.4095 0.0757 0.0288 6.339 57.081 39.240 4727.352 6.449 174.542 3.765 0.67 372253. 0.5766
|
|
28.36 0.1782 0.4538 0.0735 0.0289 6.341 57.096 38.056 4728.604 6.451 169.273 3.650 0.67 372614. 0.5505
|
|
31.90 0.2005 0.4949 0.0710 0.0288 6.324 56.941 36.796 4715.755 6.433 163.667 3.539 0.67 372997. 0.5249
|
|
35.44 0.2228 0.5331 0.0684 0.0286 6.286 56.599 35.458 4687.436 6.395 157.719 3.431 0.67 373403. 0.4995
|
|
38.99 0.2451 0.5685 0.0657 0.0283 6.225 56.053 34.042 4642.217 6.333 151.421 3.326 0.67 373832. 0.4745
|
|
42.53 0.2674 0.6012 0.0628 0.0279 6.140 55.285 32.546 4578.589 6.246 144.763 3.224 0.67 374285. 0.4497
|
|
46.08 0.2896 0.6312 0.0598 0.0274 6.028 54.281 30.969 4495.428 6.133 137.751 3.125 0.67 374761. 0.4251
|
|
49.62 0.3119 0.6586 0.0566 0.0268 5.890 53.036 29.319 4392.315 5.992 130.411 3.028 0.67 375261. 0.4008
|
|
53.17 0.3342 0.6835 0.0533 0.0260 5.725 51.548 27.601 4269.142 5.824 122.769 2.932 0.67 375786. 0.3767
|
|
56.71 0.3565 0.7057 0.0498 0.0252 5.533 49.819 25.821 4125.893 5.628 114.853 2.839 0.67 376334. 0.3526
|
|
60.26 0.3787 0.7252 0.0463 0.0242 5.314 47.847 23.986 3962.597 5.406 106.688 2.745 0.67 376907. 0.3287
|
|
63.80 0.4010 0.7418 0.0427 0.0231 5.068 45.634 22.100 3779.328 5.156 98.301 2.652 0.67 377505. 0.3048
|
|
67.34 0.4233 0.7553 0.0389 0.0218 4.796 43.182 20.170 3576.232 4.879 89.718 2.558 0.67 378127. 0.2809
|
|
70.89 0.4456 0.7651 0.0351 0.0205 4.497 40.493 18.203 3353.535 4.575 80.965 2.462 0.67 378774. 0.2568
|
|
74.43 0.4679 0.7707 0.0313 0.0190 4.173 37.571 16.203 3111.584 4.245 72.071 2.362 0.67 379447. 0.2324
|
|
77.98 0.4901 0.7711 0.0274 0.0174 3.823 34.423 14.178 2850.873 3.889 63.065 2.256 0.67 380144. 0.2077
|
|
81.52 0.5124 0.7649 0.0234 0.0157 3.449 31.057 12.136 2572.073 3.509 53.981 2.140 0.68 380867. 0.1823
|
|
85.07 0.5347 0.7494 0.0195 0.0139 3.052 27.483 10.084 2276.076 3.105 44.855 2.010 0.68 381616. 0.1560
|
|
88.61 0.5570 0.7205 0.0155 0.0120 2.634 23.715 8.032 1964.044 2.679 35.725 1.855 0.68 382390. 0.1285
|
|
92.16 0.5793 0.6702 0.0116 0.0100 2.196 19.772 5.989 1637.474 2.234 26.639 1.659 0.68 383190. 0.0993
|
|
95.70 0.6015 0.5814 0.0077 0.0079 1.741 15.676 3.967 1298.244 1.771 17.644 1.386 0.68 384015. 0.0675
|
|
99.24 0.6238 0.4113 0.0038 0.0058 1.272 11.454 1.977 948.583 1.294 8.794 0.945 0.68 384865. 0.0325
|
|
102.79 0.6461 0.0061 0.0000 0.0036 0.789 7.103 0.018 588.241 0.802 0.078 0.014 0.68 385707. 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 0.0900 0.0282 9.244 72.833 60.923 6893.605 8.229 270.984 4.008 0.76 423132. 0.7649
|
|
4.04 0.0222 0.0691 0.0887 0.0285 9.357 73.722 59.995 6977.744 8.329 266.858 3.900 0.76 423387. 0.7385
|
|
8.09 0.0445 0.1345 0.0872 0.0288 9.461 74.542 58.987 7055.338 8.422 262.376 3.792 0.76 423663. 0.7121
|
|
12.13 0.0667 0.1961 0.0856 0.0291 9.554 75.273 57.897 7124.528 8.504 257.524 3.686 0.76 423961. 0.6857
|
|
16.18 0.0890 0.2540 0.0838 0.0294 9.633 75.896 56.718 7183.476 8.575 252.282 3.581 0.76 424280. 0.6594
|
|
20.22 0.1112 0.3084 0.0819 0.0296 9.696 76.389 55.448 7230.198 8.630 246.634 3.478 0.76 424622. 0.6333
|
|
24.27 0.1335 0.3593 0.0799 0.0297 9.739 76.732 54.083 7262.599 8.669 240.562 3.378 0.76 424988. 0.6073
|
|
28.31 0.1557 0.4070 0.0778 0.0298 9.761 76.900 52.620 7278.540 8.688 234.052 3.279 0.76 425378. 0.5815
|
|
32.36 0.1780 0.4515 0.0754 0.0297 9.757 76.871 51.055 7275.797 8.685 227.092 3.183 0.76 425793. 0.5560
|
|
36.40 0.2002 0.4929 0.0730 0.0296 9.725 76.621 49.387 7252.149 8.657 219.672 3.089 0.76 426234. 0.5307
|
|
40.45 0.2225 0.5314 0.0704 0.0295 9.662 76.126 47.613 7205.312 8.601 211.782 2.997 0.76 426700. 0.5056
|
|
44.49 0.2447 0.5672 0.0676 0.0292 9.565 75.362 45.731 7132.944 8.514 203.413 2.908 0.76 427193. 0.4808
|
|
48.54 0.2669 0.6003 0.0646 0.0287 9.431 74.301 43.739 7032.528 8.394 194.553 2.821 0.76 427712. 0.4561
|
|
52.58 0.2892 0.6307 0.0615 0.0282 9.256 72.922 41.638 6902.014 8.239 185.207 2.736 0.76 428258. 0.4317
|
|
56.62 0.3114 0.6587 0.0583 0.0276 9.039 71.215 39.435 6740.500 8.046 175.405 2.654 0.77 428832. 0.4074
|
|
60.67 0.3337 0.6842 0.0549 0.0268 8.781 69.179 37.137 6547.790 7.816 165.186 2.573 0.77 429433. 0.3833
|
|
64.71 0.3559 0.7072 0.0514 0.0258 8.481 66.814 34.754 6323.933 7.549 154.587 2.493 0.77 430061. 0.3593
|
|
68.76 0.3782 0.7275 0.0477 0.0248 8.139 64.122 32.294 6069.083 7.244 143.644 2.413 0.77 430717. 0.3353
|
|
72.80 0.4004 0.7450 0.0440 0.0236 7.756 61.104 29.764 5783.504 6.904 132.390 2.334 0.77 431401. 0.3113
|
|
76.85 0.4227 0.7594 0.0402 0.0223 7.332 57.767 27.172 5467.604 6.526 120.863 2.254 0.77 432113. 0.2873
|
|
80.89 0.4449 0.7703 0.0362 0.0209 6.869 54.115 24.527 5121.963 6.114 109.097 2.172 0.77 432853. 0.2630
|
|
84.94 0.4672 0.7769 0.0323 0.0194 6.366 50.158 21.837 4747.418 5.667 97.131 2.086 0.77 433621. 0.2384
|
|
88.98 0.4894 0.7782 0.0282 0.0178 5.827 45.907 19.111 4345.102 5.187 85.004 1.995 0.77 434418. 0.2132
|
|
93.03 0.5116 0.7726 0.0242 0.0160 5.252 41.380 16.358 3916.554 4.675 72.761 1.894 0.77 435243. 0.1873
|
|
97.07 0.5339 0.7573 0.0201 0.0142 4.645 36.596 13.590 3463.760 4.135 60.450 1.780 0.77 436098. 0.1604
|
|
101.12 0.5561 0.7277 0.0160 0.0122 4.009 31.583 10.819 2989.279 3.568 48.124 1.642 0.77 436981. 0.1320
|
|
105.16 0.5784 0.6750 0.0119 0.0102 3.348 26.374 8.058 2496.303 2.980 35.844 1.464 0.77 437893. 0.1016
|
|
109.20 0.6006 0.5812 0.0079 0.0081 2.667 21.011 5.323 1988.704 2.374 23.677 1.214 0.78 438834. 0.0685
|
|
113.25 0.6229 0.4025 0.0039 0.0060 1.973 15.541 2.629 1470.949 1.756 11.694 0.811 0.78 439803. 0.0321
|
|
117.29 0.6451 -0.0070 0.0000 0.0039 1.264 9.957 -0.028 942.399 1.125 -0.126 -0.014 0.78 440759. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 9000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.0925 0.0326 15.227 106.639 79.208 11354.955 12.048 352.315 3.164 0.86 475922. 0.6884
|
|
4.55 0.0222 0.0619 0.0912 0.0327 15.289 107.069 78.069 11400.812 12.097 347.251 3.106 0.86 476211. 0.6709
|
|
9.10 0.0445 0.1215 0.0897 0.0328 15.334 107.386 76.824 11434.477 12.132 341.712 3.047 0.86 476524. 0.6530
|
|
13.65 0.0667 0.1788 0.0881 0.0329 15.360 107.569 75.467 11454.066 12.153 335.678 2.988 0.86 476862. 0.6347
|
|
18.19 0.0889 0.2336 0.0864 0.0329 15.365 107.603 73.993 11457.589 12.157 329.120 2.929 0.86 477224. 0.6160
|
|
22.74 0.1112 0.2861 0.0845 0.0329 15.345 107.465 72.395 11442.990 12.141 322.014 2.870 0.86 477613. 0.5969
|
|
27.29 0.1334 0.3362 0.0825 0.0328 15.299 107.138 70.669 11408.150 12.104 314.335 2.810 0.86 478029. 0.5775
|
|
31.84 0.1557 0.3838 0.0803 0.0326 15.222 106.601 68.809 11350.906 12.044 306.063 2.750 0.86 478472. 0.5576
|
|
36.39 0.1779 0.4290 0.0780 0.0324 15.112 105.832 66.813 11269.029 11.957 297.182 2.689 0.86 478943. 0.5374
|
|
40.94 0.2001 0.4717 0.0755 0.0320 14.966 104.809 64.676 11160.134 11.841 287.677 2.629 0.86 479443. 0.5168
|
|
45.48 0.2224 0.5120 0.0729 0.0316 14.780 103.510 62.396 11021.796 11.694 277.536 2.568 0.86 479973. 0.4959
|
|
50.03 0.2446 0.5498 0.0700 0.0312 14.552 101.909 59.971 10851.340 11.514 266.750 2.507 0.86 480532. 0.4746
|
|
54.58 0.2668 0.5852 0.0670 0.0306 14.276 99.977 57.397 10645.645 11.295 255.301 2.445 0.86 481121. 0.4530
|
|
59.13 0.2891 0.6180 0.0638 0.0299 13.949 97.688 54.674 10401.875 11.037 243.192 2.384 0.86 481740. 0.4310
|
|
63.68 0.3113 0.6483 0.0605 0.0290 13.569 95.028 51.812 10118.626 10.736 230.460 2.322 0.86 482390. 0.4087
|
|
68.23 0.3336 0.6762 0.0570 0.0281 13.136 91.992 48.821 9795.415 10.393 217.156 2.261 0.86 483070. 0.3862
|
|
72.77 0.3558 0.7009 0.0534 0.0271 12.657 88.638 45.712 9438.241 10.014 203.326 2.197 0.86 483781. 0.3631
|
|
77.32 0.3780 0.7221 0.0496 0.0260 12.134 84.979 42.495 9048.585 9.601 189.019 2.130 0.86 484523. 0.3395
|
|
81.87 0.4003 0.7395 0.0458 0.0248 11.567 81.008 39.182 8625.759 9.152 174.281 2.060 0.86 485296. 0.3153
|
|
86.42 0.4225 0.7524 0.0418 0.0235 10.960 76.753 35.782 8172.704 8.672 159.159 1.986 0.86 486100. 0.2904
|
|
90.97 0.4447 0.7604 0.0377 0.0221 10.307 72.179 32.308 7685.687 8.155 143.706 1.907 0.87 486936. 0.2650
|
|
95.52 0.4670 0.7627 0.0336 0.0206 9.608 67.288 28.771 7164.823 7.602 127.973 1.821 0.87 487802. 0.2388
|
|
100.07 0.4892 0.7576 0.0294 0.0190 8.869 62.114 25.183 6613.926 7.018 112.015 1.727 0.87 488701. 0.2119
|
|
104.61 0.5114 0.7428 0.0252 0.0173 8.097 56.701 21.558 6037.570 6.406 95.890 1.620 0.87 489631. 0.1838
|
|
109.16 0.5337 0.7146 0.0209 0.0156 7.296 51.094 17.910 5440.509 5.773 79.665 1.493 0.87 490594. 0.1545
|
|
113.71 0.5559 0.6676 0.0166 0.0139 6.475 45.346 14.256 4828.417 5.123 63.409 1.339 0.87 491588. 0.1236
|
|
118.26 0.5782 0.5931 0.0124 0.0121 5.643 39.518 10.613 4207.859 4.465 47.206 1.144 0.87 492615. 0.0911
|
|
122.81 0.6004 0.4769 0.0082 0.0103 4.809 33.676 7.003 3585.876 3.805 31.147 0.886 0.87 493674. 0.0573
|
|
127.36 0.6226 0.2939 0.0040 0.0085 3.982 27.890 3.447 2969.696 3.151 15.332 0.526 0.87 494764. 0.0239
|
|
131.90 0.6449 -0.0065 -0.0001 0.0068 3.158 22.113 -0.059 2354.568 2.498 -0.261 -0.011 0.87 495852. 0.0000
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|
PROP RPM = 10000
|
|
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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) - - -
|
|
0.00 0.0000 0.0000 0.0932 0.0414 26.509 167.079 98.514 19767.455 18.877 438.190 2.260 0.95 528763. 0.5485
|
|
5.12 0.0225 0.0500 0.0920 0.0414 26.558 167.389 97.317 19804.145 18.912 432.868 2.229 0.95 529081. 0.5376
|
|
10.24 0.0450 0.0986 0.0908 0.0415 26.562 167.418 95.983 19807.561 18.915 426.933 2.198 0.95 529426. 0.5265
|
|
15.36 0.0676 0.1459 0.0894 0.0414 26.516 167.125 94.501 19772.854 18.882 420.339 2.168 0.95 529800. 0.5152
|
|
20.47 0.0901 0.1919 0.0878 0.0412 26.412 166.472 92.859 19695.580 18.808 413.038 2.138 0.95 530204. 0.5038
|
|
25.59 0.1126 0.2367 0.0861 0.0410 26.246 165.426 91.048 19571.832 18.690 404.981 2.110 0.95 530639. 0.4922
|
|
30.71 0.1351 0.2804 0.0842 0.0406 26.014 163.960 89.057 19398.408 18.524 396.125 2.082 0.95 531106. 0.4804
|
|
35.83 0.1576 0.3228 0.0822 0.0401 25.711 162.054 86.878 19172.887 18.309 386.432 2.055 0.95 531606. 0.4684
|
|
40.95 0.1802 0.3642 0.0799 0.0395 25.337 159.694 84.503 18893.738 18.042 375.871 2.029 0.95 532139. 0.4559
|
|
46.07 0.2027 0.4043 0.0775 0.0388 24.890 156.875 81.929 18560.117 17.724 364.419 2.002 0.95 532706. 0.4431
|
|
51.18 0.2252 0.4433 0.0749 0.0380 24.369 153.591 79.150 18171.648 17.353 352.058 1.976 0.95 533307. 0.4297
|
|
56.30 0.2477 0.4810 0.0720 0.0371 23.774 149.843 76.163 17728.160 16.929 338.775 1.949 0.95 533943. 0.4158
|
|
61.42 0.2703 0.5172 0.0690 0.0361 23.104 145.624 72.965 17228.982 16.452 324.550 1.921 0.96 534614. 0.4012
|
|
66.54 0.2928 0.5519 0.0658 0.0349 22.360 140.931 69.557 16673.746 15.922 309.389 1.892 0.96 535321. 0.3858
|
|
71.66 0.3153 0.5850 0.0624 0.0336 21.542 135.778 65.950 16064.095 15.340 293.346 1.862 0.96 536062. 0.3697
|
|
76.78 0.3378 0.6161 0.0588 0.0322 20.655 130.185 62.162 15402.416 14.708 276.495 1.831 0.96 536839. 0.3529
|
|
81.90 0.3603 0.6452 0.0551 0.0307 19.701 124.171 58.208 14690.865 14.029 258.910 1.797 0.96 537651. 0.3352
|
|
87.01 0.3829 0.6711 0.0512 0.0292 18.706 117.902 54.102 13949.240 13.321 240.648 1.759 0.96 538498. 0.3164
|
|
92.13 0.4054 0.6915 0.0472 0.0276 17.715 111.652 49.859 13209.757 12.614 221.774 1.712 0.96 539380. 0.2955
|
|
97.25 0.4279 0.7047 0.0430 0.0261 16.741 105.513 45.495 12483.474 11.921 202.360 1.653 0.96 540298. 0.2726
|
|
102.37 0.4504 0.7050 0.0388 0.0248 15.882 100.101 41.016 11843.129 11.309 182.437 1.571 0.96 541251. 0.2460
|
|
107.49 0.4729 0.6920 0.0345 0.0236 15.096 95.146 36.446 11256.900 10.750 162.110 1.468 0.96 542239. 0.2167
|
|
112.61 0.4955 0.6685 0.0301 0.0223 14.291 90.075 31.817 10656.920 10.177 141.522 1.354 0.96 543263. 0.1867
|
|
117.72 0.5180 0.6324 0.0257 0.0210 13.479 84.957 27.152 10051.388 9.598 120.774 1.225 0.96 544323. 0.1561
|
|
122.84 0.5405 0.5811 0.0213 0.0198 12.672 79.869 22.480 9449.391 9.024 99.992 1.079 0.97 545419. 0.1251
|
|
127.96 0.5630 0.5121 0.0169 0.0185 11.880 74.875 17.830 8858.609 8.459 79.306 0.913 0.97 546551. 0.0942
|
|
133.08 0.5856 0.4228 0.0125 0.0173 11.109 70.020 13.235 8284.176 7.911 58.871 0.725 0.97 547720. 0.0645
|
|
138.20 0.6081 0.3104 0.0083 0.0162 10.368 65.346 8.734 7731.208 7.383 38.848 0.512 0.97 548927. 0.0370
|
|
143.32 0.6306 0.1724 0.0041 0.0151 9.657 60.868 4.356 7201.422 6.877 19.374 0.274 0.97 550176. 0.0140
|
|
148.43 0.6531 0.0018 0.0000 0.0139 8.922 56.237 0.040 6653.467 6.354 0.179 0.003 0.97 551503. 0.0000
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