427 lines
76 KiB
Plaintext
427 lines
76 KiB
Plaintext
22x12WE (22x12WE.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 0.1004 0.0386 0.016 1.009 0.749 11.938 0.114 3.333 28.471 0.09 55834. 0.6573
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0.50 0.0240 0.0607 0.0987 0.0390 0.016 1.019 0.737 12.053 0.115 3.277 27.726 0.09 55873. 0.6348
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1.00 0.0480 0.1182 0.0969 0.0393 0.016 1.028 0.723 12.157 0.116 3.217 26.986 0.09 55915. 0.6121
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1.50 0.0719 0.1725 0.0950 0.0396 0.016 1.035 0.709 12.248 0.117 3.153 26.254 0.09 55960. 0.5896
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2.00 0.0959 0.2237 0.0929 0.0398 0.017 1.041 0.694 12.321 0.118 3.085 25.530 0.09 56009. 0.5670
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2.50 0.1199 0.2718 0.0907 0.0400 0.017 1.046 0.677 12.375 0.118 3.012 24.815 0.09 56061. 0.5446
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3.00 0.1439 0.3169 0.0883 0.0401 0.017 1.049 0.660 12.408 0.118 2.934 24.111 0.09 56116. 0.5222
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3.50 0.1679 0.3590 0.0859 0.0401 0.017 1.049 0.641 12.415 0.119 2.851 23.416 0.09 56175. 0.5000
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4.00 0.1919 0.3983 0.0832 0.0401 0.017 1.048 0.621 12.394 0.118 2.763 22.731 0.09 56238. 0.4778
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4.50 0.2158 0.4348 0.0804 0.0399 0.017 1.043 0.600 12.343 0.118 2.670 22.056 0.09 56305. 0.4557
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5.00 0.2398 0.4685 0.0774 0.0396 0.016 1.036 0.578 12.258 0.117 2.571 21.389 0.09 56376. 0.4337
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5.50 0.2638 0.4994 0.0743 0.0392 0.016 1.026 0.555 12.136 0.116 2.467 20.728 0.09 56450. 0.4117
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6.00 0.2878 0.5276 0.0710 0.0387 0.016 1.012 0.530 11.975 0.114 2.357 20.073 0.09 56529. 0.3897
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6.50 0.3118 0.5530 0.0675 0.0381 0.016 0.995 0.504 11.772 0.112 2.242 19.420 0.09 56611. 0.3677
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6.99 0.3358 0.5755 0.0639 0.0373 0.015 0.974 0.477 11.527 0.110 2.121 18.767 0.09 56698. 0.3457
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7.49 0.3597 0.5950 0.0601 0.0363 0.015 0.950 0.449 11.240 0.107 1.996 18.110 0.09 56789. 0.3236
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7.99 0.3837 0.6114 0.0562 0.0353 0.015 0.922 0.420 10.913 0.104 1.867 17.444 0.09 56884. 0.3014
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8.49 0.4077 0.6242 0.0522 0.0341 0.014 0.891 0.390 10.545 0.101 1.733 16.764 0.09 56984. 0.2791
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8.99 0.4317 0.6333 0.0481 0.0328 0.014 0.857 0.359 10.137 0.097 1.597 16.062 0.09 57087. 0.2567
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9.49 0.4557 0.6381 0.0439 0.0313 0.013 0.819 0.328 9.690 0.093 1.457 15.331 0.09 57195. 0.2340
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9.99 0.4797 0.6379 0.0396 0.0298 0.012 0.778 0.296 9.205 0.088 1.314 14.561 0.09 57307. 0.2111
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10.49 0.5036 0.6319 0.0352 0.0281 0.012 0.734 0.263 8.682 0.083 1.170 13.738 0.09 57423. 0.1879
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10.99 0.5276 0.6190 0.0308 0.0263 0.011 0.687 0.230 8.124 0.078 1.023 12.845 0.09 57544. 0.1643
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11.49 0.5516 0.5974 0.0264 0.0243 0.010 0.636 0.197 7.530 0.072 0.876 11.857 0.09 57669. 0.1403
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11.99 0.5756 0.5646 0.0219 0.0223 0.009 0.583 0.163 6.903 0.066 0.727 10.740 0.09 57798. 0.1158
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12.49 0.5996 0.5172 0.0174 0.0202 0.008 0.528 0.130 6.245 0.060 0.578 9.444 0.09 57932. 0.0908
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12.99 0.6236 0.4494 0.0130 0.0180 0.007 0.470 0.097 5.559 0.053 0.430 7.891 0.09 58070. 0.0654
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13.49 0.6475 0.3523 0.0085 0.0157 0.007 0.410 0.064 4.847 0.046 0.283 5.956 0.09 58213. 0.0401
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13.99 0.6715 0.2099 0.0042 0.0133 0.006 0.348 0.031 4.114 0.039 0.138 3.423 0.09 58360. 0.0161
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14.49 0.6955 -0.0085 -0.0001 0.0109 0.005 0.284 -0.001 3.363 0.032 -0.004 -0.134 0.09 58509. 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 0.1008 0.0363 0.121 3.800 3.010 89.917 0.429 13.390 15.185 0.17 111665. 0.7027
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1.00 0.0240 0.0648 0.0991 0.0367 0.122 3.842 2.960 90.918 0.434 13.167 14.767 0.17 111744. 0.6776
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2.00 0.0481 0.1260 0.0973 0.0371 0.123 3.881 2.906 91.828 0.438 12.927 14.355 0.17 111828. 0.6527
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3.00 0.0721 0.1837 0.0954 0.0374 0.124 3.914 2.848 92.626 0.442 12.670 13.948 0.17 111919. 0.6279
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4.01 0.0961 0.2379 0.0933 0.0377 0.125 3.943 2.787 93.290 0.445 12.395 13.549 0.17 112016. 0.6032
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5.01 0.1202 0.2888 0.0911 0.0379 0.126 3.964 2.721 93.797 0.448 12.102 13.157 0.17 112121. 0.5788
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6.01 0.1442 0.3364 0.0888 0.0380 0.126 3.978 2.651 94.125 0.449 11.789 12.772 0.17 112232. 0.5546
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7.01 0.1682 0.3809 0.0863 0.0381 0.126 3.983 2.576 94.248 0.450 11.457 12.396 0.17 112351. 0.5306
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8.01 0.1923 0.4224 0.0836 0.0381 0.126 3.979 2.496 94.144 0.450 11.104 12.027 0.17 112477. 0.5068
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9.01 0.2163 0.4609 0.0808 0.0379 0.126 3.964 2.412 93.787 0.448 10.729 11.666 0.17 112611. 0.4832
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10.01 0.2403 0.4966 0.0778 0.0377 0.125 3.937 2.323 93.155 0.445 10.333 11.311 0.18 112753. 0.4598
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11.02 0.2644 0.5294 0.0746 0.0373 0.124 3.897 2.229 92.221 0.440 9.915 10.963 0.18 112902. 0.4366
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12.02 0.2884 0.5595 0.0713 0.0368 0.122 3.844 2.130 90.957 0.434 9.474 10.621 0.18 113060. 0.4134
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13.02 0.3124 0.5869 0.0678 0.0361 0.120 3.776 2.026 89.346 0.427 9.010 10.283 0.18 113226. 0.3904
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14.02 0.3365 0.6115 0.0642 0.0353 0.117 3.693 1.917 87.383 0.417 8.526 9.949 0.18 113401. 0.3674
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15.02 0.3605 0.6332 0.0604 0.0344 0.114 3.595 1.804 85.072 0.406 8.022 9.616 0.18 113583. 0.3444
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16.02 0.3845 0.6520 0.0565 0.0333 0.111 3.483 1.687 82.414 0.393 7.502 9.282 0.18 113774. 0.3215
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17.02 0.4086 0.6675 0.0524 0.0321 0.106 3.356 1.566 79.415 0.379 6.966 8.945 0.18 113974. 0.2986
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18.02 0.4326 0.6796 0.0483 0.0307 0.102 3.215 1.443 76.077 0.363 6.417 8.601 0.18 114182. 0.2755
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19.03 0.4566 0.6878 0.0441 0.0293 0.097 3.060 1.316 72.405 0.346 5.855 8.246 0.18 114398. 0.2523
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20.03 0.4807 0.6915 0.0398 0.0276 0.092 2.891 1.188 68.405 0.327 5.283 7.876 0.18 114623. 0.2289
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21.03 0.5047 0.6898 0.0354 0.0259 0.086 2.708 1.057 64.083 0.306 4.703 7.483 0.18 114857. 0.2052
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22.03 0.5287 0.6817 0.0310 0.0240 0.080 2.512 0.925 59.449 0.284 4.115 7.059 0.18 115099. 0.1811
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23.03 0.5528 0.6654 0.0265 0.0220 0.073 2.304 0.792 54.513 0.260 3.523 6.590 0.18 115350. 0.1564
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24.03 0.5768 0.6381 0.0220 0.0199 0.066 2.083 0.658 49.292 0.235 2.928 6.057 0.18 115610. 0.1311
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25.03 0.6008 0.5960 0.0176 0.0177 0.059 1.851 0.524 43.803 0.209 2.333 5.430 0.18 115879. 0.1049
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26.04 0.6249 0.5319 0.0131 0.0154 0.051 1.609 0.391 38.070 0.182 1.740 4.660 0.18 116156. 0.0777
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27.04 0.6489 0.4335 0.0087 0.0130 0.043 1.358 0.259 32.122 0.153 1.152 3.657 0.18 116442. 0.0496
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28.04 0.6729 0.2763 0.0043 0.0105 0.035 1.098 0.129 25.991 0.124 0.573 2.248 0.18 116737. 0.0215
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29.04 0.6969 0.0026 0.0000 0.0080 0.026 0.832 0.001 19.697 0.094 0.004 0.021 0.18 117035. 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 0.0355 0.398 8.356 6.810 296.588 0.944 30.289 10.414 0.26 167491. 0.7248
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1.51 0.0241 0.0668 0.0997 0.0359 0.402 8.455 6.696 300.093 0.955 29.786 10.121 0.26 167609. 0.6986
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3.01 0.0482 0.1298 0.0979 0.0363 0.407 8.545 6.575 303.292 0.965 29.245 9.833 0.26 167737. 0.6725
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4.52 0.0722 0.1890 0.0959 0.0367 0.410 8.624 6.445 306.108 0.974 28.666 9.549 0.26 167873. 0.6466
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6.02 0.0963 0.2447 0.0938 0.0369 0.414 8.691 6.305 308.465 0.982 28.045 9.271 0.26 168020. 0.6209
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7.53 0.1204 0.2969 0.0916 0.0372 0.416 8.742 6.156 310.285 0.988 27.383 8.999 0.26 168178. 0.5955
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9.03 0.1445 0.3457 0.0893 0.0373 0.418 8.776 5.997 311.486 0.991 26.676 8.733 0.26 168345. 0.5704
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10.54 0.1686 0.3913 0.0867 0.0374 0.418 8.790 5.828 311.986 0.993 25.923 8.473 0.26 168524. 0.5456
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12.04 0.1926 0.4339 0.0841 0.0373 0.418 8.782 5.648 311.702 0.992 25.124 8.219 0.26 168715. 0.5210
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13.55 0.2167 0.4734 0.0812 0.0372 0.416 8.749 5.458 310.549 0.989 24.276 7.971 0.26 168916. 0.4967
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15.05 0.2408 0.5100 0.0782 0.0369 0.414 8.690 5.256 308.445 0.982 23.379 7.729 0.26 169130. 0.4726
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16.56 0.2649 0.5438 0.0751 0.0366 0.409 8.602 5.043 305.299 0.972 22.432 7.492 0.26 169356. 0.4488
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18.06 0.2890 0.5749 0.0717 0.0360 0.404 8.481 4.818 301.012 0.958 21.432 7.260 0.26 169593. 0.4251
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19.57 0.3131 0.6032 0.0682 0.0354 0.396 8.326 4.582 295.523 0.941 20.381 7.032 0.26 169844. 0.4015
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21.07 0.3371 0.6289 0.0645 0.0346 0.387 8.137 4.335 288.815 0.919 19.282 6.808 0.26 170106. 0.3780
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22.58 0.3612 0.6518 0.0607 0.0336 0.377 7.914 4.078 280.895 0.894 18.141 6.585 0.26 170382. 0.3547
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24.08 0.3853 0.6718 0.0568 0.0325 0.364 7.657 3.813 271.770 0.865 16.960 6.364 0.26 170670. 0.3314
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25.59 0.4094 0.6888 0.0527 0.0313 0.351 7.366 3.540 261.451 0.832 15.745 6.141 0.26 170970. 0.3082
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27.09 0.4335 0.7025 0.0485 0.0299 0.335 7.042 3.260 249.950 0.796 14.499 5.915 0.26 171283. 0.2848
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28.60 0.4575 0.7126 0.0443 0.0284 0.318 6.685 2.973 237.282 0.755 13.226 5.684 0.26 171609. 0.2614
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30.10 0.4816 0.7184 0.0399 0.0268 0.300 6.296 2.682 223.464 0.711 11.929 5.444 0.26 171948. 0.2378
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31.61 0.5057 0.7192 0.0355 0.0250 0.280 5.875 2.386 208.520 0.664 10.613 5.190 0.27 172300. 0.2138
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33.11 0.5298 0.7138 0.0311 0.0231 0.258 5.423 2.087 192.481 0.613 9.282 4.917 0.27 172665. 0.1895
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34.62 0.5539 0.7006 0.0266 0.0210 0.235 4.941 1.785 175.387 0.558 7.940 4.616 0.27 173043. 0.1645
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36.12 0.5779 0.6768 0.0221 0.0188 0.211 4.432 1.482 157.292 0.501 6.592 4.274 0.27 173434. 0.1388
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37.63 0.6020 0.6380 0.0175 0.0166 0.185 3.895 1.179 138.259 0.440 5.244 3.868 0.27 173838. 0.1120
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39.13 0.6261 0.5767 0.0131 0.0142 0.159 3.335 0.877 118.374 0.377 3.903 3.362 0.27 174256. 0.0840
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40.64 0.6502 0.4783 0.0086 0.0117 0.131 2.754 0.579 97.736 0.311 2.573 2.685 0.27 174687. 0.0545
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42.14 0.6743 0.3115 0.0042 0.0092 0.103 2.154 0.284 76.466 0.243 1.264 1.686 0.27 175130. 0.0240
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43.65 0.6984 -0.0083 -0.0001 0.0065 0.073 1.538 -0.005 54.597 0.174 -0.023 -0.043 0.27 175576. 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 0.1021 0.0352 0.935 14.735 12.192 697.344 1.665 54.232 7.930 0.35 223309. 0.7385
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2.01 0.0241 0.0678 0.1004 0.0357 0.947 14.915 11.991 705.863 1.685 53.337 7.705 0.35 223467. 0.7116
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4.01 0.0482 0.1317 0.0986 0.0361 0.957 15.080 11.775 713.645 1.704 52.374 7.484 0.35 223637. 0.6849
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6.02 0.0723 0.1918 0.0966 0.0364 0.966 15.225 11.543 720.506 1.720 51.342 7.266 0.35 223820. 0.6584
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8.03 0.0963 0.2483 0.0946 0.0367 0.974 15.346 11.294 726.264 1.734 50.236 7.053 0.35 224017. 0.6322
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10.04 0.1204 0.3012 0.0923 0.0369 0.980 15.441 11.028 730.730 1.744 49.054 6.845 0.35 224227. 0.6063
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12.04 0.1445 0.3507 0.0900 0.0371 0.984 15.504 10.745 733.705 1.752 47.793 6.642 0.35 224451. 0.5807
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14.05 0.1686 0.3969 0.0874 0.0371 0.986 15.531 10.443 734.990 1.755 46.449 6.444 0.35 224691. 0.5554
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16.06 0.1927 0.4401 0.0847 0.0371 0.985 15.518 10.122 734.383 1.753 45.021 6.251 0.35 224945. 0.5304
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18.06 0.2168 0.4802 0.0819 0.0370 0.981 15.461 9.781 731.684 1.747 43.506 6.063 0.35 225215. 0.5057
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20.07 0.2409 0.5174 0.0789 0.0367 0.975 15.355 9.420 726.690 1.735 41.902 5.880 0.35 225500. 0.4813
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22.08 0.2649 0.5518 0.0757 0.0363 0.964 15.197 9.039 719.182 1.717 40.207 5.701 0.35 225802. 0.4571
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24.09 0.2890 0.5835 0.0723 0.0358 0.951 14.980 8.637 708.926 1.692 38.418 5.526 0.35 226120. 0.4331
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26.09 0.3131 0.6125 0.0688 0.0352 0.933 14.702 8.214 695.760 1.661 36.536 5.355 0.35 226454. 0.4093
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28.10 0.3372 0.6389 0.0651 0.0343 0.911 14.361 7.772 679.644 1.623 34.569 5.187 0.35 226805. 0.3856
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30.11 0.3613 0.6627 0.0612 0.0334 0.886 13.959 7.312 660.587 1.577 32.524 5.021 0.35 227173. 0.3621
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32.11 0.3854 0.6836 0.0572 0.0323 0.856 13.494 6.837 638.608 1.525 30.409 4.856 0.35 227557. 0.3386
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34.12 0.4095 0.7017 0.0531 0.0310 0.823 12.969 6.347 613.731 1.465 28.232 4.691 0.35 227959. 0.3152
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36.13 0.4336 0.7166 0.0489 0.0296 0.786 12.382 5.845 585.982 1.399 25.998 4.524 0.35 228377. 0.2917
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38.14 0.4576 0.7280 0.0446 0.0281 0.745 11.736 5.332 555.395 1.326 23.716 4.354 0.35 228812. 0.2682
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40.14 0.4817 0.7354 0.0403 0.0264 0.700 11.030 4.809 522.012 1.246 21.391 4.179 0.35 229265. 0.2444
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42.15 0.5058 0.7381 0.0358 0.0245 0.652 10.267 4.279 485.891 1.160 19.032 3.994 0.35 229734. 0.2203
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44.16 0.5299 0.7349 0.0313 0.0226 0.600 9.448 3.742 447.105 1.067 16.645 3.796 0.35 230221. 0.1959
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46.17 0.5540 0.7242 0.0268 0.0205 0.544 8.574 3.201 405.753 0.969 14.239 3.578 0.35 230726. 0.1708
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48.17 0.5781 0.7034 0.0223 0.0183 0.485 7.648 2.658 361.962 0.864 11.822 3.331 0.35 231248. 0.1448
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50.18 0.6022 0.6679 0.0177 0.0160 0.424 6.675 2.115 315.892 0.754 9.406 3.036 0.36 231787. 0.1178
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52.19 0.6262 0.6099 0.0132 0.0135 0.359 5.658 1.574 267.746 0.639 7.000 2.666 0.36 232344. 0.0892
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54.19 0.6503 0.5137 0.0087 0.0110 0.292 4.602 1.038 217.774 0.520 4.618 2.162 0.36 232919. 0.0588
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56.20 0.6744 0.3432 0.0043 0.0084 0.223 3.513 0.511 166.270 0.397 2.271 1.393 0.36 233510. 0.0265
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58.21 0.6985 -0.0087 -0.0001 0.0057 0.152 2.394 -0.008 113.272 0.270 -0.038 -0.034 0.36 234102. 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 0.1030 0.0353 1.828 23.047 19.226 1363.377 2.604 85.519 6.396 0.44 279115. 0.7480
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2.51 0.0241 0.0683 0.1013 0.0357 1.851 23.334 18.912 1380.369 2.636 84.120 6.214 0.44 279313. 0.7208
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5.02 0.0481 0.1327 0.0995 0.0361 1.872 23.597 18.574 1395.893 2.666 82.615 6.035 0.44 279526. 0.6937
|
|
7.52 0.0722 0.1932 0.0976 0.0365 1.890 23.828 18.210 1409.587 2.692 80.999 5.860 0.44 279756. 0.6669
|
|
10.03 0.0963 0.2501 0.0955 0.0368 1.906 24.023 17.821 1421.087 2.714 79.267 5.688 0.44 280002. 0.6404
|
|
12.54 0.1204 0.3034 0.0933 0.0370 1.918 24.174 17.404 1430.013 2.731 77.414 5.520 0.44 280266. 0.6142
|
|
15.05 0.1444 0.3533 0.0909 0.0371 1.926 24.274 16.959 1435.976 2.743 75.435 5.357 0.44 280547. 0.5884
|
|
17.55 0.1685 0.4000 0.0883 0.0372 1.929 24.318 16.485 1438.575 2.747 73.325 5.198 0.44 280847. 0.5628
|
|
20.06 0.1926 0.4435 0.0856 0.0372 1.928 24.299 15.981 1437.413 2.745 71.081 5.043 0.44 281166. 0.5376
|
|
22.57 0.2167 0.4840 0.0828 0.0370 1.920 24.209 15.445 1432.088 2.735 68.700 4.892 0.44 281504. 0.5127
|
|
25.08 0.2407 0.5216 0.0797 0.0368 1.907 24.042 14.878 1422.198 2.716 66.178 4.745 0.44 281862. 0.4881
|
|
27.58 0.2648 0.5565 0.0765 0.0364 1.887 23.790 14.278 1407.317 2.688 63.511 4.602 0.44 282240. 0.4638
|
|
30.09 0.2889 0.5887 0.0731 0.0359 1.860 23.446 13.645 1386.978 2.649 60.694 4.462 0.44 282638. 0.4396
|
|
32.60 0.3129 0.6182 0.0695 0.0352 1.825 23.004 12.979 1360.845 2.599 57.731 4.326 0.44 283056. 0.4157
|
|
35.11 0.3370 0.6452 0.0658 0.0344 1.782 22.463 12.282 1328.826 2.538 54.630 4.192 0.44 283496. 0.3919
|
|
37.61 0.3611 0.6696 0.0619 0.0334 1.731 21.823 11.557 1290.934 2.466 51.406 4.061 0.44 283956. 0.3682
|
|
40.12 0.3852 0.6913 0.0579 0.0323 1.673 21.083 10.807 1247.209 2.382 48.071 3.930 0.44 284437. 0.3446
|
|
42.63 0.4092 0.7102 0.0538 0.0310 1.606 20.246 10.035 1197.697 2.287 44.635 3.800 0.44 284939. 0.3211
|
|
45.14 0.4333 0.7261 0.0495 0.0296 1.532 19.313 9.242 1142.452 2.182 41.110 3.669 0.44 285462. 0.2975
|
|
47.64 0.4574 0.7386 0.0452 0.0280 1.450 18.283 8.432 1081.538 2.066 37.506 3.536 0.44 286006. 0.2739
|
|
50.15 0.4815 0.7473 0.0408 0.0263 1.361 17.159 7.607 1015.041 1.939 33.836 3.399 0.44 286572. 0.2500
|
|
52.66 0.5055 0.7516 0.0363 0.0244 1.265 15.942 6.769 943.071 1.801 30.109 3.256 0.44 287159. 0.2259
|
|
55.17 0.5296 0.7502 0.0317 0.0224 1.161 14.636 5.921 865.779 1.654 26.338 3.102 0.44 287767. 0.2013
|
|
57.67 0.5537 0.7417 0.0271 0.0203 1.051 13.242 5.067 783.360 1.496 22.537 2.934 0.44 288398. 0.1761
|
|
60.18 0.5777 0.7235 0.0225 0.0180 0.933 11.767 4.208 696.063 1.329 18.718 2.742 0.44 289050. 0.1500
|
|
62.69 0.6018 0.6911 0.0179 0.0156 0.810 10.214 3.350 604.213 1.154 14.899 2.515 0.44 289724. 0.1227
|
|
65.20 0.6259 0.6364 0.0134 0.0131 0.682 8.591 2.495 508.215 0.971 11.097 2.227 0.44 290420. 0.0938
|
|
67.70 0.6500 0.5430 0.0088 0.0106 0.548 6.907 1.648 408.569 0.780 7.330 1.830 0.45 291137. 0.0626
|
|
70.21 0.6740 0.3716 0.0044 0.0079 0.410 5.171 0.814 305.868 0.584 3.621 1.207 0.45 291876. 0.0291
|
|
72.72 0.6981 -0.0049 0.0000 0.0052 0.268 3.384 -0.007 200.159 0.382 -0.030 -0.015 0.45 292614. 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 0.1042 0.0356 3.185 33.461 28.007 2375.288 3.780 124.576 5.348 0.52 334904. 0.7549
|
|
3.01 0.0241 0.0685 0.1025 0.0360 3.226 33.883 27.555 2405.286 3.828 122.563 5.196 0.52 335143. 0.7275
|
|
6.02 0.0481 0.1331 0.1007 0.0364 3.262 34.269 27.067 2432.682 3.872 120.394 5.047 0.52 335400. 0.7003
|
|
9.02 0.0722 0.1938 0.0988 0.0368 3.295 34.610 26.543 2456.837 3.910 118.062 4.900 0.52 335677. 0.6733
|
|
12.03 0.0962 0.2509 0.0967 0.0371 3.322 34.895 25.980 2477.106 3.942 115.560 4.757 0.52 335974. 0.6467
|
|
15.04 0.1203 0.3044 0.0944 0.0373 3.343 35.116 25.378 2492.814 3.967 112.879 4.617 0.52 336292. 0.6204
|
|
18.05 0.1444 0.3546 0.0920 0.0375 3.357 35.264 24.733 2503.277 3.984 110.014 4.481 0.52 336631. 0.5944
|
|
21.05 0.1684 0.4014 0.0895 0.0375 3.363 35.327 24.046 2507.787 3.991 106.956 4.349 0.52 336992. 0.5688
|
|
24.06 0.1925 0.4452 0.0868 0.0375 3.360 35.297 23.314 2505.641 3.988 103.702 4.220 0.52 337376. 0.5435
|
|
27.07 0.2166 0.4860 0.0839 0.0374 3.347 35.163 22.537 2496.132 3.973 100.245 4.095 0.52 337783. 0.5185
|
|
30.08 0.2406 0.5239 0.0808 0.0371 3.324 34.916 21.713 2478.561 3.945 96.580 3.973 0.53 338214. 0.4938
|
|
33.09 0.2647 0.5592 0.0776 0.0367 3.288 34.544 20.842 2452.182 3.903 92.704 3.855 0.53 338669. 0.4694
|
|
36.09 0.2887 0.5917 0.0741 0.0362 3.240 34.037 19.921 2416.179 3.845 88.608 3.740 0.53 339148. 0.4452
|
|
39.10 0.3128 0.6217 0.0705 0.0355 3.178 33.385 18.951 2369.933 3.772 84.294 3.627 0.53 339651. 0.4211
|
|
42.11 0.3369 0.6492 0.0667 0.0346 3.102 32.587 17.936 2313.260 3.682 79.778 3.517 0.53 340180. 0.3972
|
|
45.12 0.3609 0.6742 0.0628 0.0336 3.012 31.642 16.879 2246.185 3.575 75.079 3.408 0.53 340733. 0.3735
|
|
48.12 0.3850 0.6965 0.0587 0.0325 2.908 30.552 15.786 2168.780 3.452 70.215 3.301 0.53 341311. 0.3498
|
|
51.13 0.4091 0.7162 0.0545 0.0312 2.791 29.317 14.659 2081.128 3.312 65.202 3.195 0.53 341915. 0.3262
|
|
54.14 0.4331 0.7329 0.0502 0.0297 2.660 27.939 13.502 1983.331 3.157 60.057 3.088 0.53 342543. 0.3026
|
|
57.15 0.4572 0.7464 0.0458 0.0281 2.515 26.420 12.319 1875.504 2.985 54.795 2.979 0.53 343197. 0.2789
|
|
60.16 0.4812 0.7563 0.0414 0.0263 2.357 24.762 11.114 1757.801 2.798 49.434 2.868 0.53 343876. 0.2550
|
|
63.16 0.5053 0.7618 0.0368 0.0244 2.186 22.968 9.890 1630.419 2.595 43.989 2.751 0.53 344581. 0.2308
|
|
66.17 0.5294 0.7621 0.0322 0.0224 2.003 21.041 8.651 1493.621 2.377 38.478 2.627 0.53 345312. 0.2061
|
|
69.18 0.5534 0.7554 0.0275 0.0202 1.807 18.986 7.401 1347.754 2.145 32.921 2.491 0.53 346068. 0.1807
|
|
72.19 0.5775 0.7393 0.0229 0.0179 1.600 16.810 6.146 1193.261 1.899 27.338 2.336 0.53 346851. 0.1545
|
|
75.20 0.6016 0.7094 0.0182 0.0154 1.382 14.520 4.890 1030.717 1.640 21.753 2.152 0.53 347659. 0.1269
|
|
78.20 0.6256 0.6575 0.0135 0.0129 1.154 12.127 3.640 860.842 1.370 16.190 1.918 0.53 348494. 0.0976
|
|
81.21 0.6497 0.5664 0.0089 0.0102 0.918 9.643 2.401 684.529 1.089 10.680 1.591 0.53 349355. 0.0658
|
|
84.22 0.6737 0.3934 0.0044 0.0075 0.674 7.083 1.181 502.834 0.800 5.254 1.065 0.54 350241. 0.0309
|
|
87.23 0.6978 -0.0115 -0.0001 0.0047 0.423 4.447 -0.021 315.670 0.502 -0.093 -0.030 0.54 351121. 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 0.1057 0.0361 5.134 46.226 38.670 3828.358 5.223 172.002 4.581 0.61 390671. 0.7598
|
|
3.52 0.0241 0.0687 0.1040 0.0366 5.200 46.817 38.052 3877.324 5.289 169.257 4.451 0.61 390952. 0.7324
|
|
7.04 0.0483 0.1334 0.1022 0.0370 5.259 47.357 37.386 3921.985 5.350 166.293 4.324 0.61 391255. 0.7051
|
|
10.56 0.0724 0.1943 0.1002 0.0373 5.312 47.831 36.668 3961.283 5.404 163.101 4.199 0.61 391581. 0.6781
|
|
14.07 0.0965 0.2515 0.0981 0.0377 5.356 48.228 35.897 3994.159 5.449 159.670 4.076 0.61 391931. 0.6514
|
|
17.59 0.1206 0.3052 0.0959 0.0379 5.390 48.534 35.069 4019.504 5.483 155.989 3.957 0.61 392305. 0.6250
|
|
21.11 0.1448 0.3555 0.0934 0.0381 5.413 48.735 34.183 4036.180 5.506 152.046 3.841 0.61 392705. 0.5990
|
|
24.63 0.1689 0.4026 0.0909 0.0381 5.422 48.818 33.236 4043.031 5.515 147.834 3.729 0.61 393130. 0.5733
|
|
28.15 0.1930 0.4466 0.0881 0.0381 5.416 48.768 32.227 4038.899 5.510 143.344 3.619 0.61 393583. 0.5480
|
|
31.67 0.2171 0.4876 0.0852 0.0379 5.394 48.572 31.153 4022.634 5.488 138.568 3.513 0.61 394062. 0.5229
|
|
35.19 0.2413 0.5259 0.0820 0.0376 5.355 48.215 30.014 3993.086 5.447 133.501 3.409 0.61 394569. 0.4981
|
|
38.70 0.2654 0.5614 0.0788 0.0372 5.296 47.683 28.807 3949.057 5.387 128.136 3.309 0.61 395104. 0.4736
|
|
42.22 0.2895 0.5943 0.0753 0.0367 5.216 46.961 27.532 3889.229 5.306 122.461 3.211 0.61 395668. 0.4493
|
|
45.74 0.3137 0.6247 0.0716 0.0359 5.113 46.035 26.187 3812.552 5.201 116.479 3.115 0.61 396261. 0.4252
|
|
49.26 0.3378 0.6526 0.0677 0.0351 4.987 44.902 24.778 3718.715 5.073 110.212 3.022 0.61 396882. 0.4012
|
|
52.78 0.3619 0.6781 0.0637 0.0340 4.838 43.563 23.311 3607.771 4.922 103.686 2.931 0.61 397533. 0.3774
|
|
56.30 0.3860 0.7010 0.0596 0.0328 4.667 42.018 21.791 3479.848 4.747 96.926 2.840 0.62 398213. 0.3536
|
|
59.82 0.4102 0.7212 0.0553 0.0314 4.472 40.270 20.224 3335.103 4.550 89.956 2.750 0.62 398922. 0.3299
|
|
63.33 0.4343 0.7387 0.0509 0.0299 4.256 38.321 18.615 3173.714 4.330 82.800 2.660 0.62 399660. 0.3061
|
|
66.85 0.4584 0.7530 0.0464 0.0282 4.018 36.174 16.969 2995.881 4.087 75.480 2.569 0.62 400428. 0.2823
|
|
70.37 0.4825 0.7637 0.0418 0.0264 3.757 33.831 15.292 2801.865 3.822 68.017 2.475 0.62 401226. 0.2582
|
|
73.89 0.5067 0.7702 0.0371 0.0244 3.476 31.298 13.588 2592.007 3.536 60.437 2.378 0.62 402054. 0.2338
|
|
77.41 0.5308 0.7715 0.0324 0.0223 3.174 28.578 11.862 2366.746 3.229 52.764 2.273 0.62 402911. 0.2088
|
|
80.93 0.5549 0.7659 0.0277 0.0200 2.852 25.679 10.123 2126.666 2.901 45.025 2.159 0.62 403799. 0.1832
|
|
84.45 0.5791 0.7510 0.0229 0.0177 2.511 22.610 8.374 1872.516 2.554 37.249 2.028 0.62 404717. 0.1566
|
|
87.96 0.6032 0.7219 0.0181 0.0151 2.153 19.383 6.626 1605.257 2.190 29.470 1.872 0.62 405666. 0.1285
|
|
91.48 0.6273 0.6700 0.0134 0.0125 1.778 16.012 4.884 1326.105 1.809 21.725 1.671 0.62 406645. 0.0985
|
|
95.00 0.6514 0.5758 0.0086 0.0098 1.390 12.516 3.160 1036.569 1.414 14.054 1.383 0.62 407655. 0.0655
|
|
98.52 0.6756 0.3878 0.0040 0.0070 0.990 8.916 1.462 738.421 1.007 6.503 0.898 0.62 408693. 0.0290
|
|
102.04 0.6997
|
|
|
|
|
|
|
|
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 0.1076 0.0369 7.837 61.746 51.402 5844.250 6.976 228.635 3.989 0.70 446408. 0.7628
|
|
4.00 0.0240 0.0680 0.1059 0.0374 7.937 62.533 50.604 5918.757 7.065 225.084 3.878 0.70 446729. 0.7357
|
|
7.99 0.0480 0.1321 0.1041 0.0378 8.028 63.252 49.740 5986.726 7.146 221.243 3.768 0.70 447076. 0.7088
|
|
11.99 0.0720 0.1925 0.1022 0.0382 8.108 63.883 48.808 6046.491 7.217 217.097 3.661 0.70 447449. 0.6822
|
|
15.99 0.0959 0.2493 0.1001 0.0385 8.175 64.411 47.804 6096.423 7.277 212.633 3.557 0.70 447849. 0.6559
|
|
19.99 0.1199 0.3027 0.0978 0.0387 8.227 64.816 46.725 6134.842 7.323 207.834 3.455 0.70 448276. 0.6298
|
|
23.98 0.1439 0.3528 0.0954 0.0389 8.261 65.082 45.568 6160.020 7.353 202.687 3.355 0.70 448733. 0.6041
|
|
27.98 0.1679 0.3998 0.0928 0.0390 8.274 65.190 44.330 6170.199 7.365 197.179 3.259 0.70 449219. 0.5787
|
|
31.98 0.1919 0.4437 0.0900 0.0389 8.266 65.121 43.008 6163.630 7.357 191.299 3.165 0.70 449735. 0.5536
|
|
35.98 0.2159 0.4848 0.0871 0.0388 8.232 64.856 41.600 6138.583 7.327 185.038 3.074 0.70 450282. 0.5288
|
|
39.97 0.2398 0.5232 0.0839 0.0385 8.171 64.378 40.105 6093.330 7.273 178.387 2.985 0.70 450860. 0.5042
|
|
43.97 0.2638 0.5589 0.0806 0.0381 8.081 63.668 38.520 6026.111 7.193 171.338 2.899 0.70 451469. 0.4799
|
|
47.97 0.2878 0.5921 0.0771 0.0375 7.959 62.705 36.843 5934.989 7.084 163.877 2.816 0.70 452111. 0.4558
|
|
51.97 0.3118 0.6229 0.0734 0.0367 7.802 61.471 35.073 5818.242 6.945 156.003 2.734 0.70 452786. 0.4319
|
|
55.96 0.3358 0.6513 0.0695 0.0358 7.611 59.961 33.215 5675.267 6.774 147.740 2.655 0.70 453493. 0.4080
|
|
59.96 0.3598 0.6773 0.0655 0.0348 7.384 58.174 31.278 5506.119 6.572 139.125 2.577 0.70 454233. 0.3843
|
|
63.96 0.3838 0.7009 0.0613 0.0335 7.122 56.113 29.269 5311.027 6.340 130.190 2.500 0.70 455005. 0.3607
|
|
67.96 0.4077 0.7220 0.0569 0.0321 6.826 53.780 27.196 5090.256 6.076 120.969 2.423 0.70 455811. 0.3371
|
|
71.95 0.4317 0.7404 0.0525 0.0306 6.496 51.179 25.066 4844.095 5.782 111.493 2.347 0.70 456649. 0.3134
|
|
75.95 0.4557 0.7558 0.0479 0.0289 6.132 48.314 22.884 4572.861 5.458 101.790 2.270 0.71 457521. 0.2896
|
|
79.95 0.4797 0.7679 0.0432 0.0270 5.735 45.187 20.659 4276.960 5.105 91.891 2.191 0.71 458425. 0.2656
|
|
83.95 0.5037 0.7761 0.0385 0.0250 5.306 41.806 18.397 3956.899 4.723 81.828 2.109 0.71 459364. 0.2412
|
|
87.94 0.5277 0.7794 0.0337 0.0228 4.846 38.176 16.104 3613.342 4.313 71.632 2.022 0.71 460336. 0.2164
|
|
91.94 0.5517 0.7764 0.0289 0.0205 4.355 34.308 13.790 3247.208 3.876 61.338 1.926 0.71 461341. 0.1908
|
|
95.94 0.5756 0.7647 0.0240 0.0181 3.835 30.214 11.463 2859.716 3.414 50.987 1.818 0.71 462381. 0.1642
|
|
99.94 0.5996 0.7400 0.0191 0.0155 3.289 25.911 9.132 2452.444 2.927 40.619 1.689 0.71 463455. 0.1361
|
|
103.93 0.6236 0.6940 0.0143 0.0128 2.719 21.420 6.809 2027.423 2.420 30.285 1.523 0.71 464563. 0.1060
|
|
107.93 0.6476 0.6091 0.0094 0.0100 2.128 16.769 4.505 1587.184 1.895 20.037 1.287 0.71 465705. 0.0729
|
|
111.93 0.6716 0.4381 0.0047 0.0072 1.522 11.989 2.234 1134.779 1.355 9.936 0.893 0.71 466880. 0.0356
|
|
115.93 0.6956 -0.0015 0.0000 0.0042 0.899 7.085 -0.004 670.570 0.800 -0.019 -0.003 0.72 468049. 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 0.1099 0.0387 11.710 82.008 66.461 8732.263 9.265 295.620 3.452 0.79 502102. 0.7506
|
|
4.49 0.0239 0.0662 0.1083 0.0391 11.829 82.838 65.464 8820.652 9.359 291.186 3.366 0.79 502466. 0.7264
|
|
8.97 0.0479 0.1291 0.1065 0.0395 11.936 83.589 64.382 8900.604 9.444 286.369 3.281 0.79 502859. 0.7021
|
|
13.46 0.0718 0.1886 0.1045 0.0398 12.029 84.240 63.209 8969.919 9.517 281.153 3.196 0.79 503280. 0.6777
|
|
17.95 0.0957 0.2449 0.1024 0.0400 12.105 84.770 61.942 9026.391 9.577 275.518 3.113 0.79 503733. 0.6534
|
|
22.43 0.1196 0.2980 0.1002 0.0402 12.160 85.158 60.576 9067.634 9.621 269.441 3.030 0.79 504217. 0.6290
|
|
26.92 0.1436 0.3480 0.0977 0.0403 12.191 85.378 59.106 9091.125 9.646 262.905 2.949 0.79 504734. 0.6047
|
|
31.40 0.1675 0.3950 0.0951 0.0403 12.196 85.408 57.530 9094.271 9.649 255.893 2.869 0.79 505283. 0.5804
|
|
35.89 0.1914 0.4392 0.0923 0.0403 12.169 85.221 55.843 9074.401 9.628 248.388 2.791 0.79 505867. 0.5563
|
|
40.38 0.2153 0.4806 0.0894 0.0400 12.108 84.794 54.042 9028.874 9.580 240.378 2.715 0.79 506485. 0.5323
|
|
44.86 0.2393 0.5193 0.0862 0.0397 12.009 84.100 52.125 8955.027 9.502 231.854 2.640 0.79 507138. 0.5084
|
|
49.35 0.2632 0.5554 0.0828 0.0393 11.868 83.115 50.091 8850.135 9.390 222.804 2.567 0.79 507827. 0.4846
|
|
53.84 0.2871 0.5890 0.0793 0.0386 11.682 81.810 47.934 8711.187 9.243 213.212 2.496 0.79 508552. 0.4609
|
|
58.32 0.3111 0.6203 0.0755 0.0379 11.446 80.158 45.655 8535.309 9.056 203.072 2.426 0.79 509313. 0.4372
|
|
62.81 0.3350 0.6492 0.0715 0.0369 11.159 78.148 43.258 8321.210 8.829 192.412 2.358 0.79 510111. 0.4136
|
|
67.29 0.3589 0.6759 0.0674 0.0358 10.821 75.779 40.755 8068.993 8.561 181.279 2.291 0.79 510945. 0.3901
|
|
71.78 0.3828 0.7001 0.0631 0.0345 10.432 73.055 38.156 7778.960 8.254 169.718 2.225 0.79 511815. 0.3665
|
|
76.27 0.4068 0.7219 0.0587 0.0331 9.993 69.983 35.470 7451.877 7.907 157.771 2.159 0.79 512722. 0.3429
|
|
80.75 0.4307 0.7409 0.0541 0.0314 9.506 66.569 32.707 7088.346 7.521 145.480 2.093 0.79 513666. 0.3192
|
|
85.24 0.4546 0.7570 0.0494 0.0297 8.971 62.823 29.875 6689.460 7.098 132.883 2.026 0.79 514646. 0.2953
|
|
89.73 0.4785 0.7695 0.0446 0.0278 8.390 58.754 26.983 6256.204 6.638 120.019 1.956 0.79 515664. 0.2710
|
|
94.21 0.5025 0.7778 0.0398 0.0257 7.765 54.377 24.039 5790.086 6.143 106.927 1.883 0.80 516718. 0.2463
|
|
98.70 0.5264 0.7807 0.0348 0.0235 7.098 49.707 21.054 5292.879 5.616 93.648 1.804 0.80 517810. 0.2208
|
|
103.19 0.5503 0.7764 0.0298 0.0211 6.392 44.767 18.037 4766.854 5.058 80.229 1.716 0.80 518939. 0.1944
|
|
107.67 0.5742 0.7619 0.0248 0.0187 5.652 39.583 14.999 4214.872 4.472 66.717 1.614 0.80 520105. 0.1667
|
|
112.16 0.5982 0.7323 0.0198 0.0161 4.882 34.188 11.953 3640.390 3.863 53.166 1.489 0.80 521310. 0.1373
|
|
116.64 0.6221 0.6782 0.0147 0.0135 4.087 28.622 8.912 3047.644 3.234 39.641 1.326 0.80 522552. 0.1056
|
|
121.13 0.6460 0.5813 0.0097 0.0108 3.274 22.930 5.892 2441.609 2.591 26.210 1.095 0.80 523833. 0.0709
|
|
125.62 0.6700 0.3978 0.0048 0.0081 2.451 17.167 2.911 1827.959 1.940 12.949 0.722 0.80 525150. 0.0329
|
|
130.10 0.6939 -0.0062 0.0000 0.0054 1.620 11.342 -0.029 1207.748 1.281 -0.129 -0.011 0.80 526464. 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 0.1125 0.0447 18.533 116.813 83.967 13820.409 13.198 373.487 2.756 0.87 557743. 0.6735
|
|
4.99 0.0240 0.0593 0.1109 0.0448 18.580 117.105 82.777 13854.900 13.230 368.191 2.710 0.87 558151. 0.6576
|
|
9.98 0.0479 0.1165 0.1091 0.0449 18.607 117.274 81.475 13874.951 13.250 362.402 2.663 0.87 558591. 0.6412
|
|
14.97 0.0719 0.1717 0.1072 0.0449 18.611 117.302 80.058 13878.238 13.253 356.096 2.616 0.87 559065. 0.6244
|
|
19.96 0.0958 0.2248 0.1052 0.0448 18.590 117.168 78.517 13862.360 13.238 349.242 2.569 0.87 559573. 0.6071
|
|
24.95 0.1198 0.2758 0.1029 0.0447 18.539 116.850 76.846 13824.757 13.202 341.810 2.521 0.87 560117. 0.5895
|
|
29.94 0.1437 0.3246 0.1005 0.0445 18.456 116.327 75.039 13762.877 13.143 333.775 2.473 0.87 560697. 0.5714
|
|
34.93 0.1677 0.3713 0.0979 0.0442 18.337 115.577 73.092 13674.104 13.058 325.114 2.424 0.87 561315. 0.5528
|
|
39.92 0.1916 0.4158 0.0951 0.0438 18.179 114.577 71.000 13555.847 12.945 315.807 2.376 0.87 561972. 0.5339
|
|
44.91 0.2156 0.4580 0.0921 0.0433 17.977 113.305 68.758 13405.335 12.801 305.837 2.326 0.87 562666. 0.5145
|
|
49.90 0.2395 0.4981 0.0889 0.0427 17.728 111.736 66.365 13219.715 12.624 295.190 2.277 0.88 563401. 0.4947
|
|
54.89 0.2635 0.5360 0.0855 0.0420 17.428 109.844 63.816 12995.785 12.410 283.852 2.227 0.88 564175. 0.4745
|
|
59.88 0.2874 0.5716 0.0819 0.0412 17.071 107.594 61.106 12729.603 12.156 271.801 2.177 0.88 564989. 0.4539
|
|
64.87 0.3114 0.6049 0.0780 0.0402 16.652 104.956 58.235 12417.532 11.858 259.027 2.127 0.88 565843. 0.4329
|
|
69.86 0.3353 0.6360 0.0740 0.0390 16.169 101.913 55.207 12057.562 11.514 245.562 2.077 0.88 566738. 0.4115
|
|
74.85 0.3593 0.6648 0.0697 0.0377 15.624 98.475 52.038 11650.736 11.126 231.465 2.026 0.88 567673. 0.3898
|
|
79.84 0.3832 0.6902 0.0653 0.0362 15.033 94.754 48.739 11210.470 10.705 216.789 1.972 0.88 568649. 0.3672
|
|
84.83 0.4072 0.7122 0.0607 0.0347 14.395 90.727 45.322 10734.029 10.250 201.594 1.915 0.88 569665. 0.3439
|
|
89.82 0.4311 0.7297 0.0560 0.0331 13.720 86.473 41.800 10230.786 9.770 185.926 1.853 0.88 570721. 0.3196
|
|
94.81 0.4551 0.7426 0.0511 0.0313 13.000 81.935 38.184 9693.851 9.257 169.844 1.787 0.88 571818. 0.2945
|
|
99.80 0.4790 0.7503 0.0462 0.0295 12.233 77.100 34.488 9121.885 8.711 153.404 1.715 0.88 572956. 0.2686
|
|
104.79 0.5030 0.7517 0.0412 0.0275 11.421 71.985 30.724 8516.649 8.133 136.662 1.636 0.88 574134. 0.2419
|
|
109.78 0.5269 0.7449 0.0360 0.0255 10.572 66.635 26.904 7883.664 7.528 119.670 1.548 0.88 575353. 0.2141
|
|
114.77 0.5509 0.7275 0.0309 0.0234 9.693 61.093 23.041 7228.033 6.902 102.487 1.446 0.89 576614. 0.1851
|
|
119.76 0.5748 0.6957 0.0257 0.0212 8.791 55.409 19.150 6555.486 6.260 85.180 1.325 0.89 577915. 0.1546
|
|
124.75 0.5988 0.6440 0.0204 0.0190 7.876 49.642 15.248 5873.217 5.609 67.824 1.178 0.89 579258. 0.1226
|
|
129.74 0.6228 0.5646 0.0152 0.0168 6.958 43.853 11.354 5188.342 4.955 50.503 0.993 0.89 580643. 0.0892
|
|
134.73 0.6467 0.4450 0.0100 0.0146 6.047 38.110 7.490 4508.906 4.306 33.316 0.753 0.89 582070. 0.0550
|
|
139.72 0.6707 0.2661 0.0049 0.0124 5.153 32.481 3.680 3842.844 3.670 16.369 0.434 0.89 583537. 0.0222
|
|
144.71 0.6946 -0.0067 -0.0001 0.0103 4.271 26.919 -0.074 3184.889 3.041 -0.329 -0.011 0.89 585021. 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 0.1130 0.0555 30.633 175.521 102.055 22842.838 19.830 453.942 2.026 0.96 613468. 0.5460
|
|
5.72 0.0250 0.0502 0.1116 0.0555 30.634 175.529 100.780 22843.859 19.831 448.270 2.001 0.96 613923. 0.5358
|
|
11.45 0.0499 0.0992 0.1100 0.0554 30.580 175.219 99.353 22803.568 19.796 441.921 1.976 0.96 614418. 0.5254
|
|
17.17 0.0749 0.1469 0.1082 0.0552 30.465 174.558 97.762 22717.549 19.722 434.847 1.952 0.96 614955. 0.5147
|
|
22.89 0.0999 0.1935 0.1063 0.0549 30.283 173.517 95.997 22582.045 19.604 426.997 1.928 0.96 615535. 0.5039
|
|
28.62 0.1249 0.2390 0.1041 0.0544 30.031 172.072 94.047 22393.971 19.441 418.322 1.905 0.96 616161. 0.4927
|
|
34.34 0.1498 0.2833 0.1017 0.0538 29.704 170.201 91.901 22150.418 19.229 408.774 1.882 0.96 616832. 0.4812
|
|
40.06 0.1748 0.3265 0.0991 0.0531 29.301 167.888 89.549 21849.451 18.968 398.316 1.859 0.96 617551. 0.4692
|
|
45.78 0.1998 0.3685 0.0963 0.0522 28.819 165.127 86.987 21490.180 18.656 386.919 1.836 0.96 618317. 0.4567
|
|
51.51 0.2248 0.4093 0.0932 0.0512 28.256 161.905 84.208 21070.752 18.292 374.555 1.813 0.96 619132. 0.4436
|
|
57.23 0.2497 0.4488 0.0899 0.0500 27.611 158.207 81.205 20589.496 17.874 361.202 1.789 0.96 619995. 0.4299
|
|
62.95 0.2747 0.4870 0.0863 0.0487 26.881 154.023 77.977 20044.973 17.401 346.840 1.764 0.96 620907. 0.4156
|
|
68.68 0.2997 0.5236 0.0825 0.0472 26.063 149.338 74.516 19435.285 16.872 331.446 1.739 0.96 621868. 0.4004
|
|
74.40 0.3247 0.5585 0.0784 0.0456 25.156 144.141 70.823 18758.963 16.285 315.022 1.712 0.97 622878. 0.3844
|
|
80.12 0.3496 0.5917 0.0741 0.0438 24.162 138.442 66.915 18017.246 15.641 297.638 1.685 0.97 623937. 0.3675
|
|
85.85 0.3746 0.6229 0.0695 0.0418 23.083 132.260 62.812 17212.695 14.943 279.388 1.655 0.97 625045. 0.3499
|
|
91.57 0.3996 0.6510 0.0648 0.0398 21.953 125.787 58.531 16370.245 14.211 260.348 1.622 0.97 626201. 0.3309
|
|
97.29 0.4245 0.6728 0.0599 0.0378 20.854 119.490 54.085 15550.728 13.500 240.570 1.578 0.97 627406. 0.3094
|
|
103.02 0.4495 0.6871 0.0548 0.0358 19.788 113.382 49.494 14755.819 12.810 220.147 1.521 0.97 628658. 0.2855
|
|
108.74 0.4745 0.6862 0.0495 0.0343 18.911 108.359 44.758 14102.223 12.242 199.083 1.440 0.97 629959. 0.2569
|
|
114.46 0.4995 0.6755 0.0442 0.0327 18.037 103.351 39.921 13450.442 11.677 177.569 1.346 0.97 631308. 0.2269
|
|
120.18 0.5244 0.6539 0.0388 0.0311 17.158 98.312 35.009 12794.628 11.107 155.719 1.241 0.97 632704. 0.1958
|
|
125.91 0.5494 0.6199 0.0333 0.0295 16.275 93.253 30.049 12136.169 10.536 133.656 1.123 0.97 634150. 0.1642
|
|
131.63 0.5744 0.5712 0.0278 0.0279 15.406 88.277 25.071 11488.597 9.973 111.516 0.990 0.98 635644. 0.1322
|
|
137.35 0.5994 0.5059 0.0223 0.0264 14.560 83.429 20.113 10857.679 9.426 89.464 0.840 0.98 637187. 0.1005
|
|
143.08 0.6243 0.4225 0.0168 0.0249 13.743 78.745 15.218 10248.104 8.897 67.688 0.674 0.98 638780. 0.0701
|
|
148.80 0.6493 0.3192 0.0115 0.0235 12.962 74.271 10.427 9665.873 8.391 46.381 0.489 0.98 640426. 0.0421
|
|
154.52 0.6743 0.1948 0.0064 0.0221 12.220 70.019 5.776 9112.535 7.911 25.693 0.288 0.98 642133. 0.0184
|
|
160.25 0.6993 0.0464 0.0014 0.0208 11.489 65.833 1.248 8567.690 7.438 5.549 0.066 0.98 643948. 0.0020
|
|
165.97 0.7242
|
|
|
|
|
|
|