649 lines
115 KiB
Plaintext
649 lines
115 KiB
Plaintext
12x12N (12x12N.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 0.1204 0.0744 0.001 0.094 0.080 1.111 0.011 0.354 32.470 0.05 17467. 0.4478
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0.46 0.0402 0.0635 0.1199 0.0759 0.002 0.096 0.079 1.133 0.011 0.352 31.726 0.05 17486. 0.4367
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0.91 0.0803 0.1238 0.1194 0.0775 0.002 0.098 0.079 1.157 0.011 0.351 30.943 0.05 17507. 0.4250
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1.37 0.1205 0.1808 0.1188 0.0792 0.002 0.100 0.079 1.182 0.011 0.349 30.127 0.05 17532. 0.4128
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1.83 0.1606 0.2344 0.1181 0.0810 0.002 0.102 0.078 1.209 0.012 0.347 29.285 0.05 17561. 0.4001
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2.28 0.2008 0.2844 0.1173 0.0829 0.002 0.105 0.078 1.237 0.012 0.345 28.427 0.05 17592. 0.3870
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2.74 0.2410 0.3308 0.1163 0.0847 0.002 0.107 0.077 1.265 0.012 0.342 27.560 0.05 17628. 0.3737
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3.19 0.2811 0.3738 0.1152 0.0866 0.002 0.109 0.076 1.293 0.012 0.338 26.692 0.05 17668. 0.3600
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3.65 0.3213 0.4134 0.1137 0.0884 0.002 0.112 0.075 1.320 0.013 0.334 25.829 0.05 17712. 0.3462
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4.11 0.3615 0.4498 0.1120 0.0900 0.002 0.114 0.074 1.344 0.013 0.329 24.978 0.05 17759. 0.3322
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4.56 0.4016 0.4830 0.1099 0.0914 0.002 0.115 0.073 1.365 0.013 0.323 24.141 0.05 17812. 0.3181
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5.02 0.4418 0.5133 0.1075 0.0925 0.002 0.117 0.071 1.381 0.013 0.316 23.321 0.05 17868. 0.3039
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5.48 0.4819 0.5406 0.1046 0.0932 0.002 0.118 0.069 1.392 0.013 0.307 22.518 0.05 17929. 0.2895
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5.93 0.5221 0.5652 0.1012 0.0935 0.002 0.118 0.067 1.396 0.013 0.298 21.732 0.05 17994. 0.2749
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6.39 0.5623 0.5871 0.0974 0.0933 0.002 0.118 0.064 1.393 0.013 0.286 20.960 0.05 18064. 0.2600
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6.85 0.6024 0.6062 0.0930 0.0924 0.002 0.117 0.061 1.380 0.013 0.273 20.198 0.05 18138. 0.2449
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7.30 0.6426 0.6224 0.0881 0.0910 0.002 0.115 0.058 1.358 0.013 0.259 19.443 0.05 18216. 0.2294
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7.76 0.6827 0.6357 0.0827 0.0888 0.002 0.112 0.055 1.326 0.013 0.243 18.689 0.05 18298. 0.2136
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8.21 0.7229 0.6456 0.0769 0.0861 0.002 0.109 0.051 1.285 0.012 0.226 17.928 0.05 18384. 0.1976
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8.67 0.7631 0.6519 0.0707 0.0827 0.002 0.104 0.047 1.236 0.012 0.208 17.149 0.05 18475. 0.1812
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9.13 0.8032 0.6538 0.0642 0.0789 0.002 0.100 0.042 1.179 0.011 0.189 16.340 0.05 18569. 0.1646
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9.58 0.8434 0.6506 0.0576 0.0746 0.001 0.094 0.038 1.115 0.011 0.169 15.485 0.05 18667. 0.1477
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10.04 0.8836 0.6411 0.0507 0.0699 0.001 0.088 0.034 1.044 0.010 0.149 14.564 0.05 18769. 0.1304
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10.50 0.9237 0.6235 0.0437 0.0648 0.001 0.082 0.029 0.968 0.009 0.129 13.550 0.05 18874. 0.1126
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10.95 0.9639 0.5955 0.0366 0.0593 0.001 0.075 0.024 0.885 0.008 0.108 12.401 0.05 18983. 0.0943
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11.41 1.0040 0.5531 0.0294 0.0534 0.001 0.067 0.019 0.798 0.008 0.086 11.059 0.05 19096. 0.0754
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11.87 1.0442 0.4903 0.0222 0.0472 0.001 0.060 0.015 0.705 0.007 0.065 9.425 0.05 19212. 0.0558
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12.32 1.0844 0.3961 0.0148 0.0406 0.001 0.051 0.010 0.607 0.006 0.044 7.333 0.05 19332. 0.0355
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12.78 1.1245 0.2505 0.0075 0.0338 0.001 0.043 0.005 0.504 0.005 0.022 4.471 0.05 19455. 0.0154
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13.24 1.1647 0.0103 0.0002 0.0267 0.001 0.034 0.000 0.398 0.004 0.001 0.178 0.05 19582. 0.0001
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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 0.1209 0.0664 0.011 0.335 0.320 7.933 0.038 1.422 18.279 0.10 34934. 0.5053
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0.92 0.0406 0.0720 0.1205 0.0679 0.011 0.343 0.319 8.113 0.039 1.417 17.812 0.10 34972. 0.4916
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1.84 0.0811 0.1400 0.1201 0.0696 0.011 0.351 0.317 8.310 0.040 1.412 17.323 0.10 35016. 0.4772
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2.77 0.1217 0.2038 0.1195 0.0713 0.011 0.360 0.316 8.523 0.041 1.405 16.815 0.10 35066. 0.4622
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3.69 0.1622 0.2634 0.1189 0.0732 0.012 0.370 0.314 8.748 0.042 1.398 16.294 0.10 35123. 0.4466
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4.61 0.2028 0.3185 0.1181 0.0752 0.012 0.380 0.312 8.982 0.043 1.389 15.765 0.10 35188. 0.4307
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5.53 0.2433 0.3694 0.1172 0.0772 0.012 0.390 0.310 9.220 0.044 1.378 15.235 0.10 35261. 0.4146
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6.45 0.2839 0.4161 0.1160 0.0792 0.013 0.400 0.307 9.456 0.045 1.364 14.709 0.10 35341. 0.3983
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7.37 0.3245 0.4587 0.1146 0.0810 0.013 0.409 0.303 9.682 0.046 1.347 14.190 0.10 35430. 0.3819
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8.30 0.3650 0.4976 0.1129 0.0828 0.013 0.418 0.298 9.890 0.047 1.327 13.682 0.10 35528. 0.3654
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9.22 0.4056 0.5329 0.1108 0.0843 0.014 0.426 0.293 10.072 0.048 1.303 13.188 0.10 35634. 0.3489
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10.14 0.4461 0.5649 0.1083 0.0855 0.014 0.432 0.286 10.218 0.049 1.273 12.709 0.10 35749. 0.3325
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11.06 0.4867 0.5938 0.1054 0.0864 0.014 0.436 0.279 10.319 0.049 1.239 12.245 0.10 35873. 0.3160
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11.98 0.5272 0.6197 0.1020 0.0868 0.014 0.438 0.270 10.366 0.049 1.199 11.796 0.10 36006. 0.2995
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12.90 0.5678 0.6428 0.0981 0.0866 0.014 0.437 0.259 10.349 0.049 1.153 11.362 0.10 36148. 0.2829
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13.83 0.6084 0.6631 0.0936 0.0859 0.014 0.433 0.247 10.257 0.049 1.100 10.940 0.10 36298. 0.2661
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14.75 0.6489 0.6807 0.0886 0.0844 0.014 0.426 0.234 10.084 0.048 1.041 10.529 0.10 36457. 0.2491
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15.67 0.6895 0.6956 0.0830 0.0823 0.013 0.415 0.219 9.831 0.047 0.976 10.126 0.10 36624. 0.2320
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16.59 0.7300 0.7075 0.0771 0.0795 0.013 0.402 0.204 9.502 0.045 0.906 9.727 0.10 36800. 0.2147
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17.51 0.7706 0.7161 0.0708 0.0762 0.012 0.385 0.187 9.102 0.043 0.833 9.327 0.10 36984. 0.1973
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18.44 0.8111 0.7210 0.0643 0.0723 0.012 0.365 0.170 8.638 0.041 0.756 8.921 0.10 37175. 0.1798
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19.36 0.8517 0.7213 0.0575 0.0679 0.011 0.343 0.152 8.114 0.039 0.676 8.500 0.10 37375. 0.1621
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20.28 0.8923 0.7160 0.0506 0.0631 0.010 0.318 0.134 7.534 0.036 0.595 8.054 0.10 37582. 0.1440
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21.20 0.9328 0.7034 0.0436 0.0578 0.009 0.292 0.115 6.900 0.033 0.512 7.569 0.10 37797. 0.1256
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22.12 0.9734 0.6811 0.0364 0.0520 0.008 0.263 0.096 6.215 0.030 0.428 7.023 0.10 38019. 0.1065
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23.04 1.0139 0.6446 0.0292 0.0459 0.007 0.232 0.077 5.482 0.026 0.343 6.381 0.10 38249. 0.0866
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23.97 1.0545 0.5865 0.0219 0.0394 0.006 0.199 0.058 4.702 0.022 0.257 5.582 0.10 38485. 0.0657
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24.89 1.0950 0.4919 0.0146 0.0325 0.005 0.164 0.039 3.880 0.019 0.172 4.509 0.10 38729. 0.0433
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25.81 1.1356 0.3283 0.0073 0.0253 0.004 0.128 0.019 3.018 0.014 0.086 2.901 0.10 38980. 0.0197
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26.73 1.1762 0.0049 0.0001 0.0178 0.003 0.090 0.000 2.123 0.010 0.001 0.041 0.10 39237. 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 0.1212 0.0631 0.034 0.717 0.721 25.445 0.081 3.207 12.851 0.14 52401. 0.5335
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1.39 0.0407 0.0761 0.1208 0.0646 0.035 0.734 0.719 26.061 0.083 3.196 12.507 0.14 52458. 0.5184
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2.78 0.0814 0.1478 0.1204 0.0663 0.036 0.753 0.716 26.737 0.085 3.185 12.146 0.14 52524. 0.5025
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4.16 0.1222 0.2149 0.1199 0.0681 0.037 0.774 0.713 27.468 0.087 3.171 11.773 0.14 52600. 0.4860
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5.55 0.1629 0.2773 0.1193 0.0701 0.038 0.796 0.709 28.243 0.090 3.155 11.390 0.14 52686. 0.4691
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6.94 0.2036 0.3349 0.1185 0.0721 0.039 0.818 0.705 29.051 0.092 3.135 11.004 0.14 52784. 0.4517
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8.33 0.2443 0.3877 0.1176 0.0741 0.040 0.842 0.699 29.873 0.095 3.111 10.618 0.14 52893. 0.4342
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9.72 0.2851 0.4360 0.1164 0.0761 0.041 0.865 0.693 30.690 0.098 3.080 10.235 0.14 53015. 0.4165
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11.11 0.3258 0.4800 0.1150 0.0781 0.042 0.887 0.684 31.475 0.100 3.043 9.860 0.14 53149. 0.3988
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12.49 0.3665 0.5200 0.1133 0.0799 0.043 0.907 0.674 32.201 0.102 2.998 9.494 0.14 53297. 0.3811
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13.88 0.4072 0.5562 0.1113 0.0815 0.044 0.925 0.662 32.839 0.105 2.943 9.139 0.14 53457. 0.3635
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15.27 0.4479 0.5889 0.1088 0.0827 0.045 0.940 0.647 33.356 0.106 2.878 8.797 0.14 53631. 0.3460
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16.66 0.4887 0.6184 0.1059 0.0836 0.045 0.950 0.630 33.721 0.107 2.800 8.468 0.14 53819. 0.3285
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18.05 0.5294 0.6449 0.1024 0.0841 0.045 0.955 0.609 33.900 0.108 2.710 8.151 0.14 54019. 0.3111
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19.44 0.5701 0.6685 0.0985 0.0840 0.045 0.954 0.586 33.858 0.108 2.605 7.846 0.15 54234. 0.2936
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20.82 0.6108 0.6894 0.0940 0.0832 0.045 0.946 0.559 33.560 0.107 2.486 7.552 0.15 54461. 0.2760
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22.21 0.6515 0.7078 0.0889 0.0818 0.044 0.929 0.529 32.986 0.105 2.351 7.268 0.15 54701. 0.2584
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23.60 0.6923 0.7235 0.0833 0.0797 0.043 0.905 0.495 32.135 0.102 2.204 6.993 0.15 54954. 0.2407
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24.99 0.7330 0.7364 0.0773 0.0769 0.042 0.874 0.460 31.021 0.099 2.045 6.723 0.15 55220. 0.2229
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26.38 0.7737 0.7464 0.0710 0.0736 0.040 0.836 0.422 29.664 0.094 1.878 6.455 0.15 55497. 0.2051
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27.76 0.8144 0.7529 0.0644 0.0697 0.038 0.791 0.383 28.082 0.089 1.704 6.186 0.15 55787. 0.1872
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29.15 0.8552 0.7554 0.0576 0.0652 0.035 0.741 0.343 26.292 0.084 1.524 5.910 0.15 56088. 0.1692
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30.54 0.8959 0.7527 0.0507 0.0603 0.033 0.685 0.301 24.304 0.077 1.340 5.622 0.15 56401. 0.1509
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31.93 0.9366 0.7435 0.0436 0.0549 0.030 0.623 0.259 22.129 0.070 1.153 5.311 0.15 56726. 0.1322
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33.32 0.9773 0.7251 0.0364 0.0490 0.027 0.557 0.216 19.773 0.063 0.963 4.964 0.15 57062. 0.1129
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34.71 1.0180 0.6934 0.0291 0.0428 0.023 0.486 0.173 17.246 0.055 0.771 4.557 0.15 57408. 0.0928
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36.09 1.0588 0.6404 0.0218 0.0361 0.020 0.410 0.130 14.557 0.046 0.578 4.047 0.15 57766. 0.0713
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37.48 1.0995 0.5498 0.0145 0.0291 0.016 0.330 0.086 11.718 0.037 0.384 3.346 0.15 58135. 0.0481
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38.87 1.1402 0.3813 0.0073 0.0217 0.012 0.246 0.043 8.742 0.028 0.192 2.237 0.15 58513. 0.0227
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40.26 1.1809 0.0028 0.0000 0.0140 0.008 0.159 0.000 5.649 0.018 0.001 0.016 0.15 58901. 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 0.1214 0.0613 0.079 1.237 1.284 58.563 0.140 5.710 9.942 0.19 69867. 0.5508
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1.86 0.0408 0.0786 0.1210 0.0628 0.081 1.269 1.280 60.036 0.143 5.692 9.669 0.19 69943. 0.5348
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3.71 0.0816 0.1526 0.1206 0.0645 0.083 1.303 1.275 61.654 0.147 5.672 9.382 0.19 70032. 0.5181
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5.57 0.1224 0.2217 0.1201 0.0663 0.085 1.340 1.270 63.403 0.151 5.649 9.086 0.19 70133. 0.5007
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7.42 0.1633 0.2857 0.1195 0.0683 0.088 1.379 1.264 65.265 0.156 5.621 8.783 0.19 70249. 0.4828
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9.28 0.2041 0.3447 0.1188 0.0703 0.090 1.420 1.256 67.206 0.160 5.587 8.477 0.19 70379. 0.4646
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11.13 0.2449 0.3988 0.1179 0.0724 0.093 1.462 1.247 69.188 0.165 5.545 8.172 0.19 70526. 0.4461
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12.99 0.2857 0.4481 0.1168 0.0745 0.095 1.504 1.235 71.158 0.170 5.492 7.870 0.19 70689. 0.4276
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14.84 0.3265 0.4929 0.1154 0.0764 0.098 1.544 1.220 73.057 0.174 5.427 7.575 0.19 70868. 0.4091
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16.70 0.3673 0.5335 0.1137 0.0783 0.100 1.581 1.202 74.819 0.179 5.347 7.288 0.19 71066. 0.3907
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18.55 0.4082 0.5702 0.1116 0.0799 0.102 1.614 1.180 76.371 0.182 5.250 7.010 0.19 71281. 0.3724
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20.41 0.4490 0.6033 0.1092 0.0812 0.104 1.641 1.154 77.638 0.185 5.134 6.743 0.19 71514. 0.3542
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22.26 0.4898 0.6332 0.1062 0.0822 0.105 1.660 1.123 78.541 0.188 4.997 6.487 0.19 71765. 0.3362
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24.12 0.5306 0.6600 0.1028 0.0827 0.106 1.669 1.087 78.999 0.189 4.836 6.242 0.19 72034. 0.3182
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25.97 0.5714 0.6839 0.0989 0.0826 0.106 1.668 1.045 78.925 0.188 4.649 6.006 0.19 72320. 0.3002
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27.83 0.6122 0.7052 0.0943 0.0819 0.105 1.653 0.997 78.241 0.187 4.435 5.780 0.19 72625. 0.2822
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29.68 0.6531 0.7240 0.0892 0.0805 0.103 1.625 0.943 76.892 0.184 4.195 5.563 0.19 72947. 0.2642
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31.54 0.6939 0.7403 0.0836 0.0784 0.100 1.582 0.884 74.876 0.179 3.931 5.354 0.19 73285. 0.2461
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33.39 0.7347 0.7539 0.0776 0.0756 0.097 1.526 0.820 72.228 0.172 3.648 5.150 0.20 73641. 0.2280
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35.25 0.7755 0.7648 0.0712 0.0722 0.093 1.458 0.753 68.995 0.165 3.349 4.949 0.20 74013. 0.2100
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37.11 0.8163 0.7725 0.0646 0.0682 0.087 1.378 0.683 65.219 0.156 3.037 4.749 0.20 74401. 0.1919
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38.96 0.8571 0.7764 0.0578 0.0638 0.082 1.288 0.611 60.936 0.145 2.716 4.546 0.20 74804. 0.1737
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40.82 0.8980 0.7756 0.0508 0.0588 0.075 1.187 0.537 56.174 0.134 2.388 4.335 0.20 75223. 0.1553
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42.67 0.9388 0.7687 0.0437 0.0533 0.068 1.077 0.462 50.954 0.122 2.053 4.109 0.20 75658. 0.1365
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44.53 0.9796 0.7534 0.0365 0.0474 0.061 0.957 0.385 45.297 0.108 1.714 3.859 0.20 76107. 0.1172
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46.38 1.0204 0.7254 0.0292 0.0410 0.053 0.829 0.308 39.224 0.094 1.372 3.567 0.20 76572. 0.0969
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48.24 1.0612 0.6768 0.0219 0.0343 0.044 0.692 0.231 32.756 0.078 1.028 3.201 0.20 77051. 0.0752
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50.09 1.1020 0.5906 0.0145 0.0271 0.035 0.548 0.154 25.922 0.062 0.684 2.689 0.20 77544. 0.0516
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51.95 1.1428 0.4217 0.0072 0.0196 0.025 0.396 0.077 18.760 0.045 0.341 1.852 0.20 78051. 0.0251
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53.80 1.1837 0.0018 0.0000 0.0118 0.015 0.239 0.000 11.311 0.027 0.001 0.008 0.20 78569. 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 0.1216 0.0601 0.151 1.897 2.008 112.232 0.214 8.934 8.117 0.24 87333. 0.5625
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2.32 0.0409 0.0804 0.1212 0.0617 0.154 1.946 2.003 115.124 0.220 8.908 7.890 0.24 87428. 0.5460
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4.65 0.0818 0.1559 0.1208 0.0634 0.159 2.000 1.996 118.305 0.226 8.878 7.652 0.24 87539. 0.5286
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6.97 0.1227 0.2263 0.1203 0.0652 0.163 2.058 1.988 121.752 0.233 8.843 7.406 0.24 87666. 0.5106
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9.29 0.1635 0.2915 0.1198 0.0672 0.168 2.120 1.979 125.424 0.240 8.801 7.155 0.24 87811. 0.4922
|
|
11.62 0.2044 0.3515 0.1191 0.0693 0.173 2.185 1.967 129.261 0.247 8.749 6.902 0.24 87975. 0.4733
|
|
13.94 0.2453 0.4063 0.1182 0.0714 0.179 2.251 1.953 133.183 0.254 8.685 6.650 0.24 88158. 0.4543
|
|
16.26 0.2862 0.4563 0.1171 0.0734 0.184 2.317 1.934 137.090 0.262 8.604 6.400 0.24 88362. 0.4353
|
|
18.59 0.3271 0.5016 0.1157 0.0755 0.189 2.381 1.912 140.865 0.269 8.504 6.156 0.24 88588. 0.4162
|
|
20.91 0.3680 0.5426 0.1141 0.0774 0.194 2.441 1.884 144.374 0.276 8.381 5.920 0.24 88835. 0.3973
|
|
23.23 0.4089 0.5796 0.1120 0.0790 0.198 2.493 1.851 147.475 0.282 8.231 5.691 0.24 89105. 0.3786
|
|
25.55 0.4498 0.6130 0.1096 0.0804 0.201 2.536 1.810 150.016 0.287 8.050 5.472 0.24 89397. 0.3600
|
|
27.88 0.4906 0.6431 0.1066 0.0814 0.204 2.567 1.762 151.842 0.290 7.836 5.262 0.24 89711. 0.3415
|
|
30.20 0.5315 0.6702 0.1032 0.0819 0.205 2.583 1.705 152.790 0.292 7.584 5.062 0.24 90049. 0.3232
|
|
32.52 0.5724 0.6944 0.0992 0.0818 0.205 2.581 1.639 152.689 0.292 7.292 4.870 0.24 90408. 0.3049
|
|
34.85 0.6133 0.7159 0.0947 0.0811 0.203 2.559 1.564 151.380 0.289 6.957 4.686 0.24 90790. 0.2866
|
|
37.17 0.6542 0.7350 0.0895 0.0797 0.199 2.515 1.479 148.759 0.284 6.580 4.511 0.24 91194. 0.2683
|
|
39.49 0.6951 0.7517 0.0839 0.0776 0.194 2.448 1.386 144.818 0.277 6.166 4.342 0.24 91619. 0.2500
|
|
41.82 0.7360 0.7659 0.0779 0.0748 0.187 2.360 1.286 139.625 0.267 5.721 4.178 0.24 92065. 0.2317
|
|
44.14 0.7769 0.7775 0.0715 0.0714 0.179 2.253 1.181 133.270 0.255 5.251 4.018 0.25 92531. 0.2135
|
|
46.46 0.8177 0.7860 0.0648 0.0674 0.169 2.127 1.071 125.839 0.240 4.762 3.859 0.25 93017. 0.1952
|
|
48.79 0.8586 0.7910 0.0579 0.0629 0.157 1.985 0.957 117.399 0.224 4.258 3.698 0.25 93524. 0.1769
|
|
51.11 0.8995 0.7916 0.0509 0.0579 0.145 1.826 0.841 108.005 0.206 3.742 3.533 0.25 94049. 0.1585
|
|
53.43 0.9404 0.7865 0.0438 0.0523 0.131 1.652 0.723 97.700 0.187 3.217 3.358 0.25 94594. 0.1396
|
|
55.76 0.9813 0.7734 0.0365 0.0464 0.116 1.463 0.604 86.524 0.165 2.685 3.164 0.25 95158. 0.1202
|
|
58.08 1.0222 0.7484 0.0292 0.0399 0.100 1.260 0.483 74.516 0.142 2.148 2.939 0.25 95740. 0.0999
|
|
60.40 1.0631 0.7035 0.0219 0.0331 0.083 1.043 0.362 61.724 0.118 1.608 2.657 0.25 96341. 0.0781
|
|
62.72 1.1039 0.6211 0.0145 0.0258 0.065 0.815 0.240 48.204 0.092 1.068 2.259 0.25 96959. 0.0541
|
|
65.05 1.1448 0.4529 0.0072 0.0182 0.046 0.575 0.119 34.031 0.065 0.530 1.588 0.25 97595. 0.0268
|
|
67.37 1.1857 -0.0040 0.0000 0.0103 0.026 0.326 -0.001 19.286 0.037 -0.003 -0.014 0.25 98244. 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 0.1217 0.0594 0.257 2.697 2.896 191.477 0.305 12.881 6.860 0.29 104799. 0.5708
|
|
2.79 0.0409 0.0815 0.1214 0.0609 0.263 2.768 2.888 196.491 0.313 12.845 6.666 0.29 104913. 0.5539
|
|
5.58 0.0819 0.1581 0.1210 0.0626 0.271 2.846 2.879 202.017 0.322 12.805 6.463 0.29 105046. 0.5362
|
|
8.37 0.1228 0.2295 0.1206 0.0645 0.279 2.930 2.868 208.013 0.331 12.757 6.254 0.29 105199. 0.5178
|
|
11.16 0.1637 0.2955 0.1200 0.0665 0.288 3.020 2.855 214.411 0.341 12.699 6.039 0.29 105373. 0.4990
|
|
13.95 0.2046 0.3562 0.1193 0.0686 0.297 3.115 2.839 221.109 0.352 12.627 5.823 0.29 105569. 0.4798
|
|
16.74 0.2456 0.4116 0.1185 0.0707 0.306 3.211 2.819 227.968 0.363 12.537 5.608 0.29 105790. 0.4604
|
|
19.53 0.2865 0.4620 0.1174 0.0728 0.315 3.308 2.793 234.816 0.374 12.425 5.396 0.29 106035. 0.4409
|
|
22.32 0.3274 0.5077 0.1161 0.0749 0.324 3.401 2.762 241.445 0.384 12.284 5.188 0.29 106305. 0.4216
|
|
25.11 0.3683 0.5490 0.1144 0.0768 0.332 3.488 2.722 247.623 0.394 12.109 4.987 0.29 106603. 0.4023
|
|
27.90 0.4093 0.5863 0.1124 0.0785 0.339 3.565 2.674 253.098 0.403 11.896 4.793 0.29 106927. 0.3832
|
|
30.69 0.4502 0.6199 0.1100 0.0799 0.345 3.629 2.616 257.606 0.410 11.638 4.607 0.29 107278. 0.3644
|
|
33.48 0.4911 0.6502 0.1071 0.0809 0.350 3.675 2.547 260.870 0.415 11.331 4.429 0.29 107656. 0.3457
|
|
36.27 0.5320 0.6774 0.1037 0.0814 0.352 3.699 2.466 262.604 0.418 10.969 4.259 0.29 108062. 0.3271
|
|
39.06 0.5730 0.7018 0.0997 0.0814 0.352 3.698 2.372 262.510 0.418 10.549 4.098 0.29 108494. 0.3086
|
|
41.86 0.6139 0.7235 0.0951 0.0807 0.349 3.667 2.263 260.308 0.414 10.066 3.943 0.29 108953. 0.2901
|
|
44.65 0.6548 0.7429 0.0900 0.0793 0.343 3.604 2.141 255.812 0.407 9.522 3.796 0.29 109439. 0.2715
|
|
47.44 0.6957 0.7599 0.0843 0.0772 0.334 3.508 2.006 249.008 0.396 8.923 3.654 0.29 109950. 0.2531
|
|
50.23 0.7367 0.7746 0.0782 0.0744 0.322 3.381 1.861 240.010 0.382 8.280 3.518 0.29 110486. 0.2347
|
|
53.02 0.7776 0.7867 0.0718 0.0710 0.307 3.226 1.709 228.977 0.364 7.600 3.385 0.29 111046. 0.2163
|
|
55.81 0.8185 0.7959 0.0651 0.0670 0.290 3.044 1.550 216.053 0.344 6.893 3.253 0.30 111631. 0.1980
|
|
58.60 0.8594 0.8018 0.0582 0.0624 0.270 2.837 1.386 201.359 0.320 6.164 3.121 0.30 112240. 0.1797
|
|
61.39 0.9004 0.8036 0.0512 0.0574 0.248 2.606 1.218 184.989 0.294 5.417 2.986 0.30 112872. 0.1611
|
|
64.18 0.9413 0.8000 0.0440 0.0518 0.224 2.353 1.047 167.018 0.266 4.657 2.844 0.30 113527. 0.1423
|
|
66.97 0.9822 0.7889 0.0367 0.0457 0.198 2.078 0.874 147.516 0.235 3.887 2.687 0.30 114205. 0.1228
|
|
69.76 1.0231 0.7664 0.0294 0.0392 0.170 1.783 0.699 126.553 0.201 3.110 2.506 0.30 114905. 0.1025
|
|
72.55 1.0641 0.7249 0.0220 0.0323 0.140 1.468 0.524 104.210 0.166 2.329 2.279 0.30 115626. 0.0806
|
|
75.34 1.1050 0.6467 0.0146 0.0250 0.108 1.135 0.348 80.588 0.128 1.548 1.958 0.30 116370. 0.0565
|
|
78.13 1.1459 0.4815 0.0073 0.0173 0.075 0.786 0.173 55.818 0.089 0.770 1.406 0.30 117134. 0.0286
|
|
80.92 1.1868 -0.0009 0.0000 0.0093 0.040 0.423 0.000 30.045 0.048 -0.001 -0.003 0.31 117913. 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 0.1219 0.0589 0.404 3.640 3.947 301.448 0.411 17.555 5.938 0.33 122264. 0.5769
|
|
3.26 0.0410 0.0824 0.1216 0.0604 0.415 3.736 3.936 309.432 0.422 17.509 5.770 0.33 122397. 0.5598
|
|
6.52 0.0819 0.1598 0.1212 0.0621 0.427 3.843 3.925 318.244 0.434 17.456 5.593 0.33 122552. 0.5418
|
|
9.78 0.1229 0.2319 0.1208 0.0640 0.440 3.958 3.911 327.824 0.447 17.395 5.411 0.33 122730. 0.5232
|
|
13.03 0.1638 0.2985 0.1203 0.0660 0.453 4.082 3.894 338.066 0.461 17.320 5.224 0.33 122934. 0.5041
|
|
16.29 0.2048 0.3597 0.1196 0.0681 0.468 4.212 3.873 348.810 0.476 17.227 5.036 0.33 123163. 0.4846
|
|
19.55 0.2458 0.4155 0.1188 0.0703 0.483 4.345 3.846 359.836 0.491 17.109 4.848 0.33 123420. 0.4650
|
|
22.81 0.2867 0.4663 0.1178 0.0724 0.497 4.478 3.813 370.866 0.506 16.961 4.663 0.33 123707. 0.4453
|
|
26.07 0.3277 0.5123 0.1165 0.0745 0.512 4.607 3.771 381.569 0.521 16.774 4.483 0.34 124023. 0.4256
|
|
29.33 0.3687 0.5538 0.1148 0.0765 0.525 4.728 3.719 391.569 0.534 16.541 4.308 0.34 124370. 0.4062
|
|
32.58 0.4096 0.5912 0.1129 0.0782 0.537 4.835 3.654 400.457 0.546 16.255 4.139 0.34 124749. 0.3869
|
|
35.84 0.4506 0.6250 0.1104 0.0796 0.547 4.924 3.576 407.804 0.556 15.907 3.978 0.34 125159. 0.3678
|
|
39.10 0.4915 0.6554 0.1076 0.0807 0.554 4.989 3.483 413.162 0.564 15.492 3.824 0.34 125601. 0.3489
|
|
42.36 0.5325 0.6828 0.1042 0.0812 0.558 5.024 3.373 416.068 0.568 15.002 3.677 0.34 126075. 0.3302
|
|
45.62 0.5735 0.7073 0.1002 0.0812 0.558 5.024 3.244 416.042 0.568 14.430 3.537 0.34 126581. 0.3115
|
|
48.88 0.6144 0.7293 0.0956 0.0806 0.553 4.982 3.096 412.629 0.563 13.773 3.404 0.34 127118. 0.2928
|
|
52.13 0.6554 0.7489 0.0905 0.0792 0.544 4.897 2.930 405.529 0.553 13.030 3.277 0.34 127685. 0.2742
|
|
55.39 0.6964 0.7662 0.0848 0.0771 0.529 4.766 2.746 394.713 0.538 12.213 3.155 0.34 128282. 0.2556
|
|
58.65 0.7373 0.7812 0.0787 0.0743 0.510 4.593 2.548 380.363 0.519 11.333 3.038 0.34 128909. 0.2371
|
|
61.91 0.7783 0.7938 0.0722 0.0708 0.486 4.380 2.339 362.730 0.495 10.403 2.925 0.34 129564. 0.2187
|
|
65.17 0.8192 0.8036 0.0655 0.0668 0.459 4.130 2.121 342.051 0.467 9.435 2.813 0.34 130248. 0.2003
|
|
68.43 0.8602 0.8103 0.0586 0.0622 0.427 3.846 1.897 318.515 0.435 8.437 2.701 0.35 130960. 0.1819
|
|
71.68 0.9012 0.8130 0.0515 0.0571 0.392 3.529 1.667 292.275 0.399 7.415 2.587 0.35 131698. 0.1633
|
|
74.94 0.9421 0.8107 0.0443 0.0514 0.353 3.181 1.433 263.452 0.359 6.375 2.467 0.35 132464. 0.1444
|
|
78.20 0.9831 0.8012 0.0369 0.0453 0.311 2.803 1.196 232.157 0.317 5.320 2.337 0.35 133256. 0.1250
|
|
81.46 1.0241 0.7808 0.0296 0.0388 0.266 2.397 0.957 198.504 0.271 4.256 2.186 0.35 134074. 0.1046
|
|
84.72 1.0650 0.7421 0.0221 0.0318 0.218 1.964 0.716 162.623 0.222 3.186 1.998 0.35 134918. 0.0827
|
|
87.98 1.1060 0.6675 0.0147 0.0243 0.167 1.505 0.476 124.680 0.170 2.116 1.731 0.35 135786. 0.0584
|
|
91.23 1.1469 0.5048 0.0073 0.0166 0.114 1.025 0.236 84.886 0.116 1.051 1.262 0.35 136679. 0.0300
|
|
94.49 1.1879 -0.0041 0.0000 0.0085 0.058 0.525 -0.001 43.470 0.059 -0.004 -0.010 0.36 137589. 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 0.1221 0.0585 0.600 4.728 5.162 447.462 0.534 22.960 5.232 0.38 139728. 0.5813
|
|
3.75 0.0413 0.0836 0.1217 0.0601 0.616 4.855 5.149 459.485 0.548 22.902 5.083 0.38 139882. 0.5639
|
|
7.50 0.0825 0.1620 0.1214 0.0618 0.634 4.995 5.134 472.788 0.564 22.837 4.926 0.38 140060. 0.5457
|
|
11.26 0.1238 0.2350 0.1210 0.0637 0.653 5.148 5.117 487.284 0.582 22.761 4.763 0.38 140266. 0.5268
|
|
15.01 0.1651 0.3024 0.1205 0.0658 0.674 5.312 5.096 502.818 0.600 22.668 4.597 0.38 140500. 0.5074
|
|
18.76 0.2063 0.3643 0.1199 0.0679 0.696 5.485 5.070 519.146 0.620 22.551 4.429 0.38 140765. 0.4877
|
|
22.51 0.2476 0.4206 0.1191 0.0701 0.719 5.662 5.036 535.935 0.640 22.402 4.262 0.38 141063. 0.4677
|
|
26.26 0.2889 0.4718 0.1181 0.0723 0.741 5.840 4.994 552.752 0.660 22.212 4.098 0.38 141394. 0.4478
|
|
30.01 0.3302 0.5180 0.1168 0.0744 0.763 6.013 4.940 569.083 0.679 21.971 3.937 0.38 141760. 0.4278
|
|
33.77 0.3714 0.5598 0.1152 0.0764 0.784 6.174 4.872 584.339 0.698 21.669 3.781 0.38 142162. 0.4081
|
|
37.52 0.4127 0.5974 0.1132 0.0782 0.802 6.317 4.787 597.883 0.714 21.294 3.632 0.38 142600. 0.3886
|
|
41.27 0.4540 0.6312 0.1108 0.0797 0.817 6.435 4.685 609.041 0.727 20.838 3.489 0.38 143076. 0.3692
|
|
45.02 0.4952 0.6617 0.1079 0.0807 0.828 6.520 4.561 617.115 0.737 20.289 3.353 0.39 143588. 0.3501
|
|
48.77 0.5365 0.6891 0.1044 0.0813 0.833 6.565 4.415 621.384 0.742 19.639 3.223 0.39 144138. 0.3311
|
|
52.53 0.5778 0.7137 0.1004 0.0812 0.833 6.562 4.244 621.101 0.741 18.879 3.099 0.39 144724. 0.3122
|
|
56.28 0.6190 0.7358 0.0957 0.0805 0.825 6.504 4.047 615.573 0.735 18.003 2.982 0.39 145346. 0.2934
|
|
60.03 0.6603 0.7554 0.0904 0.0791 0.810 6.385 3.825 604.367 0.721 17.014 2.871 0.39 146003. 0.2745
|
|
63.78 0.7016 0.7729 0.0847 0.0768 0.788 6.207 3.580 587.473 0.701 15.925 2.764 0.39 146696. 0.2557
|
|
67.53 0.7429 0.7881 0.0784 0.0739 0.758 5.971 3.317 565.189 0.675 14.753 2.662 0.39 147422. 0.2370
|
|
71.28 0.7841 0.8008 0.0719 0.0704 0.721 5.683 3.039 537.906 0.642 13.518 2.563 0.39 148181. 0.2184
|
|
75.04 0.8254 0.8109 0.0650 0.0662 0.679 5.346 2.750 505.980 0.604 12.231 2.465 0.39 148974. 0.1999
|
|
78.79 0.8667 0.8178 0.0580 0.0614 0.630 4.963 2.452 469.698 0.561 10.906 2.368 0.40 149798. 0.1813
|
|
82.54 0.9079 0.8208 0.0508 0.0562 0.576 4.536 2.147 429.287 0.512 9.549 2.268 0.40 150654. 0.1625
|
|
86.29 0.9492 0.8186 0.0434 0.0503 0.516 4.067 1.836 384.929 0.459 8.168 2.164 0.40 151541. 0.1434
|
|
90.04 0.9905 0.8091 0.0360 0.0441 0.452 3.558 1.522 336.797 0.402 6.770 2.050 0.40 152458. 0.1236
|
|
93.79 1.0317 0.7882 0.0285 0.0373 0.382 3.012 1.205 285.069 0.340 5.359 1.917 0.40 153406. 0.1029
|
|
97.55 1.0730 0.7473 0.0209 0.0301 0.308 2.430 0.886 229.953 0.274 3.941 1.748 0.40 154383. 0.0804
|
|
101.30 1.1143 0.6655 0.0134 0.0225 0.230 1.814 0.567 171.719 0.205 2.524 1.499 0.40 155389. 0.0552
|
|
105.05 1.1556 0.4726 0.0059 0.0145 0.148 1.170 0.250 110.705 0.132 1.114 1.026 0.41 156423. 0.0251
|
|
108.80 1.1968
|
|
|
|
|
|
|
|
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 0.1222 0.0583 0.852 5.964 6.542 635.047 0.674 29.099 4.672 0.43 157191. 0.5844
|
|
4.19 0.0410 0.0835 0.1219 0.0599 0.874 6.124 6.527 652.050 0.692 29.031 4.540 0.43 157363. 0.5671
|
|
8.39 0.0820 0.1618 0.1216 0.0616 0.900 6.301 6.510 670.891 0.712 28.955 4.401 0.43 157562. 0.5490
|
|
12.58 0.1230 0.2348 0.1212 0.0635 0.927 6.494 6.490 691.461 0.734 28.866 4.257 0.43 157791. 0.5303
|
|
16.77 0.1640 0.3022 0.1208 0.0656 0.957 6.701 6.465 713.556 0.757 28.757 4.110 0.43 158052. 0.5109
|
|
20.97 0.2050 0.3641 0.1202 0.0677 0.988 6.920 6.435 736.849 0.782 28.621 3.961 0.43 158347. 0.4913
|
|
25.16 0.2460 0.4205 0.1195 0.0699 1.020 7.146 6.395 760.879 0.807 28.446 3.812 0.43 158678. 0.4714
|
|
29.35 0.2870 0.4717 0.1185 0.0721 1.053 7.373 6.345 785.049 0.833 28.221 3.666 0.43 159046. 0.4515
|
|
33.55 0.3280 0.5180 0.1173 0.0743 1.084 7.594 6.280 808.633 0.858 27.934 3.523 0.43 159453. 0.4316
|
|
37.74 0.3690 0.5599 0.1158 0.0763 1.114 7.802 6.198 830.799 0.882 27.570 3.384 0.43 159900. 0.4119
|
|
41.93 0.4100 0.5976 0.1139 0.0781 1.141 7.989 6.096 850.636 0.903 27.116 3.251 0.43 160387. 0.3924
|
|
46.13 0.4510 0.6315 0.1116 0.0797 1.163 8.144 5.971 867.185 0.920 26.560 3.123 0.43 160916. 0.3732
|
|
50.32 0.4920 0.6622 0.1087 0.0808 1.179 8.259 5.820 879.450 0.933 25.888 3.002 0.43 161486. 0.3541
|
|
54.51 0.5330 0.6897 0.1054 0.0814 1.189 8.325 5.641 886.404 0.941 25.089 2.886 0.43 162097. 0.3352
|
|
58.70 0.5740 0.7146 0.1014 0.0815 1.189 8.330 5.430 886.990 0.941 24.151 2.776 0.44 162748. 0.3163
|
|
62.90 0.6150 0.7369 0.0969 0.0809 1.180 8.266 5.186 880.202 0.934 23.066 2.672 0.44 163440. 0.2976
|
|
67.09 0.6560 0.7568 0.0917 0.0795 1.160 8.127 4.909 865.363 0.918 21.837 2.573 0.44 164171. 0.2788
|
|
71.28 0.6970 0.7746 0.0860 0.0774 1.130 7.911 4.604 842.380 0.894 20.477 2.479 0.44 164941. 0.2601
|
|
75.48 0.7380 0.7903 0.0798 0.0746 1.088 7.622 4.274 811.636 0.861 19.010 2.388 0.44 165749. 0.2414
|
|
79.67 0.7790 0.8037 0.0733 0.0711 1.038 7.266 3.925 773.682 0.821 17.458 2.301 0.44 166594. 0.2229
|
|
83.86 0.8200 0.8145 0.0665 0.0670 0.978 6.847 3.561 729.035 0.774 15.839 2.215 0.44 167475. 0.2044
|
|
88.06 0.8610 0.8225 0.0595 0.0623 0.909 6.368 3.185 678.118 0.720 14.168 2.131 0.44 168392. 0.1859
|
|
92.25 0.9020 0.8269 0.0523 0.0571 0.833 5.834 2.800 621.261 0.659 12.456 2.045 0.45 169344. 0.1673
|
|
96.44 0.9430 0.8266 0.0450 0.0513 0.749 5.247 2.408 558.735 0.593 10.712 1.955 0.45 170330. 0.1484
|
|
100.64 0.9840 0.8199 0.0376 0.0451 0.658 4.609 2.011 490.781 0.521 8.944 1.858 0.45 171351. 0.1289
|
|
104.83 1.0250 0.8032 0.0301 0.0384 0.560 3.922 1.609 417.647 0.443 7.158 1.748 0.45 172405. 0.1084
|
|
109.02 1.0660 0.7696 0.0225 0.0312 0.455 3.189 1.206 339.619 0.360 5.363 1.610 0.45 173491. 0.0864
|
|
113.22 1.1070 0.7019 0.0150 0.0236 0.345 2.414 0.801 257.060 0.273 3.565 1.414 0.45 174610. 0.0619
|
|
117.41 1.1480 0.5467 0.0075 0.0157 0.229 1.601 0.399 170.433 0.181 1.775 1.062 0.46 175761. 0.0328
|
|
121.60 1.1890 0.0019 0.0000 0.0074 0.108 0.754 0.001 80.236 0.085 0.003 0.004 0.46 176929. 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 0.1224 0.0583 1.167 7.353 8.088 869.997 0.831 35.976 4.217 0.48 174654. 0.5864
|
|
4.66 0.0410 0.0837 0.1221 0.0598 1.198 7.551 8.071 893.316 0.853 35.898 4.098 0.48 174845. 0.5692
|
|
9.32 0.0820 0.1624 0.1218 0.0616 1.233 7.769 8.051 919.217 0.878 35.812 3.973 0.48 175066. 0.5512
|
|
13.99 0.1231 0.2356 0.1215 0.0635 1.271 8.009 8.029 947.567 0.905 35.711 3.843 0.48 175320. 0.5324
|
|
18.65 0.1641 0.3033 0.1211 0.0655 1.312 8.267 8.001 978.105 0.934 35.588 3.710 0.48 175610. 0.5132
|
|
23.31 0.2051 0.3654 0.1205 0.0677 1.355 8.540 7.966 1010.398 0.965 35.432 3.576 0.48 175938. 0.4935
|
|
27.97 0.2461 0.4220 0.1199 0.0699 1.400 8.823 7.921 1043.821 0.997 35.231 3.442 0.48 176305. 0.4736
|
|
32.63 0.2872 0.4734 0.1190 0.0722 1.445 9.108 7.862 1077.547 1.029 34.969 3.309 0.48 176714. 0.4537
|
|
37.29 0.3282 0.5199 0.1178 0.0744 1.489 9.387 7.786 1110.567 1.061 34.630 3.180 0.48 177167. 0.4338
|
|
41.96 0.3692 0.5618 0.1163 0.0765 1.531 9.650 7.688 1141.713 1.090 34.197 3.054 0.48 177663. 0.4141
|
|
46.62 0.4102 0.5996 0.1145 0.0783 1.569 9.887 7.566 1169.697 1.117 33.653 2.934 0.48 178205. 0.3946
|
|
51.28 0.4513 0.6336 0.1122 0.0799 1.600 10.085 7.415 1193.159 1.139 32.980 2.819 0.48 178793. 0.3753
|
|
55.94 0.4923 0.6643 0.1094 0.0811 1.624 10.233 7.231 1210.692 1.156 32.162 2.709 0.48 179427. 0.3562
|
|
60.60 0.5333 0.6920 0.1061 0.0818 1.637 10.319 7.011 1220.852 1.166 31.185 2.605 0.48 180107. 0.3372
|
|
65.26 0.5743 0.7169 0.1022 0.0818 1.639 10.330 6.752 1222.155 1.167 30.033 2.506 0.48 180832. 0.3184
|
|
69.93 0.6153 0.7394 0.0976 0.0812 1.627 10.254 6.451 1213.191 1.159 28.696 2.412 0.49 181602. 0.2996
|
|
74.59 0.6564 0.7595 0.0925 0.0799 1.600 10.083 6.110 1192.997 1.139 27.176 2.323 0.49 182415. 0.2807
|
|
79.25 0.6974 0.7776 0.0867 0.0778 1.557 9.817 5.731 1161.423 1.109 25.492 2.238 0.49 183272. 0.2620
|
|
83.91 0.7384 0.7935 0.0805 0.0749 1.501 9.458 5.322 1118.998 1.069 23.671 2.157 0.49 184171. 0.2433
|
|
88.57 0.7794 0.8072 0.0740 0.0714 1.430 9.014 4.888 1066.491 1.018 21.743 2.079 0.49 185112. 0.2248
|
|
93.23 0.8205 0.8186 0.0671 0.0673 1.347 8.491 4.436 1004.630 0.959 19.730 2.003 0.49 186092. 0.2062
|
|
97.90 0.8615 0.8270 0.0601 0.0626 1.253 7.894 3.968 934.008 0.892 17.651 1.927 0.49 187112. 0.1877
|
|
102.56 0.9025 0.8321 0.0528 0.0573 1.147 7.227 3.489 855.091 0.817 15.520 1.851 0.50 188172. 0.1690
|
|
107.22 0.9435 0.8328 0.0454 0.0515 1.030 6.494 3.001 768.259 0.734 13.348 1.772 0.50 189269. 0.1501
|
|
111.88 0.9846 0.8272 0.0379 0.0451 0.904 5.696 2.505 673.846 0.643 11.144 1.686 0.50 190404. 0.1305
|
|
116.54 1.0256 0.8120 0.0303 0.0383 0.767 4.836 2.005 572.200 0.546 8.918 1.589 0.50 191577. 0.1100
|
|
121.20 1.0666 0.7805 0.0227 0.0311 0.622 3.919 1.502 463.717 0.443 6.679 1.469 0.50 192786. 0.0880
|
|
125.87 1.1076 0.7157 0.0151 0.0234 0.468 2.949 0.998 348.904 0.333 4.438 1.297 0.50 194030. 0.0633
|
|
130.53 1.1486 0.5633 0.0075 0.0153 0.306 1.931 0.496 228.410 0.218 2.205 0.984 0.51 195310. 0.0339
|
|
135.19 1.1897 -0.0040 0.0000 0.0069 0.138 0.870 -0.002 102.918 0.098 -0.007 -0.007 0.51 196607. 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 0.1226 0.0583 1.553 8.901 9.801 1158.439 1.006 43.595 3.837 0.52 192116. 0.5874
|
|
5.13 0.0410 0.0839 0.1223 0.0598 1.595 9.139 9.782 1189.430 1.033 43.509 3.730 0.52 192326. 0.5704
|
|
10.26 0.0821 0.1627 0.1221 0.0616 1.641 9.405 9.760 1223.941 1.063 43.414 3.617 0.52 192569. 0.5525
|
|
15.39 0.1231 0.2361 0.1218 0.0635 1.692 9.696 9.736 1261.824 1.095 43.304 3.500 0.52 192848. 0.5339
|
|
20.52 0.1642 0.3040 0.1214 0.0656 1.747 10.010 9.705 1302.762 1.131 43.170 3.379 0.52 193167. 0.5147
|
|
25.65 0.2052 0.3662 0.1209 0.0677 1.805 10.344 9.667 1346.205 1.169 42.998 3.257 0.52 193527. 0.4952
|
|
30.78 0.2462 0.4230 0.1203 0.0700 1.866 10.691 9.617 1391.335 1.208 42.774 3.135 0.53 193931. 0.4754
|
|
35.91 0.2873 0.4745 0.1194 0.0723 1.927 11.042 9.550 1437.053 1.248 42.479 3.014 0.53 194380. 0.4555
|
|
41.04 0.3283 0.5211 0.1184 0.0746 1.987 11.387 9.463 1481.995 1.287 42.093 2.896 0.53 194878. 0.4357
|
|
46.17 0.3693 0.5631 0.1169 0.0767 2.044 11.715 9.351 1524.562 1.323 41.592 2.782 0.53 195424. 0.4160
|
|
51.30 0.4104 0.6009 0.1152 0.0786 2.096 12.010 9.208 1562.984 1.357 40.956 2.672 0.53 196021. 0.3965
|
|
56.43 0.4514 0.6350 0.1129 0.0803 2.139 12.259 9.029 1595.385 1.385 40.163 2.567 0.53 196668. 0.3772
|
|
61.56 0.4925 0.6658 0.1102 0.0815 2.172 12.447 8.811 1619.827 1.406 39.192 2.467 0.53 197365. 0.3581
|
|
66.69 0.5335 0.6936 0.1069 0.0822 2.192 12.558 8.548 1634.327 1.419 38.023 2.372 0.53 198114. 0.3392
|
|
71.82 0.5745 0.7186 0.1030 0.0824 2.195 12.577 8.237 1636.863 1.421 36.638 2.282 0.53 198912. 0.3203
|
|
76.95 0.6156 0.7412 0.0985 0.0818 2.180 12.490 7.874 1625.509 1.411 35.026 2.197 0.53 199760. 0.3015
|
|
82.08 0.6566 0.7615 0.0933 0.0805 2.144 12.286 7.461 1598.931 1.388 33.186 2.116 0.53 200656. 0.2827
|
|
87.20 0.6976 0.7798 0.0876 0.0783 2.088 11.963 7.001 1556.897 1.352 31.142 2.040 0.54 201600. 0.2639
|
|
92.33 0.7387 0.7960 0.0813 0.0755 2.012 11.527 6.504 1500.105 1.302 28.928 1.966 0.54 202590. 0.2452
|
|
97.46 0.7797 0.8101 0.0747 0.0719 1.917 10.985 5.976 1429.607 1.241 26.580 1.896 0.54 203626. 0.2266
|
|
102.59 0.8208 0.8218 0.0678 0.0677 1.806 10.346 5.424 1346.400 1.169 24.125 1.827 0.54 204706. 0.2081
|
|
107.72 0.8618 0.8308 0.0607 0.0630 1.678 9.615 4.853 1251.300 1.086 21.588 1.759 0.54 205830. 0.1895
|
|
112.85 0.9028 0.8366 0.0534 0.0576 1.535 8.798 4.268 1144.943 0.994 18.986 1.691 0.54 206996. 0.1708
|
|
117.98 0.9439 0.8380 0.0459 0.0517 1.378 7.898 3.672 1027.847 0.892 16.332 1.620 0.55 208205. 0.1518
|
|
123.11 0.9849 0.8335 0.0383 0.0453 1.208 6.919 3.066 900.469 0.782 13.638 1.544 0.55 209455. 0.1322
|
|
128.24 1.0259 0.8199 0.0307 0.0384 1.024 5.865 2.454 763.273 0.663 10.916 1.458 0.55 210745. 0.1117
|
|
133.37 1.0670 0.7904 0.0230 0.0310 0.827 4.739 1.838 616.799 0.535 8.176 1.352 0.55 212076. 0.0896
|
|
138.50 1.1080 0.7284 0.0153 0.0232 0.619 3.548 1.221 461.727 0.401 5.432 1.200 0.56 213447. 0.0648
|
|
143.63 1.1491 0.5795 0.0076 0.0150 0.401 2.297 0.607 298.945 0.260 2.698 0.920 0.56 214855. 0.0351
|
|
148.76 1.1901 -0.0057 0.0000 0.0065 0.173 0.994 -0.003 129.360 0.112 -0.011 -0.009 0.56 216281. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 12000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1228 0.0584 2.021 10.614 11.682 1506.932 1.199 51.962 3.516 0.57 209577. 0.5877
|
|
5.60 0.0410 0.0839 0.1225 0.0600 2.075 10.897 11.661 1547.042 1.231 51.868 3.419 0.57 209806. 0.5709
|
|
11.20 0.0821 0.1628 0.1223 0.0617 2.135 11.212 11.638 1591.837 1.267 51.767 3.316 0.57 210071. 0.5532
|
|
16.79 0.1231 0.2363 0.1220 0.0636 2.201 11.560 11.612 1641.168 1.306 51.651 3.209 0.57 210375. 0.5347
|
|
22.39 0.1642 0.3042 0.1217 0.0657 2.273 11.936 11.580 1694.671 1.349 51.510 3.099 0.57 210722. 0.5157
|
|
27.99 0.2052 0.3666 0.1213 0.0679 2.349 12.338 11.540 1751.678 1.394 51.328 2.988 0.57 211114. 0.4963
|
|
33.59 0.2463 0.4235 0.1207 0.0702 2.429 12.757 11.486 1811.155 1.441 51.088 2.876 0.57 211554. 0.4767
|
|
39.18 0.2873 0.4751 0.1199 0.0725 2.510 13.183 11.413 1871.687 1.489 50.766 2.766 0.57 212045. 0.4569
|
|
44.78 0.3284 0.5217 0.1189 0.0749 2.590 13.604 11.317 1931.471 1.537 50.338 2.658 0.57 212587. 0.4372
|
|
50.38 0.3694 0.5638 0.1176 0.0771 2.666 14.005 11.191 1988.375 1.582 49.776 2.553 0.58 213183. 0.4176
|
|
55.98 0.4105 0.6017 0.1159 0.0791 2.736 14.369 11.028 2040.018 1.623 49.051 2.452 0.58 213833. 0.3981
|
|
61.57 0.4515 0.6358 0.1137 0.0808 2.794 14.678 10.822 2083.855 1.658 48.137 2.356 0.58 214539. 0.3789
|
|
67.17 0.4926 0.6667 0.1111 0.0821 2.839 14.913 10.568 2117.270 1.685 47.007 2.264 0.58 215301. 0.3599
|
|
72.77 0.5336 0.6945 0.1078 0.0828 2.867 15.056 10.260 2137.595 1.701 45.637 2.177 0.58 216118. 0.3410
|
|
78.37 0.5747 0.7197 0.1040 0.0830 2.873 15.088 9.893 2142.123 1.705 44.005 2.095 0.58 216990. 0.3222
|
|
83.96 0.6157 0.7424 0.0995 0.0825 2.854 14.991 9.464 2128.288 1.694 42.094 2.017 0.58 217916. 0.3034
|
|
89.56 0.6568 0.7629 0.0943 0.0812 2.808 14.751 8.972 2094.276 1.667 39.905 1.943 0.58 218895. 0.2846
|
|
95.16 0.6978 0.7814 0.0885 0.0791 2.735 14.367 8.423 2039.731 1.623 37.466 1.873 0.59 219926. 0.2658
|
|
100.76 0.7389 0.7979 0.0823 0.0762 2.636 13.844 7.828 1965.561 1.564 34.817 1.806 0.59 221008. 0.2471
|
|
106.35 0.7799 0.8123 0.0756 0.0726 2.512 13.194 7.195 1873.166 1.491 32.002 1.742 0.59 222139. 0.2285
|
|
111.95 0.8210 0.8244 0.0686 0.0684 2.365 12.424 6.533 1763.893 1.404 29.057 1.680 0.59 223318. 0.2099
|
|
117.55 0.8620 0.8340 0.0614 0.0635 2.198 11.543 5.847 1638.836 1.304 26.008 1.618 0.59 224546. 0.1913
|
|
123.15 0.9031 0.8403 0.0541 0.0581 2.010 10.557 5.144 1498.852 1.193 22.879 1.557 0.59 225819. 0.1726
|
|
128.74 0.9441 0.8426 0.0465 0.0521 1.803 9.471 4.426 1344.631 1.070 19.686 1.493 0.60 227139. 0.1536
|
|
134.34 0.9852 0.8392 0.0388 0.0456 1.578 8.289 3.697 1176.779 0.936 16.443 1.425 0.60 228504. 0.1340
|
|
139.94 1.0262 0.8269 0.0311 0.0386 1.336 7.015 2.960 995.909 0.793 13.164 1.348 0.60 229913. 0.1134
|
|
145.54 1.0673 0.7993 0.0233 0.0311 1.076 5.654 2.217 802.731 0.639 9.862 1.253 0.60 231366. 0.0912
|
|
151.13 1.1083 0.7402 0.0155 0.0232 0.802 4.213 1.473 598.141 0.476 6.553 1.117 0.61 232862. 0.0663
|
|
156.73 1.1494 0.5949 0.0077 0.0149 0.514 2.700 0.732 383.317 0.305 3.255 0.866 0.61 234399. 0.0362
|
|
162.33 1.1904 -0.0071 0.0000 0.0062 0.214 1.123 -0.003 159.444 0.127 -0.016 -0.010 0.61 235954. 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 0.1230 0.0586 2.580 12.509 13.732 1923.963 1.413 61.081 3.237 0.62 227038. 0.5866
|
|
6.07 0.0411 0.0837 0.1228 0.0602 2.648 12.838 13.710 1974.618 1.450 60.981 3.149 0.62 227285. 0.5701
|
|
12.13 0.0821 0.1625 0.1225 0.0619 2.724 13.207 13.686 2031.360 1.492 60.876 3.056 0.62 227571. 0.5528
|
|
18.20 0.1232 0.2360 0.1223 0.0638 2.808 13.615 13.660 2094.059 1.538 60.758 2.959 0.62 227900. 0.5347
|
|
24.26 0.1642 0.3040 0.1220 0.0659 2.900 14.059 13.628 2162.327 1.588 60.615 2.859 0.62 228276. 0.5160
|
|
30.33 0.2053 0.3665 0.1217 0.0681 2.998 14.534 13.586 2235.396 1.642 60.431 2.757 0.62 228700. 0.4968
|
|
36.39 0.2463 0.4235 0.1212 0.0705 3.100 15.032 13.530 2312.012 1.698 60.183 2.654 0.62 229176. 0.4774
|
|
42.46 0.2874 0.4752 0.1205 0.0729 3.206 15.542 13.454 2390.417 1.756 59.845 2.553 0.62 229707. 0.4579
|
|
48.52 0.3285 0.5219 0.1195 0.0752 3.310 16.048 13.351 2468.316 1.813 59.385 2.453 0.62 230294. 0.4383
|
|
54.59 0.3695 0.5640 0.1183 0.0775 3.410 16.533 13.213 2542.931 1.868 58.771 2.357 0.62 230939. 0.4189
|
|
60.65 0.4106 0.6019 0.1167 0.0796 3.502 16.977 13.032 2611.113 1.918 57.965 2.264 0.62 231643. 0.3996
|
|
66.72 0.4516 0.6361 0.1146 0.0814 3.580 17.356 12.800 2669.470 1.961 56.935 2.175 0.63 232408. 0.3805
|
|
72.78 0.4927 0.6670 0.1120 0.0827 3.640 17.649 12.510 2714.484 1.994 55.646 2.090 0.63 233233. 0.3615
|
|
78.85 0.5337 0.6949 0.1088 0.0836 3.678 17.832 12.156 2742.597 2.015 54.069 2.010 0.63 234119. 0.3427
|
|
84.91 0.5748 0.7202 0.1050 0.0838 3.688 17.881 11.730 2750.244 2.020 52.176 1.935 0.63 235065. 0.3240
|
|
90.98 0.6159 0.7430 0.1005 0.0833 3.666 17.776 11.229 2734.053 2.008 49.947 1.863 0.63 236069. 0.3052
|
|
97.05 0.6569 0.7637 0.0954 0.0820 3.610 17.500 10.653 2691.607 1.977 47.383 1.795 0.63 237131. 0.2865
|
|
103.11 0.6980 0.7824 0.0896 0.0799 3.517 17.050 10.007 2622.370 1.926 44.512 1.731 0.63 238249. 0.2677
|
|
109.18 0.7390 0.7992 0.0833 0.0770 3.389 16.433 9.304 2527.491 1.857 41.386 1.670 0.64 239422. 0.2490
|
|
115.24 0.7801 0.8139 0.0766 0.0734 3.230 15.661 8.556 2408.812 1.769 38.057 1.611 0.64 240649. 0.2304
|
|
121.31 0.8212 0.8265 0.0696 0.0691 3.042 14.747 7.772 2268.117 1.666 34.568 1.554 0.64 241929. 0.2118
|
|
127.37 0.8622 0.8365 0.0623 0.0642 2.825 13.698 6.959 2106.858 1.548 30.953 1.498 0.64 243260. 0.1932
|
|
133.44 0.9033 0.8435 0.0548 0.0587 2.583 12.523 6.124 1926.170 1.415 27.238 1.442 0.64 244641. 0.1745
|
|
139.50 0.9443 0.8466 0.0472 0.0526 2.316 11.228 5.271 1726.954 1.269 23.444 1.384 0.65 246072. 0.1554
|
|
145.57 0.9854 0.8442 0.0394 0.0460 2.025 9.818 4.404 1510.006 1.109 19.588 1.323 0.65 247552. 0.1357
|
|
151.63 1.0264 0.8333 0.0316 0.0389 1.711 8.297 3.527 1276.113 0.937 15.687 1.253 0.65 249080. 0.1151
|
|
157.70 1.0675 0.8076 0.0237 0.0313 1.376 6.672 2.643 1026.192 0.754 11.755 1.168 0.65 250655. 0.0929
|
|
163.76 1.1086 0.7512 0.0157 0.0232 1.021 4.950 1.756 761.404 0.559 7.813 1.046 0.66 252276. 0.0678
|
|
169.83 1.1496 0.6097 0.0078 0.0147 0.648 3.142 0.873 483.308 0.355 3.881 0.819 0.66 253942. 0.0374
|
|
175.89 1.1907 -0.0083 0.0000 0.0059 0.260 1.258 -0.005 193.533 0.142 -0.020 -0.011 0.66 255624. 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 0.1232 0.0592 3.254 14.649 15.951 2426.447 1.655 70.951 2.982 0.67 244497. 0.5823
|
|
6.53 0.0411 0.0831 0.1230 0.0607 3.338 15.027 15.928 2488.990 1.698 70.846 2.903 0.67 244763. 0.5664
|
|
13.07 0.0821 0.1614 0.1228 0.0625 3.432 15.451 15.904 2559.246 1.746 70.740 2.819 0.67 245071. 0.5496
|
|
19.60 0.1232 0.2346 0.1226 0.0644 3.536 15.921 15.878 2637.127 1.799 70.624 2.731 0.67 245425. 0.5321
|
|
26.13 0.1643 0.3025 0.1223 0.0664 3.651 16.435 15.847 2722.232 1.857 70.486 2.640 0.67 245828. 0.5139
|
|
32.66 0.2053 0.3649 0.1220 0.0687 3.773 16.987 15.806 2813.681 1.919 70.307 2.548 0.67 246284. 0.4953
|
|
39.20 0.2464 0.4219 0.1216 0.0710 3.902 17.569 15.751 2910.001 1.985 70.062 2.455 0.67 246796. 0.4764
|
|
45.73 0.2874 0.4737 0.1210 0.0734 4.035 18.167 15.675 3009.037 2.052 69.722 2.363 0.67 247366. 0.4574
|
|
52.26 0.3285 0.5205 0.1202 0.0759 4.168 18.764 15.568 3107.929 2.120 69.247 2.272 0.67 247997. 0.4383
|
|
58.79 0.3696 0.5629 0.1191 0.0782 4.296 19.339 15.422 3203.172 2.185 68.597 2.184 0.67 248691. 0.4193
|
|
65.33 0.4106 0.6010 0.1176 0.0803 4.413 19.867 15.226 3290.748 2.245 67.726 2.099 0.67 249449. 0.4004
|
|
71.86 0.4517 0.6355 0.1156 0.0822 4.514 20.324 14.971 3366.319 2.296 66.592 2.017 0.67 250273. 0.3816
|
|
78.39 0.4928 0.6666 0.1131 0.0836 4.593 20.680 14.648 3425.361 2.336 65.152 1.940 0.67 251162. 0.3630
|
|
84.92 0.5338 0.6947 0.1100 0.0845 4.644 20.909 14.247 3463.260 2.362 63.369 1.866 0.68 252116. 0.3444
|
|
91.46 0.5749 0.7201 0.1062 0.0848 4.661 20.982 13.761 3475.360 2.371 61.209 1.796 0.68 253135. 0.3258
|
|
97.99 0.6159 0.7431 0.1018 0.0844 4.636 20.872 13.185 3457.187 2.358 58.646 1.730 0.68 254217. 0.3071
|
|
104.52 0.6570 0.7640 0.0966 0.0831 4.567 20.560 12.518 3405.451 2.323 55.679 1.667 0.68 255362. 0.2884
|
|
111.06 0.6981 0.7829 0.0909 0.0810 4.451 20.039 11.768 3319.269 2.264 52.343 1.608 0.68 256568. 0.2697
|
|
117.59 0.7391 0.7999 0.0845 0.0781 4.291 19.320 10.948 3200.059 2.183 48.697 1.552 0.68 257833. 0.2511
|
|
124.12 0.7802 0.8150 0.0778 0.0744 4.090 18.415 10.073 3050.202 2.081 44.804 1.498 0.69 259156. 0.2324
|
|
130.65 0.8213 0.8280 0.0707 0.0701 3.851 17.339 9.154 2872.046 1.959 40.716 1.446 0.69 260536. 0.2139
|
|
137.19 0.8623 0.8386 0.0633 0.0651 3.577 16.105 8.200 2667.497 1.819 36.475 1.394 0.69 261970. 0.1952
|
|
143.72 0.9034 0.8462 0.0557 0.0595 3.269 14.719 7.219 2438.024 1.663 32.111 1.343 0.69 263459. 0.1765
|
|
150.25 0.9444 0.8501 0.0480 0.0533 2.930 13.190 6.216 2184.807 1.490 27.650 1.291 0.70 265002. 0.1573
|
|
156.78 0.9855 0.8486 0.0401 0.0466 2.560 11.524 5.196 1908.865 1.302 23.113 1.235 0.70 266597. 0.1376
|
|
163.32 1.0266 0.8391 0.0321 0.0393 2.161 9.727 4.163 1611.210 1.099 18.517 1.172 0.70 268243. 0.1169
|
|
169.85 1.0676 0.8152 0.0241 0.0316 1.734 7.807 3.121 1293.086 0.882 13.882 1.095 0.70 269940. 0.0946
|
|
176.38 1.1087 0.7612 0.0160 0.0233 1.282 5.773 2.075 956.171 0.652 9.231 0.984 0.71 271687. 0.0693
|
|
182.92 1.1498 0.6222 0.0080 0.0147 0.808 3.639 1.031 602.812 0.411 4.587 0.776 0.71 273482. 0.0385
|
|
189.45 1.1908 -0.0096 0.0000 0.0057 0.316 1.422 -0.006 235.560 0.161 -0.027 -0.012 0.71 275292. 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 0.1233 0.0605 4.087 17.172 18.338 3047.400 1.940 81.566 2.729 0.71 261955. 0.5715
|
|
7.00 0.0411 0.0816 0.1232 0.0620 4.188 17.598 18.313 3123.135 1.988 81.456 2.660 0.71 262239. 0.5565
|
|
14.00 0.0821 0.1587 0.1230 0.0637 4.303 18.079 18.289 3208.471 2.043 81.350 2.585 0.71 262569. 0.5407
|
|
21.00 0.1232 0.2308 0.1228 0.0655 4.430 18.614 18.264 3303.368 2.103 81.239 2.508 0.71 262948. 0.5240
|
|
28.00 0.1642 0.2979 0.1226 0.0676 4.569 19.200 18.235 3407.416 2.169 81.110 2.427 0.71 263379. 0.5068
|
|
35.00 0.2053 0.3598 0.1224 0.0698 4.720 19.832 18.198 3519.619 2.241 80.945 2.345 0.72 263867. 0.4892
|
|
41.99 0.2464 0.4165 0.1220 0.0722 4.879 20.501 18.147 3638.228 2.316 80.717 2.262 0.72 264414. 0.4712
|
|
48.99 0.2874 0.4682 0.1216 0.0746 5.043 21.190 18.073 3760.607 2.394 80.390 2.180 0.72 265023. 0.4531
|
|
55.99 0.3285 0.5152 0.1208 0.0771 5.207 21.881 17.968 3883.156 2.472 79.921 2.099 0.72 265698. 0.4350
|
|
62.99 0.3695 0.5578 0.1198 0.0794 5.366 22.547 17.819 4001.415 2.547 79.259 2.020 0.72 266440. 0.4169
|
|
69.99 0.4106 0.5964 0.1185 0.0816 5.512 23.161 17.614 4110.274 2.617 78.349 1.944 0.72 267251. 0.3989
|
|
76.99 0.4517 0.6314 0.1166 0.0834 5.638 23.690 17.341 4204.243 2.677 77.134 1.871 0.72 268132. 0.3809
|
|
83.99 0.4927 0.6632 0.1143 0.0849 5.736 24.104 16.988 4277.690 2.723 75.564 1.801 0.72 269084. 0.3630
|
|
90.99 0.5338 0.6921 0.1113 0.0858 5.800 24.370 16.544 4324.947 2.753 73.588 1.735 0.72 270106. 0.3451
|
|
97.99 0.5749 0.7182 0.1076 0.0861 5.820 24.457 15.999 4340.318 2.763 71.164 1.672 0.73 271198. 0.3270
|
|
104.99 0.6159 0.7419 0.1032 0.0857 5.791 24.333 15.346 4318.320 2.749 68.260 1.612 0.73 272359. 0.3088
|
|
111.98 0.6570 0.7633 0.0981 0.0844 5.706 23.975 14.585 4254.771 2.709 64.873 1.555 0.73 273587. 0.2903
|
|
118.98 0.6980 0.7827 0.0923 0.0823 5.563 23.375 13.723 4148.336 2.641 61.041 1.500 0.73 274880. 0.2718
|
|
125.98 0.7391 0.8001 0.0859 0.0794 5.365 22.542 12.777 4000.475 2.547 56.833 1.449 0.73 276237. 0.2532
|
|
132.98 0.7802 0.8156 0.0791 0.0757 5.115 21.491 11.764 3813.950 2.428 52.325 1.399 0.74 277656. 0.2346
|
|
139.98 0.8212 0.8290 0.0719 0.0713 4.816 20.238 10.697 3591.556 2.286 47.581 1.351 0.74 279136. 0.2160
|
|
146.98 0.8623 0.8401 0.0645 0.0662 4.473 18.796 9.589 3335.698 2.124 42.650 1.304 0.74 280675. 0.1974
|
|
153.98 0.9033 0.8484 0.0568 0.0605 4.088 17.176 8.446 3048.267 1.941 37.570 1.257 0.74 282271. 0.1786
|
|
160.98 0.9444 0.8530 0.0489 0.0542 3.662 15.388 7.277 2730.791 1.738 32.370 1.209 0.75 283925. 0.1594
|
|
167.98 0.9855 0.8526 0.0409 0.0473 3.198 13.437 6.087 2384.697 1.518 27.075 1.158 0.75 285635. 0.1397
|
|
174.98 1.0265 0.8440 0.0328 0.0399 2.698 11.335 4.880 2011.574 1.281 21.705 1.100 0.75 287400. 0.1188
|
|
181.97 1.0676 0.8210 0.0246 0.0320 2.164 9.092 3.661 1613.466 1.027 16.284 1.029 0.75 289219. 0.0963
|
|
188.97 1.1086 0.7670 0.0164 0.0237 1.600 6.723 2.436 1193.170 0.760 10.833 0.926 0.76 291091. 0.0707
|
|
195.97 1.1497 0.6250 0.0081 0.0150 1.012 4.251 1.210 754.493 0.480 5.383 0.727 0.76 293014. 0.0391
|
|
202.97 1.1908 -0.0132 -0.0001 0.0060 0.405 1.700 -0.010 301.654 0.192 -0.044 -0.015 0.76 294951. 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 0.1235 0.0629 5.155 20.307 20.888 3844.062 2.294 92.911 2.465 0.76 279411. 0.5508
|
|
7.50 0.0413 0.0791 0.1233 0.0643 5.277 20.786 20.862 3934.839 2.348 92.793 2.405 0.76 279716. 0.5371
|
|
15.00 0.0825 0.1540 0.1232 0.0660 5.414 21.329 20.837 4037.550 2.410 92.684 2.341 0.76 280069. 0.5225
|
|
22.51 0.1238 0.2243 0.1230 0.0679 5.568 21.935 20.813 4152.231 2.478 92.576 2.274 0.76 280475. 0.5072
|
|
30.01 0.1651 0.2899 0.1229 0.0700 5.738 22.602 20.787 4278.476 2.554 92.459 2.204 0.76 280938. 0.4913
|
|
37.51 0.2063 0.3506 0.1227 0.0722 5.921 23.324 20.753 4415.150 2.635 92.311 2.132 0.76 281461. 0.4749
|
|
45.01 0.2476 0.4065 0.1224 0.0746 6.115 24.090 20.707 4560.136 2.722 92.106 2.060 0.76 282048. 0.4583
|
|
52.52 0.2888 0.4576 0.1220 0.0770 6.316 24.882 20.640 4710.086 2.811 91.805 1.988 0.76 282701. 0.4415
|
|
60.02 0.3301 0.5043 0.1214 0.0795 6.518 25.675 20.539 4860.303 2.901 91.356 1.917 0.77 283425. 0.4247
|
|
67.52 0.3714 0.5470 0.1205 0.0818 6.712 26.439 20.391 5004.798 2.987 90.698 1.848 0.77 284221. 0.4080
|
|
75.02 0.4126 0.5861 0.1193 0.0840 6.888 27.135 20.181 5136.688 3.066 89.763 1.782 0.77 285092. 0.3914
|
|
82.53 0.4539 0.6219 0.1176 0.0858 7.039 27.727 19.892 5248.705 3.133 88.479 1.719 0.77 286040. 0.3749
|
|
90.03 0.4952 0.6548 0.1153 0.0872 7.153 28.176 19.509 5333.672 3.183 86.777 1.659 0.77 287064. 0.3583
|
|
97.53 0.5364 0.6850 0.1124 0.0880 7.221 28.445 19.018 5384.674 3.214 84.594 1.602 0.77 288164. 0.3416
|
|
105.03 0.5777 0.7126 0.1088 0.0882 7.235 28.500 18.407 5395.003 3.220 81.875 1.548 0.77 289340. 0.3246
|
|
112.54 0.6190 0.7378 0.1044 0.0876 7.186 28.306 17.666 5358.354 3.198 78.580 1.495 0.78 290591. 0.3073
|
|
120.04 0.6602 0.7606 0.0993 0.0862 7.067 27.840 16.795 5270.097 3.145 74.702 1.445 0.78 291914. 0.2896
|
|
127.54 0.7015 0.7814 0.0934 0.0839 6.878 27.095 15.802 5129.091 3.061 70.289 1.397 0.78 293308. 0.2716
|
|
135.04 0.7427 0.7999 0.0869 0.0807 6.621 26.083 14.709 4937.519 2.947 65.424 1.351 0.78 294770. 0.2534
|
|
142.55 0.7840 0.8163 0.0800 0.0768 6.301 24.823 13.533 4698.947 2.804 60.197 1.306 0.78 296300. 0.2350
|
|
150.05 0.8253 0.8305 0.0727 0.0722 5.923 23.332 12.294 4416.768 2.636 54.684 1.263 0.79 297894. 0.2165
|
|
157.55 0.8665 0.8421 0.0650 0.0669 5.490 21.625 11.004 4093.623 2.443 48.946 1.219 0.79 299551. 0.1978
|
|
165.05 0.9078 0.8508 0.0572 0.0610 5.004 19.713 9.673 3731.665 2.227 43.027 1.176 0.79 301271. 0.1788
|
|
172.56 0.9491 0.8555 0.0491 0.0545 4.469 17.605 8.310 3332.693 1.989 36.962 1.131 0.80 303052. 0.1594
|
|
180.06 0.9903 0.8546 0.0409 0.0474 3.888 15.314 6.920 2899.012 1.730 30.778 1.083 0.80 304893. 0.1393
|
|
187.56 1.0316 0.8441 0.0326 0.0398 3.264 12.856 5.508 2433.650 1.452 24.501 1.027 0.80 306793. 0.1178
|
|
195.06 1.0728 0.8158 0.0241 0.0317 2.602 10.251 4.081 1940.471 1.158 18.153 0.954 0.80 308751. 0.0942
|
|
202.57 1.1141 0.7477 0.0156 0.0233 1.910 7.526 2.644 1424.605 0.850 11.762 0.842 0.81 310766. 0.0669
|
|
210.07 1.1554 0.5640 0.0071 0.0146 1.197 4.715 1.205 892.573 0.533 5.361 0.612 0.81 312835. 0.0329
|
|
217.57 1.1966
|
|
|
|
|
|
|
|
PROP RPM = 17000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1236 0.0669 6.581 24.400 23.598 4907.508 2.757 104.962 2.181 0.81 296866. 0.5180
|
|
7.99 0.0414 0.0747 0.1234 0.0684 6.725 24.932 23.568 5014.610 2.817 104.829 2.132 0.81 297190. 0.5060
|
|
15.98 0.0827 0.1456 0.1233 0.0700 6.888 25.538 23.541 5136.391 2.885 104.711 2.079 0.81 297567. 0.4932
|
|
23.97 0.1241 0.2125 0.1231 0.0719 7.071 26.217 23.517 5273.047 2.962 104.602 2.023 0.81 297999. 0.4797
|
|
31.95 0.1654 0.2752 0.1230 0.0739 7.274 26.969 23.492 5424.253 3.047 104.492 1.964 0.81 298491. 0.4656
|
|
39.94 0.2068 0.3334 0.1229 0.0762 7.495 27.787 23.463 5588.819 3.139 104.364 1.904 0.81 299047. 0.4510
|
|
47.93 0.2481 0.3873 0.1227 0.0786 7.730 28.660 23.424 5764.329 3.238 104.189 1.843 0.81 299671. 0.4362
|
|
55.92 0.2895 0.4369 0.1223 0.0811 7.975 29.567 23.365 5946.713 3.340 103.928 1.782 0.81 300366. 0.4212
|
|
63.91 0.3308 0.4825 0.1219 0.0836 8.220 30.477 23.275 6129.919 3.443 103.526 1.722 0.81 301136. 0.4063
|
|
71.90 0.3722 0.5245 0.1211 0.0860 8.456 31.352 23.137 6305.831 3.542 102.912 1.664 0.81 301982. 0.3914
|
|
79.89 0.4135 0.5635 0.1201 0.0881 8.669 32.142 22.932 6464.760 3.631 102.004 1.609 0.82 302909. 0.3767
|
|
87.87 0.4549 0.5997 0.1186 0.0899 8.846 32.797 22.641 6596.431 3.705 100.709 1.557 0.82 303917. 0.3622
|
|
95.86 0.4962 0.6337 0.1165 0.0912 8.973 33.268 22.244 6691.100 3.759 98.939 1.508 0.82 305008. 0.3477
|
|
103.85 0.5376 0.6654 0.1137 0.0919 9.039 33.511 21.720 6740.132 3.786 96.611 1.462 0.82 306181. 0.3331
|
|
111.84 0.5789 0.6951 0.1103 0.0918 9.033 33.491 21.055 6735.955 3.784 93.654 1.418 0.82 307436. 0.3181
|
|
119.83 0.6203 0.7227 0.1060 0.0909 8.947 33.172 20.237 6671.854 3.748 90.012 1.376 0.82 308772. 0.3026
|
|
127.82 0.6616 0.7481 0.1009 0.0892 8.775 32.533 19.262 6543.390 3.676 85.675 1.335 0.83 310185. 0.2865
|
|
135.80 0.7030 0.7714 0.0950 0.0866 8.516 31.573 18.142 6350.327 3.567 80.694 1.296 0.83 311674. 0.2699
|
|
143.79 0.7443 0.7925 0.0885 0.0831 8.176 30.311 16.899 6096.480 3.425 75.165 1.257 0.83 313236. 0.2527
|
|
151.78 0.7857 0.8113 0.0815 0.0789 7.760 28.772 15.556 5787.003 3.251 69.195 1.219 0.83 314870. 0.2351
|
|
159.77 0.8270 0.8276 0.0740 0.0740 7.277 26.980 14.136 5426.526 3.048 62.876 1.182 0.84 316573. 0.2172
|
|
167.76 0.8684 0.8411 0.0663 0.0684 6.730 24.951 12.653 5018.387 2.819 56.282 1.144 0.84 318343. 0.1989
|
|
175.75 0.9097 0.8511 0.0582 0.0622 6.123 22.703 11.121 4566.285 2.565 49.465 1.105 0.84 320180. 0.1801
|
|
183.74 0.9511 0.8558 0.0500 0.0556 5.465 20.262 9.546 4075.219 2.289 42.463 1.063 0.85 322082. 0.1605
|
|
191.72 0.9925 0.8530 0.0416 0.0484 4.757 17.639 7.938 3547.635 1.993 35.307 1.015 0.85 324047. 0.1398
|
|
199.71 1.0338 0.8379 0.0330 0.0407 4.005 14.850 6.302 2986.758 1.678 28.031 0.957 0.85 326075. 0.1175
|
|
207.70 1.0752 0.7996 0.0243 0.0327 3.218 11.930 4.645 2399.505 1.348 20.663 0.878 0.86 328165. 0.0925
|
|
215.69 1.1165 0.7111 0.0156 0.0245 2.406 8.922 2.975 1794.458 1.008 13.235 0.752 0.86 330314. 0.0634
|
|
223.68 1.1579 0.4902 0.0068 0.0161 1.585 5.877 1.303 1181.947 0.664 5.794 0.500 0.86 332522. 0.0279
|
|
231.67 1.1992
|
|
|
|
|
|
|