649 lines
115 KiB
Plaintext
649 lines
115 KiB
Plaintext
13x5.5MR (13x55MR.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 0.0933 0.0375 0.001 0.069 0.084 0.820 0.008 0.372 46.275 0.05 19062. 0.6065
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0.24 0.0192 0.0467 0.0916 0.0376 0.001 0.069 0.082 0.821 0.008 0.365 45.339 0.05 19073. 0.5886
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0.47 0.0383 0.0915 0.0898 0.0376 0.001 0.069 0.080 0.822 0.008 0.358 44.390 0.05 19085. 0.5705
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0.71 0.0575 0.1343 0.0878 0.0376 0.001 0.069 0.079 0.822 0.008 0.350 43.433 0.05 19097. 0.5521
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0.94 0.0767 0.1751 0.0857 0.0376 0.001 0.069 0.077 0.821 0.008 0.342 42.469 0.05 19110. 0.5334
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1.18 0.0958 0.2138 0.0836 0.0375 0.001 0.069 0.075 0.819 0.008 0.333 41.494 0.05 19124. 0.5145
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1.41 0.1150 0.2504 0.0813 0.0373 0.001 0.069 0.073 0.816 0.008 0.324 40.503 0.05 19139. 0.4953
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1.65 0.1342 0.2849 0.0789 0.0371 0.001 0.069 0.071 0.812 0.008 0.314 39.501 0.05 19154. 0.4759
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1.88 0.1533 0.3172 0.0764 0.0369 0.001 0.068 0.068 0.807 0.008 0.304 38.480 0.05 19170. 0.4561
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2.12 0.1725 0.3472 0.0737 0.0366 0.001 0.068 0.066 0.800 0.008 0.294 37.438 0.05 19187. 0.4360
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2.35 0.1917 0.3748 0.0710 0.0363 0.001 0.067 0.064 0.793 0.008 0.283 36.373 0.05 19205. 0.4156
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2.59 0.2109 0.3999 0.0681 0.0359 0.001 0.066 0.061 0.784 0.007 0.271 35.278 0.05 19224. 0.3948
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2.82 0.2300 0.4223 0.0651 0.0354 0.001 0.065 0.058 0.775 0.007 0.259 34.149 0.05 19243. 0.3737
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3.06 0.2492 0.4418 0.0619 0.0349 0.001 0.065 0.056 0.763 0.007 0.247 32.982 0.05 19263. 0.3521
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3.29 0.2684 0.4582 0.0587 0.0344 0.001 0.063 0.053 0.751 0.007 0.234 31.763 0.05 19284. 0.3300
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3.53 0.2875 0.4713 0.0553 0.0337 0.001 0.062 0.050 0.737 0.007 0.220 30.490 0.05 19306. 0.3074
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3.76 0.3067 0.4807 0.0518 0.0330 0.001 0.061 0.046 0.722 0.007 0.206 29.155 0.05 19329. 0.2845
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4.00 0.3259 0.4861 0.0482 0.0323 0.001 0.060 0.043 0.705 0.007 0.192 27.751 0.05 19353. 0.2612
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4.23 0.3450 0.4872 0.0445 0.0315 0.001 0.058 0.040 0.688 0.007 0.177 26.267 0.05 19378. 0.2376
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4.47 0.3642 0.4835 0.0407 0.0306 0.001 0.057 0.036 0.670 0.006 0.162 24.693 0.05 19403. 0.2136
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4.70 0.3834 0.4744 0.0368 0.0297 0.001 0.055 0.033 0.650 0.006 0.147 23.016 0.05 19429. 0.1894
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4.94 0.4025 0.4593 0.0329 0.0288 0.001 0.053 0.029 0.629 0.006 0.131 21.222 0.05 19457. 0.1650
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5.17 0.4217 0.4374 0.0288 0.0278 0.001 0.051 0.026 0.608 0.006 0.115 19.293 0.05 19485. 0.1406
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5.41 0.4409 0.4079 0.0248 0.0268 0.001 0.049 0.022 0.585 0.006 0.099 17.209 0.05 19514. 0.1162
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5.64 0.4600 0.3696 0.0206 0.0257 0.001 0.047 0.018 0.561 0.005 0.082 14.946 0.05 19544. 0.0921
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5.88 0.4792 0.3214 0.0165 0.0246 0.001 0.045 0.015 0.537 0.005 0.066 12.477 0.05 19575. 0.0687
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6.11 0.4984 0.2617 0.0123 0.0234 0.001 0.043 0.011 0.511 0.005 0.049 9.768 0.05 19607. 0.0464
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6.35 0.5175 0.1887 0.0081 0.0222 0.001 0.041 0.007 0.484 0.005 0.032 6.781 0.05 19640. 0.0261
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6.58 0.5367 0.1002 0.0039 0.0209 0.001 0.039 0.003 0.457 0.004 0.016 3.471 0.05 19673. 0.0093
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6.82 0.5559 -0.0066 -0.0002 0.0196 0.001 0.036 0.000 0.429 0.004 -0.001 -0.219 0.05 19707. 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 0.0936 0.0345 0.008 0.255 0.336 6.034 0.029 1.493 25.222 0.10 38124. 0.6620
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0.47 0.0192 0.0511 0.0919 0.0346 0.008 0.256 0.329 6.050 0.029 1.465 24.685 0.10 38146. 0.6418
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0.94 0.0385 0.0999 0.0900 0.0347 0.008 0.256 0.323 6.062 0.029 1.435 24.144 0.10 38170. 0.6214
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1.42 0.0577 0.1465 0.0881 0.0347 0.008 0.256 0.316 6.066 0.029 1.404 23.603 0.10 38195. 0.6009
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1.89 0.0770 0.1909 0.0860 0.0347 0.008 0.256 0.308 6.061 0.029 1.371 23.063 0.10 38221. 0.5801
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2.36 0.0962 0.2330 0.0838 0.0346 0.008 0.256 0.300 6.050 0.029 1.336 22.521 0.10 38249. 0.5593
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2.83 0.1155 0.2728 0.0815 0.0345 0.008 0.255 0.292 6.030 0.029 1.300 21.976 0.10 38278. 0.5382
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3.30 0.1347 0.3103 0.0791 0.0343 0.008 0.254 0.283 6.000 0.029 1.261 21.429 0.10 38309. 0.5170
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3.78 0.1539 0.3455 0.0766 0.0341 0.008 0.252 0.274 5.962 0.028 1.221 20.878 0.10 38342. 0.4956
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4.25 0.1732 0.3784 0.0739 0.0338 0.008 0.250 0.265 5.913 0.028 1.178 20.320 0.10 38376. 0.4739
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4.72 0.1924 0.4087 0.0711 0.0335 0.008 0.247 0.255 5.855 0.028 1.134 19.756 0.10 38412. 0.4520
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5.19 0.2117 0.4365 0.0682 0.0331 0.008 0.244 0.245 5.784 0.028 1.088 19.181 0.10 38449. 0.4298
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5.66 0.2309 0.4616 0.0652 0.0326 0.008 0.241 0.234 5.702 0.027 1.040 18.595 0.10 38488. 0.4073
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6.14 0.2501 0.4840 0.0621 0.0321 0.008 0.237 0.222 5.608 0.027 0.989 17.994 0.10 38529. 0.3845
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6.61 0.2694 0.5031 0.0588 0.0315 0.007 0.232 0.211 5.500 0.026 0.937 17.371 0.10 38571. 0.3613
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7.08 0.2886 0.5191 0.0554 0.0308 0.007 0.227 0.198 5.381 0.026 0.883 16.726 0.10 38615. 0.3376
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7.55 0.3079 0.5314 0.0518 0.0300 0.007 0.222 0.186 5.250 0.025 0.827 16.054 0.10 38661. 0.3136
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8.02 0.3271 0.5399 0.0482 0.0292 0.007 0.216 0.173 5.109 0.024 0.769 15.350 0.10 38709. 0.2892
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8.49 0.3464 0.5440 0.0445 0.0284 0.007 0.209 0.160 4.956 0.024 0.710 14.608 0.10 38758. 0.2645
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8.97 0.3656 0.5433 0.0407 0.0274 0.006 0.203 0.146 4.792 0.023 0.650 13.822 0.10 38810. 0.2394
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9.44 0.3848 0.5372 0.0369 0.0264 0.006 0.195 0.132 4.618 0.022 0.588 12.983 0.10 38863. 0.2139
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9.91 0.4041 0.5249 0.0329 0.0254 0.006 0.187 0.118 4.432 0.021 0.525 12.081 0.10 38918. 0.1881
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10.38 0.4233 0.5053 0.0289 0.0242 0.006 0.179 0.104 4.236 0.020 0.461 11.103 0.10 38974. 0.1620
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10.85 0.4426 0.4774 0.0249 0.0230 0.005 0.170 0.089 4.029 0.019 0.396 10.032 0.10 39033. 0.1357
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11.33 0.4618 0.4395 0.0207 0.0218 0.005 0.161 0.074 3.811 0.018 0.331 8.850 0.10 39094. 0.1094
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11.80 0.4811 0.3895 0.0166 0.0205 0.005 0.151 0.060 3.584 0.017 0.265 7.531 0.10 39156. 0.0832
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12.27 0.5003 0.3250 0.0124 0.0191 0.004 0.141 0.045 3.347 0.016 0.198 6.041 0.10 39220. 0.0578
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12.74 0.5195 0.2423 0.0083 0.0177 0.004 0.131 0.030 3.102 0.015 0.132 4.338 0.10 39286. 0.0339
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13.21 0.5388 0.1369 0.0041 0.0163 0.004 0.120 0.015 2.849 0.014 0.066 2.363 0.10 39354. 0.0130
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13.69 0.5580 0.0018 0.0000 0.0148 0.003 0.109 0.000 2.589 0.012 0.001 0.030 0.10 39422. 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 0.0938 0.0332 0.026 0.552 0.757 19.591 0.062 3.367 17.523 0.15 57185. 0.6908
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0.71 0.0193 0.0534 0.0921 0.0333 0.026 0.554 0.743 19.654 0.063 3.303 17.140 0.15 57218. 0.6693
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1.42 0.0386 0.1043 0.0902 0.0334 0.026 0.555 0.728 19.700 0.063 3.237 16.756 0.15 57254. 0.6477
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2.13 0.0579 0.1529 0.0883 0.0334 0.026 0.556 0.712 19.722 0.063 3.167 16.372 0.15 57292. 0.6259
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2.84 0.0772 0.1991 0.0862 0.0334 0.026 0.555 0.695 19.712 0.063 3.091 15.992 0.15 57331. 0.6041
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3.55 0.0965 0.2430 0.0840 0.0334 0.026 0.554 0.677 19.680 0.063 3.013 15.612 0.15 57373. 0.5822
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4.26 0.1158 0.2845 0.0817 0.0333 0.026 0.553 0.659 19.620 0.062 2.930 15.231 0.15 57418. 0.5602
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4.97 0.1351 0.3236 0.0792 0.0331 0.026 0.550 0.639 19.521 0.062 2.843 14.851 0.15 57464. 0.5380
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5.68 0.1544 0.3603 0.0767 0.0329 0.026 0.546 0.619 19.396 0.062 2.752 14.469 0.15 57513. 0.5157
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6.39 0.1737 0.3946 0.0740 0.0326 0.026 0.542 0.597 19.230 0.061 2.656 14.086 0.15 57565. 0.4932
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7.10 0.1930 0.4264 0.0713 0.0323 0.026 0.536 0.575 19.031 0.061 2.557 13.699 0.15 57619. 0.4706
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7.81 0.2123 0.4557 0.0683 0.0318 0.025 0.529 0.551 18.787 0.060 2.452 13.308 0.15 57675. 0.4477
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8.52 0.2316 0.4823 0.0653 0.0314 0.025 0.521 0.527 18.504 0.059 2.343 12.911 0.15 57734. 0.4246
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9.23 0.2509 0.5061 0.0621 0.0308 0.024 0.512 0.501 18.177 0.058 2.229 12.506 0.15 57795. 0.4011
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9.94 0.2702 0.5268 0.0588 0.0302 0.024 0.502 0.474 17.802 0.057 2.110 12.088 0.15 57859. 0.3773
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10.65 0.2895 0.5443 0.0554 0.0295 0.023 0.490 0.447 17.385 0.055 1.987 11.658 0.15 57926. 0.3531
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11.36 0.3088 0.5584 0.0519 0.0287 0.023 0.477 0.418 16.926 0.054 1.861 11.211 0.15 57995. 0.3286
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12.07 0.3281 0.5686 0.0482 0.0278 0.022 0.463 0.389 16.427 0.052 1.731 10.744 0.15 58067. 0.3037
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12.78 0.3474 0.5746 0.0445 0.0269 0.021 0.448 0.359 15.886 0.051 1.598 10.254 0.16 58142. 0.2785
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13.49 0.3667 0.5758 0.0407 0.0259 0.021 0.431 0.329 15.305 0.049 1.461 9.735 0.16 58219. 0.2528
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14.20 0.3860 0.5716 0.0369 0.0249 0.020 0.414 0.297 14.683 0.047 1.322 9.181 0.16 58299. 0.2268
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14.91 0.4053 0.5612 0.0329 0.0238 0.019 0.395 0.265 14.020 0.045 1.180 8.584 0.16 58382. 0.2004
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15.62 0.4246 0.5434 0.0289 0.0226 0.018 0.375 0.233 13.317 0.042 1.036 7.934 0.16 58468. 0.1735
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16.33 0.4439 0.5168 0.0248 0.0213 0.017 0.354 0.200 12.574 0.040 0.890 7.218 0.16 58556. 0.1463
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17.04 0.4632 0.4796 0.0207 0.0200 0.016 0.332 0.167 11.793 0.038 0.742 6.420 0.16 58647. 0.1188
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17.75 0.4825 0.4293 0.0165 0.0186 0.015 0.309 0.133 10.974 0.035 0.594 5.516 0.16 58741. 0.0913
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18.46 0.5018 0.3624 0.0124 0.0172 0.014 0.285 0.100 10.121 0.032 0.444 4.477 0.16 58838. 0.0641
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19.17 0.5211 0.2741 0.0082 0.0157 0.012 0.260 0.066 9.236 0.029 0.295 3.261 0.16 58938. 0.0381
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19.88 0.5404 0.1574 0.0041 0.0141 0.011 0.234 0.033 8.323 0.026 0.147 1.806 0.16 59040. 0.0149
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20.59 0.5597 0.0011 0.0000 0.0125 0.010 0.208 0.000 7.383 0.024 0.001 0.012 0.16 59142. 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 0.0941 0.0325 0.061 0.959 1.349 45.403 0.108 6.002 13.479 0.21 76245. 0.7095
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0.95 0.0193 0.0548 0.0923 0.0326 0.061 0.963 1.324 45.564 0.109 5.889 13.180 0.21 76290. 0.6872
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1.90 0.0387 0.1071 0.0905 0.0327 0.061 0.965 1.297 45.687 0.109 5.771 12.880 0.21 76338. 0.6648
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2.85 0.0580 0.1570 0.0885 0.0327 0.061 0.967 1.269 45.749 0.109 5.645 12.582 0.21 76388. 0.6423
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3.80 0.0774 0.2044 0.0864 0.0327 0.061 0.966 1.239 45.735 0.109 5.511 12.287 0.21 76441. 0.6197
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4.74 0.0967 0.2494 0.0842 0.0327 0.061 0.965 1.207 45.666 0.109 5.371 11.993 0.21 76498. 0.5971
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5.69 0.1161 0.2920 0.0819 0.0326 0.061 0.962 1.174 45.529 0.109 5.224 11.699 0.21 76557. 0.5745
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6.64 0.1354 0.3321 0.0795 0.0324 0.061 0.957 1.139 45.297 0.108 5.067 11.407 0.21 76619. 0.5517
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7.59 0.1547 0.3698 0.0769 0.0322 0.060 0.951 1.103 45.003 0.107 4.905 11.115 0.21 76685. 0.5289
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8.54 0.1741 0.4051 0.0742 0.0319 0.060 0.943 1.064 44.606 0.106 4.734 10.822 0.21 76754. 0.5059
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9.49 0.1934 0.4379 0.0714 0.0316 0.059 0.932 1.024 44.128 0.105 4.556 10.528 0.21 76826. 0.4828
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10.44 0.2128 0.4681 0.0685 0.0311 0.058 0.920 0.982 43.541 0.104 4.369 10.231 0.21 76901. 0.4594
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11.39 0.2321 0.4957 0.0654 0.0306 0.057 0.906 0.938 42.857 0.102 4.174 9.931 0.21 76980. 0.4359
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12.33 0.2514 0.5205 0.0623 0.0301 0.056 0.889 0.893 42.066 0.100 3.971 9.626 0.21 77062. 0.4121
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13.28 0.2708 0.5423 0.0589 0.0294 0.055 0.870 0.845 41.157 0.098 3.759 9.312 0.21 77148. 0.3879
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14.23 0.2901 0.5609 0.0555 0.0287 0.054 0.848 0.796 40.142 0.096 3.539 8.990 0.21 77237. 0.3634
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15.18 0.3095 0.5761 0.0519 0.0279 0.052 0.825 0.745 39.024 0.093 3.313 8.657 0.21 77330. 0.3385
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16.13 0.3288 0.5876 0.0483 0.0270 0.051 0.799 0.693 37.803 0.090 3.081 8.310 0.21 77426. 0.3134
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17.08 0.3482 0.5949 0.0446 0.0261 0.049 0.771 0.639 36.481 0.087 2.843 7.947 0.21 77526. 0.2879
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18.03 0.3675 0.5976 0.0408 0.0251 0.047 0.741 0.584 35.056 0.084 2.600 7.562 0.21 77629. 0.2619
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18.98 0.3868 0.5949 0.0369 0.0240 0.045 0.708 0.529 33.528 0.080 2.351 7.151 0.21 77737. 0.2356
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19.92 0.4062 0.5859 0.0329 0.0228 0.043 0.674 0.472 31.898 0.076 2.098 6.708 0.21 77847. 0.2088
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20.87 0.4255 0.5696 0.0289 0.0216 0.040 0.637 0.414 30.168 0.072 1.842 6.225 0.21 77962. 0.1815
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21.82 0.4449 0.5443 0.0248 0.0203 0.038 0.599 0.355 28.338 0.068 1.581 5.690 0.21 78080. 0.1537
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22.77 0.4642 0.5080 0.0207 0.0189 0.035 0.558 0.296 26.410 0.063 1.318 5.089 0.21 78202. 0.1255
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23.72 0.4835 0.4579 0.0165 0.0174 0.033 0.515 0.237 24.390 0.058 1.053 4.403 0.21 78328. 0.0971
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24.67 0.5029 0.3897 0.0123 0.0159 0.030 0.471 0.177 22.282 0.053 0.787 3.604 0.21 78458. 0.0687
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25.62 0.5222 0.2977 0.0082 0.0144 0.027 0.425 0.117 20.094 0.048 0.522 2.651 0.21 78592. 0.0412
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26.57 0.5416 0.1726 0.0041 0.0128 0.024 0.377 0.058 17.837 0.043 0.259 1.482 0.21 78728. 0.0162
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27.51 0.5609 -0.0011 0.0000 0.0111 0.021 0.328 0.000 15.511 0.037 -0.001 -0.009 0.21 78863. 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 0.0944 0.0320 0.117 1.478 2.115 87.446 0.167 9.409 10.972 0.26 95305. 0.7231
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1.19 0.0193 0.0558 0.0926 0.0321 0.118 1.484 2.076 87.776 0.168 9.232 10.726 0.26 95361. 0.7002
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2.37 0.0387 0.1090 0.0908 0.0322 0.118 1.488 2.034 88.029 0.168 9.047 10.480 0.26 95420. 0.6772
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3.56 0.0580 0.1597 0.0888 0.0323 0.118 1.490 1.990 88.165 0.168 8.850 10.236 0.26 95483. 0.6542
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4.75 0.0774 0.2079 0.0867 0.0323 0.118 1.490 1.942 88.149 0.168 8.640 9.995 0.26 95550. 0.6312
|
|
5.93 0.0967 0.2537 0.0845 0.0322 0.118 1.488 1.893 88.022 0.168 8.421 9.755 0.26 95621. 0.6082
|
|
7.12 0.1161 0.2970 0.0822 0.0321 0.118 1.484 1.841 87.761 0.168 8.190 9.516 0.26 95695. 0.5851
|
|
8.30 0.1354 0.3378 0.0797 0.0320 0.117 1.476 1.786 87.311 0.167 7.945 9.279 0.26 95773. 0.5619
|
|
9.49 0.1548 0.3762 0.0772 0.0318 0.116 1.466 1.729 86.734 0.166 7.691 9.042 0.26 95855. 0.5388
|
|
10.68 0.1741 0.4122 0.0745 0.0315 0.115 1.453 1.669 85.955 0.164 7.422 8.806 0.26 95941. 0.5154
|
|
11.86 0.1935 0.4457 0.0717 0.0311 0.114 1.437 1.606 85.013 0.162 7.143 8.568 0.26 96032. 0.4920
|
|
13.05 0.2128 0.4766 0.0687 0.0307 0.112 1.417 1.540 83.852 0.160 6.850 8.330 0.26 96126. 0.4684
|
|
14.24 0.2322 0.5049 0.0657 0.0302 0.111 1.395 1.471 82.498 0.158 6.544 8.089 0.26 96225. 0.4446
|
|
15.42 0.2515 0.5305 0.0625 0.0296 0.109 1.368 1.400 80.928 0.155 6.226 7.845 0.26 96328. 0.4206
|
|
16.61 0.2709 0.5531 0.0591 0.0290 0.106 1.338 1.325 79.122 0.151 5.894 7.596 0.26 96435. 0.3962
|
|
17.80 0.2902 0.5726 0.0557 0.0282 0.103 1.303 1.248 77.103 0.147 5.550 7.340 0.26 96547. 0.3715
|
|
18.98 0.3096 0.5888 0.0521 0.0274 0.100 1.266 1.168 74.876 0.143 5.195 7.076 0.26 96663. 0.3465
|
|
20.17 0.3289 0.6014 0.0485 0.0265 0.097 1.225 1.086 72.441 0.138 4.832 6.801 0.26 96783. 0.3212
|
|
21.36 0.3483 0.6098 0.0447 0.0256 0.094 1.180 1.002 69.800 0.133 4.459 6.514 0.26 96908. 0.2955
|
|
22.54 0.3676 0.6137 0.0409 0.0245 0.090 1.132 0.917 66.951 0.128 4.078 6.211 0.26 97038. 0.2694
|
|
23.73 0.3870 0.6124 0.0370 0.0234 0.086 1.080 0.829 63.895 0.122 3.689 5.887 0.26 97172. 0.2429
|
|
24.91 0.4063 0.6049 0.0330 0.0222 0.081 1.025 0.740 60.631 0.116 3.293 5.538 0.26 97310. 0.2159
|
|
26.10 0.4257 0.5900 0.0290 0.0209 0.077 0.966 0.650 57.162 0.109 2.890 5.156 0.26 97454. 0.1883
|
|
27.29 0.4450 0.5662 0.0249 0.0196 0.072 0.904 0.558 53.492 0.102 2.483 4.733 0.26 97602. 0.1602
|
|
28.47 0.4644 0.5312 0.0208 0.0182 0.067 0.839 0.466 49.624 0.095 2.071 4.256 0.26 97754. 0.1316
|
|
29.66 0.4837 0.4820 0.0166 0.0167 0.061 0.770 0.372 45.567 0.087 1.656 3.707 0.26 97912. 0.1025
|
|
30.85 0.5031 0.4139 0.0124 0.0151 0.055 0.699 0.279 41.333 0.079 1.241 3.061 0.26 98074. 0.0732
|
|
32.03 0.5224 0.3202 0.0083 0.0135 0.050 0.624 0.186 36.937 0.071 0.826 2.280 0.26 98241. 0.0445
|
|
33.22 0.5418 0.1900 0.0042 0.0119 0.043 0.548 0.093 32.402 0.062 0.414 1.304 0.26 98412. 0.0180
|
|
34.41 0.5611 0.0037 0.0001 0.0101 0.037 0.469 0.001 27.724 0.053 0.007 0.025 0.26 98581. 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 0.0948 0.0317 0.201 2.111 3.058 149.819 0.238 13.602 9.258 0.31 114363. 0.7336
|
|
1.43 0.0194 0.0566 0.0930 0.0319 0.202 2.119 3.001 150.410 0.239 13.347 9.048 0.31 114430. 0.7102
|
|
2.85 0.0388 0.1106 0.0911 0.0320 0.202 2.125 2.940 150.863 0.240 13.078 8.840 0.31 114502. 0.6868
|
|
4.28 0.0582 0.1620 0.0892 0.0320 0.203 2.129 2.876 151.113 0.241 12.793 8.633 0.31 114578. 0.6634
|
|
5.71 0.0776 0.2109 0.0870 0.0320 0.203 2.129 2.808 151.096 0.240 12.489 8.429 0.31 114659. 0.6400
|
|
7.13 0.0970 0.2573 0.0848 0.0320 0.202 2.125 2.736 150.878 0.240 12.172 8.226 0.31 114743. 0.6166
|
|
8.56 0.1164 0.3012 0.0825 0.0319 0.202 2.119 2.661 150.428 0.239 11.837 8.024 0.31 114833. 0.5931
|
|
9.99 0.1357 0.3426 0.0800 0.0317 0.201 2.108 2.582 149.643 0.238 11.483 7.825 0.31 114927. 0.5696
|
|
11.41 0.1551 0.3816 0.0775 0.0315 0.199 2.094 2.499 148.632 0.237 11.115 7.625 0.31 115026. 0.5462
|
|
12.84 0.1745 0.4181 0.0747 0.0312 0.197 2.075 2.411 147.265 0.234 10.726 7.427 0.31 115130. 0.5226
|
|
14.27 0.1939 0.4521 0.0719 0.0308 0.195 2.051 2.320 145.606 0.232 10.321 7.228 0.31 115239. 0.4989
|
|
15.70 0.2133 0.4836 0.0690 0.0304 0.193 2.022 2.225 143.564 0.228 9.896 7.029 0.31 115353. 0.4750
|
|
17.12 0.2327 0.5125 0.0659 0.0299 0.189 1.989 2.125 141.176 0.225 9.453 6.828 0.31 115472. 0.4510
|
|
18.55 0.2521 0.5387 0.0627 0.0293 0.186 1.950 2.022 138.406 0.220 8.992 6.625 0.31 115596. 0.4268
|
|
19.98 0.2715 0.5620 0.0593 0.0286 0.181 1.905 1.913 135.219 0.215 8.509 6.417 0.31 115725. 0.4022
|
|
21.40 0.2909 0.5822 0.0558 0.0279 0.177 1.855 1.801 131.653 0.210 8.011 6.205 0.31 115860. 0.3773
|
|
22.83 0.3103 0.5991 0.0522 0.0271 0.171 1.799 1.686 127.717 0.203 7.497 5.986 0.31 115999. 0.3521
|
|
24.26 0.3297 0.6124 0.0486 0.0261 0.165 1.739 1.567 123.412 0.196 6.970 5.759 0.31 116145. 0.3267
|
|
25.68 0.3491 0.6217 0.0448 0.0252 0.159 1.673 1.446 118.737 0.189 6.430 5.522 0.31 116295. 0.3008
|
|
27.11 0.3685 0.6265 0.0410 0.0241 0.152 1.602 1.321 113.692 0.181 5.877 5.271 0.31 116451. 0.2746
|
|
28.54 0.3878 0.6261 0.0370 0.0229 0.145 1.525 1.195 108.276 0.172 5.314 5.004 0.31 116613. 0.2478
|
|
29.96 0.4072 0.6195 0.0330 0.0217 0.137 1.444 1.066 102.491 0.163 4.740 4.716 0.31 116780. 0.2206
|
|
31.39 0.4266 0.6056 0.0290 0.0204 0.129 1.357 0.935 96.340 0.153 4.157 4.401 0.31 116953. 0.1928
|
|
32.82 0.4460 0.5826 0.0249 0.0190 0.120 1.265 0.802 89.828 0.143 3.567 4.050 0.31 117131. 0.1643
|
|
34.24 0.4654 0.5482 0.0207 0.0176 0.111 1.169 0.668 82.965 0.132 2.971 3.652 0.31 117315. 0.1352
|
|
35.67 0.4848 0.4990 0.0165 0.0161 0.102 1.067 0.533 75.765 0.121 2.371 3.191 0.31 117505. 0.1056
|
|
37.10 0.5042 0.4300 0.0123 0.0145 0.092 0.961 0.398 68.249 0.109 1.770 2.644 0.31 117701. 0.0756
|
|
38.52 0.5236 0.3333 0.0082 0.0128 0.081 0.852 0.263 60.447 0.096 1.170 1.973 0.31 117902. 0.0458
|
|
39.95 0.5430 0.1961 0.0040 0.0111 0.070 0.738 0.129 52.400 0.083 0.575 1.119 0.31 118108. 0.0182
|
|
41.38 0.5624 -0.0065 -0.0001 0.0093 0.059 0.621 -0.003 44.079 0.070 -0.016 -0.036 0.31 118308. 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 0.0952 0.0316 0.318 2.859 4.181 236.809 0.323 18.599 8.009 0.36 133419. 0.7421
|
|
1.69 0.0197 0.0579 0.0934 0.0317 0.319 2.871 4.102 237.780 0.324 18.246 7.825 0.36 133499. 0.7181
|
|
3.38 0.0393 0.1131 0.0915 0.0318 0.320 2.880 4.018 238.520 0.325 17.874 7.641 0.36 133584. 0.6941
|
|
5.06 0.0590 0.1656 0.0895 0.0319 0.320 2.885 3.930 238.927 0.326 17.479 7.460 0.36 133675. 0.6700
|
|
6.75 0.0786 0.2155 0.0873 0.0319 0.320 2.885 3.835 238.892 0.326 17.057 7.281 0.36 133770. 0.6460
|
|
8.44 0.0983 0.2628 0.0851 0.0318 0.320 2.880 3.736 238.521 0.325 16.616 7.103 0.36 133871. 0.6221
|
|
10.12 0.1180 0.3075 0.0827 0.0317 0.319 2.871 3.631 237.753 0.324 16.151 6.927 0.36 133978. 0.5981
|
|
11.81 0.1376 0.3497 0.0802 0.0315 0.317 2.855 3.520 236.439 0.323 15.657 6.753 0.36 134090. 0.5741
|
|
13.50 0.1573 0.3894 0.0775 0.0313 0.315 2.834 3.405 234.744 0.320 15.145 6.579 0.36 134208. 0.5501
|
|
15.19 0.1769 0.4265 0.0748 0.0310 0.312 2.807 3.283 232.448 0.317 14.603 6.406 0.36 134331. 0.5259
|
|
16.88 0.1966 0.4611 0.0719 0.0306 0.308 2.773 3.156 229.668 0.313 14.039 6.233 0.36 134461. 0.5018
|
|
18.56 0.2162 0.4932 0.0688 0.0302 0.303 2.732 3.023 226.263 0.309 13.447 6.060 0.36 134597. 0.4775
|
|
20.25 0.2359 0.5225 0.0657 0.0297 0.298 2.684 2.884 222.249 0.303 12.828 5.886 0.36 134739. 0.4529
|
|
21.94 0.2556 0.5491 0.0624 0.0290 0.292 2.628 2.739 217.609 0.297 12.185 5.710 0.36 134887. 0.4282
|
|
23.62 0.2752 0.5727 0.0589 0.0283 0.285 2.563 2.588 212.280 0.290 11.512 5.530 0.36 135041. 0.4031
|
|
25.31 0.2949 0.5932 0.0554 0.0275 0.277 2.491 2.432 206.325 0.281 10.817 5.346 0.36 135201. 0.3777
|
|
27.00 0.3145 0.6103 0.0517 0.0267 0.268 2.412 2.271 199.753 0.272 10.101 5.156 0.36 135368. 0.3521
|
|
28.69 0.3342 0.6238 0.0480 0.0257 0.258 2.325 2.106 192.564 0.263 9.366 4.960 0.36 135542. 0.3261
|
|
30.38 0.3539 0.6330 0.0441 0.0247 0.248 2.231 1.936 184.759 0.252 8.613 4.754 0.36 135721. 0.2997
|
|
32.06 0.3735 0.6376 0.0402 0.0235 0.236 2.129 1.763 176.335 0.241 7.844 4.536 0.36 135908. 0.2729
|
|
33.75 0.3932 0.6366 0.0361 0.0223 0.224 2.020 1.587 167.293 0.228 7.059 4.303 0.36 136101. 0.2456
|
|
35.44 0.4128 0.6292 0.0321 0.0210 0.211 1.903 1.408 157.634 0.215 6.261 4.050 0.36 136300. 0.2177
|
|
37.12 0.4325 0.6138 0.0279 0.0197 0.198 1.779 1.225 147.366 0.201 5.450 3.771 0.36 136507. 0.1892
|
|
38.81 0.4521 0.5885 0.0237 0.0182 0.183 1.648 1.041 136.500 0.186 4.630 3.459 0.36 136720. 0.1599
|
|
40.50 0.4718 0.5504 0.0195 0.0167 0.168 1.510 0.855 125.053 0.171 3.802 3.100 0.36 136940. 0.1299
|
|
42.19 0.4915 0.4954 0.0152 0.0151 0.152 1.365 0.668 113.055 0.154 2.970 2.679 0.36 137167. 0.0992
|
|
43.88 0.5111 0.4169 0.0109 0.0134 0.135 1.214 0.480 100.545 0.137 2.137 2.167 0.36 137400. 0.0681
|
|
45.56 0.5308 0.3043 0.0067 0.0117 0.117 1.057 0.294 87.579 0.119 1.308 1.523 0.36 137640. 0.0374
|
|
47.25 0.5504 0.1392 0.0025 0.0099 0.100 0.896 0.110 74.228 0.101 0.489 0.672 0.37 137885. 0.0101
|
|
48.94 0.5701
|
|
|
|
|
|
|
|
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 0.0957 0.0315 0.473 3.729 5.491 352.957 0.421 24.422 7.056 0.41 152473. 0.7491
|
|
1.93 0.0197 0.0583 0.0939 0.0317 0.475 3.745 5.386 354.434 0.423 23.959 6.893 0.41 152565. 0.7249
|
|
3.86 0.0394 0.1139 0.0920 0.0318 0.477 3.756 5.277 355.550 0.424 23.471 6.732 0.41 152663. 0.7007
|
|
5.79 0.0590 0.1668 0.0900 0.0318 0.478 3.763 5.160 356.176 0.425 22.953 6.571 0.41 152766. 0.6764
|
|
7.72 0.0787 0.2171 0.0878 0.0318 0.478 3.763 5.036 356.127 0.425 22.399 6.414 0.41 152876. 0.6522
|
|
9.65 0.0984 0.2648 0.0855 0.0318 0.477 3.757 4.906 355.554 0.424 21.820 6.258 0.41 152992. 0.6280
|
|
11.58 0.1181 0.3098 0.0831 0.0317 0.475 3.744 4.768 354.391 0.423 21.210 6.103 0.41 153114. 0.6038
|
|
13.51 0.1377 0.3524 0.0806 0.0315 0.473 3.723 4.623 352.393 0.421 20.561 5.950 0.41 153242. 0.5796
|
|
15.44 0.1574 0.3925 0.0780 0.0313 0.469 3.696 4.471 349.810 0.418 19.889 5.798 0.41 153377. 0.5555
|
|
17.37 0.1771 0.4300 0.0752 0.0310 0.464 3.659 4.311 346.321 0.413 19.176 5.646 0.41 153519. 0.5312
|
|
19.30 0.1968 0.4650 0.0723 0.0306 0.459 3.614 4.145 342.092 0.408 18.435 5.495 0.41 153668. 0.5069
|
|
21.23 0.2164 0.4974 0.0692 0.0301 0.452 3.560 3.970 336.911 0.402 17.657 5.344 0.41 153824. 0.4825
|
|
23.16 0.2361 0.5272 0.0660 0.0296 0.444 3.495 3.787 330.808 0.395 16.844 5.192 0.41 153986. 0.4578
|
|
25.09 0.2558 0.5543 0.0627 0.0289 0.434 3.421 3.597 323.752 0.386 15.998 5.039 0.41 154156. 0.4330
|
|
27.02 0.2755 0.5784 0.0592 0.0282 0.423 3.335 3.398 315.647 0.377 15.113 4.882 0.41 154333. 0.4078
|
|
28.95 0.2951 0.5994 0.0557 0.0274 0.411 3.239 3.192 306.588 0.366 14.199 4.723 0.41 154517. 0.3823
|
|
30.88 0.3148 0.6172 0.0520 0.0265 0.398 3.134 2.981 296.589 0.354 13.259 4.558 0.41 154708. 0.3566
|
|
32.81 0.3345 0.6313 0.0482 0.0255 0.383 3.018 2.764 285.651 0.341 12.293 4.388 0.41 154906. 0.3305
|
|
34.74 0.3542 0.6412 0.0443 0.0245 0.367 2.892 2.541 273.771 0.327 11.303 4.210 0.41 155112. 0.3041
|
|
36.67 0.3738 0.6466 0.0403 0.0233 0.350 2.757 2.314 260.947 0.311 10.292 4.022 0.41 155326. 0.2772
|
|
38.60 0.3935 0.6465 0.0363 0.0221 0.331 2.612 2.082 247.181 0.295 9.260 3.820 0.41 155547. 0.2498
|
|
40.53 0.4132 0.6400 0.0322 0.0208 0.312 2.456 1.846 232.474 0.277 8.211 3.602 0.41 155775. 0.2217
|
|
42.46 0.4329 0.6256 0.0280 0.0194 0.291 2.291 1.606 216.838 0.259 7.146 3.360 0.41 156012. 0.1930
|
|
44.39 0.4525 0.6012 0.0238 0.0179 0.269 2.116 1.364 200.289 0.239 6.067 3.089 0.42 156256. 0.1635
|
|
46.32 0.4722 0.5639 0.0195 0.0163 0.245 1.932 1.120 182.857 0.218 4.980 2.777 0.42 156508. 0.1331
|
|
48.25 0.4919 0.5094 0.0152 0.0147 0.221 1.739 0.874 164.585 0.196 3.886 2.408 0.42 156767. 0.1020
|
|
50.18 0.5116 0.4304 0.0109 0.0130 0.195 1.538 0.628 145.533 0.174 2.792 1.956 0.42 157035. 0.0702
|
|
52.12 0.5312 0.3156 0.0067 0.0112 0.169 1.329 0.383 125.790 0.150 1.704 1.381 0.42 157310. 0.0387
|
|
54.05 0.5509 0.1439 0.0025 0.0094 0.141 1.114 0.141 105.462 0.126 0.628 0.607 0.42 157589. 0.0103
|
|
55.98 0.5706
|
|
|
|
|
|
|
|
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 0.0963 0.0316 0.675 4.725 6.992 503.140 0.534 31.099 6.303 0.46 171525. 0.7552
|
|
2.16 0.0195 0.0582 0.0945 0.0317 0.678 4.745 6.860 505.262 0.536 30.515 6.159 0.46 171628. 0.7309
|
|
4.31 0.0391 0.1137 0.0926 0.0318 0.680 4.760 6.722 506.847 0.538 29.900 6.015 0.46 171737. 0.7067
|
|
6.47 0.0586 0.1666 0.0906 0.0319 0.681 4.769 6.575 507.768 0.539 29.248 5.874 0.46 171853. 0.6825
|
|
8.62 0.0781 0.2168 0.0884 0.0319 0.681 4.768 6.419 507.716 0.539 28.550 5.734 0.46 171976. 0.6582
|
|
10.78 0.0977 0.2645 0.0862 0.0318 0.680 4.760 6.254 506.885 0.538 27.818 5.596 0.46 172105. 0.6341
|
|
12.94 0.1172 0.3096 0.0838 0.0317 0.678 4.745 6.081 505.259 0.536 27.050 5.459 0.46 172242. 0.6100
|
|
15.09 0.1368 0.3523 0.0812 0.0315 0.674 4.718 5.898 502.422 0.533 26.233 5.324 0.46 172385. 0.5859
|
|
17.25 0.1563 0.3925 0.0786 0.0313 0.669 4.684 5.707 498.736 0.529 25.385 5.190 0.46 172536. 0.5618
|
|
19.41 0.1758 0.4302 0.0758 0.0310 0.662 4.637 5.505 493.792 0.524 24.487 5.057 0.46 172695. 0.5376
|
|
21.56 0.1954 0.4654 0.0730 0.0306 0.654 4.581 5.295 487.778 0.518 23.554 4.924 0.46 172861. 0.5134
|
|
23.72 0.2149 0.4982 0.0699 0.0302 0.644 4.512 5.075 480.390 0.510 22.572 4.791 0.46 173034. 0.4891
|
|
25.87 0.2344 0.5284 0.0667 0.0296 0.633 4.430 4.845 471.740 0.501 21.549 4.658 0.46 173216. 0.4645
|
|
28.03 0.2540 0.5559 0.0634 0.0290 0.619 4.336 4.605 461.711 0.490 20.483 4.524 0.46 173405. 0.4399
|
|
30.19 0.2735 0.5806 0.0600 0.0283 0.604 4.228 4.354 450.183 0.478 19.369 4.387 0.46 173602. 0.4148
|
|
32.34 0.2930 0.6023 0.0564 0.0275 0.586 4.107 4.095 437.286 0.464 18.217 4.248 0.46 173807. 0.3895
|
|
34.50 0.3126 0.6209 0.0527 0.0266 0.567 3.973 3.829 423.044 0.449 17.030 4.105 0.46 174020. 0.3640
|
|
36.65 0.3321 0.6359 0.0490 0.0256 0.546 3.827 3.555 407.460 0.432 15.812 3.957 0.46 174241. 0.3381
|
|
38.81 0.3517 0.6471 0.0451 0.0245 0.524 3.668 3.274 390.530 0.414 14.565 3.803 0.47 174470. 0.3118
|
|
40.97 0.3712 0.6538 0.0412 0.0234 0.499 3.496 2.988 372.252 0.395 13.289 3.640 0.47 174708. 0.2851
|
|
43.12 0.3907 0.6554 0.0371 0.0221 0.473 3.312 2.695 352.626 0.374 11.988 3.467 0.47 174954. 0.2579
|
|
45.28 0.4103 0.6509 0.0330 0.0208 0.445 3.115 2.398 331.654 0.352 10.664 3.279 0.47 175208. 0.2300
|
|
47.44 0.4298 0.6389 0.0289 0.0194 0.415 2.905 2.095 309.351 0.328 9.320 3.072 0.47 175471. 0.2015
|
|
49.59 0.4493 0.6175 0.0246 0.0179 0.383 2.683 1.789 285.739 0.303 7.959 2.840 0.47 175742. 0.1721
|
|
51.75 0.4689 0.5840 0.0204 0.0164 0.350 2.450 1.480 260.857 0.277 6.585 2.574 0.47 176022. 0.1419
|
|
53.90 0.4884 0.5341 0.0161 0.0147 0.315 2.205 1.170 234.761 0.249 5.203 2.260 0.47 176311. 0.1108
|
|
56.06 0.5079 0.4612 0.0118 0.0130 0.278 1.949 0.859 207.536 0.220 3.819 1.877 0.47 176608. 0.0788
|
|
58.22 0.5275 0.3543 0.0076 0.0113 0.240 1.684 0.549 179.298 0.190 2.441 1.388 0.47 176914. 0.0466
|
|
60.37 0.5470 0.1936 0.0033 0.0094 0.201 1.411 0.242 150.201 0.159 1.077 0.731 0.47 177226. 0.0163
|
|
62.53 0.5666
|
|
|
|
|
|
|
|
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 0.0970 0.0317 0.929 5.855 8.692 692.677 0.661 38.664 5.692 0.51 190574. 0.7604
|
|
2.38 0.0194 0.0580 0.0952 0.0318 0.933 5.879 8.531 695.605 0.664 37.945 5.563 0.51 190688. 0.7362
|
|
4.76 0.0388 0.1134 0.0933 0.0319 0.936 5.898 8.360 697.767 0.666 37.187 5.434 0.51 190809. 0.7120
|
|
7.14 0.0582 0.1661 0.0913 0.0320 0.937 5.909 8.180 699.052 0.668 36.385 5.308 0.51 190937. 0.6878
|
|
9.52 0.0776 0.2163 0.0891 0.0320 0.937 5.908 7.987 698.994 0.667 35.526 5.183 0.51 191073. 0.6637
|
|
11.90 0.0970 0.2639 0.0869 0.0319 0.936 5.898 7.784 697.819 0.666 34.624 5.060 0.51 191216. 0.6396
|
|
14.28 0.1164 0.3091 0.0845 0.0318 0.933 5.879 7.572 695.598 0.664 33.680 4.937 0.51 191366. 0.6156
|
|
16.66 0.1358 0.3518 0.0820 0.0317 0.928 5.846 7.346 691.700 0.661 32.674 4.817 0.51 191525. 0.5915
|
|
19.04 0.1553 0.3921 0.0793 0.0314 0.921 5.803 7.111 686.594 0.656 31.629 4.697 0.51 191692. 0.5676
|
|
21.42 0.1747 0.4299 0.0766 0.0311 0.912 5.746 6.863 679.823 0.649 30.525 4.579 0.51 191867. 0.5435
|
|
23.80 0.1941 0.4654 0.0737 0.0307 0.901 5.676 6.604 671.545 0.641 29.376 4.461 0.51 192050. 0.5194
|
|
26.18 0.2135 0.4984 0.0707 0.0303 0.887 5.590 6.332 661.379 0.632 28.166 4.343 0.51 192241. 0.4952
|
|
28.56 0.2329 0.5289 0.0675 0.0297 0.871 5.490 6.049 649.517 0.620 26.908 4.224 0.52 192441. 0.4708
|
|
30.94 0.2523 0.5568 0.0642 0.0291 0.853 5.373 5.755 635.743 0.607 25.597 4.106 0.52 192650. 0.4463
|
|
33.32 0.2717 0.5820 0.0608 0.0284 0.831 5.240 5.446 619.905 0.592 24.225 3.985 0.52 192867. 0.4214
|
|
35.70 0.2911 0.6044 0.0572 0.0276 0.808 5.090 5.127 602.175 0.575 22.806 3.862 0.52 193093. 0.3962
|
|
38.08 0.3105 0.6237 0.0535 0.0267 0.781 4.924 4.799 582.592 0.556 21.345 3.736 0.52 193327. 0.3708
|
|
40.46 0.3299 0.6396 0.0498 0.0257 0.753 4.743 4.461 561.158 0.536 19.845 3.606 0.52 193571. 0.3451
|
|
42.84 0.3493 0.6518 0.0459 0.0246 0.721 4.546 4.116 537.874 0.514 18.307 3.471 0.52 193823. 0.3191
|
|
45.22 0.3687 0.6598 0.0420 0.0235 0.688 4.334 3.763 512.734 0.490 16.736 3.328 0.52 194084. 0.2925
|
|
47.60 0.3881 0.6629 0.0380 0.0222 0.651 4.106 3.402 485.736 0.464 15.132 3.177 0.52 194355. 0.2655
|
|
49.98 0.4075 0.6601 0.0339 0.0209 0.613 3.862 3.035 456.885 0.436 13.500 3.013 0.52 194635. 0.2378
|
|
52.36 0.4269 0.6504 0.0297 0.0195 0.572 3.602 2.662 426.198 0.407 11.843 2.833 0.52 194923. 0.2095
|
|
54.74 0.4464 0.6317 0.0255 0.0180 0.528 3.328 2.285 393.704 0.376 10.164 2.632 0.52 195222. 0.1803
|
|
57.12 0.4658 0.6015 0.0212 0.0164 0.482 3.038 1.904 359.452 0.343 8.468 2.402 0.52 195530. 0.1502
|
|
59.50 0.4852 0.5559 0.0170 0.0148 0.434 2.734 1.520 323.517 0.309 6.762 2.131 0.52 195847. 0.1191
|
|
61.88 0.5046 0.4886 0.0127 0.0131 0.384 2.417 1.136 286.006 0.273 5.052 1.801 0.52 196173. 0.0870
|
|
64.26 0.5240 0.3891 0.0084 0.0113 0.331 2.088 0.753 247.071 0.236 3.347 1.381 0.52 196509. 0.0543
|
|
66.64 0.5434 0.2387 0.0042 0.0095 0.277 1.749 0.373 206.920 0.198 1.658 0.817 0.52 196853. 0.0226
|
|
69.02 0.5628 -0.0045 -0.0001 0.0076 0.222 1.397 -0.005 165.306 0.158 -0.024 -0.015 0.52 197181. 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 0.0978 0.0319 1.244 7.126 10.602 927.455 0.805 47.157 5.185 0.57 209619. 0.7650
|
|
2.62 0.0194 0.0582 0.0960 0.0320 1.249 7.157 10.405 931.399 0.809 46.283 5.067 0.57 209745. 0.7406
|
|
5.24 0.0389 0.1138 0.0940 0.0321 1.253 7.179 10.198 934.258 0.811 45.360 4.951 0.57 209879. 0.7164
|
|
7.86 0.0583 0.1667 0.0920 0.0322 1.255 7.192 9.978 935.964 0.813 44.384 4.836 0.57 210020. 0.6921
|
|
10.48 0.0777 0.2170 0.0899 0.0322 1.255 7.191 9.743 935.846 0.812 43.338 4.722 0.57 210170. 0.6679
|
|
13.10 0.0971 0.2648 0.0876 0.0321 1.253 7.178 9.496 934.159 0.811 42.238 4.611 0.57 210329. 0.6438
|
|
15.72 0.1166 0.3102 0.0852 0.0320 1.249 7.154 9.237 931.079 0.808 41.087 4.500 0.57 210495. 0.6197
|
|
18.34 0.1360 0.3531 0.0826 0.0318 1.241 7.113 8.961 925.720 0.804 39.860 4.391 0.57 210671. 0.5956
|
|
20.96 0.1554 0.3936 0.0800 0.0316 1.232 7.059 8.674 918.679 0.798 38.584 4.283 0.57 210855. 0.5715
|
|
23.58 0.1748 0.4317 0.0772 0.0313 1.220 6.988 8.372 909.420 0.789 37.237 4.175 0.57 211048. 0.5474
|
|
26.21 0.1943 0.4674 0.0743 0.0309 1.204 6.901 8.056 898.083 0.780 35.834 4.069 0.57 211250. 0.5233
|
|
28.83 0.2137 0.5007 0.0712 0.0304 1.186 6.794 7.724 884.196 0.768 34.357 3.962 0.57 211462. 0.4990
|
|
31.45 0.2331 0.5315 0.0680 0.0298 1.164 6.670 7.379 868.003 0.754 32.820 3.856 0.57 211683. 0.4746
|
|
34.07 0.2525 0.5598 0.0647 0.0292 1.139 6.525 7.018 849.215 0.737 31.218 3.749 0.57 211913. 0.4500
|
|
36.69 0.2720 0.5854 0.0612 0.0285 1.110 6.359 6.642 827.631 0.718 29.542 3.640 0.57 212153. 0.4250
|
|
39.31 0.2914 0.6082 0.0577 0.0276 1.077 6.174 6.252 803.479 0.698 27.808 3.529 0.57 212402. 0.3998
|
|
41.93 0.3108 0.6279 0.0540 0.0267 1.042 5.969 5.850 776.810 0.674 26.023 3.416 0.57 212661. 0.3744
|
|
44.55 0.3303 0.6443 0.0502 0.0257 1.003 5.745 5.438 747.632 0.649 24.189 3.299 0.57 212930. 0.3486
|
|
47.17 0.3497 0.6571 0.0463 0.0246 0.960 5.501 5.016 715.943 0.622 22.310 3.178 0.57 213208. 0.3225
|
|
49.79 0.3691 0.6657 0.0423 0.0234 0.914 5.238 4.584 681.738 0.592 20.390 3.050 0.57 213497. 0.2959
|
|
52.41 0.3885 0.6695 0.0382 0.0222 0.865 4.956 4.143 645.013 0.560 18.430 2.914 0.57 213795. 0.2687
|
|
55.03 0.4080 0.6674 0.0341 0.0208 0.812 4.655 3.695 605.778 0.526 16.435 2.767 0.57 214103. 0.2410
|
|
57.65 0.4274 0.6584 0.0299 0.0194 0.756 4.334 3.240 564.053 0.490 14.410 2.605 0.57 214422. 0.2125
|
|
60.27 0.4468 0.6405 0.0256 0.0179 0.697 3.995 2.778 519.882 0.451 12.358 2.424 0.57 214751. 0.1831
|
|
62.89 0.4662 0.6110 0.0213 0.0163 0.635 3.637 2.312 473.331 0.411 10.286 2.216 0.57 215090. 0.1527
|
|
65.51 0.4857 0.5658 0.0170 0.0146 0.569 3.262 1.844 424.503 0.369 8.200 1.970 0.57 215440. 0.1212
|
|
68.13 0.5051 0.4983 0.0127 0.0128 0.501 2.870 1.374 373.546 0.324 6.111 1.668 0.57 215800. 0.0886
|
|
70.75 0.5245 0.3973 0.0084 0.0110 0.430 2.464 0.906 320.671 0.278 4.028 1.281 0.57 216171. 0.0552
|
|
73.37 0.5439 0.2421 0.0041 0.0092 0.357 2.045 0.442 266.161 0.231 1.965 0.753 0.57 216549. 0.0227
|
|
75.99 0.5634 -0.0157 -0.0002 0.0072 0.281 1.610 -0.022 209.498 0.182 -0.097 -0.047 0.57 216904. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 12000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.0987 0.0322 1.628 8.552 12.732 1214.128 0.966 56.630 4.756 0.62 228660. 0.7690
|
|
2.90 0.0197 0.0591 0.0968 0.0323 1.635 8.589 12.493 1219.378 0.970 55.569 4.647 0.62 228800. 0.7442
|
|
5.81 0.0394 0.1155 0.0949 0.0324 1.640 8.615 12.240 1223.076 0.973 54.445 4.539 0.62 228949. 0.7196
|
|
8.71 0.0592 0.1692 0.0928 0.0324 1.643 8.630 11.973 1225.215 0.975 53.257 4.432 0.62 229107. 0.6950
|
|
11.61 0.0789 0.2203 0.0906 0.0324 1.643 8.627 11.687 1224.870 0.975 51.983 4.328 0.62 229274. 0.6703
|
|
14.51 0.0986 0.2688 0.0882 0.0324 1.639 8.610 11.385 1222.343 0.973 50.639 4.224 0.62 229451. 0.6459
|
|
17.42 0.1183 0.3147 0.0858 0.0323 1.633 8.578 11.068 1217.869 0.969 49.231 4.122 0.62 229637. 0.6214
|
|
20.32 0.1381 0.3582 0.0832 0.0321 1.623 8.525 10.731 1210.289 0.963 47.730 4.021 0.62 229833. 0.5969
|
|
23.22 0.1578 0.3992 0.0804 0.0318 1.610 8.455 10.379 1200.419 0.955 46.167 3.922 0.62 230039. 0.5725
|
|
26.12 0.1775 0.4378 0.0776 0.0314 1.592 8.364 10.008 1187.425 0.945 44.515 3.823 0.62 230255. 0.5480
|
|
29.03 0.1972 0.4739 0.0746 0.0310 1.571 8.252 9.621 1171.625 0.932 42.793 3.724 0.62 230482. 0.5235
|
|
31.93 0.2170 0.5076 0.0714 0.0305 1.545 8.117 9.214 1152.348 0.917 40.982 3.626 0.62 230718. 0.4988
|
|
34.83 0.2367 0.5387 0.0681 0.0299 1.515 7.958 8.789 1129.810 0.899 39.092 3.528 0.62 230966. 0.4739
|
|
37.73 0.2564 0.5673 0.0647 0.0292 1.480 7.774 8.346 1103.765 0.878 37.122 3.430 0.62 231223. 0.4489
|
|
40.64 0.2761 0.5931 0.0611 0.0284 1.440 7.564 7.883 1073.922 0.855 35.062 3.329 0.62 231492. 0.4235
|
|
43.54 0.2959 0.6160 0.0574 0.0276 1.395 7.330 7.404 1040.604 0.828 32.933 3.227 0.62 231771. 0.3979
|
|
46.44 0.3156 0.6357 0.0536 0.0266 1.346 7.071 6.911 1003.862 0.799 30.741 3.123 0.62 232061. 0.3720
|
|
49.34 0.3353 0.6521 0.0496 0.0255 1.292 6.788 6.405 963.706 0.767 28.489 3.015 0.62 232362. 0.3457
|
|
52.25 0.3550 0.6646 0.0456 0.0244 1.234 6.481 5.886 920.129 0.732 26.183 2.902 0.62 232674. 0.3190
|
|
55.15 0.3748 0.6727 0.0415 0.0231 1.171 6.150 5.356 873.126 0.695 23.825 2.783 0.62 232997. 0.2918
|
|
58.05 0.3945 0.6757 0.0373 0.0218 1.103 5.795 4.816 822.699 0.655 21.420 2.655 0.62 233331. 0.2640
|
|
60.95 0.4142 0.6724 0.0331 0.0204 1.031 5.416 4.266 768.863 0.612 18.973 2.516 0.62 233677. 0.2355
|
|
63.86 0.4339 0.6614 0.0287 0.0188 0.954 5.013 3.707 711.659 0.566 16.490 2.363 0.62 234034. 0.2061
|
|
66.76 0.4537 0.6405 0.0243 0.0172 0.873 4.586 3.142 651.154 0.518 13.976 2.189 0.62 234402. 0.1758
|
|
69.66 0.4734 0.6064 0.0199 0.0156 0.788 4.138 2.572 587.460 0.467 11.440 1.986 0.62 234782. 0.1443
|
|
72.56 0.4931 0.5538 0.0155 0.0138 0.698 3.668 1.999 520.739 0.414 8.891 1.741 0.62 235174. 0.1115
|
|
75.47 0.5128 0.4741 0.0110 0.0119 0.605 3.178 1.426 451.226 0.359 6.341 1.433 0.62 235578. 0.0775
|
|
78.37 0.5326 0.3516 0.0066 0.0100 0.509 2.671 0.856 379.256 0.302 3.806 1.023 0.63 235992. 0.0429
|
|
81.27 0.5523 0.1548 0.0023 0.0081 0.409 2.150 0.292 305.212 0.243 1.300 0.434 0.63 236413. 0.0106
|
|
84.17 0.5720
|
|
|
|
|
|
|
|
PROP RPM = 13000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.0997 0.0325 2.093 10.146 15.096 1560.438 1.146 67.145 4.388 0.67 247696. 0.7725
|
|
3.09 0.0194 0.0582 0.0978 0.0326 2.102 10.189 14.819 1567.098 1.151 65.916 4.289 0.67 247846. 0.7482
|
|
6.19 0.0388 0.1137 0.0959 0.0327 2.108 10.219 14.526 1571.702 1.155 64.611 4.192 0.67 248005. 0.7239
|
|
9.28 0.0582 0.1666 0.0939 0.0328 2.111 10.236 14.217 1574.409 1.156 63.235 4.096 0.67 248174. 0.6997
|
|
12.37 0.0776 0.2170 0.0917 0.0328 2.111 10.234 13.885 1574.061 1.156 61.760 4.001 0.67 248352. 0.6755
|
|
15.47 0.0970 0.2650 0.0894 0.0327 2.106 10.213 13.534 1570.804 1.154 60.200 3.908 0.67 248541. 0.6515
|
|
18.56 0.1164 0.3105 0.0869 0.0326 2.099 10.177 13.168 1565.204 1.150 58.571 3.816 0.67 248739. 0.6274
|
|
21.66 0.1358 0.3536 0.0844 0.0324 2.086 10.115 12.777 1555.756 1.143 56.833 3.725 0.67 248948. 0.6033
|
|
24.75 0.1552 0.3944 0.0817 0.0321 2.069 10.033 12.369 1543.195 1.134 55.019 3.636 0.67 249167. 0.5794
|
|
27.84 0.1747 0.4329 0.0788 0.0318 2.048 9.929 11.940 1527.078 1.122 53.111 3.546 0.67 249397. 0.5553
|
|
30.94 0.1941 0.4690 0.0759 0.0314 2.021 9.800 11.492 1507.222 1.107 51.116 3.458 0.67 249638. 0.5312
|
|
34.03 0.2135 0.5028 0.0728 0.0309 1.989 9.643 11.020 1483.084 1.089 49.017 3.370 0.67 249889. 0.5069
|
|
37.12 0.2329 0.5342 0.0695 0.0303 1.951 9.460 10.529 1455.000 1.069 46.834 3.282 0.67 250151. 0.4826
|
|
40.22 0.2523 0.5631 0.0661 0.0296 1.908 9.248 10.017 1422.461 1.045 44.555 3.194 0.67 250425. 0.4581
|
|
43.31 0.2717 0.5895 0.0626 0.0289 1.858 9.006 9.481 1385.162 1.017 42.172 3.105 0.67 250709. 0.4331
|
|
46.40 0.2911 0.6131 0.0589 0.0280 1.802 8.735 8.926 1343.464 0.987 39.705 3.014 0.67 251005. 0.4080
|
|
49.50 0.3105 0.6338 0.0552 0.0270 1.740 8.436 8.355 1297.463 0.953 37.163 2.921 0.67 251312. 0.3825
|
|
52.59 0.3299 0.6513 0.0513 0.0260 1.673 8.109 7.768 1247.184 0.916 34.552 2.825 0.67 251630. 0.3568
|
|
55.68 0.3493 0.6654 0.0473 0.0248 1.599 7.754 7.167 1192.626 0.876 31.877 2.726 0.67 251960. 0.3306
|
|
58.78 0.3687 0.6754 0.0433 0.0236 1.520 7.372 6.551 1133.779 0.833 29.141 2.621 0.67 252301. 0.3040
|
|
61.87 0.3881 0.6807 0.0391 0.0223 1.436 6.961 5.924 1070.646 0.786 26.349 2.510 0.67 252654. 0.2768
|
|
64.97 0.4075 0.6805 0.0349 0.0209 1.345 6.523 5.285 1003.240 0.737 23.507 2.389 0.67 253019. 0.2489
|
|
68.06 0.4269 0.6734 0.0306 0.0194 1.249 6.057 4.636 931.601 0.684 20.619 2.257 0.67 253396. 0.2202
|
|
71.15 0.4463 0.6577 0.0263 0.0178 1.148 5.564 3.978 855.801 0.629 17.695 2.108 0.67 253785. 0.1905
|
|
74.25 0.4657 0.6305 0.0219 0.0162 1.041 5.045 3.314 775.957 0.570 14.740 1.937 0.68 254186. 0.1598
|
|
77.34 0.4851 0.5877 0.0175 0.0144 0.928 4.501 2.645 692.245 0.508 11.766 1.733 0.68 254599. 0.1277
|
|
80.43 0.5045 0.5222 0.0130 0.0126 0.811 3.933 1.975 604.920 0.444 8.786 1.481 0.68 255024. 0.0943
|
|
83.53 0.5240 0.4220 0.0086 0.0107 0.690 3.344 1.307 514.355 0.378 5.813 1.152 0.68 255461. 0.0597
|
|
86.62 0.5434 0.2638 0.0043 0.0088 0.565 2.738 0.645 421.054 0.309 2.868 0.695 0.68 255908. 0.0253
|
|
89.71 0.5628 -0.0090 -0.0001 0.0068 0.435 2.108 -0.016 324.240 0.238 -0.073 -0.023 0.68 256328. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 14000
|
|
|
|
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 0.1008 0.0330 2.650 11.929 17.712 1975.909 1.348 78.781 4.066 0.72 266725. 0.7753
|
|
3.36 0.0196 0.0585 0.0990 0.0331 2.661 11.980 17.387 1984.334 1.353 77.338 3.974 0.72 266889. 0.7509
|
|
6.72 0.0391 0.1144 0.0970 0.0332 2.669 12.014 17.041 1989.967 1.357 75.800 3.884 0.72 267063. 0.7265
|
|
10.08 0.0587 0.1677 0.0949 0.0332 2.673 12.033 16.677 1993.124 1.359 74.179 3.795 0.72 267248. 0.7023
|
|
13.44 0.0783 0.2184 0.0927 0.0332 2.672 12.029 16.286 1992.387 1.359 72.440 3.708 0.72 267443. 0.6780
|
|
16.80 0.0978 0.2667 0.0904 0.0332 2.666 12.001 15.871 1987.753 1.356 70.596 3.622 0.72 267649. 0.6538
|
|
20.16 0.1174 0.3125 0.0879 0.0330 2.655 11.954 15.438 1980.025 1.351 68.669 3.536 0.72 267866. 0.6296
|
|
23.52 0.1370 0.3559 0.0853 0.0328 2.638 11.877 14.976 1967.330 1.342 66.612 3.453 0.72 268095. 0.6054
|
|
26.87 0.1565 0.3970 0.0825 0.0325 2.616 11.776 14.492 1950.514 1.330 64.461 3.370 0.72 268335. 0.5813
|
|
30.23 0.1761 0.4358 0.0796 0.0322 2.587 11.646 13.983 1929.058 1.316 62.198 3.288 0.72 268586. 0.5571
|
|
33.59 0.1957 0.4722 0.0766 0.0317 2.552 11.487 13.451 1902.738 1.298 59.831 3.206 0.72 268850. 0.5329
|
|
36.95 0.2152 0.5063 0.0734 0.0312 2.509 11.295 12.891 1870.831 1.276 57.339 3.125 0.72 269125. 0.5085
|
|
40.31 0.2348 0.5380 0.0701 0.0306 2.459 11.071 12.308 1833.759 1.251 54.744 3.044 0.72 269412. 0.4839
|
|
43.67 0.2544 0.5672 0.0666 0.0299 2.402 10.812 11.699 1790.917 1.222 52.036 2.963 0.72 269711. 0.4592
|
|
47.03 0.2739 0.5939 0.0630 0.0291 2.336 10.516 11.062 1741.913 1.188 49.203 2.880 0.72 270023. 0.4341
|
|
50.39 0.2935 0.6178 0.0592 0.0281 2.263 10.186 10.403 1687.228 1.151 46.271 2.796 0.72 270346. 0.4087
|
|
53.75 0.3131 0.6387 0.0554 0.0271 2.182 9.823 9.723 1626.982 1.110 43.250 2.711 0.72 270682. 0.3830
|
|
57.11 0.3326 0.6565 0.0514 0.0260 2.094 9.425 9.026 1561.205 1.065 40.147 2.622 0.72 271030. 0.3570
|
|
60.47 0.3522 0.6707 0.0473 0.0248 1.998 8.995 8.311 1489.891 1.016 36.967 2.530 0.72 271391. 0.3305
|
|
63.83 0.3718 0.6808 0.0432 0.0236 1.895 8.531 7.580 1413.043 0.964 33.715 2.433 0.72 271764. 0.3035
|
|
67.19 0.3913 0.6861 0.0389 0.0222 1.784 8.034 6.834 1330.672 0.908 30.397 2.329 0.72 272151. 0.2759
|
|
70.55 0.4109 0.6856 0.0346 0.0207 1.667 7.503 6.074 1242.823 0.848 27.019 2.217 0.73 272550. 0.2476
|
|
73.90 0.4305 0.6779 0.0302 0.0192 1.542 6.940 5.303 1149.577 0.784 23.589 2.092 0.73 272962. 0.2183
|
|
77.26 0.4500 0.6610 0.0257 0.0175 1.410 6.346 4.522 1051.073 0.717 20.114 1.951 0.73 273387. 0.1880
|
|
80.62 0.4696 0.6317 0.0213 0.0158 1.271 5.721 3.733 947.528 0.646 16.606 1.787 0.73 273825. 0.1565
|
|
83.98 0.4892 0.5850 0.0167 0.0140 1.125 5.067 2.940 839.256 0.572 13.077 1.589 0.73 274277. 0.1234
|
|
87.34 0.5087 0.5127 0.0122 0.0121 0.975 4.387 2.145 726.713 0.496 9.542 1.339 0.73 274742. 0.0889
|
|
90.70 0.5283 0.3999 0.0077 0.0102 0.819 3.686 1.354 610.528 0.416 6.022 1.006 0.73 275219. 0.0530
|
|
94.06 0.5479 0.2171 0.0032 0.0082 0.659 2.967 0.571 491.507 0.335 2.538 0.527 0.73 275706. 0.0180
|
|
97.42 0.5674
|
|
|
|
|
|
|
|
PROP RPM = 15000
|
|
|
|
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 0.1022 0.0336 3.326 13.976 20.602 2480.267 1.579 91.636 3.767 0.77 285746. 0.7748
|
|
3.62 0.0197 0.0584 0.1003 0.0337 3.338 14.025 20.226 2489.022 1.585 89.967 3.686 0.77 285924. 0.7511
|
|
7.23 0.0393 0.1143 0.0983 0.0338 3.345 14.055 19.825 2494.267 1.588 88.181 3.605 0.77 286113. 0.7273
|
|
10.85 0.0590 0.1676 0.0962 0.0339 3.348 14.068 19.401 2496.529 1.589 86.297 3.525 0.77 286313. 0.7035
|
|
14.46 0.0786 0.2185 0.0940 0.0338 3.345 14.055 18.947 2494.240 1.588 84.277 3.445 0.77 286525. 0.6796
|
|
18.08 0.0983 0.2669 0.0916 0.0337 3.335 14.014 18.464 2487.012 1.583 82.127 3.367 0.77 286748. 0.6556
|
|
21.69 0.1179 0.3129 0.0891 0.0336 3.320 13.952 17.958 2475.964 1.576 79.879 3.290 0.77 286984. 0.6317
|
|
25.31 0.1376 0.3565 0.0864 0.0333 3.297 13.855 17.419 2458.852 1.565 77.479 3.213 0.77 287232. 0.6076
|
|
28.93 0.1573 0.3979 0.0836 0.0330 3.267 13.729 16.853 2436.448 1.551 74.964 3.137 0.77 287492. 0.5836
|
|
32.54 0.1769 0.4369 0.0806 0.0327 3.230 13.571 16.259 2408.335 1.533 72.319 3.062 0.77 287765. 0.5595
|
|
36.16 0.1966 0.4735 0.0775 0.0322 3.184 13.377 15.636 2374.006 1.511 69.549 2.987 0.77 288050. 0.5353
|
|
39.77 0.2162 0.5079 0.0743 0.0316 3.128 13.144 14.980 2332.633 1.485 66.632 2.913 0.77 288348. 0.5108
|
|
43.39 0.2359 0.5399 0.0709 0.0310 3.064 12.874 14.297 2284.678 1.454 63.592 2.838 0.77 288660. 0.4863
|
|
47.01 0.2555 0.5695 0.0674 0.0302 2.990 12.562 13.583 2229.413 1.419 60.418 2.763 0.77 288984. 0.4615
|
|
50.62 0.2752 0.5964 0.0637 0.0294 2.905 12.207 12.837 2166.372 1.379 57.097 2.688 0.77 289321. 0.4363
|
|
54.24 0.2949 0.6207 0.0598 0.0284 2.811 11.812 12.064 2096.187 1.334 53.660 2.610 0.77 289672. 0.4108
|
|
57.85 0.3145 0.6420 0.0559 0.0274 2.708 11.377 11.268 2019.042 1.285 50.118 2.531 0.77 290035. 0.3850
|
|
61.47 0.3342 0.6601 0.0518 0.0262 2.595 10.903 10.449 1935.003 1.232 46.479 2.449 0.77 290412. 0.3588
|
|
65.08 0.3538 0.6745 0.0477 0.0250 2.473 10.391 9.611 1844.124 1.174 42.750 2.364 0.78 290803. 0.3321
|
|
68.70 0.3735 0.6847 0.0434 0.0237 2.342 9.841 8.753 1746.466 1.112 38.935 2.273 0.78 291207. 0.3048
|
|
72.32 0.3931 0.6899 0.0391 0.0223 2.202 9.253 7.878 1642.126 1.045 35.043 2.176 0.78 291625. 0.2768
|
|
75.93 0.4128 0.6890 0.0347 0.0208 2.053 8.628 6.988 1531.252 0.975 31.081 2.070 0.78 292056. 0.2479
|
|
79.55 0.4325 0.6804 0.0302 0.0192 1.896 7.968 6.083 1414.074 0.900 27.056 1.951 0.78 292502. 0.2180
|
|
83.16 0.4521 0.6618 0.0256 0.0175 1.731 7.274 5.166 1290.925 0.822 22.980 1.815 0.78 292962. 0.1870
|
|
86.78 0.4718 0.6297 0.0210 0.0158 1.559 6.549 4.241 1162.273 0.740 18.864 1.655 0.78 293436. 0.1544
|
|
90.40 0.4914 0.5784 0.0164 0.0139 1.380 5.797 3.310 1028.734 0.655 14.724 1.459 0.78 293924. 0.1203
|
|
94.01 0.5111 0.4989 0.0118 0.0121 1.195 5.021 2.378 891.123 0.567 10.578 1.210 0.78 294426. 0.0846
|
|
97.63 0.5307 0.3750 0.0072 0.0102 1.006 4.229 1.450 750.485 0.478 6.449 0.876 0.78 294942. 0.0478
|
|
101.24 0.5504 0.1760 0.0026 0.0082 0.815 3.426 0.531 607.996 0.387 2.364 0.396 0.78 295466. 0.0131
|
|
104.86 0.5701
|
|
|
|
|
|
|
|
PROP RPM = 16000
|
|
|
|
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 0.1037 0.0350 4.202 16.554 23.791 3133.648 1.870 105.824 3.444 0.82 304758. 0.7611
|
|
3.86 0.0197 0.0572 0.1018 0.0351 4.207 16.574 23.363 3137.383 1.872 103.921 3.378 0.82 304949. 0.7398
|
|
7.73 0.0394 0.1122 0.0998 0.0350 4.206 16.570 22.904 3136.776 1.872 101.875 3.312 0.82 305152. 0.7182
|
|
11.59 0.0591 0.1649 0.0977 0.0350 4.201 16.548 22.417 3132.596 1.870 99.712 3.246 0.82 305368. 0.6963
|
|
15.45 0.0788 0.2154 0.0954 0.0349 4.189 16.500 21.897 3123.426 1.864 97.396 3.180 0.82 305596. 0.6742
|
|
19.32 0.0985 0.2637 0.0930 0.0347 4.168 16.420 21.340 3108.249 1.855 94.922 3.114 0.82 305837. 0.6518
|
|
23.18 0.1181 0.3098 0.0905 0.0345 4.142 16.316 20.758 3088.612 1.843 92.332 3.048 0.82 306090. 0.6293
|
|
27.04 0.1378 0.3536 0.0878 0.0342 4.106 16.176 20.137 3062.128 1.828 89.567 2.983 0.82 306357. 0.6065
|
|
30.91 0.1575 0.3953 0.0849 0.0338 4.062 16.002 19.483 3029.191 1.808 86.661 2.917 0.82 306637. 0.5835
|
|
34.77 0.1772 0.4347 0.0819 0.0334 4.009 15.794 18.797 2989.860 1.784 83.609 2.852 0.82 306930. 0.5602
|
|
38.64 0.1969 0.4719 0.0788 0.0329 3.947 15.547 18.077 2943.078 1.757 80.405 2.786 0.82 307237. 0.5367
|
|
42.50 0.2166 0.5067 0.0755 0.0323 3.873 15.257 17.318 2888.109 1.724 77.030 2.720 0.82 307558. 0.5128
|
|
46.36 0.2363 0.5392 0.0720 0.0316 3.789 14.926 16.527 2825.386 1.686 73.511 2.653 0.82 307893. 0.4887
|
|
50.23 0.2560 0.5693 0.0684 0.0308 3.694 14.551 15.701 2754.428 1.644 69.836 2.585 0.82 308242. 0.4642
|
|
54.09 0.2757 0.5966 0.0647 0.0299 3.587 14.129 14.835 2674.680 1.596 65.988 2.516 0.83 308604. 0.4391
|
|
57.95 0.2954 0.6210 0.0608 0.0289 3.469 13.665 13.940 2586.752 1.544 62.004 2.444 0.83 308980. 0.4135
|
|
61.82 0.3151 0.6423 0.0567 0.0278 3.340 13.159 13.016 2490.897 1.487 57.897 2.370 0.83 309371. 0.3875
|
|
65.68 0.3347 0.6602 0.0526 0.0267 3.201 12.610 12.068 2387.122 1.425 53.677 2.293 0.83 309776. 0.3609
|
|
69.54 0.3544 0.6742 0.0484 0.0254 3.052 12.021 11.095 2275.533 1.358 49.351 2.212 0.83 310195. 0.3338
|
|
73.41 0.3741 0.6837 0.0440 0.0241 2.892 11.391 10.100 2156.383 1.287 44.925 2.124 0.83 310628. 0.3059
|
|
77.27 0.3938 0.6876 0.0396 0.0227 2.722 10.724 9.085 2030.117 1.212 40.409 2.030 0.83 311076. 0.2772
|
|
81.13 0.4135 0.6846 0.0351 0.0212 2.544 10.022 8.051 1897.067 1.132 35.810 1.925 0.83 311539. 0.2475
|
|
85.00 0.4332 0.6731 0.0305 0.0196 2.357 9.286 7.000 1757.769 1.049 31.138 1.806 0.83 312017. 0.2166
|
|
88.86 0.4529 0.6503 0.0259 0.0180 2.163 8.520 5.936 1612.913 0.963 26.404 1.669 0.83 312510. 0.1843
|
|
92.72 0.4726 0.6125 0.0212 0.0163 1.962 7.731 4.861 1463.399 0.873 21.623 1.507 0.83 313017. 0.1505
|
|
96.59 0.4923 0.5540 0.0165 0.0146 1.757 6.922 3.780 1310.289 0.782 16.812 1.308 0.83 313540. 0.1153
|
|
100.45 0.5120 0.4663 0.0118 0.0129 1.549 6.101 2.696 1154.848 0.689 11.992 1.059 0.83 314078. 0.0788
|
|
104.32 0.5317 0.3359 0.0070 0.0112 1.339 5.275 1.617 998.637 0.596 7.194 0.735 0.83 314630. 0.0423
|
|
108.18 0.5514 0.1402 0.0024 0.0094 1.131 4.454 0.550 843.154 0.503 2.444 0.296 0.83 315190. 0.0099
|
|
112.04 0.5710
|
|
|
|
|
|
|
|
PROP RPM = 17000
|
|
|
|
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 0.1053 0.0377 5.432 20.138 27.282 4050.420 2.275 121.349 3.055 0.87 323759. 0.7230
|
|
4.10 0.0197 0.0541 0.1035 0.0376 5.417 20.085 26.802 4039.714 2.269 119.215 3.009 0.87 323963. 0.7059
|
|
8.21 0.0394 0.1066 0.1015 0.0375 5.395 20.004 26.284 4023.371 2.260 116.910 2.963 0.87 324181. 0.6883
|
|
12.31 0.0590 0.1574 0.0994 0.0373 5.367 19.899 25.734 4002.380 2.248 114.463 2.916 0.87 324411. 0.6703
|
|
16.41 0.0787 0.2064 0.0971 0.0370 5.332 19.768 25.146 3975.903 2.233 111.848 2.869 0.87 324655. 0.6518
|
|
20.51 0.0984 0.2537 0.0947 0.0367 5.286 19.600 24.515 3942.126 2.214 109.042 2.821 0.87 324913. 0.6328
|
|
24.62 0.1181 0.2991 0.0921 0.0364 5.234 19.406 23.853 3903.051 2.192 106.096 2.772 0.87 325184. 0.6134
|
|
28.72 0.1378 0.3427 0.0894 0.0359 5.172 19.175 23.147 3856.677 2.166 102.958 2.722 0.87 325469. 0.5934
|
|
32.82 0.1574 0.3845 0.0865 0.0354 5.099 18.906 22.402 3802.639 2.136 99.645 2.672 0.87 325769. 0.5731
|
|
36.92 0.1771 0.4242 0.0835 0.0349 5.018 18.605 21.621 3741.946 2.102 96.172 2.621 0.87 326082. 0.5522
|
|
41.03 0.1968 0.4620 0.0803 0.0342 4.925 18.260 20.799 3672.705 2.063 92.516 2.569 0.87 326411. 0.5308
|
|
45.13 0.2165 0.4976 0.0770 0.0335 4.820 17.872 19.934 3594.611 2.019 88.668 2.515 0.88 326753. 0.5089
|
|
49.23 0.2362 0.5311 0.0735 0.0327 4.704 17.441 19.031 3507.828 1.970 84.651 2.461 0.88 327111. 0.4864
|
|
53.33 0.2558 0.5623 0.0698 0.0318 4.575 16.962 18.087 3411.586 1.916 80.452 2.405 0.88 327483. 0.4634
|
|
57.44 0.2755 0.5904 0.0660 0.0308 4.435 16.444 17.098 3307.340 1.858 76.051 2.345 0.88 327870. 0.4393
|
|
61.54 0.2952 0.6154 0.0621 0.0298 4.286 15.890 16.073 3195.898 1.795 71.491 2.281 0.88 328271. 0.4144
|
|
65.64 0.3149 0.6366 0.0580 0.0287 4.128 15.307 15.015 3078.608 1.729 66.787 2.212 0.88 328688. 0.3884
|
|
69.75 0.3346 0.6532 0.0538 0.0275 3.966 14.702 13.927 2957.115 1.661 61.949 2.136 0.88 329119. 0.3612
|
|
73.85 0.3542 0.6653 0.0495 0.0263 3.792 14.060 12.812 2827.972 1.589 56.988 2.055 0.88 329566. 0.3333
|
|
77.95 0.3739 0.6721 0.0451 0.0251 3.609 13.382 11.671 2691.561 1.512 51.913 1.967 0.88 330027. 0.3044
|
|
82.05 0.3936 0.6726 0.0406 0.0237 3.418 12.672 10.506 2548.668 1.432 46.733 1.870 0.88 330504. 0.2746
|
|
86.16 0.4133 0.6652 0.0360 0.0224 3.219 11.935 9.320 2400.521 1.348 41.457 1.761 0.88 330997. 0.2436
|
|
90.26 0.4330 0.6480 0.0313 0.0209 3.014 11.175 8.116 2247.716 1.263 36.099 1.638 0.88 331505. 0.2114
|
|
94.36 0.4526 0.6186 0.0266 0.0195 2.805 10.398 6.895 2091.408 1.175 30.670 1.495 0.88 332029. 0.1779
|
|
98.46 0.4723 0.5736 0.0219 0.0180 2.592 9.610 5.663 1932.935 1.086 25.189 1.329 0.88 332568. 0.1433
|
|
102.57 0.4920 0.5085 0.0171 0.0165 2.379 8.820 4.423 1773.934 0.996 19.673 1.131 0.88 333124. 0.1078
|
|
106.67 0.5117 0.4175 0.0123 0.0151 2.167 8.035 3.181 1616.056 0.908 14.150 0.893 0.88 333695. 0.0722
|
|
110.77 0.5314 0.2932 0.0075 0.0136 1.959 7.265 1.945 1461.170 0.821 8.651 0.604 0.89 334282. 0.0382
|
|
114.87 0.5510 0.1258 0.0028 0.0122 1.758 6.518 0.722 1310.908 0.736 3.213 0.250 0.89 334879. 0.0096
|
|
118.98 0.5707
|
|
|
|
|
|
|