501 lines
89 KiB
Plaintext
501 lines
89 KiB
Plaintext
18x12 (18x12.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 0.0864 0.0373 0.006 0.357 0.289 4.226 0.040 1.286 31.023 0.07 25348. 0.5437
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0.50 0.0293 0.0659 0.0857 0.0381 0.006 0.365 0.287 4.321 0.041 1.276 30.108 0.07 25366. 0.5256
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1.00 0.0586 0.1277 0.0850 0.0390 0.006 0.373 0.284 4.418 0.042 1.264 29.187 0.07 25386. 0.5073
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1.50 0.0878 0.1856 0.0841 0.0398 0.006 0.382 0.281 4.514 0.043 1.251 28.266 0.07 25408. 0.4887
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2.00 0.1171 0.2394 0.0831 0.0406 0.006 0.390 0.278 4.609 0.044 1.236 27.350 0.07 25433. 0.4700
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2.50 0.1464 0.2893 0.0819 0.0414 0.006 0.397 0.274 4.700 0.045 1.219 26.444 0.07 25460. 0.4512
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2.99 0.1757 0.3355 0.0805 0.0422 0.006 0.404 0.269 4.783 0.046 1.199 25.552 0.07 25490. 0.4324
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3.49 0.2050 0.3780 0.0790 0.0428 0.007 0.411 0.264 4.857 0.046 1.176 24.677 0.07 25523. 0.4135
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3.99 0.2343 0.4170 0.0772 0.0434 0.007 0.416 0.258 4.919 0.047 1.149 23.823 0.07 25559. 0.3947
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4.49 0.2635 0.4527 0.0752 0.0438 0.007 0.420 0.252 4.965 0.047 1.119 22.989 0.07 25598. 0.3759
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4.99 0.2928 0.4853 0.0730 0.0440 0.007 0.422 0.244 4.993 0.048 1.086 22.177 0.07 25640. 0.3572
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5.49 0.3221 0.5147 0.0705 0.0441 0.007 0.423 0.236 5.000 0.048 1.049 21.385 0.07 25685. 0.3385
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5.99 0.3514 0.5413 0.0677 0.0440 0.007 0.421 0.227 4.984 0.048 1.008 20.614 0.07 25733. 0.3198
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6.49 0.3807 0.5649 0.0647 0.0436 0.007 0.418 0.216 4.945 0.047 0.963 19.859 0.07 25784. 0.3012
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6.99 0.4100 0.5856 0.0615 0.0431 0.007 0.413 0.206 4.882 0.047 0.915 19.117 0.07 25839. 0.2827
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7.49 0.4392 0.6034 0.0581 0.0423 0.006 0.405 0.194 4.796 0.046 0.865 18.383 0.07 25896. 0.2642
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7.99 0.4685 0.6181 0.0545 0.0413 0.006 0.396 0.182 4.688 0.045 0.812 17.653 0.07 25957. 0.2458
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8.49 0.4978 0.6294 0.0508 0.0402 0.006 0.385 0.170 4.557 0.044 0.756 16.921 0.07 26021. 0.2274
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8.98 0.5271 0.6373 0.0470 0.0388 0.006 0.372 0.157 4.404 0.042 0.699 16.180 0.07 26088. 0.2091
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9.48 0.5564 0.6412 0.0430 0.0373 0.006 0.358 0.144 4.230 0.040 0.640 15.422 0.07 26158. 0.1907
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9.98 0.5856 0.6406 0.0389 0.0356 0.005 0.341 0.130 4.035 0.039 0.579 14.638 0.07 26231. 0.1722
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10.48 0.6149 0.6347 0.0348 0.0337 0.005 0.323 0.116 3.820 0.036 0.517 13.813 0.07 26307. 0.1536
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10.98 0.6442 0.6225 0.0305 0.0316 0.005 0.303 0.102 3.584 0.034 0.454 12.931 0.07 26386. 0.1347
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11.48 0.6735 0.6023 0.0262 0.0293 0.004 0.281 0.088 3.328 0.032 0.391 11.968 0.07 26468. 0.1156
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11.98 0.7028 0.5718 0.0219 0.0269 0.004 0.258 0.073 3.052 0.029 0.326 10.889 0.07 26554. 0.0961
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12.48 0.7321 0.5274 0.0175 0.0243 0.004 0.233 0.059 2.758 0.026 0.261 9.641 0.07 26642. 0.0761
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12.98 0.7613 0.4632 0.0131 0.0216 0.003 0.207 0.044 2.445 0.023 0.195 8.141 0.07 26734. 0.0556
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13.48 0.7906 0.3691 0.0087 0.0187 0.003 0.179 0.029 2.116 0.020 0.130 6.248 0.07 26828. 0.0348
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13.98 0.8199 0.2268 0.0043 0.0156 0.002 0.150 0.014 1.771 0.017 0.064 3.702 0.07 26926. 0.0145
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14.47 0.8492 -0.0030 0.0000 0.0124 0.002 0.119 0.000 1.411 0.013 -0.001 -0.047 0.07 27025. 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 0.0868 0.0332 0.040 1.272 1.161 30.096 0.144 5.164 17.496 0.14 50696. 0.6145
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1.00 0.0294 0.0744 0.0861 0.0341 0.041 1.306 1.152 30.894 0.148 5.125 16.918 0.14 50732. 0.5920
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2.01 0.0589 0.1438 0.0854 0.0350 0.043 1.340 1.142 31.708 0.151 5.081 16.340 0.14 50772. 0.5693
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3.01 0.0883 0.2081 0.0845 0.0359 0.044 1.375 1.131 32.526 0.155 5.029 15.768 0.14 50817. 0.5466
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4.01 0.1177 0.2675 0.0835 0.0367 0.045 1.409 1.117 33.332 0.159 4.970 15.203 0.14 50867. 0.5238
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5.02 0.1472 0.3222 0.0823 0.0376 0.046 1.441 1.102 34.109 0.163 4.900 14.650 0.14 50922. 0.5012
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6.02 0.1766 0.3725 0.0810 0.0384 0.047 1.472 1.084 34.835 0.166 4.820 14.110 0.14 50982. 0.4788
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7.02 0.2061 0.4184 0.0794 0.0391 0.048 1.500 1.063 35.487 0.169 4.728 13.586 0.14 51049. 0.4566
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8.03 0.2355 0.4603 0.0777 0.0397 0.048 1.523 1.039 36.041 0.172 4.623 13.080 0.14 51121. 0.4347
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9.03 0.2649 0.4985 0.0757 0.0402 0.049 1.541 1.012 36.471 0.174 4.503 12.591 0.14 51200. 0.4130
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10.04 0.2944 0.5332 0.0734 0.0405 0.049 1.553 0.982 36.754 0.175 4.368 12.120 0.14 51284. 0.3915
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11.04 0.3238 0.5646 0.0709 0.0406 0.049 1.558 0.948 36.867 0.176 4.218 11.667 0.14 51375. 0.3704
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12.04 0.3532 0.5929 0.0681 0.0406 0.049 1.555 0.911 36.795 0.176 4.053 11.232 0.14 51472. 0.3495
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13.05 0.3827 0.6183 0.0651 0.0403 0.049 1.544 0.871 36.531 0.174 3.873 10.811 0.14 51576. 0.3289
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14.05 0.4121 0.6408 0.0618 0.0398 0.048 1.524 0.827 36.073 0.172 3.681 10.404 0.14 51686. 0.3085
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15.05 0.4415 0.6604 0.0584 0.0390 0.048 1.497 0.782 35.422 0.169 3.476 10.008 0.14 51802. 0.2884
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16.06 0.4710 0.6771 0.0548 0.0381 0.046 1.461 0.733 34.579 0.165 3.262 9.620 0.14 51924. 0.2685
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17.06 0.5004 0.6908 0.0511 0.0370 0.045 1.418 0.683 33.548 0.160 3.039 9.237 0.14 52053. 0.2489
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18.06 0.5299 0.7013 0.0472 0.0356 0.043 1.366 0.631 32.331 0.154 2.808 8.856 0.14 52188. 0.2294
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19.07 0.5593 0.7082 0.0432 0.0341 0.041 1.307 0.578 30.931 0.148 2.570 8.472 0.15 52329. 0.2099
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20.07 0.5887 0.7111 0.0391 0.0324 0.039 1.240 0.523 29.350 0.140 2.326 8.082 0.15 52477. 0.1905
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21.07 0.6182 0.7093 0.0349 0.0304 0.037 1.166 0.467 27.590 0.132 2.077 7.677 0.15 52631. 0.1710
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22.08 0.6476 0.7018 0.0306 0.0283 0.034 1.084 0.410 25.654 0.122 1.824 7.251 0.15 52791. 0.1514
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23.08 0.6770 0.6869 0.0263 0.0260 0.032 0.995 0.352 23.545 0.112 1.567 6.789 0.15 52957. 0.1314
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24.08 0.7065 0.6622 0.0220 0.0234 0.029 0.899 0.294 21.265 0.102 1.308 6.272 0.15 53130. 0.1109
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25.09 0.7359 0.6236 0.0176 0.0207 0.025 0.795 0.235 18.822 0.090 1.047 5.670 0.15 53308. 0.0897
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26.09 0.7653 0.5639 0.0132 0.0179 0.022 0.686 0.176 16.222 0.077 0.784 4.930 0.15 53493. 0.0675
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27.09 0.7948 0.4692 0.0088 0.0149 0.018 0.569 0.117 13.474 0.064 0.522 3.950 0.15 53684. 0.0441
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28.10 0.8242 0.3094 0.0044 0.0117 0.014 0.448 0.059 10.592 0.051 0.261 2.512 0.15 53881. 0.0198
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29.10 0.8537 0.0025 0.0000 0.0084 0.010 0.320 0.000 7.577 0.036 0.001 0.020 0.15 54080. 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 0.0870 0.0315 0.130 2.721 2.620 96.574 0.307 11.655 12.306 0.21 76043. 0.6494
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1.53 0.0299 0.0796 0.0864 0.0325 0.133 2.800 2.601 99.370 0.316 11.570 11.873 0.21 76098. 0.6242
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3.06 0.0598 0.1535 0.0856 0.0334 0.137 2.880 2.579 102.231 0.325 11.470 11.441 0.21 76159. 0.5989
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4.59 0.0898 0.2217 0.0848 0.0343 0.141 2.961 2.553 105.110 0.335 11.354 11.015 0.21 76228. 0.5737
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6.12 0.1197 0.2843 0.0838 0.0353 0.145 3.042 2.522 107.954 0.344 11.219 10.597 0.21 76304. 0.5486
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7.65 0.1496 0.3417 0.0826 0.0362 0.148 3.119 2.487 110.696 0.352 11.061 10.189 0.21 76389. 0.5238
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9.18 0.1795 0.3941 0.0812 0.0370 0.152 3.191 2.446 113.264 0.361 10.878 9.793 0.21 76482. 0.4992
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10.71 0.2094 0.4419 0.0796 0.0378 0.155 3.256 2.398 115.572 0.368 10.666 9.411 0.21 76584. 0.4751
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12.24 0.2394 0.4853 0.0778 0.0384 0.158 3.311 2.343 117.533 0.374 10.424 9.044 0.21 76696. 0.4513
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13.77 0.2693 0.5247 0.0758 0.0389 0.160 3.354 2.281 119.054 0.379 10.147 8.691 0.21 76817. 0.4279
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15.30 0.2992 0.5603 0.0734 0.0392 0.161 3.382 2.211 120.046 0.382 9.835 8.354 0.22 76947. 0.4049
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16.83 0.3291 0.5926 0.0708 0.0393 0.162 3.393 2.133 120.434 0.383 9.486 8.031 0.22 77087. 0.3823
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18.36 0.3590 0.6217 0.0680 0.0393 0.161 3.386 2.046 120.167 0.383 9.101 7.723 0.22 77238. 0.3601
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19.89 0.3890 0.6477 0.0648 0.0389 0.160 3.359 1.952 119.218 0.379 8.684 7.428 0.22 77397. 0.3383
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21.42 0.4189 0.6708 0.0615 0.0384 0.158 3.313 1.852 117.580 0.374 8.237 7.144 0.22 77567. 0.3169
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22.95 0.4488 0.6911 0.0580 0.0376 0.155 3.247 1.745 115.254 0.367 7.764 6.869 0.22 77747. 0.2958
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24.48 0.4787 0.7085 0.0543 0.0367 0.151 3.163 1.634 112.249 0.357 7.267 6.602 0.22 77936. 0.2751
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26.01 0.5087 0.7229 0.0504 0.0355 0.146 3.059 1.518 108.572 0.346 6.750 6.340 0.22 78135. 0.2546
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27.54 0.5386 0.7342 0.0464 0.0340 0.140 2.937 1.397 104.232 0.332 6.216 6.081 0.22 78344. 0.2343
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29.07 0.5685 0.7420 0.0423 0.0324 0.133 2.796 1.274 99.237 0.316 5.666 5.822 0.22 78562. 0.2142
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30.60 0.5984 0.7459 0.0381 0.0306 0.126 2.637 1.147 93.594 0.298 5.103 5.560 0.22 78790. 0.1941
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32.13 0.6283 0.7451 0.0338 0.0285 0.117 2.460 1.018 87.309 0.278 4.529 5.289 0.22 79028. 0.1740
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33.66 0.6583 0.7385 0.0295 0.0263 0.108 2.265 0.887 80.392 0.256 3.945 5.005 0.22 79276. 0.1536
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35.19 0.6882 0.7244 0.0250 0.0238 0.098 2.053 0.754 72.853 0.232 3.354 4.695 0.22 79533. 0.1329
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36.72 0.7181 0.6996 0.0206 0.0211 0.087 1.823 0.620 64.710 0.206 2.758 4.346 0.22 79799. 0.1116
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38.25 0.7480 0.6591 0.0161 0.0183 0.075 1.577 0.485 55.982 0.178 2.158 3.930 0.22 80076. 0.0892
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39.78 0.7779 0.5926 0.0116 0.0153 0.063 1.316 0.350 46.702 0.149 1.556 3.398 0.22 80361. 0.0655
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41.31 0.8079 0.4786 0.0071 0.0121 0.049 1.040 0.215 36.906 0.117 0.956 2.643 0.22 80656. 0.0399
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42.84 0.8378 0.2594 0.0027 0.0087 0.036 0.751 0.081 26.641 0.085 0.361 1.381 0.22 80959. 0.0128
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44.37 0.8677
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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 0.0873 0.0307 0.299 4.707 4.674 222.738 0.532 20.790 9.518 0.29 101389. 0.6708
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2.02 0.0296 0.0811 0.0867 0.0316 0.308 4.847 4.642 229.394 0.548 20.646 9.178 0.29 101461. 0.6445
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4.03 0.0591 0.1563 0.0860 0.0326 0.317 4.991 4.604 236.218 0.564 20.477 8.839 0.29 101541. 0.6183
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6.05 0.0887 0.2256 0.0852 0.0335 0.326 5.137 4.559 243.103 0.580 20.279 8.506 0.29 101632. 0.5921
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8.07 0.1183 0.2892 0.0842 0.0344 0.335 5.281 4.507 249.924 0.597 20.048 8.180 0.29 101732. 0.5661
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10.08 0.1479 0.3475 0.0831 0.0354 0.344 5.421 4.446 256.535 0.612 19.778 7.862 0.29 101843. 0.5404
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12.10 0.1774 0.4006 0.0818 0.0362 0.352 5.552 4.376 262.761 0.627 19.464 7.554 0.29 101965. 0.5151
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14.11 0.2070 0.4490 0.0802 0.0370 0.360 5.672 4.294 268.411 0.641 19.101 7.257 0.29 102099. 0.4902
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16.13 0.2366 0.4930 0.0785 0.0377 0.366 5.775 4.201 273.277 0.652 18.684 6.972 0.29 102245. 0.4658
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18.15 0.2662 0.5330 0.0765 0.0382 0.372 5.856 4.093 277.144 0.662 18.207 6.699 0.29 102403. 0.4418
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20.16 0.2957 0.5692 0.0742 0.0386 0.375 5.912 3.972 279.803 0.668 17.668 6.439 0.29 102573. 0.4183
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22.18 0.3253 0.6020 0.0717 0.0387 0.377 5.939 3.836 281.070 0.671 17.064 6.191 0.29 102757. 0.3953
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24.20 0.3549 0.6316 0.0689 0.0387 0.377 5.934 3.686 280.813 0.670 16.397 5.954 0.29 102953. 0.3727
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26.21 0.3845 0.6583 0.0658 0.0384 0.374 5.895 3.523 278.961 0.666 15.672 5.729 0.29 103162. 0.3505
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28.23 0.4140 0.6822 0.0626 0.0380 0.369 5.821 3.348 275.486 0.658 14.893 5.513 0.29 103384. 0.3288
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30.25 0.4436 0.7034 0.0591 0.0373 0.363 5.713 3.162 270.389 0.646 14.066 5.305 0.29 103618. 0.3075
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32.26 0.4732 0.7218 0.0554 0.0363 0.354 5.572 2.967 263.684 0.629 13.197 5.104 0.29 103866. 0.2866
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34.28 0.5027 0.7375 0.0516 0.0352 0.342 5.397 2.763 255.388 0.610 12.292 4.908 0.29 104125. 0.2660
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36.29 0.5323 0.7504 0.0477 0.0338 0.329 5.188 2.553 245.520 0.586 11.354 4.716 0.29 104398. 0.2456
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38.31 0.5619 0.7601 0.0436 0.0323 0.314 4.947 2.336 234.097 0.559 10.389 4.526 0.29 104683. 0.2255
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40.33 0.5915 0.7664 0.0395 0.0305 0.297 4.673 2.113 221.134 0.528 9.401 4.335 0.29 104981. 0.2054
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42.34 0.6210 0.7686 0.0352 0.0285 0.277 4.367 1.887 206.648 0.493 8.391 4.141 0.29 105292. 0.1854
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44.36 0.6506 0.7660 0.0309 0.0263 0.256 4.029 1.656 190.658 0.455 7.365 3.939 0.29 105615. 0.1652
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46.38 0.6802 0.7570 0.0266 0.0239 0.232 3.660 1.422 173.186 0.413 6.324 3.724 0.29 105950. 0.1447
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48.39 0.7098 0.7394 0.0221 0.0213 0.207 3.260 1.185 154.268 0.368 5.272 3.485 0.29 106298. 0.1237
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50.41 0.7393 0.7089 0.0177 0.0185 0.180 2.830 0.947 133.948 0.320 4.214 3.208 0.29 106659. 0.1018
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52.43 0.7689 0.6577 0.0132 0.0155 0.151 2.373 0.709 112.291 0.268 3.152 2.862 0.29 107032. 0.0785
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54.44 0.7985 0.5692 0.0088 0.0123 0.120 1.889 0.470 89.381 0.213 2.090 2.385 0.29 107417. 0.0533
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56.46 0.8280 0.4001 0.0043 0.0090 0.088 1.380 0.233 65.325 0.156 1.036 1.616 0.30 107813. 0.0254
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58.47 0.8576 -0.0106 -0.0001 0.0055 0.054 0.846 -0.004 40.038 0.096 -0.016 -0.041 0.30 108209. 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 0.0877 0.0302 0.574 7.241 7.332 428.346 0.818 32.612 7.764 0.36 126733. 0.6853
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2.52 0.0296 0.0827 0.0871 0.0312 0.592 7.464 7.283 441.558 0.843 32.395 7.481 0.36 126823. 0.6581
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5.05 0.0592 0.1593 0.0864 0.0321 0.610 7.694 7.226 455.132 0.869 32.141 7.201 0.36 126924. 0.6310
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7.57 0.0888 0.2298 0.0856 0.0331 0.629 7.926 7.159 468.857 0.895 31.842 6.925 0.36 127036. 0.6040
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10.09 0.1184 0.2944 0.0846 0.0340 0.647 8.156 7.080 482.489 0.921 31.490 6.655 0.36 127162. 0.5772
|
|
12.61 0.1480 0.3535 0.0835 0.0350 0.665 8.380 6.987 495.732 0.947 31.078 6.393 0.36 127301. 0.5508
|
|
15.14 0.1776 0.4074 0.0822 0.0359 0.682 8.592 6.879 508.244 0.971 30.598 6.139 0.36 127454. 0.5249
|
|
17.66 0.2072 0.4564 0.0807 0.0367 0.697 8.784 6.753 519.638 0.992 30.039 5.895 0.36 127621. 0.4994
|
|
20.18 0.2368 0.5008 0.0790 0.0374 0.710 8.951 6.608 529.498 1.011 29.394 5.661 0.36 127804. 0.4744
|
|
22.70 0.2664 0.5412 0.0770 0.0379 0.721 9.084 6.442 537.393 1.026 28.654 5.437 0.36 128002. 0.4499
|
|
25.23 0.2960 0.5778 0.0748 0.0383 0.728 9.177 6.253 542.902 1.037 27.815 5.224 0.36 128216. 0.4259
|
|
27.75 0.3256 0.6110 0.0722 0.0385 0.732 9.224 6.042 545.654 1.042 26.873 5.022 0.36 128446. 0.4024
|
|
30.27 0.3552 0.6410 0.0694 0.0385 0.731 9.219 5.807 545.378 1.042 25.830 4.830 0.36 128692. 0.3794
|
|
32.80 0.3848 0.6680 0.0664 0.0382 0.727 9.161 5.552 541.924 1.035 24.693 4.646 0.36 128953. 0.3569
|
|
35.32 0.4144 0.6924 0.0631 0.0378 0.718 9.048 5.277 535.236 1.022 23.470 4.472 0.36 129231. 0.3348
|
|
37.84 0.4440 0.7140 0.0596 0.0371 0.704 8.880 4.985 525.310 1.003 22.171 4.304 0.36 129525. 0.3132
|
|
40.36 0.4736 0.7330 0.0559 0.0361 0.687 8.658 4.677 512.174 0.978 20.805 4.142 0.36 129835. 0.2920
|
|
42.89 0.5032 0.7493 0.0521 0.0350 0.665 8.382 4.357 495.862 0.947 19.381 3.986 0.36 130160. 0.2712
|
|
45.41 0.5328 0.7629 0.0481 0.0336 0.639 8.053 4.025 476.411 0.910 17.905 3.832 0.36 130502. 0.2507
|
|
47.93 0.5624 0.7736 0.0440 0.0320 0.609 7.672 3.684 453.855 0.867 16.385 3.681 0.36 130859. 0.2303
|
|
50.46 0.5920 0.7810 0.0399 0.0302 0.574 7.239 3.333 428.224 0.818 14.827 3.531 0.36 131233. 0.2101
|
|
52.98 0.6216 0.7846 0.0356 0.0282 0.536 6.754 2.976 399.551 0.763 13.237 3.378 0.36 131622. 0.1900
|
|
55.50 0.6512 0.7836 0.0312 0.0260 0.493 6.219 2.612 367.872 0.703 11.619 3.221 0.36 132026. 0.1697
|
|
58.02 0.6808 0.7767 0.0268 0.0235 0.447 5.633 2.243 333.235 0.636 9.978 3.053 0.37 132447. 0.1491
|
|
60.55 0.7104 0.7616 0.0224 0.0209 0.397 4.999 1.871 295.707 0.565 8.320 2.869 0.37 132883. 0.1279
|
|
63.07 0.7400 0.7343 0.0179 0.0180 0.342 4.317 1.495 255.379 0.488 6.651 2.656 0.37 133334. 0.1059
|
|
65.59 0.7696 0.6870 0.0134 0.0150 0.285 3.590 1.119 212.380 0.406 4.976 2.389 0.37 133801. 0.0824
|
|
68.11 0.7992 0.6026 0.0089 0.0118 0.224 2.821 0.743 166.881 0.319 3.303 2.018 0.37 134283. 0.0567
|
|
70.64 0.8288 0.4347 0.0044 0.0084 0.160 2.013 0.369 119.094 0.227 1.639 1.404 0.37 134779. 0.0278
|
|
73.16 0.8584 -0.0103 -0.0001 0.0049 0.092 1.162 -0.005 68.767 0.131 -0.022 -0.032 0.37 135273. 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 0.0881 0.0300 0.985 10.344 10.605 734.271 1.169 47.172 6.551 0.43 152075. 0.6954
|
|
3.03 0.0296 0.0839 0.0875 0.0309 1.016 10.671 10.539 757.495 1.206 46.877 6.310 0.43 152183. 0.6678
|
|
6.06 0.0593 0.1614 0.0869 0.0319 1.048 11.008 10.460 781.412 1.244 46.527 6.072 0.43 152304. 0.6401
|
|
9.10 0.0889 0.2327 0.0861 0.0329 1.080 11.349 10.367 805.659 1.282 46.115 5.837 0.43 152439. 0.6126
|
|
12.13 0.1186 0.2981 0.0852 0.0339 1.113 11.689 10.258 829.803 1.321 45.627 5.607 0.43 152590. 0.5854
|
|
15.16 0.1482 0.3578 0.0841 0.0348 1.144 12.021 10.129 853.325 1.358 45.052 5.384 0.43 152757. 0.5585
|
|
18.19 0.1779 0.4121 0.0828 0.0358 1.174 12.335 9.977 875.613 1.394 44.376 5.168 0.43 152941. 0.5321
|
|
21.22 0.2075 0.4615 0.0814 0.0366 1.202 12.622 9.799 895.981 1.426 43.586 4.961 0.43 153142. 0.5062
|
|
24.25 0.2371 0.5063 0.0797 0.0373 1.225 12.871 9.593 913.685 1.454 42.670 4.762 0.43 153362. 0.4808
|
|
27.29 0.2668 0.5470 0.0777 0.0379 1.244 13.072 9.356 927.951 1.477 41.615 4.573 0.43 153601. 0.4560
|
|
30.32 0.2964 0.5839 0.0754 0.0383 1.258 13.214 9.085 938.026 1.493 40.412 4.393 0.43 153858. 0.4317
|
|
33.35 0.3261 0.6173 0.0729 0.0385 1.265 13.288 8.781 943.241 1.501 39.057 4.222 0.43 154135. 0.4079
|
|
36.38 0.3557 0.6476 0.0701 0.0385 1.265 13.286 8.443 943.106 1.501 37.553 4.060 0.43 154431. 0.3846
|
|
39.41 0.3854 0.6750 0.0670 0.0383 1.257 13.204 8.073 937.346 1.492 35.910 3.907 0.43 154746. 0.3618
|
|
42.44 0.4150 0.6996 0.0637 0.0378 1.242 13.043 7.675 925.853 1.474 34.138 3.760 0.43 155081. 0.3396
|
|
45.48 0.4446 0.7216 0.0602 0.0371 1.218 12.800 7.251 908.623 1.446 32.254 3.620 0.43 155435. 0.3177
|
|
48.51 0.4743 0.7411 0.0565 0.0362 1.188 12.477 6.805 885.703 1.410 30.270 3.485 0.43 155808. 0.2964
|
|
51.54 0.5039 0.7580 0.0526 0.0350 1.149 12.075 6.340 857.158 1.364 28.199 3.355 0.43 156200. 0.2753
|
|
54.57 0.5336 0.7722 0.0486 0.0336 1.104 11.594 5.857 823.054 1.310 26.052 3.228 0.43 156611. 0.2546
|
|
57.60 0.5632 0.7836 0.0445 0.0320 1.051 11.037 5.360 783.454 1.247 23.840 3.103 0.44 157041. 0.2342
|
|
60.63 0.5929 0.7919 0.0403 0.0301 0.990 10.402 4.850 738.414 1.175 21.572 2.979 0.44 157491. 0.2139
|
|
63.67 0.6225 0.7965 0.0359 0.0281 0.923 9.692 4.329 687.991 1.095 19.255 2.854 0.44 157959. 0.1936
|
|
66.70 0.6521 0.7969 0.0315 0.0258 0.848 8.907 3.799 632.251 1.006 16.897 2.725 0.44 158446. 0.1732
|
|
69.73 0.6818 0.7915 0.0271 0.0233 0.766 8.048 3.261 571.279 0.909 14.506 2.589 0.44 158952. 0.1524
|
|
72.76 0.7114 0.7784 0.0226 0.0206 0.677 7.117 2.718 505.193 0.804 12.090 2.440 0.44 159477. 0.1311
|
|
75.79 0.7411 0.7536 0.0180 0.0177 0.582 6.116 2.171 434.157 0.691 9.656 2.268 0.44 160020. 0.1089
|
|
78.82 0.7707 0.7093 0.0135 0.0146 0.481 5.049 1.622 358.399 0.570 7.214 2.052 0.44 160582. 0.0852
|
|
81.86 0.8004 0.6279 0.0089 0.0114 0.373 3.919 1.073 278.224 0.443 4.774 1.750 0.44 161162. 0.0591
|
|
84.89 0.8300 0.4594 0.0044 0.0079 0.260 2.733 0.528 194.013 0.309 2.349 1.235 0.44 161759. 0.0292
|
|
87.92 0.8596 -0.0309 -0.0002 0.0043 0.141 1.479 -0.019 104.960 0.167 -0.083 -0.080 0.44 162344. 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 0.0885 0.0299 1.560 14.042 14.508 1162.935 1.586 64.533 5.659 0.50 177415. 0.7026
|
|
3.53 0.0296 0.0845 0.0880 0.0309 1.610 14.494 14.424 1200.407 1.638 64.159 5.450 0.50 177540. 0.6748
|
|
7.07 0.0592 0.1625 0.0874 0.0319 1.662 14.962 14.324 1239.110 1.690 63.714 5.243 0.50 177681. 0.6469
|
|
10.60 0.0889 0.2343 0.0867 0.0329 1.714 15.437 14.205 1278.469 1.744 63.185 5.040 0.50 177839. 0.6192
|
|
14.14 0.1185 0.3000 0.0858 0.0339 1.767 15.912 14.064 1317.793 1.798 62.555 4.841 0.50 178014. 0.5917
|
|
17.67 0.1481 0.3601 0.0848 0.0349 1.819 16.376 13.895 1356.238 1.850 61.806 4.647 0.50 178208. 0.5647
|
|
21.21 0.1777 0.4147 0.0836 0.0358 1.868 16.818 13.696 1392.811 1.900 60.920 4.460 0.50 178423. 0.5381
|
|
24.74 0.2074 0.4643 0.0821 0.0367 1.913 17.223 13.462 1426.388 1.946 59.877 4.281 0.50 178658. 0.5120
|
|
28.28 0.2370 0.5094 0.0804 0.0374 1.952 17.578 13.188 1455.745 1.986 58.659 4.109 0.50 178914. 0.4864
|
|
31.81 0.2666 0.5502 0.0785 0.0380 1.984 17.866 12.870 1479.608 2.018 57.248 3.945 0.50 179192. 0.4614
|
|
35.35 0.2962 0.5873 0.0763 0.0385 2.007 18.072 12.507 1496.732 2.042 55.631 3.790 0.50 179493. 0.4369
|
|
38.88 0.3259 0.6210 0.0738 0.0387 2.020 18.184 12.096 1506.005 2.054 53.801 3.643 0.50 179815. 0.4130
|
|
42.42 0.3555 0.6515 0.0710 0.0387 2.020 18.192 11.637 1506.602 2.055 51.762 3.503 0.50 180161. 0.3896
|
|
45.95 0.3851 0.6791 0.0679 0.0385 2.009 18.088 11.134 1498.054 2.044 49.526 3.371 0.50 180529. 0.3667
|
|
49.49 0.4147 0.7041 0.0646 0.0381 1.985 17.873 10.591 1480.171 2.019 47.109 3.245 0.50 180919. 0.3443
|
|
53.02 0.4444 0.7265 0.0611 0.0374 1.948 17.544 10.012 1452.942 1.982 44.533 3.125 0.50 181332. 0.3224
|
|
56.56 0.4740 0.7464 0.0573 0.0364 1.899 17.103 9.401 1416.445 1.932 41.815 3.010 0.51 181767. 0.3009
|
|
60.09 0.5036 0.7638 0.0535 0.0352 1.838 16.552 8.762 1370.795 1.870 38.975 2.899 0.51 182225. 0.2798
|
|
63.63 0.5332 0.7786 0.0494 0.0338 1.765 15.892 8.100 1316.108 1.795 36.027 2.791 0.51 182705. 0.2590
|
|
67.16 0.5629 0.7907 0.0452 0.0322 1.680 15.123 7.416 1252.493 1.709 32.987 2.686 0.51 183206. 0.2384
|
|
70.69 0.5925 0.7999 0.0410 0.0303 1.582 14.249 6.715 1180.047 1.610 29.868 2.581 0.51 183730. 0.2180
|
|
74.23 0.6221 0.8057 0.0366 0.0283 1.474 13.268 5.998 1098.866 1.499 26.680 2.476 0.51 184276. 0.1977
|
|
77.76 0.6517 0.8073 0.0321 0.0259 1.353 12.184 5.268 1009.058 1.377 23.434 2.368 0.51 184844. 0.1772
|
|
81.30 0.6814 0.8037 0.0276 0.0234 1.221 10.997 4.528 910.760 1.242 20.140 2.255 0.51 185434. 0.1564
|
|
84.83 0.7110 0.7928 0.0231 0.0207 1.078 9.710 3.779 804.161 1.097 16.810 2.132 0.51 186046. 0.1351
|
|
88.37 0.7406 0.7708 0.0185 0.0177 0.925 8.326 3.025 689.523 0.941 13.454 1.990 0.51 186680. 0.1128
|
|
91.90 0.7702 0.7305 0.0138 0.0146 0.761 6.849 2.267 567.212 0.774 10.086 1.813 0.51 187334. 0.0890
|
|
95.44 0.7999 0.6549 0.0092 0.0113 0.587 5.285 1.511 437.723 0.597 6.719 1.565 0.52 188011. 0.0627
|
|
98.97 0.8295 0.4944 0.0046 0.0078 0.405 3.643 0.758 301.669 0.412 3.371 1.140 0.52 188707. 0.0323
|
|
102.51 0.8591 0.0063 0.0000 0.0041 0.212 1.909 0.005 158.126 0.216 0.022 0.014 0.52 189394. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 8000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.0890 0.0300 2.332 18.371 19.056 1738.847 2.076 84.761 4.971 0.57 202751. 0.7073
|
|
4.05 0.0297 0.0849 0.0885 0.0309 2.408 18.974 18.956 1795.856 2.144 84.316 4.788 0.57 202894. 0.6795
|
|
8.09 0.0593 0.1634 0.0880 0.0320 2.488 19.598 18.836 1854.956 2.214 83.783 4.606 0.57 203055. 0.6516
|
|
12.14 0.0890 0.2355 0.0873 0.0330 2.568 20.236 18.692 1915.291 2.286 83.142 4.427 0.57 203235. 0.6239
|
|
16.18 0.1187 0.3016 0.0865 0.0340 2.650 20.875 18.519 1975.814 2.358 82.372 4.251 0.57 203436. 0.5964
|
|
20.23 0.1483 0.3619 0.0855 0.0351 2.729 21.503 18.311 2035.234 2.429 81.447 4.081 0.57 203659. 0.5692
|
|
24.27 0.1780 0.4167 0.0844 0.0360 2.805 22.103 18.062 2092.009 2.497 80.342 3.916 0.57 203904. 0.5425
|
|
28.32 0.2077 0.4665 0.0830 0.0369 2.876 22.656 17.767 2144.382 2.560 79.029 3.758 0.57 204173. 0.5164
|
|
32.36 0.2373 0.5117 0.0814 0.0377 2.937 23.143 17.419 2190.429 2.615 77.480 3.607 0.57 204466. 0.4907
|
|
36.41 0.2670 0.5528 0.0795 0.0384 2.988 23.541 17.013 2228.152 2.660 75.673 3.463 0.57 204785. 0.4656
|
|
40.45 0.2967 0.5900 0.0773 0.0389 3.025 23.831 16.544 2255.580 2.692 73.587 3.327 0.57 205130. 0.4411
|
|
44.50 0.3263 0.6238 0.0748 0.0391 3.045 23.993 16.010 2270.956 2.711 71.212 3.198 0.57 205500. 0.4171
|
|
48.54 0.3560 0.6545 0.0720 0.0392 3.048 24.015 15.412 2272.962 2.713 68.552 3.075 0.57 205896. 0.3936
|
|
52.59 0.3857 0.6824 0.0689 0.0389 3.032 23.887 14.753 2260.846 2.699 65.622 2.960 0.58 206319. 0.3706
|
|
56.63 0.4153 0.7076 0.0656 0.0385 2.996 23.606 14.039 2234.300 2.667 62.446 2.850 0.58 206767. 0.3481
|
|
60.68 0.4450 0.7303 0.0620 0.0378 2.941 23.173 13.276 2193.310 2.618 59.050 2.745 0.58 207240. 0.3261
|
|
64.73 0.4747 0.7506 0.0582 0.0368 2.867 22.589 12.469 2138.009 2.552 55.461 2.645 0.58 207740. 0.3045
|
|
68.77 0.5043 0.7684 0.0543 0.0356 2.774 21.855 11.624 2068.591 2.469 51.704 2.549 0.58 208265. 0.2833
|
|
72.82 0.5340 0.7838 0.0502 0.0342 2.662 20.975 10.746 1985.255 2.370 47.800 2.455 0.58 208815. 0.2624
|
|
76.86 0.5636 0.7965 0.0460 0.0325 2.532 19.949 9.840 1888.183 2.254 43.770 2.364 0.58 209391. 0.2417
|
|
80.91 0.5933 0.8064 0.0416 0.0306 2.384 18.780 8.910 1777.543 2.122 39.632 2.274 0.58 209991. 0.2212
|
|
84.95 0.6230 0.8130 0.0372 0.0285 2.217 17.470 7.958 1653.491 1.974 35.399 2.183 0.58 210618. 0.2008
|
|
89.00 0.6526 0.8157 0.0326 0.0261 2.033 16.019 6.989 1516.201 1.810 31.087 2.091 0.58 211269. 0.1802
|
|
93.04 0.6823 0.8134 0.0280 0.0235 1.832 14.431 6.005 1365.882 1.630 26.710 1.994 0.58 211945. 0.1593
|
|
97.09 0.7120 0.8040 0.0234 0.0207 1.613 12.708 5.009 1202.826 1.436 22.282 1.889 0.59 212647. 0.1378
|
|
101.13 0.7416 0.7840 0.0187 0.0177 1.378 10.855 4.006 1027.440 1.226 17.817 1.768 0.59 213373. 0.1154
|
|
105.18 0.7713 0.7462 0.0140 0.0145 1.127 8.878 2.998 840.287 1.003 13.335 1.618 0.59 214123. 0.0913
|
|
109.22 0.8010 0.6732 0.0093 0.0111 0.861 6.784 1.990 642.134 0.766 8.854 1.406 0.59 214898. 0.0647
|
|
113.27 0.8306 0.5129 0.0046 0.0075 0.582 4.585 0.988 433.934 0.518 4.396 1.033 0.59 215696. 0.0335
|
|
117.31 0.8603 -0.0209 -0.0001 0.0037 0.286 2.253 -0.019 213.217 0.255 -0.085 -0.041 0.59 216470. 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 0.0895 0.0302 3.344 23.420 24.263 2493.763 2.646 107.924 4.413 0.64 228085. 0.7086
|
|
4.55 0.0297 0.0849 0.0891 0.0312 3.454 24.191 24.152 2575.878 2.733 107.427 4.253 0.64 228245. 0.6813
|
|
9.11 0.0594 0.1635 0.0886 0.0322 3.569 24.994 24.016 2661.420 2.824 106.825 4.093 0.64 228426. 0.6539
|
|
13.66 0.0891 0.2357 0.0880 0.0333 3.687 25.819 23.852 2749.207 2.917 106.094 3.935 0.64 228628. 0.6265
|
|
18.22 0.1188 0.3019 0.0873 0.0343 3.806 26.651 23.652 2837.769 3.011 105.205 3.780 0.64 228854. 0.5993
|
|
22.77 0.1484 0.3624 0.0864 0.0354 3.923 27.472 23.409 2925.254 3.104 104.123 3.630 0.64 229104. 0.5725
|
|
27.33 0.1781 0.4174 0.0853 0.0364 4.036 28.262 23.114 3009.394 3.193 102.813 3.484 0.64 229380. 0.5460
|
|
31.88 0.2078 0.4673 0.0840 0.0374 4.141 28.997 22.760 3087.575 3.276 101.236 3.343 0.64 229683. 0.5200
|
|
36.44 0.2375 0.5127 0.0824 0.0382 4.233 29.648 22.337 3156.892 3.350 99.355 3.209 0.64 230013. 0.4944
|
|
40.99 0.2672 0.5538 0.0806 0.0389 4.310 30.187 21.838 3214.291 3.410 97.135 3.082 0.64 230373. 0.4694
|
|
45.55 0.2969 0.5911 0.0784 0.0394 4.367 30.585 21.256 3256.742 3.456 94.548 2.960 0.65 230761. 0.4449
|
|
50.10 0.3266 0.6251 0.0760 0.0397 4.401 30.818 20.589 3281.520 3.482 91.579 2.846 0.65 231179. 0.4209
|
|
54.66 0.3563 0.6559 0.0732 0.0398 4.407 30.865 19.836 3286.576 3.487 88.230 2.737 0.65 231626. 0.3974
|
|
59.21 0.3860 0.6840 0.0701 0.0396 4.386 30.717 19.002 3270.717 3.470 84.520 2.635 0.65 232103. 0.3744
|
|
63.77 0.4157 0.7095 0.0668 0.0391 4.336 30.367 18.094 3233.467 3.431 80.480 2.538 0.65 232608. 0.3519
|
|
68.32 0.4453 0.7325 0.0632 0.0384 4.257 29.816 17.119 3174.803 3.369 76.146 2.446 0.65 233143. 0.3299
|
|
72.88 0.4750 0.7532 0.0594 0.0374 4.150 29.066 16.087 3094.944 3.284 71.553 2.358 0.65 233707. 0.3082
|
|
77.43 0.5047 0.7715 0.0554 0.0362 4.015 28.120 15.003 2994.209 3.177 66.734 2.273 0.65 234299. 0.2870
|
|
81.98 0.5344 0.7874 0.0512 0.0348 3.853 26.981 13.876 2872.932 3.048 61.718 2.191 0.65 234920. 0.2660
|
|
86.54 0.5641 0.8007 0.0469 0.0330 3.663 25.652 12.710 2731.422 2.898 56.533 2.111 0.65 235569. 0.2453
|
|
91.09 0.5938 0.8113 0.0425 0.0311 3.446 24.135 11.511 2569.957 2.727 51.202 2.032 0.65 236247. 0.2247
|
|
95.65 0.6235 0.8188 0.0380 0.0289 3.203 22.434 10.285 2388.789 2.535 45.746 1.953 0.66 236954. 0.2041
|
|
100.20 0.6532 0.8226 0.0333 0.0265 2.934 20.550 9.034 2188.182 2.322 40.182 1.873 0.66 237688. 0.1835
|
|
104.76 0.6829 0.8215 0.0286 0.0238 2.640 18.486 7.763 1968.453 2.089 34.531 1.789 0.66 238451. 0.1625
|
|
109.31 0.7126 0.8138 0.0239 0.0209 2.320 16.247 6.477 1730.026 1.836 28.809 1.698 0.66 239242. 0.1409
|
|
113.87 0.7422 0.7958 0.0191 0.0178 1.976 13.838 5.179 1473.497 1.563 23.037 1.594 0.66 240060. 0.1183
|
|
118.42 0.7719 0.7607 0.0143 0.0145 1.609 11.267 3.876 1199.696 1.273 17.238 1.465 0.66 240906. 0.0940
|
|
122.98 0.8016 0.6912 0.0095 0.0110 1.220 8.544 2.572 909.753 0.965 11.439 1.282 0.66 241779. 0.0670
|
|
127.53 0.8313 0.5339 0.0047 0.0073 0.811 5.683 1.274 605.077 0.642 5.666 0.955 0.66 242678. 0.0351
|
|
132.09 0.8610 -0.0335 -0.0001 0.0034 0.377 2.637 -0.036 280.792 0.298 -0.159 -0.058 0.67 243537. 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 0.0901 0.0311 4.728 29.798 30.138 3525.420 3.367 134.052 3.877 0.71 253415. 0.6939
|
|
5.06 0.0297 0.0831 0.0897 0.0321 4.877 30.737 30.021 3636.571 3.473 133.532 3.744 0.71 253592. 0.6688
|
|
10.13 0.0594 0.1604 0.0893 0.0331 5.032 31.719 29.878 3752.688 3.584 132.895 3.611 0.71 253792. 0.6434
|
|
15.19 0.0891 0.2318 0.0888 0.0341 5.193 32.729 29.702 3872.171 3.698 132.113 3.479 0.71 254017. 0.6181
|
|
20.26 0.1189 0.2975 0.0881 0.0352 5.355 33.750 29.484 3993.034 3.813 131.146 3.349 0.71 254267. 0.5928
|
|
25.32 0.1486 0.3577 0.0873 0.0363 5.515 34.762 29.216 4112.726 3.927 129.952 3.222 0.71 254544. 0.5677
|
|
30.39 0.1783 0.4128 0.0863 0.0373 5.670 35.737 28.885 4228.116 4.038 128.480 3.099 0.72 254850. 0.5429
|
|
35.45 0.2080 0.4631 0.0851 0.0382 5.814 36.645 28.480 4335.567 4.140 126.678 2.979 0.72 255187. 0.5183
|
|
40.52 0.2377 0.5089 0.0837 0.0391 5.942 37.452 27.989 4431.023 4.231 124.493 2.865 0.72 255555. 0.4941
|
|
45.58 0.2674 0.5507 0.0819 0.0398 6.048 38.121 27.400 4510.216 4.307 121.876 2.755 0.72 255955. 0.4702
|
|
50.65 0.2971 0.5887 0.0798 0.0403 6.127 38.618 26.705 4568.909 4.363 118.784 2.651 0.72 256387. 0.4466
|
|
55.71 0.3269 0.6233 0.0774 0.0406 6.173 38.908 25.898 4603.255 4.396 115.194 2.552 0.72 256852. 0.4233
|
|
60.78 0.3566 0.6548 0.0747 0.0407 6.183 38.967 24.979 4610.291 4.403 111.105 2.457 0.72 257351. 0.4004
|
|
65.84 0.3863 0.6835 0.0716 0.0405 6.153 38.781 23.952 4588.215 4.381 106.539 2.368 0.72 257882. 0.3778
|
|
70.91 0.4160 0.7095 0.0682 0.0400 6.083 38.341 22.827 4536.232 4.332 101.536 2.282 0.72 258446. 0.3555
|
|
75.97 0.4457 0.7331 0.0646 0.0393 5.973 37.648 21.614 4454.166 4.253 96.141 2.201 0.72 259042. 0.3336
|
|
81.04 0.4754 0.7542 0.0608 0.0383 5.823 36.701 20.324 4342.180 4.146 90.402 2.123 0.72 259671. 0.3120
|
|
86.10 0.5051 0.7731 0.0567 0.0370 5.633 35.504 18.966 4200.574 4.011 84.362 2.048 0.72 260331. 0.2907
|
|
91.17 0.5349 0.7895 0.0525 0.0355 5.404 34.060 17.550 4029.724 3.848 78.062 1.975 0.72 261024. 0.2698
|
|
96.23 0.5646 0.8035 0.0481 0.0338 5.136 32.372 16.083 3830.022 3.657 71.537 1.905 0.73 261748. 0.2490
|
|
101.30 0.5943 0.8149 0.0436 0.0318 4.830 30.444 14.572 3601.892 3.440 64.817 1.835 0.73 262503. 0.2283
|
|
106.36 0.6240 0.8233 0.0389 0.0295 4.487 28.279 13.024 3345.741 3.195 57.931 1.766 0.73 263290. 0.2077
|
|
111.43 0.6537 0.8281 0.0342 0.0270 4.106 25.881 11.444 3061.971 2.924 50.904 1.695 0.73 264109. 0.1869
|
|
116.49 0.6834 0.8283 0.0294 0.0243 3.689 23.252 9.837 2751.036 2.627 43.757 1.622 0.73 264958. 0.1658
|
|
121.56 0.7131 0.8222 0.0245 0.0213 3.237 20.400 8.209 2413.529 2.305 36.516 1.543 0.73 265839. 0.1441
|
|
126.62 0.7429 0.8063 0.0196 0.0181 2.749 17.330 6.566 2050.288 1.958 29.205 1.453 0.73 266751. 0.1213
|
|
131.69 0.7726 0.7739 0.0147 0.0147 2.229 14.052 4.913 1662.523 1.588 21.854 1.340 0.74 267693. 0.0969
|
|
136.75 0.8023 0.7079 0.0097 0.0110 1.679 10.582 3.259 1251.986 1.196 14.496 1.181 0.74 268665. 0.0695
|
|
141.82 0.8320 0.5535 0.0048 0.0072 1.101 6.940 1.612 821.096 0.784 7.168 0.890 0.74 269665. 0.0368
|
|
146.88 0.8617 -0.0494 -0.0002 0.0032 0.484 3.051 -0.061 360.915 0.345 -0.271 -0.077 0.74 270599. 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 0.0906 0.0338 6.846 39.228 36.667 5105.229 4.432 163.096 3.258 0.79 278741. 0.6430
|
|
5.58 0.0297 0.0772 0.0903 0.0348 7.039 40.334 36.552 5249.162 4.557 162.581 3.158 0.79 278935. 0.6224
|
|
11.15 0.0595 0.1495 0.0899 0.0358 7.241 41.490 36.410 5399.673 4.688 161.950 3.058 0.79 279155. 0.6016
|
|
16.73 0.0892 0.2170 0.0895 0.0368 7.449 42.680 36.234 5554.512 4.822 161.167 2.959 0.79 279400. 0.5806
|
|
22.30 0.1190 0.2797 0.0890 0.0378 7.658 43.881 36.013 5710.781 4.958 160.185 2.860 0.79 279674. 0.5595
|
|
27.88 0.1487 0.3378 0.0883 0.0389 7.865 45.064 35.735 5864.717 5.091 158.950 2.764 0.79 279979. 0.5386
|
|
33.46 0.1784 0.3916 0.0874 0.0398 8.062 46.193 35.386 6011.732 5.219 157.396 2.670 0.79 280315. 0.5177
|
|
39.03 0.2082 0.4413 0.0863 0.0407 8.243 47.229 34.949 6146.530 5.336 155.452 2.579 0.79 280685. 0.4970
|
|
44.61 0.2379 0.4873 0.0850 0.0415 8.399 48.126 34.407 6263.294 5.437 153.043 2.492 0.79 281089. 0.4764
|
|
50.19 0.2677 0.5298 0.0834 0.0421 8.524 48.839 33.745 6356.029 5.518 150.097 2.408 0.79 281529. 0.4560
|
|
55.76 0.2974 0.5691 0.0814 0.0425 8.608 49.323 32.948 6419.000 5.572 146.553 2.328 0.79 282006. 0.4356
|
|
61.34 0.3271 0.6055 0.0791 0.0427 8.646 49.540 32.008 6447.229 5.597 142.369 2.252 0.79 282519. 0.4153
|
|
66.91 0.3569 0.6391 0.0764 0.0427 8.632 49.462 30.921 6437.186 5.588 137.535 2.179 0.79 283069. 0.3949
|
|
72.49 0.3866 0.6701 0.0734 0.0423 8.565 49.078 29.693 6387.156 5.545 132.075 2.109 0.79 283655. 0.3746
|
|
78.07 0.4164 0.6985 0.0700 0.0417 8.444 48.384 28.335 6296.841 5.466 126.036 2.041 0.79 284278. 0.3542
|
|
83.64 0.4461 0.7244 0.0664 0.0409 8.270 47.385 26.861 6166.796 5.354 119.476 1.976 0.79 284936. 0.3338
|
|
89.22 0.4758 0.7478 0.0625 0.0397 8.043 46.086 25.283 5997.807 5.207 112.459 1.912 0.79 285631. 0.3134
|
|
94.79 0.5056 0.7687 0.0583 0.0384 7.765 44.494 23.615 5790.558 5.027 105.041 1.850 0.80 286360. 0.2930
|
|
100.37 0.5353 0.7871 0.0540 0.0367 7.437 42.611 21.870 5545.531 4.814 97.276 1.789 0.80 287125. 0.2727
|
|
105.95 0.5650 0.8028 0.0495 0.0349 7.058 40.440 20.056 5263.038 4.569 89.210 1.728 0.80 287924. 0.2523
|
|
111.52 0.5948 0.8157 0.0449 0.0328 6.629 37.984 18.184 4943.287 4.291 80.884 1.668 0.80 288758. 0.2319
|
|
117.10 0.6245 0.8256 0.0402 0.0304 6.150 35.241 16.262 4586.401 3.982 72.335 1.608 0.80 289627. 0.2114
|
|
122.67 0.6543 0.8319 0.0353 0.0278 5.622 32.214 14.298 4192.488 3.640 63.596 1.547 0.80 290530. 0.1907
|
|
128.25 0.6840 0.8336 0.0304 0.0249 5.045 28.908 12.297 3762.140 3.266 54.697 1.483 0.80 291467. 0.1695
|
|
133.83 0.7137 0.8287 0.0254 0.0218 4.421 25.332 10.267 3296.747 2.862 45.668 1.413 0.81 292439. 0.1475
|
|
139.40 0.7435 0.8139 0.0203 0.0185 3.752 21.497 8.215 2797.692 2.429 36.541 1.332 0.81 293444. 0.1244
|
|
144.98 0.7732 0.7815 0.0152 0.0150 3.041 17.427 6.149 2268.046 1.969 27.350 1.230 0.81 294483. 0.0994
|
|
150.56 0.8030 0.7129 0.0101 0.0113 2.296 13.155 4.077 1712.034 1.486 18.135 1.080 0.81 295554. 0.0711
|
|
156.13 0.8327 0.5498 0.0050 0.0075 1.522 8.722 2.010 1135.127 0.985 8.942 0.803 0.81 296657. 0.0371
|
|
161.71 0.8624 -0.0641 -0.0003 0.0034 0.698 3.998 -0.104 520.256 0.452 -0.461 -0.090 0.81 297661. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 12000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.0908 0.0393 10.330 54.259 43.735 7703.419 6.130 194.531 2.575 0.86 304071. 0.5551
|
|
6.13 0.0300 0.0674 0.0906 0.0403 10.580 55.571 43.624 7889.705 6.278 194.040 2.508 0.86 304283. 0.5400
|
|
12.26 0.0599 0.1311 0.0903 0.0413 10.843 56.950 43.490 8085.498 6.434 193.443 2.440 0.86 304523. 0.5245
|
|
18.39 0.0899 0.1911 0.0899 0.0423 11.114 58.375 43.323 8287.723 6.595 192.701 2.371 0.86 304791. 0.5087
|
|
24.51 0.1198 0.2475 0.0895 0.0433 11.388 59.815 43.112 8492.131 6.758 191.764 2.303 0.86 305091. 0.4929
|
|
30.64 0.1498 0.3003 0.0889 0.0444 11.657 61.228 42.843 8692.854 6.918 190.564 2.235 0.86 305424. 0.4770
|
|
36.77 0.1798 0.3498 0.0882 0.0453 11.911 62.563 42.496 8882.337 7.068 189.020 2.170 0.86 305793. 0.4611
|
|
42.90 0.2097 0.3963 0.0873 0.0462 12.138 63.755 42.050 9051.504 7.203 187.037 2.107 0.86 306199. 0.4454
|
|
49.03 0.2397 0.4400 0.0861 0.0469 12.324 64.732 41.481 9190.210 7.313 184.509 2.047 0.86 306643. 0.4298
|
|
55.16 0.2697 0.4814 0.0846 0.0474 12.455 65.418 40.766 9287.634 7.391 181.327 1.991 0.86 307128. 0.4144
|
|
61.29 0.2996 0.5206 0.0828 0.0476 12.519 65.757 39.883 9335.751 7.429 177.401 1.938 0.86 307653. 0.3989
|
|
67.41 0.3296 0.5579 0.0806 0.0476 12.508 65.699 38.818 9327.500 7.423 172.661 1.888 0.86 308220. 0.3834
|
|
73.54 0.3595 0.5933 0.0780 0.0473 12.416 65.215 37.563 9258.850 7.368 167.081 1.840 0.86 308828. 0.3676
|
|
79.67 0.3895 0.6269 0.0750 0.0466 12.242 64.301 36.124 9129.050 7.265 160.678 1.795 0.86 309477. 0.3516
|
|
85.80 0.4195 0.6586 0.0716 0.0456 11.989 62.968 34.511 8939.891 7.114 153.507 1.751 0.86 310167. 0.3353
|
|
91.93 0.4494 0.6884 0.0680 0.0444 11.660 61.240 32.743 8694.544 6.919 145.640 1.708 0.87 310897. 0.3186
|
|
98.06 0.4794 0.7160 0.0640 0.0429 11.260 59.142 30.835 8396.658 6.682 137.156 1.666 0.87 311667. 0.3015
|
|
104.19 0.5094 0.7414 0.0598 0.0411 10.795 56.698 28.807 8049.657 6.406 128.133 1.623 0.87 312476. 0.2840
|
|
110.31 0.5393 0.7642 0.0554 0.0391 10.267 53.926 26.673 7656.042 6.092 118.642 1.580 0.87 313323. 0.2660
|
|
116.44 0.5693 0.7843 0.0508 0.0368 9.679 50.838 24.449 7217.716 5.744 108.748 1.536 0.87 314210. 0.2476
|
|
122.57 0.5992 0.8014 0.0460 0.0344 9.032 47.441 22.146 6735.419 5.360 98.505 1.491 0.87 315135. 0.2288
|
|
128.70 0.6292 0.8151 0.0411 0.0317 8.326 43.734 19.775 6209.058 4.941 87.961 1.445 0.87 316097. 0.2094
|
|
134.83 0.6592 0.8248 0.0360 0.0288 7.561 39.713 17.347 5638.284 4.487 77.158 1.395 0.88 317098. 0.1895
|
|
140.96 0.6891 0.8297 0.0309 0.0256 6.736 35.380 14.869 5023.016 3.997 66.138 1.343 0.88 318136. 0.1688
|
|
147.09 0.7191 0.8232 0.0256 0.0224 5.883 30.898 12.347 4386.714 3.491 54.921 1.277 0.88 319212. 0.1462
|
|
153.22 0.7491 0.7999 0.0203 0.0190 5.001 26.268 9.791 3729.318 2.968 43.552 1.191 0.88 320325. 0.1215
|
|
159.34 0.7790 0.7505 0.0150 0.0155 4.085 21.455 7.215 3046.042 2.424 32.091 1.074 0.88 321475. 0.0941
|
|
165.47 0.8090 0.6491 0.0096 0.0120 3.146 16.525 4.629 2346.129 1.867 20.588 0.895 0.88 322661. 0.0628
|
|
171.60 0.8389 0.4259 0.0042 0.0084 2.199 11.550 2.047 1639.839 1.305 9.103 0.566 0.89 323880. 0.0264
|
|
177.73 0.8689
|
|
|
|
|
|
|
|
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 0.0892 0.0448 14.958 72.521 50.432 11154.145 8.193 224.323 2.051 0.93 329455. 0.4747
|
|
6.66 0.0301 0.0586 0.0890 0.0457 15.256 73.967 50.319 11376.523 8.357 223.819 2.006 0.93 329683. 0.4639
|
|
13.32 0.0601 0.1145 0.0888 0.0466 15.575 75.514 50.186 11614.518 8.532 223.226 1.960 0.93 329941. 0.4526
|
|
19.99 0.0902 0.1676 0.0885 0.0476 15.912 77.145 50.025 11865.300 8.716 222.510 1.912 0.93 330231. 0.4409
|
|
26.65 0.1203 0.2177 0.0881 0.0487 16.259 78.831 49.825 12124.645 8.906 221.621 1.864 0.93 330553. 0.4289
|
|
33.31 0.1503 0.2651 0.0877 0.0497 16.610 80.533 49.572 12386.345 9.099 220.494 1.815 0.93 330912. 0.4166
|
|
39.97 0.1804 0.3096 0.0871 0.0507 16.953 82.194 49.246 12641.879 9.286 219.046 1.767 0.93 331309. 0.4042
|
|
46.63 0.2105 0.3515 0.0864 0.0517 17.273 83.744 48.825 12880.227 9.461 217.174 1.719 0.93 331746. 0.3916
|
|
53.30 0.2405 0.3909 0.0854 0.0525 17.551 85.095 48.282 13088.115 9.614 214.758 1.673 0.93 332225. 0.3790
|
|
59.96 0.2706 0.4282 0.0842 0.0532 17.769 86.152 47.588 13250.685 9.733 211.670 1.629 0.93 332747. 0.3663
|
|
66.62 0.3006 0.4635 0.0826 0.0536 17.904 86.805 46.711 13351.021 9.807 207.772 1.587 0.93 333313. 0.3536
|
|
73.28 0.3307 0.4971 0.0807 0.0537 17.938 86.967 45.630 13376.055 9.826 202.964 1.547 0.93 333925. 0.3407
|
|
79.94 0.3608 0.5292 0.0784 0.0534 17.855 86.569 44.330 13314.799 9.781 197.179 1.510 0.93 334583. 0.3278
|
|
86.61 0.3908 0.5602 0.0757 0.0528 17.647 85.560 42.805 13159.577 9.667 190.399 1.475 0.94 335286. 0.3147
|
|
93.27 0.4209 0.5900 0.0726 0.0518 17.308 83.916 41.062 12906.792 9.481 182.646 1.443 0.94 336034. 0.3014
|
|
99.93 0.4510 0.6189 0.0692 0.0504 16.839 81.640 39.112 12556.681 9.224 173.972 1.413 0.94 336827. 0.2880
|
|
106.59 0.4810 0.6469 0.0654 0.0486 16.244 78.757 36.971 12113.206 8.898 164.445 1.384 0.94 337664. 0.2744
|
|
113.25 0.5111 0.6738 0.0613 0.0465 15.533 75.311 34.655 11583.289 8.509 154.148 1.357 0.94 338546. 0.2604
|
|
119.92 0.5412 0.6993 0.0569 0.0441 14.718 71.360 32.186 10975.500 8.062 143.165 1.330 0.94 339470. 0.2460
|
|
126.58 0.5712 0.7230 0.0523 0.0413 13.811 66.958 29.582 10298.505 7.565 131.582 1.303 0.94 340438. 0.2310
|
|
133.24 0.6013 0.7444 0.0475 0.0384 12.819 62.153 26.861 9559.392 7.022 119.476 1.274 0.95 341447. 0.2153
|
|
139.90 0.6314 0.7631 0.0425 0.0352 11.751 56.973 24.037 8762.806 6.437 106.917 1.244 0.95 342499. 0.1988
|
|
146.56 0.6614 0.7781 0.0374 0.0318 10.611 51.444 21.126 7912.336 5.812 93.969 1.211 0.95 343592. 0.1815
|
|
153.23 0.6915 0.7884 0.0321 0.0281 9.402 45.586 18.143 7011.348 5.150 80.700 1.174 0.95 344726. 0.1630
|
|
159.89 0.7216 0.7878 0.0267 0.0245 8.170 39.611 15.097 6092.460 4.475 67.151 1.124 0.95 345900. 0.1424
|
|
166.55 0.7516 0.7502 0.0212 0.0212 7.090 34.373 11.975 5286.747 3.883 53.266 1.027 0.95 347115. 0.1159
|
|
173.21 0.7817 0.6742 0.0156 0.0181 6.041 29.287 8.817 4504.424 3.309 39.218 0.888 0.96 348370. 0.0859
|
|
179.88 0.8117 0.5409 0.0100 0.0150 5.010 24.289 5.649 3735.775 2.744 25.128 0.686 0.96 349665. 0.0531
|
|
186.54 0.8418 0.3095 0.0044 0.0120 4.017 19.476 2.499 2995.479 2.200 11.118 0.378 0.96 350997. 0.0195
|
|
193.20 0.8719
|
|
|
|
|
|
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