427 lines
76 KiB
Plaintext
427 lines
76 KiB
Plaintext
20x15C (20x15C.dat)
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v2022-0915
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Simulation Date: 08/22/2023
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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 0.0904 0.0391 0.010 0.635 0.461 7.513 0.072 2.050 27.817 0.08 33408. 0.5540
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0.61 0.0321 0.0720 0.0899 0.0401 0.010 0.651 0.458 7.707 0.074 2.039 26.980 0.08 33434. 0.5359
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1.22 0.0642 0.1394 0.0894 0.0412 0.011 0.669 0.456 7.909 0.076 2.027 26.130 0.08 33463. 0.5175
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1.83 0.0964 0.2022 0.0887 0.0423 0.011 0.686 0.452 8.118 0.078 2.012 25.273 0.08 33496. 0.4987
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2.43 0.1285 0.2605 0.0879 0.0434 0.011 0.704 0.448 8.330 0.080 1.995 24.417 0.08 33533. 0.4797
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3.04 0.1606 0.3143 0.0870 0.0445 0.011 0.722 0.444 8.540 0.082 1.974 23.566 0.08 33574. 0.4606
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3.65 0.1927 0.3637 0.0859 0.0455 0.012 0.739 0.438 8.744 0.084 1.949 22.728 0.08 33620. 0.4414
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4.26 0.2249 0.4090 0.0846 0.0465 0.012 0.755 0.432 8.936 0.085 1.920 21.906 0.08 33670. 0.4222
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4.87 0.2570 0.4503 0.0831 0.0474 0.012 0.770 0.424 9.109 0.087 1.885 21.105 0.08 33725. 0.4031
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5.48 0.2891 0.4879 0.0814 0.0482 0.012 0.782 0.415 9.256 0.088 1.845 20.327 0.08 33785. 0.3841
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6.08 0.3212 0.5221 0.0793 0.0488 0.013 0.792 0.404 9.370 0.089 1.799 19.574 0.08 33850. 0.3652
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6.69 0.3533 0.5529 0.0769 0.0492 0.013 0.798 0.392 9.442 0.090 1.745 18.846 0.08 33920. 0.3463
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7.30 0.3855 0.5807 0.0743 0.0493 0.013 0.800 0.379 9.466 0.090 1.684 18.143 0.08 33995. 0.3275
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7.91 0.4176 0.6055 0.0713 0.0491 0.013 0.798 0.363 9.437 0.090 1.616 17.463 0.08 34076. 0.3088
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8.52 0.4497 0.6275 0.0679 0.0487 0.013 0.790 0.346 9.350 0.089 1.541 16.804 0.08 34161. 0.2902
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9.13 0.4818 0.6466 0.0643 0.0479 0.012 0.778 0.328 9.207 0.088 1.459 16.162 0.08 34252. 0.2716
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9.73 0.5140 0.6628 0.0605 0.0469 0.012 0.761 0.308 9.009 0.086 1.372 15.532 0.08 34348. 0.2531
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10.34 0.5461 0.6760 0.0565 0.0456 0.012 0.740 0.288 8.757 0.084 1.280 14.908 0.08 34449. 0.2347
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10.95 0.5782 0.6858 0.0522 0.0440 0.011 0.715 0.266 8.455 0.081 1.184 14.286 0.08 34555. 0.2163
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11.56 0.6103 0.6920 0.0478 0.0422 0.011 0.685 0.244 8.103 0.077 1.085 13.656 0.08 34665. 0.1979
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12.17 0.6424 0.6941 0.0433 0.0401 0.010 0.651 0.221 7.703 0.074 0.983 13.012 0.08 34781. 0.1794
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12.78 0.6746 0.6912 0.0387 0.0378 0.010 0.613 0.197 7.257 0.069 0.878 12.341 0.08 34902. 0.1609
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13.38 0.7067 0.6823 0.0340 0.0352 0.009 0.572 0.173 6.765 0.065 0.771 11.628 0.08 35027. 0.1421
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13.99 0.7388 0.6658 0.0292 0.0324 0.008 0.527 0.149 6.230 0.059 0.663 10.853 0.08 35157. 0.1229
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14.60 0.7709 0.6390 0.0244 0.0294 0.008 0.478 0.124 5.651 0.054 0.553 9.983 0.08 35293. 0.1033
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15.21 0.8031 0.5979 0.0195 0.0262 0.007 0.425 0.099 5.032 0.048 0.442 8.968 0.08 35433. 0.0830
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15.82 0.8352 0.5356 0.0146 0.0228 0.006 0.370 0.074 4.373 0.042 0.331 7.723 0.08 35577. 0.0618
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16.43 0.8673 0.4390 0.0097 0.0192 0.005 0.311 0.049 3.677 0.035 0.220 6.096 0.08 35727. 0.0398
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17.03 0.8994 0.2813 0.0048 0.0154 0.004 0.249 0.024 2.949 0.028 0.109 3.767 0.08 35880. 0.0173
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17.64 0.9316 -0.0036 0.0000 0.0114 0.003 0.185 0.000 2.190 0.021 -0.001 -0.047 0.08 36038. 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 0.0907 0.0354 0.073 2.300 1.850 54.433 0.260 8.228 15.414 0.16 66816. 0.6150
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1.24 0.0327 0.0808 0.0903 0.0365 0.075 2.369 1.841 56.047 0.268 8.188 14.896 0.16 66868. 0.5929
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2.47 0.0653 0.1559 0.0897 0.0376 0.077 2.440 1.830 57.743 0.276 8.139 14.374 0.16 66928. 0.5704
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3.71 0.0980 0.2253 0.0891 0.0387 0.080 2.514 1.817 59.498 0.284 8.082 13.851 0.16 66995. 0.5477
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4.95 0.1306 0.2892 0.0883 0.0399 0.082 2.590 1.801 61.285 0.293 8.012 13.331 0.16 67070. 0.5249
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6.19 0.1633 0.3476 0.0874 0.0411 0.085 2.665 1.783 63.067 0.301 7.929 12.820 0.16 67155. 0.5022
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7.42 0.1959 0.4009 0.0863 0.0422 0.087 2.739 1.760 64.803 0.309 7.829 12.320 0.16 67248. 0.4795
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8.66 0.2286 0.4492 0.0850 0.0433 0.089 2.808 1.734 66.442 0.317 7.711 11.834 0.16 67351. 0.4571
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9.90 0.2613 0.4930 0.0834 0.0442 0.091 2.871 1.702 67.928 0.324 7.570 11.364 0.16 67465. 0.4350
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11.13 0.2939 0.5326 0.0816 0.0450 0.093 2.924 1.665 69.199 0.330 7.406 10.913 0.16 67588. 0.4131
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12.37 0.3266 0.5683 0.0795 0.0457 0.094 2.966 1.622 70.189 0.335 7.214 10.480 0.16 67722. 0.3916
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13.61 0.3592 0.6005 0.0771 0.0461 0.095 2.993 1.572 70.832 0.338 6.993 10.067 0.16 67866. 0.3703
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14.84 0.3919 0.6294 0.0743 0.0463 0.095 3.003 1.515 71.068 0.339 6.741 9.672 0.16 68022. 0.3493
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16.08 0.4245 0.6553 0.0712 0.0461 0.095 2.994 1.452 70.849 0.338 6.458 9.295 0.16 68187. 0.3286
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17.32 0.4572 0.6783 0.0678 0.0457 0.094 2.965 1.382 70.155 0.335 6.146 8.934 0.16 68364. 0.3081
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18.56 0.4899 0.6985 0.0640 0.0449 0.093 2.915 1.306 68.983 0.329 5.809 8.587 0.16 68551. 0.2879
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19.79 0.5225 0.7160 0.0601 0.0438 0.090 2.846 1.225 67.345 0.322 5.450 8.251 0.16 68748. 0.2680
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21.03 0.5552 0.7306 0.0559 0.0425 0.088 2.758 1.140 65.255 0.312 5.071 7.924 0.16 68956. 0.2482
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22.27 0.5878 0.7421 0.0516 0.0408 0.084 2.651 1.051 62.728 0.300 4.677 7.602 0.16 69174. 0.2287
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23.50 0.6205 0.7503 0.0471 0.0389 0.080 2.526 0.960 59.777 0.285 4.269 7.282 0.16 69403. 0.2093
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24.74 0.6531 0.7547 0.0424 0.0367 0.076 2.384 0.865 56.413 0.269 3.850 6.959 0.16 69641. 0.1899
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25.98 0.6858 0.7546 0.0377 0.0343 0.071 2.225 0.769 52.646 0.251 3.421 6.626 0.16 69890. 0.1705
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27.21 0.7185 0.7489 0.0329 0.0316 0.065 2.049 0.671 48.485 0.231 2.985 6.277 0.16 70149. 0.1509
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28.45 0.7511 0.7358 0.0280 0.0286 0.059 1.857 0.572 43.940 0.210 2.542 5.899 0.16 70417. 0.1308
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29.69 0.7838 0.7124 0.0231 0.0254 0.052 1.649 0.471 39.023 0.186 2.095 5.474 0.16 70696. 0.1102
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30.93 0.8164 0.6736 0.0181 0.0220 0.045 1.426 0.370 33.749 0.161 1.644 4.969 0.16 70984. 0.0886
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32.16 0.8491 0.6096 0.0131 0.0183 0.038 1.189 0.268 28.137 0.134 1.193 4.324 0.16 71283. 0.0657
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33.40 0.8817 0.4991 0.0082 0.0145 0.030 0.939 0.167 22.213 0.106 0.742 3.408 0.16 71590. 0.0409
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34.64 0.9144 0.2856 0.0033 0.0104 0.021 0.677 0.066 16.010 0.076 0.295 1.881 0.17 71907. 0.0142
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35.87 0.9470
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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 0.0909 0.0340 0.236 4.964 4.173 176.176 0.561 18.563 10.745 0.24 100222. 0.6440
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1.84 0.0324 0.0836 0.0905 0.0350 0.244 5.118 4.154 181.645 0.578 18.478 10.373 0.24 100300. 0.6203
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3.68 0.0647 0.1612 0.0900 0.0361 0.251 5.280 4.131 187.402 0.597 18.375 9.999 0.24 100389. 0.5962
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5.52 0.0971 0.2328 0.0894 0.0373 0.259 5.448 4.103 193.375 0.616 18.252 9.625 0.24 100488. 0.5720
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7.36 0.1295 0.2984 0.0887 0.0385 0.267 5.620 4.070 199.474 0.635 18.104 9.255 0.24 100600. 0.5478
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9.19 0.1618 0.3584 0.0878 0.0397 0.276 5.792 4.030 205.583 0.654 17.925 8.891 0.24 100725. 0.5236
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11.03 0.1942 0.4129 0.0868 0.0408 0.284 5.961 3.982 211.563 0.673 17.710 8.536 0.24 100863. 0.4997
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12.87 0.2265 0.4623 0.0855 0.0419 0.291 6.121 3.924 217.248 0.692 17.454 8.193 0.24 101015. 0.4761
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14.71 0.2589 0.5070 0.0840 0.0429 0.298 6.267 3.856 222.453 0.708 17.150 7.861 0.24 101183. 0.4529
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16.55 0.2913 0.5474 0.0823 0.0438 0.304 6.395 3.775 226.971 0.722 16.792 7.544 0.24 101365. 0.4300
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18.39 0.3236 0.5837 0.0802 0.0445 0.309 6.496 3.681 230.582 0.734 16.374 7.241 0.24 101563. 0.4076
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20.23 0.3560 0.6165 0.0778 0.0450 0.313 6.566 3.572 233.063 0.742 15.890 6.952 0.24 101776. 0.3855
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22.07 0.3884 0.6460 0.0751 0.0452 0.314 6.599 3.448 234.205 0.745 15.338 6.678 0.24 102005. 0.3638
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23.91 0.4207 0.6725 0.0721 0.0451 0.314 6.588 3.308 233.843 0.744 14.716 6.417 0.24 102250. 0.3424
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25.74 0.4531 0.6963 0.0687 0.0447 0.311 6.533 3.154 231.887 0.738 14.029 6.169 0.24 102511. 0.3214
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27.58 0.4855 0.7174 0.0651 0.0440 0.306 6.433 2.986 228.321 0.727 13.283 5.932 0.24 102787. 0.3008
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29.42 0.5178 0.7359 0.0612 0.0430 0.299 6.288 2.807 223.171 0.710 12.486 5.705 0.24 103078. 0.2804
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31.26 0.5502 0.7518 0.0571 0.0418 0.290 6.099 2.618 216.482 0.689 11.646 5.486 0.24 103385. 0.2604
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33.10 0.5826 0.7650 0.0528 0.0402 0.279 5.869 2.421 208.302 0.663 10.769 5.272 0.24 103707. 0.2407
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34.94 0.6149 0.7753 0.0483 0.0383 0.266 5.597 2.217 198.671 0.632 9.861 5.061 0.24 104044. 0.2211
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36.78 0.6473 0.7823 0.0437 0.0362 0.252 5.286 2.007 187.627 0.597 8.927 4.852 0.24 104396. 0.2017
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38.62 0.6796 0.7855 0.0391 0.0338 0.235 4.936 1.792 175.202 0.558 7.972 4.640 0.24 104763. 0.1822
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40.46 0.7120 0.7840 0.0343 0.0311 0.216 4.548 1.573 161.427 0.514 6.998 4.420 0.24 105145. 0.1627
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42.29 0.7444 0.7765 0.0294 0.0282 0.196 4.123 1.351 146.331 0.466 6.010 4.188 0.24 105541. 0.1428
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44.13 0.7767 0.7607 0.0245 0.0251 0.174 3.661 1.126 129.954 0.414 5.011 3.932 0.25 105952. 0.1224
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45.97 0.8091 0.7325 0.0196 0.0217 0.151 3.165 0.900 112.341 0.358 4.004 3.635 0.25 106378. 0.1012
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47.81 0.8415 0.6840 0.0147 0.0180 0.125 2.636 0.673 93.556 0.298 2.994 3.263 0.25 106818. 0.0786
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49.65 0.8738 0.5981 0.0097 0.0142 0.099 2.076 0.446 73.680 0.235 1.985 2.748 0.25 107272. 0.0539
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51.49 0.9062 0.4283 0.0048 0.0102 0.071 1.488 0.221 52.819 0.168 0.983 1.897 0.25 107740. 0.0262
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53.33 0.9386 -0.0089 -0.0001 0.0060 0.042 0.874 -0.003 31.009 0.099 -0.012 -0.038 0.25 108215. 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 0.0912 0.0332 0.548 8.634 7.441 408.594 0.975 33.097 8.260 0.32 133628. 0.6610
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2.45 0.0324 0.0858 0.0908 0.0343 0.566 8.911 7.409 421.710 1.007 32.954 7.968 0.32 133732. 0.6363
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4.91 0.0648 0.1652 0.0903 0.0354 0.584 9.203 7.370 435.548 1.040 32.782 7.675 0.32 133849. 0.6113
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7.36 0.0972 0.2383 0.0898 0.0366 0.603 9.508 7.323 449.942 1.074 32.574 7.382 0.32 133982. 0.5861
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9.82 0.1296 0.3053 0.0891 0.0378 0.623 9.819 7.266 464.680 1.109 32.321 7.093 0.32 134132. 0.5609
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12.27 0.1620 0.3664 0.0882 0.0390 0.643 10.132 7.198 479.485 1.145 32.015 6.809 0.32 134298. 0.5359
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14.73 0.1944 0.4218 0.0872 0.0402 0.662 10.439 7.115 494.022 1.179 31.645 6.532 0.32 134483. 0.5112
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17.18 0.2268 0.4719 0.0860 0.0413 0.681 10.732 7.015 507.893 1.213 31.201 6.264 0.32 134686. 0.4868
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19.64 0.2592 0.5172 0.0845 0.0424 0.698 11.002 6.895 520.644 1.243 30.671 6.007 0.32 134910. 0.4628
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22.09 0.2916 0.5580 0.0828 0.0433 0.713 11.237 6.754 531.773 1.270 30.043 5.761 0.32 135153. 0.4393
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24.55 0.3240 0.5947 0.0808 0.0440 0.725 11.426 6.589 540.745 1.291 29.306 5.526 0.32 135418. 0.4162
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27.00 0.3564 0.6279 0.0784 0.0445 0.734 11.559 6.397 547.011 1.306 28.452 5.304 0.32 135703. 0.3935
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29.46 0.3888 0.6577 0.0757 0.0448 0.738 11.623 6.176 550.062 1.313 27.472 5.093 0.32 136009. 0.3713
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31.91 0.4212 0.6845 0.0727 0.0447 0.737 11.611 5.928 549.489 1.312 26.367 4.893 0.32 136336. 0.3495
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34.37 0.4536 0.7087 0.0693 0.0444 0.731 11.518 5.652 545.066 1.301 25.142 4.704 0.32 136685. 0.3281
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36.82 0.4860 0.7302 0.0656 0.0437 0.720 11.342 5.353 536.747 1.281 23.810 4.523 0.32 137054. 0.3070
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39.28 0.5184 0.7493 0.0617 0.0427 0.703 11.085 5.033 524.589 1.252 22.386 4.351 0.32 137443. 0.2864
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41.73 0.5509 0.7658 0.0575 0.0414 0.682 10.749 4.695 508.698 1.214 20.882 4.186 0.32 137854. 0.2661
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44.19 0.5833 0.7798 0.0532 0.0398 0.656 10.337 4.342 489.183 1.168 19.312 4.026 0.32 138284. 0.2461
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46.64 0.6157 0.7910 0.0487 0.0379 0.625 9.850 3.976 466.147 1.113 17.685 3.869 0.32 138735. 0.2263
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49.10 0.6481 0.7993 0.0441 0.0358 0.590 9.291 3.600 439.677 1.050 16.012 3.714 0.32 139205. 0.2067
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51.55 0.6805 0.8040 0.0394 0.0333 0.550 8.660 3.215 409.850 0.978 14.299 3.558 0.32 139696. 0.1871
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54.00 0.7129 0.8045 0.0346 0.0307 0.505 7.961 2.822 376.738 0.899 12.553 3.398 0.33 140206. 0.1675
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56.46 0.7453 0.7994 0.0297 0.0277 0.457 7.193 2.424 340.417 0.813 10.782 3.230 0.33 140736. 0.1475
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58.91 0.7777 0.7867 0.0248 0.0245 0.404 6.360 2.021 300.978 0.719 8.990 3.046 0.33 141286. 0.1270
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61.37 0.8101 0.7625 0.0198 0.0210 0.347 5.463 1.615 258.533 0.617 7.186 2.834 0.33 141855. 0.1057
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63.82 0.8425 0.7192 0.0148 0.0174 0.286 4.506 1.208 213.237 0.509 5.375 2.570 0.33 142443. 0.0829
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66.28 0.8749 0.6392 0.0098 0.0134 0.222 3.493 0.802 165.290 0.395 3.566 2.200 0.33 143050. 0.0578
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68.73 0.9073 0.4728 0.0049 0.0094 0.154 2.429 0.398 114.950 0.274 1.769 1.569 0.33 143675. 0.0290
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71.19 0.9397 -0.0077 0.0000 0.0051 0.083 1.315 -0.003 62.252 0.149 -0.015 -0.025 0.33 144307. 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 0.0915 0.0329 1.058 13.338 11.664 789.010 1.507 51.881 6.705 0.40 167032. 0.6718
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3.07 0.0324 0.0871 0.0911 0.0339 1.093 13.775 11.618 814.897 1.556 51.675 6.466 0.40 167161. 0.6466
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6.14 0.0649 0.1677 0.0907 0.0351 1.130 14.238 11.562 842.289 1.609 51.426 6.226 0.40 167309. 0.6211
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9.22 0.0973 0.2418 0.0902 0.0363 1.168 14.722 11.493 870.870 1.663 51.122 5.986 0.40 167475. 0.5954
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12.29 0.1298 0.3097 0.0895 0.0375 1.207 15.218 11.410 900.227 1.719 50.751 5.749 0.40 167661. 0.5697
|
|
15.36 0.1622 0.3714 0.0887 0.0387 1.247 15.718 11.308 929.817 1.776 50.297 5.516 0.40 167870. 0.5442
|
|
18.43 0.1946 0.4274 0.0877 0.0400 1.286 16.211 11.183 958.972 1.832 49.743 5.289 0.40 168101. 0.5190
|
|
21.50 0.2271 0.4780 0.0865 0.0411 1.323 16.683 11.033 986.897 1.885 49.073 5.070 0.40 168356. 0.4941
|
|
24.58 0.2595 0.5236 0.0851 0.0422 1.358 17.119 10.851 1012.676 1.934 48.267 4.860 0.40 168635. 0.4697
|
|
27.65 0.2920 0.5647 0.0834 0.0431 1.388 17.501 10.635 1035.297 1.977 47.305 4.659 0.40 168940. 0.4458
|
|
30.72 0.3244 0.6018 0.0814 0.0439 1.413 17.812 10.380 1053.674 2.012 46.171 4.468 0.40 169271. 0.4224
|
|
33.79 0.3568 0.6351 0.0791 0.0444 1.430 18.032 10.083 1066.700 2.037 44.847 4.287 0.40 169629. 0.3994
|
|
36.86 0.3893 0.6652 0.0764 0.0447 1.439 18.144 9.740 1073.334 2.050 43.323 4.116 0.40 170013. 0.3769
|
|
39.94 0.4217 0.6923 0.0734 0.0447 1.439 18.134 9.352 1072.744 2.049 41.597 3.954 0.40 170423. 0.3548
|
|
43.01 0.4542 0.7167 0.0700 0.0443 1.427 17.994 8.921 1064.462 2.033 39.678 3.801 0.40 170859. 0.3331
|
|
46.08 0.4866 0.7386 0.0663 0.0437 1.406 17.722 8.450 1048.377 2.002 37.588 3.656 0.40 171322. 0.3118
|
|
49.15 0.5190 0.7580 0.0623 0.0427 1.374 17.320 7.947 1024.603 1.957 35.347 3.518 0.40 171811. 0.2909
|
|
52.22 0.5515 0.7751 0.0582 0.0414 1.332 16.792 7.414 993.345 1.897 32.979 3.385 0.40 172325. 0.2704
|
|
55.30 0.5839 0.7897 0.0538 0.0398 1.280 16.141 6.858 954.829 1.824 30.503 3.258 0.40 172864. 0.2503
|
|
58.37 0.6164 0.8017 0.0493 0.0379 1.219 15.371 6.281 909.257 1.737 27.937 3.133 0.40 173429. 0.2304
|
|
61.44 0.6488 0.8109 0.0446 0.0357 1.149 14.484 5.687 856.809 1.636 25.295 3.010 0.41 174019. 0.2106
|
|
64.51 0.6812 0.8168 0.0398 0.0332 1.070 13.484 5.079 797.637 1.523 22.590 2.888 0.41 174633. 0.1909
|
|
67.58 0.7137 0.8187 0.0350 0.0305 0.981 12.372 4.459 731.889 1.398 19.832 2.763 0.41 175273. 0.1712
|
|
70.66 0.7461 0.8155 0.0300 0.0275 0.885 11.152 3.829 659.715 1.260 17.033 2.633 0.41 175937. 0.1511
|
|
73.73 0.7786 0.8052 0.0250 0.0242 0.780 9.827 3.193 581.297 1.110 14.201 2.491 0.41 176626. 0.1306
|
|
76.80 0.8110 0.7841 0.0200 0.0207 0.666 8.399 2.551 496.863 0.949 11.347 2.329 0.41 177338. 0.1091
|
|
79.87 0.8434 0.7448 0.0150 0.0169 0.545 6.875 1.907 406.717 0.777 8.484 2.127 0.41 178075. 0.0862
|
|
82.94 0.8759 0.6698 0.0099 0.0130 0.417 5.262 1.264 311.269 0.594 5.623 1.842 0.41 178836. 0.0608
|
|
86.01 0.9083 0.5067 0.0049 0.0088 0.283 3.567 0.625 211.038 0.403 2.781 1.344 0.41 179619. 0.0312
|
|
89.09 0.9408 -0.0167 -0.0001 0.0044 0.142 1.791 -0.010 105.937 0.202 -0.045 -0.043 0.41 180407. 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 0.0918 0.0327 1.820 19.117 16.857 1357.070 2.160 74.980 5.634 0.48 200434. 0.6786
|
|
3.71 0.0327 0.0884 0.0915 0.0338 1.881 19.757 16.797 1402.506 2.232 74.712 5.432 0.48 200590. 0.6531
|
|
7.42 0.0653 0.1701 0.0911 0.0350 1.946 20.437 16.723 1450.766 2.309 74.385 5.228 0.48 200768. 0.6273
|
|
11.13 0.0980 0.2452 0.0906 0.0362 2.013 21.149 16.633 1501.313 2.389 73.982 5.025 0.48 200968. 0.6012
|
|
14.84 0.1306 0.3139 0.0900 0.0375 2.083 21.883 16.521 1553.432 2.472 73.484 4.824 0.48 201194. 0.5752
|
|
18.55 0.1633 0.3763 0.0892 0.0387 2.154 22.626 16.382 1606.167 2.556 72.869 4.626 0.48 201446. 0.5494
|
|
22.26 0.1959 0.4328 0.0883 0.0400 2.224 23.361 16.212 1658.312 2.639 72.109 4.434 0.48 201726. 0.5238
|
|
25.98 0.2286 0.4838 0.0872 0.0412 2.291 24.067 16.002 1708.419 2.719 71.178 4.248 0.48 202035. 0.4986
|
|
29.69 0.2612 0.5297 0.0858 0.0423 2.353 24.720 15.748 1754.814 2.793 70.045 4.070 0.48 202374. 0.4739
|
|
33.40 0.2939 0.5711 0.0841 0.0433 2.408 25.295 15.441 1795.632 2.858 68.682 3.900 0.48 202744. 0.4497
|
|
37.11 0.3265 0.6083 0.0821 0.0441 2.453 25.763 15.076 1828.871 2.911 67.058 3.739 0.48 203146. 0.4259
|
|
40.82 0.3592 0.6417 0.0798 0.0447 2.484 26.096 14.647 1852.500 2.948 65.150 3.586 0.48 203580. 0.4027
|
|
44.53 0.3919 0.6719 0.0771 0.0450 2.500 26.267 14.150 1864.616 2.968 62.941 3.442 0.48 204047. 0.3799
|
|
48.24 0.4245 0.6992 0.0740 0.0449 2.499 26.254 13.585 1863.707 2.966 60.426 3.306 0.48 204545. 0.3575
|
|
51.95 0.4572 0.7238 0.0706 0.0446 2.479 26.046 12.955 1848.939 2.943 57.623 3.178 0.48 205076. 0.3356
|
|
55.66 0.4898 0.7459 0.0668 0.0439 2.441 25.640 12.266 1820.128 2.897 54.561 3.057 0.48 205638. 0.3141
|
|
59.37 0.5225 0.7656 0.0628 0.0429 2.384 25.040 11.527 1777.495 2.829 51.274 2.941 0.48 206232. 0.2930
|
|
63.08 0.5551 0.7830 0.0585 0.0415 2.308 24.250 10.746 1721.426 2.740 47.797 2.831 0.48 206857. 0.2723
|
|
66.79 0.5878 0.7980 0.0541 0.0398 2.216 23.277 9.928 1652.332 2.630 44.159 2.725 0.48 207513. 0.2519
|
|
70.50 0.6204 0.8105 0.0495 0.0379 2.106 22.125 9.080 1570.591 2.500 40.387 2.622 0.49 208199. 0.2318
|
|
74.22 0.6531 0.8202 0.0447 0.0356 1.980 20.800 8.206 1476.528 2.350 36.501 2.521 0.49 208916. 0.2119
|
|
77.93 0.6858 0.8267 0.0398 0.0330 1.838 19.305 7.311 1370.427 2.181 32.522 2.420 0.49 209663. 0.1920
|
|
81.64 0.7184 0.8294 0.0349 0.0302 1.680 17.645 6.399 1252.554 1.994 28.464 2.317 0.49 210440. 0.1720
|
|
85.35 0.7511 0.8270 0.0298 0.0271 1.506 15.822 5.473 1123.188 1.788 24.345 2.210 0.49 211247. 0.1517
|
|
89.06 0.7837 0.8175 0.0247 0.0237 1.318 13.843 4.536 982.663 1.564 20.178 2.094 0.49 212084. 0.1308
|
|
92.77 0.8164 0.7971 0.0196 0.0200 1.115 11.712 3.592 831.409 1.323 15.979 1.960 0.49 212950. 0.1090
|
|
96.48 0.8490 0.7575 0.0144 0.0162 0.898 9.438 2.645 670.000 1.066 11.767 1.791 0.49 213845. 0.0855
|
|
100.19 0.8817 0.6785 0.0093 0.0120 0.669 7.032 1.700 499.205 0.795 7.562 1.545 0.49 214769. 0.0591
|
|
103.90 0.9143 0.4916 0.0041 0.0077 0.429 4.508 0.761 319.994 0.509 3.386 1.079 0.50 215720. 0.0276
|
|
107.61 0.9470
|
|
|
|
|
|
|
|
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 0.0922 0.0327 2.891 26.030 23.035 2155.750 2.941 102.459 4.847 0.56 233833. 0.6824
|
|
4.33 0.0326 0.0887 0.0919 0.0338 2.988 26.907 22.964 2228.423 3.040 102.143 4.674 0.56 234015. 0.6571
|
|
8.66 0.0653 0.1707 0.0916 0.0350 3.092 27.843 22.876 2305.947 3.146 101.754 4.500 0.56 234222. 0.6314
|
|
12.98 0.0979 0.2462 0.0911 0.0362 3.202 28.829 22.768 2387.528 3.257 101.271 4.325 0.56 234455. 0.6055
|
|
17.31 0.1306 0.3151 0.0906 0.0375 3.315 29.849 22.632 2472.075 3.372 100.666 4.152 0.56 234718. 0.5796
|
|
21.64 0.1632 0.3778 0.0899 0.0388 3.430 30.888 22.461 2558.096 3.490 99.908 3.983 0.56 235011. 0.5538
|
|
25.97 0.1959 0.4345 0.0890 0.0401 3.545 31.921 22.248 2643.652 3.606 98.959 3.817 0.56 235337. 0.5282
|
|
30.29 0.2285 0.4857 0.0880 0.0414 3.656 32.920 21.983 2726.380 3.719 97.779 3.657 0.56 235697. 0.5030
|
|
34.62 0.2611 0.5318 0.0867 0.0426 3.760 33.851 21.655 2803.513 3.825 96.323 3.504 0.56 236092. 0.4783
|
|
38.95 0.2938 0.5732 0.0851 0.0436 3.851 34.678 21.256 2871.942 3.918 94.549 3.357 0.56 236523. 0.4541
|
|
43.28 0.3264 0.6105 0.0832 0.0445 3.927 35.358 20.776 2928.322 3.995 92.412 3.218 0.56 236992. 0.4303
|
|
47.60 0.3591 0.6441 0.0809 0.0451 3.982 35.853 20.206 2969.244 4.051 89.876 3.087 0.56 237498. 0.4071
|
|
51.93 0.3917 0.6745 0.0782 0.0454 4.012 36.121 19.540 2991.499 4.081 86.914 2.963 0.56 238042. 0.3842
|
|
56.26 0.4244 0.7019 0.0752 0.0454 4.013 36.134 18.777 2992.515 4.082 83.521 2.846 0.56 238624. 0.3618
|
|
60.59 0.4570 0.7267 0.0717 0.0451 3.984 35.872 17.922 2970.825 4.053 79.715 2.736 0.56 239243. 0.3398
|
|
64.91 0.4896 0.7491 0.0680 0.0444 3.924 35.331 16.983 2926.065 3.992 75.538 2.632 0.56 239900. 0.3183
|
|
69.24 0.5223 0.7692 0.0639 0.0434 3.833 34.516 15.971 2858.583 3.900 71.040 2.534 0.56 240593. 0.2971
|
|
73.57 0.5549 0.7871 0.0596 0.0420 3.713 33.435 14.898 2769.025 3.777 66.267 2.440 0.56 241322. 0.2763
|
|
77.90 0.5876 0.8026 0.0551 0.0404 3.565 32.096 13.773 2658.098 3.626 61.264 2.350 0.56 242088. 0.2559
|
|
82.22 0.6202 0.8157 0.0505 0.0384 3.388 30.506 12.605 2526.453 3.447 56.067 2.263 0.57 242889. 0.2357
|
|
86.55 0.6528 0.8262 0.0456 0.0361 3.184 28.673 11.400 2374.647 3.239 50.708 2.178 0.57 243725. 0.2157
|
|
90.88 0.6855 0.8337 0.0407 0.0335 2.954 26.602 10.165 2203.167 3.006 45.214 2.093 0.57 244597. 0.1957
|
|
95.21 0.7181 0.8376 0.0356 0.0306 2.699 24.300 8.904 2012.457 2.745 39.607 2.007 0.57 245504. 0.1757
|
|
99.53 0.7508 0.8368 0.0305 0.0274 2.418 21.770 7.623 1802.981 2.460 33.909 1.918 0.57 246445. 0.1554
|
|
103.86 0.7834 0.8295 0.0253 0.0239 2.112 19.021 6.327 1575.278 2.149 28.142 1.822 0.57 247421. 0.1344
|
|
108.19 0.8161 0.8119 0.0201 0.0202 1.784 16.060 5.020 1330.039 1.814 22.327 1.712 0.57 248431. 0.1125
|
|
112.52 0.8487 0.7765 0.0148 0.0162 1.432 12.898 3.707 1068.194 1.457 16.490 1.574 0.58 249475. 0.0889
|
|
116.85 0.8813 0.7038 0.0096 0.0120 1.061 9.551 2.396 790.988 1.079 10.658 1.374 0.58 250552. 0.0624
|
|
121.17 0.9140 0.5271 0.0044 0.0076 0.671 6.037 1.094 500.009 0.682 4.865 0.992 0.58 251661. 0.0304
|
|
125.50 0.9466
|
|
|
|
|
|
|
|
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 0.0926 0.0329 4.344 34.221 30.212 3238.999 3.866 134.382 4.231 0.63 267231. 0.6822
|
|
4.92 0.0325 0.0881 0.0923 0.0340 4.489 35.363 30.135 3347.124 3.995 134.039 4.084 0.63 267437. 0.6577
|
|
9.84 0.0650 0.1698 0.0921 0.0352 4.644 36.588 30.040 3462.999 4.134 133.617 3.934 0.63 267671. 0.6327
|
|
14.76 0.0974 0.2450 0.0917 0.0365 4.808 37.883 29.921 3585.584 4.280 133.088 3.785 0.63 267935. 0.6074
|
|
19.69 0.1299 0.3138 0.0912 0.0378 4.980 39.233 29.770 3713.411 4.433 132.418 3.636 0.64 268232. 0.5821
|
|
24.61 0.1624 0.3765 0.0906 0.0391 5.155 40.617 29.578 3844.373 4.589 131.564 3.490 0.64 268564. 0.5568
|
|
29.53 0.1949 0.4332 0.0899 0.0404 5.331 42.004 29.334 3975.665 4.746 130.477 3.347 0.64 268933. 0.5318
|
|
34.45 0.2274 0.4845 0.0889 0.0417 5.503 43.358 29.024 4103.771 4.899 129.098 3.208 0.64 269340. 0.5070
|
|
39.37 0.2598 0.5307 0.0877 0.0430 5.665 44.633 28.635 4224.486 5.043 127.368 3.074 0.64 269787. 0.4827
|
|
44.29 0.2923 0.5722 0.0863 0.0441 5.811 45.780 28.152 4333.013 5.172 125.222 2.947 0.64 270276. 0.4587
|
|
49.21 0.3248 0.6097 0.0845 0.0450 5.933 46.742 27.562 4424.126 5.281 122.597 2.826 0.64 270806. 0.4352
|
|
54.14 0.3573 0.6434 0.0823 0.0457 6.024 47.464 26.853 4492.432 5.362 119.440 2.711 0.64 271380. 0.4122
|
|
59.06 0.3898 0.6739 0.0797 0.0461 6.079 47.890 26.014 4532.789 5.411 115.708 2.603 0.64 271996. 0.3895
|
|
63.98 0.4223 0.7016 0.0767 0.0462 6.090 47.977 25.042 4540.956 5.420 111.387 2.501 0.64 272656. 0.3672
|
|
68.90 0.4547 0.7266 0.0734 0.0459 6.054 47.695 23.943 4514.343 5.389 106.499 2.406 0.64 273358. 0.3453
|
|
73.82 0.4872 0.7493 0.0696 0.0453 5.970 47.038 22.728 4452.159 5.314 101.095 2.315 0.64 274103. 0.3239
|
|
78.74 0.5197 0.7699 0.0656 0.0443 5.840 46.010 21.412 4354.817 5.198 95.241 2.230 0.64 274889. 0.3028
|
|
83.66 0.5522 0.7882 0.0613 0.0430 5.664 44.621 20.010 4223.322 5.041 89.003 2.149 0.64 275716. 0.2820
|
|
88.58 0.5847 0.8043 0.0568 0.0413 5.443 42.883 18.534 4058.821 4.845 82.440 2.071 0.65 276584. 0.2616
|
|
93.51 0.6171 0.8182 0.0521 0.0393 5.180 40.807 16.998 3862.395 4.610 75.605 1.996 0.65 277493. 0.2414
|
|
98.43 0.6496 0.8297 0.0472 0.0370 4.875 38.405 15.410 3634.974 4.339 68.542 1.923 0.65 278441. 0.2214
|
|
103.35 0.6821 0.8384 0.0422 0.0344 4.529 35.683 13.778 3377.354 4.031 61.287 1.850 0.65 279430. 0.2015
|
|
108.27 0.7146 0.8438 0.0371 0.0314 4.144 32.649 12.112 3090.253 3.689 53.872 1.778 0.65 280457. 0.1815
|
|
113.19 0.7471 0.8450 0.0319 0.0282 3.721 29.312 10.415 2774.377 3.312 46.328 1.703 0.65 281524. 0.1612
|
|
118.11 0.7795 0.8403 0.0266 0.0247 3.259 25.679 8.696 2430.533 2.901 38.681 1.623 0.65 282630. 0.1404
|
|
123.03 0.8120 0.8268 0.0213 0.0210 2.762 21.762 6.961 2059.733 2.459 30.961 1.533 0.66 283775. 0.1186
|
|
127.96 0.8445 0.7978 0.0160 0.0169 2.231 17.573 5.216 1663.319 1.985 23.200 1.422 0.66 284957. 0.0953
|
|
132.88 0.8770 0.7376 0.0106 0.0126 1.667 13.134 3.470 1243.111 1.484 15.436 1.266 0.66 286178. 0.0692
|
|
137.80 0.9095 0.5927 0.0053 0.0082 1.075 8.468 1.734 801.473 0.957 7.711 0.981 0.66 287434. 0.0379
|
|
142.72 0.9420 0.0016 0.0000 0.0034 0.452 3.562 0.002 337.175 0.402 0.008 0.003 0.66 288689. 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 0.0930 0.0340 6.374 44.636 38.393 4752.830 5.043 170.772 3.664 0.71 300626. 0.6660
|
|
5.54 0.0325 0.0861 0.0928 0.0350 6.578 46.067 38.315 4905.221 5.205 170.424 3.543 0.71 300857. 0.6434
|
|
11.08 0.0650 0.1662 0.0925 0.0362 6.798 47.607 38.219 5069.237 5.379 169.998 3.420 0.71 301120. 0.6202
|
|
16.63 0.0975 0.2402 0.0922 0.0375 7.032 49.244 38.098 5243.568 5.564 169.461 3.296 0.71 301417. 0.5968
|
|
22.17 0.1301 0.3082 0.0919 0.0388 7.277 50.960 37.943 5426.240 5.757 168.772 3.172 0.71 301750. 0.5732
|
|
27.71 0.1626 0.3704 0.0914 0.0401 7.529 52.726 37.742 5614.312 5.957 167.878 3.049 0.71 302123. 0.5496
|
|
33.25 0.1951 0.4270 0.0907 0.0415 7.783 54.505 37.481 5803.748 6.158 166.713 2.929 0.72 302537. 0.5261
|
|
38.79 0.2276 0.4783 0.0899 0.0428 8.032 56.248 37.140 5989.374 6.355 165.201 2.813 0.72 302994. 0.5029
|
|
44.34 0.2601 0.5249 0.0889 0.0440 8.267 57.897 36.703 6164.929 6.541 163.254 2.700 0.72 303497. 0.4800
|
|
49.88 0.2926 0.5670 0.0875 0.0452 8.480 59.384 36.146 6323.213 6.709 160.779 2.593 0.72 304047. 0.4573
|
|
55.42 0.3251 0.6051 0.0858 0.0461 8.658 60.634 35.451 6456.385 6.850 157.685 2.490 0.72 304644. 0.4350
|
|
60.96 0.3576 0.6397 0.0838 0.0468 8.792 61.574 34.597 6556.436 6.957 153.888 2.393 0.72 305290. 0.4130
|
|
66.50 0.3902 0.6710 0.0813 0.0473 8.872 62.131 33.571 6615.787 7.020 149.324 2.302 0.72 305985. 0.3912
|
|
72.05 0.4227 0.6995 0.0784 0.0473 8.889 62.248 32.366 6628.161 7.033 143.963 2.215 0.72 306729. 0.3697
|
|
77.59 0.4552 0.7255 0.0750 0.0471 8.837 61.886 30.987 6589.700 6.992 137.829 2.133 0.72 307522. 0.3483
|
|
83.13 0.4877 0.7490 0.0713 0.0464 8.716 61.036 29.448 6499.175 6.896 130.986 2.055 0.72 308362. 0.3272
|
|
88.67 0.5202 0.7702 0.0672 0.0454 8.525 59.702 27.770 6357.147 6.745 123.522 1.981 0.72 309250. 0.3063
|
|
94.21 0.5527 0.7892 0.0629 0.0440 8.267 57.898 25.973 6165.005 6.541 115.527 1.911 0.72 310184. 0.2857
|
|
99.76 0.5852 0.8061 0.0583 0.0423 7.945 55.637 24.075 5924.295 6.286 107.084 1.843 0.73 311164. 0.2653
|
|
105.30 0.6177 0.8206 0.0535 0.0403 7.559 52.934 22.092 5636.455 5.980 98.263 1.778 0.73 312189. 0.2451
|
|
110.84 0.6503 0.8328 0.0485 0.0379 7.111 49.800 20.038 5302.725 5.626 89.127 1.714 0.73 313260. 0.2251
|
|
116.38 0.6828 0.8424 0.0434 0.0352 6.603 46.245 17.924 4924.190 5.225 79.727 1.651 0.73 314375. 0.2051
|
|
121.92 0.7153 0.8488 0.0382 0.0322 6.037 42.279 15.761 4501.857 4.777 70.105 1.588 0.73 315535. 0.1850
|
|
127.47 0.7478 0.8512 0.0328 0.0288 5.413 37.911 13.557 4036.778 4.283 60.301 1.523 0.73 316738. 0.1645
|
|
133.01 0.7803 0.8481 0.0274 0.0252 4.734 33.153 11.320 3530.158 3.746 50.353 1.454 0.74 317986. 0.1436
|
|
138.55 0.8128 0.8366 0.0219 0.0213 4.001 28.019 9.060 2983.502 3.166 40.299 1.377 0.74 319277. 0.1216
|
|
144.09 0.8453 0.8104 0.0164 0.0171 3.217 22.529 6.785 2398.892 2.545 30.182 1.283 0.74 320610. 0.0980
|
|
149.63 0.8779 0.7537 0.0109 0.0127 2.386 16.711 4.508 1779.372 1.888 20.050 1.149 0.74 321986. 0.0716
|
|
155.18 0.9104 0.6118 0.0054 0.0081 1.514 10.606 2.239 1129.294 1.198 9.960 0.899 0.74 323403. 0.0395
|
|
160.72 0.9429 -0.0223 -0.0001 0.0032 0.599 4.192 -0.031 446.344 0.474 -0.139 -0.032 0.75 324804. 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 0.0933 0.0370 9.540 60.127 47.563 7113.707 6.793 211.561 3.033 0.79 334019. 0.6136
|
|
6.16 0.0325 0.0795 0.0931 0.0381 9.815 61.860 47.486 7318.797 6.989 211.220 2.943 0.79 334275. 0.5950
|
|
12.32 0.0651 0.1540 0.0930 0.0393 10.112 63.736 47.395 7540.725 7.201 210.811 2.851 0.79 334566. 0.5758
|
|
18.48 0.0976 0.2234 0.0927 0.0405 10.430 65.740 47.280 7777.875 7.427 210.302 2.757 0.79 334895. 0.5562
|
|
24.64 0.1301 0.2877 0.0924 0.0418 10.765 67.852 47.133 8027.667 7.666 209.648 2.663 0.79 335265. 0.5364
|
|
30.80 0.1626 0.3470 0.0921 0.0432 11.112 70.036 46.940 8286.030 7.913 208.789 2.569 0.79 335677. 0.5165
|
|
36.96 0.1952 0.4014 0.0916 0.0445 11.462 72.242 46.683 8547.137 8.162 207.647 2.477 0.79 336135. 0.4966
|
|
43.12 0.2277 0.4514 0.0909 0.0458 11.805 74.407 46.341 8803.198 8.406 206.125 2.388 0.80 336642. 0.4769
|
|
49.29 0.2602 0.4972 0.0900 0.0471 12.129 76.446 45.887 9044.450 8.637 204.106 2.301 0.80 337199. 0.4573
|
|
55.45 0.2928 0.5393 0.0888 0.0482 12.417 78.263 45.293 9259.468 8.842 201.462 2.219 0.80 337808. 0.4381
|
|
61.61 0.3253 0.5781 0.0873 0.0491 12.654 79.754 44.527 9435.811 9.011 198.056 2.140 0.80 338471. 0.4190
|
|
67.77 0.3578 0.6139 0.0854 0.0498 12.821 80.812 43.561 9560.983 9.130 193.759 2.067 0.80 339189. 0.4001
|
|
73.93 0.3903 0.6472 0.0831 0.0501 12.906 81.342 42.371 9623.746 9.190 188.465 1.997 0.80 339961. 0.3814
|
|
80.09 0.4229 0.6781 0.0803 0.0501 12.895 81.273 40.944 9615.545 9.182 182.117 1.931 0.80 340789. 0.3626
|
|
86.25 0.4554 0.7068 0.0770 0.0496 12.783 80.566 39.282 9531.958 9.102 174.725 1.869 0.80 341671. 0.3437
|
|
92.41 0.4879 0.7333 0.0734 0.0488 12.569 79.222 37.402 9372.860 8.950 166.365 1.810 0.80 342607. 0.3248
|
|
98.57 0.5205 0.7575 0.0693 0.0476 12.258 77.262 35.330 9140.964 8.729 157.148 1.753 0.80 343596. 0.3057
|
|
104.73 0.5530 0.7796 0.0649 0.0460 11.855 74.717 33.092 8839.953 8.442 147.194 1.698 0.81 344637. 0.2866
|
|
110.89 0.5855 0.7993 0.0602 0.0441 11.363 71.619 30.714 8473.315 8.091 136.615 1.644 0.81 345729. 0.2673
|
|
117.05 0.6180 0.8165 0.0553 0.0419 10.787 67.988 28.217 8043.803 7.681 125.510 1.591 0.81 346872. 0.2480
|
|
123.21 0.6506 0.8311 0.0502 0.0393 10.129 63.842 25.621 7553.288 7.213 113.963 1.539 0.81 348065. 0.2285
|
|
129.37 0.6831 0.8428 0.0450 0.0365 9.391 59.190 22.942 7002.929 6.687 102.045 1.486 0.81 349308. 0.2088
|
|
135.53 0.7156 0.8512 0.0396 0.0333 8.574 54.039 20.193 6393.480 6.105 89.817 1.433 0.81 350599. 0.1889
|
|
141.69 0.7481 0.8555 0.0341 0.0298 7.678 48.394 17.386 5725.545 5.467 77.332 1.377 0.82 351940. 0.1685
|
|
147.86 0.7807 0.8544 0.0285 0.0260 6.706 42.267 14.532 5000.738 4.775 64.639 1.318 0.82 353328. 0.1474
|
|
154.02 0.8132 0.8439 0.0228 0.0220 5.666 35.710 11.642 4224.883 4.034 51.785 1.250 0.82 354765. 0.1251
|
|
160.18 0.8457 0.8175 0.0171 0.0177 4.560 28.743 8.729 3400.590 3.247 38.825 1.164 0.82 356249. 0.1009
|
|
166.34 0.8783 0.7570 0.0114 0.0132 3.401 21.435 5.804 2536.045 2.422 25.818 1.038 0.82 357780. 0.0734
|
|
172.50 0.9108 0.6028 0.0057 0.0085 2.202 13.877 2.886 1641.775 1.568 12.835 0.797 0.83 359356. 0.0397
|
|
178.66 0.9433 -0.0211 -0.0001 0.0037 0.963 6.067 -0.043 717.796 0.685 -0.190 -0.027 0.83 360917. 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 0.0932 0.0431 14.786 84.721 57.473 11025.837 9.572 255.638 2.364 0.87 367414. 0.5258
|
|
6.79 0.0326 0.0686 0.0930 0.0442 15.136 86.728 57.389 11287.072 9.799 255.266 2.306 0.87 367697. 0.5126
|
|
13.57 0.0652 0.1336 0.0929 0.0453 15.518 88.918 57.294 11572.076 10.046 254.844 2.246 0.87 368017. 0.4987
|
|
20.36 0.0977 0.1949 0.0927 0.0465 15.929 91.269 57.180 11878.015 10.312 254.335 2.183 0.87 368379. 0.4844
|
|
27.15 0.1303 0.2523 0.0924 0.0477 16.365 93.769 57.038 12203.347 10.594 253.704 2.120 0.87 368785. 0.4697
|
|
33.94 0.1629 0.3059 0.0922 0.0491 16.821 96.381 56.855 12543.257 10.889 252.891 2.056 0.87 369238. 0.4548
|
|
40.72 0.1955 0.3556 0.0918 0.0504 17.286 99.048 56.613 12890.339 11.190 251.813 1.992 0.87 369741. 0.4397
|
|
47.51 0.2281 0.4018 0.0912 0.0518 17.747 101.688 56.286 13234.037 11.489 250.361 1.929 0.87 370297. 0.4246
|
|
54.30 0.2606 0.4447 0.0905 0.0531 18.185 104.195 55.846 13560.244 11.772 248.401 1.868 0.88 370909. 0.4095
|
|
61.09 0.2932 0.4845 0.0896 0.0542 18.575 106.432 55.253 13851.434 12.025 245.768 1.809 0.88 371578. 0.3946
|
|
67.87 0.3258 0.5218 0.0883 0.0551 18.892 108.246 54.469 14087.465 12.230 242.279 1.754 0.88 372306. 0.3797
|
|
74.66 0.3584 0.5570 0.0866 0.0557 19.106 109.474 53.450 14247.316 12.368 237.747 1.702 0.88 373095. 0.3650
|
|
81.45 0.3910 0.5903 0.0845 0.0560 19.192 109.967 52.160 14311.485 12.424 232.007 1.653 0.88 373945. 0.3503
|
|
88.24 0.4235 0.6220 0.0820 0.0558 19.129 109.608 50.572 14264.746 12.383 224.943 1.608 0.88 374857. 0.3355
|
|
95.02 0.4561 0.6524 0.0789 0.0552 18.907 108.333 48.680 14098.788 12.239 216.528 1.566 0.88 375829. 0.3206
|
|
101.81 0.4887 0.6815 0.0754 0.0540 18.522 106.129 46.496 13811.989 11.990 206.816 1.527 0.88 376862. 0.3055
|
|
108.60 0.5213 0.7093 0.0714 0.0525 17.984 103.046 44.049 13410.729 11.642 195.929 1.490 0.88 377955. 0.2901
|
|
115.38 0.5538 0.7356 0.0671 0.0505 17.304 99.149 41.369 12903.534 11.202 184.008 1.454 0.89 379105. 0.2744
|
|
122.17 0.5864 0.7601 0.0624 0.0481 16.494 94.510 38.487 12299.873 10.678 171.191 1.419 0.89 380312. 0.2583
|
|
128.96 0.6190 0.7827 0.0574 0.0454 15.568 89.200 35.434 11608.719 10.078 157.612 1.384 0.89 381576. 0.2418
|
|
135.75 0.6516 0.8029 0.0522 0.0424 14.533 83.273 32.236 10837.373 9.408 143.386 1.349 0.89 382894. 0.2247
|
|
142.53 0.6842 0.8202 0.0469 0.0391 13.398 76.769 28.915 9990.987 8.673 128.614 1.313 0.89 384268. 0.2071
|
|
149.32 0.7167 0.8342 0.0413 0.0355 12.167 69.713 25.491 9072.606 7.876 113.382 1.274 0.90 385696. 0.1888
|
|
156.11 0.7493 0.8440 0.0356 0.0316 10.841 62.119 21.981 8084.378 7.018 97.771 1.233 0.90 387177. 0.1696
|
|
162.90 0.7819 0.8478 0.0298 0.0275 9.428 54.023 18.402 7030.667 6.103 81.851 1.187 0.90 388711. 0.1494
|
|
169.68 0.8145 0.8343 0.0239 0.0234 8.003 45.857 14.757 5968.016 5.181 65.640 1.122 0.90 390298. 0.1264
|
|
176.47 0.8471 0.7931 0.0179 0.0192 6.566 37.622 11.067 4896.256 4.251 49.224 1.025 0.90 391937. 0.1001
|
|
183.26 0.8796 0.7049 0.0119 0.0149 5.100 29.220 7.356 3802.793 3.301 32.719 0.877 0.91 393627. 0.0698
|
|
190.05 0.9122 0.5092 0.0059 0.0106 3.632 20.810 3.649 2708.281 2.351 16.231 0.611 0.91 395367. 0.0342
|
|
196.83 0.9448 -0.0136 -0.0001 0.0063 2.169 12.427 -0.056 1617.332 1.404 -0.251 -0.016 0.91 397118. 0.0000
|
|
|
|
|
|
|