427 lines
76 KiB
Plaintext
427 lines
76 KiB
Plaintext
22x8 (22x8.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 0.0633 0.0223 0.009 0.583 0.473 6.892 0.066 2.103 31.108 0.09 37892. 0.5704
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0.39 0.0188 0.0521 0.0620 0.0224 0.009 0.586 0.463 6.934 0.066 2.060 30.298 0.09 37908. 0.5500
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0.78 0.0376 0.1014 0.0607 0.0225 0.009 0.589 0.453 6.970 0.067 2.015 29.487 0.09 37926. 0.5294
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1.18 0.0565 0.1479 0.0593 0.0226 0.009 0.591 0.442 6.998 0.067 1.968 28.680 0.09 37946. 0.5088
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1.57 0.0753 0.1917 0.0578 0.0227 0.009 0.593 0.431 7.017 0.067 1.918 27.875 0.09 37966. 0.4882
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1.96 0.0941 0.2327 0.0562 0.0227 0.009 0.594 0.419 7.028 0.067 1.866 27.073 0.09 37988. 0.4677
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2.35 0.1129 0.2710 0.0545 0.0227 0.009 0.594 0.407 7.029 0.067 1.811 26.274 0.09 38011. 0.4471
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2.74 0.1317 0.3066 0.0528 0.0227 0.009 0.593 0.394 7.018 0.067 1.754 25.478 0.09 38036. 0.4267
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3.14 0.1506 0.3395 0.0510 0.0226 0.009 0.591 0.381 6.997 0.067 1.694 24.684 0.09 38062. 0.4063
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3.53 0.1694 0.3696 0.0491 0.0225 0.009 0.589 0.367 6.963 0.066 1.631 23.892 0.09 38090. 0.3859
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3.92 0.1882 0.3971 0.0472 0.0224 0.009 0.585 0.352 6.916 0.066 1.567 23.100 0.09 38119. 0.3657
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4.31 0.2070 0.4218 0.0452 0.0222 0.009 0.579 0.337 6.855 0.065 1.500 22.308 0.09 38150. 0.3455
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4.71 0.2259 0.4438 0.0431 0.0219 0.009 0.573 0.322 6.780 0.065 1.430 21.514 0.09 38182. 0.3254
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5.10 0.2447 0.4629 0.0409 0.0216 0.009 0.565 0.306 6.689 0.064 1.359 20.715 0.09 38216. 0.3054
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5.49 0.2635 0.4792 0.0387 0.0213 0.009 0.556 0.289 6.582 0.063 1.285 19.910 0.09 38252. 0.2854
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5.88 0.2823 0.4924 0.0364 0.0209 0.009 0.546 0.272 6.459 0.062 1.210 19.095 0.09 38289. 0.2656
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6.27 0.3011 0.5024 0.0341 0.0204 0.008 0.534 0.254 6.319 0.060 1.132 18.267 0.09 38329. 0.2458
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6.67 0.3200 0.5091 0.0317 0.0199 0.008 0.521 0.237 6.160 0.059 1.052 17.420 0.09 38370. 0.2260
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7.06 0.3388 0.5121 0.0292 0.0193 0.008 0.506 0.218 5.983 0.057 0.971 16.549 0.09 38413. 0.2062
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7.45 0.3576 0.5111 0.0267 0.0187 0.008 0.489 0.200 5.788 0.055 0.888 15.647 0.09 38457. 0.1865
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7.84 0.3764 0.5055 0.0242 0.0180 0.007 0.471 0.181 5.573 0.053 0.804 14.704 0.09 38504. 0.1667
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8.23 0.3952 0.4949 0.0216 0.0173 0.007 0.451 0.161 5.338 0.051 0.718 13.709 0.09 38552. 0.1469
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8.63 0.4141 0.4783 0.0190 0.0164 0.007 0.430 0.142 5.084 0.049 0.630 12.646 0.09 38603. 0.1270
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9.02 0.4329 0.4545 0.0163 0.0156 0.006 0.406 0.122 4.809 0.046 0.542 11.495 0.09 38655. 0.1070
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9.41 0.4517 0.4220 0.0136 0.0146 0.006 0.382 0.102 4.515 0.043 0.453 10.228 0.09 38709. 0.0870
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9.80 0.4705 0.3785 0.0109 0.0136 0.006 0.355 0.082 4.200 0.040 0.363 8.807 0.09 38765. 0.0671
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10.19 0.4894 0.3208 0.0082 0.0125 0.005 0.327 0.061 3.866 0.037 0.272 7.178 0.09 38823. 0.0473
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10.59 0.5082 0.2440 0.0055 0.0114 0.005 0.297 0.041 3.512 0.034 0.181 5.258 0.09 38883. 0.0283
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10.98 0.5270 0.1405 0.0027 0.0101 0.004 0.265 0.020 3.139 0.030 0.090 2.919 0.09 38945. 0.0111
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11.37 0.5458 -0.0043 -0.0001 0.0089 0.004 0.232 -0.001 2.742 0.026 -0.002 -0.086 0.09 39005. 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 0.0637 0.0197 0.065 2.060 1.902 48.750 0.233 8.460 17.695 0.17 75782. 0.6509
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0.79 0.0189 0.0595 0.0624 0.0199 0.066 2.077 1.864 49.142 0.235 8.289 17.201 0.17 75816. 0.6263
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1.58 0.0379 0.1156 0.0610 0.0200 0.066 2.091 1.823 49.481 0.236 8.109 16.711 0.17 75852. 0.6018
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2.37 0.0568 0.1684 0.0596 0.0201 0.067 2.103 1.780 49.758 0.238 7.918 16.227 0.17 75891. 0.5774
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3.16 0.0757 0.2179 0.0581 0.0202 0.067 2.112 1.735 49.967 0.239 7.717 15.749 0.17 75932. 0.5533
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3.95 0.0947 0.2642 0.0565 0.0202 0.067 2.117 1.688 50.099 0.239 7.506 15.278 0.17 75977. 0.5293
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4.73 0.1136 0.3074 0.0548 0.0203 0.067 2.119 1.638 50.149 0.239 7.285 14.812 0.17 76023. 0.5056
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5.52 0.1326 0.3475 0.0531 0.0203 0.067 2.118 1.586 50.109 0.239 7.053 14.353 0.17 76073. 0.4821
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6.31 0.1515 0.3846 0.0513 0.0202 0.067 2.112 1.531 49.971 0.239 6.812 13.900 0.17 76126. 0.4588
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7.10 0.1704 0.4188 0.0494 0.0201 0.067 2.102 1.475 49.728 0.237 6.560 13.452 0.17 76182. 0.4357
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7.89 0.1894 0.4500 0.0474 0.0200 0.066 2.087 1.416 49.375 0.236 6.299 13.009 0.17 76241. 0.4129
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8.68 0.2083 0.4783 0.0454 0.0198 0.066 2.067 1.355 48.903 0.233 6.028 12.570 0.17 76303. 0.3903
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9.47 0.2272 0.5037 0.0433 0.0195 0.065 2.042 1.292 48.307 0.231 5.748 12.134 0.17 76368. 0.3679
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10.26 0.2462 0.5262 0.0411 0.0192 0.064 2.011 1.227 47.581 0.227 5.460 11.701 0.18 76437. 0.3457
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11.05 0.2651 0.5457 0.0389 0.0189 0.063 1.974 1.161 46.717 0.223 5.162 11.268 0.18 76510. 0.3238
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11.84 0.2841 0.5622 0.0366 0.0185 0.061 1.932 1.092 45.709 0.218 4.857 10.834 0.18 76586. 0.3019
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12.62 0.3030 0.5755 0.0342 0.0180 0.060 1.883 1.021 44.554 0.213 4.543 10.398 0.18 76665. 0.2803
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13.41 0.3219 0.5854 0.0318 0.0175 0.058 1.828 0.949 43.244 0.206 4.222 9.956 0.18 76748. 0.2587
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14.20 0.3409 0.5918 0.0293 0.0169 0.056 1.766 0.875 41.776 0.199 3.894 9.505 0.18 76835. 0.2372
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14.99 0.3598 0.5942 0.0268 0.0162 0.054 1.697 0.800 40.145 0.192 3.559 9.041 0.18 76925. 0.2157
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15.78 0.3787 0.5921 0.0242 0.0155 0.051 1.621 0.724 38.347 0.183 3.218 8.558 0.18 77019. 0.1942
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16.57 0.3977 0.5848 0.0216 0.0147 0.049 1.537 0.646 36.380 0.174 2.872 8.050 0.18 77117. 0.1725
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17.36 0.4166 0.5712 0.0190 0.0138 0.046 1.447 0.567 34.241 0.163 2.520 7.506 0.18 77219. 0.1507
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18.15 0.4355 0.5500 0.0163 0.0129 0.043 1.349 0.487 31.928 0.152 2.164 6.913 0.18 77325. 0.1286
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18.94 0.4545 0.5189 0.0136 0.0119 0.039 1.244 0.406 29.442 0.141 1.805 6.251 0.18 77435. 0.1062
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19.73 0.4734 0.4748 0.0109 0.0108 0.036 1.132 0.324 26.783 0.128 1.442 5.490 0.18 77548. 0.0834
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20.51 0.4924 0.4125 0.0081 0.0097 0.032 1.012 0.242 23.953 0.114 1.077 4.586 0.18 77665. 0.0602
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21.30 0.5113 0.3233 0.0054 0.0085 0.028 0.886 0.160 20.957 0.100 0.711 3.461 0.18 77786. 0.0369
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22.09 0.5302 0.1914 0.0026 0.0072 0.024 0.752 0.078 17.795 0.085 0.345 1.976 0.18 77911. 0.0147
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22.88 0.5492 -0.0228 -0.0002 0.0058 0.019 0.607 -0.007 14.366 0.069 -0.032 -0.228 0.18 78023. 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 0.0641 0.0187 0.210 4.407 4.310 156.410 0.498 19.169 12.497 0.26 113670. 0.6919
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1.18 0.0189 0.0629 0.0629 0.0189 0.212 4.446 4.223 157.811 0.502 18.785 12.138 0.26 113721. 0.6653
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2.36 0.0378 0.1222 0.0615 0.0190 0.213 4.481 4.132 159.031 0.506 18.378 11.784 0.26 113775. 0.6389
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3.55 0.0568 0.1778 0.0601 0.0192 0.215 4.509 4.035 160.040 0.509 17.948 11.436 0.26 113834. 0.6127
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4.73 0.0757 0.2300 0.0585 0.0193 0.216 4.531 3.933 160.814 0.512 17.495 11.093 0.26 113896. 0.5868
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5.91 0.0946 0.2788 0.0569 0.0193 0.216 4.545 3.826 161.328 0.514 17.019 10.757 0.26 113962. 0.5612
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7.09 0.1135 0.3243 0.0553 0.0193 0.217 4.552 3.714 161.556 0.514 16.519 10.427 0.26 114033. 0.5359
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8.28 0.1324 0.3665 0.0535 0.0193 0.217 4.549 3.596 161.473 0.514 15.997 10.102 0.26 114107. 0.5110
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9.46 0.1513 0.4057 0.0517 0.0193 0.216 4.538 3.474 161.055 0.513 15.451 9.783 0.26 114187. 0.4863
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10.64 0.1703 0.4417 0.0498 0.0192 0.215 4.516 3.346 160.278 0.510 14.884 9.469 0.26 114270. 0.4620
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11.82 0.1892 0.4748 0.0478 0.0191 0.213 4.483 3.214 159.116 0.506 14.294 9.161 0.26 114359. 0.4380
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13.01 0.2081 0.5050 0.0458 0.0189 0.211 4.439 3.076 157.548 0.501 13.683 8.857 0.26 114452. 0.4143
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14.19 0.2270 0.5322 0.0437 0.0186 0.209 4.382 2.934 155.549 0.495 13.052 8.556 0.26 114550. 0.3909
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15.37 0.2459 0.5565 0.0415 0.0183 0.205 4.313 2.788 153.097 0.487 12.400 8.259 0.26 114654. 0.3678
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16.55 0.2648 0.5779 0.0392 0.0180 0.201 4.231 2.637 150.172 0.478 11.729 7.964 0.26 114762. 0.3449
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17.73 0.2838 0.5964 0.0369 0.0176 0.197 4.135 2.482 146.751 0.467 11.039 7.670 0.26 114876. 0.3223
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18.92 0.3027 0.6117 0.0346 0.0171 0.192 4.024 2.323 142.816 0.455 10.331 7.376 0.26 114995. 0.2998
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20.10 0.3216 0.6239 0.0321 0.0166 0.186 3.898 2.160 138.349 0.440 9.606 7.080 0.26 115119. 0.2775
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21.28 0.3405 0.6326 0.0297 0.0160 0.179 3.756 1.993 133.331 0.424 8.865 6.780 0.26 115249. 0.2553
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22.46 0.3594 0.6375 0.0271 0.0153 0.171 3.599 1.823 127.749 0.407 8.110 6.473 0.26 115384. 0.2331
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23.65 0.3783 0.6381 0.0246 0.0146 0.163 3.426 1.650 121.589 0.387 7.340 6.156 0.26 115526. 0.2109
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24.83 0.3973 0.6338 0.0219 0.0138 0.154 3.236 1.474 114.841 0.366 6.558 5.823 0.26 115672. 0.1886
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26.01 0.4162 0.6235 0.0193 0.0129 0.144 3.029 1.296 107.496 0.342 5.764 5.468 0.26 115825. 0.1660
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27.19 0.4351 0.6057 0.0166 0.0119 0.133 2.805 1.115 99.549 0.317 4.960 5.081 0.26 115983. 0.1431
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28.38 0.4540 0.5782 0.0139 0.0109 0.122 2.564 0.933 91.000 0.290 4.148 4.648 0.26 116147. 0.1197
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29.56 0.4729 0.5375 0.0111 0.0098 0.110 2.306 0.748 81.852 0.261 3.329 4.148 0.26 116317. 0.0957
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30.74 0.4919 0.4775 0.0084 0.0086 0.097 2.032 0.563 72.112 0.230 2.506 3.543 0.26 116493. 0.0709
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31.92 0.5108 0.3878 0.0056 0.0074 0.083 1.741 0.378 61.791 0.197 1.679 2.771 0.27 116674. 0.0454
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33.11 0.5297 0.2477 0.0029 0.0061 0.068 1.434 0.191 50.896 0.162 0.852 1.706 0.27 116861. 0.0199
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34.29 0.5486 0.0024 0.0000 0.0047 0.053 1.103 0.001 39.157 0.125 0.006 0.016 0.27 117034. 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 0.0647 0.0183 0.486 7.652 7.733 362.146 0.865 34.396 9.685 0.35 151553. 0.7183
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1.58 0.0190 0.0652 0.0634 0.0185 0.490 7.725 7.578 365.599 0.873 33.709 9.402 0.35 151622. 0.6903
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3.16 0.0379 0.1265 0.0621 0.0186 0.494 7.789 7.414 368.608 0.880 32.979 9.123 0.35 151695. 0.6626
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4.74 0.0569 0.1840 0.0606 0.0187 0.498 7.842 7.241 371.104 0.886 32.208 8.850 0.35 151774. 0.6352
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6.32 0.0759 0.2380 0.0591 0.0188 0.500 7.882 7.058 373.027 0.891 31.395 8.582 0.35 151857. 0.6081
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7.91 0.0949 0.2884 0.0575 0.0189 0.502 7.910 6.866 374.315 0.894 30.540 8.320 0.35 151946. 0.5814
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9.49 0.1138 0.3353 0.0558 0.0189 0.503 7.922 6.664 374.906 0.895 29.643 8.063 0.35 152041. 0.5551
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11.07 0.1328 0.3790 0.0540 0.0189 0.503 7.918 6.453 374.739 0.895 28.704 7.811 0.35 152141. 0.5292
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12.65 0.1518 0.4195 0.0522 0.0189 0.501 7.898 6.233 373.754 0.892 27.724 7.564 0.35 152248. 0.5037
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14.23 0.1708 0.4568 0.0503 0.0188 0.499 7.858 6.004 371.891 0.888 26.704 7.322 0.35 152360. 0.4785
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15.81 0.1897 0.4911 0.0483 0.0186 0.495 7.799 5.765 369.093 0.881 25.644 7.085 0.35 152479. 0.4537
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17.39 0.2087 0.5224 0.0462 0.0185 0.490 7.719 5.518 365.300 0.872 24.545 6.852 0.35 152604. 0.4293
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18.97 0.2277 0.5509 0.0441 0.0182 0.483 7.617 5.263 360.458 0.861 23.409 6.622 0.35 152736. 0.4052
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20.56 0.2467 0.5764 0.0419 0.0179 0.475 7.491 4.999 354.512 0.846 22.236 6.396 0.35 152875. 0.3814
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22.14 0.2656 0.5990 0.0396 0.0176 0.466 7.341 4.728 347.409 0.829 21.028 6.172 0.35 153020. 0.3579
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23.72 0.2846 0.6187 0.0372 0.0171 0.455 7.165 4.448 339.098 0.810 19.787 5.950 0.35 153173. 0.3347
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25.30 0.3036 0.6354 0.0348 0.0166 0.442 6.963 4.162 329.533 0.787 18.513 5.729 0.35 153332. 0.3117
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26.88 0.3226 0.6489 0.0324 0.0161 0.427 6.734 3.869 318.667 0.761 17.209 5.507 0.35 153499. 0.2889
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28.46 0.3415 0.6591 0.0299 0.0155 0.411 6.476 3.569 306.460 0.732 15.876 5.282 0.35 153674. 0.2662
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30.04 0.3605 0.6656 0.0273 0.0148 0.393 6.189 3.263 292.875 0.699 14.515 5.054 0.35 153856. 0.2435
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31.62 0.3795 0.6680 0.0247 0.0140 0.373 5.872 2.952 277.881 0.663 13.130 4.818 0.35 154045. 0.2208
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33.21 0.3985 0.6656 0.0221 0.0132 0.351 5.525 2.635 261.450 0.624 11.722 4.572 0.35 154242. 0.1980
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34.79 0.4174 0.6573 0.0194 0.0123 0.327 5.147 2.314 243.564 0.581 10.294 4.310 0.35 154447. 0.1749
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36.37 0.4364 0.6416 0.0167 0.0113 0.301 4.738 1.989 224.212 0.535 8.848 4.024 0.35 154659. 0.1514
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37.95 0.4554 0.6161 0.0139 0.0103 0.273 4.298 1.661 203.391 0.486 7.386 3.703 0.35 154879. 0.1273
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39.53 0.4744 0.5769 0.0111 0.0092 0.243 3.827 1.329 181.109 0.432 5.913 3.329 0.35 155107. 0.1024
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41.11 0.4933 0.5174 0.0083 0.0080 0.211 3.326 0.996 157.388 0.376 4.431 2.871 0.35 155343. 0.0764
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42.69 0.5123 0.4250 0.0055 0.0067 0.177 2.795 0.662 132.254 0.316 2.945 2.270 0.35 155586. 0.0493
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44.27 0.5313 0.2726 0.0027 0.0053 0.142 2.234 0.327 105.717 0.252 1.456 1.404 0.35 155835. 0.0214
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45.86 0.5503 -0.0292 -0.0002 0.0039 0.102 1.611 -0.024 76.245 0.182 -0.108 -0.145 0.35 156029. 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 0.0655 0.0182 0.941 11.861 12.229 701.652 1.340 54.395 7.905 0.44 189431. 0.7373
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1.98 0.0190 0.0665 0.0642 0.0183 0.950 11.978 11.986 708.586 1.353 53.313 7.672 0.44 189518. 0.7084
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3.96 0.0380 0.1291 0.0628 0.0185 0.958 12.080 11.728 714.628 1.365 52.165 7.443 0.44 189610. 0.6799
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5.93 0.0570 0.1878 0.0614 0.0186 0.965 12.165 11.455 719.643 1.374 50.950 7.219 0.44 189709. 0.6517
|
|
7.91 0.0760 0.2428 0.0598 0.0187 0.970 12.230 11.166 723.504 1.382 49.668 7.000 0.44 189814. 0.6239
|
|
9.89 0.0949 0.2942 0.0582 0.0188 0.974 12.274 10.863 726.090 1.387 48.319 6.786 0.44 189926. 0.5965
|
|
11.87 0.1139 0.3422 0.0565 0.0188 0.975 12.294 10.545 727.279 1.389 46.904 6.576 0.44 190044. 0.5696
|
|
13.85 0.1329 0.3868 0.0547 0.0188 0.975 12.289 10.212 726.948 1.388 45.422 6.372 0.44 190171. 0.5430
|
|
15.82 0.1519 0.4281 0.0529 0.0188 0.972 12.255 9.864 724.979 1.385 43.875 6.171 0.44 190304. 0.5169
|
|
17.80 0.1709 0.4663 0.0509 0.0187 0.967 12.192 9.502 721.252 1.377 42.263 5.975 0.44 190445. 0.4912
|
|
19.78 0.1899 0.5015 0.0489 0.0185 0.960 12.098 9.125 715.654 1.367 40.588 5.783 0.44 190595. 0.4659
|
|
21.76 0.2089 0.5337 0.0468 0.0183 0.950 11.970 8.735 708.068 1.352 38.852 5.595 0.44 190752. 0.4410
|
|
23.74 0.2279 0.5630 0.0446 0.0181 0.937 11.806 8.331 698.385 1.334 37.056 5.411 0.44 190917. 0.4165
|
|
25.71 0.2469 0.5894 0.0424 0.0178 0.921 11.605 7.914 686.495 1.311 35.202 5.229 0.44 191091. 0.3923
|
|
27.69 0.2658 0.6130 0.0401 0.0174 0.902 11.365 7.485 672.294 1.284 33.292 5.050 0.44 191274. 0.3685
|
|
29.67 0.2848 0.6338 0.0377 0.0170 0.879 11.084 7.043 655.683 1.252 31.329 4.872 0.44 191465. 0.3449
|
|
31.65 0.3038 0.6515 0.0353 0.0165 0.854 10.761 6.591 636.566 1.216 29.315 4.696 0.44 191665. 0.3215
|
|
33.63 0.3228 0.6663 0.0328 0.0159 0.825 10.394 6.127 614.854 1.174 27.252 4.520 0.44 191875. 0.2984
|
|
35.60 0.3418 0.6778 0.0303 0.0153 0.792 9.981 5.653 590.464 1.128 25.143 4.342 0.44 192093. 0.2753
|
|
37.58 0.3608 0.6857 0.0277 0.0146 0.755 9.523 5.169 563.326 1.076 22.991 4.162 0.44 192321. 0.2524
|
|
39.56 0.3798 0.6897 0.0251 0.0138 0.715 9.016 4.676 533.373 1.019 20.800 3.977 0.44 192558. 0.2294
|
|
41.54 0.3988 0.6890 0.0224 0.0129 0.671 8.462 4.175 500.553 0.956 18.572 3.783 0.44 192805. 0.2062
|
|
43.52 0.4178 0.6826 0.0196 0.0120 0.623 7.858 3.667 464.830 0.888 16.311 3.578 0.44 193062. 0.1828
|
|
45.49 0.4367 0.6692 0.0169 0.0110 0.572 7.204 3.152 426.179 0.814 14.022 3.355 0.44 193328. 0.1589
|
|
47.47 0.4557 0.6461 0.0141 0.0099 0.516 6.501 2.632 384.597 0.735 11.709 3.104 0.44 193603. 0.1343
|
|
49.45 0.4747 0.6095 0.0113 0.0088 0.456 5.749 2.108 340.101 0.650 9.377 2.811 0.44 193889. 0.1089
|
|
51.43 0.4937 0.5522 0.0085 0.0076 0.393 4.948 1.581 292.730 0.559 7.031 2.449 0.44 194184. 0.0821
|
|
53.41 0.5127 0.4604 0.0056 0.0063 0.325 4.100 1.052 242.543 0.463 4.677 1.967 0.44 194488. 0.0538
|
|
55.38 0.5317 0.3031 0.0028 0.0049 0.254 3.204 0.522 189.555 0.362 2.320 1.248 0.44 194800. 0.0240
|
|
57.36 0.5507
|
|
|
|
|
|
|
|
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 0.0665 0.0182 1.631 17.135 17.880 1216.329 1.936 79.528 6.667 0.52 227301. 0.7519
|
|
2.37 0.0190 0.0673 0.0652 0.0184 1.648 17.308 17.527 1228.612 1.955 77.961 6.471 0.52 227406. 0.7225
|
|
4.74 0.0379 0.1305 0.0638 0.0186 1.662 17.458 17.153 1239.301 1.972 76.294 6.278 0.52 227517. 0.6934
|
|
7.12 0.0569 0.1899 0.0623 0.0187 1.674 17.583 16.756 1248.155 1.987 74.530 6.089 0.52 227636. 0.6648
|
|
9.49 0.0759 0.2456 0.0608 0.0188 1.683 17.679 16.337 1254.955 1.997 72.668 5.905 0.52 227763. 0.6365
|
|
11.86 0.0949 0.2976 0.0591 0.0189 1.689 17.742 15.896 1259.482 2.005 70.707 5.725 0.52 227898. 0.6087
|
|
14.23 0.1138 0.3462 0.0574 0.0189 1.692 17.771 15.433 1261.526 2.008 68.647 5.549 0.52 228041. 0.5814
|
|
16.60 0.1328 0.3914 0.0556 0.0189 1.691 17.762 14.948 1260.871 2.007 66.490 5.377 0.52 228193. 0.5545
|
|
18.97 0.1518 0.4334 0.0537 0.0188 1.686 17.712 14.442 1257.312 2.001 64.237 5.210 0.52 228354. 0.5280
|
|
21.35 0.1708 0.4722 0.0518 0.0187 1.677 17.618 13.914 1250.643 1.990 61.889 5.046 0.52 228524. 0.5020
|
|
23.72 0.1897 0.5080 0.0497 0.0186 1.664 17.477 13.365 1240.661 1.975 59.448 4.886 0.52 228704. 0.4764
|
|
26.09 0.2087 0.5409 0.0476 0.0184 1.646 17.287 12.796 1227.168 1.953 56.917 4.730 0.52 228893. 0.4512
|
|
28.46 0.2277 0.5710 0.0454 0.0181 1.623 17.045 12.207 1209.970 1.926 54.298 4.576 0.52 229092. 0.4264
|
|
30.83 0.2467 0.5982 0.0432 0.0178 1.594 16.748 11.600 1188.880 1.892 51.595 4.425 0.53 229301. 0.4020
|
|
33.20 0.2656 0.6226 0.0408 0.0174 1.561 16.393 10.973 1163.716 1.852 48.809 4.277 0.53 229521. 0.3779
|
|
35.58 0.2846 0.6442 0.0384 0.0170 1.521 15.979 10.329 1134.304 1.805 45.945 4.130 0.53 229751. 0.3540
|
|
37.95 0.3036 0.6629 0.0360 0.0165 1.476 15.502 9.668 1100.477 1.751 43.005 3.985 0.53 229991. 0.3305
|
|
40.32 0.3226 0.6787 0.0335 0.0159 1.424 14.962 8.992 1062.081 1.690 39.994 3.840 0.53 230243. 0.3071
|
|
42.69 0.3415 0.6914 0.0309 0.0153 1.366 14.354 8.299 1018.971 1.622 36.916 3.694 0.53 230505. 0.2839
|
|
45.06 0.3605 0.7007 0.0283 0.0145 1.302 13.679 7.593 971.020 1.545 33.774 3.547 0.53 230778. 0.2607
|
|
47.43 0.3795 0.7061 0.0256 0.0137 1.231 12.934 6.874 918.114 1.461 30.574 3.396 0.53 231063. 0.2374
|
|
49.81 0.3984 0.7072 0.0229 0.0129 1.153 12.117 6.142 860.163 1.369 27.320 3.239 0.53 231359. 0.2141
|
|
52.18 0.4174 0.7028 0.0201 0.0119 1.069 11.229 5.399 797.096 1.269 24.017 3.072 0.53 231667. 0.1904
|
|
54.55 0.4364 0.6916 0.0173 0.0109 0.977 10.268 4.647 728.873 1.160 20.672 2.892 0.53 231986. 0.1663
|
|
56.92 0.4554 0.6712 0.0145 0.0098 0.879 9.234 3.887 655.487 1.043 17.290 2.690 0.53 232317. 0.1414
|
|
59.29 0.4743 0.6377 0.0116 0.0086 0.774 8.128 3.121 576.965 0.918 13.881 2.453 0.53 232659. 0.1156
|
|
61.66 0.4933 0.5839 0.0087 0.0074 0.662 6.950 2.349 493.379 0.785 10.450 2.160 0.53 233013. 0.0883
|
|
64.04 0.5123 0.4956 0.0059 0.0061 0.543 5.703 1.576 404.827 0.644 7.008 1.765 0.53 233377. 0.0591
|
|
66.41 0.5313 0.3395 0.0030 0.0047 0.418 4.386 0.800 311.351 0.496 3.560 1.166 0.53 233752. 0.0278
|
|
68.78 0.5502 -0.0047 0.0000 0.0031 0.280 2.938 -0.007 208.572 0.332 -0.032 -0.016 0.53 234062. 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 0.0678 0.0184 2.624 23.627 24.801 1956.726 2.669 110.314 5.749 0.61 265161. 0.7636
|
|
2.78 0.0190 0.0679 0.0665 0.0186 2.651 23.870 24.316 1976.849 2.697 108.156 5.579 0.61 265284. 0.7337
|
|
5.55 0.0381 0.1318 0.0651 0.0188 2.674 24.081 23.799 1994.306 2.721 105.858 5.413 0.61 265415. 0.7043
|
|
8.33 0.0571 0.1917 0.0636 0.0189 2.694 24.254 23.251 2008.695 2.740 103.422 5.250 0.61 265556. 0.6752
|
|
11.10 0.0761 0.2479 0.0620 0.0190 2.708 24.387 22.672 2019.654 2.755 100.846 5.092 0.61 265705. 0.6466
|
|
13.88 0.0952 0.3004 0.0603 0.0191 2.718 24.473 22.062 2026.828 2.765 98.131 4.937 0.61 265865. 0.6185
|
|
16.66 0.1142 0.3495 0.0586 0.0191 2.722 24.510 21.420 2029.871 2.769 95.276 4.786 0.61 266034. 0.5908
|
|
19.43 0.1333 0.3952 0.0567 0.0191 2.720 24.493 20.747 2028.439 2.767 92.284 4.639 0.61 266213. 0.5636
|
|
22.21 0.1523 0.4377 0.0548 0.0191 2.712 24.417 20.044 2022.193 2.759 89.156 4.496 0.61 266403. 0.5368
|
|
24.99 0.1713 0.4771 0.0528 0.0190 2.697 24.280 19.311 2010.802 2.743 85.895 4.356 0.61 266604. 0.5105
|
|
27.76 0.1904 0.5135 0.0507 0.0188 2.674 24.076 18.548 1993.940 2.720 82.503 4.219 0.61 266816. 0.4847
|
|
30.54 0.2094 0.5470 0.0485 0.0186 2.644 23.803 17.757 1971.289 2.689 78.984 4.086 0.61 267039. 0.4592
|
|
33.31 0.2284 0.5776 0.0463 0.0183 2.605 23.455 16.938 1942.537 2.650 75.341 3.955 0.61 267273. 0.4341
|
|
36.09 0.2475 0.6055 0.0440 0.0180 2.558 23.031 16.092 1907.384 2.602 71.579 3.827 0.61 267520. 0.4094
|
|
38.87 0.2665 0.6306 0.0416 0.0176 2.502 22.526 15.221 1865.534 2.545 67.702 3.701 0.61 267778. 0.3851
|
|
41.64 0.2856 0.6529 0.0392 0.0171 2.436 21.936 14.324 1816.708 2.478 63.714 3.576 0.61 268049. 0.3610
|
|
44.42 0.3046 0.6724 0.0366 0.0166 2.361 21.259 13.404 1760.638 2.402 59.620 3.453 0.61 268332. 0.3372
|
|
47.20 0.3236 0.6891 0.0341 0.0160 2.276 20.492 12.461 1697.078 2.315 55.426 3.330 0.61 268628. 0.3135
|
|
49.97 0.3427 0.7027 0.0314 0.0153 2.180 19.631 11.497 1625.791 2.218 51.136 3.207 0.61 268936. 0.2900
|
|
52.75 0.3617 0.7129 0.0287 0.0146 2.074 18.674 10.512 1546.571 2.110 46.758 3.083 0.61 269258. 0.2666
|
|
55.52 0.3807 0.7195 0.0260 0.0138 1.957 17.620 9.509 1459.237 1.991 42.297 2.956 0.62 269593. 0.2431
|
|
58.30 0.3998 0.7217 0.0232 0.0129 1.829 16.465 8.489 1363.642 1.860 37.761 2.824 0.62 269941. 0.2194
|
|
61.08 0.4188 0.7187 0.0204 0.0119 1.689 15.210 7.454 1259.673 1.718 33.155 2.684 0.62 270303. 0.1954
|
|
63.85 0.4379 0.7089 0.0175 0.0108 1.539 13.853 6.405 1147.267 1.565 28.490 2.532 0.62 270678. 0.1709
|
|
66.63 0.4569 0.6899 0.0146 0.0097 1.376 12.394 5.345 1026.416 1.400 23.774 2.362 0.62 271066. 0.1456
|
|
69.41 0.4759 0.6577 0.0117 0.0085 1.203 10.833 4.276 897.169 1.224 19.018 2.162 0.62 271468. 0.1192
|
|
72.18 0.4950 0.6046 0.0087 0.0072 1.019 9.172 3.200 759.648 1.036 14.233 1.911 0.62 271884. 0.0912
|
|
74.96 0.5140 0.5147 0.0058 0.0058 0.823 7.414 2.120 614.020 0.838 9.431 1.566 0.62 272312. 0.0608
|
|
77.73 0.5330 0.3488 0.0028 0.0043 0.617 5.558 1.039 460.316 0.628 4.620 1.023 0.62 272751. 0.0278
|
|
80.51 0.5521
|
|
|
|
|
|
|
|
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 0.0694 0.0189 4.011 31.602 33.161 2991.146 3.570 147.499 5.028 0.70 303005. 0.7723
|
|
3.18 0.0191 0.0681 0.0681 0.0191 4.052 31.924 32.521 3021.543 3.607 144.651 4.882 0.70 303147. 0.7425
|
|
6.36 0.0382 0.1321 0.0666 0.0192 4.087 32.202 31.837 3047.887 3.638 141.612 4.738 0.70 303299. 0.7130
|
|
9.54 0.0573 0.1923 0.0651 0.0194 4.116 32.431 31.111 3069.529 3.664 138.383 4.597 0.70 303462. 0.6839
|
|
12.72 0.0763 0.2487 0.0635 0.0195 4.138 32.603 30.342 3085.873 3.683 134.963 4.460 0.70 303635. 0.6552
|
|
15.90 0.0954 0.3016 0.0618 0.0196 4.152 32.714 29.530 3096.343 3.696 131.351 4.326 0.70 303820. 0.6270
|
|
19.08 0.1145 0.3510 0.0600 0.0196 4.158 32.756 28.676 3100.379 3.701 127.550 4.195 0.70 304016. 0.5992
|
|
22.26 0.1336 0.3970 0.0581 0.0196 4.154 32.725 27.779 3097.422 3.697 123.560 4.068 0.70 304223. 0.5718
|
|
25.44 0.1527 0.4399 0.0562 0.0195 4.140 32.614 26.840 3086.939 3.685 119.384 3.944 0.70 304443. 0.5449
|
|
28.63 0.1718 0.4797 0.0541 0.0194 4.115 32.419 25.860 3068.418 3.663 115.027 3.823 0.70 304674. 0.5185
|
|
31.81 0.1908 0.5166 0.0520 0.0192 4.079 32.133 24.841 3041.366 3.630 110.491 3.705 0.70 304919. 0.4924
|
|
34.99 0.2099 0.5505 0.0498 0.0190 4.030 31.752 23.782 3005.302 3.587 105.783 3.589 0.70 305177. 0.4668
|
|
38.17 0.2290 0.5817 0.0475 0.0187 3.969 31.271 22.686 2959.760 3.533 100.906 3.476 0.70 305447. 0.4416
|
|
41.35 0.2481 0.6101 0.0451 0.0183 3.895 30.685 21.553 2904.279 3.467 95.866 3.366 0.70 305732. 0.4168
|
|
44.53 0.2672 0.6359 0.0427 0.0179 3.806 29.989 20.385 2838.428 3.388 90.671 3.257 0.70 306030. 0.3922
|
|
47.71 0.2863 0.6589 0.0401 0.0174 3.704 29.179 19.183 2761.778 3.297 85.324 3.150 0.70 306342. 0.3680
|
|
50.89 0.3053 0.6792 0.0376 0.0169 3.586 28.251 17.948 2673.932 3.192 79.834 3.045 0.70 306668. 0.3440
|
|
54.07 0.3244 0.6967 0.0349 0.0163 3.452 27.201 16.683 2574.515 3.073 74.208 2.939 0.70 307009. 0.3202
|
|
57.25 0.3435 0.7112 0.0322 0.0156 3.303 26.024 15.389 2463.174 2.940 68.452 2.834 0.70 307364. 0.2965
|
|
60.43 0.3626 0.7226 0.0294 0.0148 3.137 24.719 14.068 2339.597 2.793 62.575 2.727 0.70 307735. 0.2728
|
|
63.61 0.3817 0.7303 0.0266 0.0139 2.955 23.281 12.721 2203.507 2.630 56.585 2.619 0.70 308120. 0.2491
|
|
66.79 0.4008 0.7338 0.0238 0.0130 2.755 21.708 11.352 2054.683 2.453 50.492 2.506 0.70 308520. 0.2252
|
|
69.97 0.4198 0.7321 0.0208 0.0120 2.538 20.000 9.961 1892.952 2.260 44.305 2.387 0.70 308936. 0.2009
|
|
73.15 0.4389 0.7239 0.0179 0.0109 2.304 18.154 8.551 1718.223 2.051 38.035 2.257 0.70 309367. 0.1761
|
|
76.33 0.4580 0.7067 0.0149 0.0097 2.052 16.170 7.126 1530.484 1.827 31.696 2.112 0.71 309814. 0.1504
|
|
79.52 0.4771 0.6763 0.0119 0.0084 1.783 14.050 5.688 1329.817 1.587 25.301 1.940 0.71 310276. 0.1234
|
|
82.70 0.4962 0.6247 0.0089 0.0071 1.497 11.795 4.241 1116.415 1.333 18.866 1.723 0.71 310753. 0.0947
|
|
85.88 0.5153 0.5348 0.0058 0.0056 1.194 9.409 2.789 890.556 1.063 12.407 1.421 0.71 311245. 0.0633
|
|
89.06 0.5343 0.3621 0.0028 0.0041 0.875 6.892 1.334 652.287 0.779 5.933 0.928 0.71 311749. 0.0286
|
|
92.24 0.5534
|
|
|
|
|
|
|
|
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 0.0714 0.0203 6.131 42.934 43.194 4571.669 4.851 192.129 4.285 0.79 340827. 0.7512
|
|
3.56 0.0190 0.0653 0.0701 0.0204 6.166 43.182 42.386 4598.015 4.879 188.531 4.181 0.79 340988. 0.7260
|
|
7.13 0.0380 0.1274 0.0687 0.0205 6.194 43.378 41.519 4618.889 4.901 184.678 4.077 0.79 341161. 0.7007
|
|
10.69 0.0570 0.1862 0.0671 0.0206 6.214 43.515 40.596 4633.540 4.916 180.571 3.974 0.79 341345. 0.6753
|
|
14.25 0.0760 0.2419 0.0655 0.0206 6.224 43.588 39.615 4641.283 4.925 176.209 3.871 0.79 341542. 0.6499
|
|
17.81 0.0950 0.2944 0.0638 0.0206 6.224 43.589 38.577 4641.421 4.925 171.591 3.770 0.79 341750. 0.6245
|
|
21.38 0.1140 0.3439 0.0620 0.0206 6.213 43.513 37.482 4633.269 4.916 166.720 3.669 0.79 341972. 0.5991
|
|
24.94 0.1330 0.3903 0.0601 0.0205 6.190 43.352 36.330 4616.123 4.898 161.598 3.570 0.79 342206. 0.5739
|
|
28.50 0.1520 0.4338 0.0581 0.0204 6.154 43.100 35.123 4589.266 4.869 156.229 3.471 0.79 342455. 0.5487
|
|
32.07 0.1710 0.4743 0.0560 0.0202 6.104 42.749 33.862 4551.966 4.830 150.619 3.374 0.79 342716. 0.5237
|
|
35.63 0.1900 0.5120 0.0538 0.0200 6.039 42.294 32.548 4503.481 4.778 144.774 3.278 0.79 342992. 0.4988
|
|
39.19 0.2090 0.5469 0.0516 0.0197 5.958 41.726 31.182 4443.044 4.714 138.699 3.183 0.79 343283. 0.4741
|
|
42.75 0.2280 0.5791 0.0492 0.0194 5.860 41.039 29.767 4369.880 4.637 132.401 3.090 0.79 343588. 0.4496
|
|
46.32 0.2470 0.6086 0.0468 0.0190 5.744 40.225 28.302 4283.211 4.545 125.889 2.997 0.79 343908. 0.4253
|
|
49.88 0.2660 0.6354 0.0443 0.0186 5.609 39.277 26.792 4182.276 4.438 119.170 2.906 0.79 344243. 0.4011
|
|
53.44 0.2850 0.6595 0.0417 0.0180 5.453 38.188 25.236 4066.323 4.315 112.251 2.815 0.79 344594. 0.3772
|
|
57.01 0.3040 0.6810 0.0391 0.0175 5.276 36.952 23.638 3934.644 4.175 105.143 2.725 0.79 344960. 0.3533
|
|
60.57 0.3230 0.6997 0.0364 0.0168 5.078 35.561 21.999 3786.577 4.018 97.853 2.635 0.79 345343. 0.3296
|
|
64.13 0.3420 0.7156 0.0336 0.0161 4.857 34.011 20.322 3621.507 3.843 90.392 2.545 0.79 345742. 0.3060
|
|
67.69 0.3610 0.7284 0.0308 0.0153 4.612 32.296 18.608 3438.935 3.649 82.769 2.454 0.79 346157. 0.2824
|
|
71.26 0.3800 0.7376 0.0279 0.0144 4.343 30.416 16.861 3238.719 3.436 74.996 2.361 0.79 346588. 0.2586
|
|
74.82 0.3990 0.7429 0.0249 0.0134 4.050 28.365 15.082 3020.346 3.205 67.084 2.265 0.79 347037. 0.2346
|
|
78.38 0.4180 0.7432 0.0220 0.0123 3.733 26.144 13.275 2783.779 2.954 59.045 2.163 0.79 347502. 0.2102
|
|
81.95 0.4370 0.7372 0.0189 0.0112 3.392 23.752 11.442 2529.174 2.684 50.894 2.052 0.79 347985. 0.1851
|
|
85.51 0.4560 0.7223 0.0159 0.0100 3.026 21.195 9.588 2256.855 2.395 42.646 1.927 0.79 348484. 0.1591
|
|
89.07 0.4750 0.6946 0.0128 0.0087 2.638 18.477 7.715 1967.439 2.088 34.318 1.779 0.79 349001. 0.1318
|
|
92.63 0.4940 0.6462 0.0096 0.0074 2.229 15.607 5.830 1661.802 1.763 25.930 1.591 0.80 349534. 0.1025
|
|
96.20 0.5131 0.5613 0.0065 0.0059 1.798 12.594 3.935 1341.014 1.423 17.503 1.331 0.80 350084. 0.0704
|
|
99.76 0.5321 0.4012 0.0034 0.0045 1.349 9.447 2.035 1005.972 1.067 9.050 0.917 0.80 350648. 0.0349
|
|
103.32 0.5511 0.0175 0.0001 0.0028 0.857 6.003 0.055 639.238 0.678 0.243 0.039 0.80 351121. 0.0002
|
|
|
|
|
|
|
|
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 0.0738 0.0249 10.334 65.136 55.057 7706.353 7.359 244.894 3.240 0.87 378626. 0.6413
|
|
4.04 0.0194 0.0565 0.0724 0.0248 10.300 64.920 54.060 7680.835 7.335 240.459 3.192 0.87 378810. 0.6260
|
|
8.07 0.0387 0.1112 0.0710 0.0247 10.251 64.610 52.983 7644.152 7.300 235.670 3.144 0.87 379008. 0.6103
|
|
12.11 0.0581 0.1642 0.0694 0.0246 10.186 64.202 51.827 7595.892 7.254 230.526 3.095 0.87 379219. 0.5942
|
|
16.14 0.0775 0.2155 0.0678 0.0244 10.106 63.694 50.590 7535.696 7.196 225.023 3.045 0.87 379445. 0.5776
|
|
20.18 0.0968 0.2649 0.0660 0.0241 10.008 63.081 49.272 7463.244 7.127 219.162 2.994 0.87 379685. 0.5606
|
|
24.21 0.1162 0.3124 0.0641 0.0239 9.894 62.363 47.874 7378.246 7.046 212.945 2.943 0.87 379940. 0.5431
|
|
28.25 0.1356 0.3580 0.0622 0.0235 9.763 61.535 46.398 7280.341 6.952 206.376 2.891 0.87 380211. 0.5251
|
|
32.28 0.1550 0.4015 0.0601 0.0232 9.614 60.595 44.843 7169.157 6.846 199.463 2.837 0.87 380498. 0.5067
|
|
36.32 0.1743 0.4430 0.0579 0.0228 9.447 59.540 43.213 7044.279 6.727 192.211 2.782 0.87 380800. 0.4878
|
|
40.35 0.1937 0.4823 0.0556 0.0223 9.260 58.365 41.509 6905.264 6.594 184.632 2.727 0.87 381119. 0.4685
|
|
44.39 0.2131 0.5194 0.0532 0.0218 9.054 57.066 39.733 6751.571 6.447 176.734 2.669 0.87 381455. 0.4488
|
|
48.42 0.2324 0.5542 0.0508 0.0213 8.827 55.638 37.889 6582.589 6.286 168.530 2.611 0.88 381808. 0.4286
|
|
52.46 0.2518 0.5866 0.0482 0.0207 8.579 54.074 35.978 6397.565 6.109 160.030 2.551 0.88 382178. 0.4081
|
|
56.49 0.2712 0.6165 0.0455 0.0200 8.309 52.367 34.003 6195.654 5.916 151.247 2.489 0.88 382565. 0.3872
|
|
60.53 0.2905 0.6438 0.0428 0.0193 8.014 50.510 31.968 5975.930 5.707 142.192 2.426 0.88 382971. 0.3659
|
|
64.56 0.3099 0.6685 0.0400 0.0186 7.694 48.494 29.874 5737.387 5.479 132.879 2.362 0.88 383394. 0.3443
|
|
68.60 0.3293 0.6903 0.0371 0.0177 7.347 46.310 27.725 5478.984 5.232 123.322 2.295 0.88 383836. 0.3223
|
|
72.64 0.3486 0.7090 0.0342 0.0168 6.973 43.949 25.524 5199.635 4.965 113.532 2.227 0.88 384297. 0.3000
|
|
76.67 0.3680 0.7244 0.0312 0.0158 6.569 41.401 23.275 4898.272 4.678 103.525 2.155 0.88 384776. 0.2773
|
|
80.71 0.3874 0.7355 0.0281 0.0148 6.139 38.690 20.979 4577.537 4.371 93.314 2.079 0.88 385275. 0.2539
|
|
84.74 0.4068 0.7365 0.0250 0.0138 5.718 36.040 18.637 4263.974 4.072 82.898 1.982 0.88 385792. 0.2283
|
|
88.78 0.4261 0.7298 0.0218 0.0127 5.273 33.236 16.257 3932.241 3.755 72.310 1.875 0.88 386329. 0.2016
|
|
92.81 0.4455 0.7131 0.0185 0.0116 4.804 30.280 13.843 3582.510 3.421 61.572 1.753 0.88 386886. 0.1739
|
|
96.85 0.4649 0.6824 0.0153 0.0104 4.314 27.190 11.399 3216.943 3.072 50.705 1.607 0.88 387461. 0.1447
|
|
100.88 0.4842 0.6316 0.0120 0.0092 3.805 23.982 8.933 2837.314 2.709 39.736 1.428 0.88 388057. 0.1138
|
|
104.92 0.5036 0.5500 0.0086 0.0079 3.281 20.680 6.451 2446.721 2.336 28.692 1.196 0.88 388672. 0.0810
|
|
108.95 0.5230 0.4187 0.0053 0.0066 2.746 17.309 3.957 2047.835 1.956 17.602 0.877 0.88 389304. 0.0465
|
|
112.99 0.5423 0.1988 0.0019 0.0053 2.199 13.860 1.451 1639.858 1.566 6.455 0.401 0.89 389946. 0.0129
|
|
117.02 0.5617
|
|
|
|
|
|
|
|
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 0.0739 0.0313 17.300 99.124 66.710 12900.256 11.199 296.726 2.346 0.96 416486. 0.5109
|
|
4.48 0.0195 0.0454 0.0727 0.0313 17.279 99.006 65.683 12884.936 11.186 292.157 2.312 0.96 416684. 0.4998
|
|
8.95 0.0391 0.0894 0.0715 0.0312 17.232 98.739 64.561 12850.206 11.155 287.167 2.279 0.96 416898. 0.4883
|
|
13.43 0.0586 0.1322 0.0701 0.0311 17.156 98.304 63.341 12793.519 11.106 281.740 2.246 0.96 417127. 0.4767
|
|
17.90 0.0781 0.1737 0.0687 0.0309 17.047 97.680 62.018 12712.305 11.036 275.857 2.213 0.96 417373. 0.4648
|
|
22.38 0.0976 0.2139 0.0671 0.0306 16.902 96.847 60.590 12603.984 10.942 269.504 2.180 0.96 417635. 0.4527
|
|
26.85 0.1172 0.2529 0.0654 0.0303 16.717 95.788 59.053 12466.090 10.822 262.667 2.149 0.96 417915. 0.4404
|
|
31.33 0.1367 0.2908 0.0635 0.0299 16.490 94.483 57.405 12296.253 10.675 255.336 2.117 0.96 418213. 0.4279
|
|
35.80 0.1562 0.3276 0.0616 0.0294 16.216 92.917 55.644 12092.556 10.498 247.505 2.087 0.96 418529. 0.4152
|
|
40.28 0.1758 0.3633 0.0595 0.0288 15.896 91.082 53.770 11853.696 10.290 239.171 2.057 0.96 418864. 0.4024
|
|
44.75 0.1953 0.3980 0.0573 0.0281 15.528 88.973 51.785 11579.150 10.052 230.338 2.028 0.96 419218. 0.3893
|
|
49.23 0.2148 0.4316 0.0550 0.0274 15.112 86.591 49.688 11269.268 9.783 221.013 2.000 0.96 419591. 0.3760
|
|
53.70 0.2343 0.4641 0.0526 0.0265 14.651 83.947 47.484 10925.082 9.484 211.210 1.971 0.96 419985. 0.3623
|
|
58.18 0.2539 0.4955 0.0500 0.0256 14.145 81.049 45.177 10548.003 9.157 200.945 1.943 0.96 420398. 0.3482
|
|
62.65 0.2734 0.5255 0.0473 0.0246 13.597 77.911 42.770 10139.609 8.802 190.239 1.913 0.96 420832. 0.3337
|
|
67.13 0.2929 0.5540 0.0446 0.0236 13.010 74.546 40.268 9701.615 8.422 179.113 1.883 0.96 421286. 0.3186
|
|
71.60 0.3124 0.5808 0.0417 0.0224 12.385 70.965 37.678 9235.637 8.018 167.592 1.850 0.96 421761. 0.3029
|
|
76.08 0.3320 0.6057 0.0388 0.0212 11.725 67.181 35.005 8743.071 7.590 155.701 1.816 0.97 422257. 0.2866
|
|
80.55 0.3515 0.6281 0.0357 0.0200 11.030 63.200 32.254 8224.992 7.140 143.467 1.779 0.97 422773. 0.2694
|
|
85.03 0.3710 0.6478 0.0326 0.0187 10.302 59.027 29.433 7681.967 6.669 130.918 1.738 0.97 423311. 0.2515
|
|
89.50 0.3906 0.6637 0.0294 0.0173 9.546 54.699 26.546 7118.690 6.180 118.078 1.691 0.97 423870. 0.2324
|
|
93.98 0.4101 0.6709 0.0261 0.0160 8.814 50.503 23.596 6572.548 5.706 104.954 1.628 0.97 424450. 0.2110
|
|
98.45 0.4296 0.6567 0.0228 0.0149 8.226 47.136 20.577 6134.354 5.325 91.527 1.521 0.97 425052. 0.1841
|
|
102.93 0.4491 0.6210 0.0194 0.0140 7.736 44.324 17.503 5768.438 5.008 77.854 1.376 0.97 425675. 0.1536
|
|
107.40 0.4687 0.5691 0.0159 0.0131 7.244 41.505 14.394 5401.602 4.689 64.024 1.209 0.97 426320. 0.1223
|
|
111.88 0.4882 0.4969 0.0125 0.0122 6.760 38.737 11.260 5041.298 4.376 50.084 1.013 0.97 426987. 0.0907
|
|
116.35 0.5077 0.4004 0.0090 0.0114 6.289 36.036 8.115 4689.819 4.071 36.097 0.785 0.97 427675. 0.0596
|
|
120.83 0.5273 0.2748 0.0055 0.0106 5.830 33.407 4.972 4347.676 3.774 22.117 0.519 0.97 428384. 0.0309
|
|
125.30 0.5468 0.1137 0.0020 0.0097 5.374 30.791 1.828 4007.238 3.479 8.131 0.207 0.97 429111. 0.0075
|
|
129.78 0.5663
|
|
|
|
|
|
|