501 lines
89 KiB
Plaintext
501 lines
89 KiB
Plaintext
18x12WE (18x12WE.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 0.1050 0.0446 0.007 0.427 0.351 5.056 0.048 1.563 31.515 0.07 32617. 0.6089
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0.48 0.0280 0.0643 0.1038 0.0453 0.007 0.434 0.347 5.135 0.049 1.545 30.673 0.07 32642. 0.5892
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0.96 0.0561 0.1250 0.1025 0.0460 0.007 0.441 0.343 5.213 0.050 1.525 29.828 0.07 32670. 0.5693
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1.43 0.0841 0.1822 0.1010 0.0466 0.007 0.447 0.338 5.287 0.050 1.503 28.985 0.07 32701. 0.5492
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1.91 0.1122 0.2359 0.0994 0.0472 0.007 0.453 0.332 5.357 0.051 1.479 28.148 0.07 32735. 0.5291
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2.39 0.1402 0.2862 0.0976 0.0478 0.007 0.458 0.327 5.421 0.052 1.452 27.318 0.07 32772. 0.5089
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2.87 0.1682 0.3332 0.0956 0.0483 0.007 0.463 0.320 5.477 0.052 1.423 26.500 0.07 32812. 0.4886
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3.35 0.1963 0.3769 0.0935 0.0487 0.007 0.467 0.313 5.522 0.053 1.391 25.695 0.07 32855. 0.4685
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3.82 0.2243 0.4175 0.0912 0.0490 0.007 0.470 0.305 5.555 0.053 1.357 24.904 0.07 32902. 0.4483
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4.30 0.2524 0.4550 0.0886 0.0492 0.007 0.471 0.296 5.574 0.053 1.319 24.128 0.07 32952. 0.4283
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4.78 0.2804 0.4897 0.0859 0.0492 0.007 0.471 0.287 5.576 0.053 1.278 23.368 0.07 33006. 0.4083
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5.26 0.3084 0.5214 0.0829 0.0490 0.007 0.470 0.277 5.559 0.053 1.233 22.623 0.07 33063. 0.3883
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5.74 0.3365 0.5505 0.0797 0.0487 0.007 0.467 0.267 5.522 0.053 1.186 21.891 0.07 33123. 0.3684
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6.21 0.3645 0.5767 0.0762 0.0482 0.007 0.462 0.255 5.464 0.052 1.134 21.171 0.07 33188. 0.3485
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6.69 0.3926 0.6001 0.0725 0.0475 0.007 0.455 0.243 5.381 0.051 1.080 20.458 0.07 33256. 0.3285
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7.17 0.4206 0.6207 0.0686 0.0465 0.007 0.446 0.230 5.274 0.050 1.021 19.749 0.07 33327. 0.3085
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7.65 0.4487 0.6382 0.0645 0.0453 0.007 0.434 0.216 5.140 0.049 0.960 19.037 0.07 33403. 0.2882
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8.13 0.4767 0.6525 0.0601 0.0439 0.007 0.421 0.201 4.980 0.048 0.895 18.317 0.07 33482. 0.2678
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8.60 0.5047 0.6631 0.0556 0.0423 0.006 0.405 0.186 4.795 0.046 0.827 17.580 0.07 33564. 0.2470
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9.08 0.5328 0.6695 0.0508 0.0404 0.006 0.388 0.170 4.586 0.044 0.756 16.816 0.07 33651. 0.2260
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9.56 0.5608 0.6711 0.0460 0.0384 0.006 0.368 0.154 4.355 0.042 0.684 16.014 0.07 33740. 0.2047
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10.04 0.5889 0.6670 0.0410 0.0362 0.006 0.347 0.137 4.102 0.039 0.610 15.157 0.07 33834. 0.1829
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10.52 0.6169 0.6558 0.0359 0.0338 0.005 0.324 0.120 3.830 0.037 0.534 14.225 0.07 33931. 0.1607
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10.99 0.6449 0.6357 0.0308 0.0312 0.005 0.299 0.103 3.540 0.034 0.458 13.191 0.07 34032. 0.1380
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11.47 0.6730 0.6043 0.0256 0.0285 0.004 0.273 0.086 3.232 0.031 0.381 12.016 0.07 34136. 0.1146
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11.95 0.7010 0.5574 0.0204 0.0257 0.004 0.246 0.068 2.909 0.028 0.304 10.641 0.07 34244. 0.0906
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12.43 0.7291 0.4891 0.0152 0.0227 0.003 0.217 0.051 2.572 0.025 0.226 8.977 0.07 34355. 0.0660
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12.91 0.7571 0.3890 0.0101 0.0196 0.003 0.188 0.034 2.224 0.021 0.150 6.876 0.07 34470. 0.0412
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13.38 0.7851 0.2392 0.0050 0.0165 0.003 0.158 0.017 1.866 0.018 0.075 4.077 0.07 34588. 0.0172
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13.86 0.8132 0.0038 0.0001 0.0132 0.002 0.127 0.000 1.502 0.014 0.001 0.063 0.07 34710. 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 0.1054 0.0416 0.051 1.593 1.410 37.693 0.180 6.272 16.968 0.14 65232. 0.6568
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0.96 0.0282 0.0694 0.1042 0.0423 0.051 1.621 1.394 38.367 0.183 6.201 16.480 0.14 65284. 0.6343
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1.92 0.0564 0.1347 0.1028 0.0430 0.052 1.650 1.376 39.032 0.186 6.121 15.992 0.14 65341. 0.6116
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2.88 0.0846 0.1960 0.1014 0.0437 0.053 1.677 1.357 39.675 0.189 6.034 15.508 0.14 65403. 0.5888
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3.84 0.1128 0.2533 0.0998 0.0444 0.054 1.702 1.335 40.282 0.192 5.938 15.030 0.14 65471. 0.5661
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4.80 0.1409 0.3067 0.0980 0.0450 0.055 1.726 1.311 40.841 0.195 5.831 14.560 0.14 65545. 0.5434
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5.77 0.1691 0.3564 0.0960 0.0456 0.055 1.747 1.285 41.334 0.197 5.715 14.098 0.14 65626. 0.5209
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6.73 0.1973 0.4024 0.0939 0.0460 0.056 1.764 1.256 41.745 0.199 5.587 13.647 0.14 65713. 0.4986
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7.69 0.2255 0.4451 0.0915 0.0464 0.056 1.777 1.225 42.056 0.201 5.447 13.207 0.14 65807. 0.4764
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8.65 0.2537 0.4845 0.0890 0.0466 0.057 1.786 1.190 42.251 0.202 5.295 12.779 0.14 65908. 0.4545
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9.61 0.2819 0.5208 0.0862 0.0466 0.057 1.788 1.153 42.310 0.202 5.129 12.362 0.14 66016. 0.4327
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10.57 0.3101 0.5541 0.0832 0.0465 0.057 1.784 1.113 42.216 0.202 4.950 11.957 0.14 66132. 0.4112
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11.53 0.3383 0.5845 0.0799 0.0462 0.056 1.773 1.070 41.953 0.200 4.757 11.563 0.14 66254. 0.3898
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12.49 0.3664 0.6122 0.0764 0.0458 0.056 1.754 1.023 41.507 0.198 4.550 11.178 0.14 66384. 0.3685
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13.45 0.3946 0.6371 0.0727 0.0450 0.055 1.727 0.973 40.864 0.195 4.329 10.802 0.14 66521. 0.3474
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14.41 0.4228 0.6592 0.0688 0.0441 0.054 1.691 0.920 40.013 0.191 4.094 10.432 0.14 66666. 0.3262
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15.38 0.4510 0.6785 0.0646 0.0429 0.052 1.646 0.864 38.943 0.186 3.844 10.066 0.14 66818. 0.3050
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16.34 0.4792 0.6947 0.0602 0.0415 0.050 1.591 0.805 37.649 0.180 3.581 9.700 0.14 66978. 0.2837
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17.30 0.5074 0.7075 0.0556 0.0398 0.048 1.527 0.743 36.140 0.173 3.307 9.331 0.14 67144. 0.2623
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18.26 0.5356 0.7167 0.0508 0.0380 0.046 1.455 0.680 34.429 0.164 3.023 8.954 0.14 67318. 0.2406
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19.22 0.5638 0.7214 0.0459 0.0359 0.044 1.375 0.614 32.527 0.155 2.731 8.562 0.15 67500. 0.2187
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20.18 0.5919 0.7210 0.0409 0.0336 0.041 1.287 0.547 30.443 0.145 2.433 8.150 0.15 67689. 0.1965
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21.14 0.6201 0.7141 0.0358 0.0311 0.038 1.191 0.479 28.188 0.135 2.130 7.705 0.15 67885. 0.1738
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22.10 0.6483 0.6989 0.0306 0.0284 0.035 1.089 0.410 25.770 0.123 1.823 7.213 0.15 68088. 0.1505
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23.06 0.6765 0.6727 0.0254 0.0256 0.031 0.981 0.340 23.203 0.111 1.514 6.654 0.15 68298. 0.1265
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24.02 0.7047 0.6310 0.0202 0.0226 0.027 0.866 0.271 20.499 0.098 1.204 5.991 0.15 68516. 0.1016
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24.98 0.7329 0.5663 0.0151 0.0195 0.024 0.747 0.201 17.674 0.084 0.896 5.170 0.15 68741. 0.0756
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25.95 0.7611 0.4648 0.0099 0.0163 0.020 0.623 0.133 14.748 0.070 0.591 4.086 0.15 68973. 0.0486
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26.91 0.7893 0.2981 0.0049 0.0129 0.016 0.496 0.065 11.742 0.056 0.291 2.528 0.15 69212. 0.0211
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27.87 0.8174 -0.0023 0.0000 0.0096 0.012 0.367 0.000 8.680 0.041 -0.002 -0.019 0.15 69457. 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 0.1057 0.0403 0.166 3.477 3.183 123.424 0.393 14.159 11.698 0.21 97846. 0.6804
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1.44 0.0282 0.0719 0.1045 0.0411 0.169 3.543 3.147 125.770 0.400 13.999 11.350 0.21 97924. 0.6564
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2.89 0.0565 0.1393 0.1032 0.0418 0.172 3.609 3.108 128.088 0.408 13.822 11.004 0.21 98009. 0.6323
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4.33 0.0847 0.2025 0.1017 0.0426 0.175 3.672 3.063 130.335 0.415 13.626 10.661 0.21 98103. 0.6083
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5.78 0.1130 0.2614 0.1001 0.0433 0.178 3.732 3.015 132.466 0.422 13.410 10.323 0.21 98205. 0.5843
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7.22 0.1412 0.3163 0.0984 0.0439 0.180 3.787 2.961 134.431 0.428 13.171 9.991 0.21 98317. 0.5605
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8.66 0.1694 0.3672 0.0964 0.0445 0.183 3.837 2.902 136.176 0.433 12.909 9.667 0.21 98439. 0.5368
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10.11 0.1977 0.4144 0.0942 0.0450 0.185 3.878 2.838 137.644 0.438 12.621 9.350 0.21 98570. 0.5134
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11.55 0.2259 0.4580 0.0919 0.0453 0.186 3.910 2.767 138.773 0.442 12.306 9.043 0.21 98712. 0.4903
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13.00 0.2542 0.4982 0.0893 0.0456 0.187 3.930 2.689 139.501 0.444 11.963 8.744 0.21 98864. 0.4675
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14.44 0.2824 0.5353 0.0865 0.0457 0.187 3.938 2.605 139.767 0.445 11.589 8.455 0.22 99026. 0.4449
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15.89 0.3106 0.5693 0.0835 0.0456 0.187 3.931 2.515 139.509 0.444 11.185 8.175 0.22 99200. 0.4226
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17.33 0.3389 0.6005 0.0803 0.0453 0.186 3.907 2.416 138.671 0.441 10.748 7.904 0.22 99384. 0.4005
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18.77 0.3671 0.6288 0.0768 0.0448 0.184 3.865 2.311 137.199 0.437 10.280 7.641 0.22 99580. 0.3786
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20.22 0.3954 0.6545 0.0730 0.0441 0.181 3.805 2.199 135.051 0.430 9.780 7.384 0.22 99787. 0.3569
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21.66 0.4236 0.6774 0.0690 0.0432 0.177 3.724 2.079 132.187 0.421 9.247 7.134 0.22 100004. 0.3353
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23.11 0.4518 0.6976 0.0648 0.0420 0.172 3.622 1.952 128.561 0.409 8.683 6.887 0.22 100233. 0.3137
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24.55 0.4801 0.7149 0.0604 0.0406 0.167 3.498 1.818 124.159 0.395 8.088 6.642 0.22 100473. 0.2920
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25.99 0.5083 0.7290 0.0558 0.0389 0.160 3.353 1.679 119.013 0.379 7.467 6.398 0.22 100725. 0.2702
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27.44 0.5366 0.7397 0.0510 0.0370 0.152 3.188 1.534 113.162 0.360 6.824 6.150 0.22 100987. 0.2483
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28.88 0.5648 0.7463 0.0460 0.0348 0.143 3.005 1.386 106.641 0.339 6.164 5.894 0.22 101260. 0.2262
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30.33 0.5930 0.7481 0.0410 0.0325 0.133 2.803 1.234 99.483 0.317 5.490 5.627 0.22 101544. 0.2038
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31.77 0.6213 0.7439 0.0359 0.0300 0.123 2.584 1.080 91.722 0.292 4.804 5.341 0.22 101839. 0.1810
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33.21 0.6495 0.7320 0.0307 0.0272 0.112 2.349 0.924 83.392 0.265 4.111 5.027 0.22 102145. 0.1575
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34.66 0.6778 0.7095 0.0255 0.0243 0.100 2.100 0.767 74.534 0.237 3.413 4.670 0.22 102462. 0.1333
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36.10 0.7060 0.6720 0.0203 0.0213 0.087 1.837 0.610 65.194 0.208 2.715 4.246 0.22 102789. 0.1081
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37.55 0.7342 0.6114 0.0151 0.0181 0.074 1.562 0.454 55.430 0.176 2.019 3.715 0.22 103128. 0.0816
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38.99 0.7625 0.5122 0.0099 0.0148 0.061 1.277 0.299 45.308 0.144 1.331 2.996 0.22 103477. 0.0534
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40.43 0.7907 0.3396 0.0049 0.0114 0.047 0.984 0.147 34.909 0.111 0.656 1.916 0.22 103837. 0.0240
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41.88 0.8190 -0.0021 0.0000 0.0079 0.033 0.685 -0.001 24.309 0.077 -0.003 -0.011 0.22 104205. 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 0.1061 0.0397 0.386 6.088 5.682 288.098 0.688 25.272 8.945 0.29 130458. 0.6951
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1.93 0.0283 0.0733 0.1050 0.0405 0.394 6.208 5.618 293.786 0.701 24.991 8.674 0.29 130561. 0.6702
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3.85 0.0565 0.1420 0.1037 0.0413 0.402 6.327 5.548 299.412 0.715 24.678 8.405 0.29 130675. 0.6453
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5.78 0.0848 0.2063 0.1022 0.0420 0.409 6.442 5.470 304.874 0.728 24.332 8.138 0.29 130801. 0.6205
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7.71 0.1131 0.2662 0.1006 0.0427 0.416 6.552 5.384 310.063 0.740 23.949 7.876 0.29 130938. 0.5958
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9.64 0.1413 0.3219 0.0988 0.0434 0.422 6.653 5.289 314.860 0.752 23.526 7.619 0.29 131087. 0.5712
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11.56 0.1696 0.3736 0.0969 0.0440 0.428 6.743 5.185 319.133 0.762 23.061 7.369 0.29 131249. 0.5469
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13.49 0.1979 0.4214 0.0947 0.0445 0.433 6.820 5.070 322.744 0.770 22.549 7.125 0.29 131425. 0.5229
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15.42 0.2261 0.4656 0.0924 0.0449 0.437 6.879 4.944 325.546 0.777 21.989 6.888 0.29 131614. 0.4992
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17.35 0.2544 0.5064 0.0898 0.0451 0.439 6.918 4.806 327.387 0.782 21.378 6.658 0.29 131817. 0.4758
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19.27 0.2827 0.5439 0.0870 0.0452 0.440 6.933 4.656 328.118 0.783 20.712 6.437 0.29 132035. 0.4528
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21.20 0.3110 0.5784 0.0840 0.0451 0.439 6.922 4.494 327.590 0.782 19.991 6.223 0.29 132267. 0.4300
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23.13 0.3392 0.6100 0.0807 0.0449 0.437 6.881 4.319 325.664 0.777 19.212 6.016 0.29 132513. 0.4076
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25.06 0.3675 0.6388 0.0772 0.0444 0.432 6.809 4.131 322.215 0.769 18.376 5.815 0.29 132775. 0.3853
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26.98 0.3958 0.6650 0.0734 0.0437 0.425 6.701 3.930 317.133 0.757 17.482 5.621 0.29 133051. 0.3633
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28.91 0.4240 0.6884 0.0694 0.0428 0.416 6.557 3.716 310.321 0.741 16.530 5.432 0.29 133342. 0.3413
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30.84 0.4523 0.7093 0.0652 0.0416 0.405 6.375 3.489 301.673 0.720 15.520 5.246 0.29 133648. 0.3195
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32.77 0.4806 0.7273 0.0607 0.0401 0.390 6.152 3.250 291.146 0.695 14.456 5.063 0.29 133969. 0.2975
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34.69 0.5088 0.7423 0.0561 0.0384 0.374 5.892 3.000 278.815 0.666 13.345 4.881 0.29 134305. 0.2756
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36.62 0.5371 0.7541 0.0512 0.0365 0.355 5.595 2.742 264.772 0.632 12.196 4.697 0.29 134655. 0.2535
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38.55 0.5654 0.7620 0.0463 0.0343 0.334 5.264 2.476 249.101 0.595 11.015 4.509 0.29 135020. 0.2313
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40.48 0.5936 0.7654 0.0412 0.0320 0.311 4.900 2.205 231.879 0.554 9.809 4.314 0.29 135400. 0.2088
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42.40 0.6219 0.7632 0.0360 0.0294 0.286 4.505 1.930 213.184 0.509 8.583 4.105 0.29 135794. 0.1859
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44.33 0.6502 0.7536 0.0308 0.0266 0.259 4.080 1.651 193.103 0.461 7.343 3.877 0.29 136202. 0.1624
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46.26 0.6784 0.7339 0.0256 0.0237 0.230 3.629 1.370 171.733 0.410 6.095 3.619 0.29 136626. 0.1381
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48.18 0.7067 0.6997 0.0204 0.0206 0.200 3.152 1.090 149.188 0.356 4.846 3.312 0.29 137064. 0.1127
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50.11 0.7350 0.6427 0.0151 0.0173 0.168 2.654 0.810 125.607 0.300 3.603 2.925 0.29 137516. 0.0858
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52.04 0.7632 0.5461 0.0100 0.0139 0.136 2.137 0.534 101.156 0.241 2.375 2.394 0.29 137983. 0.0570
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53.97 0.7915 0.3709 0.0049 0.0105 0.102 1.607 0.263 76.031 0.182 1.169 1.568 0.29 138463. 0.0262
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55.89 0.8198 -0.0034 0.0000 0.0069 0.068 1.065 -0.002 50.413 0.120 -0.007 -0.014 0.30 138954. 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 0.1067 0.0394 0.749 9.444 8.921 558.654 1.067 39.680 7.243 0.36 163066. 0.7052
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2.41 0.0283 0.0742 0.1055 0.0402 0.764 9.635 8.823 569.982 1.089 39.245 7.021 0.36 163195. 0.6798
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4.82 0.0565 0.1437 0.1042 0.0410 0.779 9.825 8.714 581.198 1.110 38.762 6.801 0.36 163338. 0.6544
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7.23 0.0848 0.2086 0.1028 0.0418 0.794 10.009 8.594 592.101 1.131 38.226 6.583 0.36 163495. 0.6291
|
|
9.64 0.1131 0.2691 0.1012 0.0425 0.808 10.185 8.460 602.475 1.151 37.632 6.369 0.36 163666. 0.6039
|
|
12.05 0.1414 0.3254 0.0994 0.0432 0.821 10.347 8.313 612.081 1.169 36.975 6.160 0.36 163853. 0.5789
|
|
14.46 0.1696 0.3775 0.0974 0.0438 0.832 10.492 8.150 620.660 1.185 36.250 5.956 0.36 164056. 0.5542
|
|
16.87 0.1979 0.4257 0.0953 0.0443 0.842 10.615 7.971 627.934 1.199 35.453 5.757 0.36 164276. 0.5299
|
|
19.28 0.2262 0.4703 0.0930 0.0447 0.850 10.711 7.774 633.612 1.210 34.579 5.565 0.36 164513. 0.5058
|
|
21.69 0.2545 0.5114 0.0904 0.0450 0.855 10.775 7.559 637.395 1.217 33.623 5.379 0.36 164767. 0.4821
|
|
24.10 0.2827 0.5493 0.0876 0.0451 0.857 10.802 7.325 638.981 1.220 32.582 5.200 0.36 165039. 0.4587
|
|
26.51 0.3110 0.5841 0.0845 0.0450 0.856 10.786 7.071 638.076 1.219 31.453 5.027 0.36 165330. 0.4357
|
|
28.92 0.3393 0.6160 0.0813 0.0448 0.851 10.724 6.797 634.402 1.212 30.233 4.860 0.36 165639. 0.4130
|
|
31.33 0.3676 0.6452 0.0777 0.0443 0.842 10.611 6.502 627.707 1.199 28.921 4.698 0.36 165966. 0.3905
|
|
33.74 0.3958 0.6717 0.0740 0.0436 0.828 10.443 6.186 617.774 1.180 27.517 4.542 0.36 166312. 0.3683
|
|
36.14 0.4241 0.6957 0.0700 0.0426 0.811 10.217 5.850 604.407 1.154 26.023 4.390 0.36 166676. 0.3462
|
|
38.55 0.4524 0.7170 0.0657 0.0414 0.788 9.930 5.494 587.395 1.122 24.436 4.242 0.36 167059. 0.3241
|
|
40.96 0.4806 0.7356 0.0612 0.0400 0.760 9.579 5.118 566.646 1.082 22.763 4.096 0.36 167460. 0.3021
|
|
43.37 0.5089 0.7514 0.0565 0.0383 0.727 9.167 4.725 542.302 1.036 21.016 3.952 0.36 167880. 0.2800
|
|
45.78 0.5372 0.7640 0.0516 0.0363 0.690 8.698 4.318 514.544 0.983 19.208 3.807 0.36 168319. 0.2579
|
|
48.19 0.5655 0.7730 0.0466 0.0341 0.648 8.174 3.901 483.534 0.923 17.350 3.659 0.36 168775. 0.2356
|
|
50.60 0.5937 0.7777 0.0415 0.0317 0.603 7.597 3.474 449.426 0.858 15.451 3.506 0.36 169250. 0.2130
|
|
53.01 0.6220 0.7770 0.0363 0.0291 0.553 6.971 3.040 412.374 0.788 13.521 3.343 0.36 169743. 0.1900
|
|
55.42 0.6503 0.7694 0.0311 0.0263 0.500 6.298 2.601 372.547 0.712 11.569 3.167 0.36 170255. 0.1665
|
|
57.83 0.6786 0.7522 0.0258 0.0233 0.443 5.581 2.159 330.140 0.631 9.605 2.967 0.37 170784. 0.1421
|
|
60.24 0.7068 0.7209 0.0205 0.0201 0.383 4.824 1.717 285.382 0.545 7.639 2.730 0.37 171332. 0.1166
|
|
62.65 0.7351 0.6672 0.0153 0.0168 0.320 4.033 1.278 238.551 0.456 5.683 2.429 0.37 171897. 0.0895
|
|
65.06 0.7634 0.5740 0.0101 0.0134 0.255 3.212 0.843 189.980 0.363 3.749 2.012 0.37 172481. 0.0602
|
|
67.47 0.7917 0.3987 0.0050 0.0099 0.188 2.368 0.416 140.062 0.267 1.851 1.348 0.37 173082. 0.0284
|
|
69.88 0.8199 0.0006 0.0000 0.0063 0.120 1.507 0.000 89.156 0.170 0.002 0.002 0.37 173695. 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 0.1073 0.0394 1.292 13.577 12.921 963.776 1.534 57.473 6.081 0.43 195669. 0.7125
|
|
2.89 0.0283 0.0747 0.1061 0.0402 1.319 13.858 12.783 983.747 1.566 56.857 5.894 0.43 195824. 0.6869
|
|
5.79 0.0566 0.1448 0.1049 0.0410 1.346 14.137 12.628 1003.540 1.597 56.170 5.708 0.43 195996. 0.6612
|
|
8.68 0.0849 0.2102 0.1034 0.0418 1.372 14.408 12.457 1022.805 1.628 55.407 5.524 0.43 196184. 0.6355
|
|
11.57 0.1131 0.2711 0.1018 0.0425 1.396 14.667 12.266 1041.157 1.657 54.559 5.344 0.43 196390. 0.6101
|
|
14.46 0.1414 0.3276 0.1001 0.0432 1.419 14.907 12.055 1058.173 1.684 53.620 5.167 0.43 196615. 0.5848
|
|
17.36 0.1697 0.3801 0.0982 0.0438 1.439 15.121 11.821 1073.398 1.708 52.582 4.995 0.43 196859. 0.5599
|
|
20.25 0.1980 0.4286 0.0960 0.0444 1.457 15.303 11.564 1086.340 1.729 51.438 4.828 0.43 197124. 0.5352
|
|
23.14 0.2263 0.4734 0.0937 0.0448 1.470 15.446 11.282 1096.488 1.745 50.180 4.667 0.43 197408. 0.5110
|
|
26.03 0.2546 0.5148 0.0911 0.0450 1.480 15.542 10.972 1103.312 1.756 48.804 4.511 0.43 197714. 0.4870
|
|
28.93 0.2828 0.5529 0.0883 0.0452 1.484 15.584 10.634 1106.279 1.761 47.302 4.360 0.43 198042. 0.4635
|
|
31.82 0.3111 0.5880 0.0853 0.0451 1.482 15.564 10.268 1104.870 1.758 45.671 4.215 0.43 198391. 0.4403
|
|
34.71 0.3394 0.6202 0.0820 0.0449 1.473 15.476 9.871 1098.593 1.748 43.906 4.075 0.43 198762. 0.4174
|
|
37.60 0.3677 0.6497 0.0784 0.0444 1.458 15.313 9.444 1087.003 1.730 42.008 3.941 0.43 199156. 0.3948
|
|
40.50 0.3960 0.6765 0.0746 0.0437 1.435 15.069 8.987 1069.716 1.703 39.974 3.811 0.43 199572. 0.3724
|
|
43.39 0.4243 0.7008 0.0706 0.0427 1.403 14.741 8.500 1046.387 1.665 37.807 3.684 0.43 200010. 0.3501
|
|
46.28 0.4525 0.7226 0.0663 0.0415 1.363 14.322 7.982 1016.644 1.618 35.505 3.561 0.43 200470. 0.3280
|
|
49.18 0.4808 0.7417 0.0617 0.0400 1.315 13.810 7.436 980.318 1.560 33.076 3.441 0.43 200953. 0.3058
|
|
52.07 0.5091 0.7581 0.0570 0.0383 1.257 13.209 6.866 937.648 1.492 30.539 3.321 0.43 201458. 0.2837
|
|
54.96 0.5374 0.7714 0.0521 0.0363 1.192 12.523 6.275 888.947 1.415 27.912 3.202 0.43 201984. 0.2614
|
|
57.85 0.5657 0.7813 0.0471 0.0341 1.119 11.756 5.668 834.502 1.328 25.210 3.081 0.44 202533. 0.2391
|
|
60.75 0.5940 0.7871 0.0419 0.0316 1.039 10.912 5.047 774.579 1.233 22.450 2.955 0.44 203104. 0.2164
|
|
63.64 0.6222 0.7877 0.0367 0.0290 0.951 9.994 4.416 709.454 1.129 19.643 2.823 0.44 203696. 0.1934
|
|
66.53 0.6505 0.7816 0.0314 0.0261 0.857 9.008 3.778 639.422 1.018 16.804 2.680 0.44 204310. 0.1698
|
|
69.42 0.6788 0.7663 0.0260 0.0231 0.757 7.957 3.135 564.828 0.899 13.946 2.518 0.44 204946. 0.1453
|
|
72.32 0.7071 0.7373 0.0207 0.0198 0.652 6.847 2.492 486.078 0.774 11.086 2.326 0.44 205604. 0.1197
|
|
75.21 0.7354 0.6863 0.0154 0.0165 0.541 5.686 1.853 403.665 0.642 8.240 2.082 0.44 206283. 0.0924
|
|
78.10 0.7637 0.5955 0.0101 0.0130 0.427 4.482 1.220 318.181 0.506 5.427 1.739 0.44 206984. 0.0626
|
|
80.99 0.7919 0.4193 0.0050 0.0094 0.309 3.245 0.600 230.329 0.367 2.667 1.181 0.44 207706. 0.0298
|
|
83.89 0.8202 -0.0063 0.0000 0.0057 0.189 1.982 -0.005 140.722 0.224 -0.023 -0.017 0.44 208442. 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 0.1080 0.0395 2.058 18.530 17.709 1534.644 2.094 78.770 5.234 0.50 228266. 0.7180
|
|
3.37 0.0283 0.0750 0.1069 0.0403 2.101 18.921 17.524 1567.045 2.138 77.949 5.072 0.50 228448. 0.6922
|
|
6.75 0.0566 0.1453 0.1056 0.0411 2.145 19.310 17.318 1599.198 2.182 77.031 4.912 0.50 228648. 0.6663
|
|
10.12 0.0848 0.2110 0.1042 0.0419 2.187 19.688 17.088 1630.521 2.224 76.008 4.753 0.50 228868. 0.6405
|
|
13.50 0.1131 0.2721 0.1027 0.0427 2.227 20.049 16.832 1660.399 2.265 74.869 4.598 0.50 229109. 0.6149
|
|
16.87 0.1414 0.3289 0.1009 0.0434 2.264 20.384 16.547 1688.144 2.303 73.603 4.446 0.50 229372. 0.5896
|
|
20.25 0.1697 0.3815 0.0990 0.0440 2.297 20.684 16.232 1713.012 2.337 72.201 4.298 0.50 229657. 0.5645
|
|
23.62 0.1980 0.4302 0.0969 0.0446 2.326 20.940 15.884 1734.204 2.366 70.651 4.154 0.50 229966. 0.5397
|
|
27.00 0.2263 0.4752 0.0946 0.0450 2.348 21.141 15.500 1750.890 2.389 68.944 4.015 0.50 230299. 0.5153
|
|
30.37 0.2545 0.5168 0.0920 0.0453 2.363 21.278 15.079 1762.206 2.404 67.072 3.881 0.50 230656. 0.4913
|
|
33.75 0.2828 0.5551 0.0892 0.0454 2.370 21.339 14.619 1767.289 2.411 65.026 3.752 0.50 231039. 0.4676
|
|
37.12 0.3111 0.5903 0.0861 0.0454 2.367 21.315 14.119 1765.294 2.408 62.800 3.628 0.50 231447. 0.4443
|
|
40.50 0.3394 0.6228 0.0828 0.0451 2.354 21.196 13.577 1755.422 2.395 60.390 3.508 0.50 231881. 0.4214
|
|
43.87 0.3677 0.6525 0.0793 0.0447 2.329 20.973 12.993 1736.952 2.370 57.791 3.393 0.50 232341. 0.3987
|
|
47.24 0.3960 0.6797 0.0754 0.0439 2.292 20.639 12.366 1709.253 2.332 55.006 3.282 0.50 232826. 0.3762
|
|
50.62 0.4242 0.7043 0.0714 0.0430 2.242 20.186 11.698 1671.772 2.281 52.034 3.174 0.50 233338. 0.3539
|
|
53.99 0.4525 0.7265 0.0670 0.0418 2.178 19.608 10.988 1623.913 2.215 48.875 3.069 0.50 233876. 0.3316
|
|
57.37 0.4808 0.7461 0.0625 0.0402 2.099 18.901 10.238 1565.379 2.135 45.539 2.966 0.51 234440. 0.3094
|
|
60.74 0.5091 0.7630 0.0577 0.0385 2.007 18.070 9.454 1496.543 2.042 42.051 2.865 0.51 235029. 0.2872
|
|
64.12 0.5374 0.7770 0.0527 0.0365 1.901 17.121 8.642 1417.910 1.934 38.438 2.764 0.51 235645. 0.2649
|
|
67.49 0.5656 0.7877 0.0476 0.0342 1.783 16.059 7.806 1329.941 1.814 34.721 2.662 0.51 236285. 0.2425
|
|
70.87 0.5939 0.7944 0.0424 0.0317 1.654 14.889 6.952 1233.072 1.682 30.920 2.557 0.51 236952. 0.2198
|
|
74.24 0.6222 0.7962 0.0371 0.0290 1.512 13.617 6.082 1127.744 1.538 27.055 2.446 0.51 237643. 0.1967
|
|
77.62 0.6505 0.7916 0.0317 0.0261 1.360 12.249 5.203 1014.442 1.384 23.144 2.326 0.51 238360. 0.1730
|
|
80.99 0.6788 0.7781 0.0263 0.0230 1.199 10.791 4.318 893.723 1.219 19.206 2.191 0.51 239102. 0.1484
|
|
84.36 0.7071 0.7513 0.0209 0.0197 1.028 9.252 3.432 766.249 1.045 15.264 2.031 0.51 239870. 0.1227
|
|
87.74 0.7353 0.7029 0.0156 0.0163 0.849 7.641 2.550 632.823 0.863 11.341 1.827 0.51 240663. 0.0951
|
|
91.11 0.7636 0.6148 0.0102 0.0127 0.663 5.970 1.678 494.412 0.674 7.462 1.539 0.51 241480. 0.0650
|
|
94.49 0.7919 0.4387 0.0050 0.0091 0.472 4.252 0.822 352.167 0.480 3.657 1.059 0.52 242323. 0.0313
|
|
97.86 0.8202 -0.0111 -0.0001 0.0053 0.278 2.500 -0.012 207.058 0.282 -0.053 -0.026 0.52 243179. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 8000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1089 0.0397 3.092 24.362 23.318 2305.884 2.752 103.717 4.587 0.57 260857. 0.7220
|
|
3.85 0.0283 0.0751 0.1078 0.0406 3.159 24.886 23.083 2355.399 2.812 102.675 4.445 0.57 261064. 0.6962
|
|
7.71 0.0565 0.1454 0.1066 0.0414 3.225 25.405 22.821 2404.604 2.870 101.506 4.305 0.57 261293. 0.6703
|
|
11.56 0.0848 0.2111 0.1052 0.0422 3.289 25.913 22.527 2452.605 2.928 100.199 4.166 0.57 261544. 0.6446
|
|
15.41 0.1130 0.2723 0.1037 0.0430 3.350 26.397 22.198 2498.460 2.982 98.738 4.030 0.57 261819. 0.6189
|
|
19.26 0.1413 0.3291 0.1020 0.0438 3.408 26.848 21.832 2541.115 3.033 97.110 3.897 0.57 262120. 0.5936
|
|
23.12 0.1695 0.3818 0.1001 0.0444 3.459 27.252 21.425 2579.427 3.079 95.299 3.767 0.57 262446. 0.5685
|
|
26.97 0.1978 0.4306 0.0980 0.0450 3.503 27.598 20.974 2612.175 3.118 93.292 3.642 0.57 262799. 0.5437
|
|
30.82 0.2260 0.4757 0.0956 0.0454 3.538 27.872 20.476 2638.079 3.149 91.077 3.520 0.57 263179. 0.5193
|
|
34.68 0.2543 0.5174 0.0931 0.0457 3.562 28.060 19.928 2655.827 3.170 88.640 3.403 0.57 263588. 0.4953
|
|
38.53 0.2825 0.5558 0.0903 0.0459 3.573 28.147 19.328 2664.095 3.180 85.971 3.291 0.57 264026. 0.4716
|
|
42.38 0.3108 0.5913 0.0872 0.0458 3.569 28.121 18.674 2661.598 3.177 83.061 3.182 0.57 264493. 0.4483
|
|
46.23 0.3390 0.6239 0.0839 0.0456 3.550 27.967 17.964 2647.105 3.160 79.903 3.078 0.57 264989. 0.4253
|
|
50.09 0.3673 0.6539 0.0803 0.0451 3.513 27.676 17.198 2619.514 3.127 76.495 2.978 0.58 265515. 0.4025
|
|
53.94 0.3956 0.6813 0.0765 0.0444 3.457 27.236 16.375 2577.864 3.077 72.836 2.881 0.58 266070. 0.3801
|
|
57.79 0.4238 0.7063 0.0724 0.0434 3.381 26.638 15.496 2521.315 3.010 68.927 2.788 0.58 266655. 0.3577
|
|
61.65 0.4521 0.7288 0.0680 0.0422 3.284 25.874 14.561 2448.978 2.923 64.768 2.697 0.58 267270. 0.3355
|
|
65.50 0.4803 0.7489 0.0634 0.0407 3.165 24.938 13.573 2360.350 2.817 60.371 2.608 0.58 267914. 0.3132
|
|
69.35 0.5086 0.7664 0.0586 0.0389 3.025 23.835 12.538 2255.966 2.693 55.768 2.521 0.58 268587. 0.2910
|
|
73.20 0.5368 0.7811 0.0535 0.0368 2.865 22.574 11.465 2136.593 2.550 50.996 2.434 0.58 269290. 0.2686
|
|
77.06 0.5651 0.7926 0.0484 0.0345 2.686 21.162 10.360 2002.941 2.391 46.083 2.346 0.58 270022. 0.2462
|
|
80.91 0.5933 0.8002 0.0431 0.0320 2.489 19.606 9.230 1855.675 2.215 41.056 2.256 0.58 270783. 0.2234
|
|
84.76 0.6216 0.8032 0.0377 0.0292 2.274 17.913 8.080 1695.473 2.024 35.940 2.162 0.58 271572. 0.2003
|
|
88.62 0.6498 0.8001 0.0323 0.0262 2.042 16.092 6.916 1523.066 1.818 30.761 2.059 0.58 272391. 0.1766
|
|
92.47 0.6781 0.7884 0.0268 0.0231 1.796 14.150 5.743 1339.306 1.599 25.545 1.945 0.58 273238. 0.1519
|
|
96.32 0.7064 0.7640 0.0213 0.0197 1.536 12.099 4.568 1145.205 1.367 20.320 1.809 0.59 274114. 0.1261
|
|
100.17 0.7346 0.7187 0.0159 0.0162 1.263 9.952 3.399 941.983 1.124 15.118 1.637 0.59 275019. 0.0984
|
|
104.03 0.7629 0.6344 0.0105 0.0126 0.980 7.725 2.242 731.122 0.873 9.973 1.391 0.59 275952. 0.0679
|
|
107.88 0.7911 0.4617 0.0052 0.0089 0.690 5.435 1.107 514.391 0.614 4.925 0.976 0.59 276913. 0.0335
|
|
111.73 0.8194 0.0003 0.0000 0.0051 0.393 3.099 0.000 293.312 0.350 0.002 0.001 0.59 277891. 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 0.0401 4.448 31.151 29.787 3317.031 3.519 132.495 4.073 0.64 293438. 0.7247
|
|
4.33 0.0282 0.0750 0.1089 0.0410 4.545 31.832 29.502 3389.516 3.596 131.226 3.948 0.64 293671. 0.6990
|
|
8.66 0.0565 0.1452 0.1077 0.0419 4.642 32.510 29.181 3461.681 3.673 129.796 3.823 0.64 293928. 0.6733
|
|
13.00 0.0847 0.2108 0.1064 0.0427 4.737 33.172 28.819 3532.211 3.748 128.189 3.701 0.64 294211. 0.6476
|
|
17.33 0.1130 0.2720 0.1049 0.0435 4.827 33.806 28.414 3599.703 3.819 126.384 3.580 0.64 294521. 0.6221
|
|
21.66 0.1412 0.3288 0.1032 0.0443 4.912 34.397 27.959 3662.606 3.886 124.363 3.462 0.64 294859. 0.5968
|
|
25.99 0.1694 0.3815 0.1013 0.0450 4.988 34.929 27.452 3719.230 3.946 122.105 3.348 0.64 295226. 0.5718
|
|
30.32 0.1977 0.4303 0.0992 0.0456 5.053 35.385 26.887 3767.770 3.998 119.594 3.237 0.64 295624. 0.5471
|
|
34.66 0.2259 0.4755 0.0969 0.0460 5.104 35.747 26.261 3806.350 4.039 116.810 3.129 0.64 296053. 0.5228
|
|
38.99 0.2542 0.5172 0.0944 0.0464 5.140 35.997 25.571 3833.032 4.067 113.738 3.026 0.64 296514. 0.4988
|
|
43.32 0.2824 0.5557 0.0916 0.0465 5.157 36.118 24.812 3845.878 4.081 110.364 2.926 0.65 297007. 0.4752
|
|
47.65 0.3106 0.5913 0.0885 0.0465 5.154 36.091 23.983 3842.993 4.078 106.675 2.831 0.65 297533. 0.4519
|
|
51.99 0.3389 0.6241 0.0852 0.0462 5.126 35.899 23.081 3822.585 4.056 102.664 2.739 0.65 298092. 0.4289
|
|
56.32 0.3671 0.6544 0.0816 0.0458 5.073 35.528 22.105 3783.036 4.014 98.324 2.650 0.65 298685. 0.4062
|
|
60.65 0.3953 0.6821 0.0777 0.0450 4.993 34.964 21.056 3722.937 3.950 93.657 2.565 0.65 299310. 0.3837
|
|
64.98 0.4236 0.7074 0.0736 0.0440 4.883 34.195 19.933 3641.068 3.863 88.663 2.483 0.65 299970. 0.3614
|
|
69.31 0.4518 0.7303 0.0691 0.0428 4.742 33.209 18.737 3536.167 3.752 83.343 2.403 0.65 300662. 0.3391
|
|
73.65 0.4801 0.7508 0.0645 0.0412 4.569 32.001 17.471 3407.443 3.615 77.710 2.326 0.65 301387. 0.3169
|
|
77.98 0.5083 0.7689 0.0596 0.0394 4.366 30.575 16.144 3255.628 3.454 71.807 2.249 0.65 302146. 0.2946
|
|
82.31 0.5365 0.7842 0.0545 0.0373 4.133 28.943 14.766 3081.848 3.270 65.679 2.173 0.65 302937. 0.2722
|
|
86.64 0.5648 0.7964 0.0493 0.0349 3.872 27.114 13.346 2887.154 3.063 59.365 2.097 0.65 303761. 0.2497
|
|
90.97 0.5930 0.8050 0.0439 0.0323 3.584 25.099 11.893 2672.520 2.836 52.899 2.018 0.65 304617. 0.2269
|
|
95.31 0.6213 0.8091 0.0384 0.0295 3.271 22.905 10.412 2438.940 2.588 46.315 1.936 0.66 305505. 0.2037
|
|
99.64 0.6495 0.8072 0.0329 0.0265 2.933 20.544 8.913 2187.494 2.321 39.644 1.848 0.66 306426. 0.1799
|
|
103.97 0.6777 0.7972 0.0273 0.0232 2.574 18.026 7.402 1919.424 2.037 32.922 1.749 0.66 307379. 0.1551
|
|
108.30 0.7060 0.7748 0.0217 0.0198 2.194 15.366 5.887 1636.209 1.736 26.186 1.632 0.66 308364. 0.1291
|
|
112.64 0.7342 0.7320 0.0162 0.0162 1.796 12.581 4.378 1339.643 1.421 19.475 1.482 0.66 309381. 0.1011
|
|
116.97 0.7625 0.6505 0.0107 0.0125 1.384 9.691 2.886 1031.906 1.095 12.837 1.269 0.66 310430. 0.0702
|
|
121.30 0.7907 0.4789 0.0052 0.0087 0.960 6.721 1.421 715.625 0.759 6.321 0.901 0.66 311511. 0.0350
|
|
125.63 0.8189 -0.0050 0.0000 0.0048 0.527 3.691 -0.008 393.056 0.417 -0.035 -0.009 0.66 312608. 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 0.1111 0.0409 6.223 39.224 37.165 4640.678 4.432 165.309 3.632 0.71 326008. 0.7219
|
|
4.81 0.0282 0.0743 0.1101 0.0418 6.355 40.056 36.831 4739.123 4.526 163.826 3.525 0.71 326267. 0.6974
|
|
9.62 0.0564 0.1441 0.1090 0.0427 6.487 40.888 36.453 4837.547 4.620 162.144 3.418 0.71 326552. 0.6727
|
|
14.43 0.0846 0.2094 0.1077 0.0435 6.617 41.705 36.025 4934.165 4.712 160.241 3.312 0.71 326866. 0.6479
|
|
19.23 0.1128 0.2704 0.1062 0.0443 6.741 42.490 35.542 5027.084 4.801 158.090 3.207 0.71 327211. 0.6232
|
|
24.04 0.1411 0.3272 0.1046 0.0451 6.858 43.226 34.997 5114.134 4.884 155.666 3.104 0.71 327586. 0.5986
|
|
28.85 0.1693 0.3799 0.1028 0.0458 6.964 43.892 34.385 5192.948 4.959 152.943 3.003 0.72 327995. 0.5741
|
|
33.66 0.1975 0.4287 0.1007 0.0464 7.055 44.467 33.700 5260.978 5.024 149.896 2.905 0.72 328437. 0.5498
|
|
38.47 0.2257 0.4740 0.0985 0.0469 7.128 44.928 32.936 5315.516 5.076 146.501 2.810 0.72 328914. 0.5258
|
|
43.28 0.2539 0.5158 0.0959 0.0472 7.180 45.251 32.090 5353.757 5.112 142.738 2.719 0.72 329427. 0.5020
|
|
48.09 0.2821 0.5545 0.0931 0.0474 7.205 45.413 31.157 5372.851 5.131 138.588 2.630 0.72 329976. 0.4786
|
|
52.90 0.3103 0.5902 0.0901 0.0474 7.201 45.388 30.134 5369.974 5.128 134.034 2.545 0.72 330561. 0.4554
|
|
57.70 0.3385 0.6232 0.0867 0.0471 7.164 45.156 29.017 5342.441 5.102 129.067 2.464 0.72 331183. 0.4326
|
|
62.51 0.3667 0.6536 0.0831 0.0466 7.091 44.694 27.806 5287.856 5.050 123.679 2.385 0.72 331842. 0.4100
|
|
67.32 0.3950 0.6816 0.0792 0.0459 6.979 43.987 26.499 5204.212 4.970 117.870 2.310 0.72 332538. 0.3876
|
|
72.13 0.4232 0.7073 0.0750 0.0449 6.826 43.020 25.099 5089.806 4.860 111.642 2.237 0.72 333272. 0.3653
|
|
76.94 0.4514 0.7306 0.0706 0.0436 6.629 41.779 23.605 4942.907 4.720 104.997 2.166 0.72 334042. 0.3431
|
|
81.75 0.4796 0.7516 0.0658 0.0420 6.386 40.252 22.021 4762.311 4.548 97.948 2.097 0.72 334848. 0.3208
|
|
86.56 0.5078 0.7702 0.0609 0.0401 6.100 38.449 20.357 4548.964 4.344 90.549 2.030 0.72 335692. 0.2985
|
|
91.36 0.5360 0.7862 0.0557 0.0380 5.772 36.382 18.628 4304.469 4.110 82.856 1.963 0.72 336571. 0.2762
|
|
96.17 0.5642 0.7992 0.0503 0.0355 5.405 34.065 16.844 4030.333 3.849 74.921 1.896 0.73 337486. 0.2536
|
|
100.98 0.5924 0.8087 0.0449 0.0329 4.999 31.510 15.015 3727.956 3.560 66.786 1.827 0.73 338437. 0.2308
|
|
105.79 0.6206 0.8139 0.0393 0.0300 4.558 28.727 13.151 3398.788 3.246 58.494 1.755 0.73 339424. 0.2075
|
|
110.60 0.6488 0.8134 0.0337 0.0268 4.083 25.732 11.261 3044.445 2.907 50.087 1.678 0.73 340447. 0.1835
|
|
115.41 0.6771 0.8049 0.0280 0.0235 3.576 22.541 9.354 2666.836 2.547 41.608 1.591 0.73 341504. 0.1586
|
|
120.22 0.7053 0.7843 0.0222 0.0200 3.042 19.172 7.442 2268.283 2.166 33.103 1.488 0.73 342598. 0.1323
|
|
125.02 0.7335 0.7433 0.0165 0.0163 2.483 15.651 5.536 1851.667 1.768 24.625 1.356 0.73 343726. 0.1040
|
|
129.83 0.7617 0.6631 0.0109 0.0125 1.905 12.007 3.649 1420.561 1.357 16.231 1.165 0.73 344890. 0.0725
|
|
134.64 0.7899 0.4908 0.0054 0.0086 1.313 8.277 1.795 979.304 0.935 7.985 0.831 0.74 346089. 0.0363
|
|
139.45 0.8181 -0.0075 0.0000 0.0047 0.713 4.494 -0.014 531.723 0.508 -0.064 -0.012 0.74 347306. 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 0.1124 0.0434 8.778 50.299 45.484 6546.083 5.683 202.314 3.152 0.79 358565. 0.6929
|
|
5.28 0.0282 0.0711 0.1114 0.0442 8.937 51.210 45.112 6664.672 5.786 200.656 3.070 0.79 358848. 0.6722
|
|
10.56 0.0563 0.1383 0.1104 0.0449 9.095 52.115 44.686 6782.448 5.888 198.762 2.988 0.79 359161. 0.6512
|
|
15.84 0.0845 0.2018 0.1092 0.0457 9.249 52.997 44.200 6897.125 5.988 196.600 2.907 0.79 359506. 0.6299
|
|
21.12 0.1126 0.2616 0.1078 0.0464 9.396 53.835 43.646 7006.256 6.082 194.136 2.826 0.79 359884. 0.6085
|
|
26.40 0.1408 0.3177 0.1063 0.0471 9.531 54.610 43.016 7107.110 6.170 191.336 2.745 0.79 360296. 0.5869
|
|
31.68 0.1690 0.3703 0.1045 0.0477 9.651 55.299 42.303 7196.718 6.248 188.164 2.666 0.79 360745. 0.5653
|
|
36.96 0.1971 0.4194 0.1025 0.0482 9.752 55.876 41.499 7271.896 6.313 184.586 2.588 0.79 361232. 0.5435
|
|
42.24 0.2253 0.4652 0.1003 0.0486 9.829 56.318 40.596 7329.378 6.363 180.572 2.512 0.79 361757. 0.5218
|
|
47.52 0.2534 0.5079 0.0978 0.0488 9.878 56.597 39.589 7365.763 6.394 176.093 2.438 0.79 362321. 0.5000
|
|
52.80 0.2816 0.5475 0.0950 0.0489 9.893 56.688 38.472 7377.570 6.405 171.124 2.365 0.79 362925. 0.4782
|
|
58.08 0.3098 0.5842 0.0920 0.0488 9.872 56.563 37.240 7361.309 6.390 165.644 2.295 0.79 363569. 0.4565
|
|
63.36 0.3379 0.6182 0.0887 0.0485 9.808 56.196 35.890 7313.580 6.349 159.638 2.226 0.79 364254. 0.4347
|
|
68.64 0.3661 0.6496 0.0850 0.0479 9.697 55.563 34.420 7231.173 6.278 153.098 2.159 0.79 364980. 0.4129
|
|
73.92 0.3942 0.6785 0.0811 0.0471 9.536 54.641 32.829 7111.184 6.173 146.021 2.094 0.79 365746. 0.3911
|
|
79.20 0.4224 0.7050 0.0769 0.0461 9.321 53.410 31.118 6950.994 6.034 138.413 2.031 0.79 366553. 0.3692
|
|
84.48 0.4506 0.7291 0.0724 0.0447 9.049 51.850 29.289 6747.926 5.858 130.276 1.969 0.79 367400. 0.3473
|
|
89.76 0.4787 0.7508 0.0675 0.0431 8.716 49.943 27.343 6499.767 5.643 121.622 1.908 0.79 368287. 0.3252
|
|
95.04 0.5069 0.7701 0.0625 0.0411 8.325 47.698 25.296 6207.587 5.389 112.517 1.848 0.80 369214. 0.3030
|
|
100.32 0.5350 0.7867 0.0572 0.0389 7.876 45.130 23.164 5873.367 5.099 103.032 1.789 0.80 370181. 0.2806
|
|
105.60 0.5632 0.8003 0.0518 0.0364 7.374 42.254 20.960 5499.099 4.774 93.231 1.729 0.80 371187. 0.2580
|
|
110.88 0.5913 0.8104 0.0462 0.0337 6.822 39.089 18.698 5087.112 4.416 83.168 1.667 0.80 372232. 0.2350
|
|
116.16 0.6195 0.8158 0.0405 0.0307 6.222 35.653 16.389 4639.939 4.028 72.896 1.602 0.80 373316. 0.2114
|
|
121.44 0.6477 0.8151 0.0347 0.0276 5.580 31.970 14.044 4160.635 3.612 62.467 1.531 0.80 374439. 0.1870
|
|
126.72 0.6758 0.8054 0.0288 0.0242 4.898 28.067 11.676 3652.763 3.171 51.933 1.450 0.80 375600. 0.1615
|
|
132.00 0.7040 0.7819 0.0230 0.0207 4.185 23.978 9.297 3120.625 2.709 41.352 1.351 0.80 376800. 0.1343
|
|
137.28 0.7321 0.7353 0.0171 0.0170 3.446 19.744 6.921 2569.512 2.231 30.786 1.222 0.81 378038. 0.1048
|
|
142.56 0.7603 0.6453 0.0113 0.0133 2.690 15.412 4.566 2005.710 1.741 20.308 1.032 0.81 379315. 0.0719
|
|
147.84 0.7885 0.4599 0.0056 0.0095 1.926 11.037 2.247 1436.421 1.247 9.996 0.710 0.81 380630. 0.0347
|
|
153.12 0.8166 -0.0067 0.0000 0.0058 1.164 6.669 -0.019 867.914 0.753 -0.084 -0.010 0.81 381967. 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 0.1136 0.0493 12.956 68.048 54.706 9661.065 7.688 243.334 2.568 0.86 391109. 0.6193
|
|
5.76 0.0282 0.0636 0.1127 0.0500 13.130 68.965 54.311 9791.300 7.792 241.575 2.516 0.86 391416. 0.6044
|
|
11.53 0.0564 0.1245 0.1118 0.0506 13.299 69.849 53.854 9916.735 7.891 239.542 2.463 0.86 391756. 0.5892
|
|
17.29 0.0845 0.1827 0.1107 0.0512 13.456 70.675 53.326 10034.022 7.985 237.195 2.411 0.86 392132. 0.5738
|
|
23.05 0.1127 0.2383 0.1094 0.0517 13.597 71.418 52.718 10139.470 8.069 234.488 2.358 0.86 392544. 0.5582
|
|
28.82 0.1409 0.2914 0.1080 0.0522 13.718 72.052 52.018 10229.590 8.140 231.374 2.306 0.86 392994. 0.5423
|
|
34.58 0.1691 0.3419 0.1063 0.0526 13.813 72.553 51.216 10300.690 8.197 227.808 2.255 0.86 393485. 0.5261
|
|
40.34 0.1972 0.3899 0.1044 0.0528 13.878 72.894 50.302 10349.005 8.235 223.744 2.205 0.86 394017. 0.5097
|
|
46.11 0.2254 0.4355 0.1023 0.0529 13.907 73.046 49.267 10370.712 8.253 219.138 2.155 0.86 394591. 0.4930
|
|
51.87 0.2536 0.4788 0.0998 0.0529 13.896 72.986 48.101 10362.113 8.246 213.953 2.105 0.86 395209. 0.4760
|
|
57.63 0.2818 0.5197 0.0971 0.0527 13.839 72.686 46.796 10319.471 8.212 208.151 2.057 0.86 395871. 0.4587
|
|
63.40 0.3099 0.5583 0.0941 0.0523 13.731 72.120 45.347 10239.223 8.148 201.703 2.009 0.86 396577. 0.4410
|
|
69.16 0.3381 0.5946 0.0908 0.0516 13.568 71.267 43.748 10118.005 8.052 194.589 1.961 0.86 397328. 0.4228
|
|
74.92 0.3663 0.6286 0.0872 0.0508 13.347 70.103 41.996 9952.771 7.920 186.796 1.914 0.86 398124. 0.4043
|
|
80.69 0.3945 0.6603 0.0832 0.0497 13.063 68.610 40.090 9740.782 7.751 178.322 1.867 0.86 398964. 0.3853
|
|
86.45 0.4226 0.6897 0.0790 0.0484 12.712 66.769 38.033 9479.542 7.544 169.172 1.820 0.86 399849. 0.3658
|
|
92.21 0.4508 0.7166 0.0744 0.0468 12.292 64.562 35.825 9166.133 7.294 159.351 1.773 0.87 400778. 0.3459
|
|
97.97 0.4790 0.7411 0.0695 0.0449 11.798 61.970 33.470 8798.124 7.001 148.874 1.725 0.87 401751. 0.3254
|
|
103.74 0.5072 0.7630 0.0643 0.0428 11.234 59.004 30.985 8376.988 6.666 137.821 1.678 0.87 402767. 0.3044
|
|
109.50 0.5353 0.7813 0.0589 0.0404 10.610 55.727 28.389 7911.858 6.296 126.275 1.627 0.87 403826. 0.2827
|
|
115.26 0.5635 0.7953 0.0533 0.0378 9.933 52.171 25.700 7406.980 5.894 114.315 1.574 0.87 404928. 0.2601
|
|
121.03 0.5917 0.8037 0.0476 0.0350 9.209 48.371 22.934 6867.495 5.465 102.009 1.515 0.87 406072. 0.2365
|
|
126.79 0.6199 0.8055 0.0417 0.0321 8.439 44.324 20.105 6292.859 5.008 89.427 1.449 0.87 407258. 0.2118
|
|
132.55 0.6480 0.7989 0.0358 0.0290 7.623 40.039 17.230 5684.479 4.524 76.638 1.375 0.87 408487. 0.1860
|
|
138.32 0.6762 0.7801 0.0297 0.0258 6.772 35.568 14.323 5049.685 4.018 63.707 1.286 0.88 409757. 0.1587
|
|
144.08 0.7044 0.7429 0.0237 0.0224 5.896 30.967 11.400 4396.513 3.499 50.709 1.176 0.88 411068. 0.1295
|
|
149.84 0.7326 0.6768 0.0176 0.0191 5.007 26.299 8.481 3733.743 2.971 37.725 1.030 0.88 412422. 0.0978
|
|
155.61 0.7607 0.5628 0.0116 0.0157 4.119 21.633 5.586 3071.352 2.444 24.848 0.825 0.88 413817. 0.0636
|
|
161.37 0.7889 0.3634 0.0057 0.0124 3.245 17.046 2.741 2420.062 1.926 12.190 0.514 0.88 415253. 0.0277
|
|
167.13 0.8171 -0.0070 -0.0001 0.0091 2.395 12.580 -0.038 1785.979 1.421 -0.167 -0.010 0.89 416718. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 13000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1129 0.0568 18.979 92.016 63.851 14152.506 10.396 284.010 2.046 0.93 423724. 0.5330
|
|
6.29 0.0284 0.0553 0.1123 0.0576 19.232 93.241 63.484 14341.013 10.534 282.377 2.008 0.93 424051. 0.5215
|
|
12.57 0.0567 0.1086 0.1115 0.0583 19.474 94.416 63.053 14521.750 10.667 280.458 1.969 0.93 424414. 0.5098
|
|
18.86 0.0851 0.1597 0.1106 0.0590 19.698 95.503 62.545 14688.811 10.790 278.200 1.931 0.93 424816. 0.4979
|
|
25.15 0.1135 0.2088 0.1096 0.0596 19.894 96.455 61.948 14835.315 10.897 275.543 1.894 0.93 425258. 0.4859
|
|
31.44 0.1419 0.2560 0.1083 0.0600 20.053 97.226 61.246 14953.808 10.984 272.422 1.858 0.93 425742. 0.4739
|
|
37.72 0.1702 0.3014 0.1069 0.0604 20.164 97.764 60.425 15036.633 11.045 268.769 1.823 0.93 426272. 0.4619
|
|
44.01 0.1986 0.3452 0.1052 0.0605 20.218 98.023 59.468 15076.401 11.075 264.514 1.789 0.93 426848. 0.4497
|
|
50.30 0.2270 0.3874 0.1032 0.0605 20.204 97.957 58.362 15066.354 11.067 259.594 1.757 0.93 427472. 0.4375
|
|
56.58 0.2554 0.4282 0.1010 0.0602 20.116 97.530 57.092 15000.703 11.019 253.946 1.726 0.93 428145. 0.4252
|
|
62.87 0.2837 0.4677 0.0984 0.0597 19.948 96.712 55.647 14874.880 10.927 247.518 1.697 0.93 428868. 0.4126
|
|
69.16 0.3121 0.5058 0.0955 0.0590 19.694 95.482 54.017 14685.579 10.787 240.266 1.668 0.93 429641. 0.3997
|
|
75.44 0.3405 0.5426 0.0923 0.0579 19.352 93.824 52.194 14430.634 10.600 232.157 1.640 0.93 430464. 0.3863
|
|
81.73 0.3688 0.5779 0.0887 0.0566 18.920 91.732 50.174 14108.819 10.364 223.172 1.613 0.93 431337. 0.3724
|
|
88.02 0.3972 0.6118 0.0848 0.0551 18.398 89.202 47.955 13719.706 10.078 213.306 1.585 0.94 432260. 0.3579
|
|
94.31 0.4256 0.6439 0.0806 0.0532 17.786 86.234 45.541 13263.255 9.743 202.566 1.557 0.94 433233. 0.3426
|
|
100.59 0.4540 0.6741 0.0759 0.0511 17.083 82.825 42.931 12738.854 9.357 190.959 1.529 0.94 434254. 0.3265
|
|
106.88 0.4823 0.7022 0.0710 0.0488 16.288 78.968 40.132 12145.723 8.922 178.507 1.499 0.94 435324. 0.3095
|
|
113.17 0.5107 0.7280 0.0657 0.0461 15.404 74.684 37.164 11486.802 8.438 165.306 1.467 0.94 436442. 0.2916
|
|
119.45 0.5391 0.7508 0.0602 0.0432 14.447 70.046 34.055 10773.447 7.914 151.475 1.434 0.94 437607. 0.2727
|
|
125.74 0.5674 0.7677 0.0545 0.0403 13.463 65.271 30.823 10039.038 7.374 137.099 1.393 0.94 438819. 0.2520
|
|
132.03 0.5958 0.7764 0.0486 0.0373 12.465 60.436 27.489 9295.406 6.828 122.273 1.341 0.94 440077. 0.2293
|
|
138.32 0.6242 0.7690 0.0426 0.0345 11.542 55.958 24.063 8606.564 6.322 107.034 1.268 0.95 441380. 0.2028
|
|
144.60 0.6526 0.7483 0.0364 0.0317 10.604 51.412 20.580 7907.392 5.808 91.539 1.180 0.95 442730. 0.1746
|
|
150.89 0.6809 0.7114 0.0302 0.0289 9.651 46.791 17.063 7196.759 5.286 75.897 1.075 0.95 444125. 0.1448
|
|
157.18 0.7093 0.6522 0.0239 0.0260 8.700 42.180 13.539 6487.574 4.766 60.222 0.947 0.95 445565. 0.1135
|
|
163.46 0.7377 0.5633 0.0178 0.0233 7.767 37.658 10.038 5792.002 4.255 44.648 0.786 0.95 447051. 0.0812
|
|
169.75 0.7661 0.4347 0.0117 0.0206 6.866 33.291 6.594 5120.268 3.761 29.330 0.584 0.96 448582. 0.0489
|
|
176.04 0.7944 0.2535 0.0057 0.0180 6.010 29.137 3.246 4481.425 3.292 14.437 0.328 0.96 450161. 0.0193
|
|
182.32 0.8228 0.0006 0.0000 0.0155 5.187 25.150 0.006 3868.133 2.841 0.027 0.001 0.96 451802. 0.0000
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