427 lines
76 KiB
Plaintext
427 lines
76 KiB
Plaintext
20.5x12WE (205x12WE.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 0.1042 0.0415 0.012 0.762 0.587 9.012 0.086 2.609 29.525 0.08 46791. 0.6473
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0.49 0.0253 0.0619 0.1026 0.0420 0.012 0.770 0.578 9.115 0.087 2.569 28.742 0.08 46826. 0.6252
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0.98 0.0506 0.1205 0.1009 0.0424 0.012 0.779 0.568 9.211 0.088 2.526 27.963 0.08 46863. 0.6031
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1.47 0.0759 0.1757 0.0990 0.0428 0.012 0.786 0.557 9.296 0.089 2.479 27.190 0.08 46904. 0.5810
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1.97 0.1013 0.2277 0.0970 0.0431 0.013 0.792 0.546 9.370 0.089 2.428 26.427 0.08 46948. 0.5589
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2.46 0.1266 0.2766 0.0948 0.0434 0.013 0.797 0.534 9.429 0.090 2.374 25.674 0.08 46995. 0.5369
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2.95 0.1519 0.3223 0.0925 0.0436 0.013 0.801 0.521 9.471 0.090 2.316 24.932 0.08 47045. 0.5149
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3.44 0.1772 0.3650 0.0900 0.0437 0.013 0.802 0.507 9.494 0.091 2.253 24.201 0.08 47099. 0.4930
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3.93 0.2025 0.4047 0.0873 0.0437 0.013 0.803 0.492 9.496 0.091 2.187 23.482 0.08 47157. 0.4713
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4.42 0.2278 0.4416 0.0845 0.0436 0.013 0.801 0.476 9.473 0.090 2.116 22.775 0.08 47218. 0.4496
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4.91 0.2531 0.4756 0.0815 0.0434 0.013 0.797 0.459 9.424 0.090 2.040 22.077 0.08 47283. 0.4280
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5.41 0.2785 0.5069 0.0783 0.0430 0.013 0.790 0.441 9.346 0.089 1.960 21.389 0.08 47352. 0.4064
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5.90 0.3038 0.5354 0.0749 0.0425 0.012 0.781 0.422 9.237 0.088 1.876 20.709 0.08 47424. 0.3849
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6.39 0.3291 0.5611 0.0714 0.0419 0.012 0.769 0.402 9.093 0.087 1.786 20.033 0.08 47501. 0.3634
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6.88 0.3544 0.5839 0.0676 0.0410 0.012 0.753 0.380 8.913 0.085 1.692 19.359 0.08 47582. 0.3418
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7.37 0.3797 0.6038 0.0637 0.0400 0.012 0.735 0.358 8.698 0.083 1.594 18.684 0.08 47666. 0.3201
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7.86 0.4050 0.6206 0.0596 0.0389 0.011 0.714 0.335 8.448 0.081 1.491 18.002 0.08 47755. 0.2984
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8.35 0.4304 0.6339 0.0554 0.0376 0.011 0.690 0.312 8.165 0.078 1.386 17.308 0.08 47848. 0.2765
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8.85 0.4557 0.6435 0.0510 0.0361 0.011 0.663 0.287 7.848 0.075 1.277 16.594 0.08 47944. 0.2545
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9.34 0.4810 0.6489 0.0466 0.0345 0.010 0.634 0.262 7.499 0.072 1.166 15.852 0.08 48045. 0.2323
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9.83 0.5063 0.6494 0.0420 0.0328 0.010 0.602 0.237 7.118 0.068 1.052 15.072 0.08 48150. 0.2098
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10.32 0.5316 0.6442 0.0374 0.0309 0.009 0.567 0.211 6.707 0.064 0.937 14.239 0.08 48259. 0.1870
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10.81 0.5569 0.6320 0.0327 0.0288 0.008 0.530 0.184 6.266 0.060 0.819 13.335 0.08 48372. 0.1638
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11.30 0.5822 0.6112 0.0280 0.0267 0.008 0.490 0.158 5.797 0.055 0.701 12.334 0.08 48489. 0.1402
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11.79 0.6076 0.5792 0.0233 0.0244 0.007 0.448 0.131 5.302 0.051 0.582 11.201 0.08 48610. 0.1160
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12.29 0.6329 0.5322 0.0185 0.0220 0.006 0.404 0.104 4.782 0.046 0.463 9.881 0.08 48735. 0.0913
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12.78 0.6582 0.4645 0.0138 0.0195 0.006 0.358 0.078 4.239 0.040 0.345 8.293 0.08 48865. 0.0661
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13.27 0.6835 0.3664 0.0091 0.0169 0.005 0.311 0.051 3.677 0.035 0.227 6.299 0.08 48998. 0.0407
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13.76 0.7088 0.2207 0.0044 0.0143 0.004 0.262 0.025 3.098 0.030 0.111 3.658 0.08 49136. 0.0166
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14.25 0.7341 -0.0067 -0.0001 0.0115 0.003 0.212 -0.001 2.506 0.024 -0.003 -0.108 0.08 49276. 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 0.1046 0.0389 0.091 2.861 2.356 67.689 0.323 10.479 15.787 0.16 93580. 0.6936
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0.99 0.0254 0.0663 0.1030 0.0395 0.092 2.898 2.320 68.580 0.327 10.319 15.343 0.16 93650. 0.6689
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1.97 0.0508 0.1289 0.1013 0.0399 0.093 2.933 2.281 69.411 0.331 10.144 14.903 0.16 93725. 0.6442
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2.96 0.0762 0.1877 0.0994 0.0404 0.094 2.965 2.238 70.163 0.335 9.956 14.470 0.16 93807. 0.6197
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3.95 0.1016 0.2429 0.0974 0.0407 0.095 2.993 2.193 70.819 0.338 9.754 14.045 0.16 93895. 0.5953
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4.93 0.1270 0.2946 0.0952 0.0411 0.096 3.016 2.144 71.358 0.341 9.536 13.627 0.16 93989. 0.5711
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5.92 0.1524 0.3429 0.0929 0.0413 0.096 3.033 2.091 71.761 0.343 9.302 13.218 0.16 94091. 0.5471
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6.90 0.1778 0.3880 0.0904 0.0414 0.097 3.043 2.035 72.008 0.344 9.051 12.818 0.16 94199. 0.5233
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7.89 0.2032 0.4299 0.0877 0.0415 0.097 3.046 1.975 72.077 0.344 8.783 12.426 0.16 94315. 0.4998
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8.88 0.2287 0.4687 0.0849 0.0414 0.096 3.041 1.911 71.948 0.344 8.498 12.044 0.16 94438. 0.4765
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9.86 0.2541 0.5047 0.0818 0.0412 0.096 3.026 1.842 71.601 0.342 8.194 11.670 0.16 94569. 0.4534
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10.85 0.2795 0.5377 0.0786 0.0409 0.095 3.001 1.770 71.015 0.339 7.873 11.304 0.16 94708. 0.4305
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11.84 0.3049 0.5680 0.0752 0.0404 0.094 2.965 1.693 70.167 0.335 7.532 10.946 0.16 94854. 0.4077
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12.82 0.3303 0.5955 0.0716 0.0397 0.093 2.918 1.612 69.035 0.330 7.171 10.593 0.16 95009. 0.3850
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13.81 0.3557 0.6202 0.0678 0.0389 0.091 2.857 1.527 67.604 0.323 6.792 10.245 0.16 95171. 0.3623
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14.80 0.3811 0.6421 0.0639 0.0379 0.088 2.784 1.438 65.875 0.315 6.395 9.900 0.16 95342. 0.3398
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15.78 0.4065 0.6611 0.0598 0.0367 0.086 2.699 1.345 63.854 0.305 5.984 9.555 0.16 95520. 0.3172
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16.77 0.4319 0.6770 0.0555 0.0354 0.083 2.601 1.250 61.546 0.294 5.558 9.209 0.16 95707. 0.2946
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17.76 0.4573 0.6894 0.0511 0.0339 0.079 2.492 1.151 58.956 0.281 5.121 8.857 0.16 95901. 0.2720
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18.74 0.4827 0.6980 0.0467 0.0323 0.075 2.370 1.050 56.089 0.268 4.673 8.495 0.16 96104. 0.2492
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19.73 0.5081 0.7021 0.0421 0.0305 0.071 2.238 0.948 52.953 0.253 4.216 8.118 0.16 96315. 0.2262
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20.71 0.5335 0.7010 0.0375 0.0285 0.066 2.094 0.843 49.553 0.237 3.751 7.719 0.16 96534. 0.2029
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21.70 0.5589 0.6934 0.0328 0.0264 0.062 1.940 0.738 45.899 0.219 3.281 7.289 0.17 96762. 0.1792
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22.69 0.5843 0.6777 0.0280 0.0242 0.056 1.775 0.631 42.002 0.201 2.807 6.814 0.17 96997. 0.1549
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23.67 0.6097 0.6511 0.0233 0.0218 0.051 1.601 0.524 37.875 0.181 2.330 6.273 0.17 97241. 0.1300
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24.66 0.6351 0.6093 0.0185 0.0193 0.045 1.417 0.417 33.534 0.160 1.853 5.636 0.17 97493. 0.1041
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25.65 0.6606 0.5450 0.0138 0.0167 0.039 1.226 0.310 29.000 0.138 1.379 4.848 0.17 97754. 0.0772
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26.63 0.6860 0.4452 0.0091 0.0140 0.033 1.027 0.204 24.298 0.116 0.909 3.813 0.17 98022. 0.0493
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27.62 0.7114 0.2828 0.0045 0.0112 0.026 0.822 0.100 19.456 0.093 0.446 2.336 0.17 98299. 0.0212
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28.61 0.7368 -0.0074 -0.0001 0.0083 0.019 0.613 -0.002 14.494 0.069 -0.008 -0.059 0.17 98580. 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 0.1051 0.0380 0.299 6.276 5.325 222.767 0.709 23.687 10.843 0.24 140366. 0.7162
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1.48 0.0254 0.0684 0.1035 0.0385 0.303 6.364 5.244 225.886 0.719 23.326 10.530 0.24 140471. 0.6902
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2.96 0.0509 0.1328 0.1018 0.0390 0.307 6.446 5.156 228.802 0.728 22.934 10.221 0.24 140584. 0.6643
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4.44 0.0763 0.1932 0.0999 0.0395 0.310 6.521 5.061 231.452 0.737 22.511 9.918 0.24 140707. 0.6386
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5.93 0.1017 0.2499 0.0979 0.0399 0.313 6.586 4.958 233.773 0.744 22.055 9.620 0.24 140839. 0.6131
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7.41 0.1272 0.3029 0.0957 0.0402 0.316 6.641 4.848 235.699 0.750 21.563 9.329 0.24 140981. 0.5879
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8.89 0.1526 0.3524 0.0934 0.0404 0.318 6.682 4.729 237.159 0.755 21.036 9.045 0.24 141134. 0.5630
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10.37 0.1780 0.3985 0.0909 0.0406 0.319 6.708 4.602 238.084 0.758 20.470 8.767 0.24 141297. 0.5383
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11.85 0.2035 0.4414 0.0882 0.0406 0.320 6.717 4.466 238.401 0.759 19.866 8.497 0.24 141471. 0.5140
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13.33 0.2289 0.4812 0.0853 0.0406 0.319 6.707 4.321 238.039 0.758 19.221 8.234 0.24 141657. 0.4899
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14.81 0.2543 0.5181 0.0823 0.0404 0.318 6.675 4.167 236.926 0.754 18.535 7.977 0.24 141854. 0.4661
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16.29 0.2798 0.5520 0.0790 0.0401 0.315 6.621 4.003 234.990 0.748 17.808 7.727 0.24 142062. 0.4426
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17.78 0.3052 0.5831 0.0756 0.0396 0.311 6.541 3.830 232.157 0.739 17.037 7.483 0.25 142282. 0.4192
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19.26 0.3307 0.6116 0.0720 0.0389 0.306 6.433 3.647 228.341 0.727 16.222 7.244 0.25 142515. 0.3960
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20.74 0.3561 0.6373 0.0682 0.0381 0.300 6.297 3.454 223.495 0.711 15.363 7.010 0.25 142759. 0.3729
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22.22 0.3815 0.6603 0.0642 0.0371 0.292 6.131 3.252 217.618 0.693 14.466 6.779 0.25 143015. 0.3499
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23.70 0.4070 0.6805 0.0601 0.0359 0.283 5.937 3.043 210.727 0.671 13.534 6.549 0.25 143284. 0.3270
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25.18 0.4324 0.6977 0.0558 0.0346 0.272 5.715 2.826 202.838 0.646 12.571 6.320 0.25 143564. 0.3041
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26.66 0.4578 0.7117 0.0514 0.0331 0.260 5.465 2.604 193.968 0.617 11.581 6.088 0.25 143857. 0.2812
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28.14 0.4833 0.7221 0.0469 0.0314 0.247 5.188 2.376 184.134 0.586 10.568 5.852 0.25 144162. 0.2582
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29.63 0.5087 0.7283 0.0423 0.0296 0.232 4.884 2.143 173.357 0.552 9.534 5.608 0.25 144479. 0.2350
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31.11 0.5341 0.7297 0.0377 0.0276 0.217 4.555 1.907 161.660 0.515 8.483 5.351 0.25 144809. 0.2115
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32.59 0.5596 0.7251 0.0329 0.0254 0.200 4.200 1.668 149.074 0.475 7.419 5.075 0.25 145151. 0.1876
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34.07 0.5850 0.7127 0.0282 0.0231 0.182 3.821 1.427 135.637 0.432 6.347 4.772 0.25 145505. 0.1631
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35.55 0.6104 0.6899 0.0234 0.0207 0.163 3.420 1.185 121.394 0.386 5.270 4.426 0.25 145872. 0.1379
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37.03 0.6359 0.6522 0.0186 0.0181 0.143 2.998 0.942 106.404 0.339 4.192 4.017 0.25 146251. 0.1116
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38.51 0.6613 0.5920 0.0138 0.0155 0.122 2.556 0.701 90.738 0.289 3.120 3.506 0.25 146642. 0.0840
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40.00 0.6867 0.4940 0.0091 0.0127 0.100 2.099 0.463 74.485 0.237 2.058 2.818 0.25 147046. 0.0549
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41.48 0.7122 0.3254 0.0045 0.0098 0.077 1.627 0.228 57.744 0.184 1.013 1.790 0.25 147462. 0.0245
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42.96 0.7376 -0.0054 -0.0001 0.0069 0.054 1.143 -0.003 40.575 0.129 -0.012 -0.029 0.25 147883. 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 0.1058 0.0376 0.701 11.040 9.523 522.481 1.247 42.359 8.267 0.33 187146. 0.7302
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1.98 0.0254 0.0695 0.1042 0.0381 0.711 11.201 9.379 530.068 1.265 41.718 8.026 0.33 187286. 0.7035
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3.95 0.0509 0.1349 0.1024 0.0386 0.720 11.351 9.223 537.171 1.282 41.023 7.787 0.33 187437. 0.6769
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5.93 0.0763 0.1963 0.1005 0.0391 0.729 11.487 9.054 543.637 1.298 40.271 7.554 0.33 187601. 0.6506
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7.90 0.1018 0.2538 0.0985 0.0395 0.737 11.607 8.871 549.315 1.311 39.459 7.325 0.33 187778. 0.6245
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9.88 0.1272 0.3076 0.0963 0.0398 0.743 11.707 8.675 554.044 1.323 38.585 7.102 0.33 187968. 0.5987
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11.86 0.1527 0.3578 0.0940 0.0401 0.748 11.784 8.463 557.656 1.331 37.645 6.884 0.33 188172. 0.5732
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13.83 0.1781 0.4046 0.0915 0.0403 0.751 11.833 8.237 559.980 1.337 36.636 6.671 0.33 188391. 0.5480
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15.81 0.2036 0.4481 0.0888 0.0403 0.752 11.851 7.994 560.840 1.339 35.558 6.465 0.33 188624. 0.5232
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17.78 0.2290 0.4884 0.0859 0.0403 0.751 11.834 7.735 560.063 1.337 34.407 6.264 0.33 188872. 0.4987
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19.76 0.2545 0.5258 0.0828 0.0401 0.748 11.780 7.460 557.477 1.331 33.182 6.070 0.33 189135. 0.4745
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21.74 0.2799 0.5603 0.0796 0.0398 0.741 11.683 7.168 552.910 1.320 31.882 5.880 0.33 189413. 0.4506
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23.71 0.3054 0.5920 0.0762 0.0393 0.732 11.541 6.858 546.178 1.304 30.504 5.695 0.33 189708. 0.4269
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25.69 0.3308 0.6211 0.0725 0.0386 0.720 11.349 6.530 537.079 1.282 29.046 5.515 0.33 190018. 0.4034
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27.67 0.3563 0.6475 0.0687 0.0378 0.705 11.104 6.185 525.488 1.255 27.511 5.338 0.33 190345. 0.3800
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29.64 0.3817 0.6712 0.0647 0.0368 0.686 10.806 5.824 511.405 1.221 25.905 5.165 0.33 190687. 0.3568
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31.62 0.4072 0.6922 0.0605 0.0356 0.664 10.457 5.449 494.863 1.181 24.236 4.994 0.33 191046. 0.3337
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33.59 0.4326 0.7104 0.0562 0.0342 0.638 10.056 5.061 475.901 1.136 22.512 4.824 0.33 191421. 0.3106
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35.57 0.4581 0.7255 0.0518 0.0327 0.610 9.605 4.663 454.556 1.085 20.739 4.652 0.33 191812. 0.2875
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37.55 0.4835 0.7372 0.0472 0.0310 0.578 9.105 4.254 430.871 1.029 18.924 4.479 0.33 192219. 0.2644
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39.52 0.5090 0.7449 0.0426 0.0291 0.543 8.556 3.838 404.893 0.967 17.072 4.299 0.33 192643. 0.2411
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41.50 0.5344 0.7481 0.0379 0.0271 0.505 7.959 3.415 376.680 0.899 15.190 4.112 0.33 193083. 0.2175
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43.47 0.5599 0.7455 0.0332 0.0249 0.464 7.318 2.987 346.304 0.827 13.285 3.912 0.33 193539. 0.1935
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45.45 0.5853 0.7356 0.0284 0.0226 0.421 6.632 2.555 313.854 0.749 11.363 3.692 0.33 194012. 0.1689
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47.43 0.6108 0.7157 0.0236 0.0201 0.375 5.905 2.121 279.447 0.667 9.434 3.442 0.33 194501. 0.1435
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49.40 0.6362 0.6814 0.0187 0.0175 0.326 5.139 1.687 243.222 0.581 7.504 3.146 0.33 195008. 0.1170
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51.38 0.6617 0.6246 0.0139 0.0148 0.275 4.339 1.255 205.355 0.490 5.584 2.773 0.33 195530. 0.0889
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53.35 0.6871 0.5291 0.0092 0.0119 0.223 3.509 0.828 166.059 0.396 3.683 2.262 0.33 196069. 0.0589
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55.33 0.7125 0.3572 0.0045 0.0090 0.168 2.654 0.408 125.585 0.300 1.813 1.473 0.33 196625. 0.0269
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57.31 0.7380 -0.0066 -0.0001 0.0060 0.113 1.776 -0.005 84.045 0.201 -0.022 -0.026 0.33 197184. 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 0.1065 0.0375 1.366 17.216 14.992 1018.431 1.945 66.683 6.677 0.41 233917. 0.7399
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2.47 0.0254 0.0702 0.1050 0.0381 1.386 17.472 14.767 1033.586 1.974 65.686 6.480 0.41 234093. 0.7128
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4.94 0.0509 0.1361 0.1032 0.0386 1.405 17.712 14.524 1047.785 2.001 64.602 6.287 0.41 234283. 0.6858
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7.41 0.0763 0.1980 0.1013 0.0391 1.422 17.931 14.260 1060.727 2.026 63.429 6.098 0.41 234488. 0.6591
|
|
9.88 0.1018 0.2560 0.0993 0.0395 1.438 18.123 13.975 1072.108 2.048 62.161 5.912 0.41 234710. 0.6326
|
|
12.35 0.1272 0.3102 0.0971 0.0398 1.450 18.284 13.668 1081.604 2.066 60.794 5.732 0.41 234948. 0.6065
|
|
14.82 0.1526 0.3608 0.0948 0.0401 1.460 18.407 13.337 1088.887 2.080 59.322 5.555 0.41 235204. 0.5807
|
|
17.29 0.1781 0.4080 0.0923 0.0403 1.467 18.487 12.982 1093.610 2.089 57.743 5.384 0.41 235477. 0.5553
|
|
19.75 0.2035 0.4519 0.0896 0.0403 1.469 18.518 12.602 1095.431 2.092 56.052 5.218 0.41 235769. 0.5302
|
|
22.22 0.2290 0.4926 0.0867 0.0403 1.467 18.494 12.196 1094.000 2.089 54.247 5.056 0.41 236079. 0.5054
|
|
24.69 0.2544 0.5304 0.0836 0.0401 1.460 18.409 11.763 1088.978 2.080 52.324 4.900 0.41 236409. 0.4810
|
|
27.16 0.2798 0.5653 0.0803 0.0398 1.448 18.257 11.304 1080.023 2.063 50.281 4.747 0.41 236758. 0.4569
|
|
29.63 0.3053 0.5975 0.0769 0.0393 1.431 18.033 10.817 1066.776 2.037 48.116 4.599 0.41 237126. 0.4330
|
|
32.10 0.3307 0.6270 0.0732 0.0386 1.407 17.730 10.302 1048.832 2.003 45.824 4.455 0.41 237515. 0.4093
|
|
34.57 0.3562 0.6539 0.0694 0.0378 1.376 17.343 9.759 1025.932 1.959 43.408 4.314 0.41 237923. 0.3858
|
|
37.04 0.3816 0.6782 0.0653 0.0368 1.338 16.872 9.191 998.066 1.906 40.880 4.177 0.41 238352. 0.3624
|
|
39.51 0.4070 0.6999 0.0611 0.0355 1.294 16.318 8.600 965.298 1.844 38.252 4.041 0.41 238801. 0.3392
|
|
41.98 0.4325 0.7188 0.0568 0.0342 1.244 15.682 7.989 927.704 1.772 35.536 3.906 0.41 239270. 0.3160
|
|
44.45 0.4579 0.7348 0.0523 0.0326 1.187 14.967 7.361 885.357 1.691 32.742 3.771 0.41 239759. 0.2929
|
|
46.92 0.4834 0.7475 0.0477 0.0309 1.124 14.172 6.718 838.339 1.601 29.880 3.634 0.41 240268. 0.2696
|
|
49.39 0.5088 0.7566 0.0431 0.0290 1.055 13.300 6.061 786.746 1.503 26.960 3.494 0.41 240798. 0.2462
|
|
51.86 0.5342 0.7612 0.0383 0.0269 0.980 12.352 5.394 730.689 1.396 23.993 3.348 0.41 241348. 0.2226
|
|
54.32 0.5597 0.7604 0.0335 0.0247 0.899 11.331 4.718 670.314 1.280 20.988 3.193 0.41 241919. 0.1985
|
|
56.79 0.5851 0.7526 0.0287 0.0223 0.812 10.241 4.037 605.799 1.157 17.957 3.023 0.41 242510. 0.1738
|
|
59.26 0.6106 0.7352 0.0238 0.0198 0.721 9.084 3.353 537.370 1.026 14.913 2.830 0.41 243121. 0.1483
|
|
61.73 0.6360 0.7039 0.0190 0.0171 0.624 7.866 2.668 465.311 0.889 11.868 2.601 0.41 243754. 0.1216
|
|
64.20 0.6614 0.6504 0.0141 0.0144 0.523 6.592 1.987 389.972 0.745 8.838 2.311 0.42 244407. 0.0932
|
|
66.67 0.6869 0.5581 0.0093 0.0115 0.418 5.271 1.313 311.781 0.595 5.838 1.910 0.42 245080. 0.0626
|
|
69.14 0.7123 0.3860 0.0046 0.0085 0.310 3.909 0.649 231.241 0.442 2.888 1.273 0.42 245774. 0.0294
|
|
71.61 0.7378 -0.0019 0.0000 0.0055 0.199 2.511 -0.002 148.558 0.284 -0.009 -0.006 0.42 246472. 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 0.1075 0.0377 2.370 24.900 21.789 1767.590 2.813 96.918 5.591 0.49 280678. 0.7470
|
|
2.96 0.0254 0.0705 0.1060 0.0382 2.406 25.278 21.468 1794.402 2.856 95.489 5.426 0.49 280889. 0.7196
|
|
5.93 0.0509 0.1368 0.1042 0.0388 2.440 25.632 21.118 1819.536 2.896 93.935 5.264 0.49 281118. 0.6924
|
|
8.89 0.0763 0.1990 0.1024 0.0393 2.471 25.955 20.739 1842.453 2.932 92.249 5.106 0.49 281365. 0.6655
|
|
11.85 0.1018 0.2572 0.1003 0.0397 2.498 26.239 20.329 1862.615 2.964 90.423 4.950 0.49 281632. 0.6389
|
|
14.81 0.1272 0.3117 0.0981 0.0401 2.520 26.476 19.886 1879.458 2.991 88.452 4.799 0.49 281919. 0.6125
|
|
17.78 0.1526 0.3625 0.0958 0.0403 2.538 26.658 19.408 1892.390 3.012 86.329 4.652 0.49 282227. 0.5866
|
|
20.74 0.1781 0.4100 0.0933 0.0405 2.549 26.777 18.895 1900.808 3.025 84.047 4.509 0.49 282556. 0.5610
|
|
23.70 0.2035 0.4541 0.0905 0.0406 2.553 26.823 18.345 1904.102 3.030 81.601 4.370 0.49 282907. 0.5357
|
|
26.67 0.2289 0.4951 0.0876 0.0405 2.550 26.789 17.758 1901.661 3.027 78.986 4.235 0.49 283281. 0.5109
|
|
29.63 0.2544 0.5332 0.0845 0.0403 2.538 26.665 17.131 1892.882 3.013 76.199 4.105 0.49 283677. 0.4863
|
|
32.59 0.2798 0.5684 0.0813 0.0400 2.517 26.444 16.465 1877.171 2.988 73.236 3.978 0.49 284097. 0.4621
|
|
35.55 0.3053 0.6009 0.0778 0.0395 2.486 26.116 15.758 1853.896 2.951 70.093 3.855 0.49 284540. 0.4381
|
|
38.52 0.3307 0.6308 0.0741 0.0388 2.444 25.672 15.010 1822.355 2.900 66.764 3.736 0.49 285008. 0.4143
|
|
41.48 0.3561 0.6582 0.0702 0.0380 2.390 25.104 14.221 1782.069 2.836 63.253 3.619 0.49 285499. 0.3907
|
|
44.44 0.3816 0.6830 0.0661 0.0369 2.324 24.413 13.394 1733.003 2.758 59.576 3.506 0.49 286014. 0.3672
|
|
47.41 0.4070 0.7053 0.0619 0.0357 2.247 23.600 12.534 1675.271 2.666 55.752 3.394 0.49 286554. 0.3439
|
|
50.37 0.4324 0.7249 0.0575 0.0343 2.158 22.666 11.645 1609.003 2.561 51.797 3.283 0.49 287117. 0.3206
|
|
53.33 0.4579 0.7416 0.0530 0.0327 2.058 21.614 10.730 1534.337 2.442 47.726 3.172 0.49 287705. 0.2974
|
|
56.30 0.4833 0.7552 0.0483 0.0309 1.946 20.446 9.792 1451.414 2.310 43.556 3.060 0.49 288317. 0.2741
|
|
59.26 0.5088 0.7653 0.0436 0.0290 1.824 19.164 8.835 1360.402 2.165 39.299 2.946 0.49 288953. 0.2506
|
|
62.22 0.5342 0.7711 0.0388 0.0269 1.692 17.771 7.862 1261.505 2.008 34.972 2.827 0.49 289614. 0.2269
|
|
65.18 0.5596 0.7718 0.0339 0.0246 1.549 16.270 6.877 1154.971 1.838 30.589 2.701 0.50 290299. 0.2027
|
|
68.15 0.5851 0.7657 0.0290 0.0222 1.396 14.666 5.883 1041.120 1.657 26.168 2.563 0.50 291009. 0.1779
|
|
71.11 0.6105 0.7504 0.0241 0.0196 1.234 12.965 4.884 920.354 1.465 21.725 2.407 0.50 291743. 0.1523
|
|
74.07 0.6359 0.7215 0.0192 0.0169 1.064 11.173 3.885 793.173 1.262 17.282 2.222 0.50 292502. 0.1253
|
|
77.04 0.6614 0.6708 0.0143 0.0141 0.885 9.300 2.891 660.201 1.051 12.859 1.986 0.50 293286. 0.0967
|
|
80.00 0.6868 0.5808 0.0094 0.0111 0.700 7.356 1.907 522.200 0.831 8.481 1.656 0.50 294095. 0.0655
|
|
82.96 0.7123 0.4073 0.0046 0.0081 0.510 5.354 0.938 380.065 0.605 4.174 1.120 0.50 294927. 0.0310
|
|
85.92 0.7377 -0.0094 -0.0001 0.0050 0.314 3.297 -0.013 234.059 0.373 -0.057 -0.025 0.50 295761. 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 0.1088 0.0380 3.802 34.231 29.994 2834.971 3.867 133.415 4.799 0.57 327425. 0.7523
|
|
3.48 0.0256 0.0710 0.1072 0.0386 3.861 34.762 29.558 2878.952 3.927 131.473 4.657 0.57 327673. 0.7247
|
|
6.95 0.0512 0.1377 0.1055 0.0392 3.916 35.260 29.082 2920.172 3.984 129.355 4.517 0.57 327943. 0.6972
|
|
10.43 0.0768 0.2003 0.1036 0.0397 3.966 35.713 28.564 2957.720 4.035 127.051 4.380 0.57 328234. 0.6701
|
|
13.91 0.1023 0.2589 0.1015 0.0401 4.011 36.112 28.002 2990.717 4.080 124.552 4.247 0.57 328549. 0.6432
|
|
17.38 0.1279 0.3137 0.0993 0.0405 4.047 36.444 27.393 3018.211 4.117 121.846 4.117 0.57 328888. 0.6167
|
|
20.86 0.1535 0.3649 0.0969 0.0408 4.076 36.698 26.737 3039.224 4.146 118.925 3.990 0.57 329251. 0.5905
|
|
24.34 0.1791 0.4126 0.0944 0.0410 4.094 36.861 26.030 3052.752 4.165 115.780 3.867 0.57 329640. 0.5648
|
|
27.81 0.2047 0.4571 0.0916 0.0410 4.101 36.922 25.270 3057.791 4.171 112.402 3.748 0.57 330055. 0.5393
|
|
31.29 0.2303 0.4984 0.0887 0.0410 4.095 36.868 24.457 3053.326 4.165 108.787 3.633 0.57 330496. 0.5143
|
|
34.77 0.2558 0.5367 0.0855 0.0408 4.075 36.687 23.590 3038.368 4.145 104.927 3.521 0.57 330965. 0.4896
|
|
38.24 0.2814 0.5723 0.0822 0.0404 4.039 36.368 22.666 3011.933 4.109 100.819 3.413 0.57 331461. 0.4651
|
|
41.72 0.3070 0.6051 0.0786 0.0399 3.987 35.898 21.685 2972.998 4.056 96.456 3.308 0.57 331985. 0.4410
|
|
45.20 0.3326 0.6353 0.0749 0.0392 3.916 35.263 20.645 2920.409 3.984 91.831 3.206 0.57 332537. 0.4170
|
|
48.67 0.3582 0.6630 0.0709 0.0383 3.826 34.454 19.548 2853.387 3.893 86.948 3.107 0.57 333117. 0.3932
|
|
52.15 0.3838 0.6883 0.0667 0.0372 3.717 33.470 18.398 2771.893 3.781 81.832 3.010 0.57 333726. 0.3696
|
|
55.63 0.4094 0.7110 0.0624 0.0359 3.589 32.313 17.201 2676.126 3.651 76.509 2.915 0.57 334363. 0.3461
|
|
59.10 0.4349 0.7310 0.0579 0.0344 3.441 30.987 15.963 2566.307 3.501 71.001 2.821 0.57 335028. 0.3226
|
|
62.58 0.4605 0.7483 0.0533 0.0328 3.276 29.494 14.688 2442.671 3.332 65.332 2.727 0.58 335722. 0.2992
|
|
66.06 0.4861 0.7624 0.0485 0.0309 3.092 27.838 13.382 2305.461 3.145 59.521 2.633 0.58 336445. 0.2757
|
|
69.53 0.5117 0.7730 0.0437 0.0289 2.890 26.020 12.048 2154.963 2.940 53.591 2.536 0.58 337196. 0.2519
|
|
73.01 0.5373 0.7795 0.0388 0.0267 2.671 24.047 10.693 1991.522 2.717 47.561 2.435 0.58 337975. 0.2279
|
|
76.49 0.5629 0.7807 0.0338 0.0244 2.435 21.922 9.320 1815.572 2.477 41.454 2.328 0.58 338784. 0.2034
|
|
79.96 0.5885 0.7752 0.0288 0.0218 2.183 19.653 7.935 1627.653 2.220 35.294 2.211 0.58 339621. 0.1783
|
|
83.44 0.6140 0.7601 0.0237 0.0192 1.916 17.248 6.544 1428.456 1.949 29.107 2.078 0.58 340487. 0.1521
|
|
86.92 0.6396 0.7307 0.0187 0.0164 1.634 14.717 5.153 1218.841 1.663 22.920 1.918 0.58 341383. 0.1246
|
|
90.40 0.6652 0.6776 0.0137 0.0134 1.341 12.073 3.769 999.879 1.364 16.766 1.710 0.58 342307. 0.0950
|
|
93.87 0.6908 0.5799 0.0087 0.0104 1.036 9.332 2.401 772.880 1.054 10.679 1.409 0.58 343260. 0.0625
|
|
97.35 0.7164 0.3790 0.0038 0.0072 0.723 6.513 1.056 539.369 0.736 4.698 0.888 0.58 344241. 0.0261
|
|
100.83 0.7420
|
|
|
|
|
|
|
|
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 0.1103 0.0386 5.764 45.411 39.713 4298.142 5.131 176.645 4.191 0.65 374152. 0.7559
|
|
3.94 0.0254 0.0703 0.1087 0.0392 5.854 46.121 39.155 4365.314 5.211 174.161 4.068 0.65 374435. 0.7286
|
|
7.88 0.0507 0.1363 0.1070 0.0398 5.938 46.787 38.544 4428.324 5.286 171.445 3.948 0.65 374741. 0.7015
|
|
11.82 0.0761 0.1984 0.1052 0.0403 6.016 47.394 37.879 4485.814 5.355 168.485 3.830 0.65 375073. 0.6747
|
|
15.76 0.1015 0.2566 0.1031 0.0408 6.083 47.929 37.155 4536.439 5.415 165.266 3.715 0.65 375430. 0.6481
|
|
19.69 0.1268 0.3111 0.1010 0.0412 6.140 48.376 36.370 4578.771 5.466 161.776 3.603 0.65 375815. 0.6219
|
|
23.63 0.1522 0.3620 0.0986 0.0415 6.184 48.720 35.522 4611.345 5.504 158.000 3.494 0.65 376227. 0.5960
|
|
27.57 0.1775 0.4096 0.0961 0.0416 6.212 48.945 34.606 4632.651 5.530 153.928 3.388 0.65 376668. 0.5705
|
|
31.51 0.2029 0.4539 0.0933 0.0417 6.224 49.035 33.622 4641.173 5.540 149.548 3.286 0.65 377138. 0.5453
|
|
35.45 0.2283 0.4952 0.0904 0.0417 6.216 48.975 32.566 4635.410 5.533 144.854 3.187 0.65 377639. 0.5205
|
|
39.39 0.2536 0.5337 0.0873 0.0415 6.187 48.747 31.438 4613.873 5.507 139.836 3.091 0.65 378169. 0.4960
|
|
43.33 0.2790 0.5694 0.0839 0.0411 6.135 48.338 30.236 4575.124 5.461 134.489 2.998 0.65 378731. 0.4718
|
|
47.27 0.3044 0.6025 0.0804 0.0406 6.058 47.730 28.958 4517.656 5.393 128.807 2.907 0.65 379324. 0.4478
|
|
51.21 0.3297 0.6330 0.0766 0.0399 5.954 46.908 27.603 4439.798 5.300 122.777 2.820 0.65 379948. 0.4241
|
|
55.15 0.3551 0.6612 0.0727 0.0390 5.820 45.856 26.170 4340.207 5.181 116.403 2.735 0.65 380604. 0.4004
|
|
59.08 0.3804 0.6869 0.0685 0.0379 5.657 44.572 24.666 4218.680 5.036 109.713 2.652 0.66 381292. 0.3770
|
|
63.02 0.4058 0.7102 0.0641 0.0366 5.465 43.059 23.098 4075.508 4.865 102.741 2.571 0.66 382012. 0.3536
|
|
66.96 0.4312 0.7311 0.0596 0.0352 5.245 41.321 21.474 3911.042 4.668 95.519 2.490 0.66 382763. 0.3303
|
|
70.90 0.4565 0.7493 0.0550 0.0335 4.996 39.363 19.801 3725.644 4.447 88.075 2.411 0.66 383546. 0.3070
|
|
74.84 0.4819 0.7646 0.0502 0.0316 4.720 37.187 18.084 3519.693 4.201 80.438 2.330 0.66 384362. 0.2837
|
|
78.78 0.5073 0.7767 0.0453 0.0296 4.417 34.798 16.330 3293.606 3.931 72.635 2.249 0.66 385209. 0.2601
|
|
82.72 0.5326 0.7849 0.0404 0.0274 4.087 32.202 14.544 3047.900 3.638 64.693 2.164 0.66 386088. 0.2363
|
|
86.66 0.5580 0.7884 0.0354 0.0250 3.732 29.405 12.734 2783.197 3.322 56.641 2.075 0.66 386999. 0.2120
|
|
90.60 0.5834 0.7858 0.0303 0.0225 3.353 26.416 10.906 2500.284 2.984 48.509 1.978 0.66 387942. 0.1870
|
|
94.54 0.6087 0.7747 0.0252 0.0198 2.950 23.245 9.067 2200.144 2.626 40.331 1.869 0.66 388918. 0.1611
|
|
98.47 0.6341 0.7511 0.0201 0.0169 2.527 19.905 7.226 1884.022 2.249 32.143 1.740 0.66 389926. 0.1339
|
|
102.41 0.6594 0.7069 0.0150 0.0140 2.083 16.413 5.393 1553.460 1.854 23.986 1.574 0.66 390967. 0.1047
|
|
106.35 0.6848 0.6248 0.0099 0.0109 1.623 12.788 3.576 1210.364 1.445 15.905 1.340 0.67 392040. 0.0725
|
|
110.29 0.7102 0.4573 0.0050 0.0077 1.149 9.055 1.787 857.030 1.023 7.949 0.946 0.67 393144. 0.0362
|
|
114.23 0.7355 0.0141 0.0001 0.0044 0.663 5.225 0.031 494.500 0.590 0.137 0.028 0.67 394254. 0.0001
|
|
|
|
|
|
|
|
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 0.1121 0.0397 8.424 58.993 51.086 6281.637 6.665 227.231 3.689 0.73 420855. 0.7546
|
|
4.43 0.0253 0.0696 0.1105 0.0403 8.550 59.877 50.394 6375.701 6.765 224.151 3.585 0.73 421174. 0.7284
|
|
8.86 0.0507 0.1352 0.1089 0.0408 8.669 60.708 49.633 6464.211 6.859 220.768 3.483 0.73 421520. 0.7023
|
|
13.28 0.0760 0.1970 0.1070 0.0413 8.777 61.469 48.801 6545.223 6.945 217.066 3.382 0.73 421894. 0.6762
|
|
17.71 0.1014 0.2549 0.1051 0.0418 8.873 62.140 47.892 6616.753 7.021 213.025 3.283 0.73 422298. 0.6503
|
|
22.14 0.1267 0.3093 0.1029 0.0422 8.954 62.703 46.903 6676.700 7.084 208.626 3.186 0.73 422733. 0.6246
|
|
26.57 0.1521 0.3602 0.1005 0.0424 9.015 63.137 45.830 6722.838 7.133 203.852 3.092 0.73 423199. 0.5991
|
|
31.00 0.1774 0.4077 0.0980 0.0426 9.056 63.419 44.669 6752.866 7.165 198.688 3.000 0.73 423698. 0.5740
|
|
35.43 0.2028 0.4521 0.0952 0.0427 9.071 63.527 43.417 6764.433 7.177 193.119 2.911 0.73 424229. 0.5491
|
|
39.85 0.2281 0.4935 0.0923 0.0427 9.059 63.441 42.072 6755.209 7.167 187.134 2.825 0.73 424795. 0.5244
|
|
44.28 0.2534 0.5321 0.0891 0.0424 9.016 63.137 40.630 6722.889 7.133 180.724 2.741 0.73 425395. 0.5001
|
|
48.71 0.2788 0.5681 0.0857 0.0421 8.938 62.596 39.092 6665.252 7.072 173.880 2.660 0.73 426029. 0.4761
|
|
53.14 0.3041 0.6014 0.0822 0.0415 8.824 61.796 37.454 6580.128 6.982 166.594 2.582 0.74 426699. 0.4522
|
|
57.57 0.3295 0.6323 0.0783 0.0408 8.670 60.716 35.714 6465.113 6.860 158.854 2.506 0.74 427404. 0.4286
|
|
61.99 0.3548 0.6608 0.0743 0.0399 8.473 59.336 33.871 6318.145 6.704 150.658 2.432 0.74 428144. 0.4050
|
|
66.42 0.3802 0.6871 0.0700 0.0388 8.232 57.652 31.934 6138.820 6.513 142.042 2.359 0.74 428920. 0.3816
|
|
70.85 0.4055 0.7109 0.0656 0.0374 7.949 55.668 29.912 5927.577 6.289 133.050 2.289 0.74 429732. 0.3583
|
|
75.28 0.4309 0.7324 0.0610 0.0359 7.624 53.390 27.816 5684.975 6.032 123.725 2.219 0.74 430580. 0.3350
|
|
79.71 0.4562 0.7513 0.0563 0.0342 7.257 50.822 25.653 5411.563 5.742 114.104 2.150 0.74 431463. 0.3117
|
|
84.14 0.4816 0.7675 0.0514 0.0323 6.850 47.971 23.432 5107.934 5.420 104.225 2.081 0.74 432382. 0.2883
|
|
88.56 0.5069 0.7804 0.0464 0.0301 6.403 44.842 21.161 4774.770 5.066 94.122 2.010 0.74 433336. 0.2647
|
|
92.99 0.5322 0.7897 0.0413 0.0279 5.918 41.444 18.847 4412.930 4.682 83.832 1.937 0.74 434326. 0.2407
|
|
97.42 0.5576 0.7944 0.0362 0.0254 5.396 37.786 16.500 4023.514 4.269 73.391 1.860 0.74 435351. 0.2163
|
|
101.85 0.5829 0.7930 0.0310 0.0228 4.838 33.883 14.128 3607.915 3.828 62.839 1.776 0.74 436413. 0.1911
|
|
106.28 0.6083 0.7831 0.0258 0.0200 4.248 29.751 11.740 3167.933 3.361 52.220 1.681 0.75 437511. 0.1648
|
|
110.70 0.6336 0.7605 0.0205 0.0171 3.629 25.412 9.348 2705.841 2.871 41.580 1.567 0.75 438644. 0.1371
|
|
115.13 0.6590 0.7166 0.0153 0.0140 2.983 20.891 6.963 2224.510 2.360 30.972 1.420 0.75 439814. 0.1072
|
|
119.56 0.6843 0.6329 0.0101 0.0109 2.317 16.223 4.599 1727.474 1.833 20.455 1.207 0.75 441020. 0.0741
|
|
123.99 0.7097 0.4590 0.0050 0.0077 1.635 11.447 2.269 1218.922 1.293 10.094 0.844 0.75 442262. 0.0364
|
|
128.42 0.7350 -0.0080 0.0000 0.0044 0.939 6.578 -0.022 700.445 0.743 -0.097 -0.014 0.75 443503. 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 0.1142 0.0429 12.485 78.690 64.265 9309.988 8.890 285.853 3.131 0.81 467524. 0.7184
|
|
4.91 0.0253 0.0658 0.1127 0.0433 12.615 79.511 63.443 9407.115 8.983 282.194 3.059 0.81 467878. 0.6974
|
|
9.82 0.0506 0.1286 0.1111 0.0437 12.734 80.260 62.534 9495.655 9.068 278.150 2.987 0.81 468264. 0.6761
|
|
14.73 0.0759 0.1882 0.1093 0.0441 12.838 80.916 61.532 9573.298 9.142 273.696 2.915 0.81 468681. 0.6546
|
|
19.64 0.1012 0.2448 0.1074 0.0444 12.924 81.459 60.433 9637.579 9.203 268.805 2.844 0.81 469131. 0.6328
|
|
24.55 0.1264 0.2985 0.1052 0.0446 12.989 81.869 59.230 9686.118 9.250 263.453 2.774 0.81 469616. 0.6110
|
|
29.45 0.1517 0.3491 0.1029 0.0447 13.030 82.125 57.917 9716.411 9.278 257.616 2.704 0.81 470136. 0.5889
|
|
34.36 0.1770 0.3969 0.1004 0.0448 13.042 82.205 56.492 9725.770 9.287 251.274 2.635 0.81 470692. 0.5668
|
|
39.27 0.2023 0.4419 0.0976 0.0447 13.023 82.083 54.948 9711.384 9.274 244.408 2.566 0.81 471285. 0.5445
|
|
44.18 0.2276 0.4841 0.0947 0.0445 12.968 81.736 53.283 9670.366 9.235 237.002 2.499 0.82 471915. 0.5221
|
|
49.09 0.2529 0.5236 0.0915 0.0442 12.874 81.140 51.493 9599.777 9.167 229.042 2.433 0.82 472584. 0.4997
|
|
54.00 0.2782 0.5606 0.0881 0.0437 12.735 80.268 49.577 9496.688 9.069 220.519 2.368 0.82 473291. 0.4772
|
|
58.91 0.3035 0.5950 0.0845 0.0431 12.549 79.097 47.532 9358.063 8.936 211.423 2.304 0.82 474038. 0.4546
|
|
63.82 0.3287 0.6269 0.0806 0.0423 12.311 77.596 45.355 9180.466 8.767 201.739 2.241 0.82 474823. 0.4319
|
|
68.73 0.3540 0.6565 0.0765 0.0412 12.016 75.736 43.044 8960.495 8.557 191.461 2.179 0.82 475648. 0.4092
|
|
73.64 0.3793 0.6837 0.0722 0.0400 11.663 73.509 40.609 8696.936 8.305 180.630 2.118 0.82 476512. 0.3863
|
|
78.55 0.4046 0.7085 0.0676 0.0386 11.252 70.919 38.063 8390.521 8.012 169.303 2.058 0.82 477415. 0.3633
|
|
83.46 0.4299 0.7307 0.0629 0.0370 10.786 67.983 35.417 8043.164 7.681 157.534 1.997 0.82 478358. 0.3402
|
|
88.36 0.4552 0.7502 0.0581 0.0352 10.266 64.704 32.683 7655.251 7.310 145.373 1.936 0.82 479340. 0.3169
|
|
93.27 0.4805 0.7666 0.0531 0.0333 9.692 61.087 29.872 7227.320 6.902 132.869 1.875 0.82 480360. 0.2933
|
|
98.18 0.5058 0.7795 0.0480 0.0311 9.067 57.146 26.993 6760.992 6.456 120.065 1.811 0.82 481420. 0.2693
|
|
103.09 0.5311 0.7880 0.0427 0.0288 8.392 52.894 24.057 6258.011 5.976 107.007 1.744 0.82 482519. 0.2448
|
|
108.00 0.5563 0.7911 0.0374 0.0263 7.672 48.357 21.075 5721.259 5.463 93.741 1.671 0.83 483657. 0.2195
|
|
112.91 0.5816 0.7866 0.0321 0.0237 6.911 43.562 18.057 5153.896 4.922 80.318 1.589 0.83 484834. 0.1933
|
|
117.82 0.6069 0.7715 0.0267 0.0210 6.115 38.542 15.016 4559.920 4.354 66.789 1.494 0.83 486051. 0.1657
|
|
122.73 0.6322 0.7402 0.0213 0.0182 5.289 33.337 11.964 3944.134 3.766 53.215 1.376 0.83 487308. 0.1362
|
|
127.64 0.6575 0.6833 0.0158 0.0152 4.442 27.996 8.917 3312.249 3.163 39.663 1.221 0.83 488604. 0.1044
|
|
132.55 0.6828 0.5815 0.0105 0.0123 3.581 22.573 5.892 2670.683 2.550 26.209 1.001 0.83 489939. 0.0695
|
|
137.46 0.7081 0.3921 0.0052 0.0093 2.718 17.129 2.908 2026.612 1.935 12.933 0.651 0.83 491314. 0.0318
|
|
142.37 0.7334 -0.0061 -0.0001 0.0064 1.854 11.688 -0.030 1382.855 1.321 -0.132 -0.010 0.84 492696. 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 0.1160 0.0507 19.680 112.763 78.999 14675.319 12.740 351.386 2.442 0.89 514173. 0.6212
|
|
5.48 0.0257 0.0578 0.1146 0.0510 19.763 113.238 78.065 14737.095 12.794 347.232 2.403 0.89 514568. 0.6076
|
|
10.97 0.0514 0.1137 0.1131 0.0511 19.819 113.559 77.019 14778.965 12.830 342.582 2.364 0.89 514998. 0.5938
|
|
16.45 0.0771 0.1677 0.1114 0.0512 19.844 113.706 75.855 14798.028 12.846 337.401 2.325 0.89 515466. 0.5796
|
|
21.94 0.1027 0.2199 0.1095 0.0512 19.836 113.656 74.562 14791.557 12.841 331.650 2.286 0.89 515972. 0.5651
|
|
27.42 0.1284 0.2702 0.1074 0.0510 19.789 113.390 73.132 14756.944 12.811 325.293 2.248 0.90 516518. 0.5502
|
|
32.91 0.1541 0.3187 0.1051 0.0508 19.702 112.889 71.559 14691.690 12.754 318.296 2.209 0.90 517105. 0.5349
|
|
38.39 0.1798 0.3653 0.1025 0.0505 19.570 112.132 69.835 14593.223 12.669 310.627 2.171 0.90 517734. 0.5192
|
|
43.88 0.2055 0.4100 0.0998 0.0500 19.390 111.100 67.954 14458.935 12.552 302.260 2.132 0.90 518405. 0.5030
|
|
49.36 0.2312 0.4528 0.0968 0.0494 19.158 109.772 65.911 14286.116 12.402 293.171 2.093 0.90 519120. 0.4863
|
|
54.85 0.2568 0.4937 0.0935 0.0487 18.871 108.128 63.701 14072.074 12.216 283.340 2.053 0.90 519879. 0.4690
|
|
60.33 0.2825 0.5325 0.0900 0.0478 18.525 106.147 61.321 13814.278 11.992 272.754 2.013 0.90 520681. 0.4513
|
|
65.82 0.3082 0.5693 0.0863 0.0467 18.117 103.809 58.769 13510.054 11.728 261.403 1.973 0.90 521529. 0.4329
|
|
71.30 0.3339 0.6039 0.0823 0.0455 17.642 101.088 56.040 13155.904 11.421 249.267 1.932 0.90 522421. 0.4140
|
|
76.78 0.3596 0.6364 0.0780 0.0441 17.096 97.956 53.135 12748.350 11.067 236.342 1.890 0.90 523358. 0.3944
|
|
82.27 0.3853 0.6666 0.0735 0.0425 16.477 94.409 50.065 12286.725 10.666 222.688 1.848 0.90 524339. 0.3743
|
|
87.75 0.4109 0.6944 0.0688 0.0407 15.786 90.453 46.848 11771.865 10.219 208.380 1.805 0.90 525365. 0.3536
|
|
93.24 0.4366 0.7191 0.0639 0.0388 15.039 86.170 43.499 11214.437 9.735 193.485 1.759 0.90 526435. 0.3321
|
|
98.72 0.4623 0.7395 0.0588 0.0368 14.252 81.659 40.032 10627.409 9.226 178.064 1.709 0.90 527549. 0.3094
|
|
104.21 0.4880 0.7541 0.0535 0.0346 13.436 76.985 36.461 10019.093 8.698 162.177 1.651 0.91 528707. 0.2853
|
|
109.69 0.5137 0.7610 0.0482 0.0325 12.606 72.229 32.797 9400.162 8.160 145.879 1.582 0.91 529909. 0.2594
|
|
115.18 0.5394 0.7605 0.0427 0.0303 11.735 67.241 29.059 8750.989 7.597 129.253 1.506 0.91 531155. 0.2324
|
|
120.66 0.5651 0.7508 0.0371 0.0279 10.826 62.029 25.262 8072.689 7.008 112.368 1.419 0.91 532445. 0.2042
|
|
126.15 0.5907 0.7286 0.0315 0.0255 9.891 56.672 21.424 7375.421 6.403 95.295 1.318 0.91 533779. 0.1746
|
|
131.63 0.6164 0.6896 0.0258 0.0231 8.939 51.217 17.562 6665.487 5.786 78.116 1.195 0.91 535157. 0.1433
|
|
137.12 0.6421 0.6273 0.0201 0.0206 7.983 45.739 13.696 5952.551 5.168 60.921 1.044 0.91 536580. 0.1105
|
|
142.60 0.6678 0.5325 0.0145 0.0181 7.035 40.307 9.851 5245.717 4.554 43.815 0.852 0.91 538047. 0.0765
|
|
148.09 0.6935 0.3913 0.0089 0.0157 6.108 34.995 6.052 4554.403 3.954 26.917 0.603 0.92 539558. 0.0424
|
|
153.57 0.7192 0.1831 0.0034 0.0134 5.212 29.865 2.330 3886.717 3.374 10.365 0.272 0.92 541113. 0.0119
|
|
159.05 0.7448
|
|
|
|
|
|
|