427 lines
76 KiB
Plaintext
427 lines
76 KiB
Plaintext
20.5x14E (205x14E.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 0.0951 0.0387 0.011 0.710 0.535 8.400 0.080 2.381 28.901 0.08 37544. 0.6052
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0.56 0.0287 0.0687 0.0941 0.0394 0.011 0.723 0.530 8.556 0.082 2.356 28.078 0.08 37572. 0.5849
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1.12 0.0575 0.1333 0.0930 0.0401 0.012 0.736 0.523 8.711 0.083 2.328 27.252 0.08 37603. 0.5643
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1.67 0.0862 0.1939 0.0918 0.0408 0.012 0.749 0.516 8.863 0.085 2.297 26.428 0.08 37637. 0.5436
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2.23 0.1149 0.2505 0.0904 0.0415 0.012 0.761 0.509 9.008 0.086 2.262 25.610 0.08 37675. 0.5228
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2.79 0.1437 0.3033 0.0888 0.0421 0.012 0.773 0.500 9.144 0.087 2.224 24.802 0.08 37717. 0.5020
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3.35 0.1724 0.3523 0.0871 0.0427 0.012 0.783 0.490 9.267 0.088 2.182 24.006 0.08 37762. 0.4812
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3.90 0.2012 0.3976 0.0853 0.0431 0.013 0.792 0.480 9.373 0.090 2.135 23.225 0.08 37812. 0.4606
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4.46 0.2299 0.4395 0.0832 0.0435 0.013 0.799 0.468 9.458 0.090 2.083 22.461 0.08 37865. 0.4400
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5.02 0.2586 0.4780 0.0810 0.0438 0.013 0.805 0.456 9.518 0.091 2.027 21.715 0.08 37923. 0.4196
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5.58 0.2874 0.5133 0.0785 0.0440 0.013 0.807 0.442 9.549 0.091 1.965 20.988 0.08 37984. 0.3993
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6.14 0.3161 0.5455 0.0758 0.0439 0.013 0.807 0.427 9.546 0.091 1.898 20.278 0.08 38051. 0.3792
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6.69 0.3448 0.5748 0.0729 0.0438 0.013 0.803 0.410 9.506 0.091 1.826 19.585 0.08 38121. 0.3592
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7.25 0.3736 0.6011 0.0698 0.0434 0.013 0.797 0.393 9.425 0.090 1.748 18.908 0.08 38196. 0.3392
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7.81 0.4023 0.6246 0.0665 0.0428 0.012 0.786 0.374 9.299 0.089 1.664 18.243 0.08 38275. 0.3193
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8.37 0.4310 0.6452 0.0629 0.0420 0.012 0.771 0.354 9.125 0.087 1.574 17.587 0.08 38359. 0.2994
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8.93 0.4598 0.6627 0.0590 0.0410 0.012 0.752 0.332 8.900 0.085 1.478 16.936 0.08 38448. 0.2794
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9.48 0.4885 0.6770 0.0550 0.0397 0.012 0.729 0.310 8.624 0.082 1.377 16.283 0.08 38541. 0.2593
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10.04 0.5172 0.6877 0.0508 0.0382 0.011 0.702 0.286 8.300 0.079 1.272 15.622 0.08 38638. 0.2391
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10.60 0.5460 0.6944 0.0464 0.0365 0.011 0.670 0.261 7.931 0.076 1.162 14.944 0.08 38740. 0.2186
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11.16 0.5747 0.6964 0.0419 0.0346 0.010 0.635 0.236 7.518 0.072 1.050 14.237 0.08 38846. 0.1980
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11.71 0.6035 0.6927 0.0373 0.0325 0.009 0.597 0.210 7.065 0.067 0.935 13.489 0.08 38956. 0.1770
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12.27 0.6322 0.6822 0.0327 0.0303 0.009 0.556 0.184 6.573 0.063 0.817 12.680 0.08 39071. 0.1556
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12.83 0.6609 0.6630 0.0279 0.0278 0.008 0.511 0.157 6.046 0.058 0.699 11.786 0.08 39190. 0.1337
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13.39 0.6897 0.6322 0.0232 0.0253 0.007 0.464 0.130 5.487 0.052 0.580 10.772 0.08 39314. 0.1113
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13.95 0.7184 0.5858 0.0184 0.0225 0.007 0.414 0.103 4.898 0.047 0.460 9.581 0.08 39442. 0.0882
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14.50 0.7471 0.5168 0.0136 0.0197 0.006 0.362 0.077 4.283 0.041 0.341 8.128 0.08 39574. 0.0645
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15.06 0.7759 0.4136 0.0089 0.0168 0.005 0.308 0.050 3.648 0.035 0.224 6.263 0.08 39710. 0.0402
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15.62 0.8046 0.2538 0.0043 0.0138 0.004 0.253 0.024 2.996 0.029 0.109 3.706 0.08 39851. 0.0166
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16.18 0.8333 -0.0099 -0.0001 0.0107 0.003 0.197 -0.001 2.334 0.022 -0.003 -0.139 0.08 39996. 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 0.0954 0.0361 0.084 2.651 2.149 62.732 0.300 9.557 15.536 0.16 75086. 0.6518
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1.12 0.0288 0.0739 0.0945 0.0368 0.086 2.707 2.126 64.043 0.306 9.459 15.060 0.16 75142. 0.6286
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2.24 0.0577 0.1432 0.0934 0.0376 0.088 2.762 2.102 65.355 0.312 9.348 14.586 0.16 75205. 0.6052
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3.36 0.0865 0.2078 0.0921 0.0383 0.089 2.816 2.074 66.645 0.318 9.225 14.115 0.16 75274. 0.5818
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4.48 0.1153 0.2679 0.0907 0.0391 0.091 2.869 2.043 67.889 0.324 9.087 13.649 0.16 75351. 0.5584
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5.60 0.1442 0.3237 0.0892 0.0397 0.093 2.919 2.009 69.059 0.330 8.934 13.192 0.16 75434. 0.5352
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6.72 0.1730 0.3753 0.0875 0.0403 0.094 2.964 1.971 70.126 0.335 8.765 12.745 0.16 75525. 0.5121
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7.84 0.2018 0.4228 0.0857 0.0409 0.095 3.003 1.928 71.059 0.339 8.578 12.309 0.16 75625. 0.4893
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8.95 0.2306 0.4666 0.0836 0.0413 0.096 3.035 1.882 71.823 0.343 8.371 11.885 0.16 75732. 0.4667
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10.07 0.2595 0.5067 0.0813 0.0416 0.097 3.059 1.831 72.385 0.346 8.145 11.474 0.16 75848. 0.4444
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11.19 0.2883 0.5435 0.0789 0.0418 0.098 3.073 1.775 72.709 0.347 7.897 11.076 0.16 75972. 0.4224
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12.31 0.3171 0.5771 0.0762 0.0419 0.098 3.075 1.715 72.761 0.347 7.628 10.690 0.16 76105. 0.4007
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13.43 0.3460 0.6076 0.0733 0.0417 0.097 3.064 1.649 72.507 0.346 7.336 10.317 0.16 76247. 0.3793
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14.55 0.3748 0.6351 0.0701 0.0414 0.096 3.039 1.579 71.915 0.343 7.021 9.956 0.16 76398. 0.3580
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15.67 0.4036 0.6599 0.0667 0.0408 0.095 2.999 1.502 70.953 0.339 6.683 9.605 0.16 76558. 0.3370
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16.79 0.4325 0.6818 0.0631 0.0400 0.093 2.941 1.421 69.591 0.332 6.321 9.262 0.16 76727. 0.3160
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17.91 0.4613 0.7008 0.0593 0.0390 0.091 2.866 1.334 67.805 0.324 5.935 8.926 0.16 76905. 0.2951
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19.03 0.4901 0.7170 0.0552 0.0377 0.088 2.772 1.243 65.595 0.313 5.528 8.594 0.16 77091. 0.2742
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20.15 0.5189 0.7299 0.0510 0.0362 0.084 2.662 1.147 62.979 0.301 5.103 8.263 0.16 77287. 0.2533
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21.27 0.5478 0.7392 0.0466 0.0345 0.080 2.535 1.048 59.977 0.286 4.663 7.928 0.17 77492. 0.2323
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22.39 0.5766 0.7443 0.0420 0.0326 0.076 2.392 0.946 56.608 0.270 4.210 7.584 0.17 77705. 0.2112
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23.51 0.6054 0.7445 0.0374 0.0304 0.071 2.235 0.842 52.891 0.253 3.747 7.224 0.17 77928. 0.1898
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24.63 0.6343 0.7385 0.0327 0.0281 0.066 2.064 0.737 48.845 0.233 3.277 6.840 0.17 78159. 0.1680
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25.75 0.6631 0.7246 0.0280 0.0256 0.060 1.880 0.630 44.492 0.212 2.801 6.420 0.17 78399. 0.1458
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26.86 0.6919 0.7000 0.0232 0.0229 0.053 1.684 0.522 39.855 0.190 2.323 5.944 0.17 78647. 0.1229
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27.98 0.7208 0.6602 0.0184 0.0201 0.047 1.478 0.415 34.964 0.167 1.845 5.381 0.17 78905. 0.0992
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29.10 0.7496 0.5973 0.0137 0.0172 0.040 1.261 0.308 29.849 0.143 1.370 4.681 0.17 79171. 0.0744
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30.22 0.7784 0.4962 0.0090 0.0141 0.033 1.038 0.203 24.552 0.117 0.902 3.745 0.17 79445. 0.0483
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31.34 0.8073 0.3246 0.0044 0.0110 0.026 0.808 0.100 19.115 0.091 0.443 2.363 0.17 79729. 0.0213
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32.46 0.8361 -0.0032 0.0000 0.0078 0.018 0.574 -0.001 13.587 0.065 -0.003 -0.023 0.17 80019. 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 0.0958 0.0351 0.276 5.797 4.853 205.764 0.655 21.587 10.698 0.24 112626. 0.6745
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1.68 0.0289 0.0763 0.0948 0.0359 0.282 5.925 4.804 210.309 0.669 21.367 10.360 0.24 112711. 0.6499
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3.36 0.0577 0.1477 0.0937 0.0366 0.288 6.054 4.748 214.865 0.684 21.121 10.024 0.24 112805. 0.6252
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5.04 0.0866 0.2142 0.0925 0.0374 0.294 6.180 4.687 219.354 0.698 20.846 9.691 0.24 112909. 0.6005
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6.72 0.1154 0.2760 0.0912 0.0381 0.300 6.302 4.617 223.693 0.712 20.539 9.363 0.24 113024. 0.5759
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8.40 0.1443 0.3331 0.0896 0.0388 0.305 6.418 4.541 227.789 0.725 20.197 9.041 0.24 113150. 0.5514
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10.08 0.1732 0.3858 0.0880 0.0395 0.311 6.523 4.455 231.541 0.737 19.817 8.727 0.24 113287. 0.5273
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11.77 0.2020 0.4344 0.0861 0.0400 0.315 6.616 4.361 234.837 0.748 19.396 8.422 0.24 113436. 0.5034
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13.45 0.2309 0.4790 0.0840 0.0405 0.319 6.693 4.256 237.563 0.756 18.932 8.127 0.24 113597. 0.4799
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15.13 0.2597 0.5200 0.0818 0.0408 0.321 6.751 4.142 239.600 0.763 18.423 7.841 0.24 113771. 0.4567
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16.81 0.2886 0.5574 0.0793 0.0411 0.323 6.785 4.017 240.826 0.767 17.865 7.565 0.24 113958. 0.4339
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18.49 0.3175 0.5916 0.0766 0.0411 0.323 6.793 3.880 241.121 0.768 17.258 7.299 0.25 114159. 0.4115
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20.17 0.3463 0.6227 0.0737 0.0410 0.322 6.772 3.732 240.367 0.765 16.600 7.042 0.25 114372. 0.3894
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21.85 0.3752 0.6509 0.0705 0.0406 0.320 6.718 3.572 238.451 0.759 15.889 6.795 0.25 114599. 0.3676
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23.53 0.4040 0.6762 0.0671 0.0401 0.315 6.628 3.400 235.266 0.749 15.124 6.555 0.25 114839. 0.3460
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25.21 0.4329 0.6989 0.0635 0.0393 0.309 6.500 3.216 230.705 0.734 14.306 6.323 0.25 115093. 0.3246
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26.89 0.4618 0.7188 0.0596 0.0383 0.301 6.330 3.020 224.677 0.715 13.433 6.097 0.25 115360. 0.3033
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28.57 0.4906 0.7359 0.0555 0.0370 0.291 6.119 2.813 217.186 0.691 12.512 5.875 0.25 115641. 0.2820
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30.25 0.5195 0.7500 0.0513 0.0355 0.279 5.868 2.597 208.286 0.663 11.550 5.655 0.25 115936. 0.2608
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31.93 0.5483 0.7608 0.0468 0.0338 0.266 5.580 2.373 198.041 0.630 10.553 5.434 0.25 116243. 0.2396
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33.62 0.5772 0.7677 0.0423 0.0318 0.250 5.255 2.142 186.515 0.594 9.529 5.209 0.25 116564. 0.2182
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35.30 0.6061 0.7701 0.0376 0.0296 0.233 4.896 1.907 173.771 0.553 8.481 4.977 0.25 116898. 0.1967
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36.98 0.6349 0.7669 0.0329 0.0273 0.214 4.504 1.667 159.876 0.509 7.417 4.731 0.25 117246. 0.1748
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38.66 0.6638 0.7563 0.0281 0.0247 0.194 4.082 1.426 144.902 0.461 6.341 4.463 0.25 117606. 0.1525
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40.34 0.6926 0.7357 0.0233 0.0220 0.173 3.633 1.183 128.934 0.410 5.260 4.160 0.25 117980. 0.1295
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42.02 0.7215 0.7007 0.0186 0.0191 0.150 3.157 0.940 112.068 0.357 4.180 3.804 0.25 118367. 0.1055
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43.70 0.7504 0.6430 0.0138 0.0161 0.127 2.660 0.699 94.420 0.301 3.108 3.356 0.25 118767. 0.0803
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45.38 0.7792 0.5462 0.0091 0.0130 0.102 2.145 0.461 76.127 0.242 2.050 2.746 0.25 119180. 0.0533
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47.06 0.8081 0.3721 0.0045 0.0098 0.077 1.616 0.228 57.348 0.183 1.014 1.804 0.25 119605. 0.0247
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48.74 0.8369 0.0049 0.0000 0.0065 0.051 1.077 0.002 38.244 0.122 0.009 0.023 0.25 120041. 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 0.0963 0.0346 0.645 10.170 8.669 481.275 1.149 38.559 8.170 0.33 150163. 0.6885
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2.24 0.0289 0.0778 0.0953 0.0354 0.660 10.402 8.582 492.287 1.175 38.174 7.907 0.33 150277. 0.6630
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4.49 0.0578 0.1504 0.0942 0.0362 0.675 10.636 8.485 503.340 1.202 37.743 7.646 0.33 150402. 0.6375
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6.73 0.0867 0.2180 0.0930 0.0370 0.690 10.866 8.377 514.249 1.228 37.259 7.388 0.33 150541. 0.6120
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8.98 0.1156 0.2807 0.0917 0.0377 0.704 11.090 8.255 524.811 1.253 36.718 7.134 0.33 150695. 0.5867
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11.22 0.1445 0.3387 0.0902 0.0385 0.717 11.301 8.119 534.803 1.277 36.114 6.886 0.33 150863. 0.5616
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13.46 0.1734 0.3921 0.0885 0.0391 0.729 11.495 7.968 543.974 1.299 35.442 6.644 0.33 151046. 0.5368
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15.71 0.2023 0.4413 0.0866 0.0397 0.740 11.665 7.801 552.060 1.318 34.697 6.409 0.33 151245. 0.5123
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17.95 0.2312 0.4865 0.0846 0.0402 0.749 11.807 7.615 558.780 1.334 33.873 6.182 0.33 151461. 0.4883
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20.19 0.2601 0.5278 0.0823 0.0406 0.756 11.914 7.412 563.845 1.346 32.967 5.962 0.33 151694. 0.4646
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22.44 0.2890 0.5657 0.0798 0.0408 0.760 11.980 7.188 566.958 1.354 31.974 5.751 0.33 151944. 0.4413
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24.68 0.3179 0.6003 0.0771 0.0408 0.761 11.999 6.945 567.828 1.356 30.891 5.548 0.33 152212. 0.4185
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26.93 0.3467 0.6318 0.0742 0.0407 0.759 11.963 6.681 566.167 1.352 29.716 5.352 0.33 152498. 0.3959
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29.17 0.3756 0.6604 0.0710 0.0404 0.753 11.869 6.395 561.699 1.341 28.445 5.164 0.33 152801. 0.3738
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31.41 0.4045 0.6862 0.0676 0.0399 0.743 11.710 6.088 554.168 1.323 27.078 4.983 0.33 153122. 0.3519
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33.66 0.4334 0.7093 0.0639 0.0391 0.729 11.480 5.758 543.306 1.297 25.612 4.807 0.33 153462. 0.3302
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35.90 0.4623 0.7298 0.0600 0.0380 0.709 11.176 5.407 528.897 1.263 24.050 4.637 0.33 153819. 0.3086
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38.14 0.4912 0.7476 0.0559 0.0367 0.685 10.796 5.036 510.938 1.220 22.399 4.470 0.33 154195. 0.2871
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40.39 0.5201 0.7625 0.0516 0.0352 0.657 10.345 4.648 489.557 1.169 20.674 4.306 0.33 154588. 0.2657
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42.63 0.5490 0.7743 0.0472 0.0334 0.623 9.824 4.246 464.904 1.110 18.887 4.143 0.33 155000. 0.2443
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44.88 0.5779 0.7824 0.0426 0.0314 0.586 9.237 3.833 437.129 1.044 17.049 3.977 0.33 155429. 0.2229
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47.12 0.6068 0.7863 0.0379 0.0292 0.545 8.587 3.411 406.386 0.970 15.170 3.807 0.33 155876. 0.2012
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49.36 0.6357 0.7849 0.0331 0.0268 0.500 7.878 2.981 372.832 0.890 13.261 3.627 0.33 156340. 0.1793
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51.61 0.6646 0.7766 0.0283 0.0242 0.451 7.114 2.548 336.646 0.804 11.332 3.433 0.33 156822. 0.1568
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53.85 0.6935 0.7588 0.0235 0.0214 0.400 6.298 2.112 298.031 0.711 9.394 3.214 0.33 157322. 0.1337
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56.10 0.7224 0.7270 0.0186 0.0185 0.345 5.435 1.677 257.225 0.614 7.457 2.956 0.33 157839. 0.1096
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58.34 0.7513 0.6729 0.0138 0.0154 0.288 4.533 1.244 214.512 0.512 5.534 2.631 0.33 158373. 0.0840
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60.58 0.7802 0.5789 0.0091 0.0122 0.228 3.597 0.818 170.229 0.406 3.639 2.180 0.34 158925. 0.0564
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62.83 0.8091 0.4017 0.0045 0.0090 0.167 2.636 0.401 124.770 0.298 1.784 1.458 0.34 159494. 0.0264
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65.07 0.8380 -0.0059 0.0000 0.0056 0.105 1.659 -0.004 78.519 0.187 -0.016 -0.021 0.34 160075. 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 0.0968 0.0344 1.255 15.815 13.625 935.564 1.787 60.603 6.605 0.41 187696. 0.6979
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2.80 0.0289 0.0786 0.0959 0.0353 1.284 16.186 13.493 957.507 1.829 60.016 6.392 0.41 187837. 0.6720
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5.61 0.0578 0.1519 0.0948 0.0361 1.314 16.559 13.344 979.563 1.871 59.355 6.179 0.41 187995. 0.6460
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8.41 0.0867 0.2201 0.0937 0.0369 1.343 16.928 13.177 1001.365 1.912 58.613 5.969 0.41 188169. 0.6202
|
|
11.22 0.1156 0.2833 0.0923 0.0377 1.371 17.285 12.990 1022.508 1.953 57.780 5.762 0.41 188360. 0.5944
|
|
14.02 0.1444 0.3418 0.0908 0.0384 1.398 17.624 12.781 1042.547 1.991 56.848 5.560 0.41 188570. 0.5690
|
|
16.82 0.1733 0.3956 0.0892 0.0391 1.423 17.935 12.547 1060.982 2.026 55.808 5.364 0.41 188800. 0.5438
|
|
19.63 0.2022 0.4452 0.0873 0.0397 1.445 18.211 12.287 1077.284 2.057 54.652 5.173 0.41 189049. 0.5190
|
|
22.43 0.2311 0.4906 0.0853 0.0402 1.463 18.441 11.999 1090.892 2.083 53.371 4.989 0.41 189319. 0.4946
|
|
25.24 0.2600 0.5323 0.0830 0.0406 1.477 18.616 11.682 1101.226 2.103 51.959 4.811 0.41 189611. 0.4707
|
|
28.04 0.2889 0.5705 0.0805 0.0408 1.485 18.725 11.333 1107.700 2.116 50.410 4.641 0.41 189924. 0.4472
|
|
30.85 0.3178 0.6053 0.0778 0.0409 1.488 18.759 10.952 1109.723 2.119 48.716 4.477 0.41 190259. 0.4240
|
|
33.65 0.3467 0.6371 0.0749 0.0408 1.484 18.709 10.539 1106.722 2.114 46.875 4.319 0.41 190616. 0.4013
|
|
36.45 0.3756 0.6661 0.0717 0.0404 1.473 18.564 10.091 1098.151 2.097 44.883 4.168 0.41 190996. 0.3789
|
|
39.26 0.4045 0.6922 0.0683 0.0399 1.453 18.316 9.608 1083.491 2.069 42.737 4.022 0.41 191398. 0.3569
|
|
42.06 0.4333 0.7158 0.0646 0.0391 1.424 17.956 9.091 1062.217 2.029 40.435 3.882 0.41 191822. 0.3350
|
|
44.87 0.4622 0.7367 0.0607 0.0381 1.386 17.477 8.538 1033.883 1.975 37.977 3.746 0.41 192269. 0.3133
|
|
47.67 0.4911 0.7551 0.0565 0.0368 1.339 16.879 7.954 998.465 1.907 35.379 3.613 0.41 192739. 0.2917
|
|
50.47 0.5200 0.7707 0.0522 0.0352 1.282 16.164 7.343 956.204 1.826 32.662 3.483 0.41 193231. 0.2702
|
|
53.28 0.5489 0.7834 0.0477 0.0334 1.217 15.339 6.710 907.397 1.733 29.845 3.354 0.41 193746. 0.2487
|
|
56.08 0.5778 0.7926 0.0431 0.0314 1.143 14.408 6.058 852.340 1.628 26.946 3.224 0.41 194282. 0.2271
|
|
58.89 0.6067 0.7978 0.0383 0.0291 1.061 13.377 5.392 791.331 1.511 23.982 3.090 0.41 194841. 0.2054
|
|
61.69 0.6356 0.7980 0.0335 0.0267 0.972 12.251 4.714 724.690 1.384 20.969 2.951 0.41 195421. 0.1834
|
|
64.50 0.6645 0.7917 0.0286 0.0240 0.875 11.035 4.030 652.767 1.247 17.924 2.800 0.42 196024. 0.1609
|
|
67.30 0.6933 0.7763 0.0237 0.0212 0.772 9.736 3.341 575.969 1.100 14.863 2.631 0.42 196648. 0.1377
|
|
70.10 0.7222 0.7477 0.0189 0.0182 0.664 8.364 2.654 494.772 0.945 11.804 2.433 0.42 197294. 0.1134
|
|
72.91 0.7511 0.6973 0.0140 0.0151 0.549 6.927 1.971 409.747 0.783 8.767 2.182 0.42 197962. 0.0877
|
|
75.71 0.7800 0.6076 0.0092 0.0118 0.431 5.436 1.298 321.571 0.614 5.772 1.830 0.42 198652. 0.0597
|
|
78.52 0.8089 0.4320 0.0045 0.0085 0.310 3.906 0.639 231.038 0.441 2.844 1.255 0.42 199363. 0.0287
|
|
81.32 0.8378 0.0001 0.0000 0.0051 0.186 2.348 0.000 138.917 0.265 0.000 0.000 0.42 200089. 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 0.0975 0.0345 2.171 22.806 19.760 1618.912 2.577 87.894 5.536 0.49 225223. 0.7044
|
|
3.36 0.0289 0.0790 0.0966 0.0353 2.223 23.352 19.576 1657.673 2.638 87.074 5.356 0.49 225392. 0.6783
|
|
6.73 0.0578 0.1527 0.0956 0.0362 2.275 23.901 19.368 1696.697 2.700 86.148 5.177 0.49 225581. 0.6522
|
|
10.09 0.0867 0.2213 0.0944 0.0370 2.327 24.446 19.133 1735.330 2.762 85.104 5.001 0.49 225790. 0.6261
|
|
13.46 0.1156 0.2848 0.0931 0.0378 2.377 24.974 18.869 1772.863 2.822 83.928 4.827 0.49 226020. 0.6002
|
|
16.82 0.1444 0.3435 0.0917 0.0385 2.425 25.476 18.572 1808.499 2.878 82.607 4.658 0.49 226272. 0.5745
|
|
20.19 0.1733 0.3976 0.0900 0.0392 2.469 25.939 18.239 1841.351 2.931 81.129 4.493 0.49 226548. 0.5492
|
|
23.55 0.2022 0.4474 0.0882 0.0399 2.508 26.350 17.869 1870.481 2.977 79.479 4.333 0.49 226848. 0.5242
|
|
26.92 0.2311 0.4931 0.0862 0.0404 2.541 26.693 17.457 1894.886 3.016 77.647 4.179 0.49 227173. 0.4997
|
|
30.28 0.2600 0.5350 0.0839 0.0408 2.566 26.956 17.001 1913.542 3.045 75.622 4.030 0.49 227523. 0.4756
|
|
33.65 0.2889 0.5734 0.0814 0.0410 2.582 27.123 16.500 1925.399 3.064 73.393 3.887 0.49 227899. 0.4519
|
|
37.01 0.3178 0.6085 0.0787 0.0411 2.587 27.180 15.952 1929.416 3.071 70.953 3.750 0.49 228302. 0.4287
|
|
40.38 0.3467 0.6405 0.0758 0.0410 2.581 27.112 15.354 1924.573 3.063 68.294 3.618 0.49 228731. 0.4058
|
|
43.74 0.3755 0.6697 0.0726 0.0407 2.561 26.905 14.706 1909.900 3.040 65.411 3.492 0.49 229187. 0.3833
|
|
47.11 0.4044 0.6962 0.0691 0.0402 2.527 26.547 14.007 1884.481 2.999 62.302 3.371 0.49 229670. 0.3611
|
|
50.47 0.4333 0.7201 0.0654 0.0394 2.477 26.024 13.256 1847.399 2.940 58.963 3.255 0.49 230181. 0.3392
|
|
53.84 0.4622 0.7415 0.0615 0.0383 2.411 25.326 12.454 1797.847 2.861 55.393 3.142 0.49 230718. 0.3174
|
|
57.20 0.4911 0.7604 0.0573 0.0370 2.328 24.452 11.604 1735.743 2.763 51.616 3.032 0.49 231282. 0.2957
|
|
60.57 0.5200 0.7766 0.0529 0.0354 2.228 23.406 10.715 1661.504 2.644 47.660 2.925 0.49 231873. 0.2741
|
|
63.93 0.5489 0.7900 0.0483 0.0336 2.113 22.196 9.792 1575.646 2.508 43.556 2.819 0.50 232491. 0.2525
|
|
67.30 0.5778 0.8001 0.0436 0.0315 1.983 20.830 8.842 1478.693 2.353 39.329 2.712 0.50 233136. 0.2308
|
|
70.66 0.6066 0.8064 0.0388 0.0292 1.839 19.316 7.870 1371.173 2.182 35.005 2.603 0.50 233806. 0.2090
|
|
74.02 0.6355 0.8079 0.0340 0.0267 1.681 17.660 6.881 1253.646 1.995 30.608 2.490 0.50 234503. 0.1869
|
|
77.39 0.6644 0.8033 0.0290 0.0240 1.511 15.872 5.882 1126.738 1.793 26.161 2.368 0.50 235227. 0.1644
|
|
80.75 0.6933 0.7900 0.0241 0.0211 1.329 13.963 4.876 991.167 1.577 21.690 2.232 0.50 235976. 0.1410
|
|
84.12 0.7222 0.7639 0.0191 0.0181 1.137 11.943 3.872 847.782 1.349 17.221 2.071 0.50 236752. 0.1167
|
|
87.48 0.7511 0.7166 0.0142 0.0149 0.935 9.827 2.874 697.599 1.110 12.783 1.869 0.50 237553. 0.0907
|
|
90.85 0.7800 0.6301 0.0093 0.0115 0.727 7.633 1.890 541.827 0.862 8.407 1.582 0.50 238381. 0.0623
|
|
94.21 0.8089 0.4551 0.0046 0.0081 0.512 5.380 0.928 381.892 0.608 4.127 1.102 0.50 239234. 0.0304
|
|
97.58 0.8377 -0.0057 0.0000 0.0047 0.294 3.087 -0.006 219.139 0.349 -0.029 -0.013 0.50 240104. 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 0.0984 0.0347 3.470 31.241 27.125 2587.362 3.530 120.651 4.755 0.57 262742. 0.7088
|
|
3.92 0.0289 0.0791 0.0975 0.0356 3.554 32.003 26.884 2650.454 3.616 119.582 4.601 0.57 262940. 0.6828
|
|
7.85 0.0577 0.1530 0.0965 0.0364 3.640 32.772 26.612 2714.097 3.703 118.369 4.447 0.57 263160. 0.6567
|
|
11.77 0.0866 0.2216 0.0954 0.0373 3.724 33.534 26.302 2777.229 3.789 116.993 4.296 0.57 263403. 0.6306
|
|
15.69 0.1155 0.2853 0.0941 0.0381 3.807 34.276 25.953 2838.692 3.873 115.437 4.147 0.57 263672. 0.6047
|
|
19.62 0.1444 0.3441 0.0927 0.0389 3.885 34.982 25.558 2897.172 3.952 113.681 4.001 0.57 263966. 0.5790
|
|
23.54 0.1732 0.3983 0.0911 0.0396 3.958 35.635 25.114 2951.222 4.026 111.706 3.860 0.57 264288. 0.5536
|
|
27.46 0.2021 0.4482 0.0893 0.0402 4.022 36.215 24.616 2999.286 4.092 109.493 3.723 0.57 264638. 0.5287
|
|
31.39 0.2310 0.4940 0.0872 0.0408 4.076 36.704 24.062 3039.727 4.147 107.026 3.590 0.57 265017. 0.5041
|
|
35.31 0.2598 0.5361 0.0850 0.0412 4.118 37.079 23.446 3070.849 4.189 104.288 3.463 0.57 265426. 0.4800
|
|
39.23 0.2887 0.5746 0.0826 0.0415 4.145 37.322 22.766 3090.947 4.217 101.265 3.341 0.57 265866. 0.4562
|
|
43.16 0.3176 0.6099 0.0798 0.0416 4.155 37.411 22.020 3098.304 4.227 97.945 3.224 0.57 266336. 0.4330
|
|
47.08 0.3464 0.6421 0.0769 0.0415 4.145 37.326 21.205 3091.254 4.217 94.318 3.111 0.57 266837. 0.4101
|
|
51.00 0.3753 0.6716 0.0737 0.0412 4.115 37.048 20.319 3068.216 4.186 90.378 3.004 0.57 267370. 0.3875
|
|
54.93 0.4042 0.6984 0.0702 0.0406 4.060 36.558 19.362 3027.698 4.130 86.120 2.900 0.57 267934. 0.3653
|
|
58.85 0.4331 0.7227 0.0665 0.0398 3.980 35.840 18.332 2968.224 4.049 81.539 2.801 0.57 268530. 0.3433
|
|
62.77 0.4619 0.7445 0.0625 0.0388 3.873 34.877 17.229 2888.451 3.940 76.634 2.705 0.58 269158. 0.3214
|
|
66.70 0.4908 0.7639 0.0582 0.0374 3.739 33.666 16.060 2788.175 3.804 71.434 2.613 0.58 269816. 0.2997
|
|
70.62 0.5197 0.7807 0.0538 0.0358 3.578 32.216 14.834 2668.053 3.640 65.982 2.522 0.58 270506. 0.2780
|
|
74.54 0.5485 0.7948 0.0492 0.0339 3.391 30.536 13.561 2528.919 3.450 60.319 2.432 0.58 271227. 0.2564
|
|
78.47 0.5774 0.8058 0.0444 0.0318 3.180 28.637 12.248 2371.628 3.235 54.481 2.342 0.58 271979. 0.2347
|
|
82.39 0.6063 0.8131 0.0395 0.0295 2.946 26.529 10.904 2197.045 2.997 48.503 2.251 0.58 272761. 0.2128
|
|
86.31 0.6352 0.8159 0.0346 0.0269 2.690 24.223 9.537 2006.090 2.737 42.419 2.156 0.58 273575. 0.1906
|
|
90.23 0.6640 0.8128 0.0296 0.0242 2.414 21.732 8.153 1799.776 2.455 36.263 2.055 0.58 274418. 0.1679
|
|
94.16 0.6929 0.8014 0.0245 0.0212 2.118 19.069 6.760 1579.281 2.154 30.070 1.942 0.58 275292. 0.1445
|
|
98.08 0.7218 0.7778 0.0195 0.0181 1.805 16.252 5.368 1345.991 1.836 23.876 1.809 0.58 276196. 0.1200
|
|
102.00 0.7506 0.7336 0.0144 0.0148 1.477 13.301 3.984 1101.572 1.503 17.722 1.641 0.59 277131. 0.0937
|
|
105.93 0.7795 0.6507 0.0095 0.0114 1.137 10.239 2.620 848.013 1.157 11.652 1.401 0.59 278095. 0.0649
|
|
109.85 0.8084 0.4775 0.0047 0.0079 0.788 7.096 1.285 587.664 0.802 5.715 0.992 0.59 279090. 0.0322
|
|
113.77 0.8373 -0.0080 0.0000 0.0043 0.433 3.897 -0.011 322.723 0.440 -0.051 -0.016 0.59 280103. 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 0.0993 0.0351 5.238 41.267 35.780 3905.862 4.662 159.148 4.155 0.65 300251. 0.7114
|
|
4.48 0.0288 0.0790 0.0985 0.0360 5.368 42.288 35.484 4002.555 4.778 157.834 4.021 0.65 300477. 0.6856
|
|
8.96 0.0577 0.1527 0.0976 0.0369 5.499 43.322 35.146 4100.418 4.895 156.331 3.888 0.65 300728. 0.6597
|
|
13.44 0.0865 0.2213 0.0965 0.0377 5.629 44.351 34.761 4197.822 5.011 154.618 3.756 0.65 301006. 0.6338
|
|
17.92 0.1154 0.2848 0.0953 0.0386 5.757 45.356 34.322 4292.951 5.124 152.665 3.626 0.65 301313. 0.6081
|
|
22.40 0.1442 0.3436 0.0939 0.0394 5.879 46.316 33.824 4383.748 5.233 150.448 3.500 0.65 301650. 0.5826
|
|
26.88 0.1731 0.3978 0.0923 0.0402 5.992 47.205 33.259 4467.936 5.333 147.937 3.376 0.65 302018. 0.5573
|
|
31.36 0.2019 0.4477 0.0906 0.0408 6.092 47.999 32.623 4543.078 5.423 145.108 3.257 0.65 302418. 0.5325
|
|
35.84 0.2307 0.4936 0.0886 0.0414 6.178 48.670 31.910 4606.619 5.499 141.936 3.142 0.65 302851. 0.5080
|
|
40.31 0.2596 0.5357 0.0864 0.0419 6.244 49.191 31.115 4655.915 5.558 138.399 3.031 0.65 303319. 0.4840
|
|
44.79 0.2884 0.5744 0.0839 0.0421 6.287 49.533 30.233 4688.316 5.596 134.477 2.925 0.65 303822. 0.4603
|
|
49.27 0.3173 0.6098 0.0812 0.0423 6.304 49.669 29.261 4701.166 5.612 130.152 2.823 0.65 304360. 0.4371
|
|
53.75 0.3461 0.6423 0.0783 0.0422 6.292 49.571 28.195 4691.886 5.601 125.411 2.726 0.65 304933. 0.4143
|
|
58.23 0.3750 0.6720 0.0750 0.0419 6.247 49.213 27.033 4658.028 5.560 120.245 2.632 0.66 305542. 0.3917
|
|
62.71 0.4038 0.6991 0.0716 0.0413 6.165 48.572 25.775 4597.310 5.488 114.647 2.543 0.66 306188. 0.3695
|
|
67.19 0.4326 0.7238 0.0678 0.0405 6.045 47.623 24.418 4507.488 5.380 108.610 2.457 0.66 306869. 0.3475
|
|
71.67 0.4615 0.7460 0.0637 0.0394 5.882 46.344 22.962 4386.476 5.236 102.134 2.374 0.66 307586. 0.3256
|
|
76.15 0.4903 0.7659 0.0595 0.0381 5.678 44.732 21.415 4233.822 5.054 95.254 2.294 0.66 308340. 0.3039
|
|
80.63 0.5192 0.7833 0.0549 0.0364 5.432 42.795 19.790 4050.483 4.835 88.026 2.216 0.66 309128. 0.2822
|
|
85.11 0.5480 0.7981 0.0502 0.0345 5.147 40.547 18.099 3837.756 4.581 80.507 2.139 0.66 309952. 0.2605
|
|
89.59 0.5769 0.8100 0.0454 0.0323 4.824 38.003 16.354 3596.970 4.294 72.745 2.062 0.66 310811. 0.2387
|
|
94.07 0.6057 0.8183 0.0404 0.0299 4.465 35.177 14.566 3329.463 3.974 64.788 1.984 0.66 311705. 0.2168
|
|
98.55 0.6345 0.8223 0.0354 0.0273 4.072 32.083 12.743 3036.650 3.625 56.682 1.903 0.66 312634. 0.1945
|
|
103.03 0.6634 0.8207 0.0303 0.0245 3.648 28.739 10.898 2720.104 3.247 48.472 1.817 0.66 313597. 0.1717
|
|
107.51 0.6922 0.8113 0.0251 0.0214 3.194 25.163 9.039 2381.635 2.843 40.205 1.721 0.67 314595. 0.1481
|
|
111.98 0.7211 0.7900 0.0199 0.0182 2.713 21.378 7.179 2023.386 2.415 31.932 1.609 0.67 315627. 0.1234
|
|
116.46 0.7499 0.7489 0.0148 0.0148 2.210 17.411 5.330 1647.938 1.967 23.706 1.467 0.67 316693. 0.0969
|
|
120.94 0.7788 0.6697 0.0097 0.0113 1.688 13.296 3.504 1258.431 1.502 15.588 1.263 0.67 317794. 0.0677
|
|
125.42 0.8076 0.4991 0.0048 0.0077 1.151 9.072 1.718 858.616 1.025 7.644 0.908 0.67 318929. 0.0341
|
|
129.90 0.8364 -0.0093 0.0000 0.0041 0.606 4.776 -0.016 452.044 0.540 -0.072 -0.016 0.67 320084. 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 0.1004 0.0362 7.685 53.821 45.790 5730.890 6.081 203.673 3.624 0.73 337749. 0.7019
|
|
5.03 0.0288 0.0775 0.0997 0.0370 7.864 55.075 45.447 5864.418 6.222 202.149 3.515 0.73 338003. 0.6783
|
|
10.06 0.0576 0.1503 0.0988 0.0379 8.046 56.348 45.052 5999.943 6.366 200.393 3.406 0.73 338284. 0.6543
|
|
15.10 0.0864 0.2182 0.0978 0.0387 8.228 57.619 44.598 6135.260 6.510 198.372 3.297 0.73 338596. 0.6302
|
|
20.13 0.1152 0.2814 0.0967 0.0396 8.405 58.864 44.075 6267.871 6.650 196.047 3.189 0.73 338941. 0.6061
|
|
25.16 0.1440 0.3401 0.0954 0.0404 8.576 60.057 43.476 6394.949 6.785 193.381 3.084 0.73 339319. 0.5820
|
|
30.19 0.1728 0.3944 0.0939 0.0411 8.734 61.169 42.792 6513.311 6.911 190.337 2.980 0.73 339732. 0.5579
|
|
35.22 0.2016 0.4445 0.0922 0.0418 8.877 62.166 42.013 6619.518 7.024 186.876 2.879 0.73 340182. 0.5341
|
|
40.26 0.2304 0.4907 0.0902 0.0424 8.998 63.015 41.134 6709.882 7.119 182.965 2.781 0.73 340670. 0.5104
|
|
45.29 0.2592 0.5332 0.0881 0.0428 9.093 63.679 40.146 6780.570 7.194 178.571 2.685 0.73 341197. 0.4870
|
|
50.32 0.2880 0.5722 0.0856 0.0431 9.156 64.121 39.044 6827.605 7.244 173.667 2.594 0.73 341762. 0.4639
|
|
55.35 0.3168 0.6080 0.0830 0.0432 9.182 64.303 37.822 6846.997 7.265 168.230 2.505 0.74 342368. 0.4410
|
|
60.38 0.3456 0.6408 0.0800 0.0432 9.166 64.188 36.475 6834.763 7.252 162.241 2.421 0.74 343013. 0.4184
|
|
65.42 0.3744 0.6708 0.0768 0.0429 9.102 63.740 35.001 6787.023 7.201 155.685 2.339 0.74 343699. 0.3961
|
|
70.45 0.4032 0.6983 0.0733 0.0423 8.985 62.923 33.398 6700.133 7.109 148.556 2.261 0.74 344426. 0.3740
|
|
75.48 0.4320 0.7233 0.0695 0.0415 8.811 61.707 31.665 6570.561 6.972 140.845 2.186 0.74 345192. 0.3521
|
|
80.51 0.4608 0.7460 0.0654 0.0404 8.576 60.058 29.800 6395.027 6.785 132.549 2.114 0.74 346000. 0.3302
|
|
85.54 0.4896 0.7664 0.0610 0.0390 8.278 57.969 27.813 6172.596 6.549 123.710 2.044 0.74 346847. 0.3085
|
|
90.58 0.5184 0.7845 0.0564 0.0373 7.918 55.452 25.720 5904.605 6.265 114.402 1.976 0.74 347734. 0.2868
|
|
95.61 0.5472 0.8001 0.0516 0.0353 7.500 52.526 23.538 5592.986 5.934 104.697 1.909 0.74 348660. 0.2651
|
|
100.64 0.5760 0.8128 0.0467 0.0331 7.027 49.209 21.282 5239.775 5.560 94.661 1.842 0.74 349626. 0.2432
|
|
105.67 0.6048 0.8222 0.0416 0.0306 6.500 45.521 18.965 4847.087 5.143 84.357 1.775 0.75 350631. 0.2212
|
|
110.71 0.6336 0.8273 0.0364 0.0279 5.924 41.484 16.602 4417.201 4.687 73.845 1.705 0.75 351674. 0.1988
|
|
115.74 0.6624 0.8270 0.0312 0.0250 5.301 37.121 14.205 3952.681 4.194 63.183 1.630 0.75 352756. 0.1758
|
|
120.77 0.6912 0.8190 0.0259 0.0218 4.635 32.462 11.788 3456.583 3.668 52.435 1.547 0.75 353877. 0.1520
|
|
125.80 0.7200 0.7990 0.0205 0.0185 3.933 27.541 9.367 2932.606 3.112 41.664 1.449 0.75 355036. 0.1269
|
|
130.83 0.7488 0.7587 0.0153 0.0151 3.199 22.401 6.956 2385.312 2.531 30.942 1.323 0.75 356234. 0.0999
|
|
135.87 0.7776 0.6790 0.0100 0.0115 2.441 17.095 4.575 1820.286 1.931 20.348 1.140 0.75 357469. 0.0698
|
|
140.90 0.8064 0.5047 0.0049 0.0079 1.669 11.685 2.241 1244.215 1.320 9.969 0.817 0.76 358742. 0.0350
|
|
145.93 0.8352 -0.0121 -0.0001 0.0042 0.890 6.232 -0.028 663.570 0.704 -0.123 -0.019 0.76 360038. 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 0.1016 0.0399 11.616 73.215 57.185 8662.162 8.272 254.361 2.994 0.81 375233. 0.6481
|
|
5.58 0.0287 0.0714 0.1009 0.0406 11.835 74.591 56.814 8825.055 8.427 252.708 2.920 0.81 375512. 0.6300
|
|
11.16 0.0575 0.1391 0.1002 0.0414 12.054 75.974 56.381 8988.668 8.584 250.784 2.845 0.81 375824. 0.6114
|
|
16.73 0.0862 0.2032 0.0993 0.0421 12.270 77.336 55.877 9149.750 8.737 248.542 2.770 0.81 376169. 0.5926
|
|
22.31 0.1149 0.2636 0.0982 0.0428 12.478 78.646 55.291 9304.763 8.885 245.934 2.695 0.81 376549. 0.5736
|
|
27.89 0.1437 0.3205 0.0970 0.0435 12.672 79.871 54.610 9449.706 9.024 242.905 2.621 0.81 376968. 0.5544
|
|
33.47 0.1724 0.3739 0.0956 0.0441 12.847 80.975 53.823 9580.310 9.149 239.402 2.548 0.81 377426. 0.5351
|
|
39.04 0.2011 0.4239 0.0940 0.0446 12.997 81.920 52.917 9692.074 9.255 235.373 2.476 0.81 377925. 0.5156
|
|
44.62 0.2299 0.4707 0.0922 0.0450 13.116 82.666 51.881 9780.418 9.340 230.767 2.406 0.82 378466. 0.4960
|
|
50.20 0.2586 0.5143 0.0901 0.0453 13.197 83.176 50.705 9840.728 9.397 225.537 2.337 0.82 379050. 0.4763
|
|
55.78 0.2873 0.5550 0.0877 0.0454 13.234 83.410 49.381 9868.368 9.424 219.645 2.270 0.82 379678. 0.4565
|
|
61.36 0.3161 0.5928 0.0851 0.0454 13.221 83.328 47.899 9858.733 9.414 213.055 2.204 0.82 380351. 0.4365
|
|
66.93 0.3448 0.6277 0.0822 0.0451 13.152 82.893 46.255 9807.267 9.365 205.741 2.139 0.82 381068. 0.4164
|
|
72.51 0.3735 0.6600 0.0790 0.0447 13.021 82.067 44.443 9709.451 9.272 197.684 2.076 0.82 381830. 0.3962
|
|
78.09 0.4023 0.6896 0.0754 0.0440 12.821 80.811 42.462 9560.855 9.130 188.870 2.014 0.82 382636. 0.3757
|
|
83.67 0.4310 0.7167 0.0716 0.0431 12.548 79.087 40.308 9356.977 8.935 179.292 1.954 0.82 383488. 0.3551
|
|
89.24 0.4597 0.7412 0.0675 0.0419 12.194 76.857 37.982 9093.039 8.683 168.943 1.895 0.82 384384. 0.3342
|
|
94.82 0.4885 0.7633 0.0631 0.0404 11.757 74.100 35.492 8766.952 8.372 157.867 1.836 0.82 385325. 0.3131
|
|
100.40 0.5172 0.7827 0.0584 0.0386 11.240 70.843 32.859 8381.583 8.004 146.157 1.778 0.82 386309. 0.2918
|
|
105.98 0.5459 0.7991 0.0535 0.0365 10.646 67.100 30.105 7938.703 7.581 133.908 1.720 0.83 387337. 0.2701
|
|
111.56 0.5746 0.8123 0.0484 0.0343 9.979 62.896 27.250 7441.286 7.106 121.208 1.661 0.83 388409. 0.2482
|
|
117.13 0.6034 0.8216 0.0432 0.0317 9.242 58.253 24.311 6892.061 6.581 108.137 1.600 0.83 389523. 0.2258
|
|
122.71 0.6321 0.8260 0.0379 0.0290 8.441 53.199 21.307 6294.112 6.010 94.774 1.535 0.83 390680. 0.2029
|
|
128.29 0.6608 0.8238 0.0324 0.0260 7.580 47.777 18.254 5652.558 5.398 81.195 1.465 0.83 391879. 0.1791
|
|
133.87 0.6896 0.8119 0.0270 0.0229 6.670 42.038 15.171 4973.632 4.749 67.479 1.383 0.83 393120. 0.1542
|
|
139.44 0.7183 0.7850 0.0215 0.0196 5.719 36.048 12.075 4264.939 4.073 53.708 1.284 0.83 394404. 0.1277
|
|
145.02 0.7470 0.7330 0.0160 0.0163 4.741 29.882 8.987 3535.388 3.376 39.972 1.153 0.84 395729. 0.0989
|
|
150.60 0.7758 0.6352 0.0105 0.0129 3.749 23.626 5.929 2795.278 2.669 26.373 0.962 0.84 397097. 0.0671
|
|
156.18 0.8045 0.4422 0.0052 0.0095 2.757 17.379 2.928 2056.154 1.963 13.022 0.646 0.84 398506. 0.0316
|
|
161.76 0.8332 0.0018 0.0000 0.0061 1.782 11.233 0.007 1329.005 1.269 0.033 0.002 0.84 399946. 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 0.1021 0.0475 18.411 105.493 69.502 13729.150 11.919 309.143 2.296 0.89 412733. 0.5479
|
|
6.16 0.0289 0.0608 0.1015 0.0482 18.695 107.121 69.141 13941.109 12.103 307.537 2.249 0.89 413037. 0.5354
|
|
12.33 0.0577 0.1190 0.1009 0.0489 18.975 108.721 68.713 14149.326 12.283 305.635 2.203 0.89 413376. 0.5226
|
|
18.49 0.0866 0.1748 0.1002 0.0496 19.241 110.246 68.205 14347.807 12.456 303.377 2.156 0.89 413753. 0.5097
|
|
24.65 0.1154 0.2281 0.0993 0.0502 19.485 111.646 67.603 14529.933 12.614 300.696 2.110 0.90 414171. 0.4966
|
|
30.81 0.1443 0.2790 0.0982 0.0508 19.698 112.865 66.888 14688.546 12.751 297.518 2.065 0.90 414631. 0.4835
|
|
36.98 0.1732 0.3277 0.0970 0.0512 19.869 113.846 66.044 14816.195 12.862 293.766 2.022 0.90 415135. 0.4703
|
|
43.14 0.2020 0.3744 0.0955 0.0515 19.989 114.532 65.054 14905.552 12.940 289.362 1.980 0.90 415685. 0.4570
|
|
49.30 0.2309 0.4190 0.0938 0.0517 20.048 114.872 63.901 14949.740 12.978 284.232 1.939 0.90 416283. 0.4436
|
|
55.46 0.2597 0.4618 0.0919 0.0517 20.038 114.817 62.569 14942.613 12.972 278.306 1.899 0.90 416930. 0.4300
|
|
61.63 0.2886 0.5027 0.0896 0.0515 19.953 114.327 61.043 14878.859 12.917 271.521 1.861 0.90 417626. 0.4161
|
|
67.79 0.3175 0.5419 0.0871 0.0510 19.785 113.368 59.313 14753.984 12.808 263.825 1.823 0.90 418372. 0.4019
|
|
73.95 0.3463 0.5792 0.0842 0.0504 19.531 111.909 57.368 14564.146 12.643 255.174 1.787 0.90 419169. 0.3873
|
|
80.11 0.3752 0.6147 0.0811 0.0495 19.185 109.925 55.202 14305.958 12.419 245.537 1.750 0.90 420016. 0.3722
|
|
86.28 0.4040 0.6482 0.0775 0.0483 18.743 107.394 52.809 13976.544 12.133 234.895 1.714 0.90 420913. 0.3565
|
|
92.44 0.4329 0.6797 0.0737 0.0469 18.202 104.293 50.188 13572.973 11.783 223.236 1.677 0.90 421861. 0.3401
|
|
98.60 0.4617 0.7089 0.0695 0.0453 17.556 100.593 47.336 13091.507 11.365 210.549 1.640 0.90 422858. 0.3230
|
|
104.76 0.4906 0.7358 0.0650 0.0433 16.806 96.296 44.266 12532.281 10.879 196.897 1.602 0.91 423905. 0.3051
|
|
110.93 0.5195 0.7601 0.0602 0.0412 15.959 91.442 41.007 11900.479 10.331 182.400 1.563 0.91 425000. 0.2865
|
|
117.09 0.5483 0.7803 0.0552 0.0388 15.039 86.173 37.584 11214.823 9.736 167.174 1.520 0.91 426144. 0.2667
|
|
123.25 0.5772 0.7959 0.0500 0.0362 14.050 80.502 34.023 10476.826 9.095 151.336 1.473 0.91 427335. 0.2459
|
|
129.42 0.6060 0.8051 0.0446 0.0335 13.008 74.534 30.348 9700.026 8.421 134.987 1.419 0.91 428574. 0.2238
|
|
135.58 0.6349 0.8037 0.0390 0.0308 11.955 68.499 26.576 8914.658 7.739 118.212 1.352 0.91 429859. 0.1995
|
|
141.74 0.6638 0.7907 0.0334 0.0280 10.869 62.277 22.738 8104.883 7.036 101.138 1.272 0.91 431191. 0.1737
|
|
147.90 0.6926 0.7631 0.0277 0.0251 9.747 55.848 18.860 7268.205 6.310 83.889 1.177 0.92 432570. 0.1463
|
|
154.07 0.7215 0.7146 0.0220 0.0222 8.608 49.320 14.971 6418.634 5.572 66.593 1.058 0.92 433995. 0.1172
|
|
160.23 0.7503 0.6350 0.0163 0.0193 7.471 42.808 11.103 5571.177 4.836 49.386 0.904 0.92 435466. 0.0862
|
|
166.39 0.7792 0.5087 0.0107 0.0164 6.358 36.428 7.289 4740.837 4.116 32.422 0.697 0.92 436983. 0.0539
|
|
172.55 0.8081 0.3107 0.0052 0.0136 5.286 30.290 3.570 3941.999 3.422 15.877 0.411 0.92 438546. 0.0222
|
|
178.72 0.8369 -0.0027 0.0000 0.0110 4.266 24.441 -0.024 3180.820 2.761 -0.109 -0.003 0.93 440153. 0.0000
|
|
|
|
|
|
|