464 lines
82 KiB
Plaintext
464 lines
82 KiB
Plaintext
20x15E (20x15E.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 0.1008 0.0431 0.011 0.700 0.514 8.277 0.079 2.286 28.157 0.08 36633. 0.5922
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0.59 0.0309 0.0702 0.0999 0.0440 0.011 0.714 0.510 8.447 0.081 2.267 27.362 0.08 36663. 0.5730
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1.17 0.0618 0.1363 0.0990 0.0449 0.012 0.729 0.505 8.620 0.082 2.245 26.558 0.08 36696. 0.5536
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1.76 0.0927 0.1982 0.0979 0.0458 0.012 0.743 0.499 8.794 0.084 2.221 25.751 0.08 36733. 0.5338
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2.34 0.1236 0.2561 0.0967 0.0467 0.012 0.758 0.493 8.965 0.086 2.193 24.947 0.08 36774. 0.5139
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2.93 0.1545 0.3099 0.0953 0.0475 0.012 0.772 0.486 9.130 0.087 2.162 24.149 0.08 36819. 0.4940
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3.51 0.1854 0.3597 0.0938 0.0484 0.012 0.785 0.478 9.285 0.089 2.127 23.363 0.08 36869. 0.4740
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4.10 0.2163 0.4058 0.0921 0.0491 0.013 0.797 0.469 9.425 0.090 2.088 22.590 0.08 36923. 0.4541
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4.68 0.2473 0.4483 0.0901 0.0497 0.013 0.807 0.460 9.546 0.091 2.044 21.835 0.08 36982. 0.4343
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5.27 0.2782 0.4873 0.0880 0.0502 0.013 0.815 0.449 9.642 0.092 1.995 21.098 0.08 37045. 0.4145
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5.85 0.3091 0.5230 0.0856 0.0506 0.013 0.821 0.436 9.708 0.093 1.940 20.381 0.08 37114. 0.3949
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6.44 0.3400 0.5557 0.0829 0.0507 0.013 0.823 0.423 9.738 0.093 1.880 19.685 0.08 37188. 0.3754
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7.02 0.3709 0.5854 0.0799 0.0507 0.013 0.822 0.408 9.727 0.093 1.813 19.008 0.08 37267. 0.3561
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7.61 0.4018 0.6122 0.0767 0.0504 0.013 0.817 0.391 9.669 0.092 1.740 18.351 0.08 37350. 0.3367
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8.20 0.4327 0.6363 0.0732 0.0498 0.013 0.808 0.373 9.559 0.091 1.660 17.710 0.08 37439. 0.3174
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8.78 0.4636 0.6576 0.0694 0.0489 0.013 0.794 0.354 9.392 0.090 1.573 17.083 0.08 37533. 0.2981
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9.37 0.4945 0.6760 0.0653 0.0477 0.012 0.775 0.333 9.167 0.088 1.480 16.464 0.08 37633. 0.2786
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9.95 0.5254 0.6913 0.0609 0.0463 0.012 0.751 0.310 8.885 0.085 1.381 15.847 0.08 37737. 0.2590
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10.54 0.5563 0.7032 0.0563 0.0445 0.011 0.723 0.287 8.550 0.082 1.277 15.225 0.08 37846. 0.2393
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11.12 0.5872 0.7113 0.0515 0.0425 0.011 0.690 0.263 8.164 0.078 1.168 14.588 0.08 37960. 0.2193
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11.71 0.6181 0.7148 0.0466 0.0403 0.010 0.653 0.237 7.731 0.074 1.056 13.927 0.08 38080. 0.1991
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12.29 0.6490 0.7128 0.0415 0.0378 0.010 0.613 0.212 7.254 0.069 0.941 13.227 0.08 38204. 0.1785
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12.88 0.6800 0.7041 0.0363 0.0351 0.009 0.569 0.185 6.736 0.064 0.824 12.471 0.08 38333. 0.1575
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13.46 0.7109 0.6867 0.0311 0.0322 0.008 0.522 0.158 6.179 0.059 0.705 11.635 0.08 38467. 0.1359
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14.05 0.7418 0.6580 0.0258 0.0291 0.007 0.472 0.132 5.587 0.053 0.585 10.683 0.08 38605. 0.1137
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14.63 0.7727 0.6134 0.0205 0.0258 0.007 0.420 0.105 4.964 0.047 0.465 9.561 0.08 38749. 0.0907
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15.22 0.8036 0.5459 0.0153 0.0225 0.006 0.365 0.078 4.314 0.041 0.346 8.182 0.08 38897. 0.0670
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15.80 0.8345 0.4429 0.0101 0.0190 0.005 0.308 0.051 3.643 0.035 0.228 6.392 0.08 39050. 0.0425
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16.39 0.8654 0.2801 0.0050 0.0154 0.004 0.250 0.025 2.956 0.028 0.113 3.898 0.08 39208. 0.0182
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16.98 0.8963 0.0033 0.0000 0.0118 0.003 0.191 0.000 2.260 0.022 0.001 0.044 0.08 39370. 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 0.1011 0.0403 0.083 2.619 2.062 61.960 0.296 9.173 15.096 0.16 73265. 0.6360
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1.18 0.0311 0.0755 0.1003 0.0413 0.085 2.678 2.045 63.378 0.303 9.098 14.637 0.16 73325. 0.6142
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2.35 0.0621 0.1462 0.0993 0.0422 0.087 2.740 2.026 64.828 0.310 9.013 14.176 0.16 73392. 0.5920
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3.53 0.0932 0.2122 0.0983 0.0432 0.089 2.801 2.005 66.288 0.317 8.916 13.716 0.16 73466. 0.5697
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4.70 0.1242 0.2735 0.0971 0.0441 0.091 2.862 1.980 67.733 0.323 8.807 13.259 0.16 73549. 0.5474
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5.88 0.1553 0.3302 0.0957 0.0450 0.093 2.922 1.952 69.133 0.330 8.684 12.808 0.16 73640. 0.5250
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7.06 0.1863 0.3826 0.0942 0.0459 0.094 2.978 1.921 70.455 0.336 8.544 12.366 0.16 73740. 0.5028
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8.23 0.2174 0.4308 0.0924 0.0466 0.096 3.029 1.886 71.662 0.342 8.387 11.934 0.16 73849. 0.4808
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9.41 0.2484 0.4750 0.0905 0.0473 0.098 3.073 1.846 72.713 0.347 8.210 11.514 0.16 73967. 0.4590
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10.59 0.2795 0.5155 0.0883 0.0479 0.099 3.109 1.802 73.567 0.351 8.013 11.107 0.16 74096. 0.4374
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11.76 0.3105 0.5525 0.0859 0.0483 0.099 3.135 1.752 74.176 0.354 7.794 10.714 0.16 74234. 0.4161
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12.94 0.3416 0.5862 0.0832 0.0485 0.100 3.148 1.697 74.496 0.356 7.550 10.335 0.16 74383. 0.3950
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14.11 0.3726 0.6169 0.0803 0.0485 0.100 3.147 1.637 74.477 0.356 7.281 9.969 0.16 74542. 0.3742
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15.29 0.4037 0.6447 0.0770 0.0482 0.099 3.130 1.571 74.073 0.354 6.986 9.617 0.16 74711. 0.3536
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16.47 0.4347 0.6697 0.0734 0.0477 0.098 3.095 1.498 73.239 0.350 6.663 9.277 0.16 74890. 0.3331
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17.64 0.4658 0.6921 0.0696 0.0468 0.096 3.040 1.419 71.936 0.343 6.312 8.947 0.16 75080. 0.3127
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18.82 0.4968 0.7117 0.0654 0.0457 0.094 2.965 1.334 70.149 0.335 5.934 8.626 0.16 75280. 0.2923
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20.00 0.5279 0.7285 0.0610 0.0442 0.091 2.869 1.244 67.891 0.324 5.533 8.311 0.16 75491. 0.2719
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21.17 0.5589 0.7423 0.0563 0.0424 0.087 2.755 1.149 65.183 0.311 5.112 7.997 0.16 75711. 0.2515
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22.35 0.5900 0.7526 0.0515 0.0404 0.083 2.622 1.051 62.050 0.296 4.674 7.681 0.16 75942. 0.2310
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23.52 0.6210 0.7589 0.0465 0.0381 0.078 2.473 0.949 58.513 0.279 4.222 7.358 0.16 76182. 0.2103
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24.70 0.6521 0.7603 0.0414 0.0355 0.073 2.307 0.845 54.597 0.261 3.759 7.021 0.16 76432. 0.1894
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25.88 0.6832 0.7558 0.0362 0.0328 0.067 2.127 0.739 50.323 0.240 3.288 6.662 0.16 76693. 0.1680
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27.05 0.7142 0.7435 0.0310 0.0298 0.061 1.932 0.632 45.718 0.218 2.811 6.269 0.16 76963. 0.1462
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28.23 0.7453 0.7206 0.0257 0.0266 0.055 1.725 0.524 40.809 0.195 2.330 5.823 0.16 77243. 0.1236
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29.41 0.7763 0.6826 0.0204 0.0232 0.048 1.506 0.416 35.631 0.170 1.850 5.295 0.16 77532. 0.1002
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30.58 0.8074 0.6212 0.0151 0.0197 0.041 1.277 0.309 30.220 0.144 1.373 4.633 0.16 77831. 0.0755
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31.76 0.8384 0.5206 0.0100 0.0160 0.033 1.041 0.203 24.624 0.118 0.903 3.739 0.16 78140. 0.0494
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32.93 0.8695 0.3457 0.0049 0.0123 0.025 0.799 0.100 18.897 0.090 0.444 2.394 0.16 78458. 0.0222
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34.11 0.9005 -0.0018 0.0000 0.0085 0.018 0.553 0.000 13.087 0.062 -0.002 -0.012 0.17 78783. 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 0.1014 0.0392 0.273 5.730 4.655 203.377 0.647 20.705 10.381 0.24 109896. 0.6571
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1.77 0.0311 0.0779 0.1006 0.0402 0.279 5.868 4.618 208.271 0.663 20.539 10.056 0.24 109986. 0.6340
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3.54 0.0622 0.1508 0.0997 0.0411 0.286 6.009 4.575 213.284 0.679 20.351 9.730 0.24 110086. 0.6106
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5.30 0.0933 0.2186 0.0987 0.0421 0.293 6.152 4.527 218.341 0.695 20.137 9.405 0.24 110198. 0.5871
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7.07 0.1244 0.2815 0.0975 0.0431 0.300 6.293 4.473 223.356 0.711 19.894 9.082 0.24 110322. 0.5635
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8.84 0.1556 0.3396 0.0961 0.0440 0.306 6.430 4.411 228.229 0.726 19.618 8.765 0.24 110459. 0.5401
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10.61 0.1867 0.3931 0.0946 0.0449 0.312 6.560 4.340 232.844 0.741 19.307 8.455 0.24 110609. 0.5168
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12.37 0.2178 0.4423 0.0929 0.0457 0.318 6.679 4.261 237.074 0.755 18.954 8.153 0.24 110773. 0.4938
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14.14 0.2489 0.4873 0.0909 0.0464 0.323 6.784 4.172 240.779 0.766 18.559 7.860 0.24 110952. 0.4710
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15.91 0.2800 0.5284 0.0887 0.0470 0.327 6.869 4.073 243.813 0.776 18.115 7.576 0.24 111145. 0.4486
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17.68 0.3111 0.5660 0.0863 0.0475 0.330 6.931 3.961 246.016 0.783 17.620 7.303 0.24 111354. 0.4265
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19.45 0.3422 0.6002 0.0836 0.0477 0.332 6.965 3.838 247.228 0.787 17.071 7.041 0.24 111577. 0.4047
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21.21 0.3733 0.6314 0.0807 0.0477 0.332 6.967 3.701 247.282 0.787 16.464 6.789 0.24 111816. 0.3832
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22.98 0.4045 0.6596 0.0774 0.0475 0.330 6.931 3.551 246.016 0.783 15.797 6.548 0.24 112071. 0.3620
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24.75 0.4356 0.6852 0.0738 0.0469 0.326 6.854 3.387 243.272 0.774 15.066 6.315 0.24 112342. 0.3410
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26.52 0.4667 0.7081 0.0699 0.0461 0.320 6.731 3.209 238.912 0.760 14.271 6.091 0.24 112627. 0.3201
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28.28 0.4978 0.7284 0.0657 0.0449 0.312 6.561 3.016 232.885 0.741 13.416 5.874 0.24 112929. 0.2993
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30.05 0.5289 0.7460 0.0613 0.0434 0.302 6.346 2.812 225.227 0.717 12.507 5.663 0.24 113246. 0.2786
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31.82 0.5600 0.7608 0.0566 0.0417 0.290 6.086 2.597 216.009 0.688 11.553 5.454 0.24 113578. 0.2579
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33.59 0.5911 0.7723 0.0517 0.0396 0.275 5.784 2.374 205.308 0.654 10.561 5.245 0.24 113925. 0.2371
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35.35 0.6222 0.7802 0.0467 0.0373 0.259 5.443 2.144 193.200 0.615 9.537 5.034 0.24 114287. 0.2163
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37.12 0.6534 0.7837 0.0416 0.0347 0.241 5.065 1.908 179.761 0.572 8.489 4.815 0.24 114664. 0.1952
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38.89 0.6845 0.7816 0.0364 0.0318 0.221 4.651 1.668 165.072 0.525 7.421 4.584 0.24 115056. 0.1737
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40.66 0.7156 0.7724 0.0311 0.0288 0.200 4.204 1.426 149.218 0.475 6.341 4.333 0.24 115462. 0.1518
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42.43 0.7467 0.7533 0.0257 0.0255 0.177 3.727 1.181 132.298 0.421 5.255 4.050 0.24 115884. 0.1292
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44.19 0.7778 0.7198 0.0204 0.0221 0.153 3.224 0.937 114.428 0.364 4.169 3.715 0.25 116320. 0.1055
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45.96 0.8089 0.6634 0.0151 0.0185 0.128 2.698 0.695 95.746 0.305 3.091 3.292 0.25 116770. 0.0805
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47.73 0.8400 0.5668 0.0099 0.0147 0.102 2.153 0.456 76.414 0.243 2.030 2.709 0.25 117235. 0.0537
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49.50 0.8711 0.3885 0.0049 0.0109 0.076 1.595 0.224 56.623 0.180 0.994 1.790 0.25 117714. 0.0248
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51.26 0.9023 -0.0060 0.0000 0.0070 0.049 1.029 -0.002 36.537 0.116 -0.010 -0.027 0.25 118201. 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 0.1018 0.0387 0.638 10.051 8.307 475.659 1.136 36.951 7.922 0.32 146523. 0.6698
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2.36 0.0311 0.0793 0.1010 0.0397 0.654 10.300 8.243 487.458 1.164 36.663 7.670 0.32 146643. 0.6460
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4.72 0.0623 0.1533 0.1001 0.0406 0.670 10.556 8.169 499.564 1.193 36.336 7.417 0.32 146777. 0.6219
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7.07 0.0934 0.2222 0.0991 0.0416 0.686 10.815 8.085 511.795 1.222 35.963 7.165 0.32 146926. 0.5978
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9.43 0.1245 0.2860 0.0979 0.0426 0.703 11.071 7.990 523.948 1.251 35.539 6.917 0.32 147092. 0.5736
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11.79 0.1556 0.3449 0.0966 0.0436 0.718 11.321 7.881 535.779 1.279 35.056 6.672 0.32 147275. 0.5495
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14.15 0.1868 0.3990 0.0951 0.0445 0.734 11.559 7.758 547.012 1.306 34.508 6.433 0.32 147475. 0.5257
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16.51 0.2179 0.4486 0.0934 0.0454 0.747 11.777 7.619 557.339 1.331 33.887 6.200 0.32 147694. 0.5021
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18.86 0.2490 0.4941 0.0915 0.0461 0.760 11.969 7.461 566.423 1.352 33.188 5.975 0.32 147933. 0.4788
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21.22 0.2801 0.5357 0.0893 0.0467 0.770 12.127 7.285 573.906 1.370 32.403 5.757 0.32 148191. 0.4559
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23.58 0.3113 0.5736 0.0869 0.0471 0.777 12.243 7.088 579.408 1.383 31.526 5.548 0.32 148469. 0.4334
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25.94 0.3424 0.6081 0.0842 0.0474 0.781 12.309 6.869 582.535 1.391 30.551 5.348 0.32 148768. 0.4112
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28.30 0.3735 0.6396 0.0812 0.0474 0.782 12.317 6.626 582.887 1.392 29.472 5.156 0.32 149087. 0.3894
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30.65 0.4046 0.6682 0.0779 0.0472 0.778 12.257 6.359 580.068 1.385 28.283 4.972 0.32 149427. 0.3678
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33.01 0.4358 0.6940 0.0744 0.0467 0.769 12.123 6.066 573.698 1.370 26.980 4.796 0.32 149788. 0.3465
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35.37 0.4669 0.7173 0.0704 0.0458 0.756 11.906 5.747 563.436 1.345 25.562 4.626 0.32 150170. 0.3254
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37.73 0.4980 0.7381 0.0662 0.0447 0.736 11.604 5.403 549.147 1.311 24.033 4.463 0.32 150573. 0.3043
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40.09 0.5291 0.7564 0.0618 0.0432 0.712 11.218 5.038 530.911 1.267 22.408 4.304 0.32 150995. 0.2834
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42.44 0.5603 0.7719 0.0570 0.0414 0.682 10.753 4.654 508.891 1.215 20.701 4.148 0.32 151439. 0.2625
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44.80 0.5914 0.7843 0.0522 0.0393 0.648 10.212 4.255 483.266 1.154 18.926 3.993 0.32 151902. 0.2417
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47.16 0.6225 0.7934 0.0471 0.0370 0.609 9.598 3.843 454.215 1.084 17.093 3.837 0.32 152386. 0.2207
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49.52 0.6536 0.7983 0.0419 0.0343 0.566 8.915 3.421 421.922 1.007 15.216 3.677 0.32 152889. 0.1995
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51.88 0.6848 0.7981 0.0367 0.0315 0.518 8.169 2.991 386.577 0.923 13.304 3.509 0.32 153412. 0.1781
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54.23 0.7159 0.7912 0.0313 0.0283 0.467 7.362 2.556 348.388 0.832 11.370 3.328 0.33 153955. 0.1561
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56.59 0.7470 0.7751 0.0260 0.0250 0.412 6.500 2.119 307.596 0.734 9.424 3.124 0.33 154517. 0.1334
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58.95 0.7781 0.7453 0.0206 0.0215 0.355 5.589 1.682 264.481 0.631 7.480 2.884 0.33 155099. 0.1097
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61.31 0.8093 0.6934 0.0153 0.0179 0.294 4.636 1.248 219.379 0.524 5.550 2.580 0.33 155700. 0.0846
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63.67 0.8404 0.6017 0.0101 0.0141 0.232 3.649 0.821 172.690 0.412 3.651 2.156 0.33 156320. 0.0573
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66.02 0.8715 0.4247 0.0050 0.0102 0.167 2.639 0.404 124.879 0.298 1.797 1.467 0.33 156959. 0.0274
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68.38 0.9026 0.0003 0.0000 0.0062 0.102 1.613 0.000 76.339 0.182 0.001 0.001 0.33 157609. 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 0.1023 0.0385 1.239 15.621 13.041 924.073 1.765 58.007 6.401 0.40 183147. 0.6782
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2.95 0.0311 0.0801 0.1015 0.0395 1.271 16.017 12.943 947.511 1.810 57.572 6.196 0.40 183297. 0.6540
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5.90 0.0623 0.1549 0.1007 0.0405 1.303 16.424 12.832 971.595 1.856 57.075 5.990 0.40 183464. 0.6295
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8.85 0.0934 0.2244 0.0997 0.0415 1.336 16.836 12.704 995.972 1.902 56.508 5.785 0.40 183651. 0.6050
|
|
11.80 0.1246 0.2888 0.0985 0.0425 1.368 17.247 12.558 1020.236 1.949 55.859 5.583 0.40 183858. 0.5805
|
|
14.75 0.1557 0.3481 0.0972 0.0435 1.400 17.647 12.392 1043.904 1.994 55.118 5.384 0.40 184087. 0.5561
|
|
17.70 0.1869 0.4026 0.0957 0.0444 1.430 18.027 12.202 1066.426 2.037 54.275 5.190 0.40 184338. 0.5319
|
|
20.65 0.2180 0.4526 0.0940 0.0453 1.458 18.378 11.987 1087.183 2.076 53.317 5.001 0.40 184612. 0.5080
|
|
23.60 0.2492 0.4984 0.0921 0.0461 1.483 18.688 11.743 1105.503 2.111 52.235 4.818 0.40 184911. 0.4844
|
|
26.54 0.2803 0.5402 0.0900 0.0467 1.503 18.944 11.469 1120.669 2.140 51.016 4.642 0.40 185234. 0.4612
|
|
29.49 0.3115 0.5783 0.0876 0.0472 1.518 19.134 11.162 1131.918 2.162 49.651 4.473 0.40 185583. 0.4384
|
|
32.44 0.3426 0.6131 0.0849 0.0474 1.527 19.245 10.820 1138.466 2.174 48.128 4.311 0.40 185957. 0.4160
|
|
35.39 0.3737 0.6448 0.0819 0.0475 1.528 19.263 10.441 1139.509 2.176 46.440 4.156 0.40 186357. 0.3940
|
|
38.34 0.4049 0.6736 0.0786 0.0473 1.521 19.174 10.022 1134.258 2.166 44.578 4.008 0.40 186783. 0.3722
|
|
41.29 0.4360 0.6998 0.0750 0.0467 1.505 18.966 9.563 1121.951 2.143 42.535 3.866 0.40 187235. 0.3507
|
|
44.24 0.4672 0.7234 0.0711 0.0459 1.478 18.627 9.062 1101.899 2.104 40.306 3.730 0.40 187714. 0.3294
|
|
47.19 0.4983 0.7446 0.0668 0.0447 1.440 18.152 8.521 1073.814 2.051 37.902 3.599 0.40 188218. 0.3082
|
|
50.14 0.5295 0.7633 0.0623 0.0432 1.392 17.544 7.946 1037.841 1.982 35.343 3.473 0.40 188747. 0.2872
|
|
53.09 0.5606 0.7794 0.0576 0.0414 1.333 16.808 7.341 994.295 1.899 32.653 3.349 0.40 189302. 0.2662
|
|
56.04 0.5918 0.7926 0.0527 0.0393 1.265 15.950 6.711 943.524 1.802 29.853 3.226 0.40 189883. 0.2452
|
|
58.99 0.6229 0.8025 0.0476 0.0369 1.188 14.975 6.061 885.887 1.692 26.961 3.103 0.40 190488. 0.2242
|
|
61.94 0.6541 0.8086 0.0423 0.0342 1.102 13.891 5.395 821.744 1.569 23.998 2.978 0.41 191118. 0.2029
|
|
64.89 0.6852 0.8098 0.0370 0.0313 1.008 12.703 4.717 751.474 1.435 20.980 2.847 0.41 191773. 0.1814
|
|
67.84 0.7163 0.8047 0.0316 0.0281 0.906 11.419 4.030 675.496 1.290 17.925 2.706 0.41 192453. 0.1594
|
|
70.79 0.7475 0.7908 0.0262 0.0248 0.797 10.046 3.339 594.288 1.135 14.852 2.548 0.41 193157. 0.1366
|
|
73.73 0.7786 0.7638 0.0208 0.0212 0.682 8.595 2.649 508.417 0.971 11.781 2.363 0.41 193885. 0.1128
|
|
76.68 0.8098 0.7153 0.0154 0.0174 0.561 7.075 1.963 418.557 0.799 8.733 2.128 0.41 194637. 0.0875
|
|
79.63 0.8409 0.6270 0.0101 0.0136 0.437 5.503 1.289 325.519 0.622 5.733 1.796 0.41 195414. 0.0598
|
|
82.58 0.8721 0.4499 0.0049 0.0096 0.309 3.892 0.631 230.247 0.440 2.806 1.243 0.41 196214. 0.0290
|
|
85.53 0.9032 -0.0087 -0.0001 0.0056 0.179 2.256 -0.007 133.474 0.255 -0.030 -0.023 0.41 197024. 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 0.1029 0.0385 2.142 22.500 18.885 1597.243 2.542 83.998 5.363 0.48 219766. 0.6837
|
|
3.54 0.0311 0.0805 0.1021 0.0395 2.197 23.081 18.750 1638.453 2.608 83.399 5.190 0.48 219945. 0.6594
|
|
7.08 0.0623 0.1557 0.1013 0.0405 2.254 23.679 18.595 1680.880 2.675 82.712 5.018 0.48 220146. 0.6348
|
|
10.62 0.0934 0.2256 0.1003 0.0416 2.312 24.285 18.418 1723.912 2.744 81.923 4.846 0.48 220371. 0.6101
|
|
14.16 0.1246 0.2902 0.0992 0.0426 2.369 24.889 18.214 1766.832 2.812 81.017 4.676 0.48 220619. 0.5855
|
|
17.70 0.1557 0.3498 0.0980 0.0436 2.426 25.481 17.981 1808.797 2.879 79.979 4.509 0.48 220894. 0.5609
|
|
21.24 0.1869 0.4046 0.0965 0.0446 2.479 26.044 17.714 1848.820 2.942 78.791 4.346 0.48 221195. 0.5366
|
|
24.78 0.2180 0.4548 0.0948 0.0455 2.529 26.566 17.409 1885.816 3.001 77.436 4.187 0.48 221525. 0.5126
|
|
28.31 0.2492 0.5007 0.0930 0.0463 2.573 27.027 17.063 1918.584 3.054 75.898 4.034 0.48 221883. 0.4889
|
|
31.85 0.2803 0.5427 0.0908 0.0469 2.609 27.411 16.673 1945.848 3.097 74.161 3.886 0.48 222272. 0.4656
|
|
35.39 0.3115 0.5810 0.0884 0.0474 2.637 27.699 16.234 1966.261 3.129 72.208 3.745 0.48 222690. 0.4427
|
|
38.93 0.3426 0.6160 0.0858 0.0477 2.653 27.870 15.743 1978.423 3.149 70.024 3.609 0.48 223140. 0.4201
|
|
42.47 0.3738 0.6479 0.0828 0.0478 2.656 27.905 15.197 1980.914 3.153 67.595 3.480 0.48 223621. 0.3980
|
|
46.01 0.4049 0.6769 0.0795 0.0476 2.645 27.784 14.593 1972.334 3.139 64.911 3.356 0.48 224133. 0.3761
|
|
49.55 0.4360 0.7033 0.0759 0.0470 2.617 27.489 13.930 1951.331 3.106 61.959 3.238 0.48 224676. 0.3545
|
|
53.09 0.4672 0.7273 0.0719 0.0462 2.570 27.000 13.204 1916.677 3.050 58.733 3.125 0.48 225250. 0.3331
|
|
56.63 0.4983 0.7488 0.0677 0.0450 2.505 26.312 12.421 1867.815 2.973 55.247 3.016 0.48 225856. 0.3119
|
|
60.17 0.5295 0.7679 0.0631 0.0435 2.421 25.427 11.585 1804.973 2.873 51.532 2.911 0.48 226492. 0.2907
|
|
63.71 0.5606 0.7846 0.0583 0.0417 2.318 24.352 10.706 1728.692 2.751 47.622 2.809 0.48 227159. 0.2697
|
|
67.25 0.5918 0.7984 0.0533 0.0395 2.199 23.097 9.790 1639.584 2.609 43.546 2.708 0.48 227857. 0.2486
|
|
70.79 0.6229 0.8092 0.0482 0.0371 2.063 21.670 8.843 1538.277 2.448 39.335 2.608 0.49 228584. 0.2275
|
|
74.33 0.6541 0.8162 0.0429 0.0344 1.912 20.080 7.872 1425.410 2.269 35.016 2.505 0.49 229341. 0.2062
|
|
77.87 0.6852 0.8187 0.0375 0.0314 1.746 18.336 6.883 1301.652 2.072 30.616 2.398 0.49 230127. 0.1846
|
|
81.40 0.7164 0.8152 0.0320 0.0282 1.566 16.450 5.881 1167.744 1.859 26.159 2.284 0.49 230943. 0.1625
|
|
84.94 0.7475 0.8033 0.0265 0.0247 1.374 14.433 4.873 1024.536 1.631 21.674 2.157 0.49 231788. 0.1397
|
|
88.48 0.7787 0.7788 0.0211 0.0210 1.171 12.298 3.865 873.032 1.389 17.190 2.008 0.49 232662. 0.1158
|
|
92.02 0.8098 0.7335 0.0156 0.0172 0.958 10.064 2.864 714.436 1.137 12.739 1.818 0.49 233565. 0.0903
|
|
95.56 0.8409 0.6489 0.0102 0.0133 0.738 7.751 1.879 550.193 0.876 8.357 1.549 0.49 234497. 0.0623
|
|
99.10 0.8721 0.4734 0.0050 0.0092 0.512 5.381 0.918 381.994 0.608 4.081 1.090 0.49 235457. 0.0306
|
|
102.64 0.9032 -0.0136 -0.0001 0.0051 0.283 2.973 -0.014 211.077 0.336 -0.062 -0.030 0.50 236428. 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 0.1036 0.0387 3.418 30.773 25.872 2548.593 3.477 115.080 4.604 0.56 256379. 0.6871
|
|
4.16 0.0314 0.0813 0.1029 0.0397 3.508 31.585 25.698 2615.855 3.569 114.304 4.456 0.56 256589. 0.6627
|
|
8.32 0.0628 0.1572 0.1020 0.0408 3.601 32.424 25.497 2685.278 3.663 113.409 4.307 0.56 256826. 0.6380
|
|
12.49 0.0942 0.2276 0.1011 0.0418 3.696 33.276 25.264 2755.853 3.759 112.374 4.158 0.56 257090. 0.6132
|
|
16.65 0.1256 0.2928 0.1000 0.0429 3.790 34.128 24.995 2826.398 3.856 111.178 4.011 0.56 257383. 0.5883
|
|
20.81 0.1570 0.3528 0.0988 0.0440 3.883 34.962 24.685 2895.494 3.950 109.797 3.867 0.56 257707. 0.5636
|
|
24.97 0.1884 0.4079 0.0974 0.0450 3.971 35.759 24.327 2961.496 4.040 108.206 3.726 0.56 258063. 0.5391
|
|
29.13 0.2198 0.4584 0.0957 0.0459 4.053 36.496 23.916 3022.557 4.123 106.380 3.589 0.56 258453. 0.5149
|
|
33.30 0.2512 0.5046 0.0938 0.0467 4.126 37.149 23.447 3076.654 4.197 104.294 3.457 0.56 258877. 0.4911
|
|
37.46 0.2825 0.5468 0.0917 0.0474 4.186 37.692 22.914 3121.625 4.258 101.923 3.329 0.56 259337. 0.4676
|
|
41.62 0.3139 0.5852 0.0893 0.0479 4.231 38.098 22.312 3155.193 4.304 99.245 3.207 0.56 259832. 0.4445
|
|
45.78 0.3453 0.6204 0.0866 0.0482 4.258 38.337 21.636 3175.006 4.331 96.238 3.091 0.56 260365. 0.4218
|
|
49.94 0.3767 0.6524 0.0836 0.0483 4.263 38.381 20.882 3178.686 4.336 92.881 2.980 0.56 260934. 0.3995
|
|
54.11 0.4081 0.6816 0.0802 0.0480 4.243 38.203 20.044 3163.885 4.316 89.158 2.874 0.56 261541. 0.3774
|
|
58.27 0.4395 0.7082 0.0765 0.0475 4.195 37.774 19.122 3128.354 4.268 85.053 2.772 0.56 262185. 0.3557
|
|
62.43 0.4709 0.7323 0.0725 0.0466 4.117 37.070 18.111 3070.080 4.188 80.557 2.676 0.56 262866. 0.3341
|
|
66.59 0.5023 0.7541 0.0681 0.0454 4.007 36.082 17.017 2988.235 4.077 75.694 2.583 0.56 263583. 0.3126
|
|
70.76 0.5337 0.7735 0.0634 0.0438 3.866 34.814 15.851 2883.243 3.933 70.506 2.494 0.56 264338. 0.2913
|
|
74.92 0.5651 0.7904 0.0585 0.0418 3.696 33.278 14.623 2756.020 3.760 65.043 2.407 0.56 265128. 0.2700
|
|
79.08 0.5965 0.8046 0.0534 0.0396 3.497 31.486 13.343 2607.597 3.557 59.347 2.321 0.57 265954. 0.2487
|
|
83.24 0.6279 0.8157 0.0481 0.0370 3.271 29.450 12.019 2439.027 3.327 53.462 2.235 0.57 266815. 0.2273
|
|
87.40 0.6593 0.8231 0.0427 0.0342 3.019 27.185 10.662 2251.384 3.071 47.425 2.148 0.57 267712. 0.2058
|
|
91.57 0.6907 0.8258 0.0371 0.0311 2.743 24.702 9.279 2045.806 2.791 41.275 2.057 0.57 268643. 0.1839
|
|
95.73 0.7221 0.8225 0.0315 0.0277 2.445 22.019 7.880 1823.558 2.488 35.048 1.960 0.57 269610. 0.1614
|
|
99.89 0.7535 0.8104 0.0259 0.0241 2.127 19.152 6.472 1586.111 2.164 28.785 1.851 0.57 270610. 0.1381
|
|
104.05 0.7848 0.7849 0.0203 0.0203 1.791 16.122 5.065 1335.205 1.821 22.529 1.721 0.57 271645. 0.1136
|
|
108.21 0.8162 0.7361 0.0147 0.0163 1.439 12.955 3.671 1072.940 1.464 16.326 1.552 0.57 272715. 0.0872
|
|
112.38 0.8476 0.6409 0.0092 0.0122 1.075 9.682 2.300 801.843 1.094 10.230 1.301 0.58 273818. 0.0579
|
|
116.54 0.8790 0.4264 0.0039 0.0080 0.704 6.337 0.966 524.855 0.716 4.296 0.835 0.58 274953. 0.0241
|
|
120.70 0.9104
|
|
|
|
|
|
|
|
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 0.1043 0.0390 5.148 40.559 34.045 3838.856 4.582 151.434 4.023 0.63 292984. 0.6886
|
|
4.71 0.0311 0.0805 0.1037 0.0401 5.284 41.632 33.837 3940.412 4.704 150.508 3.895 0.63 293222. 0.6647
|
|
9.43 0.0622 0.1557 0.1029 0.0411 5.425 42.743 33.596 4045.580 4.829 149.433 3.767 0.63 293489. 0.6405
|
|
14.14 0.0933 0.2256 0.1021 0.0422 5.569 43.877 33.315 4152.888 4.957 148.183 3.639 0.63 293787. 0.6161
|
|
18.86 0.1245 0.2903 0.1011 0.0433 5.714 45.014 32.988 4260.587 5.086 146.729 3.512 0.64 294118. 0.5917
|
|
23.57 0.1556 0.3500 0.0999 0.0444 5.856 46.134 32.607 4366.560 5.212 145.037 3.387 0.64 294483. 0.5674
|
|
28.29 0.1867 0.4049 0.0986 0.0454 5.992 47.209 32.166 4468.326 5.334 143.075 3.265 0.64 294885. 0.5433
|
|
33.00 0.2178 0.4552 0.0970 0.0464 6.119 48.211 31.657 4563.104 5.447 140.809 3.147 0.64 295324. 0.5194
|
|
37.71 0.2489 0.5013 0.0952 0.0473 6.233 49.106 31.071 4647.829 5.548 138.203 3.032 0.64 295802. 0.4959
|
|
42.43 0.2800 0.5435 0.0932 0.0480 6.329 49.860 30.401 4719.230 5.633 135.224 2.922 0.64 296321. 0.4727
|
|
47.14 0.3111 0.5820 0.0908 0.0486 6.402 50.437 29.640 4773.850 5.698 131.841 2.816 0.64 296880. 0.4498
|
|
51.86 0.3423 0.6173 0.0882 0.0489 6.448 50.799 28.782 4808.135 5.739 128.023 2.715 0.64 297480. 0.4274
|
|
56.57 0.3734 0.6495 0.0853 0.0490 6.462 50.909 27.820 4818.484 5.752 123.742 2.619 0.64 298122. 0.4052
|
|
61.29 0.4045 0.6789 0.0820 0.0488 6.439 50.728 26.748 4801.349 5.731 118.976 2.527 0.64 298806. 0.3834
|
|
66.00 0.4356 0.7058 0.0783 0.0483 6.374 50.220 25.563 4753.337 5.674 113.705 2.439 0.64 299531. 0.3618
|
|
70.72 0.4667 0.7303 0.0743 0.0475 6.264 49.354 24.261 4671.302 5.576 107.913 2.356 0.64 300299. 0.3404
|
|
75.43 0.4978 0.7525 0.0700 0.0463 6.106 48.110 22.847 4553.567 5.435 101.621 2.276 0.64 301107. 0.3191
|
|
80.14 0.5289 0.7725 0.0654 0.0448 5.901 46.493 21.332 4400.496 5.253 94.884 2.199 0.64 301957. 0.2979
|
|
84.86 0.5601 0.7902 0.0605 0.0429 5.650 44.516 19.731 4213.383 5.029 87.764 2.124 0.64 302847. 0.2768
|
|
89.57 0.5912 0.8053 0.0553 0.0406 5.356 42.195 18.058 3993.764 4.767 80.320 2.051 0.65 303778. 0.2557
|
|
94.29 0.6223 0.8176 0.0500 0.0381 5.020 39.548 16.324 3743.224 4.468 72.609 1.978 0.65 304748. 0.2345
|
|
99.00 0.6534 0.8265 0.0446 0.0352 4.644 36.592 14.542 3463.382 4.134 64.681 1.904 0.65 305757. 0.2131
|
|
103.72 0.6845 0.8313 0.0390 0.0321 4.232 33.343 12.722 3155.933 3.767 56.587 1.828 0.65 306806. 0.1913
|
|
108.43 0.7156 0.8307 0.0333 0.0287 3.785 29.823 10.876 2822.747 3.369 48.376 1.748 0.65 307894. 0.1691
|
|
113.14 0.7468 0.8225 0.0276 0.0251 3.307 26.054 9.015 2465.957 2.944 40.100 1.658 0.65 309020. 0.1461
|
|
117.86 0.7779 0.8027 0.0219 0.0212 2.800 22.061 7.152 2088.100 2.492 31.814 1.554 0.65 310184. 0.1219
|
|
122.57 0.8090 0.7635 0.0162 0.0172 2.269 17.879 5.301 1692.220 2.020 23.579 1.421 0.66 311387. 0.0960
|
|
127.29 0.8401 0.6863 0.0107 0.0130 1.719 13.545 3.476 1282.003 1.530 15.463 1.230 0.66 312628. 0.0673
|
|
132.00 0.8712 0.5164 0.0052 0.0088 1.156 9.105 1.695 861.801 1.029 7.541 0.892 0.66 313906. 0.0341
|
|
136.72 0.9023 -0.0204 -0.0001 0.0044 0.583 4.592 -0.033 434.589 0.519 -0.145 -0.034 0.66 315193. 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 0.1052 0.0400 7.505 52.556 43.443 5596.185 5.938 193.237 3.521 0.71 329580. 0.6809
|
|
5.29 0.0311 0.0793 0.1046 0.0410 7.695 53.891 43.209 5738.384 6.089 192.192 3.415 0.71 329847. 0.6586
|
|
10.59 0.0621 0.1536 0.1040 0.0420 7.893 55.279 42.934 5886.176 6.245 190.969 3.308 0.71 330146. 0.6360
|
|
15.88 0.0932 0.2229 0.1032 0.0431 8.097 56.701 42.611 6037.562 6.406 189.533 3.201 0.71 330479. 0.6130
|
|
21.18 0.1242 0.2873 0.1023 0.0442 8.301 58.134 42.231 6190.165 6.568 187.844 3.094 0.71 330850. 0.5900
|
|
26.47 0.1553 0.3469 0.1012 0.0453 8.504 59.551 41.785 6341.063 6.728 185.858 2.989 0.71 331260. 0.5668
|
|
31.77 0.1864 0.4018 0.0999 0.0463 8.699 60.920 41.261 6486.794 6.883 183.530 2.885 0.72 331710. 0.5437
|
|
37.06 0.2174 0.4523 0.0984 0.0473 8.882 62.203 40.650 6623.436 7.028 180.812 2.784 0.72 332204. 0.5207
|
|
42.35 0.2485 0.4986 0.0967 0.0482 9.047 63.359 39.940 6746.559 7.158 177.655 2.685 0.72 332741. 0.4979
|
|
47.65 0.2795 0.5410 0.0947 0.0489 9.188 64.344 39.122 6851.393 7.270 174.013 2.590 0.72 333323. 0.4753
|
|
52.94 0.3106 0.5798 0.0925 0.0495 9.297 65.109 38.184 6932.841 7.356 169.841 2.498 0.72 333951. 0.4529
|
|
58.24 0.3417 0.6153 0.0899 0.0499 9.368 65.604 37.117 6985.571 7.412 165.098 2.410 0.72 334625. 0.4308
|
|
63.53 0.3727 0.6478 0.0870 0.0500 9.393 65.778 35.914 7004.113 7.432 159.745 2.326 0.72 335347. 0.4089
|
|
68.83 0.4038 0.6774 0.0837 0.0499 9.364 65.580 34.566 6983.019 7.409 153.751 2.245 0.72 336115. 0.3873
|
|
74.12 0.4348 0.7046 0.0801 0.0494 9.276 64.960 33.069 6917.030 7.339 147.090 2.168 0.72 336931. 0.3658
|
|
79.41 0.4659 0.7294 0.0761 0.0486 9.121 63.873 31.417 6801.237 7.216 139.741 2.095 0.72 337794. 0.3445
|
|
84.71 0.4970 0.7521 0.0717 0.0474 8.895 62.291 29.614 6632.771 7.038 131.725 2.025 0.72 338703. 0.3233
|
|
90.00 0.5280 0.7725 0.0670 0.0458 8.599 60.217 27.678 6411.929 6.803 123.110 1.958 0.72 339658. 0.3022
|
|
95.30 0.5591 0.7908 0.0620 0.0439 8.235 57.668 25.624 6140.531 6.515 113.977 1.893 0.73 340658. 0.2811
|
|
100.59 0.5901 0.8066 0.0568 0.0416 7.806 54.666 23.473 5820.849 6.176 104.406 1.829 0.73 341704. 0.2600
|
|
105.89 0.6212 0.8197 0.0514 0.0390 7.316 51.232 21.238 5455.248 5.788 94.469 1.766 0.73 342794. 0.2388
|
|
111.18 0.6523 0.8297 0.0459 0.0360 6.767 47.390 18.937 5046.134 5.354 84.234 1.702 0.73 343927. 0.2173
|
|
116.47 0.6833 0.8357 0.0402 0.0328 6.163 43.163 16.584 4596.056 4.877 73.766 1.637 0.73 345105. 0.1955
|
|
121.77 0.7144 0.8366 0.0344 0.0293 5.509 38.579 14.193 4107.867 4.359 63.132 1.567 0.73 346326. 0.1732
|
|
127.06 0.7454 0.8302 0.0285 0.0256 4.807 33.667 11.780 3584.892 3.804 52.398 1.490 0.73 347590. 0.1501
|
|
132.36 0.7765 0.8128 0.0227 0.0217 4.065 28.467 9.361 3031.168 3.216 41.637 1.401 0.74 348897. 0.1257
|
|
137.65 0.8076 0.7763 0.0168 0.0175 3.288 23.025 6.953 2451.677 2.601 30.928 1.286 0.74 350247. 0.0995
|
|
142.95 0.8386 0.7023 0.0111 0.0132 2.484 17.399 4.577 1852.610 1.966 20.360 1.121 0.74 351639. 0.0703
|
|
148.24 0.8697 0.5355 0.0055 0.0089 1.665 11.659 2.255 1241.483 1.317 10.031 0.824 0.74 353072. 0.0363
|
|
153.53 0.9007 0.0003 0.0000 0.0045 0.837 5.863 0.001 624.279 0.662 0.003 0.000 0.74 354520. 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 0.1060 0.0432 11.112 70.039 54.072 8286.425 7.913 240.514 2.960 0.79 366165. 0.6385
|
|
5.87 0.0310 0.0742 0.1056 0.0441 11.357 71.583 53.825 8469.171 8.087 239.415 2.883 0.79 366460. 0.6205
|
|
11.74 0.0620 0.1444 0.1050 0.0451 11.611 73.184 53.533 8658.498 8.268 238.116 2.804 0.79 366790. 0.6020
|
|
17.62 0.0930 0.2105 0.1043 0.0461 11.870 74.815 53.186 8851.493 8.453 236.573 2.725 0.79 367159. 0.5831
|
|
23.49 0.1240 0.2725 0.1035 0.0471 12.129 76.448 52.773 9044.751 8.637 234.734 2.646 0.79 367569. 0.5640
|
|
29.36 0.1550 0.3306 0.1025 0.0481 12.383 78.049 52.280 9234.104 8.818 232.542 2.568 0.79 368022. 0.5447
|
|
35.23 0.1860 0.3847 0.1014 0.0490 12.625 79.576 51.694 9414.767 8.990 229.933 2.490 0.79 368521. 0.5253
|
|
41.11 0.2170 0.4351 0.1000 0.0499 12.849 80.984 50.999 9581.343 9.150 226.843 2.414 0.80 369067. 0.5058
|
|
46.98 0.2481 0.4819 0.0984 0.0507 13.045 82.223 50.181 9727.972 9.290 223.203 2.340 0.80 369662. 0.4862
|
|
52.85 0.2791 0.5253 0.0965 0.0513 13.207 83.241 49.224 9848.428 9.405 218.948 2.267 0.80 370308. 0.4666
|
|
58.72 0.3101 0.5654 0.0944 0.0517 13.325 83.983 48.115 9936.223 9.488 214.015 2.196 0.80 371005. 0.4470
|
|
64.60 0.3411 0.6026 0.0919 0.0520 13.390 84.392 46.840 9984.619 9.535 208.344 2.128 0.80 371753. 0.4272
|
|
70.47 0.3721 0.6368 0.0890 0.0520 13.392 84.410 45.387 9986.757 9.537 201.882 2.061 0.80 372555. 0.4074
|
|
76.34 0.4031 0.6684 0.0858 0.0517 13.324 83.980 43.746 9935.778 9.488 194.583 1.997 0.80 373408. 0.3875
|
|
82.21 0.4341 0.6973 0.0822 0.0512 13.175 83.043 41.909 9824.938 9.382 186.411 1.935 0.80 374315. 0.3675
|
|
88.09 0.4651 0.7238 0.0782 0.0502 12.938 81.545 39.869 9647.792 9.213 177.338 1.874 0.80 375273. 0.3472
|
|
93.96 0.4961 0.7479 0.0738 0.0490 12.605 79.450 37.631 9399.879 8.976 167.381 1.816 0.80 376283. 0.3268
|
|
99.83 0.5271 0.7697 0.0691 0.0473 12.178 76.753 35.212 9080.838 8.672 156.623 1.759 0.80 377344. 0.3062
|
|
105.70 0.5581 0.7892 0.0640 0.0453 11.657 73.471 32.637 8692.498 8.301 145.171 1.703 0.81 378455. 0.2854
|
|
111.58 0.5891 0.8060 0.0587 0.0429 11.048 69.631 29.929 8238.156 7.867 133.125 1.648 0.81 379616. 0.2645
|
|
117.45 0.6201 0.8200 0.0532 0.0402 10.354 65.257 27.109 7720.716 7.373 120.580 1.593 0.81 380826. 0.2433
|
|
123.32 0.6511 0.8306 0.0475 0.0372 9.579 60.376 24.196 7143.249 6.821 107.625 1.536 0.81 382085. 0.2217
|
|
129.19 0.6821 0.8371 0.0416 0.0339 8.729 55.020 21.211 6509.562 6.216 94.346 1.478 0.81 383392. 0.1997
|
|
135.07 0.7132 0.8378 0.0356 0.0303 7.811 49.233 18.171 5824.854 5.562 80.826 1.415 0.81 384746. 0.1770
|
|
140.94 0.7442 0.8303 0.0296 0.0265 6.833 43.068 15.097 5095.442 4.866 67.150 1.344 0.82 386148. 0.1532
|
|
146.81 0.7752 0.8097 0.0235 0.0225 5.806 36.593 12.008 4329.363 4.134 53.411 1.258 0.82 387597. 0.1279
|
|
152.68 0.8062 0.7664 0.0175 0.0184 4.742 29.889 8.927 3536.201 3.377 39.706 1.145 0.82 389094. 0.1004
|
|
158.56 0.8372 0.6796 0.0115 0.0142 3.658 23.055 5.879 2727.675 2.605 26.151 0.978 0.82 390636. 0.0695
|
|
164.43 0.8682 0.4935 0.0057 0.0100 2.571 16.204 2.894 1917.092 1.831 12.871 0.685 0.82 392224. 0.0342
|
|
170.30 0.8992 -0.0033 0.0000 0.0058 1.495 9.423 -0.011 1114.844 1.065 -0.048 -0.004 0.83 393832. 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 0.1065 0.0503 17.251 98.845 65.707 12863.973 11.167 292.265 2.317 0.87 402754. 0.5510
|
|
6.47 0.0311 0.0643 0.1061 0.0512 17.565 100.643 65.468 13097.975 11.371 291.202 2.267 0.87 403075. 0.5382
|
|
12.95 0.0621 0.1258 0.1057 0.0522 17.888 102.493 65.183 13338.723 11.580 289.935 2.216 0.87 403436. 0.5250
|
|
19.42 0.0932 0.1843 0.1051 0.0531 18.213 104.357 64.840 13581.396 11.790 288.410 2.165 0.87 403840. 0.5116
|
|
25.89 0.1243 0.2400 0.1044 0.0541 18.533 106.193 64.426 13820.216 11.998 286.565 2.114 0.87 404288. 0.4979
|
|
32.36 0.1553 0.2928 0.1036 0.0550 18.839 107.944 63.922 14048.126 12.195 284.323 2.064 0.87 404786. 0.4841
|
|
38.84 0.1864 0.3429 0.1026 0.0558 19.119 109.549 63.310 14256.976 12.377 281.601 2.014 0.87 405333. 0.4702
|
|
45.31 0.2175 0.3904 0.1014 0.0565 19.361 110.938 62.569 14437.823 12.534 278.308 1.966 0.87 405934. 0.4562
|
|
51.78 0.2485 0.4355 0.1000 0.0571 19.554 112.041 61.679 14581.376 12.658 274.347 1.919 0.88 406589. 0.4421
|
|
58.25 0.2796 0.4784 0.0982 0.0574 19.684 112.787 60.617 14678.435 12.743 269.624 1.873 0.88 407301. 0.4278
|
|
64.73 0.3107 0.5190 0.0962 0.0576 19.740 113.105 59.363 14719.870 12.779 264.044 1.829 0.88 408070. 0.4135
|
|
71.20 0.3418 0.5577 0.0938 0.0575 19.710 112.933 57.896 14697.487 12.759 257.521 1.787 0.88 408897. 0.3988
|
|
77.67 0.3728 0.5943 0.0911 0.0571 19.585 112.221 56.201 14604.828 12.679 249.982 1.745 0.88 409783. 0.3839
|
|
84.14 0.4039 0.6290 0.0880 0.0565 19.358 110.917 54.263 14435.108 12.531 241.362 1.705 0.88 410728. 0.3685
|
|
90.62 0.4350 0.6616 0.0844 0.0555 19.018 108.973 52.070 14182.028 12.312 231.609 1.665 0.88 411731. 0.3526
|
|
97.09 0.4660 0.6921 0.0804 0.0541 18.559 106.341 49.613 13839.485 12.014 220.680 1.626 0.88 412792. 0.3360
|
|
103.56 0.4971 0.7205 0.0760 0.0524 17.974 102.991 46.894 13403.559 11.636 208.587 1.587 0.88 413911. 0.3188
|
|
110.03 0.5282 0.7466 0.0712 0.0504 17.267 98.936 43.936 12875.782 11.178 195.429 1.548 0.88 415086. 0.3010
|
|
116.51 0.5592 0.7703 0.0661 0.0480 16.442 94.209 40.769 12260.611 10.644 181.341 1.508 0.89 416316. 0.2825
|
|
122.98 0.5903 0.7914 0.0607 0.0452 15.506 88.845 37.422 11562.607 10.038 166.452 1.468 0.89 417602. 0.2635
|
|
129.45 0.6214 0.8085 0.0550 0.0423 14.483 82.988 33.921 10800.300 9.376 150.882 1.425 0.89 418942. 0.2434
|
|
135.93 0.6524 0.8206 0.0491 0.0390 13.380 76.666 30.294 9977.591 8.662 134.749 1.377 0.89 420335. 0.2224
|
|
142.40 0.6835 0.8258 0.0431 0.0356 12.215 69.988 26.565 9108.470 7.907 118.159 1.323 0.89 421781. 0.2000
|
|
148.87 0.7146 0.8202 0.0369 0.0321 11.013 63.104 22.754 8212.592 7.129 101.209 1.257 0.89 423279. 0.1759
|
|
155.34 0.7456 0.8021 0.0306 0.0285 9.757 55.907 18.894 7275.876 6.316 84.040 1.178 0.90 424829. 0.1502
|
|
161.82 0.7767 0.7651 0.0243 0.0247 8.467 48.513 15.014 6313.656 5.481 66.780 1.079 0.90 426431. 0.1226
|
|
168.29 0.8078 0.6977 0.0181 0.0209 7.167 41.065 11.143 5344.283 4.639 49.563 0.946 0.90 428084. 0.0926
|
|
174.76 0.8389 0.5798 0.0119 0.0172 5.882 33.702 7.318 4386.119 3.808 32.552 0.757 0.90 429788. 0.0601
|
|
181.23 0.8699 0.3731 0.0058 0.0135 4.638 26.577 3.581 3458.815 3.003 15.927 0.470 0.91 431542. 0.0261
|
|
187.71 0.9010 -0.0059 -0.0001 0.0101 3.449 19.761 -0.041 2571.742 2.233 -0.181 -0.007 0.91 433332. 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 0.1041 0.0570 25.376 133.282 76.400 18922.645 15.058 339.828 1.831 0.95 439463. 0.4696
|
|
7.37 0.0324 0.0580 0.1038 0.0580 25.811 135.571 76.178 19247.557 15.317 338.841 1.795 0.95 439822. 0.4597
|
|
14.73 0.0648 0.1135 0.1034 0.0590 26.272 137.988 75.914 19590.732 15.590 337.665 1.758 0.95 440227. 0.4493
|
|
22.10 0.0972 0.1665 0.1030 0.0601 26.748 140.491 75.594 19946.078 15.873 336.242 1.719 0.95 440683. 0.4385
|
|
29.47 0.1297 0.2170 0.1024 0.0612 27.230 143.022 75.201 20305.477 16.159 334.496 1.680 0.95 441192. 0.4274
|
|
36.83 0.1621 0.2649 0.1018 0.0623 27.703 145.507 74.716 20658.256 16.439 332.335 1.640 0.95 441758. 0.4160
|
|
44.20 0.1945 0.3103 0.1009 0.0633 28.149 147.851 74.112 20991.082 16.704 329.651 1.601 0.95 442384. 0.4045
|
|
51.57 0.2269 0.3534 0.0999 0.0642 28.548 149.943 73.363 21287.980 16.940 326.321 1.563 0.95 443073. 0.3928
|
|
58.93 0.2593 0.3943 0.0987 0.0649 28.873 151.651 72.438 21530.555 17.133 322.205 1.526 0.96 443828. 0.3810
|
|
66.30 0.2917 0.4332 0.0971 0.0654 29.098 152.834 71.303 21698.482 17.267 317.156 1.490 0.96 444651. 0.3692
|
|
73.67 0.3241 0.4705 0.0952 0.0656 29.195 153.340 69.923 21770.344 17.324 311.019 1.457 0.96 445543. 0.3574
|
|
81.03 0.3565 0.5063 0.0930 0.0655 29.134 153.020 68.264 21724.869 17.288 303.637 1.425 0.96 446505. 0.3455
|
|
88.40 0.3890 0.5409 0.0903 0.0649 28.888 151.731 66.290 21541.836 17.142 294.859 1.396 0.96 447539. 0.3334
|
|
95.77 0.4214 0.5745 0.0871 0.0639 28.435 149.352 63.971 21204.078 16.874 284.543 1.368 0.96 448644. 0.3211
|
|
103.13 0.4538 0.6070 0.0835 0.0624 27.764 145.828 61.286 20703.863 16.476 272.602 1.343 0.96 449821. 0.3084
|
|
110.50 0.4862 0.6385 0.0793 0.0604 26.869 141.124 58.222 20035.984 15.944 258.973 1.318 0.96 451068. 0.2951
|
|
117.87 0.5186 0.6687 0.0746 0.0579 25.755 135.272 54.794 19205.143 15.283 243.724 1.294 0.96 452384. 0.2810
|
|
125.23 0.5510 0.6974 0.0695 0.0549 24.440 128.370 51.039 18225.240 14.503 227.020 1.270 0.97 453768. 0.2662
|
|
132.60 0.5834 0.7241 0.0640 0.0516 22.950 120.540 47.000 17113.518 13.619 209.054 1.246 0.97 455218. 0.2505
|
|
139.97 0.6158 0.7484 0.0582 0.0479 21.305 111.902 42.721 15887.138 12.643 190.022 1.220 0.97 456733. 0.2339
|
|
147.33 0.6483 0.7672 0.0521 0.0440 19.581 102.848 38.238 14601.798 11.620 170.082 1.188 0.97 458312. 0.2155
|
|
154.70 0.6807 0.7780 0.0457 0.0400 17.810 93.544 33.591 13280.813 10.569 149.415 1.147 0.97 459954. 0.1951
|
|
162.07 0.7131 0.7712 0.0392 0.0363 16.141 84.778 28.803 12036.316 9.578 128.114 1.085 0.98 461658. 0.1709
|
|
169.43 0.7455 0.7358 0.0326 0.0330 14.679 77.098 23.906 10945.899 8.710 106.333 0.991 0.98 463423. 0.1421
|
|
176.80 0.7779 0.6768 0.0259 0.0297 13.230 69.491 18.993 9865.957 7.851 84.483 0.873 0.98 465249. 0.1116
|
|
184.17 0.8103 0.5870 0.0193 0.0266 11.827 62.121 14.137 8819.580 7.018 62.881 0.727 0.98 467136. 0.0802
|
|
191.53 0.8427 0.4579 0.0128 0.0236 10.499 55.142 9.412 7828.795 6.230 41.864 0.545 0.99 469084. 0.0491
|
|
198.90 0.8752 0.2795 0.0067 0.0208 9.269 48.686 4.885 6912.189 5.501 21.730 0.321 0.99 471099. 0.0208
|
|
206.27 0.9076 0.0389 0.0008 0.0183 8.131 42.709 0.575 6063.629 4.825 2.558 0.043 0.99 473220. 0.0010
|
|
213.63 0.9400
|
|
|
|
|
|
|