723 lines
128 KiB
Plaintext
723 lines
128 KiB
Plaintext
12x13 (12x13.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 0.1281 0.0829 0.002 0.105 0.085 1.238 0.012 0.376 31.014 0.05 18478. 0.4412
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0.49 0.0429 0.0648 0.1277 0.0845 0.002 0.107 0.084 1.262 0.012 0.375 30.330 0.05 18500. 0.4307
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0.98 0.0858 0.1266 0.1272 0.0862 0.002 0.109 0.084 1.288 0.012 0.374 29.602 0.05 18525. 0.4196
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1.46 0.1287 0.1849 0.1267 0.0882 0.002 0.111 0.084 1.317 0.013 0.372 28.836 0.05 18554. 0.4080
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1.95 0.1716 0.2397 0.1261 0.0903 0.002 0.114 0.083 1.348 0.013 0.371 28.040 0.05 18587. 0.3958
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2.44 0.2145 0.2909 0.1254 0.0924 0.002 0.117 0.083 1.380 0.013 0.369 27.221 0.05 18625. 0.3831
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2.93 0.2574 0.3384 0.1245 0.0947 0.002 0.120 0.082 1.414 0.014 0.366 26.389 0.05 18667. 0.3701
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3.41 0.3004 0.3823 0.1234 0.0970 0.002 0.122 0.082 1.448 0.014 0.363 25.552 0.05 18714. 0.3568
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3.90 0.3433 0.4227 0.1221 0.0992 0.002 0.125 0.081 1.481 0.014 0.359 24.717 0.05 18766. 0.3433
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4.39 0.3862 0.4596 0.1205 0.1012 0.002 0.128 0.080 1.511 0.014 0.354 23.893 0.05 18823. 0.3296
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4.88 0.4291 0.4934 0.1185 0.1030 0.002 0.130 0.078 1.538 0.015 0.348 23.082 0.05 18885. 0.3158
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5.36 0.4720 0.5241 0.1161 0.1045 0.002 0.132 0.077 1.561 0.015 0.341 22.290 0.05 18953. 0.3018
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5.85 0.5149 0.5519 0.1132 0.1056 0.002 0.133 0.075 1.576 0.015 0.333 21.516 0.05 19025. 0.2877
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6.34 0.5578 0.5769 0.1097 0.1061 0.002 0.134 0.073 1.584 0.015 0.323 20.761 0.05 19103. 0.2734
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6.83 0.6007 0.5992 0.1058 0.1060 0.002 0.134 0.070 1.583 0.015 0.311 20.023 0.05 19186. 0.2588
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7.31 0.6436 0.6188 0.1012 0.1052 0.002 0.133 0.067 1.571 0.015 0.297 19.298 0.05 19275. 0.2440
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7.80 0.6865 0.6355 0.0960 0.1037 0.002 0.131 0.063 1.548 0.015 0.282 18.582 0.05 19368. 0.2288
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8.29 0.7294 0.6494 0.0902 0.1013 0.002 0.128 0.060 1.512 0.014 0.265 17.871 0.05 19466. 0.2133
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8.78 0.7723 0.6601 0.0839 0.0981 0.002 0.124 0.055 1.465 0.014 0.247 17.157 0.05 19569. 0.1975
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9.26 0.8152 0.6672 0.0772 0.0943 0.002 0.119 0.051 1.408 0.013 0.227 16.429 0.05 19677. 0.1814
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9.75 0.8581 0.6702 0.0702 0.0899 0.002 0.113 0.046 1.342 0.013 0.206 15.677 0.05 19789. 0.1651
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10.24 0.9011 0.6681 0.0629 0.0848 0.002 0.107 0.042 1.267 0.012 0.185 14.884 0.05 19906. 0.1484
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10.73 0.9440 0.6599 0.0554 0.0793 0.002 0.100 0.037 1.184 0.011 0.163 14.032 0.05 20028. 0.1313
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11.21 0.9869 0.6438 0.0478 0.0733 0.001 0.093 0.032 1.094 0.010 0.141 13.094 0.05 20153. 0.1138
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11.70 1.0298 0.6172 0.0400 0.0668 0.001 0.084 0.026 0.998 0.010 0.118 12.031 0.05 20283. 0.0957
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12.19 1.0727 0.5762 0.0322 0.0599 0.001 0.076 0.021 0.894 0.009 0.095 10.783 0.05 20417. 0.0769
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12.68 1.1156 0.5142 0.0242 0.0525 0.001 0.066 0.016 0.785 0.007 0.071 9.252 0.05 20556. 0.0572
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13.16 1.1585 0.4194 0.0162 0.0448 0.001 0.057 0.011 0.669 0.006 0.048 7.267 0.05 20698. 0.0368
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13.65 1.2014 0.2689 0.0082 0.0367 0.001 0.046 0.005 0.548 0.005 0.024 4.493 0.05 20845. 0.0162
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14.14 1.2443 0.0109 0.0002 0.0283 0.001 0.036 0.000 0.423 0.004 0.001 0.177 0.05 20995. 0.0001
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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 0.1287 0.0747 0.012 0.377 0.340 8.918 0.043 1.513 17.300 0.10 36956. 0.4934
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0.98 0.0433 0.0729 0.1283 0.0763 0.012 0.385 0.339 9.113 0.044 1.508 16.880 0.10 37000. 0.4807
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1.97 0.0866 0.1419 0.1279 0.0781 0.013 0.394 0.338 9.330 0.045 1.504 16.433 0.10 37051. 0.4672
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2.95 0.1300 0.2067 0.1274 0.0801 0.013 0.404 0.337 9.569 0.046 1.498 15.965 0.10 37110. 0.4530
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3.94 0.1733 0.2673 0.1269 0.0823 0.013 0.415 0.335 9.826 0.047 1.492 15.480 0.10 37177. 0.4383
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4.92 0.2166 0.3234 0.1262 0.0845 0.014 0.427 0.334 10.099 0.048 1.484 14.984 0.10 37254. 0.4232
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5.91 0.2599 0.3751 0.1254 0.0869 0.014 0.439 0.331 10.380 0.050 1.474 14.482 0.10 37339. 0.4077
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6.89 0.3033 0.4225 0.1244 0.0893 0.014 0.451 0.329 10.664 0.051 1.462 13.981 0.10 37435. 0.3919
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7.88 0.3466 0.4657 0.1231 0.0916 0.015 0.462 0.325 10.941 0.052 1.447 13.485 0.10 37540. 0.3761
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8.86 0.3899 0.5050 0.1214 0.0938 0.015 0.473 0.321 11.200 0.053 1.428 12.999 0.10 37656. 0.3601
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9.85 0.4332 0.5407 0.1194 0.0957 0.015 0.483 0.316 11.432 0.055 1.404 12.526 0.10 37783. 0.3441
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10.83 0.4766 0.5730 0.1170 0.0973 0.016 0.491 0.309 11.624 0.056 1.376 12.067 0.10 37920. 0.3281
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11.82 0.5199 0.6021 0.1141 0.0985 0.016 0.497 0.302 11.765 0.056 1.341 11.624 0.10 38068. 0.3121
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12.80 0.5632 0.6283 0.1106 0.0991 0.016 0.500 0.292 11.842 0.057 1.300 11.196 0.10 38227. 0.2960
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13.78 0.6065 0.6517 0.1065 0.0991 0.016 0.500 0.282 11.843 0.057 1.252 10.784 0.10 38396. 0.2798
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14.77 0.6499 0.6724 0.1018 0.0984 0.016 0.497 0.269 11.756 0.056 1.197 10.384 0.10 38576. 0.2634
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15.75 0.6932 0.6904 0.0965 0.0969 0.016 0.489 0.255 11.572 0.055 1.134 9.996 0.10 38766. 0.2469
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16.74 0.7365 0.7058 0.0906 0.0945 0.015 0.477 0.239 11.290 0.054 1.065 9.618 0.10 38966. 0.2301
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17.72 0.7798 0.7183 0.0842 0.0914 0.015 0.461 0.222 10.913 0.052 0.989 9.245 0.10 39175. 0.2132
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18.71 0.8232 0.7277 0.0773 0.0875 0.014 0.442 0.204 10.451 0.050 0.909 8.873 0.10 39395. 0.1962
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19.69 0.8665 0.7335 0.0702 0.0830 0.013 0.419 0.186 9.910 0.047 0.826 8.496 0.10 39623. 0.1790
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20.68 0.9098 0.7349 0.0629 0.0778 0.012 0.393 0.166 9.296 0.044 0.739 8.108 0.10 39861. 0.1616
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21.66 0.9531 0.7310 0.0553 0.0721 0.012 0.364 0.146 8.616 0.041 0.650 7.698 0.10 40108. 0.1439
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22.65 0.9964 0.7200 0.0476 0.0659 0.011 0.333 0.126 7.872 0.038 0.560 7.253 0.10 40364. 0.1258
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23.63 1.0398 0.6995 0.0398 0.0592 0.009 0.299 0.105 7.067 0.034 0.468 6.752 0.10 40628. 0.1071
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24.62 1.0831 0.6651 0.0319 0.0519 0.008 0.262 0.084 6.205 0.030 0.375 6.163 0.10 40901. 0.0875
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25.60 1.1264 0.6091 0.0239 0.0443 0.007 0.224 0.063 5.289 0.025 0.281 5.427 0.10 41183. 0.0668
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26.59 1.1697 0.5159 0.0160 0.0362 0.006 0.183 0.042 4.322 0.021 0.188 4.426 0.10 41472. 0.0444
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27.57 1.2131 0.3498 0.0080 0.0277 0.004 0.140 0.021 3.309 0.016 0.094 2.894 0.10 41770. 0.0206
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28.55 1.2564 0.0051 0.0001 0.0189 0.003 0.095 0.000 2.256 0.011 0.001 0.041 0.10 42075. 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 0.1290 0.0713 0.039 0.810 0.767 28.732 0.091 3.412 12.108 0.14 55433. 0.5185
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1.48 0.0435 0.0767 0.1286 0.0729 0.039 0.828 0.765 29.399 0.094 3.402 11.801 0.14 55499. 0.5046
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2.97 0.0870 0.1492 0.1282 0.0748 0.040 0.849 0.763 30.142 0.096 3.392 11.475 0.14 55577. 0.4900
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4.45 0.1305 0.2172 0.1278 0.0768 0.042 0.872 0.760 30.959 0.099 3.380 11.133 0.14 55666. 0.4746
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5.93 0.1740 0.2804 0.1273 0.0790 0.043 0.897 0.757 31.842 0.101 3.366 10.781 0.14 55767. 0.4586
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7.42 0.2175 0.3387 0.1266 0.0813 0.044 0.923 0.753 32.778 0.104 3.350 10.420 0.14 55883. 0.4422
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8.90 0.2610 0.3923 0.1258 0.0837 0.045 0.951 0.748 33.748 0.107 3.329 10.057 0.14 56012. 0.4254
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10.38 0.3045 0.4413 0.1248 0.0861 0.047 0.978 0.742 34.726 0.111 3.302 9.696 0.14 56156. 0.4085
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11.86 0.3480 0.4858 0.1235 0.0885 0.048 1.005 0.735 35.684 0.114 3.268 9.339 0.14 56316. 0.3914
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13.35 0.3915 0.5261 0.1219 0.0907 0.049 1.031 0.725 36.586 0.116 3.226 8.991 0.14 56491. 0.3744
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14.83 0.4350 0.5626 0.1199 0.0928 0.050 1.054 0.713 37.394 0.119 3.173 8.653 0.14 56682. 0.3573
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16.31 0.4785 0.5955 0.1175 0.0944 0.051 1.073 0.699 38.067 0.121 3.108 8.327 0.14 56890. 0.3404
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17.80 0.5220 0.6252 0.1146 0.0957 0.052 1.087 0.681 38.565 0.123 3.031 8.013 0.14 57113. 0.3234
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19.28 0.5655 0.6519 0.1111 0.0964 0.052 1.094 0.661 38.846 0.124 2.938 7.713 0.15 57353. 0.3065
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20.76 0.6090 0.6757 0.1070 0.0964 0.052 1.095 0.636 38.866 0.124 2.830 7.424 0.15 57609. 0.2895
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22.25 0.6525 0.6970 0.1022 0.0957 0.052 1.087 0.608 38.585 0.123 2.704 7.146 0.15 57881. 0.2725
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23.73 0.6960 0.7156 0.0968 0.0942 0.051 1.070 0.576 37.973 0.121 2.562 6.879 0.15 58168. 0.2553
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25.21 0.7395 0.7317 0.0909 0.0918 0.050 1.043 0.540 37.020 0.118 2.403 6.620 0.15 58470. 0.2380
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26.69 0.7830 0.7452 0.0844 0.0887 0.048 1.007 0.502 35.744 0.114 2.232 6.368 0.15 58787. 0.2206
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28.18 0.8265 0.7559 0.0775 0.0848 0.046 0.963 0.461 34.171 0.109 2.051 6.119 0.15 59118. 0.2032
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29.66 0.8701 0.7633 0.0703 0.0802 0.043 0.911 0.418 32.327 0.103 1.861 5.870 0.15 59464. 0.1857
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31.14 0.9136 0.7668 0.0629 0.0750 0.041 0.852 0.374 30.231 0.096 1.665 5.616 0.15 59823. 0.1680
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32.63 0.9571 0.7654 0.0553 0.0692 0.037 0.786 0.329 27.900 0.089 1.464 5.351 0.15 60196. 0.1501
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34.11 1.0006 0.7577 0.0476 0.0629 0.034 0.714 0.283 25.347 0.081 1.259 5.067 0.15 60583. 0.1318
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35.59 1.0441 0.7412 0.0398 0.0560 0.030 0.636 0.236 22.581 0.072 1.052 4.750 0.15 60982. 0.1130
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37.08 1.0876 0.7117 0.0318 0.0486 0.026 0.553 0.189 19.613 0.062 0.842 4.379 0.15 61395. 0.0932
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38.56 1.1311 0.6612 0.0239 0.0408 0.022 0.464 0.142 16.454 0.052 0.631 3.912 0.15 61820. 0.0721
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40.04 1.1746 0.5728 0.0159 0.0325 0.018 0.370 0.094 13.118 0.042 0.420 3.263 0.15 62258. 0.0490
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41.53 1.2181 0.4033 0.0079 0.0239 0.013 0.271 0.047 9.623 0.031 0.209 2.215 0.15 62707. 0.0235
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43.01 1.2616 0.0004 0.0000 0.0149 0.008 0.169 0.000 5.989 0.019 0.000 0.002 0.15 63167. 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 0.1292 0.0694 0.089 1.401 1.366 66.315 0.158 6.074 9.340 0.19 73910. 0.5337
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1.98 0.0436 0.0790 0.1288 0.0711 0.091 1.435 1.362 67.904 0.162 6.058 9.097 0.19 73999. 0.5191
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3.96 0.0872 0.1536 0.1284 0.0729 0.093 1.472 1.358 69.680 0.166 6.041 8.840 0.19 74102. 0.5037
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5.95 0.1308 0.2234 0.1280 0.0750 0.096 1.514 1.354 71.633 0.171 6.021 8.571 0.19 74221. 0.4876
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7.93 0.1744 0.2882 0.1275 0.0772 0.099 1.558 1.348 73.747 0.176 5.998 8.293 0.19 74357. 0.4709
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9.91 0.2180 0.3479 0.1269 0.0795 0.102 1.606 1.342 75.991 0.181 5.969 8.009 0.19 74511. 0.4537
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11.89 0.2616 0.4027 0.1261 0.0820 0.105 1.655 1.334 78.321 0.187 5.933 7.724 0.19 74684. 0.4362
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13.87 0.3052 0.4525 0.1252 0.0844 0.108 1.705 1.323 80.677 0.193 5.886 7.440 0.19 74877. 0.4185
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15.86 0.3488 0.4977 0.1239 0.0868 0.111 1.754 1.310 82.987 0.198 5.827 7.161 0.19 75091. 0.4008
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17.84 0.3924 0.5386 0.1223 0.0891 0.114 1.800 1.293 85.167 0.203 5.753 6.888 0.19 75325. 0.3830
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19.82 0.4360 0.5756 0.1204 0.0912 0.117 1.841 1.272 87.126 0.208 5.660 6.624 0.19 75581. 0.3654
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21.80 0.4796 0.6089 0.1179 0.0929 0.119 1.876 1.247 88.767 0.212 5.546 6.371 0.19 75859. 0.3478
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23.78 0.5232 0.6389 0.1150 0.0942 0.121 1.902 1.216 89.990 0.215 5.408 6.128 0.19 76159. 0.3304
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25.76 0.5668 0.6659 0.1115 0.0949 0.122 1.916 1.179 90.692 0.217 5.243 5.895 0.19 76480. 0.3130
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27.75 0.6104 0.6900 0.1074 0.0950 0.122 1.918 1.135 90.772 0.217 5.050 5.673 0.19 76822. 0.2955
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29.73 0.6540 0.7116 0.1026 0.0943 0.121 1.904 1.085 90.129 0.215 4.826 5.460 0.19 77186. 0.2781
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31.71 0.6976 0.7306 0.0972 0.0928 0.119 1.874 1.028 88.688 0.212 4.571 5.256 0.20 77570. 0.2605
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33.69 0.7412 0.7472 0.0912 0.0904 0.116 1.826 0.964 86.432 0.206 4.288 5.059 0.20 77975. 0.2429
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35.67 0.7848 0.7614 0.0847 0.0873 0.112 1.762 0.895 83.399 0.199 3.982 4.869 0.20 78400. 0.2252
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37.66 0.8284 0.7729 0.0778 0.0833 0.107 1.683 0.822 79.650 0.190 3.657 4.682 0.20 78843. 0.2076
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39.64 0.8720 0.7814 0.0706 0.0787 0.101 1.590 0.746 75.246 0.180 3.318 4.497 0.20 79306. 0.1899
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41.62 0.9156 0.7863 0.0631 0.0735 0.094 1.484 0.667 70.234 0.168 2.968 4.309 0.20 79788. 0.1721
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43.60 0.9592 0.7867 0.0555 0.0677 0.087 1.366 0.587 64.651 0.154 2.609 4.116 0.20 80287. 0.1541
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45.58 1.0028 0.7813 0.0477 0.0612 0.078 1.237 0.505 58.527 0.140 2.244 3.910 0.20 80804. 0.1358
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47.57 1.0464 0.7678 0.0398 0.0543 0.070 1.096 0.421 51.888 0.124 1.874 3.682 0.20 81339. 0.1169
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49.55 1.0900 0.7421 0.0319 0.0468 0.060 0.946 0.337 44.757 0.107 1.500 3.417 0.20 81891. 0.0970
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51.53 1.1336 0.6963 0.0239 0.0389 0.050 0.785 0.253 37.164 0.089 1.123 3.082 0.20 82461. 0.0757
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53.51 1.1772 0.6129 0.0159 0.0305 0.039 0.616 0.168 29.141 0.070 0.747 2.613 0.20 83046. 0.0523
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55.49 1.2208 0.4444 0.0079 0.0217 0.028 0.438 0.083 20.731 0.049 0.371 1.827 0.20 83648. 0.0258
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57.47 1.2644 -0.0010 0.0000 0.0125 0.016 0.253 0.000 11.986 0.029 0.000 -0.004 0.21 84263. 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 0.1293 0.0682 0.171 2.153 2.136 127.343 0.243 9.503 7.609 0.24 92387. 0.5438
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2.48 0.0437 0.0806 0.1290 0.0699 0.175 2.205 2.131 130.456 0.249 9.479 7.409 0.24 92498. 0.5289
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4.96 0.0873 0.1565 0.1286 0.0718 0.180 2.264 2.125 133.940 0.256 9.453 7.197 0.24 92627. 0.5130
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7.44 0.1310 0.2276 0.1282 0.0738 0.185 2.329 2.119 137.778 0.263 9.423 6.974 0.24 92776. 0.4964
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9.92 0.1747 0.2934 0.1278 0.0760 0.190 2.399 2.111 141.938 0.271 9.388 6.745 0.24 92946. 0.4792
|
|
12.40 0.2183 0.3541 0.1272 0.0784 0.196 2.474 2.101 146.360 0.280 9.345 6.511 0.24 93139. 0.4615
|
|
14.89 0.2620 0.4095 0.1264 0.0809 0.202 2.552 2.089 150.960 0.288 9.291 6.276 0.24 93356. 0.4435
|
|
17.37 0.3056 0.4600 0.1255 0.0834 0.209 2.631 2.073 155.620 0.297 9.221 6.042 0.24 93598. 0.4254
|
|
19.85 0.3493 0.5057 0.1243 0.0858 0.215 2.708 2.053 160.200 0.306 9.131 5.812 0.24 93865. 0.4072
|
|
22.33 0.3930 0.5470 0.1227 0.0882 0.221 2.781 2.027 164.534 0.314 9.016 5.588 0.24 94159. 0.3890
|
|
24.81 0.4366 0.5842 0.1207 0.0902 0.226 2.847 1.995 168.439 0.322 8.873 5.372 0.24 94480. 0.3710
|
|
27.29 0.4803 0.6178 0.1183 0.0920 0.230 2.903 1.955 171.722 0.328 8.696 5.164 0.24 94828. 0.3530
|
|
29.77 0.5240 0.6480 0.1154 0.0933 0.234 2.944 1.907 174.184 0.333 8.481 4.965 0.24 95203. 0.3352
|
|
32.25 0.5676 0.6752 0.1119 0.0941 0.236 2.969 1.849 175.623 0.335 8.224 4.775 0.24 95606. 0.3175
|
|
34.73 0.6113 0.6995 0.1078 0.0942 0.236 2.972 1.781 175.834 0.336 7.922 4.594 0.24 96035. 0.2998
|
|
37.21 0.6550 0.7213 0.1030 0.0936 0.234 2.952 1.702 174.619 0.333 7.571 4.421 0.24 96491. 0.2821
|
|
39.69 0.6986 0.7407 0.0976 0.0921 0.230 2.905 1.612 171.829 0.328 7.172 4.256 0.24 96973. 0.2643
|
|
42.17 0.7423 0.7577 0.0916 0.0897 0.225 2.830 1.513 167.428 0.320 6.728 4.098 0.24 97480. 0.2464
|
|
44.66 0.7859 0.7723 0.0850 0.0865 0.217 2.730 1.405 161.489 0.308 6.248 3.945 0.25 98013. 0.2286
|
|
47.14 0.8296 0.7845 0.0781 0.0826 0.207 2.606 1.290 154.131 0.294 5.738 3.796 0.25 98569. 0.2108
|
|
49.62 0.8733 0.7938 0.0708 0.0779 0.195 2.459 1.170 145.472 0.278 5.206 3.649 0.25 99149. 0.1930
|
|
52.10 0.9169 0.7997 0.0634 0.0727 0.182 2.292 1.047 135.606 0.259 4.656 3.502 0.25 99752. 0.1752
|
|
54.58 0.9606 0.8015 0.0557 0.0668 0.167 2.106 0.920 124.606 0.238 4.094 3.350 0.25 100378. 0.1571
|
|
57.06 1.0043 0.7979 0.0479 0.0603 0.151 1.902 0.791 112.529 0.215 3.520 3.190 0.25 101027. 0.1388
|
|
59.54 1.0479 0.7867 0.0400 0.0533 0.133 1.681 0.661 99.426 0.190 2.939 3.014 0.25 101697. 0.1198
|
|
62.02 1.0916 0.7641 0.0320 0.0457 0.114 1.443 0.529 85.345 0.163 2.352 2.810 0.25 102389. 0.0999
|
|
64.50 1.1352 0.7222 0.0240 0.0377 0.094 1.189 0.396 70.342 0.134 1.762 2.554 0.25 103102. 0.0786
|
|
66.98 1.1789 0.6436 0.0159 0.0292 0.073 0.921 0.263 54.484 0.104 1.171 2.192 0.25 103836. 0.0550
|
|
69.46 1.2226 0.4779 0.0079 0.0203 0.051 0.640 0.131 37.859 0.072 0.583 1.569 0.26 104590. 0.0278
|
|
71.95 1.2662 -0.0001 0.0000 0.0110 0.028 0.348 0.000 20.567 0.039 0.000 0.000 0.26 105361. 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 0.1295 0.0675 0.292 3.065 3.080 217.592 0.346 13.700 6.420 0.29 110863. 0.5509
|
|
2.98 0.0437 0.0817 0.1292 0.0691 0.299 3.141 3.073 222.982 0.355 13.667 6.250 0.29 110996. 0.5357
|
|
5.96 0.0874 0.1586 0.1288 0.0710 0.307 3.226 3.065 229.020 0.364 13.631 6.069 0.29 111151. 0.5195
|
|
8.94 0.1311 0.2305 0.1284 0.0731 0.316 3.320 3.056 235.683 0.375 13.591 5.880 0.29 111330. 0.5026
|
|
11.92 0.1749 0.2971 0.1280 0.0753 0.326 3.422 3.045 242.916 0.387 13.543 5.685 0.29 111535. 0.4851
|
|
14.90 0.2186 0.3584 0.1274 0.0777 0.336 3.531 3.032 250.621 0.399 13.484 5.486 0.29 111767. 0.4671
|
|
17.88 0.2623 0.4144 0.1267 0.0802 0.347 3.644 3.015 258.650 0.412 13.409 5.286 0.29 112027. 0.4488
|
|
20.86 0.3060 0.4653 0.1258 0.0827 0.358 3.758 2.993 266.803 0.425 13.311 5.087 0.29 112318. 0.4303
|
|
23.84 0.3497 0.5114 0.1246 0.0852 0.369 3.872 2.964 274.833 0.437 13.185 4.892 0.29 112639. 0.4118
|
|
26.82 0.3934 0.5529 0.1231 0.0876 0.379 3.979 2.928 282.450 0.450 13.024 4.702 0.29 112993. 0.3934
|
|
29.80 0.4371 0.5904 0.1212 0.0897 0.388 4.076 2.882 289.332 0.460 12.820 4.518 0.29 113379. 0.3751
|
|
32.79 0.4809 0.6241 0.1188 0.0915 0.396 4.158 2.826 295.139 0.470 12.568 4.342 0.29 113797. 0.3569
|
|
35.77 0.5246 0.6545 0.1159 0.0929 0.402 4.219 2.757 299.521 0.477 12.261 4.174 0.29 114248. 0.3389
|
|
38.75 0.5683 0.6818 0.1124 0.0937 0.405 4.256 2.674 302.120 0.481 11.893 4.014 0.29 114733. 0.3209
|
|
41.73 0.6120 0.7064 0.1083 0.0938 0.406 4.262 2.576 302.577 0.482 11.458 3.861 0.29 115249. 0.3030
|
|
44.71 0.6557 0.7283 0.1035 0.0932 0.403 4.234 2.462 300.544 0.478 10.952 3.716 0.29 115797. 0.2851
|
|
47.69 0.6994 0.7479 0.0981 0.0917 0.397 4.166 2.333 295.758 0.471 10.376 3.577 0.29 116377. 0.2672
|
|
50.67 0.7431 0.7652 0.0920 0.0893 0.386 4.059 2.189 288.151 0.459 9.735 3.445 0.29 116987. 0.2492
|
|
53.65 0.7869 0.7803 0.0854 0.0861 0.373 3.914 2.032 277.851 0.442 9.040 3.318 0.29 117627. 0.2313
|
|
56.63 0.8306 0.7929 0.0785 0.0822 0.355 3.734 1.867 265.064 0.422 8.302 3.194 0.30 118297. 0.2134
|
|
59.61 0.8743 0.8029 0.0712 0.0775 0.335 3.522 1.693 249.995 0.398 7.532 3.072 0.30 118994. 0.1955
|
|
62.59 0.9180 0.8097 0.0637 0.0722 0.312 3.280 1.515 232.806 0.371 6.737 2.951 0.30 119720. 0.1776
|
|
65.57 0.9617 0.8126 0.0560 0.0662 0.286 3.009 1.331 213.625 0.340 5.922 2.827 0.30 120473. 0.1595
|
|
68.55 1.0054 0.8104 0.0481 0.0597 0.258 2.713 1.145 192.553 0.306 5.092 2.697 0.30 121253. 0.1411
|
|
71.53 1.0491 0.8011 0.0402 0.0526 0.228 2.390 0.956 169.675 0.270 4.251 2.554 0.30 122059. 0.1221
|
|
74.51 1.0928 0.7808 0.0321 0.0450 0.195 2.044 0.765 145.080 0.231 3.401 2.390 0.30 122891. 0.1022
|
|
77.49 1.1366 0.7422 0.0241 0.0369 0.159 1.674 0.573 118.865 0.189 2.547 2.185 0.30 123749. 0.0808
|
|
80.47 1.1803 0.6677 0.0160 0.0283 0.122 1.284 0.380 91.149 0.145 1.692 1.893 0.31 124631. 0.0571
|
|
83.45 1.2240 0.5050 0.0079 0.0192 0.083 0.875 0.189 62.085 0.099 0.840 1.380 0.31 125538. 0.0293
|
|
86.43 1.2677 -0.0033 0.0000 0.0099 0.043 0.449 -0.001 31.849 0.051 -0.003 -0.009 0.31 126463. 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 0.1296 0.0670 0.460 4.142 4.197 342.994 0.468 18.668 5.550 0.33 129338. 0.5560
|
|
3.48 0.0437 0.0824 0.1293 0.0686 0.471 4.245 4.187 351.554 0.480 18.626 5.403 0.33 129494. 0.5406
|
|
6.96 0.0875 0.1600 0.1290 0.0705 0.484 4.361 4.177 361.157 0.493 18.580 5.246 0.33 129675. 0.5243
|
|
10.44 0.1312 0.2326 0.1286 0.0726 0.499 4.489 4.166 371.772 0.507 18.528 5.082 0.33 129884. 0.5072
|
|
13.92 0.1750 0.2997 0.1282 0.0748 0.514 4.628 4.152 383.317 0.523 18.467 4.913 0.33 130123. 0.4895
|
|
17.40 0.2187 0.3615 0.1277 0.0772 0.531 4.777 4.135 395.642 0.540 18.391 4.740 0.33 130393. 0.4713
|
|
20.88 0.2625 0.4179 0.1270 0.0798 0.548 4.933 4.113 408.515 0.557 18.293 4.566 0.33 130697. 0.4528
|
|
24.36 0.3062 0.4691 0.1261 0.0823 0.565 5.091 4.084 421.620 0.575 18.166 4.393 0.33 131036. 0.4341
|
|
27.84 0.3499 0.5154 0.1250 0.0848 0.583 5.247 4.047 434.560 0.593 18.000 4.224 0.34 131412. 0.4155
|
|
31.32 0.3937 0.5572 0.1235 0.0873 0.599 5.396 3.999 446.867 0.610 17.786 4.059 0.34 131824. 0.3969
|
|
34.79 0.4374 0.5948 0.1216 0.0894 0.614 5.530 3.938 458.023 0.625 17.515 3.899 0.34 132275. 0.3784
|
|
38.27 0.4812 0.6287 0.1193 0.0913 0.627 5.645 3.862 467.476 0.638 17.177 3.747 0.34 132764. 0.3600
|
|
41.75 0.5249 0.6592 0.1164 0.0927 0.637 5.731 3.769 474.655 0.648 16.763 3.601 0.34 133291. 0.3418
|
|
45.23 0.5686 0.6866 0.1129 0.0935 0.642 5.784 3.657 478.985 0.653 16.265 3.463 0.34 133857. 0.3238
|
|
48.71 0.6124 0.7113 0.1088 0.0937 0.644 5.794 3.524 479.881 0.655 15.675 3.331 0.34 134460. 0.3057
|
|
52.19 0.6561 0.7334 0.1041 0.0931 0.639 5.757 3.369 476.782 0.650 14.988 3.205 0.34 135101. 0.2877
|
|
55.67 0.6999 0.7532 0.0986 0.0916 0.629 5.666 3.193 469.262 0.640 14.202 3.086 0.34 135778. 0.2697
|
|
59.15 0.7436 0.7708 0.0925 0.0893 0.613 5.521 2.996 457.203 0.624 13.327 2.972 0.34 136491. 0.2516
|
|
62.63 0.7874 0.7862 0.0859 0.0861 0.591 5.323 2.783 440.805 0.601 12.378 2.863 0.34 137239. 0.2336
|
|
66.11 0.8311 0.7993 0.0789 0.0821 0.564 5.076 2.556 420.400 0.574 11.370 2.758 0.34 138021. 0.2156
|
|
69.59 0.8748 0.8098 0.0716 0.0774 0.531 4.785 2.319 396.313 0.541 10.317 2.654 0.35 138836. 0.1977
|
|
73.07 0.9186 0.8174 0.0641 0.0720 0.495 4.453 2.075 368.809 0.503 9.228 2.552 0.35 139684. 0.1797
|
|
76.55 0.9623 0.8212 0.0563 0.0660 0.453 4.082 1.824 338.091 0.461 8.113 2.447 0.35 140564. 0.1616
|
|
80.03 1.0061 0.8202 0.0484 0.0594 0.408 3.675 1.569 304.322 0.415 6.977 2.338 0.35 141475. 0.1432
|
|
83.51 1.0498 0.8125 0.0404 0.0523 0.359 3.232 1.310 267.641 0.365 5.825 2.219 0.35 142417. 0.1242
|
|
86.99 1.0936 0.7945 0.0324 0.0446 0.306 2.755 1.048 228.187 0.311 4.662 2.083 0.35 143389. 0.1043
|
|
90.47 1.1373 0.7589 0.0242 0.0363 0.250 2.247 0.785 186.118 0.254 3.492 1.913 0.35 144391. 0.0829
|
|
93.95 1.1810 0.6884 0.0161 0.0277 0.190 1.710 0.522 141.628 0.193 2.322 1.671 0.36 145421. 0.0590
|
|
97.43 1.2248 0.5300 0.0080 0.0185 0.127 1.147 0.260 94.963 0.130 1.156 1.241 0.36 146481. 0.0309
|
|
100.91 1.2685 0.0009 0.0000 0.0091 0.062 0.560 0.000 46.405 0.063 0.001 0.002 0.36 147560. 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 0.1298 0.0667 0.683 5.385 5.488 509.681 0.608 24.412 4.884 0.38 147813. 0.5595
|
|
3.98 0.0438 0.0829 0.1295 0.0683 0.701 5.520 5.476 522.447 0.624 24.359 4.754 0.38 147991. 0.5440
|
|
7.96 0.0875 0.1611 0.1292 0.0702 0.720 5.671 5.464 536.794 0.641 24.302 4.617 0.38 148198. 0.5276
|
|
11.94 0.1313 0.2341 0.1289 0.0723 0.741 5.839 5.450 552.682 0.660 24.239 4.472 0.38 148436. 0.5105
|
|
15.92 0.1751 0.3017 0.1285 0.0746 0.764 6.022 5.433 570.000 0.680 24.165 4.323 0.38 148709. 0.4927
|
|
19.90 0.2189 0.3638 0.1280 0.0770 0.789 6.218 5.412 588.533 0.703 24.072 4.171 0.38 149019. 0.4744
|
|
23.88 0.2626 0.4205 0.1273 0.0795 0.815 6.423 5.385 607.941 0.726 23.951 4.017 0.38 149366. 0.4558
|
|
27.86 0.3064 0.4720 0.1265 0.0821 0.842 6.632 5.349 627.754 0.749 23.793 3.865 0.38 149754. 0.4371
|
|
31.83 0.3502 0.5185 0.1254 0.0847 0.868 6.840 5.302 647.374 0.773 23.585 3.715 0.38 150184. 0.4183
|
|
35.81 0.3940 0.5604 0.1239 0.0871 0.893 7.037 5.242 666.093 0.795 23.315 3.569 0.38 150656. 0.3996
|
|
39.79 0.4377 0.5981 0.1221 0.0894 0.916 7.217 5.164 683.118 0.815 22.969 3.429 0.38 151171. 0.3810
|
|
43.77 0.4815 0.6321 0.1198 0.0912 0.936 7.370 5.066 697.604 0.833 22.535 3.294 0.39 151730. 0.3625
|
|
47.75 0.5253 0.6627 0.1170 0.0927 0.950 7.487 4.946 708.680 0.846 22.001 3.166 0.39 152334. 0.3443
|
|
51.73 0.5690 0.6903 0.1135 0.0936 0.959 7.559 4.801 715.464 0.854 21.355 3.044 0.39 152981. 0.3261
|
|
55.71 0.6128 0.7151 0.1094 0.0938 0.962 7.576 4.629 717.069 0.856 20.588 2.928 0.39 153672. 0.3080
|
|
59.69 0.6566 0.7373 0.1047 0.0932 0.956 7.529 4.427 712.638 0.851 19.692 2.818 0.39 154405. 0.2899
|
|
63.67 0.7004 0.7573 0.0992 0.0918 0.941 7.412 4.196 701.519 0.837 18.665 2.713 0.39 155180. 0.2718
|
|
67.65 0.7441 0.7751 0.0931 0.0894 0.917 7.222 3.939 683.526 0.816 17.520 2.614 0.39 155997. 0.2536
|
|
71.63 0.7879 0.7908 0.0865 0.0862 0.884 6.962 3.659 658.951 0.787 16.274 2.518 0.39 156853. 0.2356
|
|
75.61 0.8317 0.8043 0.0795 0.0822 0.843 6.638 3.361 628.296 0.750 14.951 2.427 0.39 157748. 0.2175
|
|
79.59 0.8754 0.8153 0.0721 0.0774 0.794 6.255 3.050 592.055 0.707 13.568 2.337 0.40 158681. 0.1996
|
|
83.57 0.9192 0.8235 0.0645 0.0720 0.738 5.818 2.729 550.628 0.657 12.138 2.248 0.40 159652. 0.1816
|
|
87.54 0.9630 0.8281 0.0567 0.0660 0.676 5.328 2.399 504.328 0.602 10.672 2.158 0.40 160659. 0.1634
|
|
91.52 1.0068 0.8282 0.0488 0.0593 0.608 4.790 2.063 453.397 0.541 9.178 2.064 0.40 161701. 0.1450
|
|
95.50 1.0505 0.8218 0.0407 0.0521 0.534 4.206 1.723 398.049 0.475 7.662 1.963 0.40 162779. 0.1260
|
|
99.48 1.0943 0.8057 0.0326 0.0443 0.454 3.576 1.379 338.493 0.404 6.132 1.847 0.40 163892. 0.1061
|
|
103.46 1.1381 0.7726 0.0244 0.0360 0.369 2.905 1.033 274.968 0.328 4.593 1.703 0.41 165038. 0.0846
|
|
107.44 1.1819 0.7056 0.0162 0.0272 0.279 2.195 0.686 207.768 0.248 3.052 1.498 0.41 166218. 0.0607
|
|
111.42 1.2256 0.5506 0.0081 0.0180 0.184 1.450 0.341 137.269 0.164 1.518 1.127 0.41 167430. 0.0322
|
|
115.40 1.2694 -0.0019 0.0000 0.0084 0.086 0.675 -0.001 63.894 0.076 -0.002 -0.004 0.41 168664. 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 0.1299 0.0665 0.971 6.800 6.955 724.044 0.768 30.934 4.357 0.43 166287. 0.5618
|
|
4.48 0.0438 0.0833 0.1297 0.0682 0.995 6.970 6.940 742.185 0.787 30.870 4.241 0.43 166487. 0.5464
|
|
8.96 0.0876 0.1618 0.1294 0.0701 1.023 7.162 6.925 762.607 0.809 30.804 4.119 0.43 166720. 0.5300
|
|
13.44 0.1314 0.2351 0.1291 0.0721 1.053 7.375 6.909 785.274 0.833 30.730 3.990 0.43 166988. 0.5129
|
|
17.92 0.1752 0.3030 0.1287 0.0744 1.086 7.607 6.889 810.040 0.859 30.643 3.857 0.43 167295. 0.4951
|
|
22.40 0.2190 0.3654 0.1282 0.0769 1.122 7.857 6.865 836.615 0.888 30.534 3.722 0.43 167643. 0.4768
|
|
26.87 0.2628 0.4223 0.1276 0.0794 1.159 8.119 6.833 864.531 0.917 30.392 3.585 0.43 168034. 0.4582
|
|
31.35 0.3066 0.4740 0.1269 0.0820 1.198 8.388 6.790 893.122 0.948 30.203 3.448 0.43 168471. 0.4394
|
|
35.83 0.3504 0.5207 0.1258 0.0847 1.236 8.654 6.734 921.530 0.978 29.953 3.314 0.43 168954. 0.4206
|
|
40.31 0.3942 0.5627 0.1244 0.0872 1.272 8.910 6.660 948.729 1.007 29.624 3.184 0.43 169485. 0.4018
|
|
44.79 0.4380 0.6006 0.1226 0.0894 1.306 9.143 6.565 973.562 1.033 29.199 3.058 0.43 170065. 0.3832
|
|
49.27 0.4818 0.6346 0.1204 0.0914 1.334 9.342 6.444 994.793 1.056 28.662 2.938 0.43 170695. 0.3647
|
|
53.75 0.5256 0.6653 0.1176 0.0929 1.356 9.496 6.294 1011.145 1.073 27.996 2.823 0.43 171374. 0.3464
|
|
58.23 0.5693 0.6929 0.1142 0.0938 1.370 9.592 6.112 1021.329 1.084 27.188 2.714 0.44 172104. 0.3281
|
|
62.71 0.6131 0.7178 0.1101 0.0941 1.373 9.617 5.895 1024.051 1.087 26.223 2.611 0.44 172882. 0.3100
|
|
67.19 0.6569 0.7402 0.1054 0.0935 1.365 9.561 5.641 1018.068 1.080 25.091 2.513 0.44 173708. 0.2919
|
|
71.67 0.7007 0.7604 0.0999 0.0921 1.344 9.414 5.349 1002.423 1.064 23.792 2.420 0.44 174582. 0.2737
|
|
76.15 0.7445 0.7784 0.0938 0.0897 1.310 9.174 5.022 976.828 1.036 22.338 2.332 0.44 175501. 0.2555
|
|
80.62 0.7883 0.7944 0.0872 0.0865 1.263 8.844 4.666 941.695 0.999 20.756 2.248 0.44 176466. 0.2374
|
|
85.10 0.8321 0.8082 0.0801 0.0825 1.204 8.431 4.288 897.748 0.953 19.072 2.166 0.44 177474. 0.2193
|
|
89.58 0.8759 0.8197 0.0727 0.0777 1.134 7.942 3.892 845.704 0.897 17.310 2.087 0.44 178526. 0.2013
|
|
94.06 0.9197 0.8284 0.0651 0.0722 1.054 7.383 3.482 786.150 0.834 15.488 2.009 0.45 179619. 0.1833
|
|
98.54 0.9635 0.8338 0.0572 0.0661 0.965 6.757 3.062 719.537 0.763 13.619 1.930 0.45 180753. 0.1651
|
|
103.02 1.0073 0.8348 0.0492 0.0594 0.867 6.069 2.633 646.218 0.686 11.714 1.848 0.45 181928. 0.1467
|
|
107.50 1.0511 0.8297 0.0411 0.0520 0.760 5.320 2.199 566.502 0.601 9.781 1.761 0.45 183142. 0.1277
|
|
111.98 1.0949 0.8152 0.0329 0.0442 0.645 4.514 1.760 480.690 0.510 7.828 1.661 0.45 184395. 0.1077
|
|
116.46 1.1387 0.7844 0.0246 0.0357 0.522 3.654 1.318 389.127 0.413 5.863 1.536 0.46 185686. 0.0862
|
|
120.94 1.1825 0.7206 0.0164 0.0268 0.392 2.745 0.876 292.238 0.310 3.895 1.359 0.46 187015. 0.0622
|
|
125.42 1.2263 0.5694 0.0081 0.0175 0.256 1.790 0.435 190.570 0.202 1.935 1.036 0.46 188380. 0.0334
|
|
129.89 1.2701 -0.0043 0.0000 0.0078 0.114 0.796 -0.001 84.728 0.090 -0.006 -0.008 0.46 189768. 0.0000
|
|
|
|
|
|
|
|
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 0.1301 0.0665 1.331 8.391 8.597 992.802 0.948 38.238 3.927 0.48 184760. 0.5631
|
|
4.98 0.0438 0.0835 0.1298 0.0682 1.365 8.601 8.580 1017.606 0.972 38.165 3.824 0.48 184982. 0.5478
|
|
9.96 0.0876 0.1622 0.1296 0.0700 1.402 8.838 8.563 1045.585 0.998 38.088 3.715 0.48 185240. 0.5315
|
|
14.94 0.1314 0.2357 0.1293 0.0721 1.444 9.101 8.544 1076.710 1.028 38.005 3.599 0.48 185538. 0.5144
|
|
19.92 0.1753 0.3038 0.1290 0.0744 1.490 9.389 8.522 1110.812 1.061 37.907 3.480 0.48 185879. 0.4967
|
|
24.89 0.2191 0.3664 0.1285 0.0769 1.539 9.699 8.495 1147.517 1.096 37.784 3.358 0.48 186266. 0.4785
|
|
29.87 0.2629 0.4236 0.1280 0.0794 1.591 10.026 8.459 1186.208 1.133 37.623 3.234 0.48 186700. 0.4599
|
|
34.85 0.3067 0.4754 0.1273 0.0821 1.644 10.362 8.410 1225.985 1.171 37.407 3.111 0.48 187185. 0.4412
|
|
39.83 0.3505 0.5222 0.1263 0.0848 1.697 10.698 8.345 1265.664 1.209 37.117 2.990 0.48 187722. 0.4224
|
|
44.81 0.3943 0.5643 0.1250 0.0873 1.748 11.020 8.258 1303.812 1.245 36.730 2.873 0.48 188312. 0.4036
|
|
49.79 0.4381 0.6022 0.1232 0.0897 1.795 11.316 8.144 1338.798 1.278 36.225 2.759 0.48 188957. 0.3850
|
|
54.77 0.4819 0.6364 0.1210 0.0917 1.836 11.570 7.999 1368.869 1.307 35.579 2.650 0.48 189657. 0.3665
|
|
59.75 0.5258 0.6671 0.1183 0.0932 1.867 11.767 7.818 1392.219 1.329 34.773 2.547 0.48 190413. 0.3482
|
|
64.72 0.5696 0.6948 0.1149 0.0942 1.887 11.892 7.596 1407.023 1.344 33.787 2.449 0.48 191224. 0.3300
|
|
69.70 0.6134 0.7198 0.1109 0.0945 1.893 11.930 7.330 1411.461 1.348 32.606 2.356 0.48 192089. 0.3119
|
|
74.68 0.6572 0.7424 0.1062 0.0940 1.883 11.865 7.018 1403.786 1.341 31.214 2.267 0.49 193009. 0.2937
|
|
79.66 0.7010 0.7627 0.1007 0.0926 1.854 11.686 6.657 1382.642 1.320 29.611 2.184 0.49 193980. 0.2755
|
|
84.64 0.7448 0.7809 0.0946 0.0903 1.807 11.390 6.253 1347.599 1.287 27.813 2.105 0.49 195004. 0.2573
|
|
89.62 0.7886 0.7972 0.0880 0.0870 1.742 10.981 5.812 1299.209 1.241 25.852 2.029 0.49 196077. 0.2392
|
|
94.60 0.8325 0.8113 0.0808 0.0829 1.661 10.468 5.342 1238.487 1.183 23.761 1.956 0.49 197199. 0.2211
|
|
99.58 0.8763 0.8232 0.0734 0.0781 1.564 9.859 4.850 1166.441 1.114 21.571 1.886 0.49 198368. 0.2031
|
|
104.56 0.9201 0.8325 0.0657 0.0726 1.454 9.161 4.340 1083.896 1.035 19.305 1.816 0.50 199584. 0.1850
|
|
109.53 0.9639 0.8385 0.0578 0.0664 1.330 8.380 3.817 991.487 0.947 16.979 1.746 0.50 200846. 0.1668
|
|
114.51 1.0077 0.8404 0.0497 0.0596 1.193 7.520 3.284 889.714 0.850 14.606 1.674 0.50 202153. 0.1483
|
|
119.49 1.0515 0.8364 0.0415 0.0522 1.045 6.584 2.742 779.004 0.744 12.198 1.597 0.50 203503. 0.1293
|
|
124.47 1.0953 0.8234 0.0332 0.0442 0.885 5.577 2.195 659.776 0.630 9.763 1.509 0.50 204897. 0.1093
|
|
129.45 1.1392 0.7948 0.0249 0.0357 0.714 4.501 1.644 532.510 0.509 7.314 1.401 0.51 206333. 0.0878
|
|
134.43 1.1830 0.7341 0.0165 0.0266 0.533 3.362 1.093 397.796 0.380 4.860 1.246 0.51 207810. 0.0637
|
|
139.41 1.2268 0.5868 0.0082 0.0172 0.344 2.167 0.543 256.400 0.245 2.414 0.960 0.51 209328. 0.0346
|
|
144.39 1.2706 -0.0056 0.0000 0.0073 0.146 0.923 -0.002 109.160 0.104 -0.009 -0.009 0.51 210870. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 11000
|
|
|
|
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 0.1303 0.0666 1.774 10.166 10.416 1323.078 1.149 46.330 3.571 0.52 203232. 0.5635
|
|
5.48 0.0438 0.0835 0.1300 0.0682 1.818 10.419 10.397 1355.940 1.177 46.246 3.478 0.52 203476. 0.5483
|
|
10.96 0.0877 0.1623 0.1298 0.0701 1.868 10.704 10.378 1393.093 1.209 46.162 3.379 0.52 203760. 0.5323
|
|
16.44 0.1315 0.2360 0.1295 0.0722 1.924 11.023 10.358 1434.525 1.245 46.071 3.275 0.52 204088. 0.5154
|
|
21.91 0.1753 0.3042 0.1292 0.0745 1.985 11.373 10.334 1480.053 1.285 45.965 3.167 0.52 204462. 0.4978
|
|
27.39 0.2191 0.3670 0.1289 0.0769 2.051 11.750 10.304 1529.229 1.328 45.832 3.056 0.52 204887. 0.4797
|
|
32.87 0.2630 0.4243 0.1284 0.0796 2.121 12.150 10.264 1581.269 1.373 45.656 2.944 0.53 205365. 0.4612
|
|
38.35 0.3068 0.4762 0.1277 0.0823 2.193 12.563 10.211 1635.004 1.419 45.418 2.833 0.53 205898. 0.4426
|
|
43.83 0.3506 0.5231 0.1268 0.0850 2.265 12.977 10.137 1688.857 1.466 45.091 2.723 0.53 206488. 0.4239
|
|
49.31 0.3944 0.5653 0.1255 0.0876 2.335 13.377 10.038 1740.882 1.511 44.650 2.615 0.53 207137. 0.4052
|
|
54.78 0.4383 0.6033 0.1239 0.0900 2.399 13.745 9.907 1788.844 1.553 44.066 2.512 0.53 207846. 0.3866
|
|
60.26 0.4821 0.6375 0.1218 0.0921 2.455 14.064 9.737 1830.325 1.589 43.310 2.413 0.53 208617. 0.3682
|
|
65.74 0.5259 0.6683 0.1191 0.0937 2.498 14.314 9.523 1862.825 1.617 42.358 2.319 0.53 209449. 0.3499
|
|
71.22 0.5698 0.6961 0.1158 0.0948 2.526 14.475 9.259 1883.828 1.635 41.185 2.229 0.53 210341. 0.3317
|
|
76.70 0.6136 0.7212 0.1118 0.0951 2.536 14.529 8.941 1890.838 1.641 39.770 2.145 0.53 211294. 0.3136
|
|
82.18 0.6574 0.7438 0.1071 0.0947 2.523 14.457 8.565 1881.466 1.633 38.096 2.065 0.53 212307. 0.2955
|
|
87.65 0.7012 0.7643 0.1017 0.0933 2.486 14.245 8.129 1853.841 1.609 36.159 1.989 0.54 213377. 0.2773
|
|
93.13 0.7451 0.7828 0.0955 0.0909 2.424 13.887 7.639 1807.332 1.569 33.979 1.917 0.54 214504. 0.2591
|
|
98.61 0.7889 0.7993 0.0888 0.0877 2.337 13.390 7.103 1742.662 1.513 31.596 1.849 0.54 215686. 0.2409
|
|
104.09 0.8327 0.8138 0.0817 0.0836 2.228 12.764 6.531 1661.207 1.442 29.051 1.783 0.54 216922. 0.2228
|
|
109.57 0.8765 0.8260 0.0742 0.0787 2.098 12.020 5.931 1564.349 1.358 26.382 1.720 0.54 218210. 0.2048
|
|
115.05 0.9204 0.8358 0.0664 0.0731 1.949 11.166 5.309 1453.226 1.262 23.616 1.657 0.55 219549. 0.1867
|
|
120.53 0.9642 0.8425 0.0584 0.0669 1.782 10.210 4.671 1328.709 1.153 20.776 1.594 0.55 220938. 0.1685
|
|
126.00 1.0080 0.8452 0.0503 0.0600 1.598 9.155 4.019 1191.480 1.034 17.877 1.530 0.55 222377. 0.1500
|
|
131.48 1.0519 0.8422 0.0420 0.0524 1.398 8.007 3.357 1042.118 0.905 14.933 1.461 0.55 223864. 0.1309
|
|
136.96 1.0957 0.8307 0.0336 0.0443 1.182 6.771 2.688 881.191 0.765 11.955 1.383 0.55 225398. 0.1109
|
|
142.44 1.1395 0.8041 0.0252 0.0357 0.951 5.450 2.014 709.341 0.616 8.957 1.288 0.56 226979. 0.0894
|
|
147.92 1.1833 0.7464 0.0167 0.0265 0.707 4.052 1.338 527.369 0.458 5.953 1.151 0.56 228605. 0.0651
|
|
153.40 1.2272 0.6029 0.0083 0.0169 0.451 2.584 0.665 336.311 0.292 2.957 0.897 0.56 230275. 0.0357
|
|
158.87 1.2710 -0.0067 0.0000 0.0069 0.184 1.055 -0.003 137.293 0.119 -0.013 -0.010 0.56 231971. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 12000
|
|
|
|
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 0.1304 0.0668 2.310 12.133 12.413 1722.527 1.371 55.214 3.269 0.57 221702. 0.5631
|
|
5.98 0.0438 0.0835 0.1302 0.0684 2.367 12.431 12.392 1764.931 1.404 55.121 3.185 0.57 221968. 0.5482
|
|
11.96 0.0877 0.1622 0.1300 0.0703 2.431 12.770 12.372 1812.986 1.443 55.029 3.095 0.57 222278. 0.5323
|
|
17.93 0.1315 0.2359 0.1298 0.0723 2.503 13.148 12.350 1866.723 1.485 54.933 3.001 0.57 222635. 0.5156
|
|
23.91 0.1754 0.3043 0.1295 0.0746 2.583 13.566 12.325 1925.960 1.533 54.822 2.903 0.57 223044. 0.4983
|
|
29.89 0.2192 0.3672 0.1292 0.0771 2.669 14.018 12.294 1990.188 1.584 54.684 2.802 0.57 223507. 0.4804
|
|
35.87 0.2630 0.4245 0.1288 0.0798 2.760 14.499 12.253 2058.458 1.638 54.500 2.700 0.57 224027. 0.4621
|
|
41.85 0.3069 0.4766 0.1282 0.0825 2.855 14.998 12.195 2129.307 1.694 54.245 2.598 0.57 224608. 0.4436
|
|
47.82 0.3507 0.5235 0.1273 0.0853 2.951 15.501 12.116 2200.701 1.751 53.891 2.497 0.57 225251. 0.4250
|
|
53.80 0.3946 0.5658 0.1262 0.0880 3.044 15.989 12.006 2270.070 1.806 53.403 2.399 0.58 225959. 0.4064
|
|
59.78 0.4384 0.6038 0.1246 0.0905 3.130 16.443 11.858 2334.411 1.858 52.746 2.304 0.58 226733. 0.3880
|
|
65.76 0.4822 0.6380 0.1226 0.0926 3.206 16.837 11.664 2390.455 1.902 51.884 2.213 0.58 227574. 0.3696
|
|
71.74 0.5261 0.6689 0.1200 0.0944 3.265 17.150 11.417 2434.806 1.938 50.784 2.127 0.58 228481. 0.3514
|
|
77.72 0.5699 0.6967 0.1168 0.0955 3.304 17.356 11.110 2464.060 1.961 49.416 2.045 0.58 229456. 0.3333
|
|
83.69 0.6138 0.7219 0.1128 0.0959 3.319 17.432 10.736 2474.860 1.969 47.754 1.968 0.58 230496. 0.3152
|
|
89.67 0.6576 0.7447 0.1081 0.0955 3.304 17.355 10.291 2464.001 1.961 45.776 1.894 0.58 231602. 0.2972
|
|
95.65 0.7014 0.7654 0.1027 0.0941 3.257 17.108 9.774 2428.956 1.933 43.476 1.825 0.59 232771. 0.2790
|
|
101.63 0.7453 0.7840 0.0966 0.0918 3.177 16.685 9.190 2368.822 1.885 40.878 1.760 0.59 234002. 0.2608
|
|
107.61 0.7891 0.8008 0.0898 0.0885 3.064 16.091 8.550 2284.513 1.818 38.029 1.697 0.59 235293. 0.2427
|
|
113.58 0.8329 0.8156 0.0826 0.0844 2.921 15.340 7.864 2177.857 1.733 34.981 1.638 0.59 236643. 0.2246
|
|
119.56 0.8768 0.8283 0.0751 0.0795 2.750 14.444 7.144 2050.714 1.632 31.778 1.580 0.59 238050. 0.2065
|
|
125.54 0.9206 0.8385 0.0672 0.0738 2.554 13.415 6.398 1904.618 1.516 28.457 1.524 0.60 239512. 0.1884
|
|
131.52 0.9645 0.8458 0.0592 0.0675 2.334 12.261 5.630 1740.746 1.385 25.042 1.467 0.60 241030. 0.1702
|
|
137.50 1.0083 0.8492 0.0509 0.0605 2.092 10.988 4.846 1560.007 1.241 21.554 1.409 0.60 242601. 0.1516
|
|
143.47 1.0521 0.8473 0.0425 0.0528 1.828 9.602 4.049 1363.172 1.085 18.009 1.347 0.60 244224. 0.1325
|
|
149.45 1.0960 0.8371 0.0341 0.0446 1.543 8.107 3.242 1150.986 0.916 14.422 1.278 0.60 245899. 0.1125
|
|
155.43 1.1398 0.8125 0.0255 0.0358 1.239 6.510 2.430 924.293 0.736 10.808 1.192 0.61 247625. 0.0909
|
|
161.41 1.1837 0.7576 0.0170 0.0265 0.917 4.819 1.615 684.147 0.544 7.183 1.071 0.61 249400. 0.0665
|
|
167.39 1.2275 0.6181 0.0084 0.0167 0.579 3.042 0.802 431.923 0.344 3.567 0.842 0.61 251223. 0.0369
|
|
173.36 1.2713 -0.0088 0.0000 0.0066 0.227 1.191 -0.004 169.094 0.135 -0.019 -0.012 0.62 253072. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 13000
|
|
|
|
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 0.1306 0.0671 2.952 14.310 14.589 2200.994 1.617 64.894 3.007 0.62 240172. 0.5615
|
|
6.52 0.0441 0.0837 0.1304 0.0687 3.024 14.660 14.567 2254.715 1.656 64.792 2.930 0.62 240461. 0.5469
|
|
13.03 0.0882 0.1628 0.1302 0.0706 3.106 15.057 14.545 2315.792 1.701 64.694 2.849 0.62 240799. 0.5312
|
|
19.55 0.1323 0.2368 0.1300 0.0727 3.197 15.502 14.522 2384.327 1.751 64.594 2.763 0.62 241189. 0.5148
|
|
26.07 0.1765 0.3054 0.1298 0.0750 3.299 15.995 14.497 2460.172 1.807 64.482 2.673 0.62 241635. 0.4976
|
|
32.58 0.2206 0.3686 0.1295 0.0775 3.410 16.532 14.466 2542.756 1.868 64.343 2.580 0.62 242140. 0.4799
|
|
39.10 0.2647 0.4262 0.1292 0.0802 3.528 17.106 14.423 2630.961 1.933 64.155 2.487 0.62 242709. 0.4618
|
|
45.62 0.3088 0.4785 0.1286 0.0830 3.652 17.704 14.364 2722.963 2.000 63.890 2.393 0.62 243344. 0.4434
|
|
52.13 0.3529 0.5256 0.1279 0.0858 3.777 18.310 14.278 2816.160 2.069 63.511 2.300 0.62 244048. 0.4249
|
|
58.65 0.3970 0.5680 0.1268 0.0886 3.899 18.902 14.158 2907.159 2.135 62.976 2.209 0.62 244822. 0.4064
|
|
65.17 0.4411 0.6060 0.1253 0.0912 4.012 19.453 13.993 2991.928 2.198 62.240 2.121 0.62 245669. 0.3880
|
|
71.68 0.4852 0.6403 0.1233 0.0935 4.112 19.934 13.772 3066.014 2.252 61.257 2.037 0.63 246590. 0.3697
|
|
78.20 0.5294 0.6711 0.1208 0.0953 4.190 20.316 13.486 3124.764 2.295 59.985 1.958 0.63 247584. 0.3515
|
|
84.72 0.5735 0.6990 0.1175 0.0964 4.242 20.568 13.126 3163.540 2.324 58.386 1.882 0.63 248652. 0.3334
|
|
91.23 0.6176 0.7242 0.1136 0.0969 4.261 20.661 12.685 3177.801 2.334 56.425 1.811 0.63 249793. 0.3153
|
|
97.75 0.6617 0.7470 0.1089 0.0964 4.242 20.567 12.158 3163.283 2.324 54.077 1.743 0.63 251006. 0.2972
|
|
104.27 0.7058 0.7678 0.1033 0.0950 4.180 20.264 11.542 3116.703 2.289 51.337 1.680 0.63 252288. 0.2790
|
|
110.78 0.7499 0.7866 0.0971 0.0926 4.073 19.746 10.844 3036.998 2.231 48.233 1.620 0.64 253637. 0.2608
|
|
117.30 0.7940 0.8035 0.0902 0.0892 3.923 19.021 10.078 2925.509 2.149 44.825 1.562 0.64 255053. 0.2425
|
|
123.82 0.8382 0.8185 0.0829 0.0849 3.734 18.105 9.257 2784.718 2.046 41.177 1.508 0.64 256533. 0.2243
|
|
130.33 0.8823 0.8314 0.0752 0.0798 3.510 17.016 8.395 2617.098 1.922 37.343 1.455 0.64 258076. 0.2061
|
|
136.85 0.9264 0.8418 0.0672 0.0739 3.252 15.764 7.501 2424.663 1.781 33.365 1.403 0.65 259679. 0.1879
|
|
143.37 0.9705 0.8494 0.0589 0.0673 2.962 14.362 6.581 2208.952 1.623 29.274 1.351 0.65 261342. 0.1695
|
|
149.88 1.0146 0.8530 0.0505 0.0601 2.643 12.816 5.642 1971.148 1.448 25.094 1.298 0.65 263064. 0.1508
|
|
156.40 1.0587 0.8511 0.0420 0.0522 2.296 11.133 4.686 1712.259 1.258 20.844 1.241 0.65 264843. 0.1314
|
|
162.92 1.1028 0.8406 0.0333 0.0437 1.922 9.319 3.719 1433.276 1.053 16.543 1.177 0.66 266678. 0.1110
|
|
169.44 1.1469 0.8145 0.0246 0.0346 1.523 7.382 2.745 1135.332 0.834 12.209 1.097 0.66 268568. 0.0888
|
|
175.95 1.1911 0.7543 0.0158 0.0250 1.099 5.331 1.768 819.875 0.602 7.862 0.978 0.66 270513. 0.0636
|
|
182.47 1.2352 0.5887 0.0071 0.0149 0.656 3.179 0.793 488.876 0.359 3.528 0.736 0.66 272509. 0.0320
|
|
188.99 1.2793
|
|
|
|
|
|
|
|
PROP RPM = 14000
|
|
|
|
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 0.1308 0.0678 3.725 16.772 16.945 2778.061 1.895 75.371 2.767 0.67 258639. 0.5569
|
|
6.98 0.0439 0.0825 0.1306 0.0694 3.813 17.168 16.920 2843.704 1.940 75.262 2.699 0.67 258949. 0.5428
|
|
13.95 0.0877 0.1606 0.1305 0.0712 3.914 17.620 16.898 2918.470 1.991 75.161 2.626 0.67 259310. 0.5278
|
|
20.93 0.1316 0.2339 0.1303 0.0733 4.026 18.127 16.875 3002.560 2.048 75.061 2.549 0.67 259726. 0.5120
|
|
27.90 0.1754 0.3020 0.1301 0.0756 4.152 18.691 16.851 3095.886 2.112 74.954 2.469 0.67 260201. 0.4955
|
|
34.88 0.2193 0.3648 0.1299 0.0780 4.288 19.307 16.822 3197.887 2.181 74.824 2.386 0.67 260740. 0.4785
|
|
41.86 0.2631 0.4223 0.1296 0.0807 4.435 19.968 16.782 3307.351 2.256 74.647 2.302 0.67 261345. 0.4610
|
|
48.83 0.3070 0.4746 0.1291 0.0835 4.589 20.661 16.725 3422.220 2.334 74.394 2.217 0.67 262021. 0.4433
|
|
55.81 0.3508 0.5218 0.1285 0.0864 4.746 21.369 16.642 3539.438 2.414 74.023 2.133 0.67 262770. 0.4254
|
|
62.79 0.3947 0.5643 0.1276 0.0892 4.901 22.066 16.521 3654.889 2.493 73.484 2.050 0.67 263594. 0.4075
|
|
69.76 0.4385 0.6026 0.1262 0.0919 5.047 22.722 16.350 3763.574 2.567 72.723 1.970 0.67 264495. 0.3896
|
|
76.74 0.4824 0.6371 0.1244 0.0942 5.176 23.303 16.116 3859.881 2.633 71.683 1.894 0.67 265474. 0.3717
|
|
83.71 0.5262 0.6682 0.1220 0.0961 5.281 23.774 15.807 3937.921 2.686 70.311 1.821 0.68 266533. 0.3540
|
|
90.69 0.5701 0.6963 0.1190 0.0974 5.353 24.100 15.413 3991.768 2.723 68.557 1.751 0.68 267671. 0.3362
|
|
97.67 0.6139 0.7217 0.1152 0.0980 5.385 24.243 14.924 4015.580 2.739 66.381 1.686 0.68 268886. 0.3184
|
|
104.64 0.6578 0.7448 0.1107 0.0977 5.369 24.172 14.332 4003.779 2.731 63.748 1.624 0.68 270178. 0.3005
|
|
111.62 0.7016 0.7658 0.1053 0.0964 5.299 23.858 13.635 3951.820 2.696 60.649 1.565 0.68 271545. 0.2826
|
|
118.60 0.7455 0.7849 0.0991 0.0942 5.173 23.291 12.840 3857.790 2.631 57.111 1.510 0.68 272985. 0.2645
|
|
125.57 0.7893 0.8022 0.0923 0.0909 4.993 22.477 11.961 3723.003 2.539 53.200 1.457 0.69 274494. 0.2464
|
|
132.55 0.8332 0.8176 0.0850 0.0867 4.761 21.436 11.014 3550.521 2.422 48.992 1.407 0.69 276073. 0.2283
|
|
139.52 0.8770 0.8311 0.0773 0.0816 4.484 20.186 10.016 3343.571 2.281 44.552 1.359 0.69 277718. 0.2103
|
|
146.50 0.9209 0.8423 0.0693 0.0758 4.164 18.745 8.978 3104.816 2.118 39.933 1.312 0.69 279428. 0.1921
|
|
153.48 0.9647 0.8508 0.0611 0.0692 3.804 17.124 7.907 2836.316 1.935 35.172 1.265 0.70 281202. 0.1739
|
|
160.45 1.0086 0.8558 0.0526 0.0620 3.406 15.333 6.812 2539.626 1.732 30.300 1.217 0.70 283037. 0.1553
|
|
167.43 1.0524 0.8558 0.0440 0.0541 2.972 13.379 5.697 2216.037 1.512 25.339 1.166 0.70 284934. 0.1361
|
|
174.40 1.0963 0.8483 0.0353 0.0456 2.503 11.270 4.566 1866.786 1.273 20.311 1.109 0.71 286891. 0.1159
|
|
181.38 1.1401 0.8272 0.0264 0.0364 2.003 9.016 3.425 1493.374 1.019 15.235 1.040 0.71 288907. 0.0941
|
|
188.36 1.1840 0.7774 0.0176 0.0268 1.472 6.628 2.279 1097.829 0.749 10.136 0.941 0.71 290980. 0.0695
|
|
195.33 1.2278 0.6443 0.0087 0.0167 0.916 4.123 1.133 682.960 0.466 5.039 0.752 0.72 293108. 0.0392
|
|
202.31 1.2717 -0.0100 0.0000 0.0062 0.338 1.522 -0.006 252.037 0.172 -0.028 -0.011 0.72 295261. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 15000
|
|
|
|
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 0.1310 0.0693 4.682 19.673 19.478 3491.367 2.223 86.638 2.530 0.71 277106. 0.5461
|
|
7.47 0.0438 0.0809 0.1308 0.0709 4.788 20.119 19.451 3570.507 2.273 86.519 2.471 0.71 277437. 0.5329
|
|
14.94 0.0877 0.1577 0.1307 0.0726 4.909 20.628 19.427 3660.879 2.331 86.413 2.407 0.71 277823. 0.5188
|
|
22.41 0.1315 0.2298 0.1305 0.0747 5.046 21.203 19.405 3762.795 2.395 86.315 2.339 0.71 278268. 0.5038
|
|
29.89 0.1753 0.2971 0.1304 0.0769 5.198 21.842 19.383 3876.248 2.468 86.215 2.268 0.72 278776. 0.4882
|
|
37.36 0.2192 0.3594 0.1302 0.0794 5.365 22.543 19.356 4000.667 2.547 86.097 2.194 0.72 279352. 0.4721
|
|
44.83 0.2630 0.4165 0.1299 0.0820 5.545 23.298 19.321 4134.720 2.632 85.939 2.119 0.72 279999. 0.4555
|
|
52.30 0.3068 0.4686 0.1296 0.0849 5.734 24.095 19.268 4276.021 2.722 85.706 2.044 0.72 280721. 0.4387
|
|
59.77 0.3507 0.5159 0.1291 0.0877 5.929 24.911 19.189 4420.906 2.814 85.354 1.969 0.72 281521. 0.4217
|
|
67.24 0.3945 0.5586 0.1283 0.0906 6.121 25.719 19.070 4564.269 2.906 84.824 1.895 0.72 282401. 0.4047
|
|
74.71 0.4383 0.5973 0.1271 0.0933 6.302 26.482 18.896 4699.730 2.992 84.051 1.824 0.72 283364. 0.3876
|
|
82.18 0.4822 0.6324 0.1254 0.0956 6.464 27.160 18.651 4820.094 3.069 82.962 1.755 0.72 284412. 0.3706
|
|
89.66 0.5260 0.6641 0.1232 0.0976 6.595 27.711 18.320 4917.876 3.131 81.489 1.690 0.72 285545. 0.3536
|
|
97.13 0.5698 0.6930 0.1203 0.0989 6.686 28.093 17.889 4985.665 3.174 79.570 1.627 0.73 286762. 0.3366
|
|
104.60 0.6136 0.7192 0.1167 0.0995 6.727 28.266 17.345 5016.274 3.193 77.151 1.568 0.73 288064. 0.3194
|
|
112.07 0.6575 0.7430 0.1122 0.0993 6.709 28.190 16.679 5002.859 3.185 74.190 1.512 0.73 289448. 0.3020
|
|
119.54 0.7013 0.7645 0.1069 0.0980 6.624 27.835 15.888 4939.747 3.145 70.671 1.459 0.73 290913. 0.2843
|
|
127.01 0.7451 0.7841 0.1007 0.0957 6.469 27.184 14.978 4824.299 3.071 66.623 1.408 0.73 292456. 0.2665
|
|
134.48 0.7890 0.8018 0.0939 0.0924 6.246 26.246 13.966 4657.789 2.965 62.123 1.360 0.74 294074. 0.2485
|
|
141.96 0.8328 0.8177 0.0866 0.0882 5.959 25.040 12.873 4443.747 2.829 57.259 1.314 0.74 295766. 0.2305
|
|
149.43 0.8766 0.8316 0.0788 0.0831 5.614 23.587 11.716 4185.999 2.665 52.114 1.269 0.74 297529. 0.2125
|
|
156.90 0.9205 0.8434 0.0707 0.0771 5.214 21.907 10.510 3887.871 2.475 46.748 1.226 0.74 299362. 0.1944
|
|
164.37 0.9643 0.8525 0.0623 0.0705 4.763 20.015 9.265 3552.017 2.261 41.210 1.183 0.75 301263. 0.1761
|
|
171.84 1.0081 0.8583 0.0537 0.0631 4.265 17.921 7.989 3180.469 2.025 35.534 1.139 0.75 303230. 0.1575
|
|
179.31 1.0520 0.8593 0.0450 0.0551 3.721 15.637 6.688 2775.078 1.767 29.747 1.093 0.75 305263. 0.1382
|
|
186.78 1.0958 0.8527 0.0361 0.0464 3.135 13.173 5.367 2337.832 1.488 23.873 1.041 0.76 307359. 0.1180
|
|
194.25 1.1396 0.8324 0.0271 0.0371 2.509 10.544 4.032 1871.198 1.191 17.935 0.977 0.76 309518. 0.0960
|
|
201.73 1.1835 0.7823 0.0181 0.0274 1.849 7.768 2.688 1378.560 0.878 11.958 0.885 0.76 311738. 0.0709
|
|
209.20 1.2273 0.6460 0.0090 0.0172 1.159 4.872 1.343 864.579 0.550 5.972 0.704 0.77 314017. 0.0399
|
|
216.67 1.2711 0.0009 0.0000 0.0066 0.449 1.887 0.001 334.794 0.213 0.003 0.001 0.77 316323. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 16000
|
|
|
|
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 0.1311 0.0720 5.908 23.273 22.184 4405.568 2.629 98.676 2.284 0.76 295570. 0.5260
|
|
7.97 0.0438 0.0780 0.1310 0.0736 6.034 23.770 22.155 4499.556 2.685 98.544 2.233 0.76 295923. 0.5140
|
|
15.93 0.0876 0.1522 0.1308 0.0753 6.178 24.338 22.129 4607.183 2.750 98.431 2.179 0.76 296334. 0.5011
|
|
23.90 0.1314 0.2222 0.1307 0.0773 6.342 24.981 22.107 4728.909 2.822 98.332 2.120 0.76 296808. 0.4875
|
|
31.86 0.1753 0.2877 0.1306 0.0795 6.524 25.699 22.086 4864.835 2.903 98.238 2.059 0.76 297349. 0.4732
|
|
39.83 0.2191 0.3485 0.1304 0.0820 6.724 26.489 22.063 5014.429 2.993 98.135 1.996 0.76 297962. 0.4583
|
|
47.80 0.2629 0.4045 0.1302 0.0846 6.941 27.344 22.032 5176.229 3.089 98.000 1.931 0.76 298650. 0.4431
|
|
55.76 0.3067 0.4559 0.1300 0.0874 7.171 28.249 21.987 5347.509 3.192 97.799 1.865 0.77 299418. 0.4276
|
|
63.73 0.3505 0.5028 0.1296 0.0903 7.408 29.181 21.916 5523.871 3.297 97.484 1.800 0.77 300269. 0.4119
|
|
71.70 0.3943 0.5455 0.1289 0.0932 7.642 30.106 21.805 5698.967 3.401 96.990 1.735 0.77 301205. 0.3963
|
|
79.66 0.4381 0.5844 0.1279 0.0959 7.864 30.980 21.636 5864.530 3.500 96.239 1.673 0.77 302229. 0.3806
|
|
87.63 0.4820 0.6200 0.1264 0.0983 8.061 31.754 21.390 6011.015 3.588 95.142 1.614 0.77 303344. 0.3650
|
|
95.59 0.5258 0.6528 0.1244 0.1002 8.219 32.375 21.046 6128.598 3.658 93.612 1.558 0.77 304550. 0.3494
|
|
103.56 0.5696 0.6829 0.1217 0.1015 8.325 32.795 20.586 6207.965 3.705 91.566 1.504 0.77 305847. 0.3337
|
|
111.53 0.6134 0.7105 0.1182 0.1020 8.369 32.966 19.994 6240.511 3.725 88.935 1.453 0.78 307235. 0.3177
|
|
119.49 0.6572 0.7359 0.1138 0.1017 8.339 32.849 19.259 6218.329 3.711 85.664 1.405 0.78 308711. 0.3014
|
|
127.46 0.7010 0.7591 0.1086 0.1003 8.227 32.409 18.374 6134.959 3.662 81.729 1.358 0.78 310274. 0.2847
|
|
135.43 0.7448 0.7802 0.1025 0.0979 8.029 31.630 17.347 5987.467 3.574 77.157 1.314 0.78 311920. 0.2676
|
|
143.39 0.7887 0.7992 0.0957 0.0945 7.748 30.521 16.195 5777.630 3.448 72.036 1.271 0.79 313648. 0.2502
|
|
151.36 0.8325 0.8163 0.0883 0.0901 7.389 29.107 14.944 5509.987 3.289 66.471 1.230 0.79 315454. 0.2325
|
|
159.32 0.8763 0.8312 0.0805 0.0848 6.959 27.413 13.615 5189.344 3.097 60.559 1.190 0.79 317336. 0.2147
|
|
167.29 0.9201 0.8438 0.0723 0.0788 6.463 25.460 12.225 4819.566 2.876 54.377 1.150 0.79 319292. 0.1967
|
|
175.26 0.9639 0.8536 0.0638 0.0720 5.906 23.264 10.787 4403.795 2.628 47.980 1.111 0.80 321320. 0.1784
|
|
183.22 1.0077 0.8599 0.0550 0.0645 5.290 20.838 9.310 3944.627 2.354 41.412 1.071 0.80 323419. 0.1597
|
|
191.19 1.0515 0.8611 0.0461 0.0563 4.619 18.197 7.802 3444.674 2.056 34.704 1.027 0.80 325587. 0.1403
|
|
199.16 1.0954 0.8538 0.0371 0.0475 3.899 15.359 6.268 2907.347 1.735 27.882 0.978 0.81 327823. 0.1197
|
|
207.12 1.1392 0.8308 0.0279 0.0382 3.134 12.347 4.715 2337.242 1.395 20.972 0.915 0.81 330126. 0.0971
|
|
215.09 1.1830 0.7734 0.0186 0.0285 2.334 9.194 3.147 1740.376 1.039 13.999 0.820 0.81 332494. 0.0711
|
|
223.05 1.2268 0.6203 0.0093 0.0184 1.508 5.941 1.573 1124.597 0.671 6.996 0.634 0.82 334924. 0.0389
|
|
231.02 1.2706 -0.0005 0.0000 0.0082 0.669 2.636 -0.001 498.989 0.298 -0.002 0.000 0.82 337387. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 17000
|
|
|
|
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 0.1312 0.0766 7.540 27.956 25.057 5622.871 3.158 111.456 2.021 0.81 314032. 0.4947
|
|
8.47 0.0438 0.0735 0.1310 0.0782 7.688 28.505 25.023 5733.277 3.221 111.303 1.980 0.81 314407. 0.4842
|
|
16.93 0.0876 0.1436 0.1309 0.0799 7.859 29.136 24.994 5860.204 3.292 111.174 1.935 0.81 314843. 0.4729
|
|
25.40 0.1315 0.2100 0.1307 0.0818 8.052 29.853 24.970 6004.253 3.373 111.067 1.886 0.81 315346. 0.4609
|
|
33.86 0.1753 0.2724 0.1306 0.0840 8.268 30.655 24.949 6165.668 3.463 110.973 1.835 0.81 315921. 0.4483
|
|
42.33 0.2191 0.3307 0.1305 0.0865 8.507 31.542 24.928 6344.023 3.564 110.881 1.782 0.81 316571. 0.4351
|
|
50.79 0.2629 0.3847 0.1304 0.0891 8.767 32.505 24.903 6537.833 3.672 110.769 1.728 0.81 317301. 0.4216
|
|
59.26 0.3067 0.4344 0.1302 0.0919 9.044 33.531 24.866 6744.055 3.788 110.604 1.672 0.81 318116. 0.4078
|
|
67.72 0.3506 0.4801 0.1299 0.0948 9.330 34.592 24.806 6957.525 3.908 110.337 1.617 0.81 319017. 0.3938
|
|
76.19 0.3944 0.5220 0.1294 0.0977 9.616 35.651 24.708 7170.406 4.028 109.901 1.563 0.82 320009. 0.3799
|
|
84.65 0.4382 0.5606 0.1286 0.1005 9.886 36.652 24.552 7371.917 4.141 109.207 1.511 0.82 321095. 0.3660
|
|
93.12 0.4820 0.5964 0.1273 0.1029 10.123 37.533 24.314 7548.922 4.240 108.149 1.461 0.82 322276. 0.3522
|
|
101.58 0.5258 0.6298 0.1255 0.1048 10.309 38.221 23.969 7687.367 4.318 106.613 1.414 0.82 323555. 0.3385
|
|
110.05 0.5697 0.6612 0.1230 0.1060 10.426 38.656 23.492 7774.881 4.367 104.493 1.370 0.82 324933. 0.3248
|
|
118.51 0.6135 0.6907 0.1197 0.1063 10.461 38.785 22.863 7800.858 4.382 101.696 1.329 0.82 326407. 0.3108
|
|
126.98 0.6573 0.7183 0.1155 0.1057 10.402 38.565 22.066 7756.636 4.357 98.151 1.290 0.83 327977. 0.2964
|
|
135.44 0.7011 0.7440 0.1104 0.1041 10.239 37.963 21.092 7635.527 4.289 93.818 1.253 0.83 329640. 0.2814
|
|
143.91 0.7449 0.7677 0.1044 0.1014 9.971 36.967 19.947 7435.218 4.177 88.723 1.217 0.83 331392. 0.2657
|
|
152.37 0.7888 0.7894 0.0977 0.0976 9.600 35.594 18.651 7158.945 4.021 82.961 1.182 0.83 333231. 0.2495
|
|
160.84 0.8326 0.8089 0.0902 0.0929 9.137 33.876 17.234 6813.417 3.827 76.655 1.147 0.84 335153. 0.2329
|
|
169.30 0.8764 0.8262 0.0823 0.0873 8.590 31.847 15.720 6405.343 3.598 69.922 1.113 0.84 337156. 0.2158
|
|
177.77 0.9202 0.8409 0.0740 0.0810 7.966 29.533 14.131 5939.885 3.337 62.854 1.079 0.84 339238. 0.1983
|
|
186.23 0.9640 0.8525 0.0654 0.0739 7.271 26.957 12.482 5421.935 3.046 55.519 1.044 0.85 341397. 0.1804
|
|
194.70 1.0079 0.8593 0.0565 0.0662 6.515 24.155 10.783 4858.354 2.729 47.963 1.007 0.85 343630. 0.1616
|
|
203.16 1.0517 0.8590 0.0474 0.0580 5.703 21.145 9.043 4252.990 2.389 40.225 0.964 0.85 345937. 0.1418
|
|
211.63 1.0955 0.8477 0.0381 0.0492 4.840 17.943 7.270 3608.852 2.027 32.338 0.914 0.86 348315. 0.1205
|
|
220.09 1.1393 0.8161 0.0286 0.0400 3.934 14.585 5.470 2933.464 1.648 24.332 0.846 0.86 350764. 0.0967
|
|
228.56 1.1831 0.7417 0.0191 0.0305 3.000 11.122 3.651 2237.059 1.257 16.240 0.740 0.86 353281. 0.0692
|
|
237.02 1.2269 0.5607 0.0095 0.0209 2.054 7.616 1.822 1531.833 0.860 8.106 0.540 0.87 355865. 0.0356
|
|
245.49 1.2708 -0.0013 0.0000 0.0113 1.115 4.134 -0.002 831.405 0.467 -0.010 -0.001 0.87 358495. 0.0000
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PROP RPM = 18000
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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 0.1309 0.0831 9.704 33.978 28.037 7236.077 3.839 124.709 1.757 0.86 332504. 0.4550
|
|
8.98 0.0439 0.0679 0.1307 0.0846 9.874 34.574 27.994 7362.833 3.906 124.518 1.725 0.86 332902. 0.4461
|
|
17.96 0.0878 0.1329 0.1306 0.0862 10.071 35.265 27.958 7510.106 3.984 124.358 1.689 0.86 333364. 0.4366
|
|
26.94 0.1317 0.1948 0.1304 0.0882 10.297 36.057 27.929 7678.843 4.074 124.227 1.650 0.86 333897. 0.4263
|
|
35.91 0.1756 0.2532 0.1303 0.0904 10.553 36.953 27.905 7869.550 4.175 124.122 1.608 0.86 334506. 0.4154
|
|
44.89 0.2195 0.3080 0.1302 0.0928 10.838 37.950 27.884 8081.934 4.288 124.029 1.565 0.86 335195. 0.4041
|
|
53.87 0.2634 0.3590 0.1301 0.0955 11.150 39.042 27.862 8314.497 4.411 123.931 1.520 0.86 335968. 0.3923
|
|
62.85 0.3073 0.4062 0.1300 0.0983 11.484 40.213 27.832 8563.831 4.543 123.796 1.474 0.86 336830. 0.3803
|
|
71.83 0.3512 0.4497 0.1298 0.1013 11.831 41.428 27.782 8822.626 4.681 123.573 1.428 0.86 337785. 0.3681
|
|
80.81 0.3951 0.4900 0.1294 0.1043 12.181 42.653 27.698 9083.497 4.819 123.201 1.383 0.86 338835. 0.3559
|
|
89.79 0.4390 0.5272 0.1287 0.1072 12.516 43.824 27.560 9332.841 4.951 122.586 1.339 0.87 339983. 0.3438
|
|
98.76 0.4828 0.5621 0.1277 0.1097 12.810 44.856 27.340 9552.621 5.068 121.607 1.298 0.87 341233. 0.3319
|
|
107.74 0.5267 0.5951 0.1261 0.1116 13.038 45.654 27.007 9722.484 5.158 120.126 1.260 0.87 342587. 0.3202
|
|
116.72 0.5706 0.6268 0.1239 0.1128 13.172 46.124 26.529 9822.601 5.211 118.002 1.225 0.87 344047. 0.3085
|
|
125.70 0.6145 0.6575 0.1209 0.1130 13.193 46.196 25.878 9837.960 5.219 115.107 1.193 0.87 345611. 0.2968
|
|
134.68 0.6584 0.6869 0.1169 0.1121 13.088 45.827 25.033 9759.401 5.178 111.349 1.163 0.88 347278. 0.2846
|
|
143.66 0.7023 0.7150 0.1120 0.1100 12.847 44.985 23.981 9580.111 5.082 106.666 1.135 0.88 349045. 0.2719
|
|
152.64 0.7462 0.7417 0.1061 0.1068 12.470 43.666 22.724 9299.204 4.933 101.076 1.108 0.88 350908. 0.2583
|
|
161.61 0.7901 0.7666 0.0994 0.1025 11.966 41.899 21.285 8922.836 4.734 94.677 1.082 0.88 352864. 0.2441
|
|
170.59 0.8340 0.7896 0.0920 0.0972 11.348 39.735 19.698 8462.092 4.489 87.615 1.056 0.89 354910. 0.2291
|
|
179.57 0.8779 0.8104 0.0840 0.0910 10.630 37.223 17.991 7927.032 4.205 80.023 1.029 0.89 357041. 0.2135
|
|
188.55 0.9218 0.8286 0.0756 0.0841 9.823 34.398 16.190 7325.371 3.886 72.012 1.002 0.89 359256. 0.1972
|
|
197.53 0.9657 0.8438 0.0669 0.0765 8.935 31.288 14.314 6663.144 3.535 63.668 0.974 0.90 361552. 0.1803
|
|
206.51 1.0096 0.8524 0.0578 0.0684 7.993 27.990 12.373 5960.693 3.162 55.036 0.942 0.90 363927. 0.1619
|
|
215.49 1.0535 0.8494 0.0485 0.0601 7.018 24.575 10.375 5233.595 2.777 46.150 0.899 0.90 366380. 0.1416
|
|
224.46 1.0974 0.8290 0.0389 0.0515 6.015 21.062 8.331 4485.439 2.380 37.055 0.842 0.91 368908. 0.1189
|
|
233.44 1.1413 0.7811 0.0292 0.0427 4.983 17.450 6.253 3716.129 1.971 27.813 0.763 0.91 371510. 0.0933
|
|
242.42 1.1852 0.6810 0.0194 0.0338 3.944 13.812 4.156 2941.358 1.560 18.485 0.641 0.92 374185. 0.0639
|
|
251.40 1.2291 0.4726 0.0096 0.0250 2.921 10.227 2.059 2177.943 1.155 9.159 0.429 0.92 376931. 0.0301
|
|
260.38 1.2730 -0.0026 0.0000 0.0166 1.934 6.771 -0.007 1441.966 0.765 -0.033 -0.002 0.92 379735. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 19000
|
|
|
|
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 0.1296 0.0898 12.329 40.897 30.917 9193.438 4.621 137.520 1.525 0.90 351026. 0.4147
|
|
9.53 0.0441 0.0627 0.1294 0.0911 12.510 41.499 30.858 9328.578 4.688 137.258 1.500 0.90 351448. 0.4075
|
|
19.06 0.0883 0.1231 0.1291 0.0926 12.724 42.208 30.807 9488.134 4.769 137.029 1.473 0.90 351940. 0.3997
|
|
28.60 0.1324 0.1808 0.1290 0.0945 12.973 43.034 30.763 9673.626 4.862 136.835 1.442 0.91 352506. 0.3912
|
|
38.13 0.1766 0.2356 0.1288 0.0965 13.257 43.979 30.726 9886.104 4.969 136.671 1.410 0.91 353153. 0.3821
|
|
47.66 0.2207 0.2873 0.1287 0.0989 13.579 45.045 30.694 10125.805 5.089 136.528 1.375 0.91 353886. 0.3725
|
|
57.19 0.2649 0.3356 0.1285 0.1015 13.935 46.228 30.664 10391.636 5.223 136.392 1.338 0.91 354708. 0.3624
|
|
66.72 0.3090 0.3805 0.1284 0.1043 14.323 47.513 30.628 10680.493 5.368 136.234 1.301 0.91 355624. 0.3520
|
|
76.25 0.3532 0.4220 0.1282 0.1073 14.733 48.873 30.578 10986.302 5.522 136.012 1.262 0.91 356638. 0.3413
|
|
85.79 0.3973 0.4604 0.1278 0.1103 15.152 50.264 30.499 11299.000 5.679 135.661 1.224 0.91 357753. 0.3306
|
|
95.32 0.4415 0.4961 0.1273 0.1133 15.561 51.620 30.371 11603.841 5.832 135.091 1.187 0.91 358973. 0.3199
|
|
104.85 0.4856 0.5294 0.1265 0.1160 15.930 52.846 30.166 11879.274 5.970 134.177 1.152 0.92 360300. 0.3093
|
|
114.38 0.5298 0.5609 0.1251 0.1182 16.231 53.843 29.851 12103.540 6.083 132.779 1.119 0.92 361736. 0.2989
|
|
123.91 0.5739 0.5910 0.1232 0.1196 16.433 54.512 29.394 12253.928 6.159 130.746 1.088 0.92 363283. 0.2884
|
|
133.44 0.6181 0.6201 0.1205 0.1201 16.502 54.740 28.757 12305.206 6.185 127.912 1.060 0.92 364942. 0.2779
|
|
142.98 0.6622 0.6485 0.1170 0.1195 16.406 54.422 27.905 12233.734 6.149 124.120 1.035 0.92 366711. 0.2672
|
|
152.51 0.7064 0.6763 0.1124 0.1174 16.122 53.481 26.811 12022.220 6.042 119.257 1.012 0.93 368589. 0.2561
|
|
162.04 0.7505 0.7036 0.1068 0.1139 15.643 51.891 25.472 11664.809 5.863 113.300 0.990 0.93 370572. 0.2444
|
|
171.57 0.7946 0.7301 0.1002 0.1091 14.984 49.708 23.912 11173.934 5.616 106.361 0.971 0.93 372657. 0.2321
|
|
181.10 0.8388 0.7554 0.0929 0.1032 14.171 47.009 22.167 10567.213 5.311 98.598 0.951 0.94 374839. 0.2190
|
|
190.63 0.8829 0.7791 0.0850 0.0963 13.226 43.873 20.271 9862.259 4.957 90.165 0.932 0.94 377114. 0.2052
|
|
200.17 0.9271 0.8008 0.0765 0.0886 12.167 40.363 18.254 9073.265 4.560 81.195 0.913 0.94 379479. 0.1906
|
|
209.70 0.9712 0.8197 0.0677 0.0802 11.011 36.526 16.140 8210.659 4.127 71.791 0.892 0.95 381930. 0.1751
|
|
219.23 1.0154 0.8320 0.0584 0.0713 9.796 32.497 13.942 7305.151 3.672 62.014 0.866 0.95 384466. 0.1580
|
|
228.76 1.0595 0.8272 0.0489 0.0626 8.600 28.530 11.663 6413.309 3.223 51.876 0.825 0.95 387084. 0.1377
|
|
238.29 1.1037 0.7905 0.0390 0.0545 7.481 24.816 9.307 5578.406 2.804 41.397 0.757 0.96 389782. 0.1129
|
|
247.83 1.1478 0.7188 0.0290 0.0463 6.364 21.110 6.922 4745.295 2.385 30.789 0.662 0.96 392558. 0.0851
|
|
257.36 1.1920 0.5912 0.0191 0.0384 5.275 17.500 4.545 3933.766 1.977 20.216 0.524 0.97 395410. 0.0546
|
|
266.89 1.2361 0.3726 0.0093 0.0309 4.240 14.066 2.220 3162.008 1.589 9.874 0.318 0.97 398336. 0.0232
|
|
276.42 1.2803 -0.0065 -0.0001 0.0239 3.277 10.871 -0.029 2443.695 1.228 -0.128 -0.005 0.98 401332. 0.0000
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