501 lines
89 KiB
Plaintext
501 lines
89 KiB
Plaintext
18x14 (18x14.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 0.0408 0.006 0.391 0.298 4.627 0.044 1.326 29.214 0.07 25339. 0.5199
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0.57 0.0332 0.0704 0.0887 0.0418 0.006 0.401 0.297 4.743 0.045 1.320 28.374 0.07 25359. 0.5038
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1.13 0.0664 0.1366 0.0882 0.0429 0.007 0.411 0.295 4.866 0.046 1.313 27.514 0.07 25382. 0.4873
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1.70 0.0997 0.1984 0.0877 0.0440 0.007 0.422 0.293 4.994 0.048 1.305 26.641 0.07 25408. 0.4703
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2.27 0.1329 0.2558 0.0870 0.0452 0.007 0.433 0.291 5.126 0.049 1.295 25.761 0.07 25437. 0.4531
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2.83 0.1661 0.3089 0.0862 0.0464 0.007 0.445 0.289 5.259 0.050 1.283 24.883 0.07 25469. 0.4357
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3.40 0.1993 0.3577 0.0853 0.0475 0.007 0.456 0.285 5.390 0.051 1.269 24.011 0.07 25505. 0.4181
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3.96 0.2326 0.4024 0.0842 0.0487 0.007 0.466 0.282 5.516 0.053 1.253 23.153 0.07 25545. 0.4005
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4.53 0.2658 0.4432 0.0828 0.0497 0.008 0.476 0.277 5.633 0.054 1.232 22.312 0.07 25588. 0.3828
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5.10 0.2990 0.4802 0.0812 0.0506 0.008 0.485 0.272 5.734 0.055 1.209 21.492 0.07 25636. 0.3652
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5.66 0.3322 0.5138 0.0793 0.0513 0.008 0.492 0.265 5.816 0.056 1.180 20.696 0.07 25688. 0.3475
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6.23 0.3655 0.5442 0.0771 0.0518 0.008 0.496 0.258 5.872 0.056 1.147 19.925 0.07 25744. 0.3299
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6.80 0.3987 0.5714 0.0745 0.0520 0.008 0.498 0.249 5.897 0.056 1.109 19.179 0.07 25804. 0.3122
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7.36 0.4319 0.5957 0.0716 0.0519 0.008 0.498 0.240 5.888 0.056 1.066 18.458 0.07 25868. 0.2945
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7.93 0.4651 0.6172 0.0684 0.0515 0.008 0.494 0.229 5.843 0.056 1.017 17.758 0.07 25937. 0.2769
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8.49 0.4984 0.6359 0.0648 0.0508 0.008 0.487 0.217 5.761 0.055 0.965 17.075 0.07 26009. 0.2592
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9.06 0.5316 0.6516 0.0610 0.0498 0.008 0.477 0.204 5.643 0.054 0.908 16.404 0.07 26086. 0.2416
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9.63 0.5648 0.6643 0.0570 0.0484 0.007 0.464 0.191 5.492 0.052 0.848 15.739 0.07 26167. 0.2240
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10.19 0.5980 0.6736 0.0527 0.0468 0.007 0.449 0.176 5.308 0.051 0.785 15.073 0.07 26252. 0.2064
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10.76 0.6313 0.6792 0.0483 0.0449 0.007 0.431 0.162 5.093 0.049 0.719 14.398 0.07 26341. 0.1887
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11.33 0.6645 0.6805 0.0438 0.0428 0.007 0.410 0.147 4.849 0.046 0.652 13.704 0.07 26434. 0.1710
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11.89 0.6977 0.6767 0.0391 0.0404 0.006 0.387 0.131 4.576 0.044 0.582 12.980 0.07 26531. 0.1531
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12.46 0.7309 0.6668 0.0344 0.0377 0.006 0.361 0.115 4.275 0.041 0.512 12.208 0.07 26632. 0.1350
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13.03 0.7642 0.6491 0.0296 0.0348 0.005 0.334 0.099 3.948 0.038 0.440 11.368 0.07 26737. 0.1166
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13.59 0.7974 0.6211 0.0247 0.0317 0.005 0.304 0.083 3.594 0.034 0.367 10.423 0.07 26845. 0.0976
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14.16 0.8306 0.5787 0.0198 0.0284 0.004 0.272 0.066 3.215 0.031 0.294 9.324 0.07 26958. 0.0781
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14.72 0.8638 0.5153 0.0148 0.0248 0.004 0.238 0.049 2.812 0.027 0.220 7.983 0.07 27074. 0.0579
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15.29 0.8971 0.4189 0.0098 0.0211 0.003 0.202 0.033 2.387 0.023 0.146 6.249 0.07 27194. 0.0369
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15.86 0.9303 0.2653 0.0049 0.0171 0.003 0.164 0.016 1.942 0.019 0.073 3.816 0.07 27318. 0.0159
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16.42 0.9635 -0.0015 0.0000 0.0130 0.002 0.125 0.000 1.479 0.014 0.000 -0.020 0.07 27445. 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 0.0894 0.0366 0.044 1.402 1.197 33.178 0.158 5.322 16.358 0.14 50679. 0.5833
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1.15 0.0338 0.0800 0.0890 0.0376 0.046 1.443 1.191 34.146 0.163 5.300 15.827 0.14 50719. 0.5632
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2.31 0.0677 0.1546 0.0886 0.0388 0.047 1.486 1.185 35.174 0.168 5.273 15.287 0.14 50765. 0.5426
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3.46 0.1015 0.2236 0.0881 0.0400 0.049 1.532 1.178 36.251 0.173 5.241 14.743 0.14 50818. 0.5217
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4.61 0.1353 0.2871 0.0874 0.0412 0.050 1.579 1.170 37.363 0.178 5.203 14.199 0.14 50877. 0.5006
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5.77 0.1691 0.3453 0.0866 0.0424 0.052 1.627 1.159 38.490 0.184 5.156 13.660 0.14 50944. 0.4794
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6.92 0.2030 0.3983 0.0857 0.0437 0.053 1.674 1.147 39.607 0.189 5.100 13.130 0.14 51018. 0.4583
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8.07 0.2368 0.4463 0.0845 0.0448 0.055 1.719 1.131 40.681 0.194 5.032 12.612 0.14 51099. 0.4373
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9.23 0.2706 0.4898 0.0832 0.0459 0.056 1.761 1.113 41.677 0.199 4.950 12.110 0.14 51189. 0.4164
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10.38 0.3044 0.5290 0.0815 0.0469 0.057 1.798 1.091 42.551 0.203 4.851 11.626 0.14 51288. 0.3958
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11.53 0.3383 0.5642 0.0795 0.0477 0.058 1.828 1.064 43.257 0.207 4.734 11.161 0.14 51395. 0.3754
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12.69 0.3721 0.5959 0.0772 0.0482 0.059 1.849 1.034 43.749 0.209 4.597 10.716 0.14 51510. 0.3551
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13.84 0.4059 0.6243 0.0746 0.0485 0.059 1.859 0.998 43.983 0.210 4.439 10.291 0.14 51635. 0.3351
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14.99 0.4397 0.6496 0.0715 0.0484 0.059 1.856 0.957 43.926 0.210 4.258 9.885 0.14 51768. 0.3153
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16.14 0.4736 0.6721 0.0682 0.0480 0.058 1.841 0.912 43.562 0.208 4.057 9.496 0.14 51909. 0.2956
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17.30 0.5074 0.6918 0.0645 0.0473 0.058 1.813 0.863 42.892 0.205 3.837 9.123 0.14 52060. 0.2762
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18.45 0.5412 0.7087 0.0605 0.0462 0.056 1.772 0.810 41.922 0.200 3.602 8.762 0.14 52219. 0.2570
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19.60 0.5751 0.7227 0.0563 0.0448 0.055 1.718 0.754 40.664 0.194 3.353 8.409 0.15 52386. 0.2380
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20.76 0.6089 0.7336 0.0520 0.0431 0.052 1.654 0.695 39.129 0.187 3.093 8.062 0.15 52561. 0.2192
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21.91 0.6427 0.7411 0.0474 0.0411 0.050 1.577 0.635 37.327 0.178 2.824 7.715 0.15 52745. 0.2004
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23.06 0.6765 0.7446 0.0428 0.0389 0.047 1.490 0.573 35.268 0.168 2.547 7.364 0.15 52938. 0.1816
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24.22 0.7104 0.7434 0.0380 0.0363 0.044 1.393 0.509 32.958 0.157 2.263 7.002 0.15 53138. 0.1628
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25.37 0.7442 0.7364 0.0332 0.0335 0.041 1.285 0.444 30.404 0.145 1.974 6.621 0.15 53347. 0.1438
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26.52 0.7780 0.7217 0.0282 0.0304 0.037 1.167 0.378 27.614 0.132 1.681 6.207 0.15 53563. 0.1244
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27.68 0.8118 0.6964 0.0233 0.0271 0.033 1.039 0.311 24.595 0.117 1.384 5.739 0.15 53788. 0.1044
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28.83 0.8457 0.6552 0.0182 0.0235 0.029 0.903 0.244 21.357 0.102 1.086 5.184 0.15 54020. 0.0835
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29.98 0.8795 0.5884 0.0132 0.0197 0.024 0.757 0.177 17.912 0.086 0.786 4.477 0.15 54261. 0.0614
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31.14 0.9133 0.4753 0.0082 0.0157 0.019 0.603 0.110 14.277 0.068 0.488 3.482 0.15 54509. 0.0376
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32.29 0.9471 0.2632 0.0032 0.0115 0.014 0.443 0.043 10.471 0.050 0.191 1.859 0.15 54764. 0.0126
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33.44 0.9810
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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 0.0896 0.0349 0.143 3.009 2.699 106.796 0.340 12.004 11.462 0.21 76017. 0.6138
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1.73 0.0337 0.0838 0.0893 0.0360 0.148 3.102 2.688 110.089 0.350 11.956 11.075 0.21 76078. 0.5919
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3.45 0.0675 0.1616 0.0888 0.0371 0.152 3.200 2.675 113.594 0.362 11.899 10.681 0.21 76147. 0.5695
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5.18 0.1012 0.2334 0.0883 0.0383 0.157 3.304 2.660 117.275 0.373 11.830 10.286 0.21 76226. 0.5469
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6.90 0.1350 0.2993 0.0877 0.0396 0.162 3.411 2.641 121.084 0.385 11.747 9.893 0.21 76314. 0.5241
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8.63 0.1687 0.3595 0.0870 0.0408 0.168 3.521 2.618 124.957 0.398 11.646 9.504 0.21 76413. 0.5013
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10.35 0.2025 0.4140 0.0860 0.0421 0.173 3.629 2.591 128.807 0.410 11.524 9.123 0.21 76524. 0.4787
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12.08 0.2362 0.4634 0.0849 0.0433 0.178 3.734 2.557 132.531 0.422 11.375 8.752 0.21 76646. 0.4562
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13.80 0.2699 0.5079 0.0836 0.0444 0.182 3.832 2.517 136.003 0.433 11.194 8.393 0.21 76780. 0.4341
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15.53 0.3037 0.5479 0.0820 0.0454 0.187 3.918 2.468 139.081 0.443 10.978 8.049 0.22 76927. 0.4122
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17.25 0.3374 0.5839 0.0800 0.0463 0.190 3.990 2.410 141.608 0.451 10.720 7.719 0.22 77087. 0.3906
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18.98 0.3712 0.6162 0.0778 0.0468 0.192 4.041 2.342 143.423 0.457 10.416 7.405 0.22 77260. 0.3694
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20.71 0.4049 0.6451 0.0751 0.0472 0.194 4.068 2.262 144.375 0.460 10.063 7.107 0.22 77445. 0.3485
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22.43 0.4386 0.6710 0.0721 0.0471 0.194 4.067 2.172 144.348 0.459 9.660 6.824 0.22 77644. 0.3278
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24.16 0.4724 0.6942 0.0688 0.0468 0.192 4.037 2.071 143.284 0.456 9.211 6.555 0.22 77856. 0.3075
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25.88 0.5061 0.7146 0.0651 0.0461 0.189 3.977 1.960 141.172 0.449 8.719 6.298 0.22 78080. 0.2875
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27.61 0.5399 0.7324 0.0612 0.0451 0.185 3.889 1.842 138.035 0.439 8.192 6.052 0.22 78317. 0.2677
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29.33 0.5736 0.7475 0.0570 0.0437 0.180 3.773 1.716 133.907 0.426 7.634 5.813 0.22 78567. 0.2483
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31.06 0.6074 0.7598 0.0526 0.0421 0.173 3.630 1.585 128.824 0.410 7.050 5.581 0.22 78830. 0.2290
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32.78 0.6411 0.7690 0.0481 0.0401 0.165 3.460 1.449 122.820 0.391 6.445 5.351 0.22 79104. 0.2100
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34.51 0.6748 0.7748 0.0435 0.0379 0.155 3.266 1.309 115.923 0.369 5.822 5.121 0.22 79391. 0.1910
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36.23 0.7086 0.7764 0.0387 0.0353 0.145 3.047 1.166 108.157 0.344 5.184 4.888 0.22 79691. 0.1720
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37.96 0.7423 0.7730 0.0339 0.0325 0.133 2.805 1.019 99.546 0.317 4.534 4.645 0.22 80002. 0.1529
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39.69 0.7761 0.7629 0.0289 0.0294 0.121 2.539 0.871 90.112 0.287 3.875 4.385 0.22 80325. 0.1334
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41.41 0.8098 0.7435 0.0240 0.0261 0.107 2.251 0.721 79.882 0.254 3.208 4.096 0.22 80661. 0.1134
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43.14 0.8435 0.7102 0.0189 0.0225 0.092 1.941 0.570 68.887 0.219 2.537 3.756 0.22 81008. 0.0925
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44.86 0.8773 0.6539 0.0139 0.0187 0.077 1.611 0.419 57.171 0.182 1.864 3.325 0.22 81367. 0.0702
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46.59 0.9110 0.5543 0.0089 0.0146 0.060 1.262 0.268 44.788 0.143 1.192 2.714 0.22 81737. 0.0458
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48.31 0.9448 0.3565 0.0039 0.0104 0.043 0.896 0.118 31.807 0.101 0.525 1.683 0.22 82119. 0.0189
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50.04 0.9785 -0.1915 -0.0011 0.0058 0.024 0.504 -0.034 17.877 0.057 -0.153 -0.873 0.22 82460. 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 0.0898 0.0340 0.331 5.213 4.809 246.723 0.589 21.391 8.841 0.29 101355. 0.6320
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2.29 0.0336 0.0857 0.0895 0.0351 0.341 5.379 4.791 254.545 0.608 21.311 8.537 0.29 101435. 0.6091
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4.58 0.0671 0.1651 0.0891 0.0362 0.353 5.555 4.770 262.884 0.628 21.215 8.229 0.29 101527. 0.5859
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6.87 0.1007 0.2384 0.0886 0.0374 0.364 5.740 4.744 271.659 0.649 21.100 7.920 0.29 101631. 0.5623
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9.15 0.1343 0.3055 0.0880 0.0387 0.377 5.933 4.712 280.763 0.670 20.960 7.612 0.29 101748. 0.5387
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11.44 0.1678 0.3666 0.0873 0.0400 0.389 6.129 4.674 290.043 0.692 20.789 7.309 0.29 101879. 0.5151
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13.73 0.2014 0.4221 0.0864 0.0412 0.401 6.325 4.627 299.306 0.715 20.580 7.012 0.29 102025. 0.4916
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16.02 0.2350 0.4721 0.0854 0.0425 0.413 6.515 4.570 308.305 0.736 20.326 6.723 0.29 102187. 0.4685
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18.31 0.2685 0.5172 0.0841 0.0436 0.425 6.693 4.500 316.749 0.756 20.017 6.444 0.29 102364. 0.4456
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20.60 0.3021 0.5577 0.0825 0.0447 0.435 6.853 4.416 324.301 0.774 19.644 6.177 0.29 102558. 0.4231
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22.89 0.3357 0.5941 0.0806 0.0456 0.443 6.986 4.316 330.590 0.789 19.197 5.921 0.29 102769. 0.4010
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25.17 0.3692 0.6267 0.0784 0.0462 0.450 7.084 4.197 335.230 0.800 18.669 5.679 0.29 102997. 0.3793
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27.46 0.4028 0.6560 0.0758 0.0466 0.453 7.139 4.059 337.857 0.807 18.054 5.449 0.29 103243. 0.3579
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29.75 0.4364 0.6824 0.0729 0.0466 0.454 7.146 3.901 338.182 0.807 17.350 5.232 0.29 103505. 0.3368
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32.04 0.4699 0.7059 0.0696 0.0463 0.451 7.101 3.724 336.046 0.802 16.562 5.026 0.29 103785. 0.3161
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34.33 0.5035 0.7269 0.0659 0.0457 0.444 7.003 3.529 331.415 0.791 15.698 4.830 0.29 104081. 0.2958
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36.62 0.5370 0.7454 0.0620 0.0447 0.435 6.853 3.320 324.328 0.774 14.768 4.643 0.29 104395. 0.2758
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38.91 0.5706 0.7613 0.0579 0.0434 0.422 6.653 3.099 314.864 0.752 13.783 4.464 0.29 104725. 0.2561
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41.19 0.6042 0.7747 0.0536 0.0418 0.406 6.405 2.867 303.106 0.724 12.750 4.290 0.29 105072. 0.2367
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43.48 0.6377 0.7852 0.0491 0.0398 0.388 6.110 2.626 289.131 0.690 11.679 4.119 0.29 105435. 0.2176
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45.77 0.6713 0.7926 0.0444 0.0376 0.366 5.769 2.377 273.007 0.652 10.575 3.950 0.29 105814. 0.1985
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48.06 0.7049 0.7963 0.0397 0.0351 0.342 5.384 2.123 254.793 0.608 9.444 3.780 0.29 106209. 0.1795
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50.35 0.7384 0.7956 0.0348 0.0323 0.315 4.956 1.864 234.541 0.560 8.291 3.605 0.29 106620. 0.1604
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52.64 0.7720 0.7892 0.0299 0.0293 0.285 4.486 1.601 212.306 0.507 7.120 3.420 0.29 107048. 0.1410
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54.93 0.8056 0.7747 0.0249 0.0259 0.252 3.976 1.335 188.149 0.449 5.936 3.217 0.29 107491. 0.1212
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57.21 0.8391 0.7482 0.0199 0.0223 0.217 3.426 1.066 162.143 0.387 4.743 2.983 0.30 107949. 0.1004
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59.50 0.8727 0.7020 0.0149 0.0185 0.180 2.840 0.797 134.386 0.321 3.547 2.691 0.30 108423. 0.0783
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61.79 0.9063 0.6185 0.0099 0.0145 0.141 2.219 0.529 105.004 0.251 2.351 2.283 0.30 108912. 0.0541
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64.08 0.9398 0.4494 0.0049 0.0102 0.099 1.567 0.262 74.157 0.177 1.163 1.600 0.30 109416. 0.0267
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66.37 0.9734 -0.0104 -0.0001 0.0058 0.056 0.885 -0.003 41.900 0.100 -0.015 -0.036 0.30 109926. 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 0.0901 0.0335 0.637 8.028 7.533 474.892 0.907 33.509 7.195 0.36 126691. 0.6438
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2.86 0.0336 0.0872 0.0898 0.0346 0.657 8.288 7.507 490.276 0.936 33.392 6.945 0.36 126792. 0.6203
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5.73 0.0672 0.1680 0.0894 0.0358 0.680 8.566 7.476 506.710 0.968 33.251 6.692 0.36 126906. 0.5964
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8.59 0.1008 0.2424 0.0889 0.0370 0.703 8.859 7.437 524.045 1.001 33.082 6.437 0.36 127036. 0.5723
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11.45 0.1344 0.3105 0.0884 0.0382 0.727 9.164 7.391 542.076 1.035 32.875 6.184 0.36 127183. 0.5481
|
|
14.31 0.1680 0.3724 0.0877 0.0395 0.752 9.475 7.334 560.510 1.070 32.621 5.935 0.36 127347. 0.5239
|
|
17.18 0.2015 0.4285 0.0868 0.0408 0.776 9.787 7.264 578.964 1.106 32.308 5.690 0.36 127530. 0.4999
|
|
20.04 0.2351 0.4791 0.0858 0.0421 0.801 10.091 7.177 596.956 1.140 31.924 5.453 0.36 127732. 0.4762
|
|
22.90 0.2687 0.5246 0.0846 0.0433 0.823 10.378 7.072 613.905 1.172 31.454 5.225 0.36 127954. 0.4529
|
|
25.77 0.3023 0.5654 0.0830 0.0444 0.844 10.635 6.943 629.138 1.202 30.884 5.006 0.36 128197. 0.4300
|
|
28.63 0.3359 0.6021 0.0812 0.0453 0.861 10.851 6.789 641.913 1.226 30.198 4.797 0.36 128461. 0.4074
|
|
31.49 0.3695 0.6349 0.0790 0.0460 0.874 11.012 6.606 651.453 1.244 29.382 4.599 0.36 128746. 0.3853
|
|
34.35 0.4031 0.6645 0.0764 0.0464 0.881 11.107 6.391 657.020 1.255 28.427 4.412 0.36 129054. 0.3636
|
|
37.22 0.4367 0.6910 0.0735 0.0464 0.882 11.124 6.144 658.027 1.257 27.330 4.235 0.36 129382. 0.3422
|
|
40.08 0.4703 0.7149 0.0702 0.0462 0.877 11.058 5.867 654.141 1.249 26.098 4.068 0.36 129733. 0.3212
|
|
42.94 0.5039 0.7362 0.0665 0.0455 0.865 10.908 5.563 645.281 1.232 24.745 3.910 0.36 130104. 0.3007
|
|
45.81 0.5375 0.7550 0.0626 0.0446 0.847 10.676 5.235 631.521 1.206 23.286 3.760 0.36 130497. 0.2804
|
|
48.67 0.5711 0.7715 0.0584 0.0433 0.822 10.363 4.887 613.011 1.171 21.737 3.616 0.36 130910. 0.2606
|
|
51.53 0.6046 0.7854 0.0541 0.0416 0.791 9.972 4.522 589.917 1.127 20.113 3.477 0.36 131344. 0.2410
|
|
54.40 0.6382 0.7967 0.0495 0.0397 0.754 9.507 4.143 562.393 1.074 18.426 3.341 0.36 131799. 0.2217
|
|
57.26 0.6718 0.8051 0.0449 0.0374 0.712 8.969 3.752 530.575 1.013 16.688 3.207 0.37 132274. 0.2025
|
|
60.12 0.7054 0.8100 0.0401 0.0349 0.663 8.361 3.351 494.578 0.945 14.906 3.073 0.37 132769. 0.1834
|
|
62.98 0.7390 0.8108 0.0352 0.0321 0.610 7.683 2.943 454.511 0.868 13.089 2.937 0.37 133284. 0.1642
|
|
65.85 0.7726 0.8063 0.0302 0.0290 0.550 6.939 2.528 410.479 0.784 11.244 2.793 0.37 133819. 0.1448
|
|
68.71 0.8062 0.7943 0.0252 0.0256 0.486 6.130 2.108 362.604 0.693 9.377 2.637 0.37 134373. 0.1248
|
|
71.57 0.8398 0.7711 0.0202 0.0219 0.417 5.258 1.685 311.035 0.594 7.496 2.458 0.37 134947. 0.1040
|
|
74.44 0.8734 0.7291 0.0151 0.0181 0.343 4.327 1.261 255.964 0.489 5.609 2.234 0.37 135541. 0.0818
|
|
77.30 0.9070 0.6509 0.0100 0.0139 0.265 3.341 0.837 197.644 0.377 3.723 1.921 0.37 136153. 0.0573
|
|
80.16 0.9406 0.4860 0.0050 0.0096 0.183 2.306 0.416 136.397 0.260 1.850 1.383 0.37 136784. 0.0291
|
|
83.02 0.9741 -0.0048 0.0000 0.0051 0.097 1.222 -0.002 72.296 0.138 -0.009 -0.013 0.37 137421. 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 0.0903 0.0333 1.092 11.472 10.879 814.388 1.296 48.389 6.059 0.43 152027. 0.6514
|
|
3.44 0.0336 0.0882 0.0900 0.0343 1.128 11.849 10.844 841.137 1.339 48.234 5.847 0.43 152147. 0.6277
|
|
6.88 0.0673 0.1698 0.0897 0.0355 1.166 12.253 10.802 869.783 1.384 48.048 5.633 0.43 152285. 0.6035
|
|
10.32 0.1009 0.2450 0.0893 0.0368 1.207 12.680 10.751 900.085 1.433 47.822 5.418 0.43 152441. 0.5791
|
|
13.76 0.1345 0.3138 0.0888 0.0380 1.249 13.125 10.689 931.698 1.483 47.544 5.204 0.43 152617. 0.5546
|
|
17.19 0.1681 0.3763 0.0881 0.0394 1.293 13.582 10.612 964.126 1.534 47.201 4.992 0.43 152814. 0.5301
|
|
20.63 0.2018 0.4329 0.0873 0.0407 1.337 14.041 10.516 996.708 1.586 46.774 4.785 0.43 153033. 0.5059
|
|
24.07 0.2354 0.4838 0.0863 0.0420 1.379 14.490 10.397 1028.598 1.637 46.246 4.585 0.43 153276. 0.4819
|
|
27.51 0.2690 0.5296 0.0851 0.0432 1.420 14.915 10.250 1058.771 1.685 45.594 4.391 0.43 153543. 0.4583
|
|
30.95 0.3026 0.5707 0.0836 0.0443 1.456 15.299 10.071 1086.032 1.728 44.796 4.206 0.43 153834. 0.4351
|
|
34.39 0.3363 0.6075 0.0818 0.0453 1.487 15.623 9.853 1109.053 1.765 43.828 4.030 0.43 154152. 0.4123
|
|
37.83 0.3699 0.6406 0.0797 0.0460 1.511 15.868 9.593 1126.443 1.793 42.670 3.863 0.43 154495. 0.3900
|
|
41.27 0.4035 0.6703 0.0771 0.0464 1.525 16.015 9.286 1136.870 1.809 41.306 3.705 0.43 154865. 0.3680
|
|
44.71 0.4371 0.6970 0.0742 0.0465 1.528 16.049 8.933 1139.268 1.813 39.733 3.556 0.43 155260. 0.3465
|
|
48.15 0.4708 0.7211 0.0709 0.0463 1.519 15.961 8.534 1133.022 1.803 37.959 3.416 0.43 155682. 0.3253
|
|
51.58 0.5044 0.7426 0.0672 0.0456 1.499 15.749 8.094 1117.963 1.779 36.004 3.284 0.43 156129. 0.3046
|
|
55.02 0.5380 0.7619 0.0633 0.0447 1.467 15.414 7.619 1094.216 1.741 33.891 3.158 0.43 156601. 0.2842
|
|
58.46 0.5716 0.7787 0.0591 0.0434 1.424 14.961 7.114 1062.044 1.690 31.645 3.038 0.44 157098. 0.2642
|
|
61.90 0.6053 0.7932 0.0547 0.0417 1.370 14.393 6.584 1021.743 1.626 29.287 2.923 0.44 157620. 0.2445
|
|
65.34 0.6389 0.8051 0.0501 0.0398 1.306 13.715 6.033 973.592 1.550 26.835 2.811 0.44 158167. 0.2250
|
|
68.78 0.6725 0.8142 0.0454 0.0375 1.231 12.930 5.464 917.833 1.461 24.306 2.700 0.44 158739. 0.2058
|
|
72.22 0.7061 0.8201 0.0405 0.0349 1.146 12.040 4.881 854.678 1.360 21.712 2.590 0.44 159334. 0.1866
|
|
75.66 0.7398 0.8222 0.0356 0.0320 1.052 11.049 4.286 784.315 1.248 19.066 2.479 0.44 159953. 0.1673
|
|
79.10 0.7734 0.8192 0.0306 0.0289 0.948 9.959 3.682 706.935 1.125 16.378 2.362 0.44 160597. 0.1478
|
|
82.53 0.8070 0.8092 0.0255 0.0254 0.835 8.773 3.071 622.753 0.991 13.658 2.236 0.44 161264. 0.1277
|
|
85.97 0.8406 0.7886 0.0204 0.0217 0.713 7.495 2.454 532.030 0.847 10.916 2.092 0.44 161954. 0.1068
|
|
89.41 0.8743 0.7500 0.0152 0.0178 0.583 6.129 1.835 435.110 0.692 8.164 1.913 0.44 162668. 0.0845
|
|
92.85 0.9079 0.6760 0.0101 0.0136 0.446 4.683 1.217 332.442 0.529 5.414 1.661 0.45 163404. 0.0597
|
|
96.29 0.9415 0.5140 0.0050 0.0092 0.301 3.164 0.603 224.601 0.357 2.682 1.218 0.45 164162. 0.0308
|
|
99.73 0.9751 -0.0129 -0.0001 0.0046 0.150 1.572 -0.007 111.583 0.178 -0.032 -0.029 0.45 164924. 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 0.0906 0.0332 1.730 15.576 14.853 1289.952 1.760 66.065 5.223 0.50 177360. 0.6561
|
|
4.02 0.0337 0.0887 0.0903 0.0343 1.787 16.091 14.810 1332.638 1.818 65.876 5.041 0.50 177501. 0.6324
|
|
8.03 0.0673 0.1710 0.0900 0.0354 1.849 16.645 14.759 1378.490 1.881 65.648 4.856 0.50 177661. 0.6082
|
|
12.05 0.1010 0.2467 0.0897 0.0367 1.914 17.232 14.697 1427.154 1.947 65.370 4.671 0.50 177843. 0.5837
|
|
16.06 0.1346 0.3159 0.0892 0.0380 1.982 17.848 14.619 1478.110 2.016 65.026 4.486 0.50 178048. 0.5591
|
|
20.08 0.1683 0.3788 0.0886 0.0394 2.053 18.481 14.522 1530.593 2.088 64.596 4.304 0.50 178278. 0.5346
|
|
24.09 0.2019 0.4357 0.0879 0.0407 2.124 19.121 14.401 1583.555 2.160 64.056 4.125 0.50 178534. 0.5103
|
|
28.11 0.2356 0.4869 0.0869 0.0421 2.193 19.750 14.249 1635.644 2.231 63.380 3.951 0.50 178817. 0.4862
|
|
32.12 0.2692 0.5329 0.0858 0.0433 2.260 20.348 14.059 1685.191 2.299 62.535 3.784 0.50 179129. 0.4625
|
|
36.14 0.3029 0.5741 0.0843 0.0445 2.320 20.892 13.824 1730.236 2.360 61.490 3.624 0.50 179470. 0.4392
|
|
40.15 0.3365 0.6111 0.0826 0.0455 2.372 21.355 13.537 1768.581 2.413 60.211 3.472 0.50 179841. 0.4164
|
|
44.17 0.3702 0.6443 0.0805 0.0462 2.411 21.709 13.189 1797.916 2.453 58.667 3.327 0.50 180242. 0.3939
|
|
48.18 0.4038 0.6741 0.0779 0.0467 2.435 21.928 12.778 1816.020 2.477 56.835 3.191 0.50 180674. 0.3719
|
|
52.20 0.4375 0.7010 0.0750 0.0468 2.442 21.989 12.299 1821.089 2.484 54.708 3.063 0.50 181136. 0.3502
|
|
56.21 0.4711 0.7253 0.0717 0.0466 2.430 21.880 11.757 1812.064 2.472 52.297 2.943 0.51 181629. 0.3290
|
|
60.23 0.5048 0.7471 0.0681 0.0460 2.399 21.597 11.158 1788.632 2.440 49.630 2.829 0.51 182152. 0.3081
|
|
64.25 0.5384 0.7666 0.0641 0.0450 2.348 21.142 10.508 1750.980 2.389 46.738 2.722 0.51 182704. 0.2876
|
|
68.26 0.5721 0.7839 0.0599 0.0437 2.279 20.521 9.815 1699.535 2.318 43.657 2.619 0.51 183286. 0.2675
|
|
72.28 0.6057 0.7988 0.0554 0.0420 2.192 19.740 9.086 1634.792 2.230 40.416 2.521 0.51 183896. 0.2477
|
|
76.29 0.6394 0.8113 0.0508 0.0400 2.088 18.803 8.328 1557.223 2.124 37.042 2.426 0.51 184536. 0.2282
|
|
80.31 0.6730 0.8211 0.0460 0.0377 1.968 17.716 7.545 1467.237 2.002 33.558 2.332 0.51 185204. 0.2088
|
|
84.32 0.7067 0.8279 0.0411 0.0351 1.831 16.484 6.741 1365.187 1.862 29.983 2.240 0.51 185900. 0.1895
|
|
88.34 0.7404 0.8310 0.0361 0.0322 1.678 15.110 5.920 1251.389 1.707 26.333 2.146 0.51 186624. 0.1702
|
|
92.35 0.7740 0.8294 0.0310 0.0290 1.510 13.598 5.086 1126.154 1.536 22.623 2.048 0.51 187376. 0.1506
|
|
96.37 0.8077 0.8211 0.0259 0.0255 1.327 11.952 4.241 989.832 1.350 18.866 1.944 0.52 188155. 0.1305
|
|
100.38 0.8413 0.8028 0.0207 0.0217 1.130 10.177 3.390 842.851 1.150 15.078 1.824 0.52 188962. 0.1095
|
|
104.40 0.8750 0.7673 0.0155 0.0176 0.920 8.280 2.535 685.769 0.936 11.274 1.676 0.52 189796. 0.0870
|
|
108.41 0.9086 0.6974 0.0102 0.0134 0.696 6.271 1.680 519.321 0.708 7.473 1.467 0.52 190657. 0.0620
|
|
112.43 0.9423 0.5391 0.0051 0.0089 0.462 4.159 0.831 344.451 0.470 3.694 1.094 0.52 191543. 0.0325
|
|
116.45 0.9759 -0.0210 -0.0001 0.0041 0.216 1.943 -0.015 160.919 0.220 -0.065 -0.041 0.52 192429. 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 0.0909 0.0332 2.586 20.377 19.464 1928.663 2.302 86.576 4.577 0.57 202692. 0.6583
|
|
4.62 0.0339 0.0895 0.0907 0.0343 2.673 21.057 19.415 1993.021 2.379 86.359 4.418 0.57 202853. 0.6347
|
|
9.24 0.0678 0.1725 0.0904 0.0355 2.766 21.790 19.356 2062.420 2.462 86.097 4.257 0.57 203038. 0.6105
|
|
13.86 0.1017 0.2489 0.0901 0.0368 2.865 22.572 19.284 2136.390 2.550 85.774 4.094 0.57 203247. 0.5861
|
|
18.49 0.1356 0.3186 0.0896 0.0381 2.969 23.394 19.193 2214.191 2.643 85.372 3.932 0.57 203484. 0.5615
|
|
23.11 0.1695 0.3820 0.0891 0.0395 3.077 24.244 19.079 2294.702 2.739 84.862 3.771 0.57 203749. 0.5369
|
|
27.73 0.2034 0.4393 0.0884 0.0409 3.187 25.107 18.933 2376.342 2.837 84.212 3.614 0.57 204044. 0.5126
|
|
32.35 0.2372 0.4908 0.0876 0.0423 3.295 25.959 18.747 2457.021 2.933 83.385 3.461 0.57 204371. 0.4884
|
|
36.97 0.2711 0.5370 0.0865 0.0437 3.398 26.774 18.511 2534.121 3.025 82.337 3.313 0.57 204732. 0.4647
|
|
41.59 0.3050 0.5784 0.0851 0.0449 3.493 27.518 18.215 2604.520 3.109 81.019 3.172 0.57 205126. 0.4413
|
|
46.22 0.3389 0.6155 0.0834 0.0459 3.573 28.153 17.847 2664.693 3.181 79.383 3.038 0.57 205555. 0.4183
|
|
50.84 0.3728 0.6488 0.0813 0.0467 3.635 28.642 17.398 2710.919 3.236 77.386 2.911 0.58 206020. 0.3958
|
|
55.46 0.4067 0.6787 0.0787 0.0472 3.674 28.945 16.860 2739.629 3.270 74.994 2.791 0.58 206520. 0.3736
|
|
60.08 0.4406 0.7057 0.0758 0.0473 3.685 29.033 16.231 2747.931 3.280 72.196 2.679 0.58 207055. 0.3518
|
|
64.70 0.4745 0.7300 0.0725 0.0471 3.667 28.887 15.514 2734.160 3.264 69.007 2.574 0.58 207626. 0.3305
|
|
69.32 0.5084 0.7520 0.0687 0.0465 3.618 28.503 14.718 2697.831 3.220 65.465 2.474 0.58 208232. 0.3094
|
|
73.95 0.5423 0.7717 0.0647 0.0455 3.539 27.885 13.852 2639.265 3.150 61.615 2.381 0.58 208872. 0.2888
|
|
78.57 0.5762 0.7892 0.0604 0.0441 3.432 27.038 12.928 2559.161 3.055 57.505 2.291 0.58 209547. 0.2686
|
|
83.19 0.6101 0.8044 0.0558 0.0423 3.297 25.973 11.955 2458.323 2.934 53.176 2.206 0.58 210254. 0.2486
|
|
87.81 0.6439 0.8173 0.0511 0.0403 3.135 24.697 10.941 2337.515 2.790 48.665 2.123 0.58 210995. 0.2289
|
|
92.43 0.6778 0.8275 0.0462 0.0379 2.947 23.216 9.893 2197.402 2.623 44.004 2.042 0.58 211769. 0.2094
|
|
97.05 0.7117 0.8347 0.0412 0.0351 2.734 21.538 8.817 2038.552 2.433 39.218 1.962 0.59 212576. 0.1899
|
|
101.68 0.7456 0.8383 0.0360 0.0321 2.496 19.667 7.718 1861.472 2.222 34.330 1.881 0.59 213415. 0.1703
|
|
106.30 0.7795 0.8371 0.0308 0.0287 2.235 17.609 6.601 1666.660 1.989 29.360 1.796 0.59 214286. 0.1504
|
|
110.92 0.8134 0.8292 0.0255 0.0251 1.951 15.369 5.469 1454.675 1.736 24.327 1.705 0.59 215189. 0.1300
|
|
115.54 0.8473 0.8109 0.0202 0.0211 1.644 12.955 4.328 1226.212 1.464 19.251 1.601 0.59 216123. 0.1086
|
|
120.16 0.8812 0.7742 0.0149 0.0169 1.317 10.377 3.182 982.185 1.172 14.155 1.470 0.59 217089. 0.0855
|
|
124.78 0.9151 0.6986 0.0095 0.0125 0.971 7.647 2.038 723.802 0.864 9.065 1.277 0.59 218085. 0.0594
|
|
129.41 0.9490 0.5123 0.0042 0.0078 0.607 4.782 0.901 452.591 0.540 4.008 0.903 0.60 219111. 0.0279
|
|
134.03 0.9829
|
|
|
|
|
|
|
|
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 0.0912 0.0335 3.712 25.995 24.720 2767.988 2.937 109.954 4.051 0.64 228021. 0.6565
|
|
5.17 0.0337 0.0888 0.0910 0.0346 3.833 26.846 24.668 2858.565 3.033 109.723 3.914 0.64 228202. 0.6337
|
|
10.35 0.0674 0.1712 0.0908 0.0358 3.965 27.767 24.606 2956.598 3.137 109.446 3.775 0.64 228408. 0.6104
|
|
15.52 0.1012 0.2472 0.0905 0.0370 4.106 28.752 24.529 3061.548 3.248 109.105 3.634 0.64 228641. 0.5867
|
|
20.69 0.1349 0.3168 0.0902 0.0384 4.254 29.794 24.433 3172.521 3.366 108.676 3.493 0.64 228905. 0.5628
|
|
25.86 0.1686 0.3802 0.0897 0.0398 4.409 30.880 24.309 3288.082 3.489 108.126 3.353 0.64 229200. 0.5389
|
|
31.04 0.2023 0.4375 0.0891 0.0412 4.568 31.988 24.149 3406.147 3.614 107.415 3.216 0.64 229529. 0.5151
|
|
36.21 0.2360 0.4892 0.0884 0.0426 4.726 33.094 23.942 3523.869 3.739 106.493 3.082 0.64 229893. 0.4915
|
|
41.38 0.2697 0.5355 0.0874 0.0440 4.878 34.162 23.674 3637.585 3.860 105.303 2.952 0.64 230295. 0.4682
|
|
46.55 0.3035 0.5771 0.0861 0.0453 5.019 35.150 23.332 3742.812 3.971 103.781 2.827 0.65 230734. 0.4452
|
|
51.73 0.3372 0.6143 0.0845 0.0464 5.142 36.010 22.900 3834.379 4.068 101.859 2.709 0.65 231212. 0.4226
|
|
56.90 0.3709 0.6477 0.0825 0.0473 5.239 36.689 22.364 3906.711 4.145 99.475 2.596 0.65 231730. 0.4003
|
|
62.07 0.4046 0.6777 0.0801 0.0478 5.303 37.137 21.713 3954.332 4.196 96.581 2.491 0.65 232287. 0.3783
|
|
67.24 0.4383 0.7049 0.0773 0.0481 5.327 37.309 20.943 3972.658 4.215 93.154 2.391 0.65 232885. 0.3567
|
|
72.42 0.4721 0.7295 0.0740 0.0479 5.309 37.179 20.056 3958.854 4.200 89.208 2.298 0.65 233522. 0.3354
|
|
77.59 0.5058 0.7518 0.0703 0.0473 5.246 36.739 19.062 3911.954 4.151 84.787 2.210 0.65 234198. 0.3146
|
|
82.76 0.5395 0.7719 0.0663 0.0464 5.139 35.991 17.975 3832.298 4.066 79.951 2.127 0.65 234912. 0.2940
|
|
87.94 0.5732 0.7898 0.0620 0.0450 4.990 34.944 16.808 3720.879 3.948 74.761 2.049 0.65 235664. 0.2738
|
|
93.11 0.6069 0.8056 0.0575 0.0433 4.799 33.611 15.574 3578.914 3.797 69.272 1.974 0.65 236454. 0.2539
|
|
98.28 0.6406 0.8192 0.0527 0.0412 4.570 32.002 14.284 3407.583 3.616 63.536 1.901 0.66 237281. 0.2342
|
|
103.45 0.6744 0.8303 0.0478 0.0388 4.302 30.127 12.948 3207.938 3.404 57.594 1.831 0.66 238145. 0.2147
|
|
108.63 0.7081 0.8387 0.0427 0.0361 3.997 27.995 11.574 2980.872 3.163 51.481 1.761 0.66 239044. 0.1953
|
|
113.80 0.7418 0.8437 0.0375 0.0330 3.657 25.612 10.168 2727.164 2.894 45.228 1.691 0.66 239980. 0.1758
|
|
118.97 0.7755 0.8444 0.0322 0.0296 3.282 22.986 8.736 2447.546 2.597 38.860 1.619 0.66 240952. 0.1560
|
|
124.14 0.8092 0.8392 0.0269 0.0259 2.874 20.124 7.285 2142.808 2.274 32.402 1.542 0.66 241959. 0.1357
|
|
129.32 0.8430 0.8248 0.0215 0.0219 2.433 17.035 5.819 1813.923 1.925 25.881 1.455 0.67 243001. 0.1144
|
|
134.49 0.8767 0.7946 0.0160 0.0177 1.961 13.732 4.345 1462.148 1.551 19.325 1.348 0.67 244077. 0.0916
|
|
139.66 0.9104 0.7317 0.0106 0.0132 1.461 10.229 2.870 1089.167 1.156 12.765 1.195 0.67 245188. 0.0660
|
|
144.84 0.9441 0.5794 0.0052 0.0084 0.935 6.547 1.403 697.152 0.740 6.239 0.913 0.67 246332. 0.0352
|
|
150.01 0.9778 -0.0707 -0.0002 0.0034 0.380 2.658 -0.067 283.040 0.300 -0.298 -0.107 0.67 247447. 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 0.0915 0.0346 5.256 33.128 30.621 3919.416 3.743 136.202 3.544 0.71 253349. 0.6392
|
|
5.74 0.0337 0.0864 0.0914 0.0356 5.419 34.154 30.568 4040.788 3.859 135.968 3.431 0.71 253548. 0.6184
|
|
11.49 0.0674 0.1670 0.0912 0.0368 5.596 35.268 30.506 4172.581 3.985 135.692 3.316 0.71 253776. 0.5971
|
|
17.23 0.1011 0.2416 0.0910 0.0380 5.785 36.464 30.430 4314.154 4.120 135.353 3.199 0.71 254035. 0.5753
|
|
22.97 0.1348 0.3103 0.0907 0.0394 5.987 37.734 30.334 4464.415 4.263 134.925 3.082 0.71 254327. 0.5533
|
|
28.71 0.1685 0.3732 0.0903 0.0408 6.198 39.062 30.209 4621.527 4.413 134.370 2.965 0.72 254653. 0.5312
|
|
34.46 0.2021 0.4304 0.0898 0.0422 6.414 40.425 30.045 4782.741 4.567 133.640 2.849 0.72 255018. 0.5091
|
|
40.20 0.2358 0.4822 0.0892 0.0436 6.630 41.790 29.827 4944.234 4.721 132.672 2.736 0.72 255421. 0.4871
|
|
45.94 0.2695 0.5290 0.0883 0.0450 6.841 43.115 29.539 5101.013 4.871 131.391 2.627 0.72 255865. 0.4654
|
|
51.68 0.3032 0.5712 0.0872 0.0463 7.036 44.348 29.162 5246.882 5.010 129.711 2.521 0.72 256352. 0.4438
|
|
57.43 0.3369 0.6092 0.0857 0.0474 7.207 45.428 28.674 5374.613 5.132 127.540 2.420 0.72 256882. 0.4224
|
|
63.17 0.3706 0.6435 0.0839 0.0483 7.344 46.288 28.055 5476.372 5.230 124.788 2.324 0.72 257456. 0.4012
|
|
68.91 0.4043 0.6744 0.0816 0.0489 7.435 46.863 27.289 5544.395 5.295 121.383 2.232 0.72 258075. 0.3802
|
|
74.65 0.4380 0.7025 0.0788 0.0491 7.472 47.097 26.368 5572.089 5.321 117.285 2.146 0.72 258738. 0.3593
|
|
80.40 0.4717 0.7279 0.0756 0.0490 7.450 46.954 25.293 5555.208 5.305 112.503 2.065 0.72 259445. 0.3386
|
|
86.14 0.5054 0.7509 0.0720 0.0484 7.365 46.421 24.076 5492.114 5.245 107.090 1.988 0.72 260196. 0.3180
|
|
91.88 0.5390 0.7716 0.0680 0.0475 7.219 45.499 22.734 5383.038 5.140 101.120 1.916 0.72 260990. 0.2977
|
|
97.63 0.5727 0.7901 0.0636 0.0461 7.012 44.198 21.285 5229.146 4.993 94.674 1.846 0.73 261826. 0.2777
|
|
103.37 0.6064 0.8065 0.0590 0.0444 6.748 42.531 19.745 5031.911 4.805 87.827 1.780 0.73 262704. 0.2578
|
|
109.11 0.6401 0.8207 0.0542 0.0423 6.427 40.510 18.131 4792.799 4.577 80.646 1.716 0.73 263622. 0.2382
|
|
114.85 0.6738 0.8326 0.0492 0.0398 6.052 38.147 16.454 4513.213 4.310 73.187 1.654 0.73 264582. 0.2187
|
|
120.60 0.7075 0.8418 0.0440 0.0370 5.625 35.453 14.725 4194.467 4.005 65.498 1.592 0.73 265581. 0.1992
|
|
126.34 0.7412 0.8479 0.0387 0.0338 5.147 32.438 12.954 3837.751 3.665 57.618 1.531 0.73 266620. 0.1796
|
|
132.08 0.7749 0.8500 0.0333 0.0304 4.619 29.111 11.147 3444.140 3.289 49.583 1.468 0.74 267699. 0.1598
|
|
137.82 0.8086 0.8466 0.0278 0.0266 4.043 25.481 9.313 3014.756 2.879 41.424 1.401 0.74 268817. 0.1394
|
|
143.57 0.8423 0.8346 0.0223 0.0225 3.421 21.561 7.458 2550.938 2.436 33.174 1.326 0.74 269974. 0.1181
|
|
149.31 0.8759 0.8079 0.0167 0.0181 2.755 17.365 5.591 2054.536 1.962 24.869 1.234 0.74 271169. 0.0951
|
|
155.05 0.9096 0.7506 0.0111 0.0135 2.049 12.917 3.720 1528.246 1.459 16.549 1.104 0.74 272402. 0.0694
|
|
160.79 0.9433 0.6085 0.0056 0.0086 1.309 8.249 1.857 975.911 0.932 8.261 0.863 0.75 273671. 0.0383
|
|
166.54 0.9770 -0.0031 0.0000 0.0035 0.532 3.356 -0.004 397.011 0.379 -0.016 -0.004 0.75 274932. 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 0.0918 0.0376 7.601 43.550 37.154 5667.750 4.920 165.261 2.973 0.79 278673. 0.5908
|
|
6.32 0.0337 0.0801 0.0917 0.0386 7.811 44.754 37.101 5824.381 5.056 165.026 2.889 0.79 278892. 0.5737
|
|
12.64 0.0674 0.1553 0.0915 0.0397 8.040 46.066 37.041 5995.104 5.204 164.758 2.802 0.79 279143. 0.5560
|
|
18.96 0.1011 0.2256 0.0913 0.0409 8.286 47.480 36.969 6179.199 5.364 164.437 2.714 0.79 279427. 0.5378
|
|
25.28 0.1348 0.2908 0.0911 0.0422 8.549 48.987 36.879 6375.301 5.535 164.036 2.624 0.79 279747. 0.5194
|
|
31.60 0.1686 0.3510 0.0908 0.0436 8.825 50.567 36.762 6580.981 5.713 163.515 2.534 0.79 280106. 0.5008
|
|
37.92 0.2023 0.4064 0.0904 0.0450 9.109 52.192 36.605 6792.476 5.897 162.819 2.444 0.79 280506. 0.4821
|
|
44.24 0.2360 0.4571 0.0899 0.0464 9.393 53.821 36.393 7004.401 6.081 161.875 2.357 0.79 280948. 0.4634
|
|
50.57 0.2697 0.5035 0.0892 0.0478 9.668 55.397 36.104 7209.563 6.259 160.590 2.271 0.79 281436. 0.4449
|
|
56.89 0.3034 0.5460 0.0882 0.0490 9.922 56.852 35.713 7398.938 6.423 158.852 2.189 0.79 281971. 0.4265
|
|
63.21 0.3371 0.5849 0.0869 0.0501 10.141 58.105 35.192 7562.006 6.565 156.535 2.111 0.79 282553. 0.4082
|
|
69.53 0.3708 0.6207 0.0853 0.0509 10.309 59.069 34.513 7687.446 6.674 153.512 2.036 0.79 283185. 0.3900
|
|
75.85 0.4045 0.6536 0.0831 0.0514 10.412 59.659 33.649 7764.254 6.740 149.672 1.966 0.79 283866. 0.3717
|
|
82.17 0.4382 0.6840 0.0805 0.0516 10.438 59.807 32.587 7783.422 6.757 144.945 1.899 0.79 284596. 0.3534
|
|
88.49 0.4719 0.7121 0.0774 0.0513 10.379 59.471 31.323 7739.693 6.719 139.327 1.836 0.79 285376. 0.3349
|
|
94.81 0.5057 0.7379 0.0738 0.0506 10.235 58.642 29.872 7631.901 6.625 132.872 1.775 0.80 286204. 0.3163
|
|
101.13 0.5394 0.7614 0.0698 0.0494 10.006 57.335 28.254 7461.687 6.478 125.672 1.717 0.80 287080. 0.2976
|
|
107.45 0.5731 0.7826 0.0654 0.0479 9.698 55.569 26.491 7231.897 6.278 117.831 1.661 0.80 288002. 0.2788
|
|
113.77 0.6068 0.8015 0.0608 0.0460 9.314 53.367 24.606 6945.404 6.029 109.449 1.607 0.80 288970. 0.2598
|
|
120.09 0.6405 0.8179 0.0559 0.0438 8.857 50.748 22.620 6604.472 5.733 100.614 1.553 0.80 289984. 0.2408
|
|
126.41 0.6742 0.8317 0.0508 0.0412 8.329 47.723 20.549 6210.775 5.392 91.401 1.501 0.80 291042. 0.2218
|
|
132.73 0.7079 0.8426 0.0455 0.0382 7.732 44.302 18.407 5765.593 5.005 81.873 1.448 0.81 292144. 0.2025
|
|
139.06 0.7416 0.8503 0.0400 0.0349 7.067 40.493 16.206 5269.879 4.575 72.085 1.395 0.81 293291. 0.1830
|
|
145.38 0.7753 0.8540 0.0345 0.0313 6.336 36.303 13.958 4724.599 4.102 62.083 1.340 0.81 294480. 0.1632
|
|
151.70 0.8090 0.8518 0.0288 0.0274 5.542 31.753 11.670 4132.446 3.587 51.909 1.281 0.81 295713. 0.1426
|
|
158.02 0.8428 0.8407 0.0231 0.0232 4.687 26.858 9.353 3495.395 3.034 41.602 1.214 0.81 296988. 0.1210
|
|
164.34 0.8765 0.8136 0.0173 0.0187 3.779 21.650 7.016 2817.631 2.446 31.205 1.129 0.82 298305. 0.0975
|
|
170.66 0.9102 0.7525 0.0115 0.0140 2.824 16.179 4.669 2105.609 1.828 20.768 1.006 0.82 299663. 0.0708
|
|
176.98 0.9439 0.5984 0.0057 0.0091 1.834 10.510 2.326 1367.808 1.187 10.346 0.771 0.82 301061. 0.0383
|
|
183.30 0.9776 -0.0132 -0.0001 0.0040 0.811 4.649 -0.022 604.971 0.525 -0.097 -0.016 0.82 302447. 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 0.0917 0.0433 11.366 59.700 44.198 8475.837 6.745 196.592 2.365 0.86 304004. 0.5126
|
|
6.90 0.0337 0.0698 0.0916 0.0443 11.633 61.102 44.142 8674.852 6.903 196.345 2.308 0.86 304243. 0.4999
|
|
13.81 0.0675 0.1361 0.0915 0.0454 11.926 62.639 44.082 8893.122 7.077 196.077 2.248 0.86 304515. 0.4866
|
|
20.71 0.1012 0.1985 0.0914 0.0466 12.244 64.308 44.014 9130.048 7.265 195.773 2.187 0.86 304824. 0.4729
|
|
27.61 0.1350 0.2570 0.0912 0.0479 12.584 66.098 43.932 9384.217 7.468 195.408 2.123 0.86 305173. 0.4588
|
|
34.52 0.1687 0.3116 0.0910 0.0493 12.945 67.990 43.827 9652.850 7.681 194.944 2.059 0.86 305563. 0.4444
|
|
41.42 0.2025 0.3623 0.0907 0.0507 13.318 69.951 43.689 9931.211 7.903 194.327 1.995 0.86 305998. 0.4299
|
|
48.32 0.2362 0.4093 0.0903 0.0521 13.695 71.929 43.498 10212.021 8.126 193.480 1.932 0.86 306479. 0.4154
|
|
55.23 0.2700 0.4528 0.0897 0.0535 14.058 73.840 43.231 10483.379 8.342 192.290 1.870 0.86 307010. 0.4009
|
|
62.13 0.3037 0.4933 0.0890 0.0548 14.392 75.595 42.857 10732.482 8.541 190.628 1.811 0.86 307592. 0.3865
|
|
69.03 0.3375 0.5311 0.0879 0.0558 14.674 77.075 42.341 10942.611 8.708 188.332 1.755 0.86 308226. 0.3723
|
|
75.94 0.3712 0.5667 0.0864 0.0566 14.879 78.148 41.642 11094.999 8.829 185.225 1.702 0.86 308914. 0.3581
|
|
82.84 0.4050 0.6005 0.0845 0.0570 14.981 78.687 40.724 11171.590 8.890 181.141 1.653 0.86 309656. 0.3440
|
|
89.74 0.4387 0.6326 0.0821 0.0569 14.964 78.594 39.559 11158.290 8.879 175.959 1.608 0.87 310454. 0.3297
|
|
96.64 0.4725 0.6634 0.0792 0.0564 14.815 77.816 38.138 11047.892 8.792 169.640 1.566 0.87 311306. 0.3152
|
|
103.55 0.5062 0.6927 0.0757 0.0553 14.538 76.357 36.472 10840.649 8.627 162.228 1.526 0.87 312212. 0.3004
|
|
110.45 0.5400 0.7205 0.0718 0.0538 14.136 74.250 34.582 10541.542 8.389 153.819 1.488 0.87 313171. 0.2852
|
|
117.35 0.5737 0.7465 0.0675 0.0518 13.623 71.553 32.496 10158.729 8.084 144.543 1.451 0.87 314181. 0.2696
|
|
124.26 0.6075 0.7704 0.0628 0.0495 13.008 68.324 30.244 9700.306 7.719 134.527 1.414 0.87 315242. 0.2535
|
|
131.16 0.6412 0.7919 0.0578 0.0468 12.301 64.611 27.853 9173.050 7.300 123.889 1.377 0.87 316352. 0.2369
|
|
138.06 0.6750 0.8107 0.0526 0.0438 11.509 60.447 25.344 8581.906 6.829 112.731 1.339 0.88 317512. 0.2198
|
|
144.97 0.7087 0.8266 0.0472 0.0405 10.634 55.854 22.738 7929.888 6.310 101.140 1.301 0.88 318719. 0.2022
|
|
151.87 0.7425 0.8388 0.0416 0.0368 9.680 50.842 20.051 7218.213 5.744 89.185 1.260 0.88 319975. 0.1839
|
|
158.77 0.7762 0.8469 0.0359 0.0329 8.646 45.413 17.295 6447.465 5.131 76.928 1.217 0.88 321277. 0.1649
|
|
165.68 0.8100 0.8481 0.0301 0.0287 7.544 39.626 14.483 5625.854 4.477 64.419 1.168 0.88 322626. 0.1449
|
|
172.58 0.8437 0.8317 0.0241 0.0245 6.428 33.762 11.617 4793.312 3.814 51.674 1.099 0.89 324022. 0.1221
|
|
179.48 0.8775 0.7928 0.0181 0.0200 5.264 27.649 8.720 3925.424 3.124 38.786 1.008 0.89 325463. 0.0970
|
|
186.39 0.9112 0.7087 0.0120 0.0155 4.070 21.379 5.804 3035.219 2.415 25.816 0.867 0.89 326949. 0.0681
|
|
193.29 0.9450 0.5190 0.0060 0.0109 2.867 15.060 2.887 2138.098 1.701 12.843 0.613 0.89 328478. 0.0339
|
|
200.19 0.9787 -0.0103 -0.0001 0.0063 1.661 8.722 -0.032 1238.369 0.985 -0.143 -0.012 0.90 330011. 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 0.0900 0.0490 16.380 79.416 50.892 12214.637 8.972 226.368 1.890 0.93 329388. 0.4395
|
|
7.51 0.0339 0.0610 0.0899 0.0499 16.683 80.883 50.819 12440.177 9.138 226.042 1.853 0.93 329647. 0.4306
|
|
15.02 0.0678 0.1194 0.0898 0.0509 17.020 82.519 50.743 12691.824 9.323 225.704 1.813 0.93 329942. 0.4211
|
|
22.53 0.1017 0.1750 0.0896 0.0521 17.393 84.326 50.662 12969.716 9.527 225.344 1.772 0.93 330277. 0.4111
|
|
30.04 0.1356 0.2276 0.0894 0.0533 17.800 86.299 50.571 13273.224 9.750 224.941 1.728 0.93 330654. 0.4006
|
|
37.55 0.1695 0.2771 0.0893 0.0546 18.238 88.425 50.464 13600.252 9.990 224.463 1.683 0.93 331077. 0.3897
|
|
45.06 0.2034 0.3234 0.0890 0.0560 18.703 90.677 50.329 13946.588 10.245 223.863 1.637 0.93 331548. 0.3785
|
|
52.57 0.2373 0.3665 0.0887 0.0574 19.183 93.008 50.150 14305.129 10.508 223.068 1.590 0.93 332070. 0.3671
|
|
60.09 0.2712 0.4066 0.0883 0.0589 19.666 95.347 49.905 14664.840 10.772 221.976 1.544 0.93 332644. 0.3554
|
|
67.60 0.3050 0.4439 0.0877 0.0602 20.125 97.573 49.559 15007.281 11.024 220.437 1.498 0.93 333274. 0.3437
|
|
75.11 0.3389 0.4786 0.0868 0.0615 20.535 99.562 49.074 15313.136 11.248 218.281 1.454 0.93 333960. 0.3319
|
|
82.62 0.3728 0.5111 0.0856 0.0625 20.864 101.157 48.406 15558.452 11.429 215.309 1.411 0.93 334705. 0.3200
|
|
90.13 0.4067 0.5417 0.0840 0.0631 21.075 102.179 47.507 15715.657 11.544 211.309 1.371 0.94 335510. 0.3081
|
|
97.64 0.4406 0.5709 0.0820 0.0633 21.133 102.459 46.337 15758.812 11.576 206.106 1.334 0.94 336375. 0.2959
|
|
105.15 0.4745 0.5988 0.0794 0.0629 21.011 101.869 44.874 15668.072 11.509 199.600 1.299 0.94 337299. 0.2837
|
|
112.66 0.5084 0.6259 0.0763 0.0619 20.695 100.335 43.116 15432.125 11.336 191.779 1.267 0.94 338283. 0.2712
|
|
120.17 0.5423 0.6523 0.0727 0.0604 20.179 97.837 41.075 15047.785 11.054 182.701 1.238 0.94 339326. 0.2587
|
|
127.68 0.5762 0.6780 0.0686 0.0583 19.470 94.398 38.773 14518.875 10.665 172.461 1.211 0.94 340426. 0.2459
|
|
135.19 0.6101 0.7030 0.0641 0.0556 18.580 90.084 36.236 13855.402 10.178 161.177 1.186 0.95 341583. 0.2328
|
|
142.70 0.6440 0.7271 0.0592 0.0525 17.528 84.982 33.492 13070.617 9.601 148.972 1.162 0.95 342796. 0.2193
|
|
150.21 0.6779 0.7496 0.0541 0.0489 16.335 79.199 30.571 12181.239 8.948 135.982 1.138 0.95 344062. 0.2052
|
|
157.72 0.7118 0.7700 0.0486 0.0450 15.021 72.828 27.501 11201.287 8.228 122.325 1.114 0.95 345383. 0.1904
|
|
165.24 0.7457 0.7875 0.0430 0.0407 13.599 65.934 24.305 10140.970 7.449 108.108 1.087 0.95 346755. 0.1747
|
|
172.75 0.7796 0.8010 0.0371 0.0362 12.079 58.561 21.003 9007.008 6.616 93.422 1.058 0.96 348180. 0.1580
|
|
180.26 0.8135 0.8089 0.0312 0.0313 10.469 50.758 17.617 7806.839 5.735 78.362 1.024 0.96 349655. 0.1400
|
|
187.77 0.8474 0.7891 0.0250 0.0268 8.969 43.484 14.135 6688.022 4.913 62.872 0.959 0.96 351180. 0.1175
|
|
195.28 0.8813 0.7238 0.0187 0.0228 7.609 36.893 10.577 5674.291 4.168 47.046 0.845 0.96 352755. 0.0896
|
|
202.79 0.9151 0.6031 0.0124 0.0188 6.274 30.419 6.997 4678.617 3.437 31.125 0.678 0.97 354379. 0.0585
|
|
210.30 0.9490 0.3858 0.0061 0.0150 4.995 24.220 3.437 3725.133 2.736 15.286 0.418 0.97 356051. 0.0253
|
|
217.81 0.9829 -0.0125 -0.0001 0.0113 3.766 18.257 -0.081 2807.974 2.063 -0.361 -0.013 0.97 357763. 0.0000
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