575 lines
102 KiB
Plaintext
575 lines
102 KiB
Plaintext
16x4E (16x4E.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 0.0495 0.0183 0.002 0.097 0.103 1.153 0.011 0.460 40.653 0.06 23948. 0.4793
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0.20 0.0132 0.0348 0.0483 0.0183 0.002 0.097 0.101 1.154 0.011 0.449 39.697 0.06 23956. 0.4626
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0.40 0.0264 0.0680 0.0471 0.0183 0.002 0.097 0.098 1.153 0.011 0.438 38.724 0.06 23963. 0.4456
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0.60 0.0396 0.0994 0.0459 0.0183 0.002 0.097 0.096 1.153 0.011 0.427 37.735 0.06 23971. 0.4285
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0.80 0.0529 0.1290 0.0446 0.0183 0.002 0.097 0.093 1.151 0.011 0.415 36.731 0.06 23979. 0.4113
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1.00 0.0661 0.1567 0.0433 0.0183 0.002 0.097 0.090 1.149 0.011 0.402 35.709 0.06 23988. 0.3939
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1.20 0.0793 0.1826 0.0419 0.0182 0.002 0.097 0.088 1.146 0.011 0.390 34.670 0.06 23997. 0.3763
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1.40 0.0925 0.2066 0.0405 0.0182 0.002 0.097 0.085 1.142 0.011 0.377 33.612 0.06 24006. 0.3586
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1.60 0.1057 0.2285 0.0391 0.0181 0.002 0.096 0.082 1.138 0.011 0.363 32.533 0.06 24016. 0.3408
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1.80 0.1189 0.2483 0.0376 0.0180 0.002 0.096 0.078 1.132 0.011 0.349 31.432 0.06 24026. 0.3228
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2.00 0.1322 0.2661 0.0360 0.0179 0.002 0.095 0.075 1.125 0.011 0.334 30.308 0.06 24037. 0.3048
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2.20 0.1454 0.2816 0.0344 0.0178 0.001 0.094 0.072 1.118 0.011 0.320 29.158 0.06 24048. 0.2866
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2.40 0.1586 0.2948 0.0328 0.0176 0.001 0.094 0.068 1.109 0.011 0.304 27.982 0.06 24060. 0.2684
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2.60 0.1718 0.3056 0.0311 0.0175 0.001 0.093 0.065 1.099 0.010 0.289 26.776 0.06 24072. 0.2501
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2.80 0.1850 0.3139 0.0293 0.0173 0.001 0.092 0.061 1.088 0.010 0.273 25.538 0.06 24084. 0.2318
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3.00 0.1982 0.3195 0.0276 0.0171 0.001 0.091 0.058 1.076 0.010 0.256 24.265 0.06 24097. 0.2135
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3.20 0.2115 0.3224 0.0258 0.0169 0.001 0.090 0.054 1.063 0.010 0.239 22.955 0.06 24111. 0.1952
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3.40 0.2247 0.3224 0.0239 0.0167 0.001 0.089 0.050 1.048 0.010 0.222 21.603 0.06 24125. 0.1770
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3.60 0.2379 0.3193 0.0220 0.0164 0.001 0.087 0.046 1.033 0.010 0.205 20.204 0.06 24140. 0.1589
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3.80 0.2511 0.3128 0.0201 0.0161 0.001 0.086 0.042 1.016 0.010 0.187 18.756 0.06 24155. 0.1410
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4.01 0.2643 0.3029 0.0182 0.0159 0.001 0.084 0.038 0.998 0.010 0.169 17.251 0.06 24171. 0.1232
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4.21 0.2775 0.2891 0.0162 0.0155 0.001 0.083 0.034 0.978 0.009 0.150 15.684 0.06 24187. 0.1058
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4.41 0.2908 0.2713 0.0142 0.0152 0.001 0.081 0.030 0.957 0.009 0.132 14.049 0.06 24204. 0.0887
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4.61 0.3040 0.2491 0.0122 0.0149 0.001 0.079 0.025 0.935 0.009 0.113 12.337 0.06 24221. 0.0721
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4.81 0.3172 0.2221 0.0101 0.0145 0.001 0.077 0.021 0.911 0.009 0.094 10.541 0.06 24239. 0.0563
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5.01 0.3304 0.1899 0.0081 0.0141 0.001 0.075 0.017 0.886 0.008 0.075 8.652 0.06 24257. 0.0413
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5.21 0.3436 0.1520 0.0060 0.0137 0.001 0.073 0.013 0.860 0.008 0.056 6.657 0.06 24277. 0.0274
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5.41 0.3568 0.1078 0.0040 0.0132 0.001 0.070 0.008 0.833 0.008 0.037 4.546 0.06 24296. 0.0152
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5.61 0.3701 0.0566 0.0020 0.0128 0.001 0.068 0.004 0.804 0.008 0.018 2.301 0.06 24316. 0.0054
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5.81 0.3833 -0.0032 -0.0001 0.0123 0.001 0.065 0.000 0.773 0.007 -0.001 -0.127 0.06 24336. 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 0.0497 0.0158 0.011 0.336 0.415 7.961 0.038 1.846 23.644 0.13 47897. 0.5586
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0.40 0.0133 0.0407 0.0485 0.0158 0.011 0.337 0.405 7.965 0.038 1.803 23.087 0.13 47911. 0.5391
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0.80 0.0265 0.0793 0.0473 0.0158 0.011 0.337 0.395 7.963 0.038 1.759 22.524 0.13 47926. 0.5194
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1.21 0.0398 0.1160 0.0461 0.0158 0.011 0.336 0.385 7.956 0.038 1.713 21.955 0.13 47942. 0.4997
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1.61 0.0530 0.1506 0.0448 0.0158 0.011 0.336 0.374 7.943 0.038 1.665 21.380 0.13 47958. 0.4798
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2.01 0.0663 0.1832 0.0435 0.0157 0.011 0.335 0.363 7.923 0.038 1.616 20.799 0.13 47976. 0.4598
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2.41 0.0795 0.2136 0.0421 0.0157 0.011 0.334 0.352 7.896 0.038 1.565 20.212 0.13 47994. 0.4397
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2.81 0.0928 0.2418 0.0407 0.0156 0.011 0.332 0.340 7.861 0.038 1.512 19.616 0.13 48013. 0.4195
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3.21 0.1061 0.2679 0.0392 0.0155 0.010 0.330 0.328 7.818 0.037 1.458 19.013 0.13 48032. 0.3992
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3.62 0.1193 0.2916 0.0377 0.0154 0.010 0.328 0.315 7.767 0.037 1.401 18.399 0.13 48053. 0.3787
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4.02 0.1326 0.3131 0.0362 0.0153 0.010 0.326 0.302 7.707 0.037 1.343 17.776 0.13 48075. 0.3583
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4.42 0.1458 0.3321 0.0345 0.0152 0.010 0.323 0.289 7.637 0.036 1.284 17.141 0.13 48097. 0.3377
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4.82 0.1591 0.3486 0.0329 0.0150 0.010 0.319 0.275 7.558 0.036 1.222 16.493 0.13 48120. 0.3171
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5.22 0.1723 0.3625 0.0312 0.0148 0.010 0.316 0.261 7.469 0.036 1.160 15.831 0.13 48145. 0.2964
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5.62 0.1856 0.3736 0.0295 0.0146 0.010 0.311 0.246 7.369 0.035 1.095 15.153 0.13 48170. 0.2757
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6.03 0.1989 0.3819 0.0277 0.0144 0.010 0.307 0.231 7.259 0.035 1.029 14.457 0.13 48196. 0.2550
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6.43 0.2121 0.3872 0.0259 0.0142 0.010 0.302 0.216 7.138 0.034 0.962 13.739 0.13 48223. 0.2343
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6.83 0.2254 0.3892 0.0240 0.0139 0.009 0.296 0.201 7.006 0.033 0.893 12.998 0.13 48252. 0.2136
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7.23 0.2386 0.3877 0.0222 0.0136 0.009 0.290 0.185 6.863 0.033 0.823 12.230 0.13 48281. 0.1929
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7.63 0.2519 0.3825 0.0202 0.0133 0.009 0.283 0.169 6.708 0.032 0.752 11.430 0.13 48312. 0.1723
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8.03 0.2651 0.3732 0.0183 0.0130 0.009 0.276 0.153 6.540 0.031 0.680 10.595 0.13 48343. 0.1519
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8.44 0.2784 0.3594 0.0163 0.0126 0.009 0.269 0.136 6.361 0.030 0.606 9.718 0.13 48376. 0.1316
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8.84 0.2917 0.3407 0.0143 0.0123 0.008 0.261 0.120 6.169 0.029 0.532 8.793 0.13 48410. 0.1115
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9.24 0.3049 0.3165 0.0123 0.0118 0.008 0.252 0.103 5.965 0.028 0.457 7.813 0.13 48444. 0.0918
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9.64 0.3182 0.2861 0.0103 0.0114 0.008 0.243 0.086 5.749 0.027 0.382 6.768 0.13 48481. 0.0727
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10.04 0.3314 0.2486 0.0082 0.0110 0.007 0.233 0.069 5.520 0.026 0.306 5.647 0.13 48518. 0.0543
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10.45 0.3447 0.2032 0.0062 0.0105 0.007 0.223 0.052 5.280 0.025 0.230 4.437 0.13 48556. 0.0370
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10.85 0.3579 0.1484 0.0041 0.0100 0.007 0.212 0.035 5.028 0.024 0.154 3.120 0.13 48596. 0.0213
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11.25 0.3712 0.0826 0.0021 0.0095 0.006 0.201 0.018 4.765 0.023 0.078 1.674 0.13 48636. 0.0081
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11.65 0.3845 0.0022 0.0000 0.0089 0.006 0.190 0.000 4.486 0.021 0.002 0.042 0.13 48674. 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 0.0499 0.0147 0.034 0.705 0.937 25.023 0.080 4.169 16.988 0.19 71844. 0.6031
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0.61 0.0133 0.0440 0.0487 0.0147 0.034 0.705 0.915 25.034 0.080 4.072 16.587 0.19 71866. 0.5820
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1.21 0.0267 0.0859 0.0475 0.0147 0.034 0.705 0.893 25.026 0.080 3.971 16.182 0.19 71889. 0.5608
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1.82 0.0400 0.1257 0.0463 0.0147 0.034 0.704 0.869 24.999 0.080 3.867 15.775 0.19 71913. 0.5394
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2.42 0.0533 0.1632 0.0450 0.0147 0.033 0.703 0.845 24.949 0.079 3.759 15.364 0.19 71938. 0.5180
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3.03 0.0666 0.1985 0.0436 0.0146 0.033 0.701 0.820 24.876 0.079 3.647 14.951 0.19 71964. 0.4965
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3.63 0.0800 0.2316 0.0422 0.0146 0.033 0.698 0.794 24.777 0.079 3.532 14.534 0.19 71991. 0.4749
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4.24 0.0933 0.2623 0.0408 0.0145 0.033 0.695 0.767 24.652 0.078 3.412 14.113 0.19 72020. 0.4533
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4.85 0.1066 0.2908 0.0393 0.0144 0.033 0.690 0.739 24.497 0.078 3.288 13.688 0.19 72050. 0.4316
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5.45 0.1199 0.3168 0.0378 0.0143 0.033 0.685 0.711 24.311 0.077 3.160 13.257 0.19 72081. 0.4098
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6.06 0.1333 0.3404 0.0362 0.0142 0.032 0.679 0.681 24.092 0.077 3.029 12.820 0.19 72113. 0.3880
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6.66 0.1466 0.3615 0.0346 0.0140 0.032 0.672 0.650 23.841 0.076 2.893 12.376 0.19 72147. 0.3661
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7.27 0.1599 0.3800 0.0329 0.0139 0.032 0.664 0.619 23.554 0.075 2.754 11.924 0.19 72182. 0.3441
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7.87 0.1732 0.3957 0.0312 0.0137 0.031 0.655 0.587 23.232 0.074 2.612 11.463 0.19 72219. 0.3221
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8.48 0.1866 0.4086 0.0295 0.0135 0.031 0.644 0.554 22.873 0.073 2.465 10.991 0.19 72257. 0.3001
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9.09 0.1999 0.4185 0.0277 0.0132 0.030 0.633 0.521 22.476 0.072 2.316 10.507 0.19 72297. 0.2780
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9.69 0.2132 0.4252 0.0259 0.0130 0.030 0.621 0.486 22.039 0.070 2.163 10.009 0.19 72338. 0.2560
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10.30 0.2265 0.4286 0.0240 0.0127 0.029 0.607 0.451 21.561 0.069 2.007 9.493 0.19 72381. 0.2339
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10.90 0.2399 0.4282 0.0221 0.0124 0.028 0.593 0.416 21.042 0.067 1.849 8.958 0.19 72426. 0.2118
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11.51 0.2532 0.4238 0.0202 0.0121 0.027 0.577 0.379 20.480 0.065 1.687 8.400 0.19 72472. 0.1897
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12.11 0.2665 0.4150 0.0182 0.0117 0.027 0.560 0.342 19.875 0.063 1.523 7.815 0.19 72520. 0.1677
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12.72 0.2798 0.4014 0.0162 0.0113 0.026 0.542 0.305 19.225 0.061 1.357 7.198 0.19 72569. 0.1458
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13.33 0.2932 0.3822 0.0142 0.0109 0.025 0.522 0.267 18.532 0.059 1.189 6.542 0.19 72620. 0.1240
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13.93 0.3065 0.3568 0.0122 0.0105 0.024 0.501 0.229 17.794 0.057 1.019 5.841 0.19 72673. 0.1025
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14.54 0.3198 0.3241 0.0101 0.0100 0.023 0.479 0.191 17.012 0.054 0.848 5.086 0.19 72728. 0.0815
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15.14 0.3331 0.2831 0.0081 0.0095 0.022 0.456 0.152 16.186 0.052 0.677 4.265 0.19 72784. 0.0610
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15.75 0.3465 0.2322 0.0060 0.0090 0.021 0.432 0.114 15.319 0.049 0.505 3.363 0.19 72842. 0.0416
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16.35 0.3598 0.1694 0.0040 0.0085 0.019 0.406 0.075 14.410 0.046 0.334 2.363 0.19 72902. 0.0237
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16.96 0.3731 0.0919 0.0020 0.0079 0.018 0.379 0.037 13.460 0.043 0.163 1.236 0.19 72963. 0.0087
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17.57 0.3864 -0.0073 -0.0001 0.0073 0.017 0.350 -0.003 12.440 0.040 -0.012 -0.095 0.19 73017. 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 0.0501 0.0141 0.076 1.201 1.674 56.831 0.136 7.444 13.356 0.25 95791. 0.6336
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0.82 0.0135 0.0469 0.0489 0.0141 0.076 1.201 1.634 56.853 0.136 7.268 13.037 0.25 95820. 0.6111
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1.64 0.0271 0.0915 0.0477 0.0141 0.076 1.201 1.593 56.827 0.136 7.086 12.715 0.25 95851. 0.5885
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2.46 0.0406 0.1337 0.0464 0.0141 0.076 1.199 1.550 56.751 0.135 6.896 12.392 0.25 95884. 0.5659
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3.28 0.0542 0.1736 0.0451 0.0141 0.076 1.196 1.506 56.620 0.135 6.700 12.067 0.25 95918. 0.5431
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4.10 0.0677 0.2111 0.0437 0.0140 0.076 1.192 1.461 56.428 0.135 6.497 11.741 0.25 95954. 0.5204
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4.92 0.0812 0.2463 0.0423 0.0139 0.075 1.187 1.413 56.173 0.134 6.286 11.412 0.25 95991. 0.4975
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5.74 0.0948 0.2790 0.0408 0.0139 0.075 1.180 1.364 55.848 0.133 6.069 11.081 0.25 96030. 0.4747
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6.56 0.1083 0.3092 0.0393 0.0138 0.074 1.172 1.314 55.449 0.132 5.844 10.747 0.25 96071. 0.4517
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7.38 0.1218 0.3370 0.0378 0.0137 0.074 1.162 1.262 54.971 0.131 5.611 10.409 0.25 96113. 0.4287
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8.20 0.1354 0.3621 0.0361 0.0135 0.073 1.150 1.208 54.411 0.130 5.372 10.067 0.25 96158. 0.4057
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9.03 0.1489 0.3846 0.0345 0.0134 0.072 1.136 1.152 53.766 0.128 5.125 9.720 0.25 96204. 0.3826
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9.85 0.1625 0.4043 0.0328 0.0132 0.071 1.121 1.095 53.033 0.127 4.872 9.367 0.25 96252. 0.3595
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10.67 0.1760 0.4212 0.0310 0.0130 0.070 1.103 1.037 52.209 0.125 4.612 9.008 0.25 96302. 0.3364
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11.49 0.1895 0.4351 0.0292 0.0127 0.069 1.084 0.977 51.290 0.122 4.346 8.640 0.25 96355. 0.3132
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12.31 0.2031 0.4458 0.0274 0.0125 0.067 1.062 0.916 50.273 0.120 4.073 8.262 0.25 96409. 0.2900
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13.13 0.2166 0.4531 0.0255 0.0122 0.066 1.039 0.853 49.156 0.117 3.795 7.873 0.25 96465. 0.2667
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13.95 0.2301 0.4568 0.0236 0.0119 0.064 1.013 0.789 47.935 0.114 3.511 7.470 0.25 96524. 0.2434
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14.77 0.2437 0.4565 0.0217 0.0116 0.063 0.985 0.724 46.607 0.111 3.223 7.051 0.25 96585. 0.2201
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15.59 0.2572 0.4518 0.0197 0.0112 0.061 0.954 0.658 45.171 0.108 2.929 6.612 0.25 96648. 0.1967
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16.41 0.2708 0.4423 0.0177 0.0108 0.059 0.922 0.591 43.625 0.104 2.631 6.149 0.25 96713. 0.1734
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17.23 0.2843 0.4274 0.0157 0.0104 0.056 0.887 0.524 41.966 0.100 2.329 5.658 0.25 96781. 0.1501
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18.05 0.2978 0.4061 0.0136 0.0100 0.054 0.849 0.455 40.196 0.096 2.023 5.133 0.26 96851. 0.1269
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18.87 0.3114 0.3777 0.0115 0.0095 0.051 0.810 0.386 38.313 0.091 1.715 4.565 0.26 96924. 0.1040
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19.69 0.3249 0.3406 0.0095 0.0090 0.049 0.767 0.316 36.320 0.087 1.405 3.946 0.26 96999. 0.0813
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20.51 0.3384 0.2934 0.0074 0.0085 0.046 0.723 0.246 34.218 0.082 1.095 3.262 0.26 97076. 0.0594
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21.33 0.3520 0.2336 0.0053 0.0079 0.043 0.676 0.176 32.010 0.076 0.784 2.498 0.26 97156. 0.0385
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22.15 0.3655 0.1582 0.0032 0.0074 0.040 0.628 0.107 29.700 0.071 0.475 1.629 0.26 97238. 0.0195
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22.97 0.3791 0.0622 0.0011 0.0068 0.037 0.576 0.037 27.279 0.065 0.165 0.618 0.26 97319. 0.0044
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23.79 0.3926
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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 0.0504 0.0137 0.145 1.825 2.629 107.964 0.206 11.694 11.045 0.32 119737. 0.6567
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1.01 0.0133 0.0478 0.0492 0.0137 0.145 1.826 2.568 107.995 0.206 11.422 10.785 0.32 119773. 0.6338
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2.02 0.0267 0.0933 0.0480 0.0137 0.145 1.825 2.504 107.935 0.206 11.139 10.524 0.32 119811. 0.6108
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3.03 0.0400 0.1365 0.0467 0.0137 0.145 1.822 2.438 107.775 0.206 10.846 10.262 0.32 119852. 0.5877
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4.05 0.0534 0.1773 0.0454 0.0137 0.144 1.817 2.370 107.509 0.205 10.543 10.000 0.32 119894. 0.5646
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5.06 0.0667 0.2158 0.0440 0.0136 0.144 1.811 2.300 107.127 0.205 10.229 9.736 0.32 119937. 0.5415
|
|
6.07 0.0801 0.2519 0.0426 0.0136 0.143 1.802 2.226 106.620 0.204 9.903 9.472 0.32 119983. 0.5183
|
|
7.08 0.0934 0.2857 0.0412 0.0135 0.142 1.792 2.151 105.979 0.202 9.567 9.205 0.32 120031. 0.4951
|
|
8.09 0.1068 0.3170 0.0397 0.0134 0.141 1.778 2.073 105.195 0.201 9.220 8.937 0.32 120081. 0.4719
|
|
9.10 0.1201 0.3458 0.0382 0.0133 0.140 1.762 1.992 104.258 0.199 8.861 8.667 0.32 120134. 0.4486
|
|
10.11 0.1335 0.3721 0.0366 0.0131 0.138 1.744 1.909 103.162 0.197 8.491 8.393 0.32 120188. 0.4253
|
|
11.12 0.1468 0.3958 0.0349 0.0130 0.137 1.723 1.824 101.901 0.195 8.111 8.117 0.32 120245. 0.4020
|
|
12.14 0.1602 0.4169 0.0332 0.0128 0.135 1.698 1.736 100.470 0.192 7.720 7.836 0.32 120304. 0.3786
|
|
13.15 0.1735 0.4351 0.0315 0.0126 0.133 1.671 1.646 98.863 0.189 7.320 7.550 0.32 120366. 0.3552
|
|
14.16 0.1869 0.4505 0.0298 0.0123 0.130 1.641 1.553 97.072 0.185 6.910 7.258 0.32 120430. 0.3318
|
|
15.17 0.2002 0.4628 0.0279 0.0121 0.128 1.607 1.459 95.092 0.182 6.490 6.959 0.32 120496. 0.3083
|
|
16.18 0.2136 0.4718 0.0261 0.0118 0.125 1.571 1.363 92.917 0.177 6.061 6.652 0.32 120565. 0.2848
|
|
17.19 0.2269 0.4774 0.0242 0.0115 0.121 1.531 1.264 90.541 0.173 5.624 6.334 0.32 120637. 0.2612
|
|
18.20 0.2403 0.4791 0.0223 0.0112 0.118 1.487 1.164 87.959 0.168 5.179 6.004 0.32 120711. 0.2376
|
|
19.21 0.2536 0.4766 0.0203 0.0108 0.114 1.440 1.062 85.166 0.163 4.726 5.658 0.32 120788. 0.2139
|
|
20.23 0.2670 0.4695 0.0184 0.0104 0.110 1.389 0.959 82.159 0.157 4.266 5.295 0.32 120868. 0.1902
|
|
21.24 0.2803 0.4571 0.0164 0.0100 0.106 1.334 0.854 78.935 0.151 3.800 4.909 0.32 120951. 0.1664
|
|
22.25 0.2937 0.4386 0.0143 0.0096 0.101 1.276 0.748 75.492 0.144 3.329 4.497 0.32 121037. 0.1427
|
|
23.26 0.3070 0.4131 0.0123 0.0091 0.096 1.214 0.642 71.831 0.137 2.854 4.051 0.32 121125. 0.1190
|
|
24.27 0.3204 0.3793 0.0102 0.0086 0.091 1.149 0.534 67.954 0.130 2.375 3.564 0.32 121217. 0.0955
|
|
25.28 0.3337 0.3354 0.0082 0.0081 0.086 1.080 0.426 63.864 0.122 1.895 3.026 0.32 121311. 0.0724
|
|
26.29 0.3471 0.2791 0.0061 0.0076 0.080 1.007 0.318 59.567 0.114 1.414 2.421 0.32 121408. 0.0501
|
|
27.30 0.3604 0.2072 0.0040 0.0070 0.074 0.931 0.210 55.070 0.105 0.935 1.731 0.32 121508. 0.0291
|
|
28.32 0.3738 0.1148 0.0020 0.0064 0.068 0.852 0.103 50.372 0.096 0.457 0.925 0.32 121610. 0.0109
|
|
29.33 0.3871 -0.0113 -0.0002 0.0058 0.061 0.765 -0.009 45.258 0.086 -0.039 -0.088 0.32 121692. 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 0.0507 0.0135 0.246 2.581 3.811 183.220 0.292 16.950 9.433 0.38 143681. 0.6753
|
|
1.21 0.0133 0.0490 0.0495 0.0135 0.246 2.581 3.722 183.248 0.292 16.556 9.213 0.38 143725. 0.6518
|
|
2.42 0.0267 0.0956 0.0483 0.0135 0.246 2.580 3.630 183.115 0.291 16.146 8.991 0.38 143771. 0.6282
|
|
3.64 0.0400 0.1398 0.0470 0.0135 0.245 2.575 3.535 182.806 0.291 15.722 8.770 0.38 143819. 0.6046
|
|
4.85 0.0533 0.1817 0.0457 0.0134 0.244 2.568 3.436 182.310 0.290 15.282 8.548 0.38 143870. 0.5810
|
|
6.06 0.0667 0.2212 0.0443 0.0134 0.244 2.558 3.333 181.610 0.289 14.827 8.325 0.38 143922. 0.5574
|
|
7.27 0.0800 0.2583 0.0429 0.0133 0.242 2.545 3.228 180.690 0.288 14.356 8.102 0.38 143978. 0.5338
|
|
8.49 0.0933 0.2930 0.0415 0.0132 0.241 2.529 3.118 179.536 0.286 13.869 7.877 0.38 144035. 0.5101
|
|
9.70 0.1067 0.3253 0.0400 0.0131 0.239 2.509 3.005 178.128 0.284 13.366 7.652 0.38 144096. 0.4864
|
|
10.91 0.1200 0.3551 0.0384 0.0130 0.237 2.486 2.888 176.452 0.281 12.847 7.424 0.38 144158. 0.4627
|
|
12.12 0.1333 0.3823 0.0368 0.0128 0.234 2.458 2.768 174.496 0.278 12.311 7.195 0.38 144224. 0.4390
|
|
13.33 0.1467 0.4070 0.0352 0.0127 0.231 2.426 2.644 172.250 0.274 11.761 6.962 0.38 144292. 0.4152
|
|
14.55 0.1600 0.4290 0.0335 0.0125 0.228 2.391 2.517 169.704 0.270 11.196 6.727 0.38 144363. 0.3914
|
|
15.76 0.1733 0.4482 0.0317 0.0123 0.224 2.350 2.387 166.847 0.266 10.616 6.488 0.38 144437. 0.3676
|
|
16.97 0.1867 0.4645 0.0300 0.0120 0.219 2.306 2.253 163.668 0.260 10.022 6.244 0.38 144514. 0.3437
|
|
18.18 0.2000 0.4778 0.0282 0.0118 0.215 2.256 2.117 160.156 0.255 9.414 5.994 0.38 144593. 0.3198
|
|
19.40 0.2133 0.4878 0.0263 0.0115 0.210 2.202 1.977 156.300 0.249 8.794 5.737 0.38 144676. 0.2958
|
|
20.61 0.2267 0.4943 0.0244 0.0112 0.204 2.143 1.835 152.091 0.242 8.161 5.472 0.38 144762. 0.2718
|
|
21.82 0.2400 0.4970 0.0225 0.0109 0.198 2.078 1.690 147.519 0.235 7.517 5.196 0.38 144851. 0.2477
|
|
23.03 0.2533 0.4955 0.0205 0.0105 0.191 2.008 1.543 142.577 0.227 6.862 4.908 0.38 144944. 0.2235
|
|
24.24 0.2667 0.4893 0.0185 0.0101 0.184 1.934 1.393 137.257 0.218 6.197 4.604 0.38 145040. 0.1993
|
|
25.46 0.2800 0.4777 0.0165 0.0097 0.176 1.853 1.242 131.556 0.209 5.523 4.281 0.38 145139. 0.1749
|
|
26.67 0.2934 0.4600 0.0145 0.0092 0.168 1.768 1.088 125.471 0.200 4.841 3.934 0.38 145241. 0.1505
|
|
27.88 0.3067 0.4350 0.0124 0.0088 0.160 1.676 0.934 119.002 0.189 4.153 3.559 0.38 145347. 0.1261
|
|
29.09 0.3200 0.4014 0.0103 0.0083 0.150 1.580 0.778 112.153 0.178 3.461 3.147 0.38 145457. 0.1018
|
|
30.30 0.3334 0.3571 0.0083 0.0077 0.141 1.478 0.622 104.929 0.167 2.766 2.688 0.38 145570. 0.0777
|
|
31.52 0.3467 0.2997 0.0062 0.0072 0.131 1.371 0.466 97.342 0.155 2.071 2.169 0.38 145686. 0.0543
|
|
32.73 0.3600 0.2253 0.0041 0.0066 0.120 1.259 0.309 89.405 0.142 1.377 1.570 0.38 145806. 0.0320
|
|
33.94 0.3734 0.1281 0.0020 0.0060 0.109 1.143 0.154 81.115 0.129 0.685 0.861 0.38 145928. 0.0124
|
|
35.15 0.3867 -0.0066 -0.0001 0.0053 0.097 1.016 -0.007 72.123 0.115 -0.030 -0.043 0.38 146028. 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 0.0511 0.0133 0.386 3.474 5.228 287.743 0.393 23.252 8.240 0.44 167623. 0.6909
|
|
1.43 0.0135 0.0505 0.0499 0.0133 0.386 3.474 5.104 287.736 0.393 22.704 8.046 0.44 167675. 0.6667
|
|
2.87 0.0270 0.0986 0.0486 0.0133 0.385 3.471 4.976 287.460 0.392 22.134 7.852 0.44 167730. 0.6423
|
|
4.30 0.0405 0.1443 0.0473 0.0133 0.385 3.464 4.843 286.891 0.391 21.543 7.657 0.44 167788. 0.6180
|
|
5.73 0.0540 0.1875 0.0460 0.0133 0.384 3.453 4.705 286.009 0.390 20.930 7.462 0.44 167848. 0.5936
|
|
7.16 0.0675 0.2282 0.0446 0.0132 0.382 3.439 4.563 284.785 0.388 20.295 7.267 0.44 167910. 0.5693
|
|
8.60 0.0810 0.2665 0.0431 0.0131 0.380 3.419 4.415 283.196 0.386 19.639 7.071 0.44 167976. 0.5449
|
|
10.03 0.0946 0.3023 0.0417 0.0130 0.377 3.396 4.263 281.214 0.384 18.960 6.875 0.44 168045. 0.5206
|
|
11.46 0.1081 0.3355 0.0401 0.0129 0.374 3.367 4.105 278.809 0.380 18.258 6.678 0.44 168116. 0.4962
|
|
12.89 0.1216 0.3662 0.0385 0.0128 0.370 3.332 3.942 275.955 0.376 17.534 6.479 0.44 168191. 0.4717
|
|
14.33 0.1351 0.3943 0.0369 0.0126 0.366 3.292 3.774 272.635 0.372 16.787 6.279 0.44 168269. 0.4473
|
|
15.76 0.1486 0.4198 0.0352 0.0125 0.361 3.246 3.601 268.831 0.367 16.019 6.076 0.44 168350. 0.4229
|
|
17.19 0.1621 0.4424 0.0335 0.0123 0.355 3.194 3.424 264.526 0.361 15.229 5.871 0.44 168435. 0.3984
|
|
18.62 0.1756 0.4623 0.0317 0.0120 0.348 3.136 3.242 259.702 0.354 14.420 5.662 0.44 168523. 0.3739
|
|
20.06 0.1891 0.4791 0.0299 0.0118 0.341 3.071 3.056 254.341 0.347 13.591 5.449 0.45 168615. 0.3493
|
|
21.49 0.2026 0.4928 0.0280 0.0115 0.333 3.000 2.865 248.423 0.339 12.744 5.231 0.45 168710. 0.3247
|
|
22.92 0.2161 0.5031 0.0261 0.0112 0.324 2.921 2.670 241.931 0.330 11.878 5.006 0.45 168808. 0.3000
|
|
24.35 0.2296 0.5097 0.0242 0.0109 0.315 2.836 2.472 234.849 0.320 10.995 4.774 0.45 168911. 0.2753
|
|
25.79 0.2431 0.5123 0.0222 0.0105 0.305 2.743 2.270 227.163 0.310 10.096 4.532 0.45 169017. 0.2504
|
|
27.22 0.2566 0.5105 0.0202 0.0101 0.293 2.643 2.064 218.859 0.299 9.182 4.278 0.45 169128. 0.2254
|
|
28.65 0.2701 0.5036 0.0181 0.0097 0.282 2.535 1.856 209.928 0.286 8.255 4.010 0.45 169242. 0.2003
|
|
30.08 0.2837 0.4910 0.0161 0.0093 0.269 2.419 1.645 200.362 0.273 7.315 3.723 0.45 169360. 0.1751
|
|
31.52 0.2972 0.4716 0.0140 0.0088 0.255 2.296 1.431 190.160 0.259 6.365 3.413 0.45 169483. 0.1497
|
|
32.95 0.3107 0.4442 0.0119 0.0083 0.240 2.165 1.216 179.322 0.245 5.408 3.075 0.45 169609. 0.1243
|
|
34.38 0.3242 0.4069 0.0098 0.0078 0.225 2.027 0.999 167.856 0.229 4.444 2.700 0.45 169740. 0.0990
|
|
35.81 0.3377 0.3575 0.0076 0.0072 0.209 1.881 0.782 155.777 0.213 3.478 2.277 0.45 169875. 0.0738
|
|
37.25 0.3512 0.2923 0.0055 0.0066 0.192 1.728 0.565 143.103 0.195 2.512 1.790 0.45 170014. 0.0493
|
|
38.68 0.3647 0.2063 0.0034 0.0060 0.174 1.568 0.348 129.854 0.177 1.549 1.217 0.45 170157. 0.0263
|
|
40.11 0.3782 0.0909 0.0013 0.0054 0.156 1.400 0.132 115.986 0.158 0.588 0.517 0.45 170300. 0.0069
|
|
41.54 0.3917
|
|
|
|
|
|
|
|
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 0.0516 0.0133 0.573 4.514 6.892 427.202 0.510 30.655 7.317 0.51 191563. 0.7045
|
|
1.63 0.0134 0.0511 0.0503 0.0133 0.573 4.512 6.730 427.100 0.510 29.934 7.147 0.51 191623. 0.6799
|
|
3.26 0.0269 0.0997 0.0491 0.0132 0.572 4.507 6.561 426.591 0.509 29.185 6.976 0.51 191686. 0.6553
|
|
4.89 0.0403 0.1459 0.0478 0.0132 0.571 4.497 6.387 425.639 0.508 28.408 6.806 0.51 191751. 0.6307
|
|
6.52 0.0538 0.1897 0.0464 0.0132 0.569 4.482 6.206 424.211 0.506 27.603 6.635 0.51 191820. 0.6062
|
|
8.15 0.0672 0.2310 0.0450 0.0131 0.566 4.461 6.018 422.271 0.504 26.769 6.464 0.51 191892. 0.5816
|
|
9.78 0.0807 0.2699 0.0436 0.0130 0.563 4.435 5.824 419.779 0.501 25.907 6.293 0.51 191967. 0.5570
|
|
11.41 0.0941 0.3062 0.0421 0.0129 0.559 4.403 5.624 416.695 0.497 25.016 6.122 0.51 192045. 0.5324
|
|
13.04 0.1076 0.3401 0.0405 0.0128 0.554 4.363 5.417 412.974 0.493 24.095 5.950 0.51 192127. 0.5078
|
|
14.67 0.1210 0.3715 0.0389 0.0127 0.548 4.317 5.203 408.578 0.488 23.144 5.776 0.51 192212. 0.4832
|
|
16.30 0.1345 0.4003 0.0373 0.0125 0.541 4.263 4.983 403.479 0.482 22.164 5.601 0.51 192301. 0.4586
|
|
17.93 0.1479 0.4265 0.0356 0.0123 0.533 4.201 4.756 397.652 0.475 21.156 5.425 0.51 192394. 0.4339
|
|
19.56 0.1614 0.4499 0.0338 0.0121 0.524 4.132 4.524 391.072 0.467 20.121 5.246 0.51 192490. 0.4092
|
|
21.19 0.1748 0.4706 0.0321 0.0119 0.515 4.054 4.285 383.711 0.458 19.059 5.065 0.51 192590. 0.3845
|
|
22.82 0.1883 0.4882 0.0302 0.0117 0.504 3.968 4.040 375.541 0.448 17.972 4.880 0.51 192694. 0.3597
|
|
24.45 0.2017 0.5028 0.0284 0.0114 0.492 3.873 3.791 366.535 0.438 16.860 4.691 0.51 192802. 0.3349
|
|
26.08 0.2152 0.5141 0.0264 0.0111 0.478 3.768 3.535 356.667 0.426 15.725 4.496 0.51 192915. 0.3100
|
|
27.71 0.2286 0.5217 0.0245 0.0107 0.464 3.655 3.275 345.912 0.413 14.567 4.294 0.51 193031. 0.2850
|
|
29.34 0.2421 0.5254 0.0225 0.0104 0.448 3.531 3.010 334.250 0.399 13.388 4.084 0.51 193152. 0.2599
|
|
30.97 0.2555 0.5247 0.0205 0.0100 0.431 3.398 2.740 321.660 0.384 12.189 3.864 0.51 193278. 0.2346
|
|
32.60 0.2690 0.5190 0.0185 0.0096 0.413 3.255 2.467 308.126 0.368 10.973 3.631 0.51 193407. 0.2092
|
|
34.23 0.2824 0.5076 0.0164 0.0091 0.394 3.102 2.190 293.640 0.351 9.741 3.383 0.51 193542. 0.1836
|
|
35.86 0.2959 0.4896 0.0143 0.0086 0.373 2.939 1.910 278.196 0.332 8.495 3.114 0.51 193681. 0.1578
|
|
37.49 0.3093 0.4634 0.0122 0.0081 0.351 2.766 1.627 261.796 0.312 7.238 2.819 0.51 193824. 0.1319
|
|
39.12 0.3228 0.4274 0.0100 0.0076 0.328 2.583 1.343 244.452 0.292 5.974 2.492 0.51 193973. 0.1059
|
|
40.75 0.3362 0.3790 0.0079 0.0070 0.303 2.390 1.058 226.183 0.270 4.706 2.121 0.51 194126. 0.0800
|
|
42.38 0.3497 0.3146 0.0058 0.0064 0.278 2.187 0.773 207.019 0.247 3.437 1.693 0.51 194284. 0.0546
|
|
44.01 0.3631 0.2286 0.0037 0.0058 0.251 1.976 0.488 186.990 0.223 2.173 1.185 0.51 194446. 0.0304
|
|
45.64 0.3766 0.1119 0.0015 0.0052 0.223 1.754 0.205 166.055 0.198 0.911 0.559 0.51 194609. 0.0093
|
|
47.27 0.3900
|
|
|
|
|
|
|
|
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 0.0521 0.0133 0.815 5.710 8.819 608.014 0.645 39.228 6.579 0.57 215500. 0.7165
|
|
1.81 0.0133 0.0511 0.0509 0.0132 0.815 5.707 8.614 607.715 0.645 38.314 6.429 0.57 215567. 0.6920
|
|
3.63 0.0266 0.0999 0.0497 0.0132 0.814 5.699 8.400 606.834 0.644 37.364 6.279 0.57 215637. 0.6673
|
|
5.44 0.0399 0.1463 0.0483 0.0132 0.812 5.685 8.179 605.322 0.642 36.379 6.128 0.57 215711. 0.6427
|
|
7.26 0.0532 0.1902 0.0470 0.0131 0.809 5.664 7.949 603.132 0.640 35.359 5.978 0.57 215788. 0.6181
|
|
9.07 0.0665 0.2318 0.0456 0.0131 0.805 5.637 7.712 600.216 0.637 34.304 5.828 0.57 215868. 0.5935
|
|
10.89 0.0798 0.2710 0.0441 0.0130 0.800 5.602 7.467 596.514 0.633 33.212 5.678 0.57 215952. 0.5689
|
|
12.70 0.0931 0.3078 0.0426 0.0129 0.794 5.559 7.213 591.976 0.628 32.085 5.527 0.57 216039. 0.5444
|
|
14.52 0.1065 0.3421 0.0411 0.0128 0.787 5.508 6.951 586.538 0.622 30.920 5.376 0.57 216130. 0.5198
|
|
16.33 0.1198 0.3740 0.0395 0.0126 0.778 5.448 6.681 580.143 0.616 29.718 5.223 0.57 216225. 0.4951
|
|
18.15 0.1331 0.4033 0.0378 0.0125 0.768 5.379 6.403 572.753 0.608 28.479 5.070 0.57 216324. 0.4705
|
|
19.96 0.1464 0.4302 0.0362 0.0123 0.757 5.300 6.116 564.332 0.599 27.205 4.916 0.57 216427. 0.4459
|
|
21.77 0.1597 0.4543 0.0344 0.0121 0.744 5.211 5.822 554.846 0.589 25.897 4.760 0.57 216534. 0.4212
|
|
23.59 0.1730 0.4758 0.0326 0.0119 0.730 5.111 5.521 544.256 0.577 24.556 4.601 0.57 216645. 0.3964
|
|
25.40 0.1863 0.4944 0.0308 0.0116 0.714 5.001 5.212 532.524 0.565 23.183 4.439 0.57 216761. 0.3717
|
|
27.22 0.1996 0.5100 0.0289 0.0113 0.697 4.880 4.896 519.613 0.551 21.779 4.274 0.57 216881. 0.3468
|
|
29.03 0.2129 0.5224 0.0270 0.0110 0.678 4.747 4.574 505.485 0.536 20.345 4.104 0.57 217006. 0.3219
|
|
30.85 0.2262 0.5313 0.0251 0.0107 0.657 4.603 4.245 490.107 0.520 18.883 3.929 0.57 217135. 0.2969
|
|
32.66 0.2395 0.5364 0.0231 0.0103 0.635 4.446 3.911 473.446 0.502 17.394 3.746 0.57 217269. 0.2717
|
|
34.48 0.2528 0.5374 0.0211 0.0099 0.611 4.278 3.570 455.477 0.483 15.880 3.555 0.57 217408. 0.2464
|
|
36.29 0.2661 0.5335 0.0191 0.0095 0.585 4.096 3.225 436.176 0.463 14.344 3.353 0.57 217551. 0.2208
|
|
38.11 0.2794 0.5242 0.0170 0.0091 0.557 3.902 2.875 415.528 0.441 12.787 3.138 0.57 217700. 0.1951
|
|
39.92 0.2927 0.5085 0.0149 0.0086 0.528 3.696 2.521 393.524 0.418 11.212 2.905 0.57 217854. 0.1692
|
|
41.73 0.3061 0.4850 0.0128 0.0081 0.496 3.476 2.163 370.167 0.393 9.623 2.651 0.57 218012. 0.1430
|
|
43.55 0.3194 0.4521 0.0107 0.0075 0.463 3.244 1.804 345.468 0.367 8.023 2.368 0.57 218176. 0.1166
|
|
45.36 0.3327 0.4074 0.0085 0.0070 0.428 3.000 1.443 319.454 0.339 6.418 2.049 0.57 218346. 0.0902
|
|
47.18 0.3460 0.3473 0.0064 0.0064 0.392 2.744 1.081 292.162 0.310 4.810 1.679 0.57 218520. 0.0640
|
|
48.99 0.3593 0.2664 0.0043 0.0057 0.354 2.476 0.721 263.640 0.280 3.207 1.240 0.57 218699. 0.0386
|
|
50.81 0.3726 0.1562 0.0021 0.0051 0.314 2.196 0.362 233.883 0.248 1.608 0.701 0.58 218881. 0.0155
|
|
52.62 0.3859 -0.0065 -0.0001 0.0044 0.270 1.892 -0.013 201.422 0.214 -0.056 -0.028 0.58 219022. 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 0.0528 0.0133 1.123 7.080 11.031 837.683 0.800 49.065 5.973 0.63 239433. 0.7275
|
|
2.05 0.0135 0.0524 0.0516 0.0133 1.122 7.074 10.769 836.992 0.799 47.899 5.836 0.63 239510. 0.7023
|
|
4.10 0.0270 0.1024 0.0503 0.0133 1.120 7.061 10.496 835.453 0.798 46.687 5.698 0.63 239590. 0.6770
|
|
6.15 0.0406 0.1498 0.0489 0.0132 1.117 7.041 10.214 832.993 0.795 45.431 5.561 0.63 239673. 0.6518
|
|
8.19 0.0541 0.1949 0.0475 0.0132 1.112 7.012 9.921 829.545 0.792 44.130 5.425 0.63 239761. 0.6266
|
|
10.24 0.0676 0.2374 0.0461 0.0131 1.106 6.973 9.618 825.038 0.788 42.783 5.288 0.63 239852. 0.6014
|
|
12.29 0.0811 0.2775 0.0446 0.0130 1.099 6.926 9.305 819.388 0.782 41.389 5.151 0.63 239948. 0.5762
|
|
14.34 0.0946 0.3152 0.0430 0.0129 1.090 6.868 8.981 812.516 0.776 39.949 5.014 0.63 240048. 0.5510
|
|
16.39 0.1082 0.3503 0.0414 0.0128 1.079 6.798 8.647 804.336 0.768 38.461 4.876 0.64 240152. 0.5258
|
|
18.44 0.1217 0.3829 0.0397 0.0126 1.066 6.718 8.301 794.763 0.759 36.924 4.738 0.64 240260. 0.5006
|
|
20.48 0.1352 0.4129 0.0380 0.0125 1.051 6.624 7.945 783.744 0.748 35.341 4.598 0.64 240373. 0.4753
|
|
22.53 0.1487 0.4403 0.0363 0.0123 1.034 6.519 7.579 771.229 0.736 33.713 4.457 0.64 240490. 0.4500
|
|
24.58 0.1622 0.4650 0.0345 0.0120 1.015 6.400 7.203 757.167 0.723 32.040 4.315 0.64 240613. 0.4247
|
|
26.63 0.1758 0.4869 0.0326 0.0118 0.994 6.267 6.818 741.502 0.708 30.326 4.170 0.64 240740. 0.3993
|
|
28.68 0.1893 0.5058 0.0308 0.0115 0.971 6.121 6.423 724.178 0.692 28.570 4.023 0.64 240872. 0.3739
|
|
30.73 0.2028 0.5216 0.0288 0.0112 0.946 5.960 6.020 705.144 0.673 26.775 3.872 0.64 241009. 0.3484
|
|
32.78 0.2163 0.5340 0.0268 0.0109 0.918 5.784 5.608 684.344 0.654 24.942 3.717 0.64 241151. 0.3228
|
|
34.82 0.2298 0.5428 0.0248 0.0105 0.887 5.593 5.187 661.731 0.632 23.073 3.556 0.64 241299. 0.2970
|
|
36.87 0.2434 0.5476 0.0228 0.0101 0.855 5.386 4.760 637.262 0.609 21.170 3.388 0.64 241452. 0.2710
|
|
38.92 0.2569 0.5479 0.0207 0.0097 0.819 5.163 4.325 610.899 0.583 19.236 3.211 0.64 241611. 0.2449
|
|
40.97 0.2704 0.5430 0.0186 0.0093 0.781 4.924 3.883 582.613 0.556 17.273 3.023 0.64 241775. 0.2185
|
|
43.02 0.2839 0.5321 0.0165 0.0088 0.741 4.669 3.436 552.384 0.527 15.285 2.822 0.64 241945. 0.1918
|
|
45.07 0.2974 0.5141 0.0143 0.0083 0.698 4.397 2.985 520.205 0.497 13.276 2.602 0.64 242121. 0.1649
|
|
47.12 0.3110 0.4874 0.0121 0.0077 0.652 4.109 2.529 486.084 0.464 11.249 2.360 0.64 242302. 0.1376
|
|
49.16 0.3245 0.4498 0.0099 0.0072 0.604 3.804 2.071 450.048 0.430 9.211 2.087 0.64 242490. 0.1101
|
|
51.21 0.3380 0.3981 0.0077 0.0065 0.553 3.484 1.611 412.142 0.394 7.168 1.773 0.64 242683. 0.0826
|
|
53.26 0.3515 0.3276 0.0055 0.0059 0.499 3.148 1.152 372.429 0.356 5.125 1.403 0.64 242882. 0.0552
|
|
55.31 0.3650 0.2307 0.0033 0.0053 0.444 2.797 0.694 330.968 0.316 3.088 0.951 0.64 243086. 0.0291
|
|
57.36 0.3786 0.0937 0.0011 0.0046 0.386 2.431 0.236 287.561 0.275 1.051 0.373 0.64 243289. 0.0066
|
|
59.41 0.3921
|
|
|
|
|
|
|
|
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 0.0536 0.0134 1.509 8.647 13.554 1125.370 0.977 60.289 5.463 0.70 263362. 0.7376
|
|
2.22 0.0133 0.0519 0.0524 0.0134 1.507 8.637 13.237 1124.041 0.976 58.876 5.341 0.70 263445. 0.7126
|
|
4.43 0.0266 0.1015 0.0511 0.0134 1.504 8.618 12.907 1121.583 0.974 57.408 5.219 0.70 263532. 0.6877
|
|
6.65 0.0399 0.1486 0.0497 0.0133 1.499 8.590 12.565 1117.908 0.970 55.887 5.098 0.70 263624. 0.6627
|
|
8.87 0.0532 0.1935 0.0483 0.0133 1.492 8.552 12.211 1112.929 0.966 54.313 4.976 0.70 263719. 0.6377
|
|
11.08 0.0665 0.2359 0.0469 0.0132 1.484 8.503 11.845 1106.552 0.961 52.685 4.855 0.70 263819. 0.6128
|
|
13.30 0.0798 0.2760 0.0454 0.0131 1.473 8.442 11.466 1098.676 0.954 51.001 4.734 0.70 263922. 0.5878
|
|
15.52 0.0931 0.3138 0.0438 0.0130 1.461 8.369 11.075 1089.198 0.946 49.262 4.612 0.70 264031. 0.5629
|
|
17.74 0.1064 0.3491 0.0422 0.0129 1.446 8.283 10.671 1078.009 0.936 47.467 4.490 0.70 264143. 0.5379
|
|
19.95 0.1197 0.3820 0.0406 0.0127 1.428 8.183 10.255 1064.998 0.925 45.614 4.367 0.70 264261. 0.5129
|
|
22.17 0.1330 0.4125 0.0389 0.0125 1.408 8.069 9.826 1050.090 0.912 43.705 4.244 0.70 264383. 0.4879
|
|
24.39 0.1463 0.4404 0.0371 0.0123 1.386 7.939 9.384 1033.225 0.897 41.742 4.120 0.70 264510. 0.4628
|
|
26.60 0.1596 0.4658 0.0353 0.0121 1.360 7.794 8.931 1014.335 0.881 39.727 3.994 0.70 264642. 0.4377
|
|
28.82 0.1729 0.4885 0.0335 0.0119 1.332 7.633 8.467 993.354 0.862 37.662 3.866 0.70 264779. 0.4126
|
|
31.04 0.1862 0.5084 0.0316 0.0116 1.301 7.455 7.992 970.211 0.842 35.547 3.736 0.70 264921. 0.3873
|
|
33.25 0.1995 0.5253 0.0297 0.0113 1.267 7.260 7.506 944.837 0.820 33.385 3.603 0.70 265069. 0.3620
|
|
35.47 0.2128 0.5390 0.0277 0.0110 1.230 7.047 7.009 917.165 0.796 31.178 3.466 0.70 265222. 0.3366
|
|
37.69 0.2261 0.5494 0.0257 0.0106 1.190 6.817 6.503 887.132 0.770 28.927 3.325 0.70 265381. 0.3110
|
|
39.91 0.2394 0.5559 0.0237 0.0102 1.146 6.567 5.988 854.684 0.742 26.635 3.178 0.70 265545. 0.2852
|
|
42.12 0.2527 0.5583 0.0216 0.0098 1.099 6.299 5.464 819.772 0.712 24.305 3.023 0.70 265716. 0.2592
|
|
44.34 0.2660 0.5559 0.0195 0.0093 1.049 6.012 4.933 782.363 0.679 21.940 2.860 0.70 265892. 0.2329
|
|
46.56 0.2793 0.5479 0.0174 0.0089 0.996 5.705 4.394 742.432 0.645 19.543 2.684 0.70 266074. 0.2063
|
|
48.77 0.2926 0.5333 0.0152 0.0084 0.939 5.378 3.849 699.971 0.608 17.120 2.494 0.70 266262. 0.1794
|
|
50.99 0.3059 0.5107 0.0131 0.0078 0.878 5.033 3.299 654.993 0.569 14.674 2.285 0.70 266457. 0.1522
|
|
53.21 0.3192 0.4781 0.0109 0.0073 0.815 4.668 2.746 607.532 0.527 12.212 2.050 0.70 266657. 0.1246
|
|
55.42 0.3325 0.4328 0.0087 0.0067 0.748 4.285 2.190 557.653 0.484 9.741 1.781 0.70 266864. 0.0967
|
|
57.64 0.3458 0.3705 0.0065 0.0060 0.678 3.884 1.634 505.443 0.439 7.267 1.466 0.70 267078. 0.0687
|
|
59.86 0.3591 0.2846 0.0043 0.0054 0.605 3.465 1.079 451.009 0.392 4.798 1.085 0.70 267297. 0.0413
|
|
62.07 0.3724 0.1644 0.0021 0.0047 0.529 3.030 0.525 394.352 0.342 2.336 0.604 0.70 267519. 0.0161
|
|
64.29 0.3858
|
|
|
|
|
|
|
|
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 0.0546 0.0136 1.989 10.446 16.429 1483.128 1.180 73.077 5.024 0.76 287283. 0.7468
|
|
2.42 0.0133 0.0522 0.0533 0.0136 1.986 10.429 16.042 1480.646 1.178 71.355 4.914 0.76 287376. 0.7218
|
|
4.85 0.0267 0.1021 0.0520 0.0136 1.980 10.401 15.640 1476.645 1.175 69.565 4.804 0.76 287472. 0.6967
|
|
7.27 0.0400 0.1496 0.0506 0.0135 1.973 10.361 15.223 1471.006 1.171 67.712 4.694 0.76 287573. 0.6716
|
|
9.69 0.0533 0.1948 0.0492 0.0135 1.963 10.309 14.792 1463.620 1.165 65.794 4.584 0.76 287679. 0.6465
|
|
12.12 0.0666 0.2376 0.0477 0.0134 1.950 10.244 14.346 1454.363 1.157 63.810 4.474 0.76 287789. 0.6214
|
|
14.54 0.0800 0.2781 0.0462 0.0133 1.935 10.165 13.885 1443.106 1.148 61.759 4.364 0.76 287903. 0.5963
|
|
16.96 0.0933 0.3163 0.0446 0.0131 1.917 10.070 13.408 1429.719 1.138 59.641 4.254 0.76 288023. 0.5712
|
|
19.39 0.1066 0.3521 0.0429 0.0130 1.896 9.960 12.917 1414.065 1.125 57.454 4.143 0.76 288147. 0.5461
|
|
21.81 0.1199 0.3855 0.0413 0.0128 1.872 9.833 12.410 1396.003 1.111 55.198 4.032 0.76 288276. 0.5209
|
|
24.23 0.1333 0.4164 0.0395 0.0127 1.844 9.688 11.887 1375.438 1.095 52.873 3.920 0.76 288411. 0.4956
|
|
26.65 0.1466 0.4448 0.0377 0.0124 1.813 9.525 11.350 1352.299 1.076 50.484 3.807 0.76 288551. 0.4703
|
|
29.08 0.1599 0.4707 0.0359 0.0122 1.779 9.343 10.798 1326.515 1.056 48.031 3.692 0.76 288696. 0.4449
|
|
31.50 0.1733 0.4938 0.0340 0.0119 1.741 9.143 10.233 1298.007 1.033 45.516 3.576 0.76 288847. 0.4195
|
|
33.92 0.1866 0.5141 0.0321 0.0116 1.699 8.922 9.654 1266.700 1.008 42.942 3.457 0.76 289004. 0.3939
|
|
36.35 0.1999 0.5314 0.0301 0.0113 1.653 8.681 9.063 1232.521 0.981 40.311 3.335 0.76 289166. 0.3682
|
|
38.77 0.2132 0.5455 0.0281 0.0110 1.603 8.420 8.459 1195.407 0.951 37.624 3.209 0.76 289334. 0.3423
|
|
41.19 0.2266 0.5560 0.0261 0.0106 1.549 8.137 7.843 1155.298 0.919 34.885 3.079 0.76 289509. 0.3162
|
|
43.62 0.2399 0.5627 0.0240 0.0102 1.491 7.833 7.216 1112.152 0.885 32.095 2.943 0.76 289689. 0.2899
|
|
46.04 0.2532 0.5650 0.0219 0.0098 1.429 7.508 6.578 1065.936 0.848 29.260 2.799 0.76 289876. 0.2633
|
|
48.46 0.2665 0.5622 0.0197 0.0094 1.363 7.161 5.931 1016.641 0.809 26.382 2.646 0.76 290069. 0.2363
|
|
50.89 0.2799 0.5536 0.0175 0.0089 1.293 6.792 5.275 964.274 0.767 23.465 2.481 0.76 290269. 0.2090
|
|
53.31 0.2932 0.5379 0.0153 0.0084 1.219 6.402 4.612 908.869 0.723 20.516 2.302 0.76 290475. 0.1813
|
|
55.73 0.3065 0.5138 0.0131 0.0078 1.141 5.990 3.943 850.491 0.677 17.540 2.103 0.77 290689. 0.1531
|
|
58.16 0.3199 0.4791 0.0109 0.0073 1.058 5.559 3.270 789.235 0.628 14.544 1.879 0.77 290909. 0.1246
|
|
60.58 0.3332 0.4307 0.0086 0.0067 0.973 5.108 2.593 725.240 0.577 11.536 1.622 0.77 291135. 0.0958
|
|
63.00 0.3465 0.3645 0.0064 0.0061 0.883 4.639 1.917 658.675 0.524 8.525 1.320 0.77 291369. 0.0670
|
|
65.42 0.3598 0.2738 0.0041 0.0054 0.791 4.154 1.241 589.721 0.469 5.520 0.955 0.77 291609. 0.0390
|
|
67.85 0.3732 0.1476 0.0019 0.0048 0.695 3.651 0.567 518.344 0.412 2.523 0.496 0.77 291851. 0.0137
|
|
70.27 0.3865
|
|
|
|
|
|
|
|
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 0.0559 0.0140 2.598 12.598 19.716 1937.573 1.423 87.695 4.615 0.83 311196. 0.7515
|
|
2.62 0.0133 0.0518 0.0545 0.0140 2.590 12.558 19.251 1931.563 1.419 85.630 4.521 0.83 311297. 0.7274
|
|
5.23 0.0266 0.1014 0.0532 0.0139 2.580 12.510 18.769 1924.151 1.413 83.484 4.424 0.83 311403. 0.7029
|
|
7.85 0.0398 0.1488 0.0518 0.0139 2.568 12.450 18.269 1914.918 1.407 81.262 4.327 0.83 311513. 0.6783
|
|
10.46 0.0531 0.1940 0.0503 0.0138 2.553 12.378 17.753 1903.754 1.398 78.963 4.230 0.83 311628. 0.6535
|
|
13.08 0.0664 0.2368 0.0488 0.0137 2.535 12.291 17.218 1890.480 1.389 76.586 4.131 0.83 311749. 0.6286
|
|
15.69 0.0797 0.2773 0.0472 0.0136 2.514 12.190 16.666 1874.945 1.377 74.130 4.032 0.83 311874. 0.6036
|
|
18.31 0.0929 0.3155 0.0456 0.0134 2.490 12.075 16.096 1857.123 1.364 71.594 3.931 0.83 312004. 0.5784
|
|
20.92 0.1062 0.3512 0.0439 0.0133 2.463 11.942 15.507 1836.737 1.349 68.976 3.829 0.83 312139. 0.5530
|
|
23.54 0.1195 0.3845 0.0422 0.0131 2.432 11.791 14.900 1813.526 1.332 66.276 3.727 0.83 312280. 0.5275
|
|
26.15 0.1328 0.4153 0.0404 0.0129 2.397 11.621 14.275 1787.340 1.313 63.494 3.622 0.83 312426. 0.5019
|
|
28.77 0.1460 0.4435 0.0386 0.0127 2.358 11.431 13.632 1758.126 1.291 60.635 3.517 0.83 312578. 0.4762
|
|
31.38 0.1593 0.4690 0.0368 0.0125 2.314 11.221 12.972 1725.918 1.268 57.701 3.409 0.83 312736. 0.4503
|
|
34.00 0.1726 0.4917 0.0348 0.0122 2.267 10.992 12.296 1690.624 1.242 54.693 3.299 0.83 312900. 0.4242
|
|
36.61 0.1859 0.5113 0.0329 0.0120 2.216 10.742 11.604 1652.171 1.214 51.615 3.186 0.83 313069. 0.3980
|
|
39.23 0.1991 0.5277 0.0309 0.0117 2.160 10.471 10.897 1610.528 1.183 48.468 3.069 0.83 313245. 0.3715
|
|
41.84 0.2124 0.5407 0.0288 0.0113 2.100 10.180 10.174 1565.675 1.150 45.255 2.947 0.83 313427. 0.3448
|
|
44.46 0.2257 0.5497 0.0267 0.0110 2.035 9.867 9.438 1517.610 1.115 41.980 2.821 0.83 313616. 0.3178
|
|
47.07 0.2390 0.5546 0.0246 0.0106 1.966 9.534 8.688 1466.384 1.077 38.644 2.687 0.83 313811. 0.2905
|
|
49.69 0.2523 0.5546 0.0225 0.0102 1.894 9.181 7.926 1412.014 1.037 35.253 2.546 0.83 314013. 0.2628
|
|
52.30 0.2655 0.5491 0.0203 0.0098 1.816 8.807 7.152 1354.547 0.995 31.811 2.395 0.83 314222. 0.2349
|
|
54.92 0.2788 0.5373 0.0180 0.0094 1.735 8.414 6.368 1294.078 0.951 28.323 2.232 0.83 314438. 0.2065
|
|
57.53 0.2921 0.5181 0.0158 0.0089 1.650 8.002 5.574 1230.732 0.904 24.795 2.054 0.83 314660. 0.1779
|
|
60.15 0.3054 0.4902 0.0135 0.0084 1.562 7.572 4.774 1164.675 0.856 21.233 1.859 0.83 314890. 0.1490
|
|
62.76 0.3186 0.4517 0.0112 0.0079 1.470 7.127 3.967 1096.101 0.805 17.647 1.642 0.83 315128. 0.1199
|
|
65.38 0.3319 0.4004 0.0089 0.0074 1.375 6.666 3.158 1025.252 0.753 14.045 1.397 0.83 315372. 0.0910
|
|
67.99 0.3452 0.3331 0.0066 0.0069 1.277 6.192 2.347 952.402 0.700 10.437 1.118 0.83 315624. 0.0628
|
|
70.61 0.3585 0.2458 0.0044 0.0063 1.177 5.707 1.537 877.814 0.645 6.836 0.794 0.83 315882. 0.0361
|
|
73.22 0.3717 0.1325 0.0021 0.0058 1.075 5.210 0.729 801.393 0.589 3.243 0.413 0.83 316144. 0.0129
|
|
75.84 0.3850
|
|
|
|
|
|
|
|
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 0.0574 0.0151 3.501 15.762 23.479 2610.734 1.781 104.435 4.079 0.89 335096. 0.7248
|
|
2.90 0.0137 0.0509 0.0560 0.0150 3.474 15.642 22.912 2590.851 1.767 101.912 4.011 0.89 335210. 0.7041
|
|
5.79 0.0273 0.1001 0.0545 0.0149 3.445 15.509 22.322 2568.912 1.752 99.289 3.941 0.89 335330. 0.6829
|
|
8.69 0.0410 0.1474 0.0530 0.0147 3.413 15.365 21.711 2544.995 1.736 96.571 3.869 0.89 335454. 0.6612
|
|
11.59 0.0546 0.1927 0.0515 0.0146 3.381 15.221 21.078 2521.221 1.720 93.755 3.792 0.89 335584. 0.6384
|
|
14.49 0.0683 0.2358 0.0499 0.0145 3.346 15.064 20.423 2495.122 1.702 90.841 3.713 0.89 335720. 0.6153
|
|
17.38 0.0820 0.2766 0.0482 0.0143 3.310 14.900 19.745 2467.974 1.683 87.827 3.629 0.89 335861. 0.5913
|
|
20.28 0.0956 0.3150 0.0465 0.0141 3.270 14.720 19.045 2438.212 1.663 84.712 3.543 0.89 336008. 0.5670
|
|
23.18 0.1093 0.3507 0.0448 0.0139 3.229 14.535 18.322 2407.586 1.642 81.495 3.452 0.89 336161. 0.5418
|
|
26.08 0.1229 0.3836 0.0429 0.0138 3.186 14.342 17.575 2375.512 1.620 78.173 3.356 0.89 336320. 0.5159
|
|
28.97 0.1366 0.4130 0.0411 0.0136 3.144 14.152 16.805 2344.146 1.599 74.750 3.252 0.89 336485. 0.4889
|
|
31.87 0.1502 0.4391 0.0391 0.0134 3.099 13.953 16.014 2311.133 1.576 71.230 3.143 0.89 336657. 0.4612
|
|
34.77 0.1639 0.4620 0.0371 0.0132 3.051 13.735 15.201 2274.946 1.552 67.616 3.031 0.89 336836. 0.4334
|
|
37.66 0.1776 0.4813 0.0351 0.0129 2.998 13.498 14.369 2235.836 1.525 63.912 2.915 0.89 337021. 0.4052
|
|
40.56 0.1912 0.4969 0.0330 0.0127 2.942 13.246 13.516 2193.994 1.497 60.121 2.794 0.89 337213. 0.3767
|
|
43.46 0.2049 0.5084 0.0309 0.0124 2.882 12.975 12.645 2149.168 1.466 56.245 2.669 0.89 337412. 0.3480
|
|
46.36 0.2185 0.5157 0.0287 0.0122 2.818 12.687 11.756 2101.462 1.433 52.290 2.537 0.89 337618. 0.3190
|
|
49.25 0.2322 0.5181 0.0265 0.0119 2.750 12.382 10.849 2050.994 1.399 48.258 2.399 0.89 337832. 0.2898
|
|
52.15 0.2459 0.5153 0.0243 0.0116 2.679 12.062 9.927 1997.912 1.363 44.155 2.254 0.89 338053. 0.2604
|
|
55.05 0.2595 0.5066 0.0220 0.0113 2.605 11.728 8.990 1942.519 1.325 39.987 2.099 0.89 338281. 0.2308
|
|
57.95 0.2732 0.4914 0.0196 0.0109 2.528 11.380 8.040 1884.995 1.286 35.760 1.934 0.89 338518. 0.2012
|
|
60.84 0.2868 0.4691 0.0173 0.0106 2.448 11.021 7.077 1825.468 1.245 31.481 1.759 0.89 338762. 0.1716
|
|
63.74 0.3005 0.4386 0.0149 0.0102 2.366 10.651 6.106 1764.220 1.203 27.158 1.570 0.89 339014. 0.1422
|
|
66.64 0.3142 0.3992 0.0125 0.0099 2.282 10.273 5.126 1701.559 1.161 22.803 1.367 0.89 339275. 0.1135
|
|
69.54 0.3278 0.3497 0.0101 0.0095 2.196 9.888 4.143 1637.835 1.117 18.426 1.147 0.89 339544. 0.0856
|
|
72.43 0.3415 0.2890 0.0077 0.0091 2.110 9.499 3.157 1573.388 1.073 14.041 0.910 0.89 339821. 0.0593
|
|
75.33 0.3551 0.2157 0.0053 0.0087 2.023 9.107 2.172 1508.481 1.029 9.663 0.653 0.89 340106. 0.0353
|
|
78.23 0.3688 0.1284 0.0029 0.0084 1.935 8.711 1.191 1442.868 0.984 5.299 0.374 0.89 340397. 0.0150
|
|
81.12 0.3824 0.0233 0.0005 0.0079 1.838 8.274 0.198 1370.464 0.935 0.882 0.066 0.90 340678. 0.0011
|
|
84.02 0.3961
|
|
|
|
|
|
|
|
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 0.0589 0.0179 5.085 21.367 27.682 3791.990 2.414 123.130 3.311 0.95 358987. 0.6389
|
|
3.17 0.0139 0.0455 0.0575 0.0176 5.016 21.076 27.013 3740.296 2.381 120.156 3.276 0.95 359114. 0.6244
|
|
6.34 0.0279 0.0900 0.0560 0.0174 4.943 20.769 26.317 3685.889 2.347 117.058 3.238 0.95 359246. 0.6093
|
|
9.51 0.0418 0.1334 0.0545 0.0171 4.866 20.447 25.594 3628.757 2.310 113.841 3.199 0.95 359384. 0.5935
|
|
12.68 0.0558 0.1755 0.0529 0.0168 4.786 20.109 24.843 3568.747 2.272 110.502 3.157 0.95 359529. 0.5771
|
|
15.85 0.0697 0.2162 0.0512 0.0165 4.704 19.765 24.065 3507.624 2.233 107.042 3.112 0.95 359679. 0.5598
|
|
19.02 0.0837 0.2550 0.0495 0.0162 4.626 19.439 23.259 3449.750 2.196 103.457 3.058 0.95 359836. 0.5409
|
|
22.19 0.0976 0.2919 0.0477 0.0160 4.545 19.097 22.425 3389.170 2.158 99.747 3.001 0.95 360000. 0.5212
|
|
25.36 0.1116 0.3264 0.0459 0.0157 4.466 18.767 21.562 3330.622 2.120 95.910 2.936 0.95 360170. 0.5000
|
|
28.53 0.1255 0.3587 0.0440 0.0154 4.384 18.421 20.671 3269.135 2.081 91.945 2.868 0.95 360347. 0.4782
|
|
31.70 0.1395 0.3874 0.0420 0.0151 4.310 18.109 19.752 3213.819 2.046 87.855 2.788 0.95 360531. 0.4543
|
|
34.87 0.1534 0.4110 0.0400 0.0149 4.254 17.874 18.804 3172.004 2.019 83.642 2.689 0.95 360722. 0.4276
|
|
38.04 0.1674 0.4286 0.0379 0.0148 4.219 17.728 17.830 3146.188 2.003 79.310 2.571 0.95 360921. 0.3981
|
|
41.21 0.1813 0.4423 0.0358 0.0147 4.182 17.571 16.832 3118.292 1.985 74.870 2.448 0.95 361127. 0.3684
|
|
44.38 0.1953 0.4517 0.0336 0.0145 4.142 17.403 15.811 3088.536 1.966 70.326 2.322 0.95 361340. 0.3386
|
|
47.55 0.2092 0.4566 0.0314 0.0144 4.101 17.231 14.767 3057.904 1.947 65.684 2.190 0.95 361562. 0.3087
|
|
50.72 0.2232 0.4566 0.0292 0.0143 4.059 17.053 13.703 3026.436 1.927 60.949 2.054 0.95 361791. 0.2788
|
|
53.89 0.2371 0.4516 0.0269 0.0141 4.015 16.870 12.618 2993.800 1.906 56.127 1.912 0.95 362029. 0.2490
|
|
57.06 0.2510 0.4414 0.0245 0.0139 3.970 16.680 11.517 2960.239 1.885 51.226 1.765 0.96 362275. 0.2196
|
|
60.23 0.2650 0.4256 0.0221 0.0138 3.924 16.488 10.399 2926.001 1.863 46.255 1.612 0.96 362529. 0.1906
|
|
63.40 0.2789 0.4041 0.0197 0.0136 3.877 16.292 9.268 2891.328 1.841 41.224 1.454 0.96 362792. 0.1623
|
|
66.57 0.2929 0.3765 0.0173 0.0135 3.831 16.096 8.126 2856.519 1.819 36.143 1.290 0.96 363064. 0.1349
|
|
69.74 0.3068 0.3427 0.0148 0.0133 3.784 15.902 6.975 2822.044 1.797 31.027 1.121 0.96 363345. 0.1086
|
|
72.91 0.3208 0.3027 0.0124 0.0131 3.738 15.708 5.821 2787.666 1.775 25.890 0.947 0.96 363635. 0.0838
|
|
76.07 0.3347 0.2563 0.0099 0.0130 3.692 15.515 4.665 2753.490 1.753 20.749 0.768 0.96 363934. 0.0609
|
|
79.24 0.3487 0.2035 0.0075 0.0128 3.647 15.324 3.512 2719.461 1.731 15.622 0.586 0.96 364243. 0.0403
|
|
82.41 0.3626 0.1444 0.0050 0.0126 3.601 15.130 2.366 2685.063 1.709 10.524 0.400 0.96 364562. 0.0225
|
|
85.58 0.3766 0.0787 0.0026 0.0125 3.551 14.920 1.224 2647.776 1.686 5.445 0.210 0.96 364892. 0.0085
|
|
88.75 0.3905 0.0014 0.0000 0.0122 3.460 14.540 0.021 2580.362 1.643 0.093 0.004 0.96 365228. 0.0000
|
|
91.92 0.4045
|
|
|
|
|
|
|