686 lines
122 KiB
Plaintext
686 lines
122 KiB
Plaintext
13x10F (13x10F.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 0.1165 0.0579 0.002 0.109 0.106 1.290 0.012 0.472 37.277 0.05 18059. 0.5479
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0.39 0.0316 0.0621 0.1155 0.0589 0.002 0.111 0.105 1.312 0.013 0.468 36.344 0.05 18075. 0.5318
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0.78 0.0633 0.1209 0.1144 0.0599 0.002 0.113 0.104 1.334 0.013 0.463 35.398 0.05 18093. 0.5155
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1.17 0.0949 0.1765 0.1131 0.0608 0.002 0.115 0.103 1.355 0.013 0.458 34.445 0.05 18114. 0.4988
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1.56 0.1266 0.2288 0.1117 0.0618 0.002 0.116 0.102 1.376 0.013 0.452 33.491 0.05 18136. 0.4819
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1.95 0.1582 0.2778 0.1100 0.0627 0.002 0.118 0.100 1.396 0.013 0.446 32.539 0.05 18160. 0.4648
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2.34 0.1898 0.3237 0.1082 0.0635 0.002 0.120 0.099 1.414 0.014 0.438 31.594 0.05 18186. 0.4476
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2.73 0.2215 0.3665 0.1062 0.0642 0.002 0.121 0.097 1.430 0.014 0.430 30.661 0.05 18215. 0.4303
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3.12 0.2531 0.4063 0.1040 0.0648 0.002 0.122 0.095 1.443 0.014 0.421 29.741 0.05 18247. 0.4130
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3.51 0.2848 0.4432 0.1015 0.0652 0.002 0.123 0.092 1.453 0.014 0.411 28.838 0.05 18280. 0.3956
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3.90 0.3164 0.4773 0.0987 0.0654 0.002 0.123 0.090 1.458 0.014 0.400 27.952 0.05 18317. 0.3781
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4.28 0.3480 0.5087 0.0956 0.0654 0.002 0.123 0.087 1.458 0.014 0.387 27.082 0.05 18356. 0.3606
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4.67 0.3797 0.5375 0.0923 0.0652 0.002 0.123 0.084 1.452 0.014 0.374 26.229 0.05 18397. 0.3431
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5.06 0.4113 0.5636 0.0886 0.0647 0.002 0.122 0.081 1.441 0.014 0.359 25.389 0.05 18441. 0.3254
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5.45 0.4430 0.5871 0.0846 0.0638 0.002 0.120 0.077 1.422 0.014 0.343 24.558 0.05 18488. 0.3076
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5.84 0.4746 0.6078 0.0803 0.0627 0.002 0.118 0.073 1.397 0.013 0.325 23.730 0.05 18537. 0.2896
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6.23 0.5063 0.6256 0.0757 0.0612 0.002 0.115 0.069 1.364 0.013 0.306 22.898 0.05 18589. 0.2712
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6.62 0.5379 0.6402 0.0707 0.0594 0.002 0.112 0.064 1.324 0.013 0.286 22.052 0.05 18644. 0.2525
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7.01 0.5695 0.6511 0.0655 0.0573 0.002 0.108 0.060 1.276 0.012 0.265 21.181 0.05 18701. 0.2334
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7.40 0.6012 0.6577 0.0600 0.0549 0.002 0.103 0.055 1.222 0.012 0.243 20.272 0.05 18760. 0.2138
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7.79 0.6328 0.6594 0.0544 0.0522 0.002 0.098 0.049 1.162 0.011 0.220 19.307 0.05 18822. 0.1938
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8.18 0.6645 0.6550 0.0485 0.0492 0.001 0.093 0.044 1.097 0.010 0.196 18.266 0.05 18887. 0.1733
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8.57 0.6961 0.6433 0.0426 0.0461 0.001 0.087 0.039 1.027 0.010 0.172 17.123 0.05 18954. 0.1522
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8.96 0.7277 0.6223 0.0365 0.0427 0.001 0.080 0.033 0.952 0.009 0.148 15.844 0.05 19024. 0.1304
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9.35 0.7594 0.5894 0.0304 0.0392 0.001 0.074 0.028 0.873 0.008 0.123 14.381 0.05 19095. 0.1080
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9.74 0.7910 0.5407 0.0242 0.0355 0.001 0.067 0.022 0.790 0.008 0.098 12.664 0.05 19170. 0.0849
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10.13 0.8227 0.4702 0.0181 0.0316 0.001 0.059 0.016 0.704 0.007 0.073 10.591 0.05 19247. 0.0613
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10.52 0.8543 0.3687 0.0119 0.0276 0.001 0.052 0.011 0.615 0.006 0.048 7.996 0.05 19326. 0.0376
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10.91 0.8859 0.2201 0.0058 0.0235 0.001 0.044 0.005 0.524 0.005 0.024 4.603 0.05 19407. 0.0152
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11.30 0.9176 -0.0049 -0.0001 0.0194 0.001 0.036 0.000 0.432 0.004 0.000 -0.099 0.05 19491. 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 0.1169 0.0533 0.013 0.402 0.426 9.508 0.045 1.893 20.300 0.10 36118. 0.5977
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0.78 0.0318 0.0678 0.1159 0.0544 0.013 0.410 0.422 9.692 0.046 1.877 19.745 0.10 36151. 0.5789
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1.57 0.0636 0.1318 0.1148 0.0554 0.013 0.417 0.418 9.878 0.047 1.859 19.185 0.10 36187. 0.5597
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2.35 0.0954 0.1919 0.1135 0.0565 0.013 0.425 0.413 10.064 0.048 1.838 18.624 0.10 36227. 0.5404
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3.13 0.1273 0.2481 0.1121 0.0575 0.014 0.433 0.408 10.245 0.049 1.815 18.065 0.10 36272. 0.5209
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3.92 0.1591 0.3006 0.1105 0.0584 0.014 0.440 0.402 10.418 0.050 1.789 17.511 0.10 36321. 0.5013
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4.70 0.1909 0.3495 0.1087 0.0593 0.014 0.447 0.396 10.578 0.051 1.760 16.965 0.10 36374. 0.4816
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5.48 0.2227 0.3949 0.1067 0.0601 0.014 0.453 0.388 10.721 0.051 1.727 16.428 0.10 36433. 0.4621
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6.27 0.2545 0.4369 0.1044 0.0608 0.015 0.458 0.380 10.840 0.052 1.691 15.904 0.10 36496. 0.4425
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7.05 0.2863 0.4757 0.1019 0.0613 0.015 0.462 0.371 10.930 0.052 1.650 15.392 0.10 36564. 0.4231
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7.83 0.3181 0.5114 0.0991 0.0616 0.015 0.464 0.361 10.985 0.052 1.605 14.894 0.10 36637. 0.4038
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8.62 0.3499 0.5443 0.0960 0.0617 0.015 0.465 0.349 11.000 0.053 1.555 14.410 0.10 36716. 0.3845
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9.40 0.3818 0.5744 0.0926 0.0615 0.015 0.464 0.337 10.969 0.052 1.500 13.940 0.10 36800. 0.3653
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10.18 0.4136 0.6018 0.0889 0.0611 0.015 0.460 0.324 10.887 0.052 1.439 13.482 0.10 36889. 0.3462
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10.97 0.4454 0.6266 0.0849 0.0603 0.014 0.454 0.309 10.750 0.051 1.374 13.035 0.10 36983. 0.3270
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11.75 0.4772 0.6487 0.0805 0.0592 0.014 0.446 0.293 10.554 0.050 1.304 12.595 0.10 37083. 0.3078
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12.53 0.5090 0.6680 0.0758 0.0578 0.014 0.435 0.276 10.296 0.049 1.228 12.159 0.10 37188. 0.2883
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13.32 0.5408 0.6843 0.0708 0.0560 0.013 0.421 0.258 9.973 0.048 1.147 11.723 0.10 37298. 0.2686
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14.10 0.5726 0.6973 0.0655 0.0538 0.013 0.405 0.239 9.590 0.046 1.061 11.282 0.10 37413. 0.2487
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14.88 0.6044 0.7065 0.0600 0.0513 0.012 0.387 0.218 9.151 0.044 0.972 10.829 0.11 37533. 0.2285
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15.67 0.6363 0.7112 0.0543 0.0486 0.012 0.366 0.198 8.661 0.041 0.880 10.356 0.11 37659. 0.2079
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16.45 0.6681 0.7104 0.0485 0.0456 0.011 0.343 0.176 8.123 0.039 0.785 9.852 0.11 37789. 0.1868
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17.23 0.6999 0.7029 0.0425 0.0423 0.010 0.319 0.155 7.541 0.036 0.688 9.305 0.11 37924. 0.1652
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18.02 0.7317 0.6867 0.0364 0.0388 0.009 0.292 0.133 6.917 0.033 0.590 8.695 0.11 38065. 0.1429
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18.80 0.7635 0.6591 0.0303 0.0351 0.008 0.264 0.110 6.255 0.030 0.491 7.997 0.11 38210. 0.1199
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19.58 0.7953 0.6155 0.0241 0.0312 0.007 0.235 0.088 5.559 0.027 0.391 7.169 0.11 38360. 0.0959
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20.36 0.8271 0.5486 0.0180 0.0271 0.006 0.204 0.065 4.834 0.023 0.291 6.145 0.11 38515. 0.0710
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21.15 0.8589 0.4455 0.0119 0.0229 0.005 0.173 0.043 4.083 0.019 0.192 4.805 0.11 38675. 0.0451
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21.93 0.8908 0.2812 0.0059 0.0186 0.004 0.140 0.021 3.314 0.016 0.095 2.925 0.11 38840. 0.0193
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22.71 0.9226 -0.0004 0.0000 0.0142 0.003 0.107 0.000 2.531 0.012 0.000 -0.004 0.11 39009. 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 0.1171 0.0514 0.041 0.871 0.960 30.904 0.098 4.268 14.084 0.15 54177. 0.6227
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1.18 0.0319 0.0707 0.1162 0.0524 0.042 0.889 0.952 31.543 0.100 4.232 13.682 0.15 54226. 0.6024
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2.36 0.0638 0.1371 0.1150 0.0535 0.043 0.907 0.942 32.191 0.102 4.192 13.279 0.15 54280. 0.5818
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3.53 0.0957 0.1994 0.1138 0.0546 0.044 0.925 0.932 32.837 0.105 4.146 12.875 0.15 54341. 0.5611
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4.71 0.1276 0.2576 0.1124 0.0556 0.045 0.943 0.921 33.471 0.107 4.094 12.474 0.15 54408. 0.5402
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5.89 0.1595 0.3118 0.1108 0.0566 0.046 0.960 0.907 34.078 0.108 4.036 12.078 0.15 54482. 0.5193
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7.07 0.1914 0.3621 0.1090 0.0576 0.046 0.976 0.893 34.642 0.110 3.971 11.688 0.15 54562. 0.4984
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8.24 0.2232 0.4087 0.1070 0.0584 0.047 0.990 0.876 35.147 0.112 3.897 11.307 0.16 54650. 0.4777
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9.42 0.2551 0.4517 0.1047 0.0591 0.048 1.002 0.858 35.573 0.113 3.815 10.935 0.16 54745. 0.4571
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10.60 0.2870 0.4914 0.1022 0.0597 0.048 1.011 0.837 35.902 0.114 3.723 10.574 0.16 54848. 0.4366
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11.78 0.3189 0.5279 0.0994 0.0600 0.048 1.017 0.814 36.112 0.115 3.621 10.224 0.16 54958. 0.4163
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12.96 0.3508 0.5615 0.0963 0.0602 0.049 1.019 0.789 36.185 0.115 3.508 9.885 0.16 55077. 0.3962
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14.13 0.3827 0.5922 0.0929 0.0600 0.048 1.017 0.761 36.100 0.115 3.384 9.558 0.16 55203. 0.3763
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15.31 0.4146 0.6203 0.0891 0.0596 0.048 1.010 0.730 35.840 0.114 3.248 9.240 0.16 55337. 0.3564
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16.49 0.4465 0.6457 0.0851 0.0588 0.047 0.997 0.697 35.391 0.113 3.100 8.932 0.16 55479. 0.3366
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17.67 0.4784 0.6685 0.0807 0.0577 0.047 0.979 0.661 34.739 0.111 2.940 8.631 0.16 55630. 0.3167
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18.85 0.5103 0.6886 0.0760 0.0563 0.045 0.954 0.622 33.870 0.108 2.768 8.334 0.16 55788. 0.2968
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20.02 0.5422 0.7058 0.0709 0.0545 0.044 0.924 0.581 32.779 0.104 2.585 8.041 0.16 55954. 0.2767
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21.20 0.5741 0.7200 0.0656 0.0523 0.042 0.887 0.538 31.479 0.100 2.391 7.746 0.16 56127. 0.2563
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22.38 0.6060 0.7305 0.0601 0.0498 0.040 0.845 0.492 29.984 0.095 2.189 7.446 0.16 56309. 0.2358
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23.56 0.6378 0.7370 0.0544 0.0471 0.038 0.798 0.445 28.307 0.090 1.981 7.136 0.16 56498. 0.2149
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24.73 0.6697 0.7383 0.0485 0.0440 0.035 0.746 0.397 26.462 0.084 1.767 6.809 0.16 56694. 0.1937
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25.91 0.7016 0.7334 0.0425 0.0407 0.033 0.689 0.348 24.460 0.078 1.549 6.456 0.16 56898. 0.1719
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27.09 0.7335 0.7203 0.0364 0.0371 0.030 0.629 0.298 22.310 0.071 1.327 6.065 0.16 57109. 0.1495
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28.27 0.7654 0.6962 0.0303 0.0333 0.027 0.564 0.248 20.026 0.064 1.103 5.618 0.16 57328. 0.1263
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29.45 0.7973 0.6565 0.0241 0.0293 0.024 0.496 0.198 17.620 0.056 0.879 5.086 0.16 57555. 0.1020
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30.62 0.8292 0.5933 0.0180 0.0251 0.020 0.426 0.147 15.107 0.048 0.655 4.419 0.16 57788. 0.0765
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31.80 0.8611 0.4918 0.0119 0.0208 0.017 0.352 0.097 12.506 0.040 0.433 3.528 0.16 58029. 0.0497
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32.98 0.8930 0.3209 0.0059 0.0164 0.013 0.277 0.048 9.836 0.031 0.214 2.220 0.16 58277. 0.0220
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34.16 0.9249 0.0018 0.0000 0.0118 0.010 0.201 0.000 7.121 0.023 0.001 0.012 0.16 58532. 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 0.1174 0.0503 0.096 1.515 1.710 71.674 0.171 7.604 10.819 0.21 72234. 0.6385
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1.57 0.0320 0.0724 0.1164 0.0513 0.098 1.547 1.695 73.216 0.175 7.541 10.503 0.21 72300. 0.6172
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3.15 0.0639 0.1405 0.1153 0.0524 0.100 1.580 1.679 74.782 0.179 7.469 10.185 0.21 72373. 0.5957
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4.72 0.0959 0.2042 0.1141 0.0535 0.102 1.613 1.661 76.348 0.182 7.389 9.868 0.21 72454. 0.5741
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6.29 0.1278 0.2636 0.1127 0.0546 0.104 1.646 1.641 77.886 0.186 7.297 9.554 0.21 72544. 0.5524
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7.87 0.1598 0.3188 0.1111 0.0557 0.106 1.677 1.617 79.361 0.189 7.194 9.244 0.21 72642. 0.5306
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9.44 0.1917 0.3700 0.1093 0.0566 0.108 1.706 1.591 80.737 0.193 7.078 8.940 0.21 72750. 0.5090
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11.01 0.2237 0.4173 0.1073 0.0575 0.110 1.732 1.562 81.972 0.196 6.948 8.643 0.21 72867. 0.4875
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12.59 0.2556 0.4610 0.1050 0.0582 0.111 1.754 1.529 83.021 0.198 6.801 8.354 0.21 72995. 0.4662
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14.16 0.2876 0.5012 0.1025 0.0588 0.112 1.772 1.492 83.837 0.200 6.638 8.073 0.21 73132. 0.4451
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15.73 0.3195 0.5382 0.0997 0.0592 0.113 1.783 1.451 84.371 0.201 6.456 7.803 0.21 73280. 0.4243
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17.31 0.3515 0.5722 0.0966 0.0593 0.113 1.787 1.406 84.574 0.202 6.254 7.541 0.21 73438. 0.4036
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18.88 0.3834 0.6033 0.0931 0.0592 0.113 1.783 1.356 84.401 0.201 6.033 7.289 0.21 73607. 0.3831
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20.45 0.4154 0.6317 0.0894 0.0588 0.112 1.771 1.302 83.807 0.200 5.790 7.045 0.21 73787. 0.3628
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22.03 0.4473 0.6576 0.0853 0.0580 0.111 1.749 1.242 82.758 0.198 5.526 6.809 0.21 73977. 0.3426
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23.60 0.4793 0.6808 0.0809 0.0570 0.109 1.716 1.178 81.220 0.194 5.241 6.580 0.21 74178. 0.3224
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25.17 0.5112 0.7014 0.0762 0.0555 0.106 1.673 1.109 79.158 0.189 4.934 6.356 0.21 74390. 0.3021
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26.75 0.5432 0.7193 0.0711 0.0537 0.103 1.618 1.035 76.560 0.183 4.606 6.134 0.21 74612. 0.2817
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28.32 0.5751 0.7342 0.0658 0.0515 0.099 1.552 0.958 73.455 0.175 4.260 5.913 0.21 74844. 0.2612
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29.89 0.6071 0.7457 0.0602 0.0490 0.094 1.477 0.877 69.877 0.167 3.899 5.690 0.21 75087. 0.2405
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31.47 0.6390 0.7533 0.0544 0.0462 0.088 1.392 0.793 65.858 0.157 3.527 5.461 0.21 75339. 0.2195
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33.04 0.6710 0.7561 0.0485 0.0431 0.082 1.298 0.707 61.427 0.147 3.145 5.220 0.21 75602. 0.1981
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34.61 0.7029 0.7530 0.0425 0.0397 0.076 1.196 0.619 56.610 0.135 2.755 4.962 0.21 75875. 0.1763
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36.19 0.7349 0.7421 0.0364 0.0361 0.069 1.087 0.530 51.433 0.123 2.359 4.678 0.21 76158. 0.1538
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37.76 0.7668 0.7206 0.0303 0.0322 0.062 0.970 0.441 45.926 0.110 1.960 4.353 0.21 76451. 0.1304
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39.33 0.7988 0.6838 0.0241 0.0281 0.054 0.848 0.351 40.120 0.096 1.560 3.965 0.21 76754. 0.1060
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40.91 0.8307 0.6235 0.0179 0.0239 0.046 0.720 0.261 34.053 0.081 1.161 3.477 0.21 77066. 0.0802
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42.48 0.8627 0.5237 0.0118 0.0195 0.037 0.587 0.172 27.767 0.066 0.766 2.812 0.21 77388. 0.0527
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44.05 0.8946 0.3483 0.0058 0.0149 0.029 0.450 0.085 21.316 0.051 0.377 1.803 0.21 77720. 0.0237
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45.63 0.9266 -0.0029 0.0000 0.0103 0.020 0.312 0.000 14.755 0.035 -0.002 -0.015 0.22 78061. 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 0.1177 0.0496 0.185 2.334 2.677 138.082 0.264 11.909 8.794 0.26 90291. 0.6495
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1.97 0.0320 0.0736 0.1167 0.0507 0.189 2.386 2.655 141.137 0.270 11.811 8.534 0.26 90373. 0.6276
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3.94 0.0640 0.1428 0.1156 0.0518 0.193 2.438 2.631 144.244 0.275 11.701 8.272 0.26 90465. 0.6055
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5.91 0.0959 0.2074 0.1144 0.0529 0.198 2.491 2.602 147.355 0.281 11.576 8.011 0.26 90566. 0.5833
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7.87 0.1279 0.2676 0.1130 0.0540 0.202 2.543 2.571 150.412 0.287 11.434 7.752 0.26 90678. 0.5610
|
|
9.84 0.1599 0.3235 0.1114 0.0551 0.206 2.592 2.535 153.351 0.293 11.274 7.497 0.26 90802. 0.5387
|
|
11.81 0.1919 0.3753 0.1096 0.0560 0.209 2.639 2.494 156.098 0.298 11.094 7.247 0.26 90937. 0.5166
|
|
13.78 0.2239 0.4231 0.1076 0.0569 0.213 2.681 2.448 158.570 0.303 10.890 7.003 0.26 91083. 0.4946
|
|
15.75 0.2559 0.4672 0.1053 0.0577 0.215 2.716 2.397 160.679 0.307 10.662 6.766 0.26 91243. 0.4728
|
|
17.72 0.2878 0.5078 0.1028 0.0583 0.218 2.744 2.340 162.331 0.310 10.407 6.537 0.26 91415. 0.4513
|
|
19.69 0.3198 0.5451 0.1000 0.0587 0.219 2.763 2.276 163.429 0.312 10.122 6.316 0.26 91600. 0.4301
|
|
21.65 0.3518 0.5794 0.0969 0.0588 0.220 2.770 2.205 163.876 0.313 9.808 6.103 0.26 91799. 0.4090
|
|
23.62 0.3838 0.6108 0.0935 0.0587 0.219 2.765 2.127 163.579 0.312 9.461 5.898 0.26 92010. 0.3882
|
|
25.59 0.4158 0.6395 0.0897 0.0583 0.218 2.746 2.042 162.454 0.310 9.081 5.700 0.26 92235. 0.3676
|
|
27.56 0.4477 0.6656 0.0856 0.0576 0.215 2.712 1.949 160.426 0.306 8.667 5.509 0.26 92474. 0.3471
|
|
29.53 0.4797 0.6892 0.0812 0.0565 0.211 2.661 1.848 157.432 0.301 8.220 5.324 0.26 92725. 0.3267
|
|
31.50 0.5117 0.7102 0.0764 0.0551 0.206 2.593 1.740 153.401 0.293 7.737 5.143 0.26 92990. 0.3062
|
|
33.47 0.5437 0.7286 0.0714 0.0533 0.199 2.507 1.624 148.307 0.283 7.223 4.966 0.26 93268. 0.2856
|
|
35.43 0.5757 0.7441 0.0660 0.0511 0.191 2.404 1.502 142.204 0.272 6.680 4.790 0.26 93559. 0.2649
|
|
37.40 0.6077 0.7564 0.0604 0.0485 0.181 2.285 1.375 135.160 0.258 6.114 4.613 0.26 93863. 0.2441
|
|
39.37 0.6396 0.7649 0.0546 0.0457 0.171 2.151 1.243 127.236 0.243 5.529 4.431 0.26 94180. 0.2230
|
|
41.34 0.6716 0.7689 0.0487 0.0425 0.159 2.003 1.108 118.488 0.226 4.930 4.242 0.26 94509. 0.2016
|
|
43.31 0.7036 0.7672 0.0427 0.0391 0.146 1.842 0.971 108.968 0.208 4.318 4.041 0.26 94851. 0.1797
|
|
45.28 0.7356 0.7580 0.0365 0.0354 0.132 1.669 0.831 98.729 0.189 3.697 3.819 0.26 95205. 0.1572
|
|
47.25 0.7676 0.7387 0.0303 0.0315 0.118 1.485 0.691 87.826 0.168 3.072 3.566 0.27 95572. 0.1338
|
|
49.21 0.7996 0.7045 0.0241 0.0274 0.102 1.290 0.549 76.325 0.146 2.444 3.265 0.27 95951. 0.1093
|
|
51.18 0.8315 0.6471 0.0180 0.0231 0.086 1.087 0.409 64.300 0.123 1.818 2.884 0.27 96343. 0.0832
|
|
53.15 0.8635 0.5495 0.0118 0.0186 0.070 0.876 0.270 51.838 0.099 1.199 2.358 0.27 96746. 0.0553
|
|
55.12 0.8955 0.3724 0.0058 0.0140 0.052 0.660 0.133 39.045 0.075 0.590 1.541 0.27 97162. 0.0253
|
|
57.09 0.9275 -0.0033 0.0000 0.0093 0.035 0.440 -0.001 26.032 0.050 -0.003 -0.013 0.27 97588. 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 0.1180 0.0492 0.317 3.332 3.865 236.542 0.376 17.193 7.412 0.31 108347. 0.6577
|
|
2.36 0.0320 0.0745 0.1170 0.0503 0.324 3.407 3.834 241.887 0.385 17.054 7.190 0.31 108446. 0.6354
|
|
4.73 0.0640 0.1443 0.1159 0.0514 0.332 3.484 3.799 247.329 0.394 16.897 6.967 0.31 108556. 0.6129
|
|
7.09 0.0960 0.2096 0.1147 0.0525 0.339 3.561 3.759 252.784 0.402 16.720 6.745 0.31 108677. 0.5902
|
|
9.45 0.1280 0.2704 0.1133 0.0536 0.346 3.637 3.714 258.152 0.411 16.518 6.525 0.31 108812. 0.5675
|
|
11.82 0.1600 0.3268 0.1118 0.0547 0.353 3.709 3.662 263.320 0.419 16.289 6.308 0.31 108960. 0.5449
|
|
14.18 0.1920 0.3789 0.1100 0.0557 0.360 3.778 3.604 268.158 0.427 16.031 6.096 0.31 109122. 0.5224
|
|
16.54 0.2240 0.4271 0.1080 0.0566 0.365 3.839 3.539 272.524 0.434 15.740 5.889 0.31 109298. 0.5000
|
|
18.91 0.2559 0.4715 0.1057 0.0574 0.370 3.892 3.465 276.261 0.440 15.412 5.689 0.31 109490. 0.4780
|
|
21.27 0.2879 0.5124 0.1032 0.0580 0.374 3.933 3.383 279.206 0.444 15.046 5.495 0.31 109697. 0.4562
|
|
23.63 0.3199 0.5499 0.1004 0.0584 0.377 3.961 3.291 281.187 0.448 14.637 5.308 0.31 109919. 0.4346
|
|
25.99 0.3519 0.5844 0.0973 0.0586 0.378 3.973 3.189 282.035 0.449 14.184 5.128 0.31 110157. 0.4133
|
|
28.36 0.3839 0.6161 0.0939 0.0585 0.378 3.967 3.076 281.587 0.448 13.684 4.955 0.31 110412. 0.3923
|
|
30.72 0.4159 0.6450 0.0901 0.0581 0.375 3.940 2.953 279.694 0.445 13.136 4.789 0.31 110682. 0.3715
|
|
33.08 0.4479 0.6714 0.0860 0.0574 0.370 3.891 2.819 276.224 0.440 12.539 4.629 0.31 110968. 0.3508
|
|
35.45 0.4799 0.6952 0.0816 0.0563 0.364 3.819 2.674 271.064 0.431 11.893 4.474 0.31 111271. 0.3302
|
|
37.81 0.5119 0.7166 0.0768 0.0549 0.354 3.720 2.517 264.091 0.420 11.196 4.323 0.31 111589. 0.3096
|
|
40.17 0.5439 0.7354 0.0717 0.0530 0.342 3.596 2.350 255.256 0.406 10.452 4.175 0.31 111923. 0.2889
|
|
42.54 0.5759 0.7514 0.0663 0.0508 0.328 3.446 2.173 244.649 0.389 9.667 4.029 0.31 112273. 0.2681
|
|
44.90 0.6079 0.7643 0.0607 0.0483 0.312 3.274 1.989 232.387 0.370 8.849 3.883 0.32 112638. 0.2472
|
|
47.26 0.6399 0.7736 0.0549 0.0454 0.293 3.079 1.799 218.578 0.348 8.003 3.734 0.32 113018. 0.2260
|
|
49.63 0.6719 0.7786 0.0490 0.0422 0.273 2.864 1.604 203.315 0.324 7.135 3.579 0.32 113414. 0.2046
|
|
51.99 0.7039 0.7781 0.0429 0.0388 0.250 2.630 1.405 186.691 0.297 6.250 3.414 0.32 113824. 0.1827
|
|
54.35 0.7359 0.7705 0.0367 0.0351 0.226 2.378 1.203 168.797 0.269 5.353 3.234 0.32 114250. 0.1601
|
|
56.72 0.7678 0.7531 0.0305 0.0311 0.201 2.109 1.000 149.732 0.238 4.448 3.029 0.32 114690. 0.1367
|
|
59.08 0.7998 0.7213 0.0243 0.0269 0.174 1.826 0.796 129.610 0.206 3.540 2.785 0.32 115146. 0.1121
|
|
61.44 0.8318 0.6666 0.0181 0.0226 0.146 1.529 0.592 108.562 0.173 2.635 2.475 0.32 115615. 0.0860
|
|
63.81 0.8638 0.5717 0.0119 0.0180 0.116 1.222 0.391 86.743 0.138 1.739 2.044 0.32 116100. 0.0577
|
|
66.17 0.8958 0.3947 0.0059 0.0134 0.086 0.906 0.193 64.338 0.102 0.858 1.361 0.32 116599. 0.0270
|
|
68.53 0.9278 0.0006 0.0000 0.0086 0.056 0.585 0.000 41.546 0.066 0.001 0.002 0.32 117110. 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 0.1183 0.0489 0.501 4.512 5.276 373.688 0.510 23.469 6.404 0.36 126402. 0.6640
|
|
2.76 0.0320 0.0751 0.1174 0.0500 0.513 4.616 5.235 382.281 0.522 23.284 6.211 0.36 126517. 0.6414
|
|
5.52 0.0640 0.1455 0.1163 0.0512 0.524 4.722 5.187 391.040 0.533 23.074 6.017 0.36 126645. 0.6186
|
|
8.28 0.0960 0.2113 0.1151 0.0523 0.536 4.828 5.134 399.827 0.545 22.835 5.824 0.36 126787. 0.5956
|
|
11.04 0.1281 0.2725 0.1137 0.0535 0.548 4.932 5.073 408.487 0.557 22.564 5.633 0.36 126944. 0.5726
|
|
13.79 0.1601 0.3292 0.1122 0.0545 0.559 5.033 5.004 416.835 0.569 22.256 5.445 0.36 127117. 0.5497
|
|
16.55 0.1921 0.3817 0.1104 0.0556 0.569 5.128 4.925 424.664 0.579 21.907 5.260 0.36 127306. 0.5269
|
|
19.31 0.2241 0.4302 0.1084 0.0565 0.579 5.213 4.837 431.742 0.589 21.513 5.081 0.36 127512. 0.5044
|
|
22.07 0.2561 0.4748 0.1062 0.0573 0.587 5.286 4.737 437.818 0.597 21.069 4.907 0.36 127736. 0.4821
|
|
24.83 0.2881 0.5159 0.1037 0.0579 0.594 5.345 4.625 442.627 0.604 20.572 4.739 0.36 127978. 0.4600
|
|
27.59 0.3201 0.5536 0.1009 0.0583 0.598 5.384 4.500 445.894 0.608 20.016 4.577 0.36 128238. 0.4383
|
|
30.35 0.3522 0.5883 0.0978 0.0585 0.600 5.402 4.361 447.344 0.610 19.399 4.422 0.36 128516. 0.4168
|
|
33.11 0.3842 0.6201 0.0944 0.0585 0.599 5.394 4.208 446.714 0.609 18.718 4.273 0.36 128813. 0.3956
|
|
35.86 0.4162 0.6493 0.0906 0.0581 0.595 5.358 4.040 443.761 0.605 17.970 4.129 0.36 129129. 0.3746
|
|
38.62 0.4482 0.6758 0.0865 0.0573 0.588 5.292 3.857 438.274 0.598 17.155 3.991 0.36 129464. 0.3538
|
|
41.38 0.4802 0.6999 0.0820 0.0563 0.577 5.193 3.658 430.067 0.587 16.272 3.858 0.37 129817. 0.3331
|
|
44.14 0.5122 0.7216 0.0772 0.0548 0.562 5.059 3.444 418.943 0.572 15.320 3.729 0.37 130189. 0.3124
|
|
46.90 0.5442 0.7407 0.0721 0.0530 0.543 4.888 3.215 404.817 0.552 14.302 3.603 0.37 130580. 0.2916
|
|
49.66 0.5762 0.7571 0.0667 0.0507 0.520 4.683 2.974 387.831 0.529 13.228 3.478 0.37 130988. 0.2707
|
|
52.42 0.6083 0.7706 0.0610 0.0482 0.494 4.446 2.722 368.173 0.502 12.107 3.353 0.37 131415. 0.2497
|
|
55.18 0.6403 0.7805 0.0552 0.0453 0.464 4.178 2.462 346.011 0.472 10.950 3.227 0.37 131860. 0.2285
|
|
57.93 0.6723 0.7863 0.0492 0.0421 0.431 3.882 2.194 321.499 0.439 9.761 3.096 0.37 132322. 0.2070
|
|
60.69 0.7043 0.7869 0.0431 0.0386 0.395 3.559 1.922 294.783 0.402 8.549 2.957 0.37 132801. 0.1850
|
|
63.45 0.7363 0.7805 0.0369 0.0348 0.357 3.212 1.646 266.011 0.363 7.320 2.806 0.37 133299. 0.1625
|
|
66.21 0.7683 0.7646 0.0306 0.0308 0.316 2.842 1.367 235.343 0.321 6.080 2.634 0.37 133813. 0.1390
|
|
68.97 0.8003 0.7347 0.0244 0.0266 0.272 2.451 1.087 202.961 0.277 4.836 2.430 0.37 134345. 0.1144
|
|
71.73 0.8324 0.6821 0.0181 0.0221 0.227 2.042 0.809 169.081 0.231 3.597 2.169 0.37 134894. 0.0880
|
|
74.49 0.8644 0.5891 0.0119 0.0175 0.180 1.617 0.533 133.954 0.183 2.370 1.804 0.37 135460. 0.0594
|
|
77.25 0.8964 0.4110 0.0059 0.0128 0.131 1.182 0.262 97.883 0.134 1.165 1.214 0.38 136043. 0.0280
|
|
80.00 0.9284 -0.0052 0.0000 0.0080 0.082 0.739 -0.002 61.187 0.083 -0.009 -0.015 0.38 136640. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 8000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1187 0.0488 0.746 5.879 6.914 556.445 0.664 30.753 5.636 0.41 144454. 0.6688
|
|
3.15 0.0320 0.0755 0.1178 0.0499 0.764 6.016 6.861 569.423 0.680 30.517 5.465 0.41 144586. 0.6461
|
|
6.31 0.0640 0.1463 0.1167 0.0511 0.781 6.156 6.800 582.668 0.696 30.248 5.294 0.41 144732. 0.6231
|
|
9.46 0.0960 0.2124 0.1156 0.0522 0.799 6.297 6.731 595.972 0.711 29.942 5.123 0.41 144895. 0.5999
|
|
12.61 0.1280 0.2739 0.1142 0.0534 0.817 6.435 6.653 609.099 0.727 29.593 4.954 0.41 145074. 0.5768
|
|
15.76 0.1601 0.3309 0.1127 0.0545 0.834 6.569 6.564 621.773 0.742 29.196 4.788 0.41 145272. 0.5537
|
|
18.92 0.1921 0.3836 0.1109 0.0555 0.850 6.695 6.463 633.679 0.756 28.745 4.626 0.41 145488. 0.5308
|
|
22.07 0.2241 0.4322 0.1090 0.0565 0.864 6.809 6.348 644.466 0.769 28.235 4.468 0.41 145724. 0.5080
|
|
25.22 0.2561 0.4770 0.1067 0.0573 0.877 6.907 6.218 653.754 0.780 27.659 4.314 0.41 145979. 0.4856
|
|
28.37 0.2881 0.5182 0.1043 0.0580 0.887 6.985 6.073 661.142 0.789 27.013 4.166 0.41 146256. 0.4634
|
|
31.53 0.3201 0.5561 0.1015 0.0584 0.893 7.039 5.910 666.211 0.795 26.289 4.024 0.41 146553. 0.4415
|
|
34.68 0.3521 0.5910 0.0984 0.0586 0.897 7.063 5.730 668.546 0.798 25.485 3.887 0.42 146871. 0.4200
|
|
37.83 0.3841 0.6229 0.0949 0.0585 0.895 7.055 5.530 667.745 0.797 24.596 3.756 0.42 147211. 0.3987
|
|
40.98 0.4161 0.6522 0.0912 0.0582 0.890 7.009 5.310 663.438 0.792 23.619 3.630 0.42 147573. 0.3776
|
|
44.14 0.4481 0.6790 0.0870 0.0574 0.879 6.924 5.070 655.306 0.782 22.552 3.509 0.42 147955. 0.3567
|
|
47.29 0.4802 0.7033 0.0826 0.0564 0.862 6.794 4.810 643.064 0.768 21.395 3.393 0.42 148359. 0.3358
|
|
50.44 0.5122 0.7252 0.0778 0.0549 0.840 6.618 4.530 626.414 0.748 20.147 3.280 0.42 148785. 0.3151
|
|
53.59 0.5442 0.7447 0.0726 0.0531 0.812 6.394 4.229 605.219 0.722 18.812 3.170 0.42 149231. 0.2942
|
|
56.75 0.5762 0.7615 0.0672 0.0508 0.777 6.125 3.912 579.686 0.692 17.402 3.061 0.42 149698. 0.2733
|
|
59.90 0.6082 0.7755 0.0615 0.0482 0.738 5.812 3.582 550.094 0.657 15.931 2.953 0.42 150186. 0.2523
|
|
63.05 0.6402 0.7861 0.0556 0.0453 0.693 5.459 3.240 516.698 0.617 14.410 2.844 0.42 150694. 0.2310
|
|
66.20 0.6722 0.7926 0.0496 0.0421 0.643 5.069 2.888 479.731 0.573 12.848 2.731 0.42 151223. 0.2095
|
|
69.36 0.7042 0.7941 0.0434 0.0385 0.589 4.643 2.530 439.412 0.525 11.255 2.612 0.42 151771. 0.1875
|
|
72.51 0.7362 0.7890 0.0372 0.0347 0.531 4.183 2.167 395.966 0.473 9.638 2.482 0.42 152339. 0.1649
|
|
75.66 0.7682 0.7747 0.0309 0.0306 0.469 3.694 1.800 349.635 0.417 8.008 2.335 0.42 152927. 0.1414
|
|
78.81 0.8003 0.7467 0.0246 0.0264 0.403 3.177 1.433 300.698 0.359 6.372 2.161 0.43 153535. 0.1167
|
|
81.97 0.8323 0.6965 0.0183 0.0219 0.335 2.636 1.066 249.477 0.298 4.742 1.938 0.43 154162. 0.0903
|
|
85.12 0.8643 0.6062 0.0121 0.0172 0.263 2.075 0.703 196.360 0.234 3.128 1.625 0.43 154809. 0.0615
|
|
88.27 0.8963 0.4295 0.0060 0.0124 0.190 1.498 0.347 141.806 0.169 1.543 1.110 0.43 155475. 0.0295
|
|
91.42 0.9283 -0.0003 0.0000 0.0076 0.116 0.912 0.000 86.303 0.103 -0.001 -0.001 0.43 156157. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 9000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1191 0.0488 1.062 7.439 8.782 792.111 0.840 39.063 5.029 0.46 162505. 0.6726
|
|
3.55 0.0320 0.0758 0.1182 0.0499 1.087 7.615 8.717 810.825 0.860 38.772 4.876 0.46 162653. 0.6498
|
|
7.09 0.0640 0.1469 0.1172 0.0511 1.113 7.794 8.642 829.946 0.881 38.440 4.723 0.46 162817. 0.6267
|
|
10.64 0.0960 0.2132 0.1161 0.0523 1.139 7.975 8.557 849.178 0.901 38.061 4.570 0.46 163000. 0.6034
|
|
14.19 0.1281 0.2749 0.1147 0.0535 1.164 8.153 8.459 868.180 0.921 37.627 4.419 0.46 163202. 0.5802
|
|
17.74 0.1601 0.3321 0.1132 0.0546 1.189 8.326 8.348 886.556 0.941 37.133 4.271 0.46 163425. 0.5570
|
|
21.28 0.1921 0.3849 0.1115 0.0556 1.212 8.488 8.222 903.846 0.959 36.570 4.126 0.46 163668. 0.5340
|
|
24.83 0.2241 0.4337 0.1096 0.0566 1.233 8.636 8.078 919.544 0.976 35.930 3.984 0.47 163933. 0.5111
|
|
28.38 0.2561 0.4786 0.1074 0.0574 1.251 8.763 7.915 933.100 0.990 35.207 3.848 0.47 164221. 0.4886
|
|
31.92 0.2881 0.5200 0.1049 0.0581 1.266 8.865 7.732 943.929 1.002 34.393 3.715 0.47 164533. 0.4663
|
|
35.47 0.3201 0.5580 0.1021 0.0586 1.276 8.935 7.527 951.427 1.009 33.481 3.588 0.47 164867. 0.4444
|
|
39.02 0.3522 0.5930 0.0990 0.0588 1.281 8.969 7.299 954.989 1.013 32.465 3.467 0.47 165226. 0.4227
|
|
42.57 0.3842 0.6251 0.0956 0.0587 1.279 8.960 7.046 954.031 1.012 31.339 3.350 0.47 165609. 0.4013
|
|
46.11 0.4162 0.6545 0.0918 0.0584 1.271 8.903 6.767 948.016 1.006 30.101 3.238 0.47 166016. 0.3802
|
|
49.66 0.4482 0.6815 0.0877 0.0577 1.256 8.795 6.463 936.477 0.994 28.748 3.130 0.47 166447. 0.3592
|
|
53.21 0.4802 0.7060 0.0832 0.0566 1.232 8.631 6.133 919.003 0.975 27.278 3.027 0.47 166902. 0.3383
|
|
56.75 0.5122 0.7282 0.0783 0.0551 1.200 8.407 5.776 895.165 0.950 25.692 2.927 0.47 167381. 0.3175
|
|
60.30 0.5443 0.7479 0.0732 0.0532 1.160 8.121 5.394 864.752 0.918 23.992 2.829 0.47 167884. 0.2966
|
|
63.85 0.5763 0.7651 0.0677 0.0510 1.110 7.777 4.990 828.051 0.879 22.197 2.733 0.47 168410. 0.2756
|
|
67.39 0.6083 0.7795 0.0620 0.0484 1.053 7.377 4.569 785.463 0.833 20.322 2.638 0.47 168959. 0.2545
|
|
70.94 0.6403 0.7907 0.0561 0.0454 0.989 6.925 4.133 737.359 0.782 18.383 2.542 0.47 169531. 0.2333
|
|
74.49 0.6723 0.7979 0.0500 0.0421 0.917 6.424 3.685 684.074 0.726 16.391 2.443 0.47 170126. 0.2117
|
|
78.04 0.7043 0.8002 0.0438 0.0385 0.839 5.878 3.228 625.925 0.664 14.358 2.339 0.48 170743. 0.1897
|
|
81.58 0.7363 0.7962 0.0375 0.0347 0.755 5.290 2.764 563.237 0.598 12.296 2.226 0.48 171383. 0.1671
|
|
85.13 0.7684 0.7832 0.0311 0.0306 0.666 4.662 2.296 496.364 0.527 10.215 2.098 0.48 172045. 0.1435
|
|
88.68 0.8004 0.7568 0.0248 0.0262 0.571 3.998 1.827 425.706 0.452 8.127 1.947 0.48 172729. 0.1188
|
|
92.22 0.8324 0.7086 0.0184 0.0217 0.472 3.303 1.359 351.735 0.373 6.046 1.753 0.48 173435. 0.0922
|
|
95.77 0.8644 0.6204 0.0122 0.0169 0.369 2.583 0.896 275.014 0.292 3.985 1.478 0.48 174163. 0.0631
|
|
99.32 0.8964 0.4439 0.0060 0.0121 0.263 1.843 0.441 196.214 0.208 1.962 1.019 0.48 174913. 0.0306
|
|
102.87 0.9284 -0.0038 0.0000 0.0071 0.156 1.090 -0.002 116.041 0.123 -0.010 -0.008 0.48 175680. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 10000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1196 0.0489 1.460 9.200 10.886 1088.447 1.039 48.421 4.536 0.52 180554. 0.6756
|
|
3.94 0.0320 0.0760 0.1187 0.0500 1.495 9.420 10.808 1114.460 1.064 48.073 4.399 0.52 180717. 0.6527
|
|
7.88 0.0640 0.1472 0.1178 0.0512 1.530 9.645 10.718 1141.078 1.090 47.674 4.260 0.52 180900. 0.6295
|
|
11.82 0.0960 0.2137 0.1166 0.0524 1.566 9.871 10.616 1167.889 1.115 47.218 4.123 0.52 181103. 0.6063
|
|
15.76 0.1280 0.2755 0.1153 0.0536 1.602 10.096 10.498 1194.424 1.141 46.695 3.986 0.52 181328. 0.5830
|
|
19.70 0.1601 0.3328 0.1139 0.0548 1.636 10.313 10.363 1220.125 1.165 46.096 3.852 0.52 181575. 0.5598
|
|
23.65 0.1921 0.3858 0.1122 0.0558 1.669 10.518 10.210 1244.353 1.188 45.412 3.721 0.52 181845. 0.5367
|
|
27.59 0.2241 0.4346 0.1102 0.0568 1.698 10.704 10.034 1266.401 1.209 44.633 3.594 0.52 182140. 0.5138
|
|
31.53 0.2561 0.4797 0.1081 0.0577 1.724 10.865 9.836 1285.497 1.228 43.749 3.470 0.52 182460. 0.4912
|
|
35.47 0.2881 0.5211 0.1056 0.0584 1.744 10.995 9.611 1300.823 1.242 42.751 3.351 0.52 182806. 0.4689
|
|
39.41 0.3201 0.5592 0.1028 0.0589 1.759 11.085 9.359 1311.534 1.252 41.631 3.237 0.52 183179. 0.4469
|
|
43.35 0.3521 0.5943 0.0997 0.0591 1.766 11.130 9.078 1316.779 1.257 40.379 3.127 0.52 183578. 0.4253
|
|
47.29 0.3841 0.6265 0.0963 0.0591 1.764 11.121 8.766 1315.743 1.256 38.991 3.022 0.52 184003. 0.4038
|
|
51.23 0.4162 0.6561 0.0925 0.0587 1.754 11.053 8.422 1307.671 1.249 37.461 2.921 0.52 184456. 0.3826
|
|
55.17 0.4482 0.6832 0.0884 0.0580 1.732 10.920 8.045 1291.906 1.234 35.786 2.825 0.52 184935. 0.3616
|
|
59.11 0.4802 0.7079 0.0839 0.0569 1.700 10.716 7.636 1267.876 1.211 33.966 2.732 0.52 185441. 0.3407
|
|
63.05 0.5122 0.7303 0.0790 0.0554 1.656 10.438 7.194 1234.984 1.179 31.998 2.642 0.52 185974. 0.3198
|
|
67.00 0.5442 0.7504 0.0738 0.0535 1.600 10.083 6.719 1192.917 1.139 29.888 2.555 0.52 186533. 0.2989
|
|
70.94 0.5762 0.7679 0.0683 0.0513 1.532 9.653 6.218 1142.057 1.091 27.657 2.469 0.52 187118. 0.2779
|
|
74.88 0.6082 0.7828 0.0626 0.0486 1.452 9.153 5.694 1082.964 1.034 25.325 2.385 0.53 187729. 0.2568
|
|
78.82 0.6402 0.7944 0.0566 0.0456 1.363 8.589 5.151 1016.153 0.970 22.911 2.299 0.53 188365. 0.2355
|
|
82.76 0.6723 0.8023 0.0505 0.0423 1.263 7.963 4.593 942.093 0.900 20.431 2.211 0.53 189026. 0.2139
|
|
86.70 0.7043 0.8055 0.0442 0.0387 1.155 7.279 4.024 861.230 0.822 17.899 2.119 0.53 189713. 0.1919
|
|
90.64 0.7363 0.8025 0.0379 0.0347 1.038 6.542 3.446 774.016 0.739 15.329 2.019 0.53 190424. 0.1692
|
|
94.58 0.7683 0.7907 0.0315 0.0306 0.913 5.756 2.863 680.944 0.650 12.734 1.907 0.53 191159. 0.1456
|
|
98.52 0.8003 0.7659 0.0250 0.0261 0.781 4.924 2.278 582.576 0.556 10.131 1.773 0.53 191919. 0.1208
|
|
102.46 0.8323 0.7197 0.0186 0.0215 0.643 4.053 1.694 479.572 0.458 7.535 1.602 0.53 192704. 0.0941
|
|
106.40 0.8643 0.6337 0.0123 0.0167 0.500 3.150 1.116 372.723 0.356 4.965 1.358 0.53 193513. 0.0648
|
|
110.35 0.8963 0.4579 0.0060 0.0118 0.353 2.223 0.549 262.969 0.251 2.441 0.947 0.54 194346. 0.0316
|
|
114.29 0.9284 -0.0061 0.0000 0.0068 0.203 1.279 -0.004 151.305 0.144 -0.018 -0.012 0.54 195198. 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 0.1201 0.0490 1.950 11.171 13.230 1453.793 1.262 58.849 4.128 0.57 198600. 0.6777
|
|
4.33 0.0320 0.0760 0.1193 0.0502 1.997 11.441 13.139 1488.912 1.293 58.444 4.003 0.57 198780. 0.6549
|
|
8.67 0.0640 0.1473 0.1184 0.0514 2.045 11.717 13.035 1524.907 1.324 57.979 3.877 0.57 198981. 0.6318
|
|
13.00 0.0960 0.2139 0.1173 0.0526 2.094 11.996 12.915 1561.227 1.355 57.444 3.752 0.57 199204. 0.6086
|
|
17.34 0.1280 0.2757 0.1160 0.0539 2.142 12.273 12.776 1597.234 1.387 56.828 3.628 0.57 199450. 0.5853
|
|
21.67 0.1600 0.3331 0.1146 0.0550 2.189 12.541 12.617 1632.177 1.417 56.121 3.506 0.57 199722. 0.5621
|
|
26.00 0.1920 0.3861 0.1129 0.0562 2.233 12.795 12.435 1665.189 1.446 55.309 3.387 0.57 200020. 0.5391
|
|
30.34 0.2240 0.4350 0.1110 0.0572 2.273 13.026 12.226 1695.307 1.472 54.382 3.271 0.57 200344. 0.5162
|
|
34.67 0.2560 0.4801 0.1089 0.0580 2.309 13.228 11.989 1721.478 1.494 53.326 3.159 0.57 200696. 0.4937
|
|
39.00 0.2880 0.5216 0.1064 0.0588 2.337 13.390 11.720 1742.590 1.513 52.130 3.050 0.57 201077. 0.4714
|
|
43.34 0.3200 0.5598 0.1037 0.0593 2.357 13.504 11.417 1757.489 1.526 50.783 2.946 0.57 201487. 0.4494
|
|
47.67 0.3520 0.5950 0.1006 0.0595 2.367 13.562 11.078 1765.018 1.532 49.275 2.847 0.57 201926. 0.4277
|
|
52.01 0.3840 0.6273 0.0972 0.0595 2.366 13.555 10.701 1764.062 1.531 47.598 2.751 0.57 202394. 0.4062
|
|
56.34 0.4160 0.6570 0.0934 0.0591 2.352 13.474 10.285 1753.593 1.522 45.745 2.660 0.57 202893. 0.3850
|
|
60.67 0.4481 0.6843 0.0892 0.0584 2.324 13.314 9.828 1732.715 1.504 43.715 2.573 0.57 203420. 0.3640
|
|
65.01 0.4801 0.7092 0.0847 0.0573 2.281 13.068 9.331 1700.650 1.476 41.505 2.489 0.57 203977. 0.3431
|
|
69.34 0.5121 0.7319 0.0798 0.0559 2.222 12.729 8.793 1656.598 1.438 39.112 2.408 0.57 204564. 0.3222
|
|
73.68 0.5441 0.7522 0.0746 0.0540 2.146 12.295 8.216 1600.104 1.389 36.543 2.329 0.58 205179. 0.3013
|
|
78.01 0.5761 0.7701 0.0690 0.0516 2.054 11.769 7.604 1531.657 1.330 33.824 2.252 0.58 205823. 0.2803
|
|
82.34 0.6081 0.7854 0.0632 0.0490 1.947 11.157 6.965 1452.016 1.261 30.980 2.176 0.58 206495. 0.2592
|
|
86.68 0.6401 0.7976 0.0572 0.0459 1.826 10.465 6.302 1361.883 1.182 28.033 2.099 0.58 207195. 0.2378
|
|
91.01 0.6721 0.8061 0.0510 0.0426 1.692 9.696 5.621 1261.898 1.095 25.003 2.020 0.58 207923. 0.2162
|
|
95.34 0.7041 0.8101 0.0447 0.0389 1.546 8.857 4.925 1152.663 1.001 21.907 1.938 0.58 208678. 0.1941
|
|
99.68 0.7361 0.8080 0.0383 0.0349 1.388 7.951 4.219 1034.796 0.898 18.764 1.849 0.58 209460. 0.1714
|
|
104.01 0.7681 0.7975 0.0318 0.0307 1.219 6.984 3.505 908.965 0.789 15.590 1.749 0.58 210269. 0.1478
|
|
108.35 0.8001 0.7743 0.0253 0.0262 1.041 5.962 2.789 775.934 0.674 12.404 1.630 0.59 211105. 0.1229
|
|
112.68 0.8321 0.7300 0.0188 0.0215 0.854 4.892 2.074 636.599 0.553 9.226 1.478 0.59 211968. 0.0961
|
|
117.01 0.8641 0.6463 0.0124 0.0166 0.660 3.781 1.367 492.037 0.427 6.079 1.260 0.59 212858. 0.0665
|
|
121.35 0.8961 0.4717 0.0061 0.0116 0.461 2.640 0.672 343.536 0.298 2.987 0.887 0.59 213773. 0.0328
|
|
125.68 0.9281 -0.0072 -0.0001 0.0065 0.258 1.479 -0.006 192.447 0.167 -0.025 -0.013 0.59 214710. 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 0.1207 0.0493 2.544 13.363 15.821 1897.261 1.510 70.374 3.782 0.62 216642. 0.6791
|
|
4.72 0.0320 0.0760 0.1199 0.0505 2.606 13.689 15.718 1943.536 1.547 69.915 3.668 0.62 216838. 0.6564
|
|
9.45 0.0639 0.1472 0.1190 0.0517 2.670 14.024 15.599 1991.053 1.584 69.386 3.554 0.62 217057. 0.6335
|
|
14.17 0.0959 0.2137 0.1180 0.0530 2.734 14.362 15.462 2039.098 1.623 68.774 3.439 0.62 217300. 0.6104
|
|
18.89 0.1279 0.2755 0.1168 0.0542 2.798 14.699 15.303 2086.832 1.661 68.067 3.326 0.62 217569. 0.5873
|
|
23.62 0.1599 0.3328 0.1154 0.0554 2.861 15.026 15.119 2133.260 1.698 67.250 3.215 0.62 217865. 0.5642
|
|
28.34 0.1918 0.3859 0.1137 0.0566 2.920 15.335 14.907 2177.236 1.733 66.308 3.106 0.62 218189. 0.5412
|
|
33.06 0.2238 0.4348 0.1119 0.0576 2.974 15.619 14.664 2217.479 1.765 65.227 3.000 0.62 218543. 0.5184
|
|
37.79 0.2558 0.4799 0.1098 0.0585 3.021 15.866 14.387 2252.591 1.793 63.992 2.897 0.62 218927. 0.4959
|
|
42.51 0.2878 0.5214 0.1074 0.0592 3.059 16.067 14.071 2281.084 1.815 62.587 2.798 0.62 219342. 0.4737
|
|
47.24 0.3197 0.5597 0.1046 0.0598 3.086 16.210 13.714 2301.427 1.831 61.000 2.703 0.62 219788. 0.4518
|
|
51.96 0.3517 0.5949 0.1016 0.0601 3.101 16.285 13.313 2312.078 1.840 59.217 2.612 0.62 220267. 0.4301
|
|
56.68 0.3837 0.6273 0.0982 0.0600 3.100 16.281 12.866 2311.546 1.839 57.228 2.525 0.62 220778. 0.4087
|
|
61.41 0.4157 0.6572 0.0944 0.0597 3.082 16.189 12.371 2298.465 1.829 55.027 2.441 0.62 221322. 0.3876
|
|
66.13 0.4476 0.6846 0.0902 0.0590 3.046 16.000 11.828 2271.637 1.808 52.609 2.362 0.63 221897. 0.3666
|
|
70.85 0.4796 0.7098 0.0857 0.0579 2.991 15.707 11.235 2230.035 1.775 49.972 2.285 0.63 222505. 0.3457
|
|
75.58 0.5116 0.7326 0.0808 0.0564 2.914 15.303 10.592 2172.613 1.729 47.113 2.211 0.63 223144. 0.3248
|
|
80.30 0.5436 0.7533 0.0755 0.0545 2.814 14.782 9.901 2098.717 1.670 44.040 2.140 0.63 223816. 0.3039
|
|
85.02 0.5755 0.7716 0.0700 0.0522 2.694 14.150 9.168 2008.947 1.599 40.780 2.070 0.63 224518. 0.2829
|
|
89.75 0.6075 0.7873 0.0641 0.0495 2.554 13.413 8.401 1904.303 1.515 37.367 2.001 0.63 225251. 0.2618
|
|
94.47 0.6395 0.8000 0.0580 0.0464 2.395 12.578 7.605 1785.725 1.421 33.828 1.932 0.63 226014. 0.2404
|
|
99.19 0.6715 0.8092 0.0518 0.0430 2.218 11.650 6.786 1654.059 1.316 30.185 1.861 0.63 226807. 0.2188
|
|
103.92 0.7034 0.8140 0.0454 0.0392 2.025 10.637 5.949 1510.114 1.202 26.462 1.787 0.63 227630. 0.1967
|
|
108.64 0.7354 0.8130 0.0389 0.0352 1.817 9.542 5.098 1354.705 1.078 22.678 1.707 0.64 228482. 0.1740
|
|
113.36 0.7674 0.8038 0.0323 0.0309 1.594 8.373 4.239 1188.718 0.946 18.855 1.617 0.64 229364. 0.1503
|
|
118.09 0.7994 0.7824 0.0258 0.0263 1.359 7.136 3.376 1013.159 0.806 15.016 1.511 0.64 230275. 0.1253
|
|
122.81 0.8313 0.7405 0.0192 0.0215 1.112 5.841 2.514 829.218 0.660 11.184 1.375 0.64 231215. 0.0984
|
|
127.53 0.8633 0.6598 0.0127 0.0166 0.856 4.496 1.661 638.320 0.508 7.387 1.180 0.64 232184. 0.0686
|
|
132.26 0.8953 0.4889 0.0063 0.0115 0.593 3.114 0.822 442.176 0.352 3.656 0.843 0.64 233181. 0.0345
|
|
136.98 0.9273 0.0053 0.0000 0.0063 0.325 1.709 0.005 242.610 0.193 0.021 0.009 0.65 234202. 0.0000
|
|
|
|
|
|
|
|
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 0.1213 0.0497 3.261 15.812 18.665 2431.985 1.786 83.023 3.481 0.67 234682. 0.6788
|
|
5.12 0.0320 0.0757 0.1206 0.0509 3.341 16.197 18.551 2491.166 1.830 82.516 3.378 0.67 234894. 0.6566
|
|
10.23 0.0639 0.1468 0.1197 0.0521 3.422 16.593 18.419 2552.152 1.875 81.927 3.273 0.67 235131. 0.6341
|
|
15.35 0.0959 0.2132 0.1187 0.0534 3.505 16.996 18.265 2614.034 1.920 81.244 3.169 0.67 235393. 0.6114
|
|
20.46 0.1278 0.2750 0.1176 0.0547 3.588 17.397 18.086 2675.755 1.966 80.448 3.066 0.67 235684. 0.5885
|
|
25.58 0.1598 0.3323 0.1162 0.0559 3.669 17.789 17.879 2736.036 2.010 79.524 2.964 0.67 236004. 0.5656
|
|
30.69 0.1918 0.3853 0.1147 0.0571 3.746 18.162 17.638 2793.385 2.052 78.453 2.864 0.67 236355. 0.5429
|
|
35.81 0.2237 0.4343 0.1129 0.0581 3.817 18.505 17.360 2846.115 2.091 77.216 2.767 0.67 236738. 0.5203
|
|
40.92 0.2557 0.4794 0.1108 0.0591 3.879 18.805 17.040 2892.370 2.125 75.795 2.672 0.67 237154. 0.4979
|
|
46.04 0.2877 0.5209 0.1084 0.0599 3.929 19.051 16.675 2930.165 2.152 74.171 2.581 0.67 237604. 0.4758
|
|
51.15 0.3196 0.5592 0.1057 0.0604 3.966 19.229 16.261 2957.456 2.172 72.328 2.494 0.67 238088. 0.4539
|
|
56.27 0.3516 0.5945 0.1027 0.0607 3.986 19.324 15.794 2972.208 2.183 70.250 2.410 0.67 238607. 0.4323
|
|
61.38 0.3835 0.6271 0.0993 0.0607 3.986 19.326 15.271 2972.467 2.183 67.925 2.330 0.68 239162. 0.4110
|
|
66.50 0.4155 0.6570 0.0955 0.0604 3.965 19.222 14.691 2956.438 2.172 65.344 2.254 0.68 239751. 0.3899
|
|
71.61 0.4475 0.6846 0.0913 0.0597 3.919 19.002 14.051 2922.552 2.147 62.501 2.181 0.68 240375. 0.3690
|
|
76.73 0.4794 0.7100 0.0868 0.0586 3.848 18.657 13.353 2869.470 2.108 59.394 2.111 0.68 241034. 0.3481
|
|
81.84 0.5114 0.7331 0.0819 0.0571 3.749 18.178 12.594 2795.859 2.054 56.020 2.043 0.68 241727. 0.3273
|
|
86.96 0.5434 0.7540 0.0766 0.0552 3.622 17.560 11.777 2700.813 1.984 52.386 1.978 0.68 242455. 0.3064
|
|
92.07 0.5753 0.7727 0.0709 0.0528 3.467 16.807 10.910 2585.049 1.899 48.526 1.914 0.68 243216. 0.2854
|
|
97.19 0.6073 0.7888 0.0650 0.0500 3.285 15.928 10.000 2449.869 1.800 44.478 1.851 0.68 244010. 0.2642
|
|
102.30 0.6392 0.8021 0.0589 0.0469 3.080 14.931 9.055 2296.505 1.687 40.276 1.788 0.68 244838. 0.2429
|
|
107.42 0.6712 0.8119 0.0525 0.0434 2.851 13.823 8.082 2126.071 1.562 35.948 1.724 0.69 245697. 0.2212
|
|
112.53 0.7032 0.8175 0.0461 0.0396 2.601 12.611 7.086 1939.626 1.425 31.519 1.657 0.69 246589. 0.1991
|
|
117.65 0.7351 0.8174 0.0395 0.0355 2.331 11.302 6.074 1738.234 1.277 27.016 1.585 0.69 247512. 0.1763
|
|
122.76 0.7671 0.8094 0.0328 0.0311 2.042 9.902 5.050 1523.051 1.119 22.464 1.504 0.69 248468. 0.1526
|
|
127.88 0.7991 0.7894 0.0261 0.0265 1.737 8.422 4.022 1295.392 0.952 17.889 1.408 0.69 249454. 0.1275
|
|
133.00 0.8310 0.7494 0.0195 0.0216 1.417 6.871 2.995 1056.839 0.776 13.320 1.285 0.69 250472. 0.1004
|
|
138.11 0.8630 0.6707 0.0128 0.0165 1.085 5.262 1.977 809.340 0.595 8.792 1.108 0.70 251522. 0.0703
|
|
143.23 0.8949 0.5004 0.0063 0.0113 0.745 3.610 0.976 555.280 0.408 4.340 0.797 0.70 252601. 0.0355
|
|
148.34 0.9269 0.0002 0.0000 0.0061 0.399 1.933 0.000 297.264 0.218 0.001 0.000 0.70 253706. 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 0.1220 0.0506 4.150 18.685 21.765 3094.939 2.111 96.812 3.190 0.72 252718. 0.6717
|
|
5.50 0.0319 0.0748 0.1213 0.0518 4.248 19.123 21.643 3167.416 2.160 96.267 3.099 0.72 252945. 0.6508
|
|
11.01 0.0639 0.1452 0.1205 0.0530 4.348 19.574 21.500 3242.208 2.211 95.630 3.008 0.72 253199. 0.6295
|
|
16.51 0.0958 0.2111 0.1196 0.0543 4.450 20.033 21.332 3318.224 2.263 94.886 2.916 0.72 253482. 0.6079
|
|
22.02 0.1278 0.2726 0.1185 0.0555 4.552 20.492 21.136 3394.172 2.315 94.014 2.824 0.72 253794. 0.5861
|
|
27.52 0.1597 0.3299 0.1172 0.0567 4.651 20.940 20.907 3468.497 2.366 92.993 2.734 0.72 254138. 0.5642
|
|
33.03 0.1916 0.3829 0.1157 0.0579 4.746 21.368 20.639 3539.377 2.414 91.801 2.645 0.72 254516. 0.5423
|
|
38.53 0.2236 0.4320 0.1139 0.0590 4.834 21.763 20.327 3604.756 2.459 90.414 2.558 0.72 254928. 0.5205
|
|
44.04 0.2555 0.4774 0.1119 0.0599 4.911 22.111 19.966 3662.355 2.498 88.811 2.473 0.72 255376. 0.4987
|
|
49.54 0.2874 0.5192 0.1096 0.0607 4.975 22.397 19.552 3709.716 2.530 86.967 2.391 0.72 255860. 0.4771
|
|
55.05 0.3194 0.5577 0.1069 0.0612 5.021 22.605 19.079 3744.261 2.554 84.863 2.311 0.73 256381. 0.4556
|
|
60.55 0.3513 0.5932 0.1039 0.0616 5.047 22.721 18.543 3763.362 2.567 82.479 2.235 0.73 256941. 0.4344
|
|
66.05 0.3833 0.6260 0.1006 0.0616 5.048 22.727 17.940 3764.431 2.568 79.799 2.162 0.73 257537. 0.4133
|
|
71.56 0.4152 0.6561 0.0968 0.0613 5.022 22.610 17.269 3745.043 2.554 76.813 2.091 0.73 258172. 0.3923
|
|
77.06 0.4471 0.6839 0.0926 0.0606 4.966 22.356 16.527 3703.042 2.526 73.513 2.024 0.73 258845. 0.3715
|
|
82.57 0.4791 0.7095 0.0881 0.0595 4.877 21.955 15.715 3636.578 2.480 69.898 1.960 0.73 259555. 0.3507
|
|
88.07 0.5110 0.7329 0.0831 0.0580 4.752 21.396 14.830 3543.907 2.417 65.965 1.898 0.73 260302. 0.3299
|
|
93.58 0.5430 0.7541 0.0778 0.0560 4.591 20.670 13.876 3423.781 2.335 61.718 1.838 0.73 261086. 0.3091
|
|
99.08 0.5749 0.7731 0.0721 0.0536 4.395 19.784 12.859 3277.017 2.235 57.199 1.780 0.73 261906. 0.2881
|
|
104.59 0.6068 0.7897 0.0661 0.0508 4.164 18.748 11.792 3105.280 2.118 52.452 1.722 0.74 262761. 0.2670
|
|
110.09 0.6388 0.8036 0.0599 0.0476 3.903 17.570 10.683 2910.163 1.985 47.516 1.665 0.74 263652. 0.2456
|
|
115.60 0.6707 0.8141 0.0535 0.0441 3.612 16.259 9.538 2693.121 1.837 42.427 1.606 0.74 264578. 0.2239
|
|
121.10 0.7026 0.8205 0.0469 0.0402 3.293 14.825 8.367 2455.545 1.675 37.215 1.545 0.74 265538. 0.2018
|
|
126.60 0.7346 0.8213 0.0402 0.0360 2.949 13.275 7.174 2198.901 1.500 31.910 1.480 0.74 266532. 0.1789
|
|
132.11 0.7665 0.8144 0.0334 0.0315 2.581 11.621 5.967 1924.820 1.313 26.542 1.406 0.74 267560. 0.1550
|
|
137.61 0.7985 0.7954 0.0266 0.0267 2.193 9.872 4.753 1635.224 1.115 21.143 1.318 0.74 268622. 0.1297
|
|
143.12 0.8304 0.7561 0.0198 0.0218 1.787 8.044 3.540 1332.462 0.909 15.748 1.205 0.75 269717. 0.1023
|
|
148.62 0.8623 0.6774 0.0131 0.0167 1.367 6.155 2.337 1019.435 0.695 10.394 1.040 0.75 270846. 0.0717
|
|
154.13 0.8943 0.5047 0.0065 0.0114 0.938 4.224 1.152 699.693 0.477 5.125 0.747 0.75 272008. 0.0362
|
|
159.63 0.9262 -0.0029 0.0000 0.0062 0.506 2.277 -0.003 377.074 0.257 -0.015 -0.004 0.75 273196. 0.0000
|
|
|
|
|
|
|
|
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 0.1227 0.0527 5.317 22.341 25.121 3964.724 2.524 111.737 2.874 0.77 270750. 0.6501
|
|
5.89 0.0319 0.0723 0.1220 0.0539 5.431 22.822 24.993 4050.111 2.578 111.168 2.799 0.77 270992. 0.6316
|
|
11.78 0.0638 0.1406 0.1213 0.0550 5.549 23.317 24.843 4138.054 2.634 110.501 2.723 0.77 271263. 0.6126
|
|
17.67 0.0957 0.2050 0.1204 0.0562 5.669 23.819 24.666 4227.178 2.691 109.713 2.647 0.77 271564. 0.5933
|
|
23.56 0.1276 0.2654 0.1194 0.0574 5.788 24.319 24.457 4315.881 2.748 108.783 2.570 0.77 271898. 0.5737
|
|
29.45 0.1595 0.3220 0.1182 0.0585 5.903 24.806 24.210 4402.238 2.803 107.685 2.494 0.77 272266. 0.5540
|
|
35.33 0.1913 0.3748 0.1168 0.0596 6.013 25.267 23.919 4484.037 2.855 106.390 2.419 0.77 272669. 0.5341
|
|
41.22 0.2232 0.4239 0.1151 0.0606 6.113 25.688 23.577 4558.810 2.902 104.872 2.346 0.78 273109. 0.5141
|
|
47.11 0.2551 0.4696 0.1132 0.0615 6.201 26.055 23.179 4623.840 2.944 103.101 2.274 0.78 273588. 0.4941
|
|
53.00 0.2870 0.5120 0.1109 0.0622 6.271 26.350 22.718 4676.242 2.977 101.049 2.204 0.78 274106. 0.4740
|
|
58.89 0.3189 0.5513 0.1083 0.0627 6.320 26.557 22.188 4712.975 3.000 98.691 2.135 0.78 274664. 0.4540
|
|
64.78 0.3508 0.5876 0.1054 0.0629 6.344 26.658 21.583 4730.957 3.012 96.003 2.069 0.78 275262. 0.4339
|
|
70.67 0.3827 0.6213 0.1021 0.0629 6.339 26.637 20.900 4727.151 3.009 92.964 2.005 0.78 275901. 0.4138
|
|
76.56 0.4146 0.6523 0.0983 0.0625 6.301 26.476 20.135 4698.690 2.991 89.560 1.944 0.78 276581. 0.3937
|
|
82.45 0.4465 0.6810 0.0942 0.0617 6.226 26.162 19.286 4642.987 2.956 85.783 1.884 0.78 277301. 0.3734
|
|
88.34 0.4784 0.7073 0.0896 0.0606 6.112 25.682 18.352 4557.773 2.902 81.630 1.826 0.78 278062. 0.3531
|
|
94.22 0.5103 0.7313 0.0846 0.0591 5.955 25.023 17.333 4440.788 2.827 77.098 1.770 0.78 278862. 0.3327
|
|
100.11 0.5422 0.7531 0.0793 0.0571 5.753 24.174 16.230 4290.110 2.731 72.192 1.716 0.78 279701. 0.3120
|
|
106.00 0.5740 0.7727 0.0735 0.0546 5.507 23.138 15.053 4106.292 2.614 66.955 1.663 0.79 280579. 0.2912
|
|
111.89 0.6059 0.7898 0.0675 0.0517 5.218 21.926 13.814 3891.223 2.477 61.443 1.610 0.79 281495. 0.2701
|
|
117.78 0.6378 0.8042 0.0611 0.0485 4.891 20.549 12.523 3646.861 2.322 55.702 1.558 0.79 282449. 0.2488
|
|
123.67 0.6697 0.8153 0.0546 0.0449 4.526 19.018 11.190 3375.104 2.149 49.773 1.504 0.79 283440. 0.2270
|
|
129.56 0.7016 0.8221 0.0480 0.0409 4.128 17.344 9.823 3078.052 1.960 43.692 1.447 0.79 284467. 0.2048
|
|
135.45 0.7335 0.8232 0.0412 0.0367 3.698 15.540 8.429 2757.891 1.756 37.494 1.386 0.79 285530. 0.1817
|
|
141.34 0.7654 0.8159 0.0343 0.0321 3.241 13.620 7.018 2417.177 1.539 31.215 1.317 0.80 286630. 0.1575
|
|
147.23 0.7973 0.7956 0.0273 0.0274 2.761 11.602 5.596 2058.966 1.311 24.890 1.233 0.80 287765. 0.1316
|
|
153.12 0.8292 0.7530 0.0204 0.0224 2.262 9.506 4.172 1686.929 1.074 18.558 1.122 0.80 288936. 0.1034
|
|
159.00 0.8611 0.6678 0.0135 0.0174 1.751 7.357 2.758 1305.550 0.831 12.266 0.958 0.80 290143. 0.0718
|
|
164.89 0.8930 0.4858 0.0067 0.0122 1.234 5.184 1.363 920.024 0.586 6.063 0.672 0.80 291385. 0.0354
|
|
170.78 0.9249 0.0001 0.0000 0.0071 0.719 3.020 0.000 535.896 0.341 0.001 0.000 0.81 292656. 0.0000
|
|
|
|
|
|
|
|
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 0.1233 0.0567 6.945 27.357 28.723 5178.556 3.091 127.758 2.516 0.83 288776. 0.6085
|
|
6.28 0.0319 0.0677 0.1227 0.0578 7.076 27.875 28.593 5276.672 3.149 127.182 2.458 0.83 289034. 0.5932
|
|
12.56 0.0638 0.1321 0.1221 0.0589 7.211 28.406 28.440 5377.141 3.209 126.501 2.399 0.83 289322. 0.5774
|
|
18.84 0.0956 0.1932 0.1213 0.0600 7.346 28.939 28.258 5478.132 3.270 125.692 2.340 0.83 289642. 0.5614
|
|
25.12 0.1275 0.2511 0.1203 0.0611 7.480 29.464 28.041 5577.509 3.329 124.727 2.280 0.83 289997. 0.5450
|
|
31.40 0.1594 0.3058 0.1192 0.0622 7.607 29.967 27.782 5672.747 3.386 123.575 2.221 0.83 290388. 0.5285
|
|
37.68 0.1913 0.3573 0.1179 0.0631 7.726 30.433 27.474 5760.974 3.438 122.203 2.163 0.83 290817. 0.5117
|
|
43.96 0.2232 0.4058 0.1163 0.0640 7.830 30.846 27.108 5839.129 3.485 120.576 2.106 0.83 291287. 0.4948
|
|
50.24 0.2551 0.4514 0.1145 0.0647 7.917 31.188 26.677 5903.935 3.524 118.659 2.049 0.83 291797. 0.4778
|
|
56.52 0.2869 0.4942 0.1123 0.0652 7.982 31.442 26.173 5951.977 3.552 116.417 1.994 0.83 292350. 0.4606
|
|
62.80 0.3188 0.5343 0.1098 0.0655 8.019 31.589 25.588 5979.808 3.569 113.817 1.941 0.83 292945. 0.4431
|
|
69.08 0.3507 0.5719 0.1069 0.0656 8.025 31.611 24.916 5984.000 3.571 110.828 1.889 0.83 293584. 0.4255
|
|
75.36 0.3826 0.6071 0.1037 0.0653 7.994 31.491 24.152 5961.219 3.558 107.427 1.838 0.83 294267. 0.4076
|
|
81.64 0.4145 0.6399 0.1000 0.0647 7.923 31.212 23.290 5908.376 3.526 103.592 1.788 0.83 294993. 0.3894
|
|
87.92 0.4463 0.6703 0.0958 0.0638 7.808 30.760 22.328 5822.748 3.475 99.314 1.739 0.83 295762. 0.3709
|
|
94.20 0.4782 0.6985 0.0913 0.0625 7.647 30.122 21.265 5702.005 3.403 94.588 1.692 0.83 296575. 0.3521
|
|
100.47 0.5101 0.7244 0.0863 0.0607 7.434 29.286 20.101 5543.769 3.309 89.410 1.645 0.84 297430. 0.3328
|
|
106.75 0.5420 0.7480 0.0808 0.0586 7.169 28.240 18.837 5345.843 3.191 83.787 1.598 0.84 298327. 0.3131
|
|
113.03 0.5739 0.7692 0.0750 0.0560 6.851 26.988 17.483 5108.806 3.049 77.765 1.552 0.84 299265. 0.2929
|
|
119.31 0.6057 0.7878 0.0689 0.0530 6.484 25.542 16.054 4835.100 2.886 71.410 1.506 0.84 300244. 0.2724
|
|
125.59 0.6376 0.8029 0.0625 0.0496 6.074 23.927 14.563 4529.391 2.703 64.775 1.458 0.84 301263. 0.2512
|
|
131.87 0.6695 0.8140 0.0559 0.0460 5.624 22.156 13.019 4194.021 2.503 57.909 1.408 0.84 302320. 0.2293
|
|
138.15 0.7014 0.8199 0.0491 0.0420 5.137 20.237 11.433 3830.811 2.286 50.856 1.354 0.85 303417. 0.2066
|
|
144.43 0.7333 0.8189 0.0421 0.0377 4.616 18.183 9.815 3442.068 2.054 43.657 1.293 0.85 304553. 0.1829
|
|
150.71 0.7652 0.8079 0.0351 0.0332 4.066 16.016 8.173 3031.785 1.809 36.354 1.223 0.85 305726. 0.1578
|
|
156.99 0.7970 0.7810 0.0280 0.0285 3.493 13.762 6.518 2605.065 1.555 28.990 1.135 0.85 306938. 0.1308
|
|
163.27 0.8289 0.7278 0.0209 0.0238 2.907 11.451 4.859 2167.640 1.294 21.613 1.017 0.85 308187. 0.1012
|
|
169.55 0.8608 0.6269 0.0138 0.0189 2.315 9.118 3.209 1725.957 1.030 14.274 0.843 0.86 309474. 0.0682
|
|
175.83 0.8927 0.4295 0.0068 0.0141 1.726 6.800 1.582 1287.316 0.768 7.035 0.557 0.86 310798. 0.0316
|
|
182.11 0.9246 -0.0041 0.0000 0.0094 1.152 4.537 -0.010 858.786 0.513 -0.043 -0.005 0.86 312153. 0.0000
|
|
|
|
|
|
|
|
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 0.1234 0.0626 9.196 34.096 32.470 6857.771 3.852 144.426 2.148 0.88 306814. 0.5523
|
|
6.69 0.0320 0.0617 0.1230 0.0637 9.354 34.680 32.345 6975.222 3.918 143.871 2.103 0.88 307085. 0.5399
|
|
13.37 0.0639 0.1207 0.1224 0.0648 9.514 35.274 32.196 7094.624 3.985 143.210 2.058 0.88 307389. 0.5272
|
|
20.06 0.0959 0.1771 0.1217 0.0659 9.673 35.864 32.018 7213.359 4.052 142.416 2.013 0.88 307728. 0.5142
|
|
26.75 0.1278 0.2308 0.1209 0.0669 9.827 36.436 31.802 7328.339 4.116 141.457 1.968 0.88 308103. 0.5010
|
|
33.43 0.1598 0.2820 0.1199 0.0679 9.972 36.971 31.542 7435.895 4.177 140.297 1.924 0.88 308518. 0.4877
|
|
40.12 0.1917 0.3307 0.1187 0.0688 10.100 37.448 31.226 7531.876 4.231 138.894 1.880 0.88 308974. 0.4743
|
|
46.81 0.2237 0.3772 0.1173 0.0695 10.207 37.843 30.846 7611.285 4.275 137.202 1.838 0.88 309472. 0.4608
|
|
53.49 0.2556 0.4214 0.1155 0.0701 10.286 38.137 30.391 7670.417 4.309 135.179 1.797 0.88 310015. 0.4472
|
|
60.18 0.2876 0.4636 0.1135 0.0704 10.333 38.308 29.852 7704.959 4.328 132.783 1.757 0.88 310604. 0.4334
|
|
66.87 0.3195 0.5038 0.1111 0.0704 10.340 38.338 29.220 7710.899 4.331 129.970 1.719 0.88 311239. 0.4194
|
|
73.55 0.3515 0.5422 0.1083 0.0702 10.305 38.207 28.486 7684.560 4.317 126.704 1.681 0.88 311920. 0.4050
|
|
80.24 0.3834 0.5786 0.1051 0.0696 10.222 37.899 27.642 7622.676 4.282 122.952 1.645 0.88 312649. 0.3903
|
|
86.93 0.4154 0.6131 0.1014 0.0687 10.088 37.401 26.684 7522.404 4.226 118.690 1.609 0.88 313425. 0.3751
|
|
93.61 0.4473 0.6458 0.0974 0.0674 9.899 36.700 25.607 7381.396 4.146 113.902 1.574 0.89 314247. 0.3594
|
|
100.30 0.4793 0.6764 0.0928 0.0658 9.652 35.786 24.411 7197.677 4.043 108.581 1.538 0.89 315115. 0.3431
|
|
106.99 0.5112 0.7050 0.0878 0.0637 9.346 34.649 23.094 6969.039 3.915 102.722 1.503 0.89 316030. 0.3260
|
|
113.67 0.5432 0.7313 0.0823 0.0611 8.976 33.279 21.656 6693.369 3.760 96.327 1.468 0.89 316989. 0.3082
|
|
120.36 0.5751 0.7553 0.0765 0.0582 8.546 31.683 20.111 6372.385 3.580 89.456 1.431 0.89 317992. 0.2898
|
|
127.05 0.6071 0.7767 0.0702 0.0549 8.059 29.878 18.477 6009.386 3.376 82.184 1.395 0.89 319038. 0.2706
|
|
133.74 0.6390 0.7944 0.0637 0.0513 7.526 27.904 16.766 5612.423 3.153 74.575 1.355 0.89 320127. 0.2504
|
|
140.42 0.6710 0.8062 0.0570 0.0474 6.963 25.815 14.991 5192.212 2.917 66.681 1.310 0.90 321257. 0.2289
|
|
147.11 0.7029 0.8097 0.0500 0.0434 6.377 23.642 13.163 4755.069 2.671 58.549 1.256 0.90 322429. 0.2056
|
|
153.80 0.7349 0.8031 0.0429 0.0393 5.767 21.382 11.294 4300.544 2.416 50.236 1.191 0.90 323642. 0.1807
|
|
160.48 0.7668 0.7834 0.0357 0.0350 5.133 19.031 9.397 3827.653 2.150 41.798 1.114 0.90 324895. 0.1541
|
|
167.17 0.7988 0.7439 0.0285 0.0306 4.485 16.627 7.484 3344.137 1.878 33.290 1.015 0.90 326188. 0.1253
|
|
173.86 0.8307 0.6735 0.0212 0.0261 3.833 14.212 5.569 2858.439 1.606 24.771 0.884 0.91 327521. 0.0941
|
|
180.54 0.8627 0.5534 0.0139 0.0217 3.190 11.829 3.667 2379.094 1.336 16.312 0.699 0.91 328894. 0.0604
|
|
187.23 0.8946 0.3493 0.0068 0.0175 2.568 9.523 1.797 1915.313 1.076 7.994 0.426 0.91 330307. 0.0258
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193.92 0.9266 -0.0057 -0.0001 0.0135 1.977 7.328 -0.022 1473.902 0.828 -0.096 -0.007 0.91 331757. 0.0000
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PROP RPM = 18000
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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 0.1220 0.0679 11.823 41.399 35.988 8816.435 4.677 160.076 1.851 0.93 324905. 0.5013
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7.12 0.0321 0.0566 0.1217 0.0690 12.024 42.104 35.876 8966.579 4.757 159.576 1.815 0.93 325190. 0.4906
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14.24 0.0643 0.1109 0.1212 0.0702 12.233 42.834 35.742 9121.943 4.839 158.981 1.777 0.93 325508. 0.4796
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21.36 0.0964 0.1628 0.1207 0.0714 12.444 43.572 35.580 9279.191 4.923 158.262 1.739 0.93 325864. 0.4682
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28.48 0.1285 0.2124 0.1200 0.0726 12.651 44.300 35.383 9434.111 5.005 157.383 1.701 0.93 326258. 0.4567
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35.60 0.1606 0.2596 0.1192 0.0737 12.849 44.991 35.140 9581.442 5.083 156.304 1.663 0.93 326694. 0.4451
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42.72 0.1928 0.3046 0.1181 0.0748 13.028 45.618 34.842 9714.910 5.154 154.976 1.627 0.93 327174. 0.4334
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49.84 0.2249 0.3476 0.1169 0.0756 13.179 46.147 34.475 9827.464 5.214 153.346 1.591 0.93 327700. 0.4217
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56.96 0.2570 0.3888 0.1154 0.0763 13.292 46.542 34.028 9911.639 5.258 151.357 1.557 0.93 328274. 0.4100
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64.07 0.2892 0.4284 0.1136 0.0767 13.357 46.769 33.487 9960.036 5.284 148.951 1.525 0.93 328897. 0.3983
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71.19 0.3213 0.4665 0.1114 0.0767 13.364 46.797 32.840 9965.847 5.287 146.071 1.495 0.93 329571. 0.3866
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78.31 0.3534 0.5033 0.1088 0.0764 13.307 46.596 32.074 9923.232 5.264 142.664 1.466 0.93 330296. 0.3747
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85.43 0.3855 0.5390 0.1057 0.0756 13.179 46.147 31.179 9827.575 5.214 138.684 1.439 0.94 331072. 0.3627
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92.55 0.4177 0.5734 0.1022 0.0745 12.975 45.433 30.147 9675.540 5.133 134.096 1.413 0.94 331899. 0.3502
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99.67 0.4498 0.6067 0.0982 0.0728 12.693 44.446 28.974 9465.171 5.021 128.875 1.388 0.94 332778. 0.3373
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106.79 0.4819 0.6386 0.0938 0.0708 12.331 43.176 27.654 9194.870 4.878 123.003 1.364 0.94 333707. 0.3238
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|
113.91 0.5141 0.6691 0.0888 0.0682 11.889 41.631 26.188 8865.699 4.703 116.484 1.340 0.94 334685. 0.3095
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|
121.03 0.5462 0.6977 0.0833 0.0652 11.369 39.809 24.578 8477.687 4.498 109.322 1.315 0.94 335712. 0.2942
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128.15 0.5783 0.7243 0.0774 0.0618 10.775 37.729 22.839 8034.824 4.263 101.587 1.289 0.94 336786. 0.2781
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|
135.27 0.6104 0.7485 0.0712 0.0580 10.115 35.419 20.991 7542.858 4.002 93.368 1.262 0.95 337907. 0.2610
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|
142.39 0.6426 0.7696 0.0646 0.0539 9.400 32.915 19.052 7009.531 3.719 84.745 1.233 0.95 339073. 0.2429
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|
149.51 0.6747 0.7837 0.0578 0.0497 8.665 30.342 17.034 6461.599 3.428 75.768 1.196 0.95 340284. 0.2227
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|
156.63 0.7068 0.7866 0.0507 0.0456 7.937 27.793 14.949 5918.751 3.140 66.493 1.146 0.95 341538. 0.1999
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163.75 0.7390 0.7702 0.0434 0.0417 7.259 25.419 12.805 5413.179 2.872 56.956 1.073 0.95 342836. 0.1733
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170.87 0.7711 0.7372 0.0360 0.0377 6.570 23.006 10.631 4899.457 2.599 47.285 0.984 0.96 344178. 0.1448
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|
177.99 0.8032 0.6813 0.0286 0.0338 5.883 20.600 8.445 4386.934 2.327 37.563 0.873 0.96 345562. 0.1145
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|
185.10 0.8353 0.5937 0.0213 0.0299 5.212 18.249 6.269 3886.421 2.062 27.884 0.732 0.96 346988. 0.0827
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192.22 0.8675 0.4630 0.0140 0.0262 4.570 16.001 4.127 3407.576 1.808 18.358 0.549 0.96 348457. 0.0504
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199.34 0.8996 0.2745 0.0069 0.0228 3.967 13.890 2.048 2957.973 1.569 9.111 0.314 0.97 349971. 0.0203
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206.46 0.9317 0.0078 0.0002 0.0195 3.403 11.915 0.048 2537.537 1.346 0.213 0.009 0.97 351547. 0.0001
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