538 lines
95 KiB
Plaintext
538 lines
95 KiB
Plaintext
17x6E (17x6E.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 0.0652 0.0235 0.003 0.167 0.171 1.974 0.019 0.763 39.389 0.07 26829. 0.5645
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0.27 0.0170 0.0459 0.0638 0.0236 0.003 0.167 0.168 1.978 0.019 0.746 38.469 0.07 26840. 0.5455
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0.54 0.0339 0.0896 0.0623 0.0236 0.003 0.167 0.164 1.981 0.019 0.729 37.542 0.07 26852. 0.5263
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0.82 0.0509 0.1311 0.0608 0.0236 0.003 0.168 0.160 1.982 0.019 0.712 36.608 0.07 26865. 0.5069
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1.09 0.0678 0.1703 0.0592 0.0236 0.003 0.167 0.156 1.982 0.019 0.693 35.667 0.07 26878. 0.4874
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1.36 0.0848 0.2072 0.0576 0.0236 0.003 0.167 0.151 1.979 0.019 0.674 34.719 0.07 26892. 0.4677
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1.63 0.1018 0.2418 0.0558 0.0235 0.003 0.167 0.147 1.973 0.019 0.653 33.762 0.07 26907. 0.4479
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1.91 0.1187 0.2740 0.0540 0.0234 0.003 0.166 0.142 1.966 0.019 0.632 32.796 0.07 26923. 0.4280
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2.18 0.1357 0.3038 0.0521 0.0233 0.003 0.165 0.137 1.955 0.019 0.610 31.820 0.07 26939. 0.4079
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2.45 0.1527 0.3312 0.0502 0.0231 0.003 0.164 0.132 1.942 0.019 0.587 30.831 0.07 26957. 0.3877
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2.72 0.1696 0.3560 0.0481 0.0229 0.003 0.163 0.127 1.926 0.018 0.563 29.829 0.07 26975. 0.3674
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2.99 0.1866 0.3782 0.0460 0.0227 0.003 0.161 0.121 1.906 0.018 0.539 28.810 0.07 26994. 0.3470
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3.27 0.2035 0.3978 0.0439 0.0224 0.003 0.159 0.115 1.884 0.018 0.513 27.771 0.07 27014. 0.3265
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3.54 0.2205 0.4145 0.0416 0.0221 0.002 0.157 0.109 1.859 0.018 0.487 26.711 0.07 27035. 0.3059
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3.81 0.2375 0.4282 0.0393 0.0218 0.002 0.155 0.103 1.831 0.017 0.460 25.624 0.07 27057. 0.2852
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4.08 0.2544 0.4388 0.0369 0.0214 0.002 0.152 0.097 1.799 0.017 0.432 24.507 0.07 27080. 0.2645
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4.36 0.2714 0.4460 0.0345 0.0210 0.002 0.149 0.091 1.764 0.017 0.404 23.355 0.07 27104. 0.2436
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4.63 0.2883 0.4497 0.0320 0.0205 0.002 0.146 0.084 1.725 0.016 0.375 22.161 0.07 27128. 0.2227
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4.90 0.3053 0.4494 0.0295 0.0201 0.002 0.142 0.078 1.684 0.016 0.345 20.920 0.07 27154. 0.2018
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5.17 0.3223 0.4450 0.0269 0.0195 0.002 0.138 0.071 1.638 0.016 0.315 19.622 0.07 27181. 0.1808
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5.45 0.3392 0.4359 0.0243 0.0189 0.002 0.134 0.064 1.590 0.015 0.285 18.259 0.07 27209. 0.1599
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5.72 0.3562 0.4216 0.0217 0.0183 0.002 0.130 0.057 1.538 0.015 0.254 16.819 0.07 27237. 0.1390
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5.99 0.3732 0.4014 0.0190 0.0176 0.002 0.125 0.050 1.482 0.014 0.222 15.288 0.07 27267. 0.1183
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6.26 0.3901 0.3747 0.0163 0.0169 0.002 0.120 0.043 1.423 0.014 0.190 13.649 0.07 27298. 0.0978
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6.53 0.4071 0.3404 0.0135 0.0162 0.002 0.115 0.036 1.361 0.013 0.159 11.882 0.07 27330. 0.0777
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6.81 0.4240 0.2972 0.0108 0.0154 0.002 0.109 0.028 1.295 0.012 0.127 9.961 0.07 27364. 0.0582
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7.08 0.4410 0.2437 0.0081 0.0146 0.002 0.104 0.021 1.227 0.012 0.094 7.854 0.07 27398. 0.0396
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7.35 0.4580 0.1779 0.0053 0.0138 0.002 0.098 0.014 1.155 0.011 0.063 5.522 0.07 27433. 0.0227
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7.62 0.4749 0.0972 0.0026 0.0129 0.001 0.091 0.007 1.081 0.010 0.031 2.910 0.07 27469. 0.0084
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7.90 0.4919 -0.0024 -0.0001 0.0120 0.001 0.085 0.000 1.004 0.010 -0.001 -0.070 0.07 27506. 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 0.0654 0.0211 0.019 0.598 0.688 14.159 0.068 3.062 22.050 0.13 53657. 0.6333
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0.55 0.0170 0.0516 0.0640 0.0211 0.019 0.600 0.674 14.204 0.068 2.997 21.516 0.13 53679. 0.6113
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1.09 0.0341 0.1006 0.0626 0.0212 0.019 0.602 0.658 14.235 0.068 2.929 20.980 0.13 53704. 0.5893
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1.64 0.0511 0.1470 0.0610 0.0212 0.019 0.602 0.642 14.252 0.068 2.857 20.445 0.13 53729. 0.5672
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2.19 0.0681 0.1909 0.0595 0.0212 0.019 0.602 0.626 14.252 0.068 2.783 19.909 0.13 53756. 0.5451
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2.73 0.0852 0.2322 0.0578 0.0212 0.019 0.602 0.608 14.235 0.068 2.705 19.374 0.13 53785. 0.5230
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3.28 0.1022 0.2709 0.0560 0.0211 0.019 0.600 0.590 14.198 0.068 2.623 18.839 0.13 53815. 0.5008
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3.83 0.1192 0.3071 0.0542 0.0210 0.019 0.598 0.571 14.139 0.068 2.538 18.303 0.13 53846. 0.4786
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4.37 0.1363 0.3407 0.0523 0.0209 0.019 0.594 0.551 14.057 0.067 2.449 17.765 0.13 53880. 0.4563
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4.92 0.1533 0.3716 0.0503 0.0208 0.019 0.590 0.530 13.950 0.067 2.356 17.225 0.13 53915. 0.4340
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5.47 0.1703 0.3999 0.0483 0.0206 0.019 0.584 0.508 13.818 0.066 2.261 16.682 0.13 53951. 0.4117
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6.01 0.1874 0.4254 0.0462 0.0203 0.018 0.577 0.486 13.661 0.065 2.162 16.135 0.13 53990. 0.3893
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6.56 0.2044 0.4482 0.0440 0.0201 0.018 0.570 0.463 13.476 0.064 2.059 15.581 0.13 54030. 0.3670
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7.11 0.2214 0.4680 0.0417 0.0197 0.018 0.561 0.439 13.264 0.063 1.954 15.019 0.13 54072. 0.3446
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7.65 0.2384 0.4848 0.0394 0.0194 0.017 0.550 0.415 13.024 0.062 1.845 14.448 0.13 54116. 0.3221
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8.20 0.2555 0.4985 0.0370 0.0190 0.017 0.539 0.390 12.755 0.061 1.734 13.863 0.13 54162. 0.2996
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8.75 0.2725 0.5087 0.0346 0.0185 0.017 0.526 0.364 12.456 0.059 1.620 13.264 0.13 54210. 0.2771
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9.30 0.2895 0.5153 0.0321 0.0181 0.016 0.512 0.338 12.126 0.058 1.504 12.645 0.14 54260. 0.2545
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9.84 0.3066 0.5178 0.0296 0.0175 0.016 0.497 0.311 11.766 0.056 1.385 12.002 0.14 54312. 0.2318
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10.39 0.3236 0.5160 0.0270 0.0169 0.015 0.481 0.284 11.375 0.054 1.264 11.331 0.14 54366. 0.2091
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10.94 0.3406 0.5093 0.0244 0.0163 0.015 0.463 0.257 10.953 0.052 1.141 10.624 0.14 54422. 0.1863
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11.48 0.3577 0.4970 0.0217 0.0156 0.014 0.444 0.229 10.500 0.050 1.017 9.873 0.14 54480. 0.1634
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12.03 0.3747 0.4782 0.0190 0.0149 0.013 0.423 0.200 10.015 0.048 0.891 9.069 0.14 54540. 0.1405
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12.58 0.3917 0.4519 0.0163 0.0141 0.013 0.401 0.172 9.500 0.045 0.764 8.197 0.14 54603. 0.1176
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13.12 0.4088 0.4166 0.0136 0.0133 0.012 0.378 0.143 8.955 0.043 0.636 7.241 0.14 54667. 0.0948
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13.67 0.4258 0.3703 0.0108 0.0125 0.011 0.354 0.114 8.381 0.040 0.508 6.179 0.14 54734. 0.0723
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14.22 0.4428 0.3103 0.0081 0.0116 0.010 0.329 0.085 7.779 0.037 0.380 4.979 0.14 54803. 0.0504
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14.76 0.4599 0.2329 0.0054 0.0106 0.010 0.302 0.057 7.151 0.034 0.252 3.598 0.14 54874. 0.0297
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15.31 0.4769 0.1326 0.0027 0.0097 0.009 0.275 0.028 6.499 0.031 0.126 1.975 0.14 54947. 0.0115
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15.86 0.4939 -0.0001 0.0000 0.0087 0.008 0.246 0.000 5.818 0.028 0.000 -0.002 0.14 55020. 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 0.0657 0.0201 0.061 1.281 1.555 45.458 0.145 6.916 15.515 0.20 80484. 0.6697
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0.84 0.0174 0.0554 0.0643 0.0201 0.061 1.285 1.521 45.624 0.145 6.767 15.125 0.20 80519. 0.6458
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1.67 0.0347 0.1080 0.0628 0.0202 0.061 1.289 1.486 45.743 0.146 6.610 14.736 0.20 80556. 0.6219
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2.51 0.0521 0.1578 0.0612 0.0202 0.061 1.291 1.449 45.809 0.146 6.446 14.349 0.20 80595. 0.5979
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3.34 0.0694 0.2047 0.0596 0.0202 0.061 1.291 1.410 45.816 0.146 6.274 13.963 0.20 80637. 0.5741
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4.18 0.0868 0.2488 0.0579 0.0202 0.061 1.289 1.370 45.758 0.146 6.093 13.579 0.20 80680. 0.5502
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5.02 0.1042 0.2902 0.0561 0.0201 0.061 1.286 1.328 45.627 0.145 5.905 13.197 0.20 80727. 0.5264
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5.85 0.1215 0.3288 0.0542 0.0200 0.061 1.280 1.283 45.418 0.145 5.708 12.815 0.20 80775. 0.5025
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6.69 0.1389 0.3646 0.0522 0.0199 0.061 1.271 1.237 45.125 0.144 5.502 12.434 0.20 80827. 0.4787
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7.52 0.1562 0.3976 0.0502 0.0197 0.060 1.261 1.189 44.742 0.142 5.289 12.054 0.20 80881. 0.4550
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8.36 0.1736 0.4278 0.0481 0.0195 0.059 1.247 1.139 44.268 0.141 5.067 11.672 0.20 80938. 0.4312
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9.20 0.1910 0.4551 0.0459 0.0193 0.059 1.231 1.088 43.698 0.139 4.838 11.289 0.20 80997. 0.4075
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10.03 0.2083 0.4795 0.0437 0.0190 0.058 1.212 1.034 43.029 0.137 4.601 10.903 0.20 81059. 0.3838
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10.87 0.2257 0.5009 0.0414 0.0186 0.057 1.191 0.979 42.259 0.135 4.357 10.512 0.20 81124. 0.3601
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11.70 0.2430 0.5191 0.0390 0.0183 0.055 1.166 0.923 41.385 0.132 4.106 10.116 0.20 81193. 0.3364
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12.54 0.2604 0.5339 0.0365 0.0178 0.054 1.138 0.865 40.403 0.129 3.848 9.712 0.20 81264. 0.3127
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13.38 0.2778 0.5452 0.0340 0.0173 0.053 1.108 0.806 39.312 0.125 3.585 9.298 0.20 81338. 0.2890
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14.21 0.2951 0.5527 0.0315 0.0168 0.051 1.074 0.745 38.109 0.121 3.315 8.871 0.20 81415. 0.2651
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15.05 0.3125 0.5560 0.0289 0.0162 0.049 1.037 0.684 36.793 0.117 3.041 8.427 0.20 81496. 0.2412
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15.88 0.3298 0.5545 0.0262 0.0156 0.047 0.996 0.621 35.362 0.113 2.761 7.963 0.20 81579. 0.2172
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16.72 0.3472 0.5476 0.0235 0.0149 0.045 0.953 0.557 33.816 0.108 2.478 7.471 0.20 81666. 0.1930
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17.56 0.3646 0.5346 0.0208 0.0142 0.043 0.906 0.492 32.154 0.102 2.190 6.946 0.20 81756. 0.1687
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18.39 0.3819 0.5142 0.0180 0.0134 0.041 0.856 0.427 30.379 0.097 1.900 6.378 0.20 81850. 0.1443
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19.23 0.3993 0.4850 0.0153 0.0126 0.038 0.803 0.361 28.491 0.091 1.608 5.754 0.20 81947. 0.1197
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20.06 0.4167 0.4448 0.0125 0.0117 0.036 0.746 0.295 26.494 0.084 1.314 5.057 0.20 82047. 0.0951
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20.90 0.4340 0.3907 0.0097 0.0108 0.033 0.687 0.229 24.393 0.078 1.020 4.264 0.20 82151. 0.0707
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21.74 0.4514 0.3182 0.0069 0.0098 0.030 0.625 0.163 22.193 0.071 0.727 3.340 0.20 82258. 0.0467
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22.57 0.4687 0.2209 0.0041 0.0088 0.027 0.561 0.098 19.901 0.063 0.436 2.232 0.20 82368. 0.0242
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23.41 0.4861 0.0878 0.0014 0.0077 0.023 0.494 0.033 17.520 0.056 0.147 0.856 0.20 82481. 0.0054
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24.24 0.5035
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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 0.0660 0.0195 0.141 2.214 2.778 104.782 0.250 12.356 12.025 0.27 107309. 0.6938
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1.10 0.0171 0.0564 0.0646 0.0196 0.141 2.223 2.719 105.186 0.251 12.094 11.725 0.27 107355. 0.6693
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2.19 0.0342 0.1099 0.0631 0.0196 0.141 2.229 2.657 105.480 0.252 11.819 11.426 0.27 107404. 0.6448
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3.29 0.0512 0.1605 0.0616 0.0197 0.142 2.232 2.592 105.649 0.252 11.531 11.130 0.27 107456. 0.6203
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4.39 0.0683 0.2084 0.0600 0.0197 0.142 2.233 2.525 105.681 0.252 11.230 10.835 0.27 107510. 0.5960
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5.48 0.0854 0.2534 0.0583 0.0196 0.142 2.231 2.454 105.561 0.252 10.914 10.543 0.27 107567. 0.5717
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6.58 0.1025 0.2958 0.0565 0.0196 0.141 2.225 2.380 105.274 0.251 10.584 10.252 0.27 107628. 0.5475
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7.68 0.1196 0.3353 0.0547 0.0195 0.141 2.215 2.302 104.804 0.250 10.240 9.963 0.27 107692. 0.5233
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8.77 0.1366 0.3721 0.0528 0.0194 0.140 2.200 2.221 104.137 0.249 9.881 9.675 0.27 107759. 0.4992
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9.87 0.1537 0.4063 0.0508 0.0192 0.138 2.182 2.137 103.262 0.247 9.507 9.389 0.27 107829. 0.4751
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10.97 0.1708 0.4376 0.0487 0.0190 0.137 2.159 2.050 102.172 0.244 9.120 9.102 0.27 107903. 0.4512
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12.06 0.1879 0.4662 0.0466 0.0188 0.135 2.131 1.960 100.859 0.241 8.719 8.815 0.27 107981. 0.4273
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13.16 0.2050 0.4920 0.0444 0.0185 0.133 2.099 1.867 99.314 0.237 8.306 8.528 0.27 108062. 0.4034
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14.26 0.2221 0.5149 0.0421 0.0181 0.131 2.061 1.771 97.531 0.233 7.879 8.238 0.27 108147. 0.3796
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15.35 0.2391 0.5348 0.0397 0.0178 0.128 2.018 1.673 95.504 0.228 7.441 7.945 0.27 108235. 0.3557
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16.45 0.2562 0.5515 0.0373 0.0173 0.125 1.970 1.572 93.224 0.223 6.992 7.648 0.27 108328. 0.3319
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17.55 0.2733 0.5650 0.0349 0.0169 0.122 1.916 1.468 90.686 0.216 6.531 7.344 0.27 108424. 0.3081
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18.64 0.2904 0.5748 0.0324 0.0164 0.118 1.857 1.363 87.886 0.210 6.061 7.032 0.27 108525. 0.2842
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19.74 0.3075 0.5807 0.0298 0.0158 0.114 1.792 1.255 84.818 0.202 5.581 6.710 0.27 108629. 0.2602
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20.84 0.3245 0.5823 0.0272 0.0152 0.109 1.722 1.145 81.479 0.195 5.093 6.374 0.27 108737. 0.2361
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21.93 0.3416 0.5789 0.0246 0.0145 0.104 1.645 1.034 77.868 0.186 4.597 6.020 0.27 108850. 0.2119
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23.03 0.3587 0.5698 0.0219 0.0138 0.099 1.563 0.921 73.984 0.177 4.095 5.644 0.27 108967. 0.1874
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24.13 0.3758 0.5540 0.0192 0.0130 0.094 1.476 0.806 69.829 0.167 3.587 5.238 0.27 109088. 0.1628
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25.22 0.3929 0.5301 0.0164 0.0122 0.088 1.382 0.691 65.406 0.156 3.075 4.794 0.27 109214. 0.1380
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26.32 0.4099 0.4960 0.0137 0.0113 0.081 1.283 0.575 60.722 0.145 2.560 4.299 0.27 109344. 0.1129
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27.42 0.4270 0.4490 0.0109 0.0104 0.075 1.179 0.459 55.786 0.133 2.044 3.736 0.27 109478. 0.0877
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28.51 0.4441 0.3850 0.0082 0.0094 0.068 1.069 0.344 50.610 0.121 1.529 3.080 0.27 109617. 0.0625
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29.61 0.4612 0.2974 0.0054 0.0084 0.061 0.955 0.228 45.211 0.108 1.016 2.291 0.27 109760. 0.0379
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30.71 0.4783 0.1760 0.0027 0.0074 0.053 0.837 0.114 39.602 0.095 0.508 1.307 0.27 109906. 0.0153
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31.80 0.4953 -0.0005 0.0000 0.0063 0.045 0.713 0.000 33.723 0.081 -0.001 -0.003 0.27 110048. 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 0.0664 0.0192 0.270 3.404 4.367 201.395 0.385 19.425 9.835 0.34 134133. 0.7115
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1.38 0.0172 0.0580 0.0650 0.0193 0.271 3.418 4.274 202.202 0.386 19.011 9.587 0.34 134191. 0.6861
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2.76 0.0344 0.1130 0.0635 0.0193 0.272 3.428 4.176 202.785 0.387 18.576 9.341 0.34 134253. 0.6608
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4.14 0.0516 0.1651 0.0619 0.0194 0.272 3.434 4.074 203.118 0.388 18.120 9.097 0.34 134318. 0.6356
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5.52 0.0688 0.2143 0.0603 0.0194 0.272 3.435 3.966 203.173 0.388 17.642 8.855 0.34 134387. 0.6104
|
|
6.90 0.0860 0.2606 0.0586 0.0193 0.272 3.430 3.854 202.921 0.388 17.142 8.614 0.34 134459. 0.5854
|
|
8.28 0.1032 0.3041 0.0568 0.0193 0.271 3.420 3.736 202.331 0.386 16.620 8.376 0.34 134536. 0.5605
|
|
9.66 0.1204 0.3447 0.0549 0.0192 0.270 3.404 3.614 201.371 0.385 16.074 8.140 0.34 134616. 0.5356
|
|
11.04 0.1376 0.3826 0.0530 0.0191 0.268 3.381 3.486 200.011 0.382 15.505 7.905 0.34 134701. 0.5109
|
|
12.42 0.1548 0.4177 0.0510 0.0189 0.266 3.351 3.353 198.232 0.379 14.913 7.671 0.34 134790. 0.4862
|
|
13.80 0.1720 0.4501 0.0489 0.0187 0.263 3.314 3.215 196.016 0.374 14.298 7.438 0.34 134884. 0.4617
|
|
15.18 0.1892 0.4796 0.0467 0.0184 0.259 3.268 3.072 193.347 0.369 13.663 7.206 0.34 134982. 0.4372
|
|
16.56 0.2064 0.5063 0.0445 0.0181 0.255 3.215 2.924 190.211 0.363 13.006 6.973 0.34 135085. 0.4127
|
|
17.94 0.2236 0.5300 0.0421 0.0178 0.250 3.154 2.772 186.590 0.356 12.330 6.739 0.34 135192. 0.3884
|
|
19.32 0.2408 0.5508 0.0398 0.0174 0.245 3.085 2.616 182.472 0.348 11.635 6.502 0.34 135304. 0.3640
|
|
20.70 0.2580 0.5684 0.0373 0.0169 0.238 3.006 2.456 177.843 0.340 10.922 6.263 0.34 135421. 0.3397
|
|
22.08 0.2751 0.5826 0.0348 0.0165 0.232 2.919 2.291 172.691 0.330 10.192 6.018 0.34 135543. 0.3154
|
|
23.46 0.2923 0.5933 0.0323 0.0159 0.224 2.823 2.124 167.004 0.319 9.446 5.768 0.34 135670. 0.2910
|
|
24.84 0.3095 0.6000 0.0297 0.0153 0.216 2.718 1.953 160.775 0.307 8.686 5.509 0.34 135802. 0.2665
|
|
26.22 0.3267 0.6023 0.0270 0.0147 0.207 2.603 1.779 153.997 0.294 7.912 5.239 0.34 135939. 0.2419
|
|
27.60 0.3439 0.5995 0.0244 0.0140 0.197 2.479 1.602 146.666 0.280 7.125 4.954 0.34 136082. 0.2171
|
|
28.98 0.3611 0.5909 0.0216 0.0132 0.186 2.346 1.423 138.782 0.265 6.329 4.650 0.34 136230. 0.1920
|
|
30.36 0.3783 0.5753 0.0189 0.0124 0.175 2.203 1.242 130.349 0.249 5.524 4.322 0.34 136383. 0.1667
|
|
31.74 0.3955 0.5511 0.0161 0.0116 0.163 2.052 1.060 121.375 0.232 4.713 3.960 0.34 136542. 0.1411
|
|
33.12 0.4127 0.5160 0.0133 0.0107 0.150 1.891 0.876 111.874 0.214 3.898 3.553 0.34 136706. 0.1152
|
|
34.50 0.4299 0.4667 0.0105 0.0097 0.137 1.722 0.693 101.867 0.195 3.082 3.085 0.34 136876. 0.0889
|
|
35.88 0.4471 0.3981 0.0078 0.0087 0.123 1.545 0.510 91.379 0.175 2.268 2.531 0.34 137052. 0.0625
|
|
37.26 0.4643 0.3019 0.0050 0.0077 0.108 1.360 0.328 80.444 0.154 1.458 1.848 0.34 137233. 0.0366
|
|
38.64 0.4815 0.1639 0.0022 0.0066 0.093 1.168 0.147 69.091 0.132 0.656 0.968 0.34 137418. 0.0129
|
|
40.02 0.4987
|
|
|
|
|
|
|
|
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 0.0669 0.0190 0.463 4.863 6.336 345.187 0.549 28.183 8.326 0.40 160954. 0.7254
|
|
1.65 0.0171 0.0586 0.0655 0.0191 0.465 4.882 6.202 346.577 0.552 27.587 8.117 0.40 161024. 0.6997
|
|
3.29 0.0342 0.1141 0.0640 0.0192 0.466 4.896 6.061 347.579 0.553 26.960 7.910 0.40 161097. 0.6741
|
|
4.94 0.0513 0.1667 0.0624 0.0192 0.467 4.904 5.914 348.144 0.554 26.304 7.704 0.40 161175. 0.6486
|
|
6.58 0.0683 0.2165 0.0608 0.0192 0.467 4.906 5.759 348.228 0.554 25.616 7.501 0.40 161257. 0.6231
|
|
8.23 0.0854 0.2633 0.0591 0.0192 0.466 4.899 5.597 347.779 0.554 24.897 7.300 0.40 161344. 0.5979
|
|
9.87 0.1025 0.3073 0.0573 0.0191 0.465 4.885 5.428 346.746 0.552 24.145 7.101 0.40 161436. 0.5727
|
|
11.52 0.1196 0.3486 0.0555 0.0190 0.463 4.861 5.252 345.071 0.549 23.360 6.903 0.40 161532. 0.5476
|
|
13.16 0.1367 0.3871 0.0535 0.0189 0.460 4.828 5.068 342.704 0.545 22.541 6.707 0.40 161633. 0.5227
|
|
14.81 0.1538 0.4228 0.0515 0.0187 0.455 4.784 4.876 339.610 0.541 21.689 6.512 0.40 161739. 0.4978
|
|
16.46 0.1709 0.4558 0.0494 0.0185 0.450 4.730 4.678 335.756 0.534 20.806 6.319 0.40 161851. 0.4731
|
|
18.10 0.1879 0.4861 0.0472 0.0183 0.444 4.664 4.472 331.117 0.527 19.892 6.126 0.40 161967. 0.4484
|
|
19.75 0.2050 0.5136 0.0450 0.0180 0.437 4.588 4.260 325.666 0.518 18.948 5.933 0.40 162090. 0.4239
|
|
21.39 0.2221 0.5382 0.0427 0.0176 0.428 4.499 4.041 319.375 0.508 17.975 5.739 0.40 162217. 0.3994
|
|
23.04 0.2392 0.5599 0.0403 0.0172 0.419 4.398 3.816 312.220 0.497 16.976 5.544 0.40 162351. 0.3749
|
|
24.68 0.2563 0.5786 0.0379 0.0168 0.408 4.285 3.586 304.178 0.484 15.950 5.347 0.40 162490. 0.3505
|
|
26.33 0.2734 0.5940 0.0354 0.0163 0.396 4.159 3.350 295.227 0.470 14.900 5.146 0.40 162635. 0.3261
|
|
27.97 0.2905 0.6060 0.0328 0.0157 0.383 4.020 3.109 285.349 0.454 13.827 4.941 0.41 162786. 0.3016
|
|
29.62 0.3075 0.6141 0.0302 0.0151 0.368 3.867 2.862 274.527 0.437 12.732 4.729 0.41 162943. 0.2770
|
|
31.27 0.3246 0.6180 0.0276 0.0145 0.352 3.701 2.612 262.751 0.418 11.618 4.509 0.41 163106. 0.2523
|
|
32.91 0.3417 0.6171 0.0249 0.0138 0.335 3.522 2.358 250.013 0.398 10.487 4.277 0.41 163275. 0.2273
|
|
34.56 0.3588 0.6106 0.0222 0.0130 0.317 3.329 2.100 236.313 0.376 9.340 4.031 0.41 163451. 0.2022
|
|
36.20 0.3759 0.5974 0.0194 0.0122 0.297 3.122 1.839 221.656 0.353 8.182 3.764 0.41 163633. 0.1767
|
|
37.85 0.3930 0.5759 0.0166 0.0114 0.276 2.903 1.577 206.055 0.328 7.014 3.471 0.41 163821. 0.1509
|
|
39.49 0.4101 0.5439 0.0139 0.0105 0.254 2.670 1.313 189.533 0.302 5.839 3.142 0.41 164016. 0.1246
|
|
41.14 0.4271 0.4981 0.0111 0.0095 0.231 2.425 1.048 172.123 0.274 4.662 2.762 0.41 164218. 0.0979
|
|
42.78 0.4442 0.4335 0.0083 0.0085 0.206 2.168 0.784 153.871 0.245 3.487 2.311 0.41 164426. 0.0708
|
|
44.43 0.4613 0.3415 0.0055 0.0074 0.181 1.899 0.521 134.834 0.215 2.318 1.753 0.41 164641. 0.0438
|
|
46.07 0.4784 0.2076 0.0028 0.0063 0.154 1.621 0.261 115.065 0.183 1.160 1.028 0.41 164861. 0.0182
|
|
47.72 0.4955 -0.0008 0.0000 0.0052 0.126 1.328 -0.001 94.272 0.150 -0.004 -0.004 0.41 165071. 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 0.0675 0.0190 0.734 6.605 8.703 547.011 0.746 38.710 7.216 0.47 187772. 0.7369
|
|
1.92 0.0171 0.0593 0.0661 0.0191 0.736 6.631 8.519 549.201 0.749 37.891 7.035 0.47 187854. 0.7108
|
|
3.84 0.0342 0.1155 0.0646 0.0191 0.739 6.650 8.325 550.759 0.751 37.030 6.856 0.47 187940. 0.6848
|
|
5.76 0.0513 0.1688 0.0630 0.0192 0.740 6.660 8.122 551.609 0.752 36.128 6.679 0.47 188031. 0.6589
|
|
7.69 0.0684 0.2191 0.0614 0.0192 0.740 6.661 7.910 551.675 0.753 35.183 6.503 0.47 188128. 0.6331
|
|
9.61 0.0855 0.2666 0.0596 0.0191 0.739 6.652 7.687 550.877 0.751 34.194 6.330 0.47 188229. 0.6075
|
|
11.53 0.1026 0.3112 0.0578 0.0191 0.736 6.631 7.455 549.131 0.749 33.160 6.158 0.47 188337. 0.5820
|
|
13.45 0.1197 0.3531 0.0560 0.0190 0.733 6.597 7.212 546.344 0.745 32.081 5.988 0.47 188449. 0.5567
|
|
15.37 0.1368 0.3922 0.0540 0.0188 0.727 6.550 6.959 542.435 0.740 30.955 5.819 0.47 188568. 0.5314
|
|
17.29 0.1539 0.4285 0.0519 0.0187 0.721 6.488 6.696 537.344 0.733 29.784 5.652 0.47 188693. 0.5063
|
|
19.22 0.1710 0.4621 0.0498 0.0184 0.712 6.412 6.423 531.021 0.724 28.568 5.486 0.47 188823. 0.4813
|
|
21.14 0.1881 0.4930 0.0476 0.0182 0.702 6.320 6.140 523.424 0.714 27.311 5.321 0.47 188960. 0.4564
|
|
23.06 0.2052 0.5211 0.0454 0.0179 0.690 6.212 5.848 514.508 0.702 26.013 5.155 0.47 189103. 0.4316
|
|
24.98 0.2223 0.5465 0.0430 0.0175 0.676 6.088 5.547 504.230 0.688 24.675 4.990 0.47 189253. 0.4068
|
|
26.90 0.2394 0.5689 0.0406 0.0171 0.661 5.947 5.238 492.551 0.672 23.299 4.824 0.47 189409. 0.3822
|
|
28.82 0.2565 0.5883 0.0382 0.0166 0.643 5.789 4.921 479.434 0.654 21.888 4.655 0.47 189572. 0.3575
|
|
30.74 0.2736 0.6044 0.0357 0.0161 0.623 5.613 4.596 464.842 0.634 20.443 4.485 0.47 189741. 0.3328
|
|
32.67 0.2907 0.6172 0.0331 0.0156 0.602 5.418 4.264 448.746 0.612 18.967 4.310 0.47 189918. 0.3081
|
|
34.59 0.3078 0.6262 0.0305 0.0150 0.578 5.206 3.926 431.122 0.588 17.461 4.130 0.47 190102. 0.2833
|
|
36.51 0.3249 0.6310 0.0278 0.0143 0.552 4.974 3.581 411.950 0.562 15.928 3.943 0.47 190292. 0.2583
|
|
38.43 0.3420 0.6311 0.0251 0.0136 0.525 4.724 3.231 391.220 0.534 14.371 3.746 0.47 190491. 0.2331
|
|
40.35 0.3591 0.6256 0.0223 0.0128 0.495 4.455 2.876 368.930 0.503 12.794 3.536 0.47 190696. 0.2076
|
|
42.27 0.3762 0.6133 0.0195 0.0120 0.463 4.167 2.518 345.090 0.471 11.200 3.309 0.47 190909. 0.1818
|
|
44.19 0.3933 0.5927 0.0167 0.0111 0.429 3.861 2.156 319.722 0.436 9.592 3.059 0.47 191129. 0.1555
|
|
46.12 0.4104 0.5615 0.0139 0.0102 0.393 3.536 1.793 292.863 0.400 7.976 2.777 0.47 191357. 0.1287
|
|
48.04 0.4275 0.5160 0.0111 0.0092 0.355 3.195 1.429 264.569 0.361 6.357 2.450 0.47 191593. 0.1014
|
|
49.96 0.4446 0.4507 0.0083 0.0082 0.315 2.836 1.066 234.914 0.320 4.741 2.058 0.48 191836. 0.0735
|
|
51.88 0.4617 0.3562 0.0055 0.0071 0.274 2.463 0.704 203.991 0.278 3.133 1.566 0.48 192087. 0.0455
|
|
53.80 0.4788 0.2154 0.0027 0.0060 0.231 2.075 0.346 171.889 0.234 1.540 0.913 0.48 192345. 0.0186
|
|
55.72 0.4959 -0.0128 -0.0001 0.0048 0.185 1.665 -0.016 137.903 0.188 -0.071 -0.053 0.48 192581. 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 0.0682 0.0191 1.098 8.654 11.491 819.102 0.978 51.111 6.363 0.54 214586. 0.7467
|
|
2.23 0.0173 0.0606 0.0668 0.0191 1.103 8.688 11.244 822.354 0.982 50.015 6.202 0.54 214681. 0.7199
|
|
4.46 0.0347 0.1180 0.0652 0.0192 1.106 8.712 10.985 824.607 0.984 48.861 6.042 0.54 214782. 0.6932
|
|
6.68 0.0520 0.1724 0.0636 0.0192 1.107 8.724 10.713 825.740 0.986 47.651 5.884 0.54 214888. 0.6667
|
|
8.91 0.0694 0.2238 0.0619 0.0192 1.107 8.723 10.428 825.635 0.986 46.383 5.729 0.54 215001. 0.6404
|
|
11.14 0.0867 0.2722 0.0602 0.0192 1.105 8.708 10.129 824.168 0.984 45.055 5.575 0.54 215120. 0.6142
|
|
13.37 0.1041 0.3177 0.0583 0.0191 1.101 8.676 9.817 821.201 0.980 43.666 5.422 0.54 215245. 0.5881
|
|
15.59 0.1214 0.3604 0.0564 0.0190 1.095 8.628 9.491 816.591 0.975 42.215 5.272 0.54 215377. 0.5622
|
|
17.82 0.1388 0.4002 0.0543 0.0188 1.087 8.560 9.150 810.210 0.967 40.700 5.122 0.54 215516. 0.5364
|
|
20.05 0.1561 0.4372 0.0522 0.0187 1.075 8.473 8.796 801.963 0.957 39.124 4.975 0.54 215662. 0.5107
|
|
22.28 0.1735 0.4715 0.0501 0.0184 1.062 8.365 8.428 791.777 0.945 37.488 4.828 0.54 215815. 0.4852
|
|
24.50 0.1908 0.5030 0.0478 0.0181 1.045 8.236 8.047 779.580 0.931 35.794 4.682 0.54 215975. 0.4598
|
|
26.73 0.2082 0.5316 0.0455 0.0178 1.026 8.086 7.654 765.306 0.914 34.045 4.536 0.54 216143. 0.4344
|
|
28.96 0.2255 0.5574 0.0431 0.0174 1.004 7.912 7.249 748.889 0.894 32.243 4.390 0.54 216318. 0.4092
|
|
31.19 0.2429 0.5802 0.0406 0.0170 0.979 7.715 6.832 730.266 0.872 30.390 4.244 0.54 216501. 0.3840
|
|
33.41 0.2602 0.5999 0.0380 0.0165 0.951 7.495 6.405 709.379 0.847 28.489 4.095 0.54 216692. 0.3588
|
|
35.64 0.2776 0.6163 0.0354 0.0160 0.920 7.250 5.967 686.173 0.819 26.542 3.944 0.54 216891. 0.3335
|
|
37.87 0.2949 0.6292 0.0328 0.0154 0.886 6.979 5.520 660.605 0.789 24.553 3.790 0.54 217098. 0.3082
|
|
40.10 0.3123 0.6382 0.0301 0.0147 0.848 6.684 5.064 632.636 0.755 22.524 3.631 0.54 217313. 0.2828
|
|
42.32 0.3296 0.6428 0.0273 0.0140 0.808 6.363 4.600 602.242 0.719 20.460 3.464 0.54 217537. 0.2572
|
|
44.55 0.3470 0.6424 0.0245 0.0132 0.764 6.016 4.129 569.407 0.680 18.365 3.289 0.54 217769. 0.2313
|
|
46.78 0.3643 0.6359 0.0217 0.0124 0.716 5.643 3.652 534.136 0.638 16.243 3.101 0.54 218010. 0.2051
|
|
49.01 0.3816 0.6222 0.0188 0.0115 0.666 5.245 3.170 496.449 0.593 14.098 2.896 0.54 218260. 0.1785
|
|
51.24 0.3990 0.5991 0.0159 0.0106 0.612 4.822 2.684 456.390 0.545 11.939 2.667 0.54 218518. 0.1513
|
|
53.46 0.4163 0.5639 0.0130 0.0096 0.555 4.374 2.196 414.027 0.494 9.769 2.406 0.54 218786. 0.1234
|
|
55.69 0.4337 0.5120 0.0101 0.0086 0.495 3.903 1.708 369.458 0.441 7.598 2.097 0.54 219062. 0.0949
|
|
57.92 0.4510 0.4358 0.0073 0.0075 0.433 3.411 1.222 322.816 0.385 5.434 1.716 0.54 219348. 0.0657
|
|
60.15 0.4684 0.3220 0.0044 0.0064 0.368 2.898 0.738 274.256 0.327 3.284 1.221 0.54 219642. 0.0363
|
|
62.37 0.4857 0.1438 0.0015 0.0052 0.300 2.365 0.260 223.849 0.267 1.155 0.526 0.54 219941. 0.0093
|
|
64.60 0.5031
|
|
|
|
|
|
|
|
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 0.0691 0.0192 1.577 11.042 14.732 1175.717 1.247 65.527 5.683 0.61 241393. 0.7551
|
|
2.47 0.0171 0.0599 0.0677 0.0193 1.583 11.083 14.421 1180.158 1.252 64.146 5.543 0.61 241499. 0.7286
|
|
4.93 0.0341 0.1168 0.0661 0.0193 1.587 11.112 14.095 1183.183 1.255 62.693 5.403 0.61 241612. 0.7022
|
|
7.40 0.0512 0.1708 0.0645 0.0194 1.589 11.125 13.752 1184.626 1.257 61.170 5.265 0.61 241731. 0.6759
|
|
9.87 0.0683 0.2218 0.0629 0.0193 1.588 11.122 13.394 1184.322 1.257 59.575 5.129 0.61 241856. 0.6498
|
|
12.33 0.0854 0.2700 0.0611 0.0193 1.585 11.102 13.018 1182.100 1.254 57.906 4.995 0.61 241988. 0.6239
|
|
14.80 0.1024 0.3154 0.0593 0.0192 1.579 11.061 12.626 1177.776 1.250 56.161 4.862 0.61 242127. 0.5981
|
|
17.26 0.1195 0.3581 0.0573 0.0191 1.571 10.999 12.216 1171.155 1.243 54.337 4.731 0.61 242273. 0.5724
|
|
19.73 0.1366 0.3980 0.0553 0.0190 1.558 10.913 11.789 1162.050 1.233 52.436 4.601 0.61 242427. 0.5469
|
|
22.20 0.1536 0.4352 0.0532 0.0188 1.543 10.803 11.344 1150.325 1.221 50.456 4.473 0.61 242588. 0.5215
|
|
24.66 0.1707 0.4698 0.0511 0.0186 1.523 10.667 10.882 1135.876 1.205 48.402 4.345 0.61 242757. 0.4962
|
|
27.13 0.1878 0.5017 0.0488 0.0183 1.500 10.505 10.404 1118.608 1.187 46.276 4.218 0.61 242933. 0.4710
|
|
29.60 0.2049 0.5309 0.0465 0.0179 1.473 10.316 9.910 1098.426 1.165 44.080 4.092 0.61 243118. 0.4459
|
|
32.06 0.2219 0.5574 0.0441 0.0176 1.442 10.098 9.401 1075.244 1.141 41.818 3.966 0.61 243311. 0.4209
|
|
34.53 0.2390 0.5811 0.0417 0.0171 1.407 9.851 8.878 1048.974 1.113 39.491 3.839 0.61 243513. 0.3960
|
|
36.99 0.2561 0.6019 0.0391 0.0167 1.367 9.575 8.342 1019.536 1.082 37.104 3.711 0.61 243722. 0.3710
|
|
39.46 0.2732 0.6195 0.0366 0.0161 1.323 9.268 7.792 986.855 1.047 34.658 3.581 0.61 243941. 0.3461
|
|
41.93 0.2902 0.6339 0.0339 0.0155 1.275 8.930 7.230 950.867 1.009 32.159 3.449 0.61 244168. 0.3210
|
|
44.39 0.3073 0.6447 0.0312 0.0149 1.222 8.560 6.657 911.517 0.967 29.610 3.312 0.61 244405. 0.2959
|
|
46.86 0.3244 0.6514 0.0285 0.0142 1.165 8.159 6.073 868.767 0.922 27.015 3.171 0.61 244650. 0.2705
|
|
49.33 0.3414 0.6535 0.0257 0.0134 1.103 7.725 5.481 822.594 0.873 24.379 3.022 0.61 244905. 0.2449
|
|
51.79 0.3585 0.6502 0.0229 0.0126 1.037 7.259 4.880 772.993 0.820 21.707 2.864 0.61 245169. 0.2190
|
|
54.26 0.3756 0.6403 0.0201 0.0118 0.966 6.762 4.273 719.988 0.764 19.006 2.692 0.61 245442. 0.1926
|
|
56.72 0.3927 0.6222 0.0172 0.0108 0.890 6.232 3.661 663.627 0.704 16.283 2.502 0.61 245725. 0.1657
|
|
59.19 0.4097 0.5934 0.0143 0.0099 0.810 5.672 3.045 603.993 0.641 13.544 2.287 0.61 246018. 0.1381
|
|
61.66 0.4268 0.5500 0.0114 0.0088 0.726 5.083 2.428 541.208 0.574 10.800 2.035 0.61 246320. 0.1098
|
|
64.12 0.4439 0.4859 0.0085 0.0078 0.638 4.465 1.812 475.439 0.504 8.059 1.728 0.61 246632. 0.0805
|
|
66.59 0.4609 0.3901 0.0056 0.0066 0.546 3.821 1.199 406.893 0.432 5.333 1.336 0.61 246954. 0.0507
|
|
69.06 0.4780 0.2418 0.0028 0.0055 0.450 3.153 0.591 335.772 0.356 2.630 0.799 0.61 247284. 0.0213
|
|
71.52 0.4951 -0.0133 -0.0001 0.0043 0.349 2.445 -0.024 260.332 0.276 -0.108 -0.042 0.61 247582. 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 0.0702 0.0195 2.191 13.812 18.468 1634.136 1.560 82.146 5.126 0.67 268194. 0.7626
|
|
2.75 0.0172 0.0604 0.0687 0.0195 2.199 13.862 18.077 1640.013 1.566 80.408 5.000 0.67 268314. 0.7358
|
|
5.51 0.0343 0.1177 0.0672 0.0196 2.204 13.894 17.666 1643.856 1.570 78.579 4.874 0.67 268440. 0.7092
|
|
8.26 0.0515 0.1721 0.0655 0.0196 2.207 13.908 17.235 1645.428 1.571 76.661 4.751 0.67 268574. 0.6828
|
|
11.01 0.0686 0.2235 0.0638 0.0196 2.205 13.900 16.783 1644.500 1.570 74.651 4.629 0.67 268715. 0.6564
|
|
13.77 0.0858 0.2721 0.0620 0.0195 2.200 13.869 16.310 1640.833 1.567 72.547 4.509 0.67 268864. 0.6303
|
|
16.52 0.1029 0.3179 0.0601 0.0195 2.191 13.812 15.815 1634.167 1.561 70.347 4.390 0.67 269020. 0.6043
|
|
19.28 0.1201 0.3610 0.0582 0.0193 2.178 13.728 15.298 1624.225 1.551 68.047 4.272 0.67 269185. 0.5784
|
|
22.03 0.1372 0.4014 0.0561 0.0192 2.160 13.614 14.759 1610.745 1.538 65.648 4.156 0.67 269358. 0.5527
|
|
24.78 0.1544 0.4390 0.0540 0.0190 2.137 13.469 14.197 1593.528 1.522 63.149 4.041 0.67 269539. 0.5271
|
|
27.54 0.1716 0.4741 0.0518 0.0187 2.109 13.291 13.614 1572.432 1.502 60.556 3.927 0.67 269729. 0.5016
|
|
30.29 0.1887 0.5064 0.0495 0.0184 2.075 13.078 13.011 1547.324 1.478 57.871 3.814 0.67 269928. 0.4762
|
|
33.04 0.2059 0.5361 0.0471 0.0181 2.036 12.831 12.387 1518.075 1.450 55.097 3.701 0.67 270136. 0.4509
|
|
35.80 0.2230 0.5631 0.0446 0.0177 1.991 12.548 11.744 1484.564 1.418 52.239 3.588 0.67 270353. 0.4257
|
|
38.55 0.2402 0.5873 0.0421 0.0172 1.940 12.228 11.083 1446.672 1.381 49.299 3.475 0.67 270579. 0.4005
|
|
41.30 0.2573 0.6086 0.0396 0.0167 1.883 11.869 10.405 1404.285 1.341 46.282 3.361 0.67 270815. 0.3753
|
|
44.06 0.2745 0.6268 0.0369 0.0162 1.820 11.472 9.711 1357.303 1.296 43.192 3.245 0.67 271060. 0.3500
|
|
46.81 0.2916 0.6417 0.0342 0.0155 1.751 11.036 9.000 1305.636 1.247 40.034 3.127 0.68 271316. 0.3247
|
|
49.57 0.3088 0.6529 0.0315 0.0149 1.675 10.559 8.276 1249.214 1.193 36.812 3.005 0.68 271581. 0.2992
|
|
52.32 0.3259 0.6602 0.0287 0.0141 1.593 10.041 7.539 1187.982 1.134 33.532 2.878 0.68 271857. 0.2736
|
|
55.07 0.3431 0.6627 0.0258 0.0134 1.505 9.483 6.790 1121.912 1.071 30.200 2.745 0.68 272142. 0.2476
|
|
57.83 0.3603 0.6598 0.0229 0.0125 1.409 8.883 6.031 1051.004 1.004 26.824 2.603 0.68 272439. 0.2212
|
|
60.58 0.3774 0.6501 0.0200 0.0116 1.308 8.243 5.263 975.294 0.931 23.411 2.448 0.68 272745. 0.1944
|
|
63.33 0.3946 0.6318 0.0171 0.0107 1.200 7.564 4.490 894.860 0.855 19.970 2.276 0.68 273063. 0.1669
|
|
66.09 0.4117 0.6023 0.0141 0.0096 1.086 6.845 3.712 809.830 0.773 16.511 2.079 0.68 273391. 0.1387
|
|
68.84 0.4289 0.5573 0.0111 0.0086 0.966 6.089 2.933 720.394 0.688 13.045 1.846 0.68 273730. 0.1095
|
|
71.59 0.4460 0.4894 0.0082 0.0075 0.841 5.298 2.155 626.813 0.599 9.585 1.559 0.68 274080. 0.0792
|
|
74.35 0.4632 0.3858 0.0053 0.0063 0.710 4.475 1.382 529.405 0.506 6.146 1.184 0.68 274441. 0.0482
|
|
77.10 0.4803 0.2202 0.0023 0.0051 0.575 3.621 0.615 428.454 0.409 2.737 0.651 0.68 274810. 0.0177
|
|
79.86 0.4975
|
|
|
|
|
|
|
|
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 0.0715 0.0198 2.973 17.034 22.758 2216.889 1.925 101.226 4.656 0.74 294986. 0.7689
|
|
3.03 0.0172 0.0604 0.0700 0.0199 2.983 17.090 22.277 2224.183 1.931 99.087 4.543 0.74 295119. 0.7422
|
|
6.06 0.0343 0.1178 0.0684 0.0199 2.989 17.125 21.771 2228.676 1.935 96.836 4.431 0.74 295259. 0.7156
|
|
9.09 0.0515 0.1722 0.0667 0.0200 2.991 17.135 21.240 2230.035 1.936 94.474 4.320 0.74 295408. 0.6892
|
|
12.12 0.0687 0.2238 0.0650 0.0199 2.988 17.119 20.683 2227.942 1.934 91.997 4.211 0.74 295565. 0.6629
|
|
15.16 0.0858 0.2726 0.0631 0.0199 2.980 17.074 20.100 2222.074 1.929 89.404 4.103 0.74 295730. 0.6367
|
|
18.19 0.1030 0.3186 0.0612 0.0198 2.966 16.997 19.490 2212.081 1.920 86.692 3.996 0.74 295904. 0.6107
|
|
21.22 0.1202 0.3619 0.0592 0.0197 2.947 16.886 18.853 2197.589 1.908 83.856 3.891 0.74 296086. 0.5848
|
|
24.25 0.1373 0.4026 0.0571 0.0195 2.921 16.737 18.187 2178.241 1.891 80.896 3.787 0.74 296278. 0.5591
|
|
27.28 0.1545 0.4406 0.0550 0.0193 2.888 16.549 17.494 2153.760 1.870 77.814 3.684 0.74 296479. 0.5334
|
|
30.31 0.1717 0.4760 0.0527 0.0190 2.848 16.320 16.774 2123.952 1.844 74.613 3.582 0.74 296690. 0.5079
|
|
33.34 0.1888 0.5088 0.0504 0.0187 2.801 16.049 16.029 2088.640 1.813 71.298 3.481 0.74 296910. 0.4824
|
|
36.37 0.2060 0.5390 0.0479 0.0183 2.746 15.734 15.259 2047.661 1.778 67.872 3.380 0.74 297140. 0.4570
|
|
39.40 0.2232 0.5665 0.0454 0.0179 2.683 15.374 14.465 2000.852 1.737 64.342 3.279 0.74 297380. 0.4317
|
|
42.43 0.2403 0.5912 0.0429 0.0174 2.612 14.969 13.649 1948.063 1.691 60.710 3.178 0.74 297631. 0.4064
|
|
45.47 0.2575 0.6131 0.0402 0.0169 2.533 14.516 12.811 1889.158 1.640 56.983 3.076 0.74 297892. 0.3811
|
|
48.50 0.2747 0.6319 0.0375 0.0163 2.446 14.015 11.952 1824.017 1.583 53.165 2.972 0.74 298163. 0.3557
|
|
51.53 0.2918 0.6475 0.0348 0.0157 2.350 13.466 11.075 1752.540 1.521 49.261 2.866 0.74 298445. 0.3302
|
|
54.56 0.3090 0.6594 0.0320 0.0150 2.246 12.868 10.179 1674.656 1.454 45.278 2.757 0.74 298738. 0.3045
|
|
57.59 0.3262 0.6674 0.0291 0.0142 2.133 12.220 9.268 1590.325 1.381 41.224 2.643 0.74 299043. 0.2786
|
|
60.62 0.3433 0.6706 0.0262 0.0134 2.011 11.522 8.342 1499.553 1.302 37.104 2.523 0.74 299358. 0.2523
|
|
63.65 0.3605 0.6681 0.0233 0.0125 1.881 10.776 7.403 1402.389 1.217 32.929 2.394 0.74 299685. 0.2255
|
|
66.68 0.3777 0.6588 0.0203 0.0116 1.742 9.981 6.454 1298.950 1.128 28.708 2.254 0.74 300023. 0.1982
|
|
69.71 0.3948 0.6407 0.0173 0.0106 1.595 9.139 5.497 1189.420 1.033 24.451 2.096 0.75 300373. 0.1701
|
|
72.75 0.4120 0.6107 0.0142 0.0096 1.440 8.253 4.535 1074.067 0.932 20.171 1.915 0.75 300735. 0.1412
|
|
75.78 0.4292 0.5644 0.0112 0.0085 1.278 7.325 3.571 953.254 0.828 15.882 1.699 0.75 301109. 0.1111
|
|
78.81 0.4463 0.4939 0.0082 0.0074 1.110 6.358 2.608 827.448 0.718 11.601 1.430 0.75 301495. 0.0799
|
|
81.84 0.4635 0.3854 0.0052 0.0062 0.935 5.357 1.651 697.208 0.605 7.344 1.074 0.75 301893. 0.0478
|
|
84.87 0.4807 0.2105 0.0022 0.0050 0.755 4.326 0.702 563.012 0.489 3.124 0.566 0.75 302299. 0.0164
|
|
87.90 0.4978
|
|
|
|
|
|
|
|
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 0.0731 0.0206 4.002 21.022 27.683 2984.605 2.375 123.132 4.207 0.81 321764. 0.7662
|
|
3.30 0.0171 0.0595 0.0715 0.0206 4.007 21.046 27.101 2988.021 2.378 120.547 4.114 0.81 321911. 0.7414
|
|
6.60 0.0343 0.1163 0.0699 0.0206 4.007 21.047 26.489 2988.163 2.378 117.825 4.021 0.81 322066. 0.7164
|
|
9.90 0.0514 0.1704 0.0682 0.0206 4.002 21.022 25.847 2984.631 2.375 114.966 3.928 0.81 322230. 0.6913
|
|
13.20 0.0685 0.2219 0.0664 0.0205 3.992 20.969 25.173 2976.999 2.369 111.967 3.835 0.81 322402. 0.6661
|
|
16.49 0.0856 0.2707 0.0646 0.0204 3.976 20.883 24.466 2964.821 2.359 108.826 3.743 0.81 322584. 0.6409
|
|
19.79 0.1028 0.3168 0.0626 0.0203 3.953 20.762 23.728 2947.625 2.346 105.540 3.651 0.81 322775. 0.6157
|
|
23.09 0.1199 0.3604 0.0606 0.0202 3.922 20.602 22.955 2924.890 2.328 102.104 3.560 0.81 322976. 0.5904
|
|
26.39 0.1370 0.4013 0.0585 0.0200 3.884 20.399 22.148 2896.134 2.305 98.515 3.469 0.81 323186. 0.5651
|
|
29.69 0.1541 0.4397 0.0562 0.0197 3.837 20.153 21.308 2861.217 2.277 94.776 3.378 0.81 323407. 0.5397
|
|
32.99 0.1713 0.4754 0.0539 0.0194 3.781 19.860 20.434 2819.648 2.244 90.892 3.287 0.81 323638. 0.5144
|
|
36.29 0.1884 0.5085 0.0516 0.0191 3.716 19.519 19.530 2771.162 2.205 86.867 3.196 0.81 323879. 0.4890
|
|
39.59 0.2055 0.5390 0.0491 0.0187 3.642 19.128 18.594 2715.632 2.161 82.708 3.106 0.81 324131. 0.4636
|
|
42.89 0.2226 0.5668 0.0465 0.0183 3.557 18.685 17.630 2652.737 2.111 78.420 3.014 0.81 324394. 0.4382
|
|
46.18 0.2398 0.5917 0.0439 0.0178 3.463 18.188 16.638 2582.284 2.055 74.008 2.922 0.81 324667. 0.4127
|
|
49.48 0.2569 0.6138 0.0412 0.0173 3.358 17.638 15.620 2504.147 1.993 69.478 2.829 0.81 324952. 0.3871
|
|
52.78 0.2740 0.6326 0.0385 0.0167 3.243 17.034 14.577 2418.340 1.924 64.837 2.734 0.81 325249. 0.3613
|
|
56.08 0.2912 0.6480 0.0357 0.0160 3.118 16.375 13.510 2324.761 1.850 60.091 2.636 0.81 325557. 0.3354
|
|
59.38 0.3083 0.6596 0.0328 0.0153 2.982 15.661 12.421 2223.453 1.769 55.247 2.534 0.81 325876. 0.3091
|
|
62.68 0.3254 0.6667 0.0299 0.0146 2.836 14.894 11.312 2114.512 1.683 50.314 2.426 0.81 326208. 0.2825
|
|
65.98 0.3425 0.6687 0.0269 0.0138 2.680 14.074 10.184 1998.151 1.590 45.300 2.312 0.81 326552. 0.2554
|
|
69.28 0.3597 0.6644 0.0239 0.0129 2.514 13.204 9.042 1874.599 1.492 40.217 2.188 0.81 326908. 0.2277
|
|
72.58 0.3768 0.6524 0.0208 0.0120 2.339 12.285 7.886 1744.194 1.388 35.075 2.051 0.81 327276. 0.1993
|
|
75.88 0.3939 0.6307 0.0177 0.0111 2.156 11.322 6.719 1607.399 1.279 29.888 1.896 0.81 327657. 0.1701
|
|
79.17 0.4110 0.5961 0.0146 0.0101 1.964 10.317 5.546 1464.790 1.166 24.670 1.717 0.81 328051. 0.1400
|
|
82.47 0.4282 0.5441 0.0115 0.0091 1.766 9.277 4.370 1317.053 1.048 19.438 1.505 0.81 328458. 0.1089
|
|
85.77 0.4453 0.4677 0.0084 0.0080 1.562 8.206 3.195 1165.001 0.927 14.212 1.244 0.81 328877. 0.0770
|
|
89.07 0.4624 0.3554 0.0053 0.0070 1.354 7.111 2.026 1009.548 0.803 9.011 0.910 0.82 329309. 0.0448
|
|
92.37 0.4795 0.1869 0.0023 0.0059 1.142 5.997 0.866 851.428 0.678 3.854 0.462 0.82 329751. 0.0149
|
|
95.67 0.4967
|
|
|
|
|
|
|
|
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 0.0750 0.0227 5.609 27.196 33.323 4182.908 3.073 148.221 3.613 0.87 348526. 0.7221
|
|
3.55 0.0170 0.0553 0.0734 0.0226 5.583 27.070 32.637 4163.489 3.058 145.170 3.555 0.87 348686. 0.7031
|
|
7.09 0.0340 0.1087 0.0718 0.0224 5.552 26.919 31.914 4140.220 3.041 141.954 3.496 0.87 348855. 0.6837
|
|
10.64 0.0510 0.1603 0.0701 0.0223 5.515 26.740 31.154 4112.779 3.021 138.574 3.436 0.87 349033. 0.6638
|
|
14.19 0.0680 0.2098 0.0683 0.0221 5.472 26.532 30.357 4080.758 2.998 135.026 3.374 0.87 349221. 0.6435
|
|
17.73 0.0850 0.2574 0.0664 0.0219 5.423 26.291 29.521 4043.749 2.970 131.308 3.311 0.87 349418. 0.6228
|
|
21.28 0.1020 0.3029 0.0644 0.0217 5.366 26.015 28.646 4001.269 2.939 127.415 3.247 0.87 349626. 0.6016
|
|
24.82 0.1190 0.3463 0.0624 0.0214 5.301 25.700 27.730 3952.790 2.904 123.344 3.182 0.87 349843. 0.5800
|
|
28.37 0.1360 0.3875 0.0602 0.0211 5.227 25.342 26.774 3897.731 2.863 119.091 3.116 0.87 350072. 0.5581
|
|
31.92 0.1530 0.4265 0.0580 0.0208 5.144 24.938 25.777 3835.587 2.817 114.656 3.048 0.88 350310. 0.5357
|
|
35.46 0.1700 0.4630 0.0556 0.0204 5.053 24.499 24.740 3768.029 2.768 110.045 2.978 0.88 350560. 0.5128
|
|
39.01 0.1869 0.4969 0.0532 0.0200 4.954 24.021 23.666 3694.538 2.714 105.265 2.905 0.88 350821. 0.4893
|
|
42.56 0.2039 0.5279 0.0507 0.0196 4.848 23.504 22.554 3615.101 2.656 100.322 2.830 0.88 351093. 0.4652
|
|
46.10 0.2209 0.5561 0.0482 0.0191 4.732 22.943 21.408 3528.807 2.592 95.222 2.752 0.88 351376. 0.4407
|
|
49.65 0.2379 0.5811 0.0455 0.0186 4.609 22.345 20.228 3436.757 2.525 89.973 2.670 0.88 351672. 0.4156
|
|
53.20 0.2549 0.6022 0.0428 0.0181 4.479 21.717 19.015 3340.251 2.454 84.579 2.582 0.88 351979. 0.3898
|
|
56.74 0.2719 0.6192 0.0400 0.0176 4.343 21.056 17.772 3238.523 2.379 79.051 2.489 0.88 352298. 0.3632
|
|
60.29 0.2889 0.6321 0.0371 0.0170 4.196 20.345 16.501 3129.215 2.299 73.396 2.392 0.88 352629. 0.3363
|
|
63.84 0.3059 0.6406 0.0342 0.0163 4.040 19.586 15.203 3012.438 2.213 67.623 2.289 0.88 352973. 0.3090
|
|
67.38 0.3229 0.6439 0.0312 0.0157 3.873 18.780 13.881 2888.413 2.122 61.743 2.180 0.88 353329. 0.2811
|
|
70.93 0.3399 0.6412 0.0282 0.0149 3.698 17.929 12.537 2757.644 2.026 55.766 2.062 0.88 353698. 0.2528
|
|
74.47 0.3569 0.6314 0.0251 0.0142 3.515 17.040 11.174 2620.844 1.925 49.704 1.934 0.88 354080. 0.2238
|
|
78.02 0.3739 0.6131 0.0220 0.0134 3.324 16.116 9.795 2478.781 1.821 43.570 1.792 0.88 354474. 0.1942
|
|
81.57 0.3909 0.5845 0.0189 0.0126 3.127 15.163 8.404 2332.124 1.713 37.380 1.634 0.88 354883. 0.1640
|
|
85.11 0.4079 0.5433 0.0158 0.0118 2.926 14.185 7.004 2181.797 1.603 31.152 1.456 0.88 355304. 0.1334
|
|
88.66 0.4249 0.4865 0.0126 0.0110 2.721 13.191 5.599 2028.880 1.490 24.905 1.252 0.88 355740. 0.1025
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92.21 0.4419 0.4104 0.0094 0.0102 2.514 12.187 4.196 1874.465 1.377 18.663 1.015 0.88 356188. 0.0720
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95.75 0.4589 0.3099 0.0063 0.0093 2.306 11.181 2.799 1719.703 1.263 12.449 0.738 0.88 356651. 0.0428
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99.30 0.4759 0.1783 0.0032 0.0085 2.099 10.178 1.414 1565.394 1.150 6.287 0.410 0.88 357125. 0.0169
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102.85 0.4929 0.0030 0.0000 0.0076 1.882 9.126 0.020 1403.590 1.031 0.090 0.007 0.88 357584. 0.0000
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PROP RPM = 14000
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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 0.0766 0.0272 8.390 37.773 39.485 6256.524 4.268 175.631 2.863 0.94 375285. 0.6227
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3.86 0.0172 0.0480 0.0750 0.0269 8.302 37.374 38.697 6190.528 4.223 172.125 2.835 0.94 375460. 0.6105
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7.73 0.0344 0.0951 0.0734 0.0266 8.204 36.935 37.862 6117.818 4.173 168.410 2.807 0.94 375645. 0.5979
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11.59 0.0516 0.1411 0.0717 0.0262 8.098 36.455 36.980 6038.346 4.119 164.486 2.778 0.94 375840. 0.5847
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15.45 0.0688 0.1861 0.0699 0.0258 7.982 35.934 36.050 5951.948 4.060 160.350 2.747 0.94 376047. 0.5710
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19.31 0.0859 0.2299 0.0680 0.0254 7.856 35.369 35.071 5858.427 3.996 155.998 2.715 0.94 376264. 0.5566
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|
23.18 0.1031 0.2725 0.0660 0.0250 7.721 34.760 34.044 5757.534 3.927 151.426 2.682 0.94 376492. 0.5417
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|
27.04 0.1203 0.3137 0.0639 0.0245 7.575 34.104 32.965 5648.936 3.853 146.630 2.647 0.94 376732. 0.5261
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30.90 0.1375 0.3536 0.0617 0.0240 7.419 33.400 31.836 5532.221 3.773 141.605 2.610 0.94 376984. 0.5098
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|
34.76 0.1547 0.3919 0.0595 0.0235 7.251 32.644 30.655 5406.975 3.688 136.352 2.571 0.94 377247. 0.4929
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|
38.63 0.1719 0.4286 0.0571 0.0229 7.071 31.835 29.424 5273.064 3.597 130.878 2.531 0.94 377523. 0.4752
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|
42.49 0.1891 0.4632 0.0546 0.0223 6.884 30.992 28.145 5133.344 3.501 125.191 2.487 0.94 377810. 0.4567
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|
46.35 0.2063 0.4951 0.0520 0.0217 6.696 30.145 26.821 4993.056 3.406 119.299 2.436 0.94 378110. 0.4368
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50.21 0.2234 0.5239 0.0494 0.0211 6.505 29.285 25.452 4850.682 3.309 113.210 2.380 0.94 378423. 0.4156
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54.08 0.2406 0.5497 0.0466 0.0204 6.306 28.390 24.042 4702.396 3.207 106.938 2.319 0.94 378749. 0.3936
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|
57.94 0.2578 0.5713 0.0438 0.0198 6.110 27.507 22.592 4556.132 3.108 100.488 2.249 0.94 379088. 0.3700
|
|
61.80 0.2750 0.5861 0.0409 0.0192 5.934 26.713 21.103 4424.706 3.018 93.866 2.163 0.94 379439. 0.3440
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|
65.66 0.2922 0.5925 0.0380 0.0187 5.785 26.046 19.577 4314.200 2.943 87.078 2.058 0.95 379805. 0.3152
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|
69.53 0.3094 0.5934 0.0349 0.0182 5.630 25.347 18.019 4198.442 2.864 80.150 1.947 0.95 380183. 0.2861
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|
73.39 0.3266 0.5879 0.0319 0.0177 5.471 24.629 16.433 4079.388 2.783 73.096 1.827 0.95 380576. 0.2564
|
|
77.25 0.3438 0.5755 0.0287 0.0172 5.306 23.887 14.823 3956.615 2.699 65.932 1.699 0.95 380982. 0.2265
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|
81.11 0.3610 0.5554 0.0256 0.0166 5.138 23.130 13.192 3831.195 2.613 58.676 1.562 0.95 381402. 0.1964
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|
84.98 0.3781 0.5266 0.0224 0.0161 4.967 22.363 11.544 3704.151 2.527 51.349 1.414 0.95 381837. 0.1663
|
|
88.84 0.3953 0.4882 0.0192 0.0155 4.797 21.595 9.886 3576.899 2.440 43.973 1.254 0.95 382286. 0.1364
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|
92.70 0.4125 0.4393 0.0159 0.0150 4.627 20.831 8.223 3450.393 2.353 36.575 1.081 0.95 382750. 0.1073
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|
96.56 0.4297 0.3789 0.0127 0.0144 4.459 20.076 6.561 3325.263 2.268 29.184 0.895 0.95 383229. 0.0794
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|
100.43 0.4469 0.3061 0.0095 0.0139 4.294 19.333 4.909 3202.322 2.184 21.833 0.695 0.95 383723. 0.0533
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|
104.29 0.4641 0.2202 0.0063 0.0134 4.133 18.607 3.272 3081.979 2.102 14.556 0.482 0.95 384232. 0.0302
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|
108.15 0.4813 0.1203 0.0032 0.0129 3.974 17.890 1.657 2963.182 2.021 7.372 0.254 0.95 384758. 0.0113
|
|
112.01 0.4985 0.0013 0.0000 0.0123 3.786 17.044 0.017 2823.061 1.926 0.074 0.003 0.95 385299. 0.0000
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