501 lines
89 KiB
Plaintext
501 lines
89 KiB
Plaintext
18x10E (18x10E.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 0.0891 0.0348 0.005 0.334 0.298 3.951 0.038 1.326 34.229 0.07 29901. 0.6093
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0.41 0.0241 0.0600 0.0878 0.0352 0.005 0.338 0.294 3.997 0.038 1.307 33.344 0.07 29921. 0.5892
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0.82 0.0482 0.1168 0.0864 0.0356 0.005 0.341 0.289 4.040 0.039 1.286 32.458 0.07 29942. 0.5689
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1.23 0.0723 0.1705 0.0849 0.0360 0.005 0.345 0.284 4.079 0.039 1.263 31.576 0.07 29964. 0.5485
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1.64 0.0963 0.2210 0.0832 0.0363 0.006 0.348 0.278 4.114 0.039 1.239 30.699 0.07 29989. 0.5281
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2.05 0.1204 0.2685 0.0815 0.0365 0.006 0.350 0.273 4.144 0.040 1.212 29.829 0.07 30016. 0.5076
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2.46 0.1445 0.3128 0.0795 0.0367 0.006 0.352 0.266 4.166 0.040 1.184 28.969 0.07 30044. 0.4871
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2.87 0.1686 0.3543 0.0775 0.0369 0.006 0.353 0.259 4.181 0.040 1.153 28.118 0.07 30075. 0.4666
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3.28 0.1927 0.3928 0.0753 0.0369 0.006 0.354 0.252 4.187 0.040 1.120 27.277 0.07 30108. 0.4462
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3.70 0.2168 0.4284 0.0729 0.0369 0.006 0.354 0.244 4.183 0.040 1.085 26.445 0.07 30143. 0.4257
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4.11 0.2409 0.4612 0.0704 0.0368 0.006 0.352 0.235 4.168 0.040 1.047 25.623 0.07 30180. 0.4053
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4.52 0.2650 0.4912 0.0677 0.0365 0.006 0.350 0.226 4.141 0.040 1.007 24.808 0.07 30219. 0.3849
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4.93 0.2890 0.5183 0.0649 0.0362 0.005 0.347 0.217 4.101 0.039 0.965 23.999 0.07 30261. 0.3644
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5.34 0.3131 0.5426 0.0618 0.0357 0.005 0.342 0.207 4.047 0.039 0.920 23.191 0.07 30306. 0.3439
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5.75 0.3372 0.5640 0.0587 0.0351 0.005 0.336 0.196 3.978 0.038 0.873 22.381 0.07 30352. 0.3233
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6.16 0.3613 0.5822 0.0553 0.0343 0.005 0.329 0.185 3.894 0.037 0.824 21.564 0.07 30401. 0.3025
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6.57 0.3854 0.5971 0.0519 0.0335 0.005 0.321 0.173 3.795 0.036 0.772 20.734 0.07 30453. 0.2815
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6.98 0.4095 0.6084 0.0482 0.0325 0.005 0.311 0.161 3.680 0.035 0.718 19.883 0.07 30507. 0.2603
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7.39 0.4336 0.6157 0.0445 0.0313 0.005 0.300 0.149 3.551 0.034 0.662 19.004 0.07 30563. 0.2390
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7.80 0.4576 0.6185 0.0406 0.0301 0.005 0.288 0.136 3.408 0.033 0.605 18.085 0.07 30622. 0.2173
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8.21 0.4817 0.6161 0.0367 0.0287 0.004 0.275 0.123 3.252 0.031 0.546 17.115 0.07 30683. 0.1954
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8.62 0.5058 0.6077 0.0327 0.0272 0.004 0.261 0.109 3.083 0.029 0.486 16.076 0.07 30747. 0.1732
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9.03 0.5299 0.5919 0.0286 0.0256 0.004 0.245 0.096 2.902 0.028 0.425 14.949 0.07 30813. 0.1507
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9.44 0.5540 0.5674 0.0245 0.0239 0.004 0.229 0.082 2.709 0.026 0.364 13.705 0.07 30881. 0.1278
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9.85 0.5781 0.5317 0.0203 0.0221 0.003 0.212 0.068 2.505 0.024 0.302 12.308 0.07 30953. 0.1046
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10.26 0.6022 0.4817 0.0162 0.0202 0.003 0.194 0.054 2.291 0.022 0.240 10.704 0.07 31026. 0.0811
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10.67 0.6263 0.4126 0.0120 0.0182 0.003 0.175 0.040 2.068 0.020 0.179 8.817 0.07 31102. 0.0576
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11.09 0.6503 0.3173 0.0079 0.0162 0.002 0.155 0.026 1.837 0.018 0.118 6.530 0.07 31181. 0.0346
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11.50 0.6744 0.1843 0.0039 0.0141 0.002 0.135 0.013 1.600 0.015 0.057 3.658 0.07 31262. 0.0135
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11.91 0.6985 -0.0064 -0.0001 0.0120 0.002 0.115 0.000 1.357 0.013 -0.002 -0.122 0.07 31344. 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 0.0895 0.0321 0.039 1.232 1.197 29.162 0.139 5.325 18.619 0.14 59802. 0.6641
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0.82 0.0242 0.0654 0.0882 0.0326 0.040 1.249 1.180 29.562 0.141 5.247 18.100 0.14 59841. 0.6409
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1.65 0.0484 0.1271 0.0867 0.0330 0.040 1.265 1.161 29.942 0.143 5.163 17.584 0.14 59883. 0.6176
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2.47 0.0725 0.1851 0.0852 0.0334 0.041 1.280 1.140 30.294 0.145 5.072 17.074 0.14 59929. 0.5943
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3.30 0.0967 0.2395 0.0836 0.0337 0.041 1.294 1.118 30.610 0.146 4.974 16.569 0.14 59978. 0.5712
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4.12 0.1209 0.2904 0.0818 0.0340 0.041 1.305 1.094 30.882 0.147 4.868 16.073 0.14 60032. 0.5481
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4.95 0.1451 0.3379 0.0799 0.0343 0.042 1.314 1.069 31.099 0.148 4.753 15.585 0.14 60089. 0.5252
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5.77 0.1693 0.3821 0.0778 0.0345 0.042 1.321 1.041 31.253 0.149 4.630 15.106 0.14 60151. 0.5024
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6.59 0.1934 0.4232 0.0756 0.0345 0.042 1.324 1.011 31.334 0.150 4.498 14.637 0.14 60217. 0.4798
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7.42 0.2176 0.4611 0.0732 0.0345 0.042 1.324 0.979 31.333 0.150 4.356 14.177 0.14 60287. 0.4574
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8.24 0.2418 0.4960 0.0707 0.0344 0.042 1.320 0.945 31.240 0.149 4.205 13.727 0.14 60362. 0.4351
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9.07 0.2660 0.5281 0.0680 0.0342 0.042 1.312 0.909 31.047 0.148 4.045 13.284 0.14 60442. 0.4129
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9.89 0.2902 0.5572 0.0651 0.0339 0.041 1.299 0.871 30.745 0.147 3.874 12.849 0.14 60526. 0.3909
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10.72 0.3143 0.5835 0.0621 0.0334 0.041 1.282 0.830 30.329 0.145 3.694 12.420 0.14 60616. 0.3690
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11.54 0.3385 0.6068 0.0589 0.0328 0.040 1.259 0.788 29.789 0.142 3.504 11.994 0.14 60709. 0.3470
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12.36 0.3627 0.6272 0.0555 0.0321 0.039 1.231 0.743 29.120 0.139 3.304 11.570 0.14 60808. 0.3251
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13.19 0.3869 0.6444 0.0520 0.0312 0.038 1.197 0.696 28.317 0.135 3.095 11.144 0.14 60912. 0.3030
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14.01 0.4111 0.6582 0.0483 0.0302 0.037 1.157 0.647 27.386 0.131 2.877 10.714 0.14 61020. 0.2809
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14.84 0.4352 0.6683 0.0446 0.0290 0.035 1.113 0.596 26.331 0.126 2.653 10.274 0.14 61134. 0.2587
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15.66 0.4594 0.6743 0.0407 0.0277 0.034 1.063 0.545 25.156 0.120 2.423 9.820 0.14 61252. 0.2362
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16.49 0.4836 0.6754 0.0367 0.0263 0.032 1.008 0.492 23.863 0.114 2.187 9.345 0.14 61376. 0.2136
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17.31 0.5078 0.6709 0.0327 0.0248 0.030 0.949 0.438 22.458 0.107 1.947 8.840 0.14 61504. 0.1907
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18.13 0.5320 0.6594 0.0286 0.0231 0.028 0.885 0.383 20.944 0.100 1.704 8.294 0.14 61637. 0.1673
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18.96 0.5561 0.6393 0.0245 0.0213 0.026 0.817 0.328 19.327 0.092 1.458 7.692 0.15 61775. 0.1435
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19.78 0.5803 0.6080 0.0203 0.0194 0.024 0.744 0.272 17.613 0.084 1.211 7.010 0.15 61918. 0.1192
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20.61 0.6045 0.5614 0.0162 0.0174 0.021 0.668 0.217 15.808 0.075 0.963 6.214 0.15 62067. 0.0943
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21.43 0.6287 0.4934 0.0120 0.0153 0.019 0.588 0.161 13.924 0.066 0.717 5.251 0.15 62220. 0.0687
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22.26 0.6529 0.3934 0.0080 0.0132 0.016 0.506 0.106 11.970 0.057 0.473 4.031 0.15 62378. 0.0429
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23.08 0.6770 0.2418 0.0039 0.0110 0.013 0.421 0.052 9.959 0.048 0.233 2.390 0.15 62541. 0.0178
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23.91 0.7012 -0.0016 0.0000 0.0087 0.011 0.334 0.000 7.904 0.038 -0.001 -0.015 0.15 62707. 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 0.0898 0.0310 0.127 2.678 2.704 95.040 0.303 12.026 12.903 0.21 89701. 0.6916
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1.24 0.0242 0.0681 0.0885 0.0315 0.129 2.717 2.665 96.448 0.307 11.852 12.531 0.21 89760. 0.6668
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2.48 0.0485 0.1321 0.0871 0.0319 0.131 2.755 2.622 97.789 0.311 11.663 12.162 0.21 89823. 0.6420
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3.72 0.0727 0.1923 0.0856 0.0323 0.133 2.790 2.576 99.037 0.315 11.458 11.798 0.21 89892. 0.6173
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4.96 0.0969 0.2486 0.0839 0.0327 0.134 2.822 2.526 100.162 0.319 11.237 11.440 0.21 89966. 0.5927
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6.20 0.1212 0.3012 0.0821 0.0330 0.136 2.849 2.472 101.135 0.322 10.997 11.088 0.21 90047. 0.5683
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7.44 0.1454 0.3502 0.0802 0.0333 0.137 2.872 2.414 101.924 0.324 10.739 10.744 0.21 90133. 0.5442
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8.67 0.1696 0.3958 0.0781 0.0335 0.137 2.888 2.352 102.497 0.326 10.461 10.407 0.21 90226. 0.5202
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9.91 0.1939 0.4380 0.0759 0.0336 0.138 2.897 2.285 102.819 0.327 10.162 10.078 0.21 90326. 0.4966
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11.15 0.2181 0.4771 0.0735 0.0336 0.138 2.898 2.213 102.858 0.327 9.842 9.757 0.21 90432. 0.4731
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12.39 0.2423 0.5131 0.0709 0.0335 0.138 2.890 2.136 102.581 0.327 9.501 9.444 0.21 90545. 0.4499
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13.63 0.2666 0.5461 0.0682 0.0333 0.137 2.873 2.054 101.959 0.325 9.137 9.138 0.21 90665. 0.4270
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14.87 0.2908 0.5762 0.0653 0.0330 0.135 2.845 1.968 100.963 0.321 8.751 8.839 0.22 90792. 0.4042
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16.11 0.3150 0.6035 0.0623 0.0325 0.134 2.805 1.876 99.567 0.317 8.344 8.545 0.22 90927. 0.3815
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17.35 0.3393 0.6279 0.0591 0.0319 0.131 2.754 1.779 97.746 0.311 7.913 8.255 0.22 91068. 0.3589
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18.59 0.3635 0.6494 0.0557 0.0312 0.128 2.690 1.677 95.471 0.304 7.461 7.969 0.22 91217. 0.3364
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19.83 0.3877 0.6678 0.0522 0.0303 0.124 2.613 1.571 92.736 0.295 6.987 7.683 0.22 91373. 0.3139
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21.07 0.4120 0.6830 0.0485 0.0293 0.120 2.523 1.460 89.551 0.285 6.495 7.396 0.22 91537. 0.2913
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22.31 0.4362 0.6947 0.0447 0.0281 0.115 2.421 1.346 85.931 0.274 5.987 7.104 0.22 91707. 0.2687
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23.54 0.4604 0.7025 0.0408 0.0267 0.110 2.307 1.229 81.887 0.261 5.465 6.806 0.22 91886. 0.2459
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24.78 0.4847 0.7057 0.0368 0.0253 0.104 2.182 1.109 77.432 0.246 4.932 6.495 0.22 92072. 0.2229
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26.02 0.5089 0.7035 0.0328 0.0237 0.097 2.045 0.987 72.579 0.231 4.389 6.167 0.22 92265. 0.1997
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27.26 0.5331 0.6948 0.0287 0.0220 0.090 1.897 0.863 67.342 0.214 3.839 5.813 0.22 92465. 0.1760
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28.50 0.5574 0.6776 0.0245 0.0202 0.083 1.739 0.738 61.740 0.197 3.284 5.423 0.22 92674. 0.1519
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29.74 0.5816 0.6494 0.0203 0.0182 0.075 1.572 0.613 55.794 0.178 2.725 4.981 0.22 92889. 0.1271
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30.98 0.6058 0.6059 0.0162 0.0162 0.066 1.395 0.487 49.531 0.158 2.167 4.461 0.22 93112. 0.1015
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32.22 0.6301 0.5399 0.0120 0.0140 0.058 1.211 0.362 42.982 0.137 1.611 3.822 0.22 93343. 0.0750
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33.46 0.6543 0.4387 0.0079 0.0118 0.049 1.020 0.239 36.190 0.115 1.061 2.991 0.22 93581. 0.0476
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34.70 0.6785 0.2769 0.0039 0.0095 0.039 0.823 0.117 29.200 0.093 0.521 1.820 0.22 93827. 0.0203
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35.94 0.7028 -0.0051 -0.0001 0.0072 0.030 0.621 -0.002 22.048 0.070 -0.007 -0.033 0.22 94076. 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 0.0902 0.0305 0.297 4.675 4.829 221.262 0.528 21.480 9.899 0.29 119598. 0.7092
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1.65 0.0242 0.0696 0.0889 0.0310 0.301 4.748 4.760 224.690 0.536 21.172 9.608 0.29 119676. 0.6834
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3.31 0.0485 0.1351 0.0875 0.0314 0.306 4.817 4.685 227.962 0.544 20.837 9.321 0.29 119761. 0.6576
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4.96 0.0727 0.1964 0.0860 0.0318 0.310 4.881 4.603 231.010 0.551 20.473 9.037 0.29 119853. 0.6320
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6.61 0.0970 0.2538 0.0843 0.0322 0.313 4.940 4.514 233.768 0.558 20.079 8.759 0.29 119952. 0.6066
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8.26 0.1212 0.3074 0.0825 0.0325 0.317 4.990 4.418 236.162 0.564 19.653 8.486 0.29 120060. 0.5815
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9.92 0.1454 0.3573 0.0806 0.0328 0.319 5.032 4.315 238.117 0.568 19.193 8.219 0.29 120175. 0.5566
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11.57 0.1697 0.4037 0.0785 0.0330 0.321 5.062 4.204 239.553 0.572 18.698 7.959 0.29 120299. 0.5320
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13.22 0.1939 0.4466 0.0763 0.0331 0.322 5.080 4.084 240.390 0.574 18.166 7.706 0.29 120432. 0.5077
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14.87 0.2181 0.4864 0.0739 0.0331 0.323 5.083 3.956 240.546 0.574 17.596 7.459 0.29 120574. 0.4836
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16.53 0.2424 0.5230 0.0713 0.0331 0.322 5.070 3.819 239.944 0.573 16.987 7.219 0.29 120725. 0.4599
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18.18 0.2666 0.5567 0.0686 0.0329 0.320 5.040 3.673 238.511 0.569 16.339 6.985 0.29 120885. 0.4364
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19.83 0.2909 0.5875 0.0657 0.0325 0.317 4.991 3.519 236.177 0.564 15.651 6.757 0.29 121055. 0.4132
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21.48 0.3151 0.6154 0.0627 0.0321 0.312 4.921 3.355 232.880 0.556 14.923 6.534 0.29 121234. 0.3901
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23.14 0.3393 0.6405 0.0595 0.0315 0.306 4.830 3.182 228.555 0.546 14.154 6.315 0.29 121423. 0.3672
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24.79 0.3636 0.6628 0.0561 0.0307 0.299 4.715 3.000 223.137 0.533 13.346 6.099 0.29 121622. 0.3444
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26.44 0.3878 0.6821 0.0525 0.0298 0.290 4.577 2.810 216.603 0.517 12.500 5.884 0.29 121830. 0.3216
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28.09 0.4120 0.6984 0.0488 0.0288 0.280 4.416 2.612 208.980 0.499 11.620 5.670 0.29 122049. 0.2988
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29.75 0.4363 0.7112 0.0450 0.0276 0.269 4.232 2.408 200.297 0.478 10.713 5.454 0.29 122277. 0.2759
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31.40 0.4605 0.7203 0.0411 0.0263 0.256 4.027 2.199 190.584 0.455 9.780 5.233 0.29 122515. 0.2530
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33.05 0.4848 0.7251 0.0371 0.0248 0.241 3.801 1.985 179.870 0.429 8.828 5.004 0.29 122763. 0.2298
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34.70 0.5090 0.7248 0.0330 0.0232 0.226 3.554 1.767 168.184 0.402 7.858 4.764 0.29 123020. 0.2064
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36.36 0.5332 0.7183 0.0289 0.0214 0.209 3.287 1.546 155.563 0.371 6.875 4.506 0.29 123288. 0.1826
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38.01 0.5575 0.7037 0.0247 0.0196 0.190 3.002 1.322 142.048 0.339 5.882 4.223 0.29 123566. 0.1583
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39.66 0.5817 0.6783 0.0205 0.0176 0.171 2.698 1.098 127.692 0.305 4.885 3.901 0.29 123854. 0.1333
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41.32 0.6060 0.6379 0.0163 0.0155 0.151 2.378 0.874 112.561 0.269 3.888 3.522 0.29 124151. 0.1073
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42.97 0.6302 0.5749 0.0122 0.0133 0.130 2.044 0.651 96.733 0.231 2.895 3.052 0.29 124459. 0.0803
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44.62 0.6544 0.4754 0.0080 0.0111 0.108 1.697 0.430 80.308 0.192 1.914 2.430 0.29 124777. 0.0520
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46.27 0.6787 0.3099 0.0040 0.0087 0.085 1.340 0.214 63.402 0.151 0.950 1.528 0.29 125104. 0.0230
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47.93 0.7029 0.0033 0.0000 0.0064 0.062 0.974 0.002 46.096 0.110 0.007 0.016 0.29 125437. 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 0.0907 0.0302 0.575 7.242 7.590 428.435 0.818 33.759 8.035 0.36 149492. 0.7216
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2.09 0.0245 0.0714 0.0894 0.0307 0.584 7.359 7.480 435.357 0.831 33.273 7.793 0.36 149591. 0.6948
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4.18 0.0490 0.1384 0.0880 0.0312 0.593 7.471 7.361 441.964 0.844 32.743 7.555 0.36 149698. 0.6682
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6.27 0.0736 0.2012 0.0865 0.0316 0.601 7.575 7.232 448.119 0.856 32.168 7.320 0.36 149815. 0.6417
|
|
8.36 0.0981 0.2598 0.0848 0.0320 0.608 7.669 7.092 453.684 0.866 31.544 7.090 0.36 149941. 0.6155
|
|
10.45 0.1226 0.3144 0.0830 0.0323 0.615 7.751 6.940 458.509 0.876 30.868 6.865 0.36 150078. 0.5895
|
|
12.54 0.1471 0.3653 0.0810 0.0326 0.620 7.817 6.775 462.436 0.883 30.137 6.645 0.36 150225. 0.5639
|
|
14.63 0.1716 0.4124 0.0789 0.0328 0.624 7.866 6.598 465.303 0.889 29.349 6.432 0.36 150383. 0.5386
|
|
16.72 0.1961 0.4561 0.0766 0.0329 0.626 7.893 6.408 466.943 0.892 28.501 6.224 0.36 150552. 0.5136
|
|
18.81 0.2207 0.4965 0.0742 0.0330 0.627 7.898 6.203 467.189 0.892 27.591 6.022 0.36 150733. 0.4889
|
|
20.90 0.2452 0.5337 0.0716 0.0329 0.625 7.876 5.984 465.883 0.890 26.618 5.826 0.36 150926. 0.4646
|
|
22.99 0.2697 0.5679 0.0688 0.0327 0.621 7.825 5.751 462.871 0.884 25.581 5.636 0.36 151130. 0.4406
|
|
25.08 0.2942 0.5991 0.0658 0.0323 0.614 7.743 5.504 458.016 0.875 24.480 5.450 0.36 151347. 0.4168
|
|
27.17 0.3187 0.6275 0.0627 0.0318 0.605 7.627 5.241 451.186 0.862 23.314 5.269 0.36 151575. 0.3932
|
|
29.25 0.3433 0.6530 0.0594 0.0312 0.593 7.476 4.965 442.249 0.845 22.083 5.092 0.36 151816. 0.3698
|
|
31.34 0.3678 0.6757 0.0559 0.0304 0.578 7.287 4.673 431.073 0.823 20.787 4.917 0.36 152070. 0.3465
|
|
33.43 0.3923 0.6954 0.0522 0.0295 0.560 7.060 4.368 417.630 0.798 19.431 4.744 0.36 152336. 0.3233
|
|
35.52 0.4168 0.7120 0.0484 0.0284 0.539 6.795 4.052 401.975 0.768 18.023 4.572 0.36 152615. 0.3000
|
|
37.61 0.4413 0.7253 0.0445 0.0271 0.515 6.494 3.725 384.170 0.734 16.570 4.398 0.36 152906. 0.2767
|
|
39.70 0.4658 0.7347 0.0405 0.0257 0.488 6.158 3.390 364.271 0.696 15.079 4.221 0.36 153210. 0.2534
|
|
41.79 0.4904 0.7398 0.0364 0.0242 0.459 5.787 3.048 342.337 0.654 13.556 4.038 0.36 153526. 0.2298
|
|
43.88 0.5149 0.7397 0.0323 0.0225 0.427 5.383 2.699 318.431 0.608 12.007 3.845 0.36 153855. 0.2059
|
|
45.97 0.5394 0.7330 0.0281 0.0206 0.392 4.947 2.347 292.629 0.559 10.438 3.637 0.36 154197. 0.1816
|
|
48.06 0.5639 0.7179 0.0238 0.0187 0.355 4.480 1.991 265.022 0.506 8.855 3.407 0.36 154551. 0.1567
|
|
50.15 0.5884 0.6912 0.0195 0.0166 0.316 3.985 1.634 235.725 0.450 7.267 3.144 0.36 154919. 0.1310
|
|
52.24 0.6130 0.6476 0.0153 0.0145 0.275 3.463 1.277 204.881 0.391 5.681 2.827 0.36 155299. 0.1042
|
|
54.33 0.6375 0.5775 0.0110 0.0122 0.232 2.919 0.923 172.666 0.330 4.106 2.425 0.36 155692. 0.0759
|
|
56.42 0.6620 0.4619 0.0069 0.0098 0.187 2.355 0.574 139.296 0.266 2.551 1.867 0.36 156098. 0.0461
|
|
58.51 0.6865 0.2560 0.0028 0.0074 0.141 1.775 0.231 105.022 0.201 1.028 0.998 0.37 156515. 0.0156
|
|
60.60 0.7110
|
|
|
|
|
|
|
|
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 0.0914 0.0302 0.991 10.406 11.007 738.687 1.176 48.959 6.758 0.43 179382. 0.7309
|
|
2.48 0.0243 0.0713 0.0901 0.0307 1.007 10.576 10.852 750.776 1.195 48.270 6.556 0.43 179499. 0.7040
|
|
4.96 0.0485 0.1383 0.0887 0.0311 1.022 10.739 10.683 762.328 1.213 47.519 6.356 0.43 179627. 0.6772
|
|
7.44 0.0728 0.2010 0.0872 0.0316 1.037 10.891 10.500 773.114 1.230 46.703 6.160 0.43 179766. 0.6507
|
|
9.92 0.0970 0.2596 0.0855 0.0320 1.050 11.029 10.301 782.896 1.246 45.817 5.968 0.43 179916. 0.6243
|
|
12.41 0.1213 0.3143 0.0837 0.0323 1.061 11.149 10.085 791.421 1.260 44.857 5.780 0.43 180078. 0.5983
|
|
14.89 0.1456 0.3652 0.0818 0.0326 1.071 11.247 9.851 798.419 1.271 43.819 5.596 0.43 180252. 0.5726
|
|
17.37 0.1698 0.4125 0.0797 0.0328 1.078 11.321 9.600 803.614 1.279 42.699 5.418 0.43 180439. 0.5472
|
|
19.85 0.1941 0.4564 0.0775 0.0329 1.082 11.364 9.329 806.721 1.284 41.494 5.245 0.43 180639. 0.5222
|
|
22.33 0.2183 0.4970 0.0750 0.0330 1.083 11.375 9.038 807.456 1.285 40.201 5.077 0.43 180853. 0.4975
|
|
24.81 0.2426 0.5345 0.0725 0.0329 1.080 11.348 8.727 805.547 1.282 38.818 4.914 0.43 181081. 0.4732
|
|
27.29 0.2669 0.5690 0.0697 0.0327 1.074 11.280 8.395 800.730 1.274 37.343 4.756 0.43 181322. 0.4492
|
|
29.77 0.2911 0.6006 0.0668 0.0324 1.063 11.168 8.043 792.765 1.262 35.775 4.602 0.43 181578. 0.4254
|
|
32.25 0.3154 0.6295 0.0637 0.0319 1.048 11.008 7.670 781.431 1.244 34.115 4.452 0.43 181848. 0.4019
|
|
34.74 0.3396 0.6556 0.0604 0.0313 1.028 10.798 7.276 766.503 1.220 32.362 4.305 0.43 182133. 0.3786
|
|
37.22 0.3639 0.6790 0.0570 0.0305 1.003 10.534 6.861 747.747 1.190 30.516 4.161 0.43 182432. 0.3553
|
|
39.70 0.3882 0.6996 0.0534 0.0296 0.972 10.214 6.426 725.076 1.154 28.582 4.020 0.43 182746. 0.3322
|
|
42.18 0.4124 0.7172 0.0496 0.0285 0.937 9.841 5.974 698.569 1.112 26.571 3.879 0.43 183075. 0.3090
|
|
44.66 0.4367 0.7317 0.0457 0.0273 0.896 9.415 5.507 668.326 1.064 24.495 3.737 0.43 183418. 0.2859
|
|
47.14 0.4609 0.7428 0.0417 0.0259 0.851 8.938 5.027 634.448 1.010 22.361 3.594 0.43 183776. 0.2627
|
|
49.62 0.4852 0.7498 0.0377 0.0244 0.801 8.410 4.537 597.029 0.950 20.180 3.447 0.43 184149. 0.2393
|
|
52.10 0.5095 0.7521 0.0335 0.0227 0.746 7.835 4.038 556.177 0.885 17.960 3.293 0.43 184536. 0.2157
|
|
54.58 0.5337 0.7486 0.0293 0.0209 0.687 7.213 3.532 512.014 0.815 15.708 3.128 0.43 184939. 0.1916
|
|
57.07 0.5580 0.7376 0.0251 0.0190 0.623 6.546 3.021 464.688 0.740 13.436 2.948 0.44 185357. 0.1670
|
|
59.55 0.5822 0.7164 0.0208 0.0169 0.556 5.837 2.507 414.385 0.660 11.152 2.744 0.44 185789. 0.1417
|
|
62.03 0.6065 0.6805 0.0166 0.0148 0.485 5.090 1.994 361.337 0.575 8.868 2.503 0.44 186237. 0.1152
|
|
64.51 0.6308 0.6220 0.0123 0.0125 0.410 4.308 1.483 305.832 0.487 6.596 2.199 0.44 186699. 0.0873
|
|
66.99 0.6550 0.5248 0.0081 0.0101 0.333 3.497 0.978 248.223 0.395 4.350 1.787 0.44 187177. 0.0576
|
|
69.47 0.6793 0.3524 0.0040 0.0077 0.253 2.661 0.482 188.929 0.301 2.144 1.157 0.44 187669. 0.0262
|
|
71.95 0.7035 -0.0036 0.0000 0.0052 0.172 1.806 -0.003 128.174 0.204 -0.014 -0.011 0.44 188166. 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 0.0922 0.0302 1.578 14.204 15.110 1176.381 1.605 67.208 5.826 0.50 209266. 0.7382
|
|
2.92 0.0244 0.0722 0.0909 0.0308 1.604 14.443 14.899 1196.141 1.632 66.269 5.649 0.50 209404. 0.7108
|
|
5.83 0.0489 0.1400 0.0895 0.0312 1.629 14.671 14.668 1215.026 1.658 65.244 5.476 0.50 209555. 0.6836
|
|
8.75 0.0733 0.2034 0.0879 0.0317 1.653 14.884 14.417 1232.651 1.682 64.126 5.305 0.50 209719. 0.6566
|
|
11.66 0.0978 0.2627 0.0863 0.0321 1.674 15.077 14.144 1248.620 1.703 62.910 5.138 0.50 209896. 0.6299
|
|
14.58 0.1222 0.3180 0.0845 0.0325 1.693 15.244 13.847 1262.515 1.722 61.591 4.975 0.50 210087. 0.6034
|
|
17.50 0.1466 0.3694 0.0825 0.0328 1.708 15.382 13.525 1273.889 1.738 60.161 4.816 0.50 210293. 0.5773
|
|
20.41 0.1711 0.4171 0.0804 0.0330 1.720 15.483 13.178 1282.281 1.749 58.617 4.661 0.50 210515. 0.5516
|
|
23.33 0.1955 0.4614 0.0781 0.0331 1.726 15.543 12.804 1287.218 1.756 56.952 4.512 0.50 210752. 0.5263
|
|
26.24 0.2200 0.5024 0.0757 0.0331 1.728 15.555 12.402 1288.234 1.757 55.163 4.366 0.50 211005. 0.5013
|
|
29.16 0.2444 0.5402 0.0730 0.0330 1.723 15.514 11.971 1284.873 1.753 53.246 4.226 0.50 211274. 0.4766
|
|
32.08 0.2688 0.5751 0.0702 0.0328 1.712 15.416 11.511 1276.702 1.742 51.200 4.089 0.50 211560. 0.4523
|
|
34.99 0.2933 0.6070 0.0672 0.0325 1.694 15.254 11.022 1263.329 1.723 49.024 3.957 0.50 211863. 0.4282
|
|
37.91 0.3177 0.6362 0.0641 0.0320 1.669 15.025 10.503 1244.384 1.698 46.718 3.828 0.50 212182. 0.4044
|
|
40.82 0.3421 0.6627 0.0607 0.0314 1.635 14.725 9.955 1219.503 1.664 44.281 3.703 0.50 212519. 0.3808
|
|
43.74 0.3666 0.6864 0.0572 0.0306 1.594 14.348 9.378 1188.300 1.621 41.712 3.579 0.50 212873. 0.3573
|
|
46.66 0.3910 0.7073 0.0535 0.0296 1.543 13.894 8.773 1150.663 1.570 39.021 3.458 0.50 213245. 0.3339
|
|
49.57 0.4155 0.7253 0.0497 0.0285 1.484 13.363 8.144 1106.727 1.510 36.224 3.338 0.50 213633. 0.3105
|
|
52.49 0.4399 0.7402 0.0457 0.0272 1.417 12.759 7.494 1056.661 1.441 33.335 3.217 0.50 214040. 0.2871
|
|
55.40 0.4643 0.7517 0.0416 0.0257 1.342 12.082 6.827 1000.624 1.365 30.367 3.095 0.51 214463. 0.2636
|
|
58.32 0.4888 0.7591 0.0375 0.0241 1.259 11.335 6.145 938.780 1.281 27.334 2.969 0.51 214904. 0.2399
|
|
61.24 0.5132 0.7618 0.0333 0.0224 1.168 10.521 5.451 871.304 1.189 24.246 2.838 0.51 215363. 0.2160
|
|
64.15 0.5377 0.7585 0.0290 0.0205 1.071 9.640 4.747 798.405 1.089 21.117 2.697 0.51 215839. 0.1916
|
|
67.07 0.5621 0.7475 0.0246 0.0185 0.966 8.698 4.038 720.342 0.983 17.959 2.542 0.51 216333. 0.1665
|
|
69.98 0.5865 0.7258 0.0203 0.0164 0.855 7.697 3.325 637.432 0.870 14.788 2.366 0.51 216845. 0.1406
|
|
72.90 0.6110 0.6884 0.0159 0.0141 0.738 6.642 2.612 550.077 0.750 11.619 2.154 0.51 217374. 0.1135
|
|
75.82 0.6354 0.6257 0.0116 0.0118 0.615 5.540 1.904 458.776 0.626 8.470 1.883 0.51 217922. 0.0847
|
|
78.73 0.6599 0.5181 0.0074 0.0094 0.488 4.397 1.205 364.143 0.497 5.360 1.501 0.51 218486. 0.0537
|
|
81.65 0.6843 0.3162 0.0032 0.0069 0.358 3.223 0.520 266.892 0.364 2.312 0.883 0.51 219068. 0.0208
|
|
84.56 0.7087
|
|
|
|
|
|
|
|
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 0.0931 0.0305 2.372 18.690 19.936 1769.040 2.112 88.674 5.111 0.57 239144. 0.7439
|
|
3.30 0.0242 0.0718 0.0918 0.0310 2.413 19.007 19.665 1799.016 2.147 87.469 4.958 0.57 239301. 0.7167
|
|
6.61 0.0485 0.1393 0.0905 0.0315 2.451 19.310 19.368 1827.689 2.182 86.151 4.807 0.57 239472. 0.6896
|
|
9.91 0.0727 0.2025 0.0890 0.0319 2.487 19.593 19.045 1854.481 2.214 84.712 4.658 0.57 239658. 0.6627
|
|
13.22 0.0969 0.2615 0.0873 0.0324 2.520 19.850 18.693 1878.814 2.243 83.146 4.513 0.57 239859. 0.6360
|
|
16.52 0.1212 0.3166 0.0855 0.0327 2.548 20.075 18.310 1900.052 2.268 81.443 4.371 0.57 240076. 0.6097
|
|
19.83 0.1454 0.3679 0.0836 0.0330 2.571 20.259 17.895 1917.534 2.289 79.597 4.233 0.57 240309. 0.5837
|
|
23.13 0.1696 0.4157 0.0815 0.0333 2.589 20.397 17.446 1930.570 2.304 77.599 4.099 0.57 240560. 0.5581
|
|
26.44 0.1939 0.4600 0.0792 0.0334 2.600 20.480 16.961 1938.464 2.314 75.445 3.969 0.57 240828. 0.5328
|
|
29.74 0.2181 0.5011 0.0768 0.0334 2.602 20.502 16.440 1940.509 2.316 73.127 3.843 0.57 241115. 0.5079
|
|
33.05 0.2423 0.5390 0.0742 0.0333 2.596 20.455 15.882 1936.028 2.311 70.642 3.721 0.57 241419. 0.4834
|
|
36.35 0.2666 0.5741 0.0714 0.0331 2.581 20.332 15.285 1924.377 2.297 67.987 3.603 0.57 241742. 0.4591
|
|
39.66 0.2908 0.6064 0.0684 0.0328 2.555 20.126 14.649 1904.961 2.274 65.160 3.488 0.57 242084. 0.4352
|
|
42.96 0.3150 0.6360 0.0653 0.0323 2.517 19.834 13.975 1877.234 2.241 62.161 3.377 0.57 242446. 0.4115
|
|
46.27 0.3393 0.6629 0.0619 0.0317 2.468 19.447 13.262 1840.663 2.197 58.991 3.268 0.57 242826. 0.3880
|
|
49.57 0.3635 0.6871 0.0584 0.0309 2.407 18.961 12.511 1794.673 2.142 55.648 3.162 0.58 243226. 0.3646
|
|
52.88 0.3878 0.7087 0.0548 0.0300 2.332 18.373 11.722 1739.005 2.076 52.142 3.057 0.58 243645. 0.3412
|
|
56.18 0.4120 0.7276 0.0509 0.0288 2.245 17.685 10.902 1673.831 1.998 48.491 2.954 0.58 244084. 0.3180
|
|
59.48 0.4362 0.7435 0.0470 0.0275 2.145 16.898 10.053 1599.408 1.909 44.717 2.851 0.58 244542. 0.2947
|
|
62.79 0.4605 0.7561 0.0429 0.0261 2.033 16.017 9.181 1515.973 1.810 40.837 2.747 0.58 245019. 0.2713
|
|
66.09 0.4847 0.7650 0.0387 0.0245 1.909 15.043 8.288 1423.768 1.699 36.865 2.640 0.58 245517. 0.2478
|
|
69.40 0.5089 0.7696 0.0345 0.0228 1.774 13.978 7.379 1323.052 1.579 32.820 2.530 0.58 246034. 0.2240
|
|
72.70 0.5332 0.7687 0.0302 0.0209 1.628 12.828 6.456 1214.127 1.449 28.716 2.412 0.58 246570. 0.1998
|
|
76.01 0.5574 0.7608 0.0258 0.0189 1.472 11.594 5.524 1097.363 1.310 24.571 2.283 0.58 247127. 0.1749
|
|
79.31 0.5816 0.7433 0.0214 0.0168 1.305 10.282 4.587 973.216 1.162 20.403 2.138 0.58 247703. 0.1493
|
|
82.62 0.6059 0.7118 0.0170 0.0145 1.129 8.899 3.649 842.261 1.005 16.233 1.965 0.58 248299. 0.1224
|
|
85.92 0.6301 0.6581 0.0127 0.0121 0.946 7.451 2.716 705.215 0.842 12.083 1.747 0.58 248915. 0.0939
|
|
89.23 0.6543 0.5653 0.0084 0.0097 0.755 5.948 1.794 562.961 0.672 7.978 1.445 0.58 249551. 0.0631
|
|
92.53 0.6786 0.3920 0.0041 0.0072 0.559 4.401 0.887 416.551 0.497 3.947 0.966 0.58 250206. 0.0297
|
|
95.84 0.7028 0.0003 0.0000 0.0046 0.357 2.816 0.000 266.505 0.318 0.002 0.001 0.59 250866. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 9000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.0942 0.0308 3.418 23.936 25.533 2548.768 2.704 113.570 4.544 0.64 269013. 0.7484
|
|
3.72 0.0242 0.0718 0.0930 0.0314 3.477 24.349 25.194 2592.663 2.751 112.065 4.408 0.64 269190. 0.7212
|
|
7.43 0.0485 0.1393 0.0916 0.0319 3.533 24.743 24.823 2634.668 2.795 110.413 4.273 0.64 269383. 0.6941
|
|
11.15 0.0727 0.2025 0.0901 0.0323 3.586 25.112 24.417 2673.931 2.837 108.607 4.142 0.64 269593. 0.6671
|
|
14.87 0.0969 0.2615 0.0885 0.0328 3.634 25.447 23.973 2709.597 2.875 106.634 4.013 0.64 269820. 0.6405
|
|
18.58 0.1211 0.3167 0.0867 0.0332 3.675 25.739 23.490 2740.743 2.908 104.485 3.887 0.64 270065. 0.6142
|
|
22.30 0.1454 0.3681 0.0847 0.0335 3.710 25.980 22.965 2766.392 2.935 102.149 3.765 0.64 270328. 0.5882
|
|
26.02 0.1696 0.4159 0.0826 0.0337 3.735 26.160 22.396 2785.541 2.956 99.617 3.647 0.64 270611. 0.5626
|
|
29.73 0.1938 0.4604 0.0804 0.0338 3.751 26.269 21.780 2797.162 2.968 96.879 3.532 0.64 270914. 0.5373
|
|
33.45 0.2180 0.5016 0.0779 0.0339 3.755 26.298 21.117 2800.232 2.971 93.930 3.421 0.64 271237. 0.5124
|
|
37.17 0.2423 0.5398 0.0753 0.0338 3.746 26.237 20.405 2793.753 2.964 90.763 3.313 0.64 271581. 0.4878
|
|
40.88 0.2665 0.5751 0.0725 0.0336 3.724 26.078 19.644 2776.788 2.946 87.375 3.209 0.64 271946. 0.4636
|
|
44.60 0.2907 0.6076 0.0695 0.0333 3.686 25.812 18.831 2748.467 2.916 83.762 3.108 0.65 272332. 0.4396
|
|
48.32 0.3150 0.6375 0.0663 0.0328 3.631 25.432 17.969 2708.003 2.873 79.926 3.010 0.65 272739. 0.4159
|
|
52.03 0.3392 0.6648 0.0629 0.0321 3.560 24.931 17.056 2654.626 2.817 75.867 2.914 0.65 273168. 0.3923
|
|
55.75 0.3634 0.6895 0.0594 0.0313 3.470 24.300 16.093 2587.515 2.745 71.582 2.821 0.65 273618. 0.3689
|
|
59.47 0.3876 0.7116 0.0557 0.0303 3.361 23.537 15.082 2506.261 2.659 67.083 2.729 0.65 274091. 0.3455
|
|
63.18 0.4119 0.7310 0.0518 0.0292 3.233 22.644 14.028 2411.104 2.558 62.396 2.639 0.65 274585. 0.3222
|
|
66.90 0.4361 0.7475 0.0477 0.0279 3.088 21.623 12.938 2302.421 2.443 57.547 2.549 0.65 275101. 0.2988
|
|
70.62 0.4603 0.7609 0.0436 0.0264 2.924 20.479 11.816 2180.564 2.314 52.557 2.458 0.65 275639. 0.2754
|
|
74.33 0.4845 0.7707 0.0394 0.0248 2.744 19.214 10.667 2045.890 2.171 47.448 2.365 0.65 276199. 0.2518
|
|
78.05 0.5088 0.7762 0.0350 0.0230 2.546 17.832 9.497 1898.783 2.015 42.241 2.269 0.65 276781. 0.2279
|
|
81.77 0.5330 0.7765 0.0307 0.0210 2.333 16.338 8.309 1739.687 1.846 36.957 2.166 0.65 277386. 0.2035
|
|
85.48 0.5572 0.7700 0.0262 0.0190 2.104 14.736 7.108 1569.137 1.665 31.617 2.055 0.65 278012. 0.1786
|
|
89.20 0.5814 0.7541 0.0218 0.0168 1.861 13.033 5.901 1387.810 1.473 26.245 1.928 0.65 278660. 0.1527
|
|
92.92 0.6057 0.7245 0.0173 0.0145 1.605 11.237 4.692 1196.545 1.270 20.869 1.779 0.65 279331. 0.1256
|
|
96.63 0.6299 0.6728 0.0129 0.0121 1.336 9.358 3.489 996.395 1.057 15.518 1.588 0.66 280024. 0.0967
|
|
100.35 0.6541 0.5815 0.0085 0.0095 1.058 7.407 2.298 788.660 0.837 10.224 1.322 0.66 280739. 0.0653
|
|
104.07 0.6784 0.4066 0.0042 0.0070 0.771 5.399 1.130 574.900 0.610 5.024 0.891 0.66 281475. 0.0309
|
|
107.78 0.7026 -0.0093 -0.0001 0.0043 0.477 3.341 -0.015 355.756 0.377 -0.069 -0.020 0.66 282214. 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 0.0955 0.0314 4.778 30.115 31.963 3562.921 3.402 142.172 4.069 0.71 298871. 0.7499
|
|
4.13 0.0242 0.0714 0.0943 0.0320 4.859 30.623 31.554 3623.105 3.460 140.351 3.950 0.71 299069. 0.7233
|
|
8.25 0.0484 0.1386 0.0930 0.0325 4.936 31.112 31.103 3680.947 3.515 138.346 3.833 0.71 299284. 0.6968
|
|
12.38 0.0726 0.2017 0.0915 0.0329 5.009 31.571 30.608 3735.247 3.567 136.144 3.717 0.71 299517. 0.6703
|
|
16.50 0.0968 0.2607 0.0899 0.0334 5.075 31.990 30.066 3784.785 3.614 133.732 3.603 0.71 299770. 0.6440
|
|
20.63 0.1210 0.3158 0.0881 0.0338 5.134 32.357 29.473 3828.239 3.656 131.095 3.492 0.71 300043. 0.6180
|
|
24.75 0.1452 0.3672 0.0862 0.0341 5.182 32.661 28.826 3864.187 3.690 128.220 3.384 0.71 300337. 0.5922
|
|
28.88 0.1694 0.4150 0.0841 0.0343 5.218 32.889 28.124 3891.163 3.716 125.095 3.278 0.72 300652. 0.5667
|
|
33.00 0.1936 0.4595 0.0818 0.0345 5.240 33.028 27.363 3907.639 3.732 121.709 3.176 0.72 300990. 0.5416
|
|
37.13 0.2178 0.5009 0.0793 0.0345 5.246 33.066 26.540 3912.099 3.736 118.052 3.077 0.72 301350. 0.5168
|
|
41.26 0.2420 0.5392 0.0767 0.0344 5.234 32.990 25.656 3903.078 3.727 114.116 2.981 0.72 301733. 0.4923
|
|
45.38 0.2662 0.5747 0.0739 0.0342 5.202 32.788 24.707 3879.230 3.704 109.898 2.889 0.72 302139. 0.4681
|
|
49.51 0.2904 0.6075 0.0708 0.0339 5.149 32.451 23.694 3839.330 3.666 105.393 2.799 0.72 302569. 0.4442
|
|
53.63 0.3146 0.6377 0.0676 0.0334 5.072 31.969 22.617 3782.276 3.612 100.602 2.712 0.72 303022. 0.4205
|
|
57.76 0.3388 0.6654 0.0642 0.0327 4.971 31.333 21.476 3707.008 3.540 95.527 2.628 0.72 303500. 0.3970
|
|
61.88 0.3630 0.6905 0.0606 0.0319 4.844 30.533 20.270 3612.393 3.450 90.163 2.545 0.72 304001. 0.3735
|
|
66.01 0.3873 0.7131 0.0568 0.0308 4.691 29.564 19.003 3497.806 3.340 84.525 2.464 0.72 304527. 0.3502
|
|
70.13 0.4115 0.7331 0.0529 0.0297 4.511 28.430 17.681 3363.563 3.212 78.644 2.384 0.72 305077. 0.3268
|
|
74.26 0.4357 0.7503 0.0488 0.0283 4.305 27.133 16.311 3210.200 3.066 72.553 2.305 0.72 305650. 0.3034
|
|
78.39 0.4599 0.7644 0.0445 0.0268 4.074 25.680 14.901 3038.235 2.901 66.280 2.225 0.72 306249. 0.2799
|
|
82.51 0.4841 0.7751 0.0402 0.0251 3.819 24.073 13.456 2848.173 2.720 59.854 2.143 0.72 306871. 0.2562
|
|
86.64 0.5083 0.7817 0.0358 0.0233 3.541 22.319 11.983 2640.582 2.522 53.298 2.058 0.72 307518. 0.2323
|
|
90.76 0.5325 0.7833 0.0313 0.0213 3.240 20.422 10.486 2416.121 2.307 46.641 1.968 0.72 308188. 0.2078
|
|
94.89 0.5567 0.7781 0.0268 0.0192 2.918 18.389 8.973 2175.622 2.078 39.911 1.871 0.73 308884. 0.1827
|
|
99.01 0.5809 0.7639 0.0223 0.0169 2.575 16.229 7.450 1920.125 1.834 33.136 1.760 0.73 309604. 0.1566
|
|
103.14 0.6051 0.7359 0.0177 0.0146 2.214 13.954 5.924 1650.965 1.577 26.352 1.628 0.73 310348. 0.1291
|
|
107.26 0.6293 0.6859 0.0132 0.0121 1.837 11.578 4.405 1369.824 1.308 19.594 1.459 0.73 311117. 0.0998
|
|
111.39 0.6535 0.5957 0.0087 0.0095 1.447 9.118 2.902 1078.815 1.030 12.906 1.220 0.73 311910. 0.0677
|
|
115.52 0.6777 0.4191 0.0043 0.0069 1.047 6.597 1.424 780.478 0.745 6.334 0.828 0.73 312727. 0.0322
|
|
119.64 0.7019 -0.0121 -0.0001 0.0042 0.638 4.023 -0.024 475.964 0.455 -0.108 -0.023 0.73 313546. 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 0.0971 0.0331 6.703 38.406 39.295 4998.292 4.339 174.783 3.566 0.79 328716. 0.7286
|
|
4.56 0.0243 0.0694 0.0959 0.0336 6.795 38.932 38.813 5066.760 4.399 172.639 3.474 0.79 328934. 0.7056
|
|
9.12 0.0486 0.1352 0.0946 0.0340 6.882 39.432 38.279 5131.854 4.455 170.263 3.383 0.79 329173. 0.6823
|
|
13.68 0.0729 0.1974 0.0931 0.0344 6.963 39.895 37.689 5192.111 4.507 167.640 3.292 0.79 329432. 0.6589
|
|
18.24 0.0973 0.2560 0.0915 0.0348 7.035 40.310 37.039 5246.051 4.554 164.749 3.202 0.79 329713. 0.6353
|
|
22.80 0.1216 0.3111 0.0897 0.0351 7.097 40.663 36.325 5292.052 4.594 161.573 3.113 0.79 330017. 0.6117
|
|
27.36 0.1459 0.3628 0.0878 0.0353 7.145 40.943 35.543 5328.395 4.626 158.094 3.026 0.79 330344. 0.5880
|
|
31.91 0.1702 0.4112 0.0857 0.0355 7.179 41.134 34.689 5353.249 4.647 154.296 2.939 0.79 330695. 0.5643
|
|
36.47 0.1945 0.4564 0.0834 0.0355 7.194 41.222 33.760 5364.712 4.657 150.163 2.854 0.79 331071. 0.5406
|
|
41.03 0.2188 0.4985 0.0809 0.0355 7.189 41.192 32.752 5360.841 4.654 145.683 2.771 0.79 331472. 0.5170
|
|
45.59 0.2432 0.5376 0.0782 0.0354 7.161 41.029 31.665 5339.685 4.635 140.847 2.690 0.79 331898. 0.4934
|
|
50.15 0.2675 0.5739 0.0753 0.0351 7.107 40.719 30.496 5299.336 4.600 135.647 2.610 0.79 332351. 0.4699
|
|
54.71 0.2918 0.6074 0.0722 0.0347 7.024 40.248 29.245 5237.986 4.547 130.081 2.532 0.79 332829. 0.4464
|
|
59.27 0.3161 0.6382 0.0690 0.0342 6.912 39.602 27.911 5153.922 4.474 124.149 2.456 0.79 333334. 0.4230
|
|
63.83 0.3404 0.6665 0.0655 0.0334 6.766 38.769 26.495 5045.481 4.380 117.851 2.382 0.79 333866. 0.3997
|
|
68.39 0.3647 0.6922 0.0618 0.0325 6.586 37.734 24.997 4910.873 4.263 111.186 2.309 0.79 334424. 0.3763
|
|
72.95 0.3891 0.7153 0.0579 0.0315 6.369 36.492 23.420 4749.184 4.123 104.170 2.237 0.79 335009. 0.3528
|
|
77.51 0.4134 0.7357 0.0538 0.0302 6.116 35.044 21.773 4560.792 3.959 96.845 2.165 0.79 335621. 0.3294
|
|
82.07 0.4377 0.7534 0.0496 0.0288 5.828 33.396 20.065 4346.267 3.773 89.251 2.094 0.79 336259. 0.3058
|
|
86.62 0.4620 0.7678 0.0452 0.0272 5.507 31.554 18.306 4106.511 3.565 81.425 2.022 0.79 336924. 0.2820
|
|
91.18 0.4863 0.7787 0.0408 0.0255 5.153 29.525 16.502 3842.446 3.336 73.401 1.948 0.79 337616. 0.2579
|
|
95.74 0.5106 0.7851 0.0362 0.0236 4.768 27.318 14.661 3555.209 3.086 65.211 1.870 0.80 338335. 0.2335
|
|
100.30 0.5349 0.7858 0.0316 0.0215 4.353 24.943 12.790 3246.202 2.818 56.891 1.787 0.80 339080. 0.2083
|
|
104.86 0.5593 0.7789 0.0269 0.0193 3.912 22.415 10.898 2917.131 2.532 48.473 1.694 0.80 339852. 0.1823
|
|
109.42 0.5836 0.7613 0.0222 0.0170 3.447 19.748 8.992 2570.109 2.231 39.998 1.587 0.80 340652. 0.1551
|
|
113.98 0.6079 0.7271 0.0175 0.0146 2.961 16.964 7.083 2207.778 1.917 31.507 1.455 0.80 341478. 0.1263
|
|
118.54 0.6322 0.6662 0.0128 0.0121 2.459 14.087 5.182 1833.362 1.592 23.048 1.282 0.80 342332. 0.0951
|
|
123.10 0.6565 0.5567 0.0082 0.0096 1.945 11.147 3.299 1450.671 1.259 14.675 1.032 0.80 343212. 0.0611
|
|
127.66 0.6808 0.3458 0.0036 0.0071 1.427 8.176 1.450 1064.040 0.924 6.448 0.618 0.80 344119. 0.0243
|
|
132.22 0.7052
|
|
|
|
|
|
|
|
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 0.0987 0.0377 9.895 51.971 47.555 7378.482 5.872 211.525 2.923 0.86 358543. 0.6572
|
|
4.94 0.0242 0.0621 0.0976 0.0379 9.970 52.364 47.016 7434.281 5.916 209.126 2.868 0.86 358780. 0.6412
|
|
9.88 0.0483 0.1219 0.0963 0.0382 10.035 52.708 46.414 7483.148 5.955 206.450 2.813 0.86 359039. 0.6248
|
|
14.82 0.0725 0.1792 0.0950 0.0384 10.089 52.991 45.745 7523.381 5.987 203.474 2.758 0.86 359321. 0.6081
|
|
19.76 0.0966 0.2341 0.0934 0.0385 10.129 53.201 45.003 7553.166 6.011 200.174 2.702 0.86 359626. 0.5910
|
|
24.70 0.1208 0.2867 0.0917 0.0386 10.153 53.326 44.183 7570.897 6.025 196.525 2.647 0.86 359956. 0.5735
|
|
29.64 0.1449 0.3368 0.0898 0.0387 10.158 53.353 43.279 7574.755 6.028 192.503 2.591 0.86 360311. 0.5557
|
|
34.58 0.1691 0.3845 0.0878 0.0386 10.142 53.269 42.286 7562.885 6.018 188.088 2.536 0.86 360692. 0.5376
|
|
39.52 0.1932 0.4298 0.0855 0.0384 10.102 53.062 41.201 7533.408 5.995 183.260 2.481 0.86 361100. 0.5190
|
|
44.47 0.2174 0.4727 0.0831 0.0382 10.037 52.717 40.018 7484.478 5.956 178.002 2.425 0.86 361536. 0.5001
|
|
49.41 0.2415 0.5133 0.0804 0.0378 9.943 52.223 38.737 7414.247 5.900 172.301 2.370 0.86 361999. 0.4808
|
|
54.35 0.2657 0.5514 0.0775 0.0374 9.817 51.565 37.354 7320.889 5.826 166.149 2.314 0.86 362490. 0.4611
|
|
59.29 0.2898 0.5871 0.0745 0.0368 9.659 50.732 35.868 7202.624 5.732 159.541 2.259 0.86 363010. 0.4410
|
|
64.23 0.3140 0.6203 0.0712 0.0360 9.465 49.712 34.280 7057.778 5.616 152.477 2.203 0.86 363558. 0.4205
|
|
69.17 0.3382 0.6511 0.0677 0.0351 9.232 48.492 32.590 6884.586 5.479 144.959 2.147 0.86 364134. 0.3996
|
|
74.11 0.3623 0.6793 0.0639 0.0341 8.959 47.058 30.797 6681.013 5.317 136.987 2.091 0.86 364740. 0.3782
|
|
79.05 0.3865 0.7049 0.0600 0.0329 8.644 45.399 28.906 6445.461 5.129 128.573 2.034 0.86 365374. 0.3565
|
|
83.99 0.4106 0.7276 0.0559 0.0315 8.288 43.532 26.925 6180.487 4.918 119.764 1.976 0.86 366036. 0.3342
|
|
88.93 0.4348 0.7466 0.0516 0.0301 7.898 41.485 24.867 5889.763 4.687 110.608 1.915 0.86 366727. 0.3113
|
|
93.87 0.4589 0.7616 0.0472 0.0284 7.474 39.258 22.741 5573.636 4.435 101.151 1.851 0.87 367447. 0.2877
|
|
98.81 0.4831 0.7714 0.0427 0.0267 7.022 36.880 20.556 5235.962 4.167 91.434 1.781 0.87 368195. 0.2632
|
|
103.75 0.5072 0.7755 0.0380 0.0249 6.536 34.332 18.323 4874.266 3.879 81.502 1.705 0.87 368972. 0.2379
|
|
108.69 0.5314 0.7728 0.0333 0.0229 6.020 31.620 16.051 4489.192 3.572 71.396 1.622 0.87 369777. 0.2118
|
|
113.63 0.5555 0.7607 0.0285 0.0208 5.477 28.769 13.750 4084.406 3.250 61.160 1.527 0.87 370611. 0.1846
|
|
118.57 0.5797 0.7356 0.0237 0.0187 4.913 25.806 11.430 3663.837 2.916 50.841 1.415 0.87 371474. 0.1559
|
|
123.51 0.6038 0.6918 0.0189 0.0165 4.334 22.763 9.103 3231.801 2.572 40.490 1.278 0.87 372366. 0.1257
|
|
128.45 0.6280 0.6201 0.0141 0.0143 3.746 19.675 6.782 2793.409 2.223 30.165 1.101 0.87 373286. 0.0935
|
|
133.40 0.6522 0.5049 0.0093 0.0120 3.157 16.583 4.481 2354.343 1.874 19.933 0.863 0.88 374236. 0.0596
|
|
138.34 0.6763 0.3177 0.0046 0.0098 2.575 13.527 2.218 1920.476 1.528 9.868 0.524 0.88 375214. 0.0254
|
|
143.28 0.7005 0.0002 0.0000 0.0076 2.002 10.518 0.001 1493.261 1.188 0.005 0.000 0.88 376204. 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 0.0991 0.0446 14.887 72.177 56.026 11101.222 8.155 249.206 2.289 0.93 388406. 0.5585
|
|
5.40 0.0244 0.0534 0.0981 0.0448 14.977 72.615 55.480 11168.498 8.204 246.775 2.253 0.93 388660. 0.5471
|
|
10.80 0.0487 0.1050 0.0970 0.0450 15.046 72.950 54.860 11220.118 8.242 244.017 2.218 0.93 388938. 0.5355
|
|
16.20 0.0731 0.1551 0.0958 0.0452 15.090 73.162 54.159 11252.682 8.266 240.898 2.183 0.93 389242. 0.5237
|
|
21.60 0.0975 0.2036 0.0944 0.0452 15.104 73.229 53.368 11262.954 8.273 237.380 2.149 0.93 389573. 0.5118
|
|
27.01 0.1219 0.2505 0.0928 0.0452 15.084 73.131 52.479 11247.971 8.262 233.428 2.116 0.93 389931. 0.4997
|
|
32.41 0.1462 0.2961 0.0911 0.0450 15.026 72.852 51.485 11205.052 8.231 229.006 2.084 0.93 390319. 0.4875
|
|
37.81 0.1706 0.3402 0.0891 0.0447 14.928 72.377 50.378 11131.980 8.177 224.083 2.053 0.93 390736. 0.4749
|
|
43.21 0.1950 0.3830 0.0869 0.0443 14.787 71.694 49.152 11026.947 8.100 218.629 2.022 0.93 391184. 0.4621
|
|
48.61 0.2194 0.4243 0.0845 0.0437 14.602 70.794 47.802 10888.552 7.998 212.622 1.991 0.93 391662. 0.4488
|
|
54.01 0.2437 0.4643 0.0819 0.0430 14.370 69.671 46.322 10715.700 7.871 206.042 1.961 0.93 392172. 0.4350
|
|
59.41 0.2681 0.5027 0.0791 0.0422 14.091 68.318 44.712 10507.628 7.718 198.878 1.930 0.93 392713. 0.4207
|
|
64.81 0.2925 0.5395 0.0760 0.0412 13.764 66.732 42.968 10263.762 7.539 191.121 1.899 0.93 393286. 0.4057
|
|
70.21 0.3169 0.5747 0.0727 0.0401 13.388 64.910 41.091 9983.551 7.334 182.774 1.867 0.93 393891. 0.3901
|
|
75.62 0.3412 0.6079 0.0691 0.0388 12.963 62.848 39.082 9666.327 7.101 173.838 1.834 0.93 394527. 0.3737
|
|
81.02 0.3656 0.6392 0.0653 0.0374 12.486 60.537 36.941 9310.853 6.839 164.312 1.800 0.93 395196. 0.3565
|
|
86.42 0.3900 0.6682 0.0613 0.0358 11.957 57.973 34.672 8916.592 6.550 154.219 1.764 0.94 395896. 0.3385
|
|
91.82 0.4144 0.6948 0.0571 0.0341 11.379 55.168 32.289 8485.158 6.233 143.623 1.726 0.94 396628. 0.3197
|
|
97.22 0.4387 0.7175 0.0527 0.0322 10.770 52.216 29.808 8031.138 5.899 132.584 1.683 0.94 397391. 0.2996
|
|
102.62 0.4631 0.7348 0.0482 0.0304 10.144 49.184 27.239 7564.735 5.557 121.158 1.633 0.94 398185. 0.2779
|
|
108.02 0.4875 0.7447 0.0435 0.0285 9.513 46.122 24.594 7093.873 5.211 109.396 1.573 0.94 399011. 0.2542
|
|
113.42 0.5119 0.7406 0.0387 0.0267 8.935 43.321 21.880 6662.992 4.894 97.324 1.489 0.94 399869. 0.2271
|
|
118.83 0.5362 0.7259 0.0338 0.0250 8.345 40.458 19.118 6222.692 4.571 85.038 1.394 0.94 400757. 0.1986
|
|
124.23 0.5606 0.6987 0.0289 0.0232 7.739 37.519 16.323 5770.687 4.239 72.606 1.283 0.94 401677. 0.1690
|
|
129.63 0.5850 0.6554 0.0239 0.0213 7.126 34.550 13.511 5313.910 3.903 60.098 1.153 0.94 402629. 0.1382
|
|
135.03 0.6094 0.5912 0.0189 0.0195 6.517 31.595 10.701 4859.430 3.570 47.596 0.999 0.95 403612. 0.1065
|
|
140.43 0.6337 0.5006 0.0140 0.0177 5.918 28.691 7.911 4412.856 3.242 35.189 0.813 0.95 404627. 0.0746
|
|
145.83 0.6581 0.3764 0.0091 0.0160 5.337 25.878 5.167 3980.172 2.924 22.982 0.589 0.95 405673. 0.0436
|
|
151.23 0.6825 0.2101 0.0044 0.0143 4.782 23.185 2.492 3566.007 2.619 11.083 0.317 0.95 406753. 0.0163
|
|
156.63 0.7069 -0.0121 -0.0002 0.0127 4.232 20.520 -0.123 3156.111 2.318 -0.545 -0.018 0.95 407870. 0.0000
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