612 lines
109 KiB
Plaintext
612 lines
109 KiB
Plaintext
14x10 (14x10.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 0.1143 0.0577 0.002 0.157 0.140 1.861 0.018 0.622 34.105 0.06 24299. 0.5347
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0.40 0.0304 0.0587 0.1131 0.0586 0.003 0.160 0.138 1.890 0.018 0.616 33.232 0.06 24320. 0.5183
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0.81 0.0608 0.1143 0.1118 0.0594 0.003 0.162 0.137 1.918 0.018 0.609 32.350 0.06 24343. 0.5015
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1.21 0.0912 0.1667 0.1103 0.0603 0.003 0.164 0.135 1.946 0.019 0.600 31.465 0.06 24369. 0.4845
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1.61 0.1216 0.2161 0.1086 0.0611 0.003 0.167 0.133 1.972 0.019 0.591 30.582 0.06 24398. 0.4674
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2.01 0.1520 0.2623 0.1068 0.0619 0.003 0.169 0.131 1.996 0.019 0.581 29.702 0.06 24429. 0.4501
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2.42 0.1824 0.3056 0.1047 0.0625 0.003 0.171 0.128 2.017 0.019 0.570 28.829 0.06 24463. 0.4327
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2.82 0.2128 0.3458 0.1025 0.0631 0.003 0.172 0.125 2.035 0.019 0.558 27.965 0.06 24500. 0.4152
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3.22 0.2431 0.3831 0.1000 0.0635 0.003 0.173 0.122 2.049 0.020 0.545 27.112 0.06 24540. 0.3976
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3.63 0.2735 0.4176 0.0973 0.0637 0.003 0.174 0.119 2.057 0.020 0.530 26.269 0.06 24583. 0.3800
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4.03 0.3039 0.4493 0.0944 0.0638 0.003 0.174 0.116 2.060 0.020 0.514 25.436 0.06 24629. 0.3624
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4.43 0.3343 0.4783 0.0912 0.0637 0.003 0.174 0.112 2.056 0.020 0.496 24.613 0.06 24679. 0.3446
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4.84 0.3647 0.5045 0.0877 0.0634 0.003 0.173 0.107 2.045 0.020 0.477 23.798 0.06 24731. 0.3268
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5.24 0.3951 0.5279 0.0839 0.0628 0.003 0.171 0.103 2.026 0.019 0.457 22.989 0.06 24787. 0.3088
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5.64 0.4255 0.5486 0.0798 0.0619 0.003 0.169 0.098 1.999 0.019 0.435 22.182 0.06 24846. 0.2907
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6.04 0.4559 0.5664 0.0755 0.0608 0.003 0.166 0.092 1.962 0.019 0.411 21.374 0.06 24908. 0.2724
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6.45 0.4863 0.5811 0.0709 0.0594 0.003 0.162 0.087 1.916 0.018 0.386 20.560 0.06 24973. 0.2539
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6.85 0.5167 0.5926 0.0662 0.0577 0.002 0.157 0.081 1.862 0.018 0.360 19.734 0.06 25042. 0.2354
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7.25 0.5471 0.6006 0.0612 0.0557 0.002 0.152 0.075 1.799 0.017 0.333 18.888 0.06 25113. 0.2167
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7.66 0.5775 0.6045 0.0561 0.0536 0.002 0.146 0.069 1.728 0.017 0.305 18.012 0.06 25188. 0.1978
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8.06 0.6079 0.6040 0.0508 0.0511 0.002 0.139 0.062 1.650 0.016 0.277 17.096 0.06 25266. 0.1787
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8.46 0.6383 0.5981 0.0454 0.0485 0.002 0.132 0.056 1.565 0.015 0.247 16.123 0.06 25347. 0.1594
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8.86 0.6686 0.5858 0.0400 0.0456 0.002 0.124 0.049 1.472 0.014 0.218 15.073 0.06 25431. 0.1397
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9.27 0.6990 0.5655 0.0344 0.0425 0.002 0.116 0.042 1.372 0.013 0.187 13.919 0.06 25518. 0.1197
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9.67 0.7294 0.5351 0.0287 0.0392 0.002 0.107 0.035 1.265 0.012 0.157 12.621 0.06 25609. 0.0992
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10.07 0.7598 0.4911 0.0230 0.0357 0.002 0.097 0.028 1.151 0.011 0.125 11.120 0.06 25702. 0.0783
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10.48 0.7902 0.4284 0.0173 0.0319 0.001 0.087 0.021 1.030 0.010 0.094 9.327 0.06 25799. 0.0569
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10.88 0.8206 0.3384 0.0115 0.0280 0.001 0.076 0.014 0.904 0.009 0.063 7.095 0.06 25898. 0.0354
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11.28 0.8510 0.2062 0.0058 0.0239 0.001 0.065 0.007 0.772 0.007 0.032 4.170 0.06 26001. 0.0147
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11.69 0.8814 0.0030 0.0001 0.0196 0.001 0.054 0.000 0.634 0.006 0.000 0.058 0.06 26106. 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 0.1148 0.0515 0.018 0.562 0.562 13.296 0.063 2.501 19.179 0.11 48598. 0.6027
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0.81 0.0306 0.0663 0.1136 0.0525 0.018 0.572 0.556 13.545 0.065 2.475 18.633 0.11 48640. 0.5826
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1.62 0.0612 0.1287 0.1123 0.0534 0.018 0.583 0.550 13.793 0.066 2.446 18.086 0.11 48687. 0.5622
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2.44 0.0919 0.1873 0.1108 0.0544 0.019 0.593 0.543 14.034 0.067 2.414 17.542 0.11 48739. 0.5416
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3.25 0.1225 0.2421 0.1092 0.0552 0.019 0.603 0.535 14.264 0.068 2.378 17.002 0.11 48797. 0.5211
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4.06 0.1531 0.2931 0.1074 0.0561 0.019 0.612 0.526 14.478 0.069 2.338 16.470 0.11 48860. 0.5005
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4.87 0.1837 0.3405 0.1053 0.0568 0.020 0.620 0.516 14.670 0.070 2.294 15.946 0.11 48929. 0.4800
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5.68 0.2143 0.3845 0.1031 0.0575 0.020 0.627 0.505 14.834 0.071 2.245 15.433 0.11 49004. 0.4595
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6.49 0.2449 0.4251 0.1006 0.0580 0.020 0.632 0.493 14.965 0.071 2.191 14.931 0.11 49085. 0.4392
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7.31 0.2756 0.4625 0.0979 0.0583 0.020 0.636 0.479 15.055 0.072 2.132 14.440 0.11 49172. 0.4190
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8.12 0.3062 0.4969 0.0949 0.0585 0.020 0.638 0.465 15.098 0.072 2.067 13.961 0.11 49265. 0.3989
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8.93 0.3368 0.5282 0.0917 0.0584 0.020 0.638 0.449 15.088 0.072 1.996 13.493 0.11 49365. 0.3789
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9.74 0.3674 0.5567 0.0881 0.0582 0.020 0.635 0.432 15.017 0.072 1.920 13.035 0.11 49472. 0.3589
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10.55 0.3980 0.5823 0.0843 0.0576 0.020 0.629 0.413 14.879 0.071 1.837 12.586 0.11 49585. 0.3390
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11.37 0.4287 0.6052 0.0802 0.0568 0.020 0.620 0.393 14.669 0.070 1.747 12.145 0.11 49704. 0.3190
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12.18 0.4593 0.6252 0.0758 0.0557 0.019 0.608 0.371 14.383 0.069 1.652 11.710 0.11 49830. 0.2991
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12.99 0.4899 0.6423 0.0712 0.0543 0.019 0.593 0.349 14.022 0.067 1.551 11.279 0.11 49962. 0.2792
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13.80 0.5205 0.6564 0.0664 0.0526 0.018 0.574 0.325 13.588 0.065 1.446 10.849 0.11 50101. 0.2592
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14.61 0.5511 0.6673 0.0614 0.0507 0.018 0.553 0.300 13.084 0.062 1.336 10.416 0.11 50246. 0.2393
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15.43 0.5817 0.6745 0.0562 0.0485 0.017 0.529 0.275 12.512 0.060 1.224 9.974 0.11 50397. 0.2193
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16.24 0.6124 0.6776 0.0509 0.0460 0.016 0.502 0.249 11.873 0.057 1.108 9.519 0.11 50555. 0.1991
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17.05 0.6430 0.6758 0.0455 0.0433 0.015 0.472 0.223 11.169 0.053 0.990 9.041 0.11 50719. 0.1788
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17.86 0.6736 0.6680 0.0400 0.0403 0.014 0.440 0.196 10.401 0.050 0.870 8.532 0.11 50890. 0.1582
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18.67 0.7042 0.6527 0.0344 0.0371 0.013 0.404 0.168 9.570 0.046 0.748 7.974 0.11 51067. 0.1371
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19.48 0.7348 0.6273 0.0287 0.0336 0.012 0.367 0.141 8.678 0.041 0.625 7.344 0.11 51250. 0.1154
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20.30 0.7655 0.5879 0.0230 0.0299 0.010 0.326 0.113 7.726 0.037 0.501 6.607 0.11 51440. 0.0929
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21.11 0.7961 0.5275 0.0172 0.0260 0.009 0.284 0.084 6.716 0.032 0.375 5.700 0.11 51635. 0.0694
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21.92 0.8267 0.4336 0.0115 0.0219 0.008 0.239 0.056 5.653 0.027 0.250 4.512 0.11 51837. 0.0448
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22.73 0.8573 0.2800 0.0057 0.0176 0.006 0.192 0.028 4.540 0.022 0.125 2.809 0.12 52045. 0.0197
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23.54 0.8879 0.0026 0.0000 0.0131 0.005 0.143 0.000 3.381 0.016 0.001 0.026 0.12 52257. 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 0.1152 0.0490 0.057 1.203 1.269 42.701 0.136 5.644 13.477 0.17 72895. 0.6363
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1.22 0.0307 0.0700 0.1140 0.0500 0.058 1.228 1.256 43.569 0.139 5.586 13.075 0.17 72959. 0.6141
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2.44 0.0614 0.1358 0.1127 0.0510 0.060 1.252 1.241 44.434 0.141 5.522 12.673 0.17 73030. 0.5918
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3.67 0.0922 0.1972 0.1112 0.0520 0.061 1.276 1.225 45.280 0.144 5.450 12.274 0.17 73109. 0.5695
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4.89 0.1229 0.2546 0.1096 0.0529 0.062 1.299 1.207 46.090 0.147 5.370 11.881 0.17 73195. 0.5471
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6.11 0.1536 0.3079 0.1077 0.0538 0.063 1.320 1.187 46.846 0.149 5.280 11.494 0.17 73290. 0.5249
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7.33 0.1843 0.3573 0.1057 0.0545 0.064 1.339 1.165 47.528 0.151 5.181 11.116 0.17 73394. 0.5028
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8.55 0.2151 0.4029 0.1035 0.0552 0.065 1.356 1.140 48.117 0.153 5.071 10.746 0.17 73507. 0.4809
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9.78 0.2458 0.4451 0.1010 0.0558 0.065 1.369 1.113 48.591 0.155 4.949 10.386 0.17 73629. 0.4592
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11.00 0.2765 0.4838 0.0983 0.0561 0.066 1.378 1.083 48.927 0.156 4.815 10.036 0.17 73761. 0.4377
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12.22 0.3072 0.5194 0.0953 0.0564 0.066 1.383 1.050 49.103 0.156 4.669 9.696 0.17 73902. 0.4164
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13.44 0.3379 0.5519 0.0920 0.0563 0.066 1.383 1.014 49.095 0.156 4.509 9.366 0.17 74053. 0.3952
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14.66 0.3687 0.5814 0.0885 0.0561 0.066 1.377 0.975 48.880 0.156 4.336 9.045 0.17 74214. 0.3743
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15.88 0.3994 0.6081 0.0846 0.0556 0.065 1.365 0.932 48.435 0.154 4.148 8.732 0.17 74384. 0.3534
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17.11 0.4301 0.6320 0.0805 0.0548 0.064 1.345 0.887 47.739 0.152 3.945 8.427 0.17 74564. 0.3326
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18.33 0.4608 0.6531 0.0761 0.0537 0.063 1.318 0.838 46.783 0.149 3.729 8.128 0.17 74754. 0.3119
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19.55 0.4915 0.6715 0.0714 0.0523 0.061 1.284 0.787 45.567 0.145 3.501 7.835 0.17 74953. 0.2913
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20.77 0.5223 0.6870 0.0666 0.0506 0.059 1.242 0.733 44.098 0.140 3.262 7.544 0.17 75163. 0.2708
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21.99 0.5530 0.6994 0.0615 0.0486 0.057 1.194 0.678 42.385 0.135 3.015 7.254 0.17 75382. 0.2503
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23.22 0.5837 0.7085 0.0563 0.0464 0.054 1.139 0.621 40.433 0.129 2.760 6.961 0.17 75611. 0.2298
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24.44 0.6144 0.7137 0.0510 0.0439 0.051 1.078 0.562 38.249 0.122 2.499 6.662 0.17 75849. 0.2093
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25.66 0.6452 0.7144 0.0455 0.0411 0.048 1.010 0.502 35.836 0.114 2.232 6.351 0.17 76097. 0.1886
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26.88 0.6759 0.7096 0.0400 0.0381 0.045 0.935 0.441 33.198 0.106 1.960 6.022 0.17 76354. 0.1675
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28.10 0.7066 0.6977 0.0344 0.0348 0.041 0.855 0.379 30.340 0.097 1.685 5.663 0.17 76621. 0.1461
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29.33 0.7373 0.6762 0.0287 0.0313 0.037 0.768 0.316 27.266 0.087 1.406 5.260 0.17 76898. 0.1240
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30.55 0.7680 0.6409 0.0230 0.0275 0.032 0.676 0.253 23.982 0.076 1.126 4.786 0.17 77184. 0.1009
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31.77 0.7988 0.5843 0.0172 0.0235 0.027 0.578 0.190 20.498 0.065 0.843 4.196 0.17 77479. 0.0766
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32.99 0.8295 0.4916 0.0114 0.0193 0.023 0.474 0.126 16.823 0.054 0.561 3.399 0.17 77783. 0.0506
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34.21 0.8602 0.3290 0.0057 0.0149 0.017 0.366 0.063 12.975 0.041 0.279 2.194 0.17 78097. 0.0230
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35.43 0.8909 -0.0010 0.0000 0.0103 0.012 0.253 0.000 8.966 0.029 -0.001 -0.006 0.17 78416. 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 0.1155 0.0477 0.132 2.080 2.262 98.443 0.235 10.062 10.423 0.22 97192. 0.6570
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1.65 0.0311 0.0730 0.1143 0.0487 0.135 2.125 2.239 100.569 0.240 9.960 10.099 0.22 97278. 0.6334
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3.30 0.0622 0.1414 0.1130 0.0497 0.138 2.170 2.214 102.690 0.245 9.846 9.777 0.22 97374. 0.6097
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4.95 0.0933 0.2052 0.1115 0.0507 0.140 2.214 2.185 104.766 0.250 9.717 9.458 0.22 97480. 0.5859
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6.60 0.1244 0.2645 0.1099 0.0517 0.143 2.256 2.152 106.756 0.255 9.573 9.144 0.22 97598. 0.5623
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8.25 0.1555 0.3195 0.1080 0.0526 0.146 2.295 2.116 108.614 0.259 9.412 8.837 0.22 97727. 0.5388
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9.90 0.1866 0.3704 0.1060 0.0534 0.148 2.331 2.076 110.293 0.263 9.233 8.536 0.22 97868. 0.5155
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11.55 0.2177 0.4173 0.1037 0.0541 0.150 2.361 2.031 111.740 0.267 9.034 8.244 0.22 98022. 0.4924
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13.20 0.2489 0.4605 0.1012 0.0547 0.151 2.386 1.982 112.901 0.270 8.814 7.961 0.22 98188. 0.4697
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14.85 0.2800 0.5002 0.0984 0.0551 0.153 2.403 1.927 113.723 0.271 8.571 7.686 0.22 98367. 0.4472
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16.50 0.3111 0.5366 0.0953 0.0553 0.153 2.412 1.867 114.147 0.273 8.305 7.420 0.22 98559. 0.4249
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18.15 0.3422 0.5697 0.0920 0.0552 0.153 2.411 1.802 114.115 0.272 8.015 7.162 0.22 98765. 0.4029
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19.80 0.3733 0.5999 0.0884 0.0550 0.152 2.400 1.731 113.568 0.271 7.699 6.912 0.22 98983. 0.3811
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21.44 0.4044 0.6271 0.0844 0.0544 0.151 2.376 1.654 112.447 0.268 7.356 6.671 0.22 99216. 0.3595
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23.09 0.4355 0.6516 0.0802 0.0536 0.148 2.339 1.571 110.706 0.264 6.987 6.436 0.22 99461. 0.3380
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24.74 0.4666 0.6733 0.0757 0.0524 0.145 2.289 1.482 108.324 0.259 6.593 6.206 0.22 99720. 0.3167
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26.39 0.4977 0.6922 0.0709 0.0510 0.141 2.225 1.389 105.305 0.251 6.178 5.982 0.22 99992. 0.2955
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28.04 0.5288 0.7083 0.0659 0.0492 0.136 2.148 1.291 101.665 0.243 5.744 5.761 0.23 100278. 0.2744
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29.69 0.5599 0.7214 0.0608 0.0472 0.131 2.059 1.190 97.423 0.233 5.295 5.542 0.23 100576. 0.2534
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31.34 0.5910 0.7312 0.0555 0.0448 0.124 1.957 1.086 92.593 0.221 4.832 5.321 0.23 100888. 0.2324
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32.99 0.6221 0.7371 0.0500 0.0422 0.117 1.842 0.980 87.189 0.208 4.358 5.097 0.23 101213. 0.2114
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34.64 0.6532 0.7386 0.0445 0.0393 0.109 1.716 0.871 81.221 0.194 3.874 4.864 0.23 101551. 0.1902
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36.29 0.6843 0.7346 0.0388 0.0362 0.100 1.578 0.760 74.697 0.178 3.382 4.617 0.23 101902. 0.1687
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37.94 0.7154 0.7232 0.0331 0.0327 0.091 1.429 0.648 67.628 0.161 2.884 4.348 0.23 102266. 0.1467
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39.59 0.7466 0.7017 0.0273 0.0291 0.080 1.268 0.535 60.026 0.143 2.380 4.043 0.23 102643. 0.1239
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41.24 0.7777 0.6650 0.0215 0.0251 0.070 1.097 0.421 51.910 0.124 1.872 3.678 0.23 103033. 0.1000
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42.89 0.8088 0.6035 0.0156 0.0210 0.058 0.915 0.306 43.301 0.103 1.363 3.210 0.23 103436. 0.0745
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44.54 0.8399 0.4967 0.0098 0.0166 0.046 0.723 0.192 34.233 0.082 0.854 2.544 0.23 103851. 0.0467
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46.19 0.8710 0.2898 0.0040 0.0120 0.033 0.523 0.078 24.744 0.059 0.347 1.431 0.23 104278. 0.0168
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47.84 0.9021
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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 0.1159 0.0469 0.254 3.196 3.546 189.066 0.361 15.772 8.507 0.28 121486. 0.6714
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2.04 0.0308 0.0738 0.1147 0.0479 0.259 3.267 3.511 193.250 0.369 15.617 8.241 0.28 121593. 0.6472
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4.09 0.0616 0.1429 0.1134 0.0489 0.265 3.337 3.472 197.430 0.377 15.443 7.976 0.28 121711. 0.6229
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6.13 0.0924 0.2072 0.1120 0.0500 0.270 3.407 3.428 201.530 0.385 15.246 7.714 0.28 121843. 0.5986
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8.17 0.1233 0.2671 0.1104 0.0509 0.276 3.473 3.378 205.470 0.392 15.026 7.457 0.28 121988. 0.5745
|
|
10.21 0.1541 0.3226 0.1086 0.0518 0.280 3.536 3.323 209.164 0.399 14.780 7.206 0.28 122148. 0.5505
|
|
12.26 0.1849 0.3740 0.1066 0.0527 0.285 3.592 3.261 212.517 0.406 14.506 6.960 0.28 122322. 0.5268
|
|
14.30 0.2157 0.4214 0.1043 0.0534 0.289 3.642 3.193 215.430 0.411 14.201 6.722 0.28 122511. 0.5034
|
|
16.34 0.2465 0.4650 0.1018 0.0540 0.292 3.682 3.117 217.802 0.416 13.864 6.491 0.28 122716. 0.4803
|
|
18.38 0.2773 0.5051 0.0991 0.0544 0.294 3.711 3.033 219.526 0.419 13.492 6.267 0.28 122936. 0.4575
|
|
20.43 0.3082 0.5419 0.0961 0.0547 0.296 3.727 2.942 220.493 0.421 13.084 6.051 0.28 123173. 0.4350
|
|
22.47 0.3390 0.5755 0.0928 0.0547 0.296 3.729 2.841 220.590 0.421 12.639 5.842 0.28 123426. 0.4128
|
|
24.51 0.3698 0.6062 0.0893 0.0545 0.295 3.714 2.732 219.703 0.420 12.153 5.641 0.28 123696. 0.3908
|
|
26.55 0.4006 0.6340 0.0854 0.0540 0.292 3.680 2.614 217.719 0.416 11.627 5.446 0.28 123981. 0.3690
|
|
28.60 0.4314 0.6590 0.0812 0.0532 0.288 3.627 2.486 214.544 0.410 11.060 5.257 0.28 124283. 0.3474
|
|
30.64 0.4622 0.6815 0.0768 0.0521 0.282 3.552 2.350 210.128 0.401 10.454 5.073 0.28 124602. 0.3260
|
|
32.68 0.4930 0.7013 0.0721 0.0507 0.274 3.456 2.206 204.472 0.391 9.814 4.894 0.28 124937. 0.3047
|
|
34.73 0.5239 0.7184 0.0672 0.0490 0.265 3.340 2.056 197.604 0.377 9.145 4.719 0.28 125288. 0.2836
|
|
36.77 0.5547 0.7327 0.0621 0.0470 0.254 3.204 1.900 189.559 0.362 8.450 4.546 0.28 125655. 0.2626
|
|
38.81 0.5855 0.7440 0.0568 0.0447 0.242 3.049 1.739 180.366 0.344 7.735 4.373 0.28 126039. 0.2417
|
|
40.85 0.6163 0.7519 0.0514 0.0422 0.228 2.875 1.574 170.050 0.325 7.001 4.198 0.28 126438. 0.2208
|
|
42.90 0.6471 0.7558 0.0459 0.0393 0.213 2.682 1.406 158.630 0.303 6.252 4.019 0.28 126854. 0.1997
|
|
44.94 0.6779 0.7548 0.0403 0.0362 0.196 2.470 1.234 146.124 0.279 5.490 3.831 0.28 127286. 0.1784
|
|
46.98 0.7088 0.7475 0.0347 0.0329 0.178 2.241 1.061 132.551 0.253 4.718 3.629 0.28 127733. 0.1567
|
|
49.02 0.7396 0.7316 0.0289 0.0292 0.158 1.994 0.885 117.933 0.225 3.937 3.404 0.29 128197. 0.1342
|
|
51.07 0.7704 0.7028 0.0231 0.0254 0.137 1.729 0.708 102.302 0.195 3.149 3.139 0.29 128676. 0.1107
|
|
53.11 0.8012 0.6534 0.0173 0.0212 0.115 1.449 0.530 85.699 0.164 2.359 2.806 0.29 129171. 0.0856
|
|
55.15 0.8320 0.5667 0.0115 0.0169 0.091 1.153 0.352 68.181 0.130 1.567 2.344 0.29 129681. 0.0583
|
|
57.20 0.8628 0.3997 0.0057 0.0124 0.067 0.842 0.175 49.822 0.095 0.779 1.594 0.29 130207. 0.0280
|
|
59.24 0.8936 -0.0036 0.0000 0.0076 0.041 0.519 -0.001 30.680 0.059 -0.004 -0.014 0.29 130738. 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 0.1163 0.0464 0.434 4.556 5.125 323.421 0.515 22.795 7.187 0.33 145779. 0.6819
|
|
2.45 0.0308 0.0748 0.1152 0.0475 0.444 4.660 5.075 330.778 0.526 22.575 6.959 0.33 145906. 0.6571
|
|
4.91 0.0617 0.1448 0.1139 0.0485 0.453 4.763 5.020 338.135 0.538 22.327 6.733 0.33 146049. 0.6322
|
|
7.36 0.0925 0.2100 0.1125 0.0495 0.463 4.865 4.957 345.358 0.550 22.048 6.510 0.33 146207. 0.6074
|
|
9.81 0.1234 0.2706 0.1109 0.0505 0.472 4.963 4.886 352.309 0.561 21.734 6.291 0.33 146381. 0.5828
|
|
12.27 0.1542 0.3267 0.1091 0.0515 0.481 5.055 4.807 358.833 0.571 21.382 6.076 0.33 146573. 0.5584
|
|
14.72 0.1850 0.3786 0.1071 0.0523 0.489 5.138 4.719 364.766 0.581 20.989 5.868 0.33 146782. 0.5342
|
|
17.17 0.2159 0.4265 0.1048 0.0531 0.496 5.211 4.621 369.933 0.589 20.552 5.665 0.33 147010. 0.5104
|
|
19.63 0.2467 0.4706 0.1024 0.0537 0.502 5.271 4.512 374.155 0.595 20.068 5.469 0.33 147256. 0.4869
|
|
22.08 0.2776 0.5111 0.0996 0.0541 0.506 5.314 4.391 377.245 0.600 19.533 5.280 0.33 147522. 0.4637
|
|
24.53 0.3084 0.5482 0.0966 0.0544 0.508 5.339 4.259 379.012 0.603 18.946 5.097 0.33 147806. 0.4409
|
|
26.98 0.3392 0.5822 0.0934 0.0544 0.509 5.343 4.115 379.258 0.604 18.303 4.921 0.34 148111. 0.4184
|
|
29.44 0.3701 0.6132 0.0898 0.0542 0.507 5.322 3.957 377.782 0.601 17.602 4.751 0.34 148435. 0.3961
|
|
31.89 0.4009 0.6413 0.0859 0.0537 0.502 5.274 3.786 374.389 0.596 16.842 4.587 0.34 148778. 0.3741
|
|
34.34 0.4318 0.6668 0.0817 0.0529 0.495 5.197 3.602 368.911 0.587 16.022 4.429 0.34 149142. 0.3523
|
|
36.80 0.4626 0.6897 0.0773 0.0518 0.484 5.089 3.405 361.259 0.575 15.146 4.275 0.34 149525. 0.3306
|
|
39.25 0.4934 0.7100 0.0725 0.0504 0.471 4.951 3.197 351.432 0.559 14.220 4.126 0.34 149927. 0.3092
|
|
41.70 0.5243 0.7277 0.0676 0.0487 0.455 4.782 2.979 339.480 0.540 13.250 3.980 0.34 150349. 0.2879
|
|
44.16 0.5551 0.7427 0.0625 0.0467 0.436 4.585 2.753 325.462 0.518 12.245 3.836 0.34 150791. 0.2668
|
|
46.61 0.5860 0.7548 0.0572 0.0444 0.415 4.359 2.520 309.430 0.492 11.209 3.694 0.34 151252. 0.2457
|
|
49.06 0.6168 0.7636 0.0518 0.0418 0.391 4.105 2.281 291.425 0.464 10.146 3.550 0.34 151733. 0.2247
|
|
51.52 0.6476 0.7686 0.0462 0.0389 0.364 3.824 2.037 271.481 0.432 9.061 3.403 0.34 152232. 0.2036
|
|
53.97 0.6785 0.7690 0.0406 0.0358 0.335 3.517 1.789 249.630 0.397 7.957 3.250 0.34 152751. 0.1822
|
|
56.42 0.7093 0.7635 0.0349 0.0324 0.303 3.182 1.537 225.904 0.360 6.838 3.086 0.34 153290. 0.1604
|
|
58.88 0.7402 0.7496 0.0291 0.0287 0.269 2.822 1.283 200.343 0.319 5.706 2.904 0.34 153847. 0.1379
|
|
61.33 0.7710 0.7234 0.0233 0.0248 0.232 2.437 1.026 173.001 0.275 4.565 2.691 0.34 154423. 0.1142
|
|
63.78 0.8018 0.6772 0.0174 0.0206 0.193 2.028 0.769 143.953 0.229 3.419 2.422 0.34 155018. 0.0890
|
|
66.24 0.8327 0.5938 0.0116 0.0163 0.152 1.596 0.511 113.297 0.180 2.272 2.045 0.34 155631. 0.0613
|
|
68.69 0.8635 0.4274 0.0058 0.0116 0.109 1.143 0.254 81.168 0.129 1.130 1.419 0.35 156262. 0.0300
|
|
71.14 0.8944 -0.0033 0.0000 0.0068 0.064 0.671 -0.001 47.652 0.076 -0.005 -0.010 0.35 156899. 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 0.1168 0.0461 0.685 6.168 7.004 510.794 0.697 31.154 6.219 0.39 170068. 0.6898
|
|
2.87 0.0309 0.0757 0.1157 0.0472 0.701 6.311 6.938 522.706 0.713 30.860 6.020 0.39 170217. 0.6646
|
|
5.74 0.0618 0.1465 0.1144 0.0483 0.717 6.455 6.863 534.628 0.729 30.528 5.823 0.39 170384. 0.6393
|
|
8.61 0.0927 0.2123 0.1130 0.0494 0.733 6.597 6.779 546.348 0.745 30.153 5.628 0.39 170569. 0.6141
|
|
11.47 0.1236 0.2735 0.1114 0.0504 0.748 6.733 6.684 557.634 0.761 29.730 5.437 0.39 170773. 0.5891
|
|
14.34 0.1546 0.3301 0.1096 0.0513 0.762 6.861 6.577 568.237 0.775 29.255 5.250 0.39 170998. 0.5643
|
|
17.21 0.1855 0.3824 0.1076 0.0522 0.775 6.978 6.457 577.889 0.788 28.723 5.068 0.39 171243. 0.5398
|
|
20.08 0.2164 0.4307 0.1054 0.0530 0.786 7.079 6.324 586.305 0.800 28.129 4.892 0.39 171510. 0.5156
|
|
22.95 0.2473 0.4751 0.1029 0.0536 0.795 7.163 6.176 593.193 0.809 27.470 4.722 0.39 171798. 0.4918
|
|
25.82 0.2782 0.5159 0.1002 0.0540 0.802 7.224 6.012 598.249 0.816 26.741 4.558 0.39 172109. 0.4684
|
|
28.69 0.3091 0.5534 0.0972 0.0543 0.806 7.259 5.832 601.165 0.820 25.939 4.400 0.39 172443. 0.4453
|
|
31.56 0.3400 0.5876 0.0939 0.0543 0.807 7.264 5.634 601.620 0.821 25.060 4.248 0.39 172800. 0.4226
|
|
34.42 0.3709 0.6189 0.0903 0.0541 0.804 7.236 5.418 599.289 0.818 24.101 4.101 0.39 173180. 0.4001
|
|
37.29 0.4019 0.6474 0.0864 0.0536 0.796 7.171 5.184 593.855 0.810 23.060 3.960 0.39 173583. 0.3779
|
|
40.16 0.4328 0.6731 0.0822 0.0529 0.785 7.064 4.931 585.050 0.798 21.935 3.823 0.39 174009. 0.3558
|
|
43.03 0.4637 0.6964 0.0777 0.0517 0.768 6.915 4.661 572.729 0.781 20.732 3.691 0.39 174458. 0.3340
|
|
45.90 0.4946 0.7170 0.0729 0.0503 0.747 6.724 4.375 556.891 0.760 19.461 3.563 0.39 174930. 0.3124
|
|
48.77 0.5255 0.7352 0.0679 0.0486 0.721 6.492 4.076 537.618 0.733 18.130 3.439 0.39 175425. 0.2910
|
|
51.64 0.5564 0.7507 0.0628 0.0465 0.691 6.218 3.765 515.004 0.703 16.748 3.316 0.39 175943. 0.2697
|
|
54.51 0.5873 0.7634 0.0574 0.0442 0.656 5.906 3.445 489.132 0.667 15.325 3.195 0.40 176484. 0.2485
|
|
57.37 0.6182 0.7729 0.0520 0.0416 0.617 5.555 3.117 460.070 0.628 13.865 3.073 0.40 177047. 0.2274
|
|
60.24 0.6492 0.7788 0.0464 0.0387 0.574 5.166 2.782 427.871 0.584 12.374 2.949 0.40 177633. 0.2061
|
|
63.11 0.6801 0.7802 0.0407 0.0355 0.526 4.740 2.441 392.587 0.536 10.857 2.820 0.40 178241. 0.1846
|
|
65.98 0.7110 0.7758 0.0349 0.0320 0.475 4.278 2.095 354.271 0.483 9.318 2.682 0.40 178871. 0.1627
|
|
68.85 0.7419 0.7634 0.0291 0.0283 0.420 3.779 1.745 312.988 0.427 7.763 2.529 0.40 179524. 0.1400
|
|
71.72 0.7728 0.7388 0.0232 0.0243 0.361 3.246 1.393 268.827 0.367 6.195 2.350 0.40 180199. 0.1162
|
|
74.59 0.8037 0.6942 0.0173 0.0200 0.298 2.679 1.039 221.909 0.303 4.620 2.123 0.40 180897. 0.0907
|
|
77.46 0.8346 0.6115 0.0114 0.0156 0.231 2.082 0.684 172.400 0.235 3.045 1.801 0.40 181615. 0.0624
|
|
80.32 0.8655 0.4396 0.0055 0.0109 0.162 1.455 0.332 120.518 0.164 1.475 1.248 0.40 182355. 0.0301
|
|
83.19 0.8965 -0.0478 -0.0003 0.0060 0.089 0.801 -0.019 66.317 0.090 -0.085 -0.131 0.40 183091. 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 0.1173 0.0461 1.021 8.041 9.191 761.034 0.908 40.880 5.478 0.44 194354. 0.6960
|
|
3.27 0.0309 0.0761 0.1162 0.0472 1.045 8.232 9.107 779.123 0.930 40.507 5.302 0.44 194524. 0.6705
|
|
6.55 0.0617 0.1472 0.1150 0.0482 1.069 8.423 9.012 797.250 0.952 40.084 5.127 0.44 194715. 0.6450
|
|
9.82 0.0926 0.2134 0.1136 0.0493 1.093 8.612 8.904 815.086 0.973 39.604 4.955 0.44 194926. 0.6196
|
|
13.10 0.1235 0.2748 0.1121 0.0504 1.116 8.793 8.782 832.287 0.993 39.062 4.786 0.44 195159. 0.5944
|
|
16.37 0.1544 0.3317 0.1103 0.0513 1.138 8.964 8.644 848.471 1.013 38.450 4.621 0.44 195415. 0.5694
|
|
19.65 0.1852 0.3842 0.1084 0.0522 1.158 9.120 8.490 863.230 1.030 37.764 4.461 0.45 195695. 0.5448
|
|
22.92 0.2161 0.4327 0.1062 0.0530 1.175 9.257 8.317 876.133 1.046 36.996 4.306 0.45 195999. 0.5205
|
|
26.19 0.2470 0.4773 0.1037 0.0537 1.189 9.369 8.125 886.734 1.058 36.142 4.156 0.45 196329. 0.4965
|
|
29.47 0.2778 0.5183 0.1010 0.0541 1.200 9.451 7.913 894.577 1.068 35.196 4.012 0.45 196684. 0.4730
|
|
32.74 0.3087 0.5560 0.0980 0.0544 1.206 9.500 7.678 899.195 1.073 34.153 3.873 0.45 197065. 0.4498
|
|
36.02 0.3396 0.5904 0.0947 0.0545 1.207 9.510 7.421 900.107 1.074 33.008 3.739 0.45 197473. 0.4269
|
|
39.29 0.3705 0.6220 0.0911 0.0543 1.203 9.475 7.140 896.824 1.071 31.757 3.611 0.45 197907. 0.4044
|
|
42.57 0.4013 0.6507 0.0872 0.0538 1.192 9.391 6.834 888.866 1.061 30.396 3.487 0.45 198367. 0.3821
|
|
45.84 0.4322 0.6768 0.0830 0.0530 1.175 9.253 6.503 875.827 1.045 28.926 3.368 0.45 198853. 0.3600
|
|
49.11 0.4631 0.7004 0.0785 0.0519 1.150 9.060 6.149 857.477 1.024 27.352 3.253 0.45 199366. 0.3381
|
|
52.39 0.4940 0.7215 0.0737 0.0505 1.118 8.809 5.775 833.810 0.995 25.686 3.141 0.45 199905. 0.3164
|
|
55.66 0.5248 0.7401 0.0687 0.0487 1.079 8.504 5.382 804.944 0.961 23.941 3.033 0.45 200470. 0.2949
|
|
58.94 0.5557 0.7562 0.0635 0.0467 1.034 8.146 4.975 771.023 0.920 22.128 2.927 0.45 201061. 0.2736
|
|
62.21 0.5866 0.7695 0.0581 0.0443 0.982 7.736 4.555 732.175 0.874 20.259 2.822 0.45 201678. 0.2524
|
|
65.49 0.6174 0.7799 0.0526 0.0417 0.923 7.274 4.124 688.503 0.822 18.342 2.717 0.45 202320. 0.2312
|
|
68.76 0.6483 0.7868 0.0470 0.0387 0.858 6.763 3.683 640.090 0.764 16.383 2.610 0.45 202988. 0.2099
|
|
72.03 0.6792 0.7894 0.0413 0.0355 0.787 6.202 3.235 587.011 0.701 14.390 2.500 0.45 203682. 0.1884
|
|
75.31 0.7101 0.7866 0.0355 0.0320 0.710 5.593 2.780 529.348 0.632 12.368 2.382 0.46 204402. 0.1665
|
|
78.58 0.7409 0.7762 0.0296 0.0283 0.627 4.936 2.321 467.197 0.558 10.322 2.253 0.46 205146. 0.1438
|
|
81.86 0.7718 0.7544 0.0237 0.0242 0.537 4.233 1.857 400.691 0.478 8.260 2.102 0.46 205916. 0.1201
|
|
85.13 0.8027 0.7136 0.0178 0.0200 0.443 3.487 1.391 330.010 0.394 6.188 1.912 0.46 206711. 0.0945
|
|
88.41 0.8335 0.6367 0.0118 0.0155 0.342 2.698 0.925 255.401 0.305 4.115 1.643 0.46 207531. 0.0662
|
|
91.68 0.8644 0.4739 0.0059 0.0107 0.238 1.872 0.461 177.190 0.212 2.049 1.179 0.46 208375. 0.0335
|
|
94.96 0.8953 -0.0020 0.0000 0.0058 0.128 1.010 -0.001 95.550 0.114 -0.005 -0.005 0.46 209221. 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 0.1179 0.0461 1.455 10.187 11.692 1084.700 1.151 52.008 4.889 0.50 218636. 0.7007
|
|
3.69 0.0309 0.0764 0.1169 0.0472 1.490 10.434 11.590 1111.002 1.179 51.551 4.732 0.50 218828. 0.6751
|
|
7.37 0.0618 0.1478 0.1157 0.0483 1.525 10.682 11.473 1137.390 1.207 51.030 4.575 0.50 219042. 0.6495
|
|
11.06 0.0927 0.2143 0.1143 0.0494 1.560 10.926 11.339 1163.390 1.234 50.437 4.421 0.50 219279. 0.6239
|
|
14.74 0.1236 0.2760 0.1128 0.0505 1.594 11.162 11.188 1188.493 1.261 49.764 4.270 0.50 219542. 0.5986
|
|
18.43 0.1544 0.3330 0.1111 0.0515 1.626 11.384 11.017 1212.141 1.286 49.002 4.122 0.50 219830. 0.5735
|
|
22.11 0.1853 0.3858 0.1091 0.0524 1.654 11.586 10.824 1233.736 1.309 48.144 3.979 0.50 220145. 0.5487
|
|
25.80 0.2162 0.4344 0.1070 0.0532 1.680 11.764 10.607 1252.646 1.329 47.181 3.841 0.50 220489. 0.5243
|
|
29.48 0.2471 0.4792 0.1045 0.0539 1.701 11.910 10.366 1268.223 1.346 46.106 3.707 0.50 220860. 0.5002
|
|
33.17 0.2780 0.5204 0.1018 0.0544 1.716 12.019 10.097 1279.800 1.358 44.913 3.579 0.50 221261. 0.4766
|
|
36.86 0.3089 0.5582 0.0988 0.0547 1.725 12.084 9.801 1286.700 1.365 43.594 3.455 0.50 221691. 0.4533
|
|
40.54 0.3398 0.5929 0.0955 0.0548 1.728 12.098 9.475 1288.230 1.367 42.144 3.336 0.50 222150. 0.4304
|
|
44.23 0.3707 0.6247 0.0919 0.0546 1.721 12.056 9.118 1283.683 1.362 40.556 3.222 0.50 222640. 0.4077
|
|
47.91 0.4016 0.6536 0.0880 0.0541 1.706 11.949 8.729 1272.367 1.350 38.828 3.112 0.50 223158. 0.3853
|
|
51.60 0.4324 0.6800 0.0838 0.0533 1.681 11.774 8.309 1253.691 1.330 36.958 3.006 0.50 223707. 0.3632
|
|
55.28 0.4633 0.7038 0.0792 0.0522 1.646 11.526 7.858 1227.318 1.302 34.953 2.904 0.51 224285. 0.3412
|
|
58.97 0.4942 0.7253 0.0744 0.0507 1.600 11.206 7.381 1193.234 1.266 32.829 2.806 0.51 224893. 0.3194
|
|
62.66 0.5251 0.7443 0.0694 0.0489 1.544 10.815 6.880 1151.611 1.222 30.602 2.710 0.51 225530. 0.2979
|
|
66.34 0.5560 0.7609 0.0641 0.0469 1.479 10.356 6.360 1102.664 1.170 28.289 2.616 0.51 226196. 0.2765
|
|
70.03 0.5869 0.7748 0.0587 0.0445 1.403 9.829 5.823 1046.578 1.110 25.902 2.524 0.51 226891. 0.2553
|
|
73.71 0.6178 0.7858 0.0532 0.0418 1.319 9.236 5.273 983.505 1.044 23.453 2.432 0.51 227615. 0.2340
|
|
77.40 0.6487 0.7934 0.0475 0.0388 1.225 8.580 4.710 913.570 0.969 20.950 2.338 0.51 228369. 0.2127
|
|
81.08 0.6796 0.7970 0.0417 0.0356 1.122 7.859 4.137 836.880 0.888 18.401 2.242 0.51 229150. 0.1911
|
|
84.77 0.7104 0.7953 0.0359 0.0320 1.011 7.077 3.556 753.551 0.800 15.815 2.140 0.51 229961. 0.1691
|
|
88.45 0.7413 0.7864 0.0299 0.0282 0.890 6.233 2.967 663.728 0.704 13.199 2.028 0.51 230800. 0.1464
|
|
92.14 0.7722 0.7664 0.0239 0.0241 0.761 5.331 2.374 567.598 0.602 10.561 1.897 0.51 231667. 0.1225
|
|
95.83 0.8031 0.7280 0.0179 0.0198 0.624 4.371 1.778 465.424 0.494 7.910 1.733 0.52 232563. 0.0969
|
|
99.51 0.8340 0.6539 0.0119 0.0152 0.480 3.358 1.182 357.564 0.379 5.256 1.499 0.52 233486. 0.0683
|
|
103.20 0.8649 0.4928 0.0059 0.0104 0.328 2.296 0.587 244.495 0.259 2.612 1.089 0.52 234436. 0.0350
|
|
106.88 0.8958 -0.0068 0.0000 0.0054 0.170 1.187 -0.004 126.417 0.134 -0.018 -0.014 0.52 235385. 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 0.1186 0.0463 2.002 12.621 14.518 1493.223 1.426 64.577 4.410 0.56 242914. 0.7043
|
|
4.10 0.0309 0.0766 0.1176 0.0474 2.052 12.933 14.397 1530.153 1.461 64.036 4.267 0.56 243126. 0.6786
|
|
8.19 0.0618 0.1482 0.1165 0.0486 2.102 13.247 14.257 1567.262 1.497 63.415 4.126 0.56 243364. 0.6529
|
|
12.29 0.0927 0.2148 0.1152 0.0497 2.151 13.556 14.097 1603.878 1.532 62.705 3.987 0.56 243628. 0.6274
|
|
16.39 0.1236 0.2766 0.1137 0.0508 2.198 13.856 13.915 1639.284 1.565 61.894 3.850 0.56 243919. 0.6019
|
|
20.48 0.1545 0.3338 0.1120 0.0518 2.243 14.138 13.708 1672.684 1.597 60.973 3.717 0.56 244240. 0.5768
|
|
24.58 0.1854 0.3866 0.1101 0.0528 2.284 14.396 13.474 1703.232 1.626 59.930 3.588 0.56 244591. 0.5520
|
|
28.68 0.2163 0.4354 0.1079 0.0536 2.320 14.623 13.209 1730.032 1.652 58.755 3.463 0.56 244973. 0.5275
|
|
32.77 0.2472 0.4803 0.1055 0.0543 2.350 14.810 12.913 1752.165 1.673 57.439 3.343 0.56 245387. 0.5035
|
|
36.87 0.2781 0.5216 0.1028 0.0548 2.372 14.949 12.584 1768.696 1.689 55.973 3.227 0.56 245833. 0.4798
|
|
40.97 0.3090 0.5596 0.0998 0.0551 2.385 15.034 12.219 1778.677 1.699 54.348 3.116 0.56 246312. 0.4565
|
|
45.06 0.3399 0.5944 0.0965 0.0552 2.389 15.055 11.816 1781.138 1.701 52.558 3.009 0.56 246824. 0.4335
|
|
49.16 0.3708 0.6264 0.0929 0.0550 2.380 15.004 11.375 1775.096 1.695 50.594 2.906 0.56 247369. 0.4108
|
|
53.26 0.4017 0.6556 0.0890 0.0545 2.360 14.873 10.893 1759.594 1.680 48.452 2.808 0.56 247947. 0.3884
|
|
57.35 0.4326 0.6822 0.0847 0.0537 2.325 14.655 10.371 1733.802 1.656 46.131 2.713 0.56 248557. 0.3662
|
|
61.45 0.4635 0.7063 0.0801 0.0526 2.276 14.345 9.811 1697.239 1.621 43.639 2.622 0.56 249201. 0.3442
|
|
65.55 0.4944 0.7281 0.0753 0.0511 2.213 13.945 9.217 1649.882 1.576 40.996 2.534 0.56 249878. 0.3224
|
|
69.64 0.5253 0.7475 0.0702 0.0493 2.135 13.456 8.593 1591.975 1.520 38.223 2.448 0.56 250587. 0.3008
|
|
73.74 0.5562 0.7645 0.0649 0.0472 2.043 12.880 7.945 1523.820 1.455 35.340 2.365 0.56 251329. 0.2794
|
|
77.84 0.5871 0.7789 0.0594 0.0448 1.939 12.219 7.276 1445.689 1.381 32.363 2.283 0.56 252103. 0.2581
|
|
81.93 0.6180 0.7906 0.0538 0.0421 1.821 11.476 6.589 1357.799 1.297 29.306 2.201 0.57 252909. 0.2368
|
|
86.03 0.6489 0.7989 0.0481 0.0391 1.690 10.653 5.886 1260.323 1.204 26.182 2.118 0.57 253747. 0.2154
|
|
90.13 0.6798 0.8034 0.0422 0.0357 1.547 9.749 5.171 1153.417 1.101 23.000 2.033 0.57 254617. 0.1938
|
|
94.22 0.7107 0.8028 0.0363 0.0321 1.391 8.767 4.445 1037.243 0.990 19.770 1.944 0.57 255519. 0.1717
|
|
98.32 0.7416 0.7952 0.0303 0.0283 1.223 7.708 3.710 911.999 0.871 16.501 1.845 0.57 256452. 0.1489
|
|
102.42 0.7725 0.7770 0.0242 0.0241 1.043 6.575 2.968 777.950 0.743 13.203 1.731 0.57 257417. 0.1250
|
|
106.51 0.8034 0.7409 0.0182 0.0197 0.852 5.371 2.223 635.461 0.607 9.888 1.587 0.57 258413. 0.0992
|
|
110.61 0.8343 0.6697 0.0121 0.0150 0.650 4.100 1.477 485.032 0.463 6.569 1.381 0.57 259439. 0.0703
|
|
114.71 0.8652 0.5109 0.0060 0.0101 0.439 2.767 0.733 327.334 0.313 3.261 1.016 0.58 260496. 0.0365
|
|
118.80 0.8961 -0.0099 -0.0001 0.0050 0.218 1.374 -0.007 162.582 0.155 -0.030 -0.019 0.58 261547. 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 0.1193 0.0465 2.681 15.362 17.678 1999.285 1.736 78.632 4.011 0.61 267187. 0.7067
|
|
4.53 0.0311 0.0771 0.1184 0.0477 2.749 15.752 17.537 2049.985 1.780 78.006 3.880 0.61 267421. 0.6810
|
|
9.06 0.0622 0.1491 0.1173 0.0489 2.818 16.144 17.375 2101.042 1.824 77.284 3.751 0.61 267683. 0.6553
|
|
13.60 0.0932 0.2160 0.1160 0.0501 2.885 16.532 17.188 2151.509 1.868 76.451 3.623 0.61 267975. 0.6296
|
|
18.13 0.1243 0.2781 0.1146 0.0512 2.951 16.907 16.973 2200.363 1.910 75.494 3.499 0.61 268298. 0.6041
|
|
22.66 0.1554 0.3355 0.1129 0.0523 3.013 17.262 16.726 2246.494 1.950 74.399 3.377 0.61 268654. 0.5789
|
|
27.19 0.1865 0.3886 0.1110 0.0533 3.069 17.586 16.446 2288.698 1.987 73.152 3.259 0.61 269044. 0.5540
|
|
31.73 0.2176 0.4375 0.1089 0.0541 3.119 17.870 16.128 2325.720 2.019 71.739 3.145 0.61 269468. 0.5294
|
|
36.26 0.2486 0.4826 0.1065 0.0549 3.160 18.105 15.771 2356.269 2.046 70.148 3.036 0.61 269928. 0.5053
|
|
40.79 0.2797 0.5240 0.1038 0.0554 3.190 18.280 15.370 2379.036 2.065 68.367 2.930 0.61 270425. 0.4815
|
|
45.32 0.3108 0.5622 0.1008 0.0557 3.209 18.385 14.925 2392.703 2.077 66.388 2.829 0.61 270957. 0.4581
|
|
49.86 0.3419 0.5972 0.0974 0.0558 3.213 18.410 14.433 2395.937 2.080 64.199 2.732 0.61 271527. 0.4351
|
|
54.39 0.3729 0.6293 0.0938 0.0556 3.202 18.344 13.892 2387.390 2.073 61.791 2.639 0.62 272134. 0.4123
|
|
58.92 0.4040 0.6587 0.0898 0.0551 3.173 18.178 13.300 2365.751 2.054 59.160 2.550 0.62 272777. 0.3898
|
|
63.45 0.4351 0.6855 0.0855 0.0542 3.124 17.903 12.658 2329.896 2.023 56.304 2.464 0.62 273457. 0.3675
|
|
67.98 0.4662 0.7099 0.0808 0.0531 3.056 17.513 11.968 2279.198 1.979 53.234 2.382 0.62 274174. 0.3453
|
|
72.52 0.4973 0.7319 0.0758 0.0515 2.969 17.009 11.236 2213.654 1.922 49.976 2.302 0.62 274927. 0.3234
|
|
77.05 0.5283 0.7516 0.0707 0.0497 2.861 16.394 10.467 2133.626 1.852 46.555 2.225 0.62 275716. 0.3017
|
|
81.58 0.5594 0.7689 0.0653 0.0475 2.735 15.672 9.667 2039.545 1.771 42.997 2.150 0.62 276541. 0.2801
|
|
86.11 0.5905 0.7836 0.0597 0.0450 2.591 14.844 8.841 1931.793 1.677 39.323 2.076 0.62 277402. 0.2587
|
|
90.65 0.6216 0.7956 0.0540 0.0422 2.428 13.913 7.992 1810.671 1.572 35.550 2.002 0.62 278299. 0.2372
|
|
95.18 0.6527 0.8044 0.0481 0.0390 2.248 12.881 7.125 1676.421 1.455 31.692 1.928 0.62 279232. 0.2157
|
|
99.71 0.6837 0.8092 0.0421 0.0356 2.051 11.751 6.241 1529.259 1.328 27.762 1.851 0.63 280199. 0.1938
|
|
104.24 0.7148 0.8090 0.0361 0.0319 1.836 10.522 5.344 1369.415 1.189 23.772 1.770 0.63 281202. 0.1715
|
|
108.78 0.7459 0.8016 0.0300 0.0279 1.605 9.199 4.437 1197.168 1.039 19.734 1.681 0.63 282240. 0.1484
|
|
113.31 0.7770 0.7832 0.0238 0.0236 1.358 7.783 3.521 1012.896 0.879 15.661 1.577 0.63 283313. 0.1240
|
|
117.84 0.8080 0.7457 0.0176 0.0190 1.096 6.279 2.600 817.125 0.709 11.567 1.443 0.63 284420. 0.0976
|
|
122.37 0.8391 0.6691 0.0113 0.0142 0.819 4.692 1.679 610.576 0.530 7.468 1.247 0.63 285562. 0.0677
|
|
126.91 0.8702 0.4871 0.0051 0.0092 0.529 3.029 0.761 394.209 0.342 3.385 0.876 0.63 286735. 0.0320
|
|
131.44 0.9013
|
|
|
|
|
|
|
|
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 0.1201 0.0470 3.518 18.477 21.181 2623.287 2.088 94.214 3.662 0.67 291454. 0.7064
|
|
4.92 0.0309 0.0764 0.1193 0.0482 3.607 18.944 21.026 2689.625 2.140 93.523 3.546 0.67 291706. 0.6814
|
|
9.83 0.0618 0.1479 0.1182 0.0494 3.697 19.416 20.845 2756.631 2.194 92.719 3.430 0.67 291990. 0.6563
|
|
14.75 0.0927 0.2144 0.1171 0.0506 3.786 19.884 20.635 2823.074 2.247 91.785 3.315 0.67 292305. 0.6312
|
|
19.67 0.1236 0.2762 0.1157 0.0518 3.872 20.339 20.392 2887.645 2.298 90.704 3.203 0.67 292655. 0.6062
|
|
24.58 0.1545 0.3334 0.1141 0.0529 3.955 20.771 20.112 2948.895 2.347 89.457 3.093 0.67 293040. 0.5814
|
|
29.50 0.1854 0.3863 0.1123 0.0539 4.030 21.167 19.790 3005.236 2.391 88.028 2.987 0.67 293462. 0.5569
|
|
34.42 0.2163 0.4351 0.1102 0.0548 4.097 21.518 19.424 3055.004 2.431 86.399 2.884 0.67 293921. 0.5327
|
|
39.33 0.2472 0.4801 0.1078 0.0555 4.152 21.810 19.010 3096.463 2.464 84.554 2.785 0.67 294419. 0.5088
|
|
44.25 0.2781 0.5216 0.1052 0.0561 4.195 22.031 18.543 3127.844 2.489 82.481 2.689 0.67 294957. 0.4853
|
|
49.17 0.3090 0.5598 0.1022 0.0564 4.221 22.169 18.023 3147.377 2.505 80.165 2.597 0.67 295534. 0.4621
|
|
54.08 0.3400 0.5950 0.0990 0.0565 4.229 22.210 17.445 3153.278 2.509 77.596 2.509 0.67 296151. 0.4393
|
|
59.00 0.3709 0.6272 0.0953 0.0564 4.216 22.143 16.808 3143.782 2.502 74.762 2.425 0.67 296808. 0.4167
|
|
63.92 0.4018 0.6568 0.0914 0.0559 4.180 21.956 16.110 3117.183 2.481 71.657 2.344 0.67 297505. 0.3943
|
|
68.83 0.4327 0.6839 0.0871 0.0551 4.120 21.638 15.350 3071.990 2.445 68.278 2.266 0.67 298241. 0.3722
|
|
73.75 0.4636 0.7086 0.0824 0.0539 4.033 21.182 14.532 3007.294 2.393 64.639 2.192 0.67 299017. 0.3502
|
|
78.67 0.4945 0.7311 0.0775 0.0524 3.920 20.588 13.661 2923.022 2.326 60.765 2.120 0.67 299832. 0.3284
|
|
83.58 0.5254 0.7512 0.0723 0.0506 3.781 19.860 12.745 2819.625 2.244 56.690 2.050 0.68 300687. 0.3068
|
|
88.50 0.5563 0.7691 0.0669 0.0484 3.618 19.001 11.791 2697.693 2.147 52.445 1.982 0.68 301580. 0.2853
|
|
93.42 0.5872 0.7846 0.0613 0.0459 3.430 18.016 10.804 2557.760 2.035 48.055 1.916 0.68 302511. 0.2639
|
|
98.33 0.6181 0.7974 0.0555 0.0430 3.219 16.906 9.789 2400.249 1.910 43.542 1.850 0.68 303481. 0.2426
|
|
103.25 0.6490 0.8073 0.0496 0.0399 2.984 15.675 8.751 2225.490 1.771 38.923 1.783 0.68 304489. 0.2211
|
|
108.17 0.6799 0.8135 0.0436 0.0365 2.727 14.325 7.692 2033.767 1.618 34.214 1.715 0.68 305536. 0.1994
|
|
113.08 0.7108 0.8150 0.0375 0.0327 2.448 12.857 6.616 1825.379 1.453 29.429 1.644 0.68 306620. 0.1772
|
|
118.00 0.7417 0.8101 0.0313 0.0287 2.147 11.274 5.526 1600.675 1.274 24.581 1.566 0.68 307742. 0.1543
|
|
122.92 0.7726 0.7954 0.0251 0.0244 1.824 9.580 4.426 1360.127 1.082 19.687 1.476 0.69 308901. 0.1301
|
|
127.83 0.8035 0.7639 0.0188 0.0198 1.481 7.779 3.319 1104.394 0.879 14.763 1.363 0.69 310097. 0.1041
|
|
132.75 0.8344 0.6990 0.0125 0.0150 1.119 5.877 2.210 834.448 0.664 9.828 1.201 0.69 311330. 0.0748
|
|
137.67 0.8653 0.5473 0.0063 0.0099 0.740 3.885 1.103 551.629 0.439 4.906 0.907 0.69 312599. 0.0399
|
|
142.58 0.8962 0.0006 0.0000 0.0046 0.344 1.807 0.001 256.478 0.204 0.002 0.001 0.69 313857. 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 0.1210 0.0482 4.586 22.236 25.034 3419.948 2.512 111.350 3.320 0.72 315714. 0.6962
|
|
5.33 0.0309 0.0752 0.1202 0.0494 4.698 22.778 24.867 3503.375 2.573 110.609 3.219 0.72 315987. 0.6729
|
|
10.66 0.0618 0.1457 0.1192 0.0506 4.811 23.325 24.671 3587.571 2.635 109.738 3.119 0.72 316292. 0.6493
|
|
15.98 0.0927 0.2116 0.1181 0.0518 4.923 23.868 24.441 3670.956 2.697 108.716 3.020 0.72 316633. 0.6257
|
|
21.31 0.1236 0.2730 0.1168 0.0529 5.031 24.394 24.172 3751.853 2.756 107.519 2.922 0.72 317011. 0.6022
|
|
26.64 0.1546 0.3301 0.1153 0.0540 5.134 24.891 23.859 3828.424 2.812 106.125 2.827 0.72 317428. 0.5787
|
|
31.97 0.1855 0.3831 0.1136 0.0550 5.228 25.348 23.496 3898.712 2.864 104.512 2.734 0.72 317885. 0.5553
|
|
37.29 0.2164 0.4321 0.1115 0.0559 5.311 25.751 23.079 3960.649 2.909 102.656 2.643 0.72 318383. 0.5322
|
|
42.62 0.2473 0.4775 0.1092 0.0566 5.380 26.085 22.603 4012.084 2.947 100.540 2.555 0.72 318924. 0.5092
|
|
47.95 0.2782 0.5193 0.1066 0.0571 5.432 26.337 22.065 4050.813 2.976 98.143 2.471 0.72 319508. 0.4864
|
|
53.28 0.3091 0.5579 0.1037 0.0575 5.464 26.492 21.459 4074.585 2.993 95.451 2.389 0.73 320135. 0.4638
|
|
58.60 0.3400 0.5935 0.1005 0.0576 5.473 26.534 20.784 4081.132 2.998 92.449 2.310 0.73 320805. 0.4414
|
|
63.93 0.3709 0.6261 0.0968 0.0574 5.455 26.450 20.037 4068.140 2.988 89.124 2.234 0.73 321519. 0.4191
|
|
69.26 0.4019 0.6561 0.0929 0.0569 5.409 26.224 19.215 4033.326 2.963 85.468 2.161 0.73 322276. 0.3970
|
|
74.59 0.4328 0.6835 0.0885 0.0561 5.330 25.842 18.318 3974.635 2.920 81.479 2.090 0.73 323077. 0.3750
|
|
79.92 0.4637 0.7086 0.0839 0.0549 5.218 25.296 17.349 3890.727 2.858 77.170 2.023 0.73 323920. 0.3531
|
|
85.24 0.4946 0.7314 0.0789 0.0533 5.071 24.585 16.316 3781.338 2.778 72.575 1.957 0.73 324806. 0.3313
|
|
90.57 0.5255 0.7520 0.0736 0.0514 4.891 23.711 15.228 3646.954 2.679 67.733 1.894 0.73 325734. 0.3097
|
|
95.90 0.5564 0.7703 0.0681 0.0492 4.678 22.680 14.092 3488.359 2.562 62.682 1.832 0.73 326704. 0.2883
|
|
101.23 0.5873 0.7863 0.0624 0.0466 4.434 21.497 12.916 3306.281 2.429 57.452 1.772 0.73 327715. 0.2669
|
|
106.55 0.6182 0.7998 0.0566 0.0437 4.159 20.164 11.707 3101.295 2.278 52.072 1.712 0.74 328768. 0.2455
|
|
111.88 0.6492 0.8103 0.0506 0.0405 3.854 18.685 10.468 2873.856 2.111 46.561 1.652 0.74 329862. 0.2240
|
|
117.21 0.6801 0.8174 0.0445 0.0370 3.519 17.063 9.204 2624.329 1.928 40.938 1.591 0.74 330998. 0.2023
|
|
122.54 0.7110 0.8199 0.0383 0.0332 3.156 15.299 7.918 2353.143 1.729 35.221 1.526 0.74 332174. 0.1800
|
|
127.87 0.7419 0.8162 0.0320 0.0291 2.764 13.399 6.616 2060.886 1.514 29.426 1.456 0.74 333391. 0.1570
|
|
133.19 0.7728 0.8027 0.0256 0.0247 2.345 11.368 5.299 1748.390 1.284 23.571 1.375 0.74 334648. 0.1326
|
|
138.52 0.8037 0.7725 0.0192 0.0200 1.900 9.212 3.974 1416.855 1.041 17.675 1.272 0.75 335946. 0.1063
|
|
143.85 0.8346 0.7082 0.0128 0.0151 1.432 6.944 2.644 1067.971 0.784 11.762 1.123 0.75 337283. 0.0765
|
|
149.18 0.8655 0.5549 0.0064 0.0099 0.944 4.577 1.317 704.006 0.517 5.858 0.849 0.75 338658. 0.0408
|
|
154.50 0.8965 -0.0065 0.0000 0.0046 0.437 2.120 -0.007 326.124 0.240 -0.031 -0.010 0.75 340016. 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 0.1218 0.0509 6.046 27.217 29.232 4508.183 3.075 130.026 2.941 0.78 339969. 0.6665
|
|
5.74 0.0309 0.0719 0.1211 0.0520 6.181 27.828 29.061 4609.286 3.144 129.263 2.860 0.78 340260. 0.6461
|
|
11.47 0.0618 0.1398 0.1203 0.0532 6.317 28.440 28.857 4710.663 3.213 128.356 2.779 0.78 340587. 0.6256
|
|
17.21 0.0927 0.2036 0.1193 0.0543 6.451 29.040 28.615 4810.138 3.281 127.279 2.698 0.78 340952. 0.6049
|
|
22.95 0.1236 0.2635 0.1181 0.0554 6.578 29.616 28.328 4905.429 3.346 126.002 2.619 0.78 341357. 0.5843
|
|
28.68 0.1545 0.3196 0.1166 0.0564 6.697 30.151 27.989 4994.143 3.406 124.493 2.542 0.78 341805. 0.5636
|
|
34.42 0.1854 0.3722 0.1150 0.0573 6.804 30.632 27.591 5073.860 3.461 122.723 2.466 0.78 342296. 0.5430
|
|
40.16 0.2164 0.4213 0.1131 0.0581 6.896 31.045 27.128 5142.143 3.507 120.666 2.393 0.78 342833. 0.5224
|
|
45.89 0.2473 0.4670 0.1108 0.0587 6.969 31.373 26.595 5196.560 3.545 118.293 2.321 0.78 343416. 0.5017
|
|
51.63 0.2782 0.5096 0.1083 0.0591 7.020 31.603 25.985 5234.632 3.571 115.583 2.252 0.78 344045. 0.4810
|
|
57.37 0.3091 0.5492 0.1054 0.0593 7.045 31.719 25.295 5253.827 3.584 112.514 2.184 0.78 344722. 0.4603
|
|
63.10 0.3400 0.5859 0.1022 0.0593 7.042 31.705 24.521 5251.563 3.582 109.068 2.118 0.78 345446. 0.4395
|
|
68.84 0.3709 0.6198 0.0986 0.0590 7.007 31.546 23.658 5225.223 3.564 105.231 2.054 0.78 346217. 0.4186
|
|
74.58 0.4018 0.6510 0.0946 0.0584 6.936 31.226 22.705 5172.175 3.528 100.990 1.991 0.78 347035. 0.3976
|
|
80.31 0.4327 0.6796 0.0903 0.0575 6.826 30.730 21.660 5089.981 3.472 96.345 1.930 0.78 347899. 0.3765
|
|
86.05 0.4636 0.7058 0.0856 0.0562 6.674 30.048 20.528 4976.992 3.395 91.311 1.871 0.79 348810. 0.3553
|
|
91.79 0.4945 0.7296 0.0805 0.0546 6.481 29.177 19.318 4832.772 3.296 85.926 1.813 0.79 349766. 0.3340
|
|
97.52 0.5254 0.7510 0.0752 0.0526 6.246 28.120 18.039 4657.761 3.177 80.239 1.757 0.79 350768. 0.3127
|
|
103.26 0.5563 0.7702 0.0696 0.0503 5.971 26.882 16.703 4452.693 3.037 74.294 1.701 0.79 351815. 0.2914
|
|
109.00 0.5872 0.7870 0.0638 0.0476 5.657 25.467 15.317 4218.257 2.877 68.130 1.647 0.79 352907. 0.2701
|
|
114.73 0.6182 0.8012 0.0579 0.0447 5.304 23.878 13.889 3955.017 2.698 61.779 1.593 0.79 354043. 0.2488
|
|
120.47 0.6491 0.8124 0.0518 0.0414 4.913 22.118 12.426 3663.627 2.499 55.269 1.538 0.79 355223. 0.2273
|
|
126.21 0.6800 0.8202 0.0456 0.0378 4.485 20.193 10.931 3344.641 2.281 48.621 1.482 0.80 356448. 0.2054
|
|
131.94 0.7109 0.8232 0.0392 0.0339 4.022 18.106 9.410 2998.952 2.046 41.854 1.423 0.80 357716. 0.1830
|
|
137.68 0.7418 0.8195 0.0328 0.0297 3.524 15.865 7.866 2627.865 1.792 34.988 1.358 0.80 359028. 0.1596
|
|
143.42 0.7727 0.8051 0.0263 0.0252 2.995 13.482 6.305 2233.192 1.523 28.043 1.281 0.80 360383. 0.1348
|
|
149.15 0.8036 0.7720 0.0197 0.0205 2.437 10.972 4.731 1817.296 1.240 21.042 1.181 0.80 361781. 0.1076
|
|
154.89 0.8345 0.7013 0.0131 0.0156 1.855 8.351 3.150 1383.271 0.944 14.010 1.033 0.80 363221. 0.0768
|
|
160.63 0.8654 0.5359 0.0065 0.0106 1.254 5.645 1.569 935.020 0.638 6.978 0.761 0.81 364702. 0.0400
|
|
166.36 0.8963 -0.0068 0.0000 0.0054 0.637 2.869 -0.010 475.185 0.324 -0.043 -0.009 0.81 366168. 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 0.1225 0.0560 8.176 34.354 33.753 6096.666 3.881 150.134 2.511 0.83 364216. 0.6114
|
|
6.15 0.0309 0.0660 0.1219 0.0571 8.338 35.034 33.583 6217.392 3.958 149.379 2.450 0.83 364524. 0.5951
|
|
12.30 0.0618 0.1288 0.1212 0.0582 8.498 35.709 33.380 6337.230 4.034 148.474 2.389 0.83 364872. 0.5785
|
|
18.45 0.0928 0.1884 0.1203 0.0592 8.653 36.361 33.135 6452.882 4.108 147.386 2.329 0.83 365260. 0.5619
|
|
24.60 0.1237 0.2448 0.1192 0.0602 8.798 36.969 32.841 6560.865 4.177 146.076 2.270 0.83 365692. 0.5453
|
|
30.74 0.1546 0.2983 0.1179 0.0611 8.928 37.514 32.487 6657.610 4.238 144.503 2.213 0.83 366170. 0.5287
|
|
36.89 0.1855 0.3490 0.1164 0.0619 9.038 37.977 32.066 6739.678 4.291 142.628 2.158 0.83 366695. 0.5122
|
|
43.04 0.2164 0.3971 0.1146 0.0625 9.124 38.339 31.568 6803.907 4.332 140.413 2.104 0.83 367270. 0.4955
|
|
49.19 0.2474 0.4426 0.1125 0.0629 9.183 38.584 30.985 6847.491 4.359 137.821 2.052 0.84 367895. 0.4788
|
|
55.34 0.2783 0.4856 0.1100 0.0631 9.210 38.700 30.311 6868.082 4.372 134.825 2.002 0.84 368571. 0.4619
|
|
61.49 0.3092 0.5262 0.1072 0.0630 9.204 38.674 29.541 6863.406 4.369 131.397 1.952 0.84 369299. 0.4447
|
|
67.64 0.3401 0.5644 0.1041 0.0627 9.161 38.492 28.668 6831.113 4.349 127.514 1.903 0.84 370077. 0.4272
|
|
73.79 0.3710 0.6002 0.1005 0.0621 9.077 38.140 27.688 6768.622 4.309 123.157 1.855 0.84 370907. 0.4092
|
|
79.94 0.4020 0.6335 0.0966 0.0613 8.949 37.602 26.599 6673.218 4.248 118.311 1.808 0.84 371787. 0.3908
|
|
86.08 0.4329 0.6645 0.0922 0.0601 8.774 36.866 25.398 6542.503 4.165 112.972 1.761 0.84 372718. 0.3719
|
|
92.23 0.4638 0.6931 0.0875 0.0585 8.549 35.922 24.091 6374.980 4.058 107.158 1.714 0.84 373698. 0.3526
|
|
98.38 0.4947 0.7193 0.0824 0.0567 8.275 34.771 22.688 6170.674 3.928 100.916 1.668 0.84 374727. 0.3329
|
|
104.53 0.5256 0.7431 0.0770 0.0544 7.953 33.417 21.201 5930.497 3.775 94.303 1.621 0.84 375805. 0.3129
|
|
110.68 0.5566 0.7644 0.0713 0.0519 7.584 31.867 19.643 5655.424 3.600 87.374 1.575 0.85 376931. 0.2926
|
|
116.83 0.5875 0.7833 0.0654 0.0491 7.169 30.124 18.025 5346.100 3.403 80.175 1.529 0.85 378105. 0.2721
|
|
122.98 0.6184 0.7994 0.0594 0.0459 6.709 28.191 16.355 5002.987 3.185 72.745 1.483 0.85 379326. 0.2513
|
|
129.13 0.6493 0.8120 0.0531 0.0425 6.208 26.085 14.639 4629.157 2.947 65.115 1.434 0.85 380595. 0.2300
|
|
135.28 0.6802 0.8196 0.0468 0.0388 5.671 23.828 12.884 4228.676 2.692 57.309 1.382 0.85 381910. 0.2079
|
|
141.43 0.7112 0.8210 0.0403 0.0349 5.097 21.416 11.096 3800.563 2.420 49.353 1.324 0.85 383272. 0.1849
|
|
147.57 0.7421 0.8138 0.0337 0.0307 4.487 18.853 9.279 3345.737 2.130 41.272 1.258 0.86 384680. 0.1606
|
|
153.72 0.7730 0.7930 0.0270 0.0263 3.845 16.158 7.439 2867.501 1.826 33.088 1.177 0.86 386135. 0.1345
|
|
159.87 0.8039 0.7486 0.0203 0.0218 3.179 13.356 5.582 2370.345 1.509 24.829 1.068 0.86 387635. 0.1058
|
|
166.02 0.8348 0.6596 0.0135 0.0171 2.494 10.478 3.716 1859.519 1.184 16.527 0.906 0.86 389181. 0.0732
|
|
172.17 0.8658 0.4720 0.0067 0.0123 1.799 7.557 1.849 1341.142 0.854 8.224 0.625 0.86 390769. 0.0356
|
|
178.32 0.8967 -0.0053 0.0000 0.0075 1.099 4.618 -0.012 819.622 0.522 -0.054 -0.007 0.87 392358. 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 0.1223 0.0626 11.102 43.734 38.343 8278.830 4.941 170.549 2.101 0.89 388491. 0.5452
|
|
6.57 0.0310 0.0592 0.1218 0.0638 11.302 44.523 38.182 8428.186 5.030 169.836 2.055 0.89 388817. 0.5322
|
|
13.15 0.0620 0.1158 0.1212 0.0649 11.503 45.312 37.991 8577.504 5.119 168.982 2.009 0.89 389183. 0.5190
|
|
19.72 0.0930 0.1698 0.1205 0.0660 11.696 46.073 37.758 8721.536 5.205 167.948 1.964 0.89 389593. 0.5057
|
|
26.30 0.1240 0.2213 0.1196 0.0670 11.875 46.780 37.475 8855.410 5.285 166.689 1.919 0.89 390049. 0.4925
|
|
32.87 0.1550 0.2705 0.1185 0.0679 12.034 47.404 37.130 8973.616 5.356 165.155 1.877 0.89 390554. 0.4793
|
|
39.45 0.1860 0.3175 0.1171 0.0686 12.163 47.914 36.712 9070.101 5.413 163.293 1.836 0.89 391111. 0.4662
|
|
46.02 0.2170 0.3625 0.1155 0.0691 12.256 48.278 36.207 9139.036 5.454 161.049 1.797 0.89 391721. 0.4532
|
|
52.60 0.2479 0.4058 0.1136 0.0694 12.304 48.471 35.605 9175.417 5.476 158.370 1.760 0.89 392387. 0.4402
|
|
59.17 0.2789 0.4474 0.1113 0.0694 12.304 48.470 34.895 9175.405 5.476 155.212 1.725 0.89 393108. 0.4271
|
|
65.74 0.3099 0.4875 0.1087 0.0691 12.252 48.263 34.068 9136.221 5.453 151.535 1.691 0.89 393886. 0.4137
|
|
72.32 0.3409 0.5259 0.1057 0.0685 12.144 47.838 33.117 9055.736 5.405 147.305 1.659 0.89 394720. 0.4001
|
|
78.89 0.3719 0.5626 0.1022 0.0676 11.978 47.185 32.036 8932.107 5.331 142.496 1.627 0.89 395609. 0.3859
|
|
85.47 0.4029 0.5977 0.0983 0.0663 11.752 46.296 30.820 8763.721 5.230 137.088 1.595 0.90 396554. 0.3711
|
|
92.04 0.4339 0.6308 0.0940 0.0647 11.465 45.164 29.469 8549.446 5.103 131.076 1.563 0.90 397554. 0.3557
|
|
98.62 0.4649 0.6621 0.0893 0.0627 11.116 43.788 27.986 8289.035 4.947 124.482 1.531 0.90 398607. 0.3395
|
|
105.19 0.4959 0.6912 0.0842 0.0604 10.706 42.173 26.383 7983.326 4.765 117.353 1.499 0.90 399713. 0.3227
|
|
111.76 0.5269 0.7183 0.0787 0.0578 10.238 40.331 24.677 7634.570 4.557 109.761 1.466 0.90 400872. 0.3052
|
|
118.34 0.5579 0.7431 0.0730 0.0548 9.716 38.274 22.881 7245.156 4.324 101.773 1.432 0.90 402082. 0.2872
|
|
124.91 0.5889 0.7654 0.0670 0.0516 9.142 36.013 21.009 6817.209 4.069 93.448 1.398 0.90 403344. 0.2685
|
|
131.49 0.6199 0.7851 0.0609 0.0481 8.518 33.556 19.073 6352.028 3.791 84.836 1.362 0.91 404656. 0.2493
|
|
138.06 0.6509 0.8013 0.0545 0.0443 7.847 30.913 17.081 5851.844 3.493 75.976 1.324 0.91 406018. 0.2293
|
|
144.64 0.6819 0.8107 0.0480 0.0404 7.154 28.180 15.038 5334.396 3.184 66.887 1.279 0.91 407430. 0.2078
|
|
151.21 0.7129 0.8065 0.0413 0.0365 6.471 25.492 12.944 4825.662 2.880 57.574 1.217 0.91 408892. 0.1835
|
|
157.79 0.7438 0.7901 0.0345 0.0325 5.759 22.688 10.815 4294.739 2.563 48.104 1.142 0.91 410404. 0.1574
|
|
164.36 0.7748 0.7550 0.0276 0.0283 5.026 19.797 8.658 3747.610 2.237 38.510 1.048 0.92 411964. 0.1292
|
|
170.93 0.8058 0.6904 0.0207 0.0241 4.280 16.858 6.482 3191.293 1.905 28.832 0.921 0.92 413572. 0.0983
|
|
177.51 0.8368 0.5763 0.0137 0.0199 3.531 13.910 4.299 2633.148 1.572 19.124 0.741 0.92 415229. 0.0644
|
|
184.08 0.8678 0.3741 0.0068 0.0157 2.791 10.993 2.127 2080.997 1.242 9.460 0.464 0.92 416932. 0.0283
|
|
190.66 0.8988 -0.0054 -0.0001 0.0116 2.063 8.127 -0.022 1538.385 0.918 -0.097 -0.006 0.92 418653. 0.0000
|
|
|
|
|
|
|