427 lines
76 KiB
Plaintext
427 lines
76 KiB
Plaintext
20.5x14EPN (205x14EPN.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 0.0949 0.0386 0.011 0.708 0.534 8.378 0.080 2.377 28.933 0.08 37544. 0.6054
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0.56 0.0288 0.0688 0.0939 0.0393 0.011 0.721 0.529 8.533 0.081 2.352 28.106 0.08 37572. 0.5850
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1.12 0.0575 0.1335 0.0928 0.0400 0.012 0.734 0.522 8.687 0.083 2.324 27.276 0.08 37603. 0.5643
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1.67 0.0863 0.1942 0.0916 0.0407 0.012 0.747 0.515 8.839 0.084 2.292 26.448 0.08 37638. 0.5435
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2.23 0.1150 0.2509 0.0902 0.0413 0.012 0.759 0.508 8.983 0.086 2.258 25.627 0.08 37676. 0.5226
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2.79 0.1438 0.3037 0.0886 0.0420 0.012 0.771 0.499 9.117 0.087 2.219 24.815 0.08 37717. 0.5016
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3.35 0.1726 0.3527 0.0869 0.0425 0.012 0.781 0.489 9.238 0.088 2.176 24.016 0.08 37763. 0.4808
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3.91 0.2013 0.3980 0.0850 0.0430 0.013 0.790 0.478 9.341 0.089 2.128 23.233 0.08 37812. 0.4600
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4.47 0.2301 0.4399 0.0829 0.0434 0.013 0.796 0.467 9.423 0.090 2.076 22.466 0.08 37866. 0.4393
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5.02 0.2588 0.4784 0.0806 0.0436 0.013 0.801 0.454 9.478 0.091 2.019 21.717 0.08 37924. 0.4188
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5.58 0.2876 0.5137 0.0781 0.0437 0.013 0.803 0.440 9.504 0.091 1.956 20.987 0.08 37985. 0.3984
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6.14 0.3163 0.5458 0.0754 0.0437 0.013 0.803 0.424 9.497 0.091 1.888 20.274 0.08 38052. 0.3781
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6.70 0.3451 0.5750 0.0725 0.0435 0.013 0.799 0.408 9.452 0.090 1.815 19.578 0.08 38122. 0.3579
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7.26 0.3739 0.6012 0.0693 0.0431 0.013 0.792 0.390 9.366 0.089 1.736 18.896 0.08 38197. 0.3379
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7.82 0.4026 0.6245 0.0659 0.0425 0.012 0.781 0.371 9.236 0.088 1.651 18.227 0.08 38277. 0.3178
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8.37 0.4314 0.6449 0.0623 0.0417 0.012 0.766 0.351 9.059 0.087 1.561 17.566 0.08 38361. 0.2978
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8.93 0.4601 0.6622 0.0585 0.0407 0.012 0.747 0.329 8.833 0.084 1.465 16.909 0.08 38449. 0.2777
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9.49 0.4889 0.6762 0.0545 0.0394 0.011 0.723 0.307 8.558 0.082 1.364 16.252 0.08 38542. 0.2576
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10.05 0.5177 0.6867 0.0503 0.0379 0.011 0.696 0.283 8.236 0.079 1.259 15.586 0.08 38640. 0.2373
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10.61 0.5464 0.6931 0.0459 0.0362 0.011 0.665 0.259 7.868 0.075 1.150 14.904 0.08 38741. 0.2169
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11.17 0.5752 0.6948 0.0415 0.0343 0.010 0.630 0.233 7.458 0.071 1.038 14.194 0.08 38848. 0.1963
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11.72 0.6039 0.6909 0.0369 0.0323 0.009 0.592 0.208 7.008 0.067 0.924 13.443 0.08 38958. 0.1754
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12.28 0.6327 0.6802 0.0323 0.0300 0.009 0.551 0.182 6.519 0.062 0.808 12.633 0.08 39073. 0.1541
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12.84 0.6615 0.6609 0.0276 0.0276 0.008 0.507 0.155 5.995 0.057 0.690 11.740 0.08 39192. 0.1324
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13.40 0.6902 0.6301 0.0229 0.0250 0.007 0.460 0.129 5.439 0.052 0.572 10.727 0.08 39316. 0.1101
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13.96 0.7190 0.5838 0.0181 0.0223 0.007 0.410 0.102 4.853 0.046 0.454 9.541 0.08 39444. 0.0873
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14.52 0.7477 0.5151 0.0135 0.0195 0.006 0.359 0.076 4.242 0.041 0.337 8.095 0.08 39577. 0.0638
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15.07 0.7765 0.4124 0.0088 0.0166 0.005 0.305 0.050 3.610 0.034 0.221 6.240 0.08 39713. 0.0398
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15.63 0.8053 0.2533 0.0043 0.0136 0.004 0.250 0.024 2.962 0.028 0.107 3.697 0.08 39854. 0.0164
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16.19 0.8340 -0.0095 -0.0001 0.0106 0.003 0.195 -0.001 2.304 0.022 -0.003 -0.134 0.08 39999. 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 0.0953 0.0360 0.084 2.642 2.145 62.525 0.299 9.542 15.563 0.16 75087. 0.6524
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1.12 0.0289 0.0741 0.0943 0.0367 0.086 2.698 2.123 63.834 0.305 9.443 15.085 0.16 75143. 0.6291
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2.24 0.0577 0.1435 0.0932 0.0375 0.087 2.753 2.098 65.142 0.311 9.331 14.607 0.16 75206. 0.6056
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3.36 0.0866 0.2082 0.0919 0.0382 0.089 2.807 2.070 66.425 0.317 9.207 14.134 0.16 75275. 0.5820
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4.48 0.1154 0.2685 0.0906 0.0389 0.091 2.859 2.039 67.660 0.323 9.068 13.666 0.16 75352. 0.5585
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5.60 0.1443 0.3243 0.0890 0.0396 0.092 2.908 2.004 68.818 0.329 8.913 13.207 0.16 75435. 0.5351
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6.72 0.1731 0.3759 0.0873 0.0402 0.094 2.953 1.965 69.868 0.334 8.741 12.758 0.16 75527. 0.5119
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7.84 0.2020 0.4235 0.0854 0.0407 0.095 2.991 1.922 70.778 0.338 8.551 12.320 0.16 75626. 0.4889
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8.96 0.2308 0.4673 0.0833 0.0411 0.096 3.022 1.875 71.515 0.341 8.342 11.894 0.16 75734. 0.4662
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10.08 0.2597 0.5075 0.0810 0.0415 0.097 3.045 1.824 72.044 0.344 8.112 11.482 0.16 75850. 0.4438
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11.20 0.2885 0.5443 0.0785 0.0416 0.097 3.057 1.767 72.331 0.345 7.861 11.082 0.16 75974. 0.4217
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12.32 0.3174 0.5778 0.0758 0.0416 0.097 3.057 1.706 72.344 0.345 7.587 10.695 0.16 76108. 0.3998
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13.44 0.3462 0.6082 0.0728 0.0415 0.097 3.045 1.639 72.050 0.344 7.292 10.320 0.16 76250. 0.3782
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14.56 0.3751 0.6357 0.0696 0.0411 0.096 3.018 1.568 71.420 0.341 6.974 9.957 0.16 76401. 0.3568
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15.68 0.4040 0.6603 0.0662 0.0405 0.094 2.976 1.491 70.425 0.336 6.632 9.603 0.16 76561. 0.3356
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16.80 0.4328 0.6820 0.0626 0.0397 0.093 2.918 1.409 69.037 0.330 6.268 9.258 0.16 76730. 0.3146
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17.92 0.4617 0.7009 0.0587 0.0387 0.090 2.842 1.322 67.241 0.321 5.882 8.920 0.16 76908. 0.2936
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19.04 0.4905 0.7168 0.0547 0.0374 0.087 2.749 1.231 65.037 0.311 5.476 8.585 0.16 77095. 0.2727
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20.17 0.5194 0.7295 0.0505 0.0359 0.084 2.639 1.136 62.436 0.298 5.052 8.252 0.16 77291. 0.2517
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21.29 0.5482 0.7385 0.0461 0.0342 0.080 2.513 1.037 59.453 0.284 4.614 7.914 0.17 77496. 0.2307
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22.41 0.5771 0.7434 0.0416 0.0323 0.075 2.371 0.936 56.106 0.268 4.164 7.569 0.17 77709. 0.2096
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23.53 0.6059 0.7434 0.0370 0.0302 0.070 2.215 0.833 52.412 0.250 3.705 7.208 0.17 77932. 0.1883
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24.65 0.6348 0.7373 0.0323 0.0278 0.065 2.045 0.728 48.391 0.231 3.238 6.824 0.17 78163. 0.1666
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25.77 0.6636 0.7233 0.0276 0.0254 0.059 1.862 0.622 44.065 0.210 2.767 6.403 0.17 78403. 0.1445
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26.89 0.6925 0.6987 0.0229 0.0227 0.053 1.668 0.516 39.457 0.188 2.294 5.927 0.17 78652. 0.1218
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28.01 0.7214 0.6590 0.0182 0.0199 0.046 1.462 0.409 34.597 0.165 1.821 5.367 0.17 78910. 0.0983
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29.13 0.7502 0.5963 0.0135 0.0170 0.040 1.247 0.304 29.517 0.141 1.352 4.670 0.17 79176. 0.0737
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30.25 0.7791 0.4957 0.0089 0.0140 0.033 1.025 0.200 24.257 0.116 0.889 3.738 0.17 79452. 0.0478
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31.37 0.8079 0.3246 0.0044 0.0109 0.025 0.797 0.098 18.861 0.090 0.437 2.361 0.17 79735. 0.0212
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32.49 0.8368 -0.0031 0.0000 0.0077 0.018 0.565 -0.001 13.375 0.064 -0.003 -0.022 0.17 80026. 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 0.0957 0.0350 0.275 5.777 4.846 205.035 0.653 21.553 10.719 0.24 112627. 0.6754
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1.68 0.0289 0.0765 0.0947 0.0357 0.281 5.905 4.796 209.573 0.667 21.332 10.379 0.24 112712. 0.6506
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3.36 0.0578 0.1481 0.0936 0.0365 0.287 6.033 4.740 214.116 0.682 21.084 10.041 0.24 112807. 0.6257
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5.05 0.0867 0.2147 0.0923 0.0373 0.293 6.158 4.678 218.585 0.696 20.806 9.706 0.24 112911. 0.6008
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6.73 0.1155 0.2766 0.0910 0.0380 0.299 6.280 4.608 222.895 0.709 20.495 9.376 0.24 113026. 0.5761
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8.41 0.1444 0.3338 0.0894 0.0387 0.304 6.394 4.530 226.948 0.722 20.149 9.053 0.24 113151. 0.5515
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10.09 0.1733 0.3867 0.0877 0.0393 0.309 6.498 4.443 230.642 0.734 19.764 8.738 0.24 113289. 0.5272
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11.78 0.2022 0.4353 0.0858 0.0399 0.314 6.589 4.347 233.864 0.744 19.337 8.432 0.24 113438. 0.5032
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13.46 0.2311 0.4799 0.0837 0.0403 0.317 6.663 4.242 236.498 0.753 18.866 8.135 0.24 113600. 0.4795
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15.14 0.2600 0.5209 0.0814 0.0406 0.320 6.717 4.125 238.424 0.759 18.349 7.848 0.24 113775. 0.4562
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16.82 0.2889 0.5583 0.0789 0.0408 0.321 6.748 3.998 239.526 0.762 17.783 7.571 0.24 113962. 0.4333
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18.50 0.3177 0.5925 0.0762 0.0409 0.321 6.753 3.859 239.687 0.763 17.167 7.303 0.25 114162. 0.4107
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20.19 0.3466 0.6236 0.0732 0.0407 0.320 6.728 3.709 238.797 0.760 16.500 7.046 0.25 114376. 0.3884
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21.87 0.3755 0.6517 0.0700 0.0404 0.317 6.670 3.548 236.751 0.754 15.781 6.797 0.25 114603. 0.3664
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23.55 0.4044 0.6769 0.0666 0.0398 0.313 6.577 3.374 233.449 0.743 15.009 6.556 0.25 114844. 0.3447
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25.23 0.4333 0.6994 0.0630 0.0390 0.307 6.446 3.189 228.795 0.728 14.186 6.322 0.25 115098. 0.3232
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26.92 0.4622 0.7192 0.0591 0.0380 0.299 6.275 2.993 222.732 0.709 13.312 6.095 0.25 115366. 0.3018
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28.60 0.4911 0.7361 0.0550 0.0367 0.289 6.065 2.786 215.256 0.685 12.393 5.871 0.25 115647. 0.2805
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30.28 0.5199 0.7499 0.0508 0.0352 0.277 5.815 2.571 206.402 0.657 11.435 5.649 0.25 115941. 0.2593
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31.96 0.5488 0.7605 0.0464 0.0335 0.263 5.528 2.348 196.220 0.625 10.443 5.427 0.25 116249. 0.2380
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33.65 0.5777 0.7672 0.0418 0.0315 0.248 5.206 2.119 184.766 0.588 9.425 5.202 0.25 116571. 0.2167
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35.33 0.6066 0.7694 0.0372 0.0293 0.231 4.849 1.885 172.102 0.548 8.385 4.968 0.25 116905. 0.1952
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37.01 0.6355 0.7660 0.0325 0.0270 0.212 4.460 1.648 158.293 0.504 7.329 4.721 0.25 117253. 0.1735
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38.69 0.6644 0.7554 0.0278 0.0244 0.192 4.041 1.408 143.414 0.456 6.263 4.453 0.25 117614. 0.1512
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40.37 0.6933 0.7348 0.0230 0.0217 0.171 3.594 1.167 127.548 0.406 5.192 4.151 0.25 117988. 0.1284
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42.06 0.7221 0.6998 0.0183 0.0189 0.149 3.122 0.927 110.795 0.353 4.124 3.795 0.25 118376. 0.1046
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43.74 0.7510 0.6422 0.0136 0.0159 0.125 2.628 0.689 93.272 0.297 3.064 3.349 0.25 118776. 0.0796
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45.42 0.7799 0.5458 0.0090 0.0128 0.101 2.116 0.454 75.115 0.239 2.019 2.741 0.25 119190. 0.0529
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47.10 0.8088 0.3719 0.0044 0.0096 0.076 1.591 0.224 56.483 0.180 0.998 1.801 0.25 119616. 0.0244
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48.79 0.8377 0.0036 0.0000 0.0064 0.050 1.058 0.001 37.535 0.119 0.006 0.017 0.25 120053. 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 0.0961 0.0345 0.643 10.132 8.655 479.511 1.145 38.500 8.187 0.33 150165. 0.6894
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2.25 0.0289 0.0780 0.0952 0.0353 0.658 10.365 8.568 490.505 1.171 38.112 7.923 0.33 150278. 0.6638
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4.49 0.0578 0.1508 0.0941 0.0361 0.673 10.598 8.471 501.530 1.197 37.677 7.661 0.33 150404. 0.6382
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6.74 0.0868 0.2186 0.0928 0.0369 0.687 10.827 8.361 512.392 1.223 37.189 7.401 0.33 150543. 0.6125
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8.98 0.1157 0.2814 0.0915 0.0376 0.701 11.049 8.238 522.885 1.248 36.642 7.146 0.33 150697. 0.5870
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11.23 0.1446 0.3394 0.0900 0.0383 0.714 11.258 8.100 532.778 1.272 36.031 6.896 0.33 150865. 0.5618
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13.47 0.1735 0.3930 0.0883 0.0390 0.727 11.449 7.947 541.815 1.293 35.350 6.653 0.33 151049. 0.5368
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15.72 0.2024 0.4422 0.0864 0.0395 0.737 11.616 7.777 549.726 1.312 34.594 6.417 0.33 151248. 0.5122
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17.96 0.2313 0.4874 0.0843 0.0400 0.746 11.753 7.589 556.228 1.328 33.758 6.189 0.33 151465. 0.4880
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20.21 0.2603 0.5288 0.0820 0.0403 0.752 11.855 7.383 561.032 1.339 32.838 5.968 0.33 151698. 0.4642
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22.46 0.2892 0.5667 0.0795 0.0406 0.756 11.915 7.156 563.851 1.346 31.830 5.756 0.33 151949. 0.4408
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24.70 0.3181 0.6012 0.0767 0.0406 0.757 11.926 6.909 564.404 1.347 30.731 5.552 0.33 152217. 0.4177
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26.95 0.3470 0.6327 0.0737 0.0404 0.754 11.884 6.641 562.420 1.343 29.540 5.356 0.33 152503. 0.3951
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29.19 0.3759 0.6612 0.0705 0.0401 0.748 11.783 6.352 557.645 1.331 28.256 5.167 0.33 152806. 0.3727
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31.44 0.4049 0.6870 0.0671 0.0395 0.737 11.618 6.042 549.832 1.313 26.876 4.984 0.33 153128. 0.3507
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33.68 0.4338 0.7100 0.0634 0.0387 0.722 11.384 5.711 538.753 1.286 25.402 4.808 0.33 153468. 0.3289
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35.93 0.4627 0.7303 0.0595 0.0377 0.703 11.078 5.359 524.261 1.252 23.837 4.636 0.33 153826. 0.3072
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38.17 0.4916 0.7479 0.0554 0.0364 0.679 10.699 4.989 506.344 1.209 22.190 4.469 0.33 154202. 0.2857
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40.42 0.5205 0.7626 0.0511 0.0349 0.651 10.250 4.603 485.079 1.158 20.473 4.304 0.33 154595. 0.2643
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42.67 0.5494 0.7742 0.0467 0.0331 0.618 9.732 4.203 460.584 1.100 18.695 4.139 0.33 155007. 0.2429
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44.91 0.5784 0.7822 0.0421 0.0311 0.581 9.149 3.792 432.994 1.034 16.869 3.973 0.33 155437. 0.2214
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47.16 0.6073 0.7859 0.0375 0.0289 0.540 8.504 3.373 402.454 0.961 15.004 3.802 0.33 155884. 0.1998
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49.40 0.6362 0.7844 0.0327 0.0265 0.495 7.800 2.947 369.124 0.881 13.110 3.622 0.33 156349. 0.1780
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51.65 0.6651 0.7760 0.0280 0.0240 0.447 7.040 2.517 333.180 0.795 11.198 3.427 0.33 156831. 0.1556
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53.89 0.6940 0.7581 0.0232 0.0212 0.395 6.230 2.086 294.831 0.704 9.278 3.209 0.33 157331. 0.1326
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56.14 0.7230 0.7264 0.0184 0.0183 0.341 5.374 1.655 254.318 0.607 7.362 2.952 0.33 157849. 0.1087
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58.38 0.7519 0.6726 0.0136 0.0152 0.284 4.478 1.228 211.927 0.506 5.461 2.628 0.33 158384. 0.0833
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60.63 0.7808 0.5791 0.0090 0.0121 0.225 3.550 0.807 167.996 0.401 3.589 2.179 0.34 158937. 0.0560
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62.88 0.8097 0.4024 0.0044 0.0088 0.165 2.597 0.396 122.916 0.293 1.760 1.460 0.34 159506. 0.0263
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65.12 0.8386 -0.0058 0.0000 0.0055 0.103 1.628 -0.003 77.064 0.184 -0.015 -0.020 0.34 160089. 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 0.0967 0.0343 1.250 15.756 13.604 932.081 1.780 60.512 6.620 0.41 187698. 0.6989
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2.81 0.0289 0.0788 0.0957 0.0351 1.279 16.127 13.471 953.994 1.822 59.921 6.405 0.41 187839. 0.6729
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5.61 0.0578 0.1523 0.0947 0.0359 1.309 16.499 13.322 975.996 1.864 59.255 6.191 0.41 187997. 0.6468
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8.42 0.0867 0.2207 0.0935 0.0367 1.338 16.866 13.153 997.709 1.905 58.505 5.980 0.41 188171. 0.6207
|
|
11.22 0.1156 0.2840 0.0921 0.0375 1.366 17.221 12.964 1018.725 1.946 57.663 5.772 0.41 188363. 0.5948
|
|
14.03 0.1446 0.3426 0.0906 0.0382 1.393 17.557 12.752 1038.575 1.984 56.720 5.569 0.41 188573. 0.5692
|
|
16.84 0.1735 0.3965 0.0889 0.0389 1.417 17.864 12.515 1056.753 2.018 55.666 5.372 0.41 188803. 0.5439
|
|
19.64 0.2024 0.4461 0.0871 0.0395 1.439 18.134 12.251 1072.719 2.049 54.493 5.180 0.41 189053. 0.5190
|
|
22.45 0.2313 0.4916 0.0850 0.0400 1.456 18.357 11.959 1085.903 2.074 53.193 4.995 0.41 189324. 0.4944
|
|
25.26 0.2602 0.5333 0.0827 0.0403 1.469 18.523 11.637 1095.731 2.093 51.760 4.817 0.41 189616. 0.4703
|
|
28.06 0.2891 0.5715 0.0802 0.0406 1.477 18.622 11.283 1101.625 2.104 50.186 4.645 0.41 189929. 0.4466
|
|
30.87 0.3180 0.6064 0.0774 0.0406 1.479 18.646 10.897 1103.024 2.107 48.469 4.481 0.41 190265. 0.4234
|
|
33.67 0.3469 0.6381 0.0745 0.0405 1.474 18.585 10.477 1099.387 2.100 46.603 4.323 0.41 190622. 0.4005
|
|
36.48 0.3758 0.6670 0.0712 0.0401 1.462 18.429 10.024 1090.204 2.082 44.589 4.171 0.41 191002. 0.3780
|
|
39.29 0.4048 0.6931 0.0678 0.0396 1.442 18.172 9.538 1074.984 2.053 42.423 4.024 0.41 191405. 0.3557
|
|
42.09 0.4337 0.7165 0.0641 0.0388 1.412 17.805 9.017 1053.270 2.012 40.107 3.883 0.41 191830. 0.3337
|
|
44.90 0.4626 0.7374 0.0601 0.0377 1.374 17.323 8.463 1024.759 1.957 37.645 3.746 0.41 192277. 0.3119
|
|
47.71 0.4915 0.7556 0.0560 0.0364 1.327 16.726 7.881 989.413 1.890 35.053 3.613 0.41 192747. 0.2903
|
|
50.51 0.5204 0.7710 0.0517 0.0349 1.270 16.015 7.272 947.377 1.809 32.348 3.482 0.41 193240. 0.2687
|
|
53.32 0.5493 0.7835 0.0472 0.0331 1.205 15.195 6.642 898.881 1.717 29.546 3.352 0.41 193755. 0.2473
|
|
56.12 0.5782 0.7925 0.0426 0.0311 1.132 14.271 5.995 844.190 1.612 26.665 3.221 0.41 194292. 0.2257
|
|
58.93 0.6071 0.7975 0.0379 0.0289 1.051 13.246 5.333 783.592 1.497 23.722 3.087 0.41 194851. 0.2040
|
|
61.74 0.6360 0.7976 0.0331 0.0264 0.962 12.127 4.661 717.399 1.370 20.732 2.947 0.41 195432. 0.1821
|
|
64.54 0.6650 0.7912 0.0283 0.0238 0.866 10.920 3.982 645.968 1.234 17.713 2.796 0.42 196035. 0.1597
|
|
67.35 0.6939 0.7759 0.0235 0.0210 0.764 9.631 3.301 569.710 1.088 14.681 2.628 0.42 196660. 0.1366
|
|
70.16 0.7228 0.7473 0.0186 0.0180 0.656 8.268 2.620 489.111 0.934 11.655 2.430 0.42 197307. 0.1126
|
|
72.96 0.7517 0.6972 0.0138 0.0149 0.543 6.842 1.945 404.742 0.773 8.652 2.180 0.42 197976. 0.0870
|
|
75.77 0.7806 0.6079 0.0091 0.0117 0.425 5.364 1.280 317.284 0.606 5.695 1.830 0.42 198666. 0.0593
|
|
78.57 0.8095 0.4330 0.0045 0.0084 0.305 3.846 0.631 227.524 0.435 2.805 1.257 0.42 199378. 0.0286
|
|
81.38 0.8384 0.0001 0.0000 0.0050 0.183 2.303 0.000 136.215 0.260 0.000 0.000 0.42 200105. 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 0.0974 0.0344 2.163 22.720 19.731 1612.861 2.567 87.764 5.549 0.49 225225. 0.7055
|
|
3.37 0.0289 0.0792 0.0965 0.0352 2.215 23.266 19.546 1651.573 2.629 86.939 5.368 0.49 225394. 0.6793
|
|
6.73 0.0578 0.1532 0.0954 0.0360 2.267 23.814 19.336 1690.510 2.691 86.006 5.188 0.49 225583. 0.6529
|
|
10.10 0.0867 0.2219 0.0943 0.0368 2.319 24.357 19.099 1729.002 2.752 84.951 5.010 0.49 225793. 0.6267
|
|
13.47 0.1156 0.2855 0.0929 0.0376 2.369 24.882 18.832 1766.318 2.811 83.763 4.836 0.49 226023. 0.6006
|
|
16.84 0.1445 0.3443 0.0915 0.0384 2.416 25.380 18.531 1801.638 2.867 82.426 4.665 0.49 226276. 0.5748
|
|
20.20 0.1734 0.3985 0.0898 0.0391 2.460 25.837 18.194 1834.059 2.919 80.928 4.499 0.49 226552. 0.5493
|
|
23.57 0.2024 0.4483 0.0879 0.0397 2.498 26.239 17.818 1862.615 2.964 79.255 4.339 0.49 226852. 0.5242
|
|
26.94 0.2313 0.4941 0.0859 0.0402 2.530 26.572 17.400 1886.297 3.002 77.395 4.184 0.49 227178. 0.4995
|
|
30.30 0.2602 0.5360 0.0836 0.0406 2.553 26.823 16.938 1904.077 3.030 75.338 4.035 0.49 227528. 0.4753
|
|
33.67 0.2891 0.5744 0.0811 0.0408 2.568 26.976 16.429 1914.931 3.048 73.075 3.891 0.49 227905. 0.4514
|
|
37.04 0.3180 0.6095 0.0783 0.0409 2.572 27.017 15.872 1917.856 3.052 70.599 3.754 0.49 228308. 0.4280
|
|
40.41 0.3469 0.6415 0.0753 0.0407 2.564 26.933 15.267 1911.897 3.043 67.905 3.622 0.49 228738. 0.4050
|
|
43.77 0.3758 0.6707 0.0721 0.0404 2.543 26.711 14.611 1896.148 3.018 64.991 3.495 0.49 229195. 0.3824
|
|
47.14 0.4047 0.6971 0.0686 0.0398 2.507 26.339 13.906 1869.743 2.976 61.853 3.373 0.49 229679. 0.3600
|
|
50.51 0.4336 0.7209 0.0649 0.0390 2.457 25.806 13.150 1831.870 2.916 58.492 3.256 0.49 230189. 0.3380
|
|
53.87 0.4625 0.7422 0.0609 0.0380 2.390 25.103 12.346 1781.983 2.836 54.916 3.143 0.49 230727. 0.3161
|
|
57.24 0.4914 0.7609 0.0568 0.0367 2.307 24.230 11.499 1719.990 2.737 51.147 3.032 0.49 231292. 0.2943
|
|
60.61 0.5203 0.7770 0.0524 0.0351 2.208 23.189 10.613 1646.135 2.620 47.208 2.924 0.49 231883. 0.2727
|
|
63.98 0.5493 0.7902 0.0479 0.0333 2.093 21.987 9.695 1560.822 2.484 43.125 2.817 0.50 232501. 0.2511
|
|
67.34 0.5782 0.8002 0.0432 0.0312 1.964 20.631 8.751 1464.515 2.331 38.925 2.710 0.50 233146. 0.2295
|
|
70.71 0.6071 0.8063 0.0384 0.0289 1.821 19.126 7.786 1357.721 2.161 34.631 2.601 0.50 233818. 0.2077
|
|
74.08 0.6360 0.8077 0.0336 0.0264 1.664 17.482 6.805 1240.995 1.975 30.268 2.487 0.50 234515. 0.1857
|
|
77.44 0.6649 0.8030 0.0287 0.0238 1.495 15.707 5.814 1114.966 1.775 25.859 2.365 0.50 235239. 0.1632
|
|
80.81 0.6938 0.7897 0.0238 0.0209 1.315 13.810 4.818 980.363 1.560 21.430 2.229 0.50 235989. 0.1400
|
|
84.18 0.7227 0.7637 0.0189 0.0179 1.124 11.806 3.824 838.048 1.334 17.007 2.069 0.50 236766. 0.1158
|
|
87.55 0.7516 0.7167 0.0140 0.0147 0.924 9.707 2.837 689.043 1.097 12.619 1.867 0.50 237568. 0.0900
|
|
90.91 0.7805 0.6307 0.0092 0.0114 0.717 7.530 1.865 534.561 0.851 8.296 1.582 0.50 238397. 0.0619
|
|
94.28 0.8094 0.4563 0.0045 0.0080 0.504 5.297 0.915 376.011 0.598 4.071 1.104 0.50 239251. 0.0302
|
|
97.65 0.8383 -0.0057 0.0000 0.0046 0.288 3.025 -0.006 214.714 0.342 -0.028 -0.013 0.50 240122. 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 0.0982 0.0346 3.457 31.125 27.086 2577.728 3.516 120.477 4.766 0.57 262744. 0.7099
|
|
3.93 0.0289 0.0794 0.0973 0.0354 3.541 31.886 26.844 2640.759 3.602 119.401 4.611 0.57 262942. 0.6837
|
|
7.85 0.0578 0.1534 0.0963 0.0363 3.626 32.653 26.569 2704.276 3.689 118.178 4.456 0.57 263162. 0.6575
|
|
11.78 0.0867 0.2222 0.0952 0.0371 3.711 33.413 26.257 2767.199 3.775 116.790 4.304 0.57 263406. 0.6312
|
|
15.70 0.1156 0.2860 0.0939 0.0380 3.793 34.151 25.903 2828.335 3.858 115.218 4.154 0.57 263675. 0.6051
|
|
19.63 0.1445 0.3449 0.0925 0.0387 3.871 34.851 25.504 2886.335 3.937 113.440 4.008 0.57 263970. 0.5793
|
|
23.56 0.1733 0.3992 0.0908 0.0394 3.942 35.496 25.054 2939.716 4.010 111.439 3.866 0.57 264292. 0.5538
|
|
27.48 0.2022 0.4491 0.0890 0.0401 4.005 36.066 24.549 2986.889 4.075 109.194 3.728 0.57 264643. 0.5287
|
|
31.41 0.2311 0.4950 0.0870 0.0406 4.058 36.540 23.986 3026.190 4.128 106.689 3.595 0.57 265023. 0.5040
|
|
35.33 0.2600 0.5371 0.0847 0.0410 4.098 36.899 23.361 3055.931 4.169 103.908 3.467 0.57 265433. 0.4797
|
|
39.26 0.2889 0.5756 0.0822 0.0413 4.123 37.123 22.671 3074.426 4.194 100.838 3.345 0.57 265873. 0.4558
|
|
43.18 0.3178 0.6109 0.0795 0.0413 4.130 37.190 21.913 3080.030 4.202 97.470 3.227 0.57 266344. 0.4324
|
|
47.11 0.3467 0.6432 0.0765 0.0412 4.119 37.083 21.087 3071.179 4.190 93.795 3.114 0.57 266846. 0.4093
|
|
51.04 0.3756 0.6726 0.0732 0.0409 4.085 36.784 20.191 3046.390 4.156 89.810 3.006 0.57 267379. 0.3866
|
|
54.96 0.4045 0.6994 0.0697 0.0403 4.029 36.275 19.225 3004.266 4.098 85.511 2.902 0.57 267944. 0.3643
|
|
58.89 0.4334 0.7235 0.0659 0.0395 3.947 35.541 18.188 2943.479 4.015 80.899 2.803 0.57 268540. 0.3421
|
|
62.81 0.4622 0.7452 0.0619 0.0384 3.839 34.571 17.083 2863.112 3.906 75.985 2.706 0.58 269168. 0.3202
|
|
66.74 0.4911 0.7645 0.0577 0.0371 3.705 33.362 15.916 2762.975 3.769 70.796 2.613 0.58 269827. 0.2984
|
|
70.67 0.5200 0.7812 0.0533 0.0355 3.545 31.919 14.696 2643.451 3.606 65.366 2.522 0.58 270517. 0.2767
|
|
74.59 0.5489 0.7951 0.0487 0.0336 3.360 30.249 13.429 2505.185 3.418 59.732 2.431 0.58 271239. 0.2550
|
|
78.52 0.5778 0.8059 0.0440 0.0315 3.150 28.363 12.125 2348.938 3.204 53.930 2.341 0.58 271991. 0.2333
|
|
82.44 0.6067 0.8131 0.0391 0.0292 2.917 26.269 10.790 2175.533 2.968 47.994 2.250 0.58 272774. 0.2115
|
|
86.37 0.6356 0.8157 0.0342 0.0266 2.663 23.979 9.433 1985.881 2.709 41.956 2.154 0.58 273588. 0.1894
|
|
90.30 0.6645 0.8126 0.0292 0.0239 2.388 21.505 8.060 1781.002 2.430 35.852 2.053 0.58 274432. 0.1668
|
|
94.22 0.6934 0.8013 0.0242 0.0210 2.095 18.862 6.681 1562.091 2.131 29.715 1.940 0.58 275307. 0.1435
|
|
98.15 0.7223 0.7777 0.0192 0.0179 1.784 16.066 5.302 1330.552 1.815 23.584 1.807 0.58 276212. 0.1191
|
|
102.07 0.7511 0.7338 0.0143 0.0146 1.459 13.138 3.934 1088.064 1.484 17.498 1.640 0.59 277147. 0.0931
|
|
106.00 0.7800 0.6514 0.0094 0.0112 1.122 10.102 2.586 836.616 1.141 11.501 1.402 0.59 278113. 0.0645
|
|
109.92 0.8089 0.4789 0.0046 0.0078 0.776 6.986 1.268 578.539 0.789 5.639 0.994 0.59 279109. 0.0320
|
|
113.85 0.8378 -0.0081 0.0000 0.0042 0.424 3.815 -0.011 315.982 0.431 -0.050 -0.016 0.59 280123. 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 0.0992 0.0350 5.219 41.115 35.730 3891.483 4.645 158.925 4.164 0.65 300254. 0.7125
|
|
4.48 0.0289 0.0792 0.0984 0.0359 5.348 42.135 35.432 3988.095 4.760 157.602 4.030 0.65 300480. 0.6866
|
|
8.96 0.0577 0.1531 0.0974 0.0367 5.479 43.168 35.092 4085.793 4.877 156.088 3.896 0.65 300731. 0.6605
|
|
13.45 0.0866 0.2218 0.0963 0.0376 5.609 44.194 34.703 4182.911 4.993 154.359 3.763 0.65 301010. 0.6345
|
|
17.93 0.1154 0.2855 0.0951 0.0385 5.736 45.194 34.259 4277.580 5.106 152.386 3.633 0.65 301317. 0.6086
|
|
22.41 0.1443 0.3444 0.0937 0.0393 5.857 46.146 33.755 4367.701 5.214 150.141 3.505 0.65 301654. 0.5829
|
|
26.89 0.1732 0.3987 0.0921 0.0400 5.969 47.025 33.183 4450.927 5.313 147.598 3.381 0.65 302022. 0.5575
|
|
31.38 0.2020 0.4486 0.0903 0.0407 6.068 47.806 32.538 4524.770 5.401 144.728 3.262 0.65 302423. 0.5325
|
|
35.86 0.2309 0.4945 0.0883 0.0412 6.151 48.459 31.814 4586.636 5.475 141.507 3.146 0.65 302857. 0.5079
|
|
40.34 0.2597 0.5367 0.0861 0.0417 6.214 48.958 31.006 4633.885 5.531 137.915 3.035 0.65 303326. 0.4837
|
|
44.82 0.2886 0.5754 0.0836 0.0419 6.254 49.275 30.110 4663.888 5.567 133.931 2.928 0.65 303829. 0.4599
|
|
49.30 0.3175 0.6109 0.0809 0.0420 6.268 49.383 29.124 4674.091 5.579 129.542 2.826 0.65 304368. 0.4365
|
|
53.79 0.3463 0.6433 0.0779 0.0419 6.252 49.256 28.043 4662.072 5.565 124.737 2.728 0.65 304942. 0.4135
|
|
58.27 0.3752 0.6730 0.0746 0.0416 6.203 48.870 26.868 4625.539 5.521 119.510 2.635 0.66 305552. 0.3909
|
|
62.75 0.4041 0.7001 0.0711 0.0410 6.118 48.203 25.598 4562.350 5.446 113.858 2.545 0.66 306198. 0.3685
|
|
67.23 0.4329 0.7246 0.0673 0.0402 5.995 47.232 24.231 4470.473 5.336 107.780 2.458 0.66 306880. 0.3464
|
|
71.71 0.4618 0.7468 0.0632 0.0391 5.831 45.943 22.772 4348.456 5.191 101.289 2.375 0.66 307598. 0.3244
|
|
76.20 0.4906 0.7665 0.0589 0.0377 5.627 44.331 21.228 4195.941 5.009 94.421 2.295 0.66 308351. 0.3026
|
|
80.68 0.5195 0.7838 0.0544 0.0361 5.382 42.404 19.609 4013.477 4.791 87.222 2.216 0.66 309140. 0.2809
|
|
85.16 0.5484 0.7985 0.0498 0.0342 5.099 40.170 17.927 3802.061 4.538 79.741 2.139 0.66 309964. 0.2592
|
|
89.64 0.5772 0.8101 0.0450 0.0320 4.778 37.643 16.193 3562.860 4.253 72.026 2.061 0.66 310824. 0.2374
|
|
94.13 0.6061 0.8183 0.0400 0.0296 4.422 34.835 14.416 3297.156 3.936 64.123 1.983 0.66 311718. 0.2155
|
|
98.61 0.6349 0.8223 0.0350 0.0270 4.032 31.763 12.607 3006.343 3.589 56.077 1.902 0.66 312647. 0.1933
|
|
103.09 0.6638 0.8206 0.0299 0.0242 3.610 28.442 10.777 2692.002 3.213 47.935 1.816 0.66 313611. 0.1706
|
|
107.57 0.6927 0.8112 0.0248 0.0212 3.159 24.892 8.935 2355.969 2.812 39.743 1.720 0.67 314610. 0.1472
|
|
112.05 0.7215 0.7901 0.0197 0.0180 2.683 21.135 7.093 2000.413 2.388 31.551 1.608 0.67 315643. 0.1226
|
|
116.54 0.7504 0.7493 0.0146 0.0146 2.183 17.200 5.264 1627.940 1.943 23.414 1.467 0.67 316711. 0.0963
|
|
121.02 0.7792 0.6706 0.0096 0.0112 1.665 13.119 3.460 1241.686 1.482 15.391 1.264 0.67 317813. 0.0673
|
|
125.50 0.8081 0.5008 0.0047 0.0076 1.134 8.932 1.696 845.368 1.009 7.546 0.910 0.67 318949. 0.0339
|
|
129.98 0.8370 -0.0091 0.0000 0.0040 0.593 4.675 -0.016 442.473 0.528 -0.069 -0.016 0.67 320105. 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 0.1003 0.0361 7.658 53.629 45.727 5710.413 6.059 203.396 3.632 0.73 337752. 0.7030
|
|
5.03 0.0288 0.0777 0.0995 0.0369 7.837 54.882 45.383 5843.836 6.201 201.863 3.522 0.73 338005. 0.6792
|
|
10.07 0.0576 0.1506 0.0987 0.0378 8.018 56.153 44.985 5979.162 6.344 200.093 3.412 0.73 338287. 0.6551
|
|
15.10 0.0865 0.2187 0.0977 0.0386 8.199 57.420 44.526 6114.112 6.487 198.053 3.303 0.73 338600. 0.6309
|
|
20.14 0.1153 0.2821 0.0965 0.0394 8.376 58.660 43.998 6246.126 6.627 195.704 3.195 0.73 338944. 0.6066
|
|
25.17 0.1441 0.3409 0.0952 0.0402 8.545 59.845 43.392 6372.289 6.761 193.006 3.089 0.73 339323. 0.5823
|
|
30.21 0.1729 0.3952 0.0937 0.0410 8.702 60.944 42.698 6489.345 6.885 189.921 2.984 0.73 339737. 0.5582
|
|
35.24 0.2017 0.4454 0.0919 0.0416 8.842 61.925 41.909 6593.768 6.996 186.410 2.883 0.73 340188. 0.5342
|
|
40.28 0.2305 0.4916 0.0900 0.0422 8.960 62.751 41.016 6681.808 7.090 182.439 2.784 0.73 340676. 0.5104
|
|
45.31 0.2594 0.5341 0.0878 0.0426 9.051 63.388 40.013 6749.607 7.162 177.976 2.689 0.73 341203. 0.4868
|
|
50.35 0.2882 0.5732 0.0853 0.0429 9.110 63.798 38.893 6793.252 7.208 172.995 2.597 0.73 341770. 0.4635
|
|
55.38 0.3170 0.6090 0.0826 0.0430 9.131 63.945 37.652 6808.854 7.224 167.475 2.508 0.74 342376. 0.4405
|
|
60.42 0.3458 0.6418 0.0796 0.0429 9.109 63.792 36.287 6792.646 7.207 161.404 2.423 0.74 343022. 0.4178
|
|
65.45 0.3746 0.6718 0.0763 0.0426 9.040 63.307 34.795 6741.006 7.152 154.770 2.341 0.74 343709. 0.3953
|
|
70.49 0.4034 0.6992 0.0728 0.0420 8.918 62.457 33.177 6650.495 7.056 147.570 2.263 0.74 344436. 0.3730
|
|
75.52 0.4323 0.7242 0.0689 0.0412 8.741 61.212 31.431 6517.858 6.916 139.803 2.187 0.74 345203. 0.3510
|
|
80.56 0.4611 0.7468 0.0648 0.0400 8.503 59.548 29.561 6340.697 6.728 131.485 2.115 0.74 346011. 0.3291
|
|
85.59 0.4899 0.7671 0.0605 0.0386 8.205 57.460 27.576 6118.355 6.492 122.659 2.044 0.74 346858. 0.3073
|
|
90.63 0.5187 0.7850 0.0559 0.0369 7.847 54.954 25.491 5851.583 6.209 113.386 1.976 0.74 347746. 0.2855
|
|
95.66 0.5475 0.8004 0.0512 0.0350 7.432 52.046 23.321 5541.857 5.880 103.730 1.909 0.74 348673. 0.2638
|
|
100.70 0.5763 0.8130 0.0462 0.0328 6.961 48.750 21.078 5190.973 5.508 93.754 1.842 0.74 349639. 0.2420
|
|
105.73 0.6052 0.8222 0.0412 0.0303 6.438 45.087 18.777 4800.943 5.094 83.518 1.774 0.75 350644. 0.2200
|
|
110.76 0.6340 0.8273 0.0360 0.0276 5.866 41.078 16.431 4374.007 4.641 73.083 1.704 0.75 351688. 0.1977
|
|
115.80 0.6628 0.8270 0.0308 0.0247 5.247 36.746 14.053 3912.759 4.152 62.508 1.629 0.75 352771. 0.1748
|
|
120.83 0.6916 0.8190 0.0256 0.0216 4.587 32.121 11.658 3420.274 3.629 51.854 1.546 0.75 353892. 0.1511
|
|
125.87 0.7204 0.7991 0.0203 0.0183 3.889 27.238 9.260 2900.299 3.077 41.187 1.448 0.75 355052. 0.1261
|
|
130.90 0.7492 0.7591 0.0151 0.0149 3.161 22.139 6.875 2357.427 2.501 30.579 1.323 0.75 356251. 0.0993
|
|
135.94 0.7781 0.6798 0.0099 0.0113 2.410 16.879 4.520 1797.248 1.907 20.106 1.141 0.75 357487. 0.0694
|
|
140.97 0.8069 0.5063 0.0049 0.0077 1.645 11.518 2.215 1226.400 1.301 9.852 0.819 0.76 358762. 0.0349
|
|
146.01 0.8357 -0.0112 -0.0001 0.0041 0.873 6.116 -0.025 651.262 0.691 -0.112 -0.018 0.76 360059. 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 0.1015 0.0397 11.578 72.977 57.110 8634.064 8.245 254.025 3.000 0.81 375236. 0.6489
|
|
5.58 0.0287 0.0716 0.1008 0.0405 11.797 74.353 56.736 8796.849 8.400 252.363 2.925 0.81 375515. 0.6307
|
|
11.16 0.0575 0.1394 0.1000 0.0412 12.016 75.734 56.300 8960.217 8.556 250.423 2.850 0.81 375827. 0.6121
|
|
16.74 0.0862 0.2036 0.0991 0.0420 12.231 77.092 55.792 9120.859 8.710 248.161 2.774 0.81 376172. 0.5932
|
|
22.32 0.1150 0.2642 0.0981 0.0427 12.438 78.395 55.199 9275.096 8.857 245.525 2.699 0.81 376553. 0.5740
|
|
27.90 0.1437 0.3211 0.0969 0.0434 12.631 79.611 54.510 9418.868 8.994 242.459 2.625 0.81 376972. 0.5547
|
|
33.48 0.1725 0.3745 0.0954 0.0439 12.804 80.700 53.711 9547.754 9.117 238.909 2.552 0.81 377431. 0.5352
|
|
39.06 0.2012 0.4246 0.0938 0.0445 12.950 81.624 52.792 9657.141 9.222 234.819 2.480 0.81 377931. 0.5157
|
|
44.64 0.2300 0.4715 0.0919 0.0448 13.065 82.345 51.740 9742.376 9.303 230.141 2.409 0.82 378472. 0.4959
|
|
50.23 0.2587 0.5152 0.0898 0.0451 13.140 82.822 50.546 9798.766 9.357 224.826 2.340 0.82 379057. 0.4761
|
|
55.81 0.2875 0.5559 0.0874 0.0452 13.171 83.016 49.199 9821.738 9.379 218.838 2.272 0.82 379686. 0.4561
|
|
61.39 0.3162 0.5936 0.0847 0.0451 13.151 82.890 47.695 9806.849 9.365 212.146 2.206 0.82 380360. 0.4360
|
|
66.97 0.3450 0.6286 0.0818 0.0449 13.075 82.408 46.027 9749.811 9.310 204.728 2.141 0.82 381077. 0.4158
|
|
72.55 0.3737 0.6609 0.0785 0.0444 12.936 81.534 44.193 9646.469 9.212 196.570 2.078 0.82 381840. 0.3954
|
|
78.13 0.4025 0.6905 0.0750 0.0437 12.730 80.235 42.191 9492.711 9.065 187.665 2.016 0.82 382647. 0.3748
|
|
83.71 0.4312 0.7175 0.0711 0.0427 12.451 78.474 40.021 9284.377 8.866 178.012 1.955 0.82 383500. 0.3540
|
|
89.29 0.4600 0.7420 0.0670 0.0415 12.093 76.221 37.686 9017.844 8.611 167.627 1.895 0.82 384396. 0.3331
|
|
94.87 0.4887 0.7639 0.0625 0.0400 11.656 73.464 35.198 8691.637 8.300 156.563 1.837 0.82 385337. 0.3119
|
|
100.45 0.5174 0.7832 0.0579 0.0382 11.141 70.220 32.575 8307.859 7.933 144.893 1.778 0.82 386322. 0.2905
|
|
106.03 0.5462 0.7995 0.0530 0.0362 10.551 66.499 29.834 7867.573 7.513 132.704 1.720 0.83 387350. 0.2689
|
|
111.61 0.5749 0.8125 0.0480 0.0339 9.888 62.322 26.995 7373.410 7.041 120.076 1.661 0.83 388422. 0.2470
|
|
117.19 0.6037 0.8217 0.0428 0.0314 9.156 57.711 24.076 6827.908 6.520 107.089 1.599 0.83 389536. 0.2246
|
|
122.77 0.6324 0.8260 0.0375 0.0287 8.360 52.692 21.093 6234.128 5.953 93.820 1.535 0.83 390694. 0.2017
|
|
128.35 0.6612 0.8237 0.0321 0.0258 7.506 47.309 18.064 5597.214 5.345 80.346 1.464 0.83 391894. 0.1781
|
|
133.93 0.6899 0.8117 0.0267 0.0227 6.602 41.614 15.006 4923.455 4.702 66.747 1.382 0.83 393136. 0.1533
|
|
139.51 0.7187 0.7848 0.0212 0.0194 5.660 35.673 11.939 4220.511 4.030 53.104 1.283 0.83 394420. 0.1269
|
|
145.10 0.7474 0.7327 0.0158 0.0161 4.690 29.560 8.882 3497.342 3.340 39.508 1.152 0.84 395747. 0.0983
|
|
150.68 0.7762 0.6350 0.0104 0.0127 3.707 23.364 5.858 2764.254 2.640 26.058 0.961 0.84 397116. 0.0666
|
|
156.26 0.8049 0.4421 0.0051 0.0094 2.726 17.181 2.892 2032.716 1.941 12.864 0.645 0.84 398526. 0.0314
|
|
161.84 0.8337 0.0018 0.0000 0.0060 1.762 11.103 0.008 1313.574 1.254 0.033 0.003 0.84 399967. 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 0.1019 0.0473 18.361 105.206 69.412 13691.786 11.886 308.744 2.299 0.89 412736. 0.5483
|
|
6.17 0.0289 0.0609 0.1014 0.0481 18.645 106.834 69.049 13903.654 12.070 307.128 2.253 0.89 413040. 0.5357
|
|
12.33 0.0577 0.1192 0.1008 0.0488 18.924 108.432 68.617 14111.607 12.251 305.210 2.205 0.89 413379. 0.5229
|
|
18.50 0.0866 0.1751 0.1000 0.0495 19.189 109.952 68.105 14309.533 12.422 302.930 2.159 0.89 413757. 0.5099
|
|
24.66 0.1155 0.2284 0.0991 0.0501 19.432 111.345 67.495 14490.712 12.580 300.217 2.113 0.90 414175. 0.4968
|
|
30.83 0.1444 0.2794 0.0980 0.0507 19.643 112.552 66.771 14647.807 12.716 296.996 2.068 0.90 414635. 0.4836
|
|
37.00 0.1732 0.3282 0.0968 0.0511 19.811 113.515 65.915 14773.196 12.825 293.189 2.024 0.90 415140. 0.4703
|
|
43.16 0.2021 0.3749 0.0953 0.0514 19.927 114.177 64.909 14859.390 12.900 288.715 1.981 0.90 415691. 0.4569
|
|
49.33 0.2310 0.4196 0.0936 0.0515 19.980 114.485 63.736 14899.354 12.934 283.498 1.940 0.90 416290. 0.4434
|
|
55.49 0.2599 0.4624 0.0916 0.0515 19.964 114.389 62.381 14886.859 12.924 277.469 1.901 0.90 416937. 0.4297
|
|
61.66 0.2887 0.5033 0.0893 0.0512 19.869 113.849 60.829 14816.646 12.863 270.566 1.862 0.90 417635. 0.4157
|
|
67.83 0.3176 0.5425 0.0867 0.0508 19.692 112.833 59.070 14684.422 12.748 262.742 1.825 0.90 418382. 0.4014
|
|
73.99 0.3465 0.5799 0.0838 0.0501 19.427 111.314 57.095 14486.716 12.576 253.960 1.788 0.90 419179. 0.3866
|
|
80.16 0.3754 0.6153 0.0806 0.0492 19.070 109.270 54.900 14220.707 12.345 244.195 1.751 0.90 420027. 0.3714
|
|
86.32 0.4042 0.6488 0.0771 0.0480 18.619 106.682 52.481 13883.964 12.053 233.436 1.714 0.90 420926. 0.3555
|
|
92.49 0.4331 0.6802 0.0732 0.0466 18.069 103.533 49.838 13474.029 11.697 221.679 1.678 0.90 421874. 0.3390
|
|
98.65 0.4620 0.7095 0.0690 0.0449 17.418 99.804 46.974 12988.763 11.276 208.942 1.640 0.90 422872. 0.3218
|
|
104.82 0.4909 0.7363 0.0645 0.0430 16.668 95.504 43.907 12429.180 10.790 195.299 1.602 0.91 423919. 0.3039
|
|
110.99 0.5197 0.7604 0.0597 0.0408 15.823 90.666 40.658 11799.537 10.243 180.849 1.563 0.91 425015. 0.2852
|
|
117.15 0.5486 0.7805 0.0547 0.0384 14.909 85.426 37.251 11117.590 9.651 165.692 1.520 0.91 426159. 0.2655
|
|
123.32 0.5775 0.7960 0.0495 0.0359 13.925 79.791 33.710 10384.226 9.015 149.941 1.472 0.91 427351. 0.2447
|
|
129.48 0.6064 0.8050 0.0441 0.0332 12.891 73.864 30.057 9612.945 8.345 133.693 1.418 0.91 428590. 0.2225
|
|
135.65 0.6352 0.8034 0.0386 0.0306 11.847 67.880 26.311 8834.146 7.669 117.032 1.351 0.91 429876. 0.1983
|
|
141.82 0.6641 0.7901 0.0330 0.0278 10.770 61.709 22.502 8030.984 6.972 100.087 1.271 0.91 431209. 0.1725
|
|
147.98 0.6930 0.7623 0.0274 0.0249 9.658 55.337 18.656 7201.727 6.252 82.982 1.175 0.92 432588. 0.1453
|
|
154.15 0.7219 0.7134 0.0217 0.0220 8.530 48.873 14.803 6360.465 5.522 65.844 1.056 0.92 434014. 0.1163
|
|
160.31 0.7507 0.6334 0.0161 0.0191 7.405 42.432 10.973 5522.237 4.794 48.809 0.901 0.92 435487. 0.0855
|
|
166.48 0.7796 0.5070 0.0106 0.0163 6.306 36.130 7.201 4702.023 4.082 32.031 0.695 0.92 437005. 0.0534
|
|
172.65 0.8085 0.3092 0.0052 0.0135 5.249 30.075 3.525 3914.048 3.398 15.681 0.409 0.92 438570. 0.0220
|
|
178.81 0.8374 -0.0027 0.0000 0.0109 4.243 24.313 -0.024 3164.225 2.747 -0.107 -0.003 0.93 440179. 0.0000
|
|
|
|
|
|
|