427 lines
76 KiB
Plaintext
427 lines
76 KiB
Plaintext
22x13EPN (22x13EPN.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 0.0888 0.0332 0.014 0.867 0.663 10.260 0.098 2.948 29.299 0.09 43574. 0.6361
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0.53 0.0253 0.0658 0.0876 0.0337 0.014 0.880 0.654 10.414 0.099 2.907 28.466 0.09 43603. 0.6138
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1.06 0.0506 0.1278 0.0862 0.0342 0.014 0.893 0.644 10.563 0.101 2.863 27.637 0.09 43634. 0.5914
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1.58 0.0760 0.1860 0.0848 0.0346 0.014 0.905 0.633 10.702 0.102 2.814 26.815 0.09 43669. 0.5689
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2.11 0.1013 0.2405 0.0832 0.0350 0.015 0.915 0.621 10.829 0.103 2.761 26.004 0.09 43707. 0.5465
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2.64 0.1266 0.2914 0.0814 0.0354 0.015 0.925 0.608 10.939 0.104 2.704 25.204 0.09 43747. 0.5241
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3.17 0.1519 0.3388 0.0795 0.0357 0.015 0.932 0.594 11.030 0.105 2.641 24.417 0.09 43791. 0.5018
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3.69 0.1772 0.3828 0.0775 0.0359 0.015 0.938 0.579 11.098 0.106 2.573 23.646 0.09 43839. 0.4797
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4.22 0.2026 0.4235 0.0753 0.0360 0.015 0.941 0.562 11.138 0.106 2.500 22.889 0.09 43890. 0.4577
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4.75 0.2279 0.4610 0.0729 0.0360 0.015 0.942 0.544 11.148 0.106 2.421 22.149 0.09 43945. 0.4359
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5.28 0.2532 0.4954 0.0704 0.0360 0.015 0.940 0.525 11.124 0.106 2.337 21.423 0.09 44003. 0.4142
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5.80 0.2785 0.5269 0.0677 0.0358 0.015 0.935 0.505 11.062 0.106 2.247 20.711 0.09 44065. 0.3926
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6.33 0.3038 0.5553 0.0648 0.0354 0.015 0.926 0.484 10.960 0.105 2.151 20.010 0.09 44131. 0.3711
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6.86 0.3292 0.5808 0.0617 0.0350 0.015 0.914 0.461 10.815 0.103 2.049 19.319 0.09 44200. 0.3497
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7.39 0.3545 0.6033 0.0585 0.0344 0.014 0.898 0.436 10.624 0.101 1.941 18.634 0.09 44274. 0.3283
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7.91 0.3798 0.6227 0.0551 0.0336 0.014 0.878 0.411 10.387 0.099 1.829 17.952 0.09 44351. 0.3070
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8.44 0.4051 0.6390 0.0515 0.0327 0.014 0.854 0.385 10.104 0.096 1.711 17.269 0.09 44433. 0.2857
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8.97 0.4305 0.6518 0.0479 0.0316 0.013 0.826 0.357 9.778 0.093 1.590 16.578 0.09 44518. 0.2643
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9.50 0.4558 0.6608 0.0441 0.0304 0.013 0.795 0.329 9.409 0.090 1.465 15.876 0.09 44607. 0.2430
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10.02 0.4811 0.6658 0.0403 0.0291 0.012 0.760 0.301 8.998 0.086 1.337 15.152 0.09 44700. 0.2216
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10.55 0.5064 0.6659 0.0363 0.0276 0.011 0.722 0.271 8.545 0.082 1.206 14.398 0.09 44797. 0.2000
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11.08 0.5317 0.6605 0.0323 0.0260 0.011 0.681 0.241 8.051 0.077 1.074 13.601 0.09 44898. 0.1782
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11.61 0.5571 0.6483 0.0283 0.0243 0.010 0.636 0.211 7.519 0.072 0.940 12.743 0.09 45003. 0.1562
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12.13 0.5824 0.6278 0.0242 0.0225 0.009 0.587 0.181 6.949 0.066 0.804 11.802 0.09 45112. 0.1338
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12.66 0.6077 0.5962 0.0201 0.0205 0.009 0.536 0.150 6.343 0.061 0.668 10.743 0.09 45225. 0.1111
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13.19 0.6330 0.5500 0.0160 0.0184 0.008 0.482 0.120 5.704 0.054 0.532 9.513 0.09 45342. 0.0878
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13.72 0.6583 0.4831 0.0119 0.0163 0.007 0.426 0.089 5.035 0.048 0.397 8.034 0.09 45464. 0.0640
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14.24 0.6837 0.3851 0.0079 0.0140 0.006 0.367 0.059 4.340 0.041 0.262 6.168 0.09 45589. 0.0400
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14.77 0.7090 0.2375 0.0039 0.0117 0.005 0.306 0.029 3.622 0.035 0.130 3.668 0.09 45717. 0.0167
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15.30 0.7343 0.0016 0.0000 0.0093 0.004 0.244 0.000 2.886 0.028 0.001 0.025 0.09 45849. 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 0.0891 0.0310 0.103 3.237 2.662 76.596 0.366 11.841 15.763 0.17 87146. 0.6859
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1.06 0.0254 0.0710 0.0879 0.0315 0.104 3.293 2.626 77.920 0.372 11.679 15.284 0.17 87204. 0.6605
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2.12 0.0509 0.1376 0.0866 0.0320 0.106 3.347 2.586 79.197 0.378 11.501 14.809 0.17 87268. 0.6351
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3.18 0.0763 0.1998 0.0851 0.0325 0.108 3.398 2.542 80.402 0.384 11.307 14.340 0.17 87337. 0.6098
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4.24 0.1017 0.2579 0.0835 0.0329 0.109 3.445 2.494 81.508 0.389 11.095 13.881 0.17 87413. 0.5847
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5.30 0.1271 0.3119 0.0818 0.0333 0.111 3.486 2.442 82.486 0.394 10.864 13.430 0.17 87495. 0.5598
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6.36 0.1526 0.3620 0.0799 0.0337 0.112 3.521 2.386 83.306 0.398 10.613 12.991 0.17 87584. 0.5352
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7.42 0.1780 0.4084 0.0779 0.0339 0.113 3.547 2.325 83.936 0.401 10.340 12.562 0.17 87680. 0.5109
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8.48 0.2034 0.4513 0.0756 0.0341 0.113 3.565 2.259 84.345 0.403 10.046 12.145 0.17 87782. 0.4868
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9.53 0.2288 0.4907 0.0732 0.0342 0.113 3.571 2.187 84.502 0.403 9.729 11.740 0.17 87892. 0.4631
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10.59 0.2543 0.5269 0.0707 0.0341 0.113 3.566 2.111 84.378 0.403 9.388 11.346 0.18 88010. 0.4396
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11.65 0.2797 0.5600 0.0679 0.0339 0.113 3.548 2.029 83.946 0.401 9.024 10.962 0.18 88135. 0.4165
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12.71 0.3051 0.5901 0.0650 0.0336 0.112 3.515 1.942 83.181 0.397 8.637 10.588 0.18 88267. 0.3935
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13.77 0.3305 0.6172 0.0619 0.0332 0.110 3.468 1.850 82.058 0.392 8.227 10.223 0.18 88408. 0.3708
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14.83 0.3560 0.6414 0.0587 0.0326 0.108 3.404 1.752 80.551 0.385 7.793 9.865 0.18 88556. 0.3483
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15.89 0.3814 0.6627 0.0552 0.0318 0.105 3.324 1.650 78.657 0.376 7.337 9.512 0.18 88712. 0.3258
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16.95 0.4068 0.6809 0.0517 0.0309 0.102 3.228 1.543 76.384 0.365 6.864 9.163 0.18 88876. 0.3036
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18.01 0.4322 0.6959 0.0480 0.0298 0.099 3.116 1.433 73.740 0.352 6.374 8.814 0.18 89048. 0.2814
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19.07 0.4577 0.7076 0.0442 0.0286 0.095 2.989 1.320 70.729 0.338 5.871 8.464 0.18 89227. 0.2593
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20.13 0.4831 0.7154 0.0403 0.0272 0.090 2.847 1.204 67.358 0.322 5.355 8.107 0.18 89415. 0.2372
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21.19 0.5085 0.7189 0.0364 0.0257 0.085 2.689 1.086 63.632 0.304 4.829 7.739 0.18 89611. 0.2151
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22.25 0.5339 0.7173 0.0323 0.0241 0.080 2.517 0.966 59.559 0.284 4.296 7.354 0.18 89814. 0.1928
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23.31 0.5594 0.7095 0.0283 0.0223 0.074 2.331 0.844 55.150 0.263 3.755 6.944 0.18 90026. 0.1702
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24.37 0.5848 0.6938 0.0242 0.0204 0.068 2.131 0.722 50.418 0.241 3.211 6.495 0.18 90246. 0.1472
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25.43 0.6102 0.6674 0.0201 0.0183 0.061 1.918 0.599 45.379 0.217 2.665 5.988 0.18 90474. 0.1236
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26.49 0.6356 0.6262 0.0160 0.0162 0.054 1.693 0.476 40.056 0.191 2.119 5.393 0.18 90710. 0.0993
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27.54 0.6611 0.5627 0.0119 0.0139 0.046 1.457 0.354 34.474 0.165 1.575 4.660 0.18 90954. 0.0740
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28.60 0.6865 0.4630 0.0078 0.0116 0.038 1.211 0.233 28.666 0.137 1.038 3.692 0.18 91206. 0.0476
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29.66 0.7119 0.2979 0.0038 0.0092 0.030 0.958 0.115 22.669 0.108 0.509 2.291 0.18 91465. 0.0207
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30.72 0.7374 -0.0073 -0.0001 0.0067 0.022 0.698 -0.002 16.510 0.079 -0.009 -0.054 0.18 91729. 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 0.0896 0.0301 0.337 7.086 6.020 251.491 0.801 26.775 10.857 0.26 130715. 0.7104
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1.59 0.0254 0.0733 0.0884 0.0307 0.343 7.216 5.938 256.108 0.815 26.413 10.517 0.26 130803. 0.6835
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3.18 0.0509 0.1420 0.0871 0.0312 0.349 7.341 5.849 260.573 0.829 26.016 10.181 0.26 130898. 0.6567
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4.77 0.0763 0.2061 0.0856 0.0317 0.355 7.460 5.751 264.797 0.843 25.580 9.851 0.26 131003. 0.6301
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6.36 0.1018 0.2657 0.0840 0.0322 0.360 7.570 5.644 268.688 0.855 25.104 9.527 0.26 131117. 0.6037
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7.95 0.1272 0.3211 0.0823 0.0326 0.365 7.668 5.527 272.147 0.866 24.584 9.212 0.26 131240. 0.5776
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9.54 0.1527 0.3725 0.0804 0.0329 0.369 7.750 5.400 275.067 0.876 24.019 8.904 0.26 131374. 0.5519
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11.13 0.1781 0.4200 0.0783 0.0332 0.372 7.814 5.262 277.341 0.883 23.405 8.605 0.26 131517. 0.5265
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12.72 0.2036 0.4639 0.0761 0.0334 0.374 7.857 5.113 278.860 0.888 22.741 8.316 0.26 131672. 0.5015
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14.31 0.2290 0.5042 0.0737 0.0335 0.375 7.875 4.952 279.516 0.890 22.025 8.035 0.26 131837. 0.4769
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15.90 0.2545 0.5413 0.0711 0.0334 0.374 7.866 4.779 279.208 0.889 21.257 7.763 0.26 132014. 0.4526
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17.50 0.2799 0.5752 0.0684 0.0333 0.373 7.828 4.594 277.842 0.884 20.435 7.500 0.26 132202. 0.4287
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19.09 0.3054 0.6061 0.0654 0.0330 0.369 7.757 4.397 275.330 0.876 19.560 7.244 0.26 132401. 0.4052
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20.68 0.3308 0.6341 0.0623 0.0325 0.364 7.652 4.189 271.583 0.864 18.631 6.995 0.26 132612. 0.3818
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22.27 0.3563 0.6592 0.0591 0.0319 0.357 7.509 3.968 266.512 0.848 17.649 6.753 0.26 132835. 0.3588
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23.86 0.3817 0.6814 0.0556 0.0312 0.349 7.328 3.736 260.103 0.828 16.618 6.515 0.26 133070. 0.3359
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25.45 0.4072 0.7007 0.0520 0.0302 0.338 7.111 3.495 252.380 0.803 15.546 6.281 0.26 133316. 0.3132
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27.04 0.4326 0.7170 0.0483 0.0291 0.326 6.857 3.246 243.365 0.775 14.437 6.049 0.26 133574. 0.2907
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28.63 0.4581 0.7301 0.0445 0.0279 0.313 6.567 2.989 233.075 0.742 13.297 5.818 0.26 133844. 0.2683
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30.22 0.4835 0.7397 0.0406 0.0265 0.297 6.241 2.727 221.527 0.705 12.130 5.583 0.26 134126. 0.2459
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31.81 0.5089 0.7452 0.0366 0.0250 0.280 5.881 2.459 208.741 0.664 10.939 5.344 0.27 134420. 0.2235
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33.40 0.5344 0.7460 0.0326 0.0233 0.261 5.487 2.188 194.745 0.620 9.731 5.095 0.27 134727. 0.2010
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34.99 0.5598 0.7411 0.0285 0.0215 0.241 5.059 1.913 179.574 0.572 8.508 4.831 0.27 135045. 0.1782
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36.58 0.5853 0.7287 0.0243 0.0196 0.219 4.600 1.636 163.272 0.520 7.275 4.544 0.27 135375. 0.1550
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38.17 0.6107 0.7062 0.0202 0.0175 0.196 4.111 1.358 145.900 0.464 6.038 4.220 0.27 135717. 0.1311
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39.76 0.6362 0.6694 0.0161 0.0153 0.171 3.593 1.080 127.532 0.406 4.803 3.840 0.27 136072. 0.1064
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41.35 0.6616 0.6102 0.0120 0.0130 0.145 3.050 0.803 108.260 0.345 3.574 3.366 0.27 136439. 0.0805
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42.94 0.6871 0.5133 0.0079 0.0106 0.118 2.485 0.530 88.198 0.281 2.358 2.727 0.27 136817. 0.0529
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44.53 0.7125 0.3432 0.0039 0.0081 0.090 1.901 0.262 67.481 0.215 1.163 1.758 0.27 137207. 0.0240
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46.12 0.7380 -0.0036 0.0000 0.0055 0.062 1.301 -0.002 46.182 0.147 -0.008 -0.018 0.27 137602. 0.0000
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PROP RPM = 4000
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V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
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(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
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0.00 0.0000 0.0000 0.0902 0.0298 0.790 12.454 10.772 589.390 1.407 47.914 8.290 0.35 174279. 0.7257
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2.12 0.0255 0.0746 0.0890 0.0303 0.805 12.691 10.628 600.617 1.434 47.275 8.026 0.35 174396. 0.6979
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4.24 0.0509 0.1444 0.0877 0.0309 0.820 12.921 10.470 611.488 1.460 46.572 7.766 0.35 174524. 0.6703
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6.36 0.0764 0.2095 0.0862 0.0314 0.834 13.139 10.297 621.789 1.484 45.802 7.511 0.35 174664. 0.6429
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8.48 0.1018 0.2701 0.0846 0.0319 0.847 13.340 10.107 631.299 1.507 44.958 7.262 0.35 174816. 0.6158
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10.60 0.1273 0.3263 0.0829 0.0323 0.858 13.519 9.900 639.775 1.527 44.036 7.019 0.35 174981. 0.5890
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12.73 0.1527 0.3784 0.0810 0.0327 0.868 13.671 9.674 646.963 1.545 43.031 6.782 0.35 175159. 0.5626
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14.85 0.1782 0.4265 0.0789 0.0330 0.875 13.790 9.429 652.599 1.558 41.939 6.553 0.35 175351. 0.5367
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16.97 0.2036 0.4710 0.0767 0.0332 0.880 13.871 9.163 656.419 1.567 40.757 6.331 0.35 175558. 0.5112
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19.09 0.2291 0.5119 0.0743 0.0333 0.883 13.907 8.876 658.161 1.571 39.481 6.117 0.35 175779. 0.4860
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21.21 0.2545 0.5495 0.0717 0.0332 0.882 13.895 8.568 657.581 1.570 38.109 5.910 0.35 176014. 0.4613
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23.33 0.2800 0.5839 0.0690 0.0331 0.878 13.829 8.238 654.447 1.562 36.641 5.709 0.35 176266. 0.4370
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25.45 0.3054 0.6154 0.0660 0.0328 0.870 13.704 7.886 648.547 1.548 35.077 5.515 0.35 176532. 0.4131
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27.57 0.3309 0.6439 0.0629 0.0323 0.858 13.517 7.513 639.665 1.527 33.416 5.327 0.35 176814. 0.3894
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29.69 0.3563 0.6696 0.0596 0.0317 0.842 13.261 7.118 627.585 1.498 31.659 5.144 0.35 177111. 0.3660
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31.81 0.3818 0.6926 0.0561 0.0309 0.821 12.937 6.703 612.262 1.462 29.814 4.965 0.35 177424. 0.3429
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33.94 0.4072 0.7127 0.0525 0.0300 0.796 12.546 6.271 593.751 1.417 27.893 4.790 0.35 177753. 0.3199
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36.06 0.4327 0.7299 0.0488 0.0289 0.767 12.089 5.824 572.101 1.366 25.906 4.618 0.35 178098. 0.2972
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38.18 0.4581 0.7440 0.0449 0.0277 0.734 11.566 5.365 547.354 1.307 23.862 4.446 0.35 178459. 0.2746
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40.30 0.4836 0.7548 0.0410 0.0262 0.697 10.978 4.894 519.549 1.240 21.769 4.273 0.35 178835. 0.2521
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42.42 0.5090 0.7618 0.0370 0.0247 0.655 10.327 4.414 488.734 1.167 19.635 4.097 0.35 179228. 0.2296
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44.54 0.5345 0.7644 0.0329 0.0230 0.610 9.614 3.927 454.973 1.086 17.466 3.915 0.35 179636. 0.2069
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46.66 0.5599 0.7615 0.0287 0.0211 0.561 8.840 3.434 418.352 0.999 15.273 3.723 0.35 180061. 0.1840
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48.78 0.5854 0.7516 0.0246 0.0191 0.508 8.008 2.937 378.980 0.905 13.062 3.514 0.36 180501. 0.1606
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50.90 0.6108 0.7321 0.0204 0.0170 0.452 7.121 2.438 337.002 0.805 10.843 3.281 0.36 180958. 0.1366
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53.02 0.6363 0.6988 0.0162 0.0148 0.392 6.183 1.939 292.598 0.699 8.625 3.006 0.36 181431. 0.1116
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55.15 0.6617 0.6434 0.0121 0.0124 0.330 5.198 1.444 245.996 0.587 6.421 2.662 0.36 181920. 0.0853
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57.27 0.6872 0.5497 0.0080 0.0100 0.265 4.173 0.953 197.473 0.471 4.240 2.190 0.36 182425. 0.0570
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59.39 0.7126 0.3779 0.0039 0.0074 0.198 3.114 0.472 147.362 0.352 2.097 1.451 0.36 182946. 0.0266
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61.51 0.7381 -0.0011 0.0000 0.0048 0.128 2.025 -0.001 95.812 0.229 -0.004 -0.004 0.36 183471. 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 0.0909 0.0297 1.541 19.425 16.973 1149.132 2.195 75.496 6.699 0.44 217836. 0.7361
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2.65 0.0255 0.0754 0.0898 0.0303 1.571 19.806 16.751 1171.612 2.238 74.508 6.485 0.44 217982. 0.7079
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5.30 0.0509 0.1459 0.0884 0.0309 1.600 20.174 16.506 1193.405 2.279 73.418 6.273 0.44 218143. 0.6798
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7.96 0.0764 0.2116 0.0870 0.0314 1.628 20.523 16.237 1214.075 2.319 72.221 6.066 0.44 218318. 0.6519
|
|
10.61 0.1018 0.2727 0.0854 0.0319 1.654 20.846 15.942 1233.187 2.355 70.908 5.863 0.44 218509. 0.6244
|
|
13.26 0.1273 0.3294 0.0837 0.0323 1.677 21.135 15.619 1250.252 2.388 69.471 5.666 0.44 218715. 0.5972
|
|
15.91 0.1528 0.3819 0.0818 0.0327 1.696 21.380 15.266 1264.761 2.416 67.903 5.475 0.44 218939. 0.5705
|
|
18.56 0.1782 0.4304 0.0797 0.0330 1.711 21.573 14.882 1276.184 2.437 66.195 5.289 0.44 219180. 0.5442
|
|
21.22 0.2037 0.4753 0.0775 0.0332 1.722 21.705 14.466 1283.992 2.452 64.343 5.110 0.44 219439. 0.5184
|
|
23.87 0.2291 0.5166 0.0751 0.0333 1.727 21.767 14.016 1287.660 2.459 62.342 4.937 0.44 219716. 0.4930
|
|
26.52 0.2546 0.5545 0.0725 0.0333 1.725 21.751 13.531 1286.696 2.457 60.188 4.770 0.44 220011. 0.4680
|
|
29.17 0.2800 0.5894 0.0697 0.0331 1.717 21.648 13.013 1280.636 2.446 57.880 4.609 0.44 220326. 0.4434
|
|
31.82 0.3055 0.6212 0.0668 0.0328 1.702 21.453 12.459 1269.057 2.424 55.419 4.453 0.44 220660. 0.4192
|
|
34.47 0.3310 0.6502 0.0636 0.0324 1.678 21.156 11.871 1251.529 2.390 52.803 4.302 0.44 221013. 0.3954
|
|
37.13 0.3564 0.6764 0.0603 0.0318 1.646 20.752 11.248 1227.621 2.345 50.033 4.156 0.44 221385. 0.3718
|
|
39.78 0.3819 0.6999 0.0568 0.0310 1.606 20.238 10.594 1197.223 2.287 47.122 4.014 0.44 221778. 0.3484
|
|
42.43 0.4073 0.7207 0.0531 0.0300 1.556 19.617 9.912 1160.443 2.216 44.090 3.874 0.44 222190. 0.3253
|
|
45.08 0.4328 0.7386 0.0493 0.0289 1.498 18.889 9.207 1117.378 2.134 40.952 3.737 0.44 222621. 0.3024
|
|
47.73 0.4583 0.7536 0.0454 0.0276 1.432 18.056 8.481 1068.110 2.040 37.722 3.601 0.44 223073. 0.2797
|
|
50.39 0.4837 0.7654 0.0415 0.0262 1.358 17.119 7.737 1012.716 1.934 34.413 3.465 0.44 223544. 0.2571
|
|
53.04 0.5092 0.7736 0.0374 0.0246 1.276 16.081 6.978 951.295 1.817 31.037 3.327 0.44 224035. 0.2344
|
|
55.69 0.5346 0.7775 0.0333 0.0229 1.185 14.943 6.207 883.972 1.688 27.607 3.185 0.44 224547. 0.2116
|
|
58.34 0.5601 0.7763 0.0291 0.0210 1.087 13.708 5.426 810.918 1.549 24.135 3.035 0.44 225078. 0.1886
|
|
60.99 0.5855 0.7683 0.0249 0.0189 0.982 12.380 4.639 732.357 1.399 20.636 2.873 0.44 225629. 0.1651
|
|
63.65 0.6110 0.7512 0.0206 0.0168 0.870 10.964 3.850 648.575 1.239 17.123 2.692 0.44 226201. 0.1409
|
|
66.30 0.6365 0.7206 0.0164 0.0145 0.751 9.465 3.061 559.939 1.069 13.613 2.479 0.45 226793. 0.1157
|
|
68.95 0.6619 0.6683 0.0122 0.0121 0.626 7.893 2.276 466.905 0.892 10.123 2.211 0.45 227404. 0.0890
|
|
71.60 0.6874 0.5771 0.0080 0.0096 0.496 6.255 1.500 370.038 0.707 6.671 1.838 0.45 228036. 0.0601
|
|
74.25 0.7128 0.4031 0.0040 0.0070 0.362 4.564 0.737 270.007 0.516 3.279 1.238 0.45 228687. 0.0284
|
|
76.91 0.7383 -0.0102 -0.0001 0.0043 0.224 2.823 -0.011 167.011 0.319 -0.050 -0.030 0.45 229340. 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 0.0919 0.0299 2.678 28.127 24.697 1996.623 3.178 109.854 5.610 0.52 261384. 0.7436
|
|
3.18 0.0254 0.0757 0.0907 0.0305 2.731 28.688 24.382 2036.486 3.241 108.453 5.430 0.52 261559. 0.7152
|
|
6.36 0.0509 0.1464 0.0894 0.0311 2.783 29.233 24.034 2075.172 3.303 106.905 5.253 0.52 261752. 0.6869
|
|
9.53 0.0763 0.2123 0.0880 0.0316 2.832 29.751 23.651 2111.914 3.361 105.200 5.079 0.52 261962. 0.6589
|
|
12.71 0.1017 0.2736 0.0864 0.0321 2.878 30.230 23.230 2145.927 3.415 103.326 4.910 0.52 262192. 0.6312
|
|
15.89 0.1271 0.3306 0.0847 0.0326 2.919 30.658 22.767 2176.354 3.464 101.270 4.745 0.52 262440. 0.6038
|
|
19.07 0.1526 0.3833 0.0828 0.0330 2.953 31.024 22.262 2202.292 3.505 99.020 4.585 0.52 262708. 0.5770
|
|
22.25 0.1780 0.4321 0.0808 0.0333 2.981 31.313 21.710 2222.800 3.538 96.566 4.430 0.52 262998. 0.5505
|
|
25.43 0.2034 0.4771 0.0785 0.0335 3.000 31.512 21.110 2236.932 3.560 93.899 4.280 0.52 263309. 0.5245
|
|
28.60 0.2288 0.5187 0.0761 0.0336 3.009 31.608 20.461 2243.762 3.571 91.012 4.136 0.52 263642. 0.4990
|
|
31.78 0.2543 0.5569 0.0735 0.0336 3.007 31.589 19.762 2242.411 3.569 87.900 3.997 0.53 263997. 0.4739
|
|
34.96 0.2797 0.5921 0.0707 0.0334 2.993 31.443 19.011 2232.062 3.552 84.560 3.863 0.53 264375. 0.4492
|
|
38.14 0.3051 0.6243 0.0678 0.0331 2.966 31.160 18.209 2211.965 3.520 80.993 3.734 0.53 264775. 0.4249
|
|
41.32 0.3305 0.6537 0.0646 0.0327 2.925 30.729 17.356 2181.377 3.472 77.199 3.609 0.53 265199. 0.4010
|
|
44.50 0.3560 0.6803 0.0612 0.0320 2.869 30.140 16.452 2139.529 3.405 73.177 3.488 0.53 265647. 0.3773
|
|
47.67 0.3814 0.7043 0.0577 0.0312 2.798 29.388 15.500 2086.185 3.320 68.945 3.370 0.53 266117. 0.3539
|
|
50.85 0.4068 0.7257 0.0540 0.0303 2.711 28.477 14.508 2021.523 3.217 64.531 3.255 0.53 266611. 0.3307
|
|
54.03 0.4322 0.7443 0.0502 0.0291 2.609 27.410 13.480 1945.728 3.097 59.959 3.142 0.53 267129. 0.3077
|
|
57.21 0.4577 0.7601 0.0462 0.0278 2.493 26.187 12.421 1858.939 2.959 55.251 3.031 0.53 267671. 0.2849
|
|
60.39 0.4831 0.7728 0.0422 0.0264 2.362 24.812 11.336 1761.302 2.803 50.423 2.919 0.53 268236. 0.2622
|
|
63.57 0.5085 0.7821 0.0381 0.0247 2.217 23.286 10.228 1652.989 2.631 45.496 2.807 0.53 268825. 0.2394
|
|
66.74 0.5340 0.7874 0.0339 0.0230 2.057 21.613 9.102 1534.224 2.442 40.487 2.691 0.53 269437. 0.2165
|
|
69.92 0.5594 0.7877 0.0296 0.0210 1.885 19.797 7.962 1405.304 2.237 35.414 2.570 0.53 270074. 0.1934
|
|
73.10 0.5848 0.7817 0.0253 0.0190 1.699 17.843 6.812 1266.627 2.016 30.299 2.439 0.53 270735. 0.1698
|
|
76.28 0.6102 0.7670 0.0210 0.0167 1.500 15.759 5.657 1118.698 1.780 25.162 2.294 0.53 271419. 0.1455
|
|
79.46 0.6357 0.7393 0.0168 0.0144 1.290 13.554 4.502 962.164 1.531 20.027 2.122 0.53 272128. 0.1201
|
|
82.64 0.6611 0.6908 0.0125 0.0119 1.070 11.239 3.354 797.834 1.270 14.919 1.907 0.54 272860. 0.0931
|
|
85.81 0.6865 0.6039 0.0083 0.0094 0.840 8.828 2.218 626.709 0.997 9.866 1.605 0.54 273617. 0.0638
|
|
88.99 0.7119 0.4331 0.0041 0.0067 0.603 6.339 1.101 449.983 0.716 4.899 1.110 0.54 274397. 0.0311
|
|
92.17 0.7374 0.0040 0.0000 0.0040 0.360 3.777 0.006 268.097 0.427 0.026 0.010 0.54 275180. 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 0.0931 0.0302 4.303 38.742 34.046 3208.559 4.377 151.437 4.813 0.61 304919. 0.7490
|
|
3.71 0.0254 0.0757 0.0919 0.0309 4.390 39.531 33.627 3273.894 4.466 149.571 4.659 0.61 305124. 0.7205
|
|
7.41 0.0508 0.1465 0.0907 0.0315 4.475 40.298 33.162 3337.375 4.553 147.503 4.507 0.61 305349. 0.6922
|
|
11.12 0.0762 0.2124 0.0892 0.0320 4.556 41.026 32.648 3397.734 4.635 145.217 4.358 0.61 305595. 0.6642
|
|
14.83 0.1017 0.2738 0.0877 0.0326 4.631 41.702 32.081 3453.692 4.711 142.694 4.213 0.61 305863. 0.6365
|
|
18.53 0.1271 0.3308 0.0860 0.0330 4.699 42.307 31.456 3503.828 4.780 139.918 4.072 0.61 306154. 0.6091
|
|
22.24 0.1525 0.3837 0.0841 0.0334 4.756 42.825 30.771 3546.651 4.838 136.871 3.935 0.61 306468. 0.5822
|
|
25.94 0.1779 0.4326 0.0821 0.0338 4.802 43.235 30.022 3580.610 4.885 133.538 3.803 0.61 306807. 0.5558
|
|
29.65 0.2033 0.4778 0.0798 0.0340 4.833 43.519 29.205 3604.152 4.917 129.905 3.675 0.61 307171. 0.5298
|
|
33.36 0.2287 0.5195 0.0774 0.0341 4.849 43.659 28.319 3615.746 4.933 125.963 3.552 0.61 307560. 0.5042
|
|
37.06 0.2542 0.5580 0.0748 0.0341 4.846 43.637 27.361 3613.950 4.930 121.703 3.434 0.61 307976. 0.4791
|
|
40.77 0.2796 0.5934 0.0720 0.0339 4.824 43.438 26.332 3597.426 4.908 117.123 3.320 0.61 308418. 0.4544
|
|
44.48 0.3050 0.6259 0.0690 0.0336 4.781 43.045 25.230 3564.948 4.863 112.222 3.210 0.61 308887. 0.4300
|
|
48.18 0.3304 0.6556 0.0658 0.0331 4.714 42.446 24.056 3515.323 4.796 107.001 3.104 0.61 309383. 0.4060
|
|
51.89 0.3558 0.6827 0.0624 0.0325 4.623 41.625 22.810 3447.308 4.703 101.459 3.001 0.61 309906. 0.3823
|
|
55.60 0.3812 0.7072 0.0588 0.0317 4.506 40.576 21.497 3360.442 4.584 95.618 2.902 0.62 310456. 0.3588
|
|
59.30 0.4066 0.7291 0.0550 0.0307 4.365 39.303 20.126 3255.020 4.440 89.519 2.804 0.62 311033. 0.3356
|
|
63.01 0.4321 0.7484 0.0511 0.0295 4.199 37.810 18.704 3131.347 4.272 83.195 2.709 0.62 311638. 0.3125
|
|
66.71 0.4575 0.7649 0.0471 0.0282 4.009 36.099 17.238 2989.674 4.078 76.675 2.615 0.62 312271. 0.2896
|
|
70.42 0.4829 0.7785 0.0430 0.0267 3.795 34.174 15.734 2830.243 3.861 69.986 2.522 0.62 312931. 0.2668
|
|
74.13 0.5083 0.7887 0.0388 0.0250 3.558 32.038 14.198 2653.345 3.620 63.153 2.427 0.62 313618. 0.2439
|
|
77.83 0.5337 0.7951 0.0345 0.0232 3.298 29.696 12.635 2459.350 3.355 56.202 2.330 0.62 314333. 0.2209
|
|
81.54 0.5591 0.7968 0.0302 0.0212 3.016 27.153 11.052 2248.753 3.068 49.159 2.229 0.62 315076. 0.1977
|
|
85.25 0.5845 0.7925 0.0258 0.0191 2.712 24.417 9.454 2022.199 2.759 42.052 2.121 0.62 315847. 0.1739
|
|
88.95 0.6100 0.7797 0.0215 0.0168 2.388 21.499 7.849 1780.524 2.429 34.912 1.999 0.62 316646. 0.1494
|
|
92.66 0.6354 0.7544 0.0171 0.0144 2.045 18.411 6.243 1524.792 2.080 27.771 1.857 0.62 317472. 0.1238
|
|
96.37 0.6608 0.7086 0.0127 0.0118 1.685 15.170 4.646 1256.338 1.714 20.665 1.677 0.62 318327. 0.0964
|
|
100.07 0.6862 0.6244 0.0084 0.0092 1.310 11.795 3.065 976.811 1.333 13.634 1.423 0.63 319209. 0.0665
|
|
103.78 0.7116 0.4532 0.0041 0.0065 0.923 8.310 1.511 688.194 0.939 6.723 0.996 0.63 320118. 0.0327
|
|
107.48 0.7370 -0.0079 0.0000 0.0037 0.524 4.720 -0.014 390.937 0.533 -0.064 -0.017 0.63 321026. 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 0.0945 0.0309 6.553 51.632 45.154 4886.933 5.833 200.846 4.191 0.70 348437. 0.7511
|
|
4.23 0.0254 0.0753 0.0934 0.0315 6.687 52.682 44.625 4986.316 5.952 198.491 4.059 0.70 348672. 0.7232
|
|
8.46 0.0508 0.1457 0.0922 0.0321 6.817 53.706 44.035 5083.271 6.068 195.868 3.929 0.70 348930. 0.6954
|
|
12.69 0.0762 0.2115 0.0908 0.0327 6.941 54.685 43.380 5175.861 6.178 192.953 3.801 0.70 349212. 0.6678
|
|
16.92 0.1015 0.2728 0.0893 0.0332 7.057 55.595 42.653 5262.071 6.281 189.721 3.677 0.70 349518. 0.6404
|
|
21.15 0.1269 0.3297 0.0876 0.0337 7.161 56.415 41.850 5339.677 6.374 186.147 3.555 0.70 349851. 0.6134
|
|
25.38 0.1523 0.3824 0.0857 0.0341 7.250 57.119 40.964 5406.275 6.453 182.208 3.437 0.70 350212. 0.5867
|
|
29.61 0.1777 0.4314 0.0837 0.0345 7.321 57.680 39.991 5459.392 6.517 177.881 3.322 0.70 350600. 0.5604
|
|
33.85 0.2031 0.4766 0.0815 0.0347 7.371 58.072 38.927 5496.505 6.561 173.146 3.212 0.70 351017. 0.5345
|
|
38.08 0.2285 0.5185 0.0790 0.0348 7.396 58.270 37.768 5515.184 6.583 167.990 3.106 0.70 351463. 0.5091
|
|
42.31 0.2538 0.5571 0.0764 0.0348 7.393 58.248 36.511 5513.151 6.581 162.402 3.004 0.70 351939. 0.4841
|
|
46.54 0.2792 0.5928 0.0736 0.0347 7.360 57.986 35.157 5488.330 6.551 156.377 2.905 0.70 352446. 0.4595
|
|
50.77 0.3046 0.6256 0.0705 0.0343 7.294 57.463 33.704 5438.844 6.492 149.914 2.811 0.70 352982. 0.4352
|
|
55.00 0.3300 0.6557 0.0673 0.0339 7.192 56.661 32.153 5362.890 6.401 143.014 2.719 0.70 353550. 0.4113
|
|
59.23 0.3554 0.6831 0.0638 0.0332 7.052 55.558 30.503 5258.577 6.277 135.676 2.631 0.70 354149. 0.3875
|
|
63.46 0.3808 0.7081 0.0602 0.0324 6.873 54.148 28.761 5125.057 6.118 127.927 2.545 0.70 354778. 0.3641
|
|
67.69 0.4061 0.7306 0.0564 0.0313 6.655 52.433 26.938 4962.763 5.924 119.820 2.462 0.70 355439. 0.3408
|
|
71.92 0.4315 0.7505 0.0524 0.0301 6.400 50.420 25.045 4772.212 5.696 111.402 2.380 0.70 356131. 0.3177
|
|
76.15 0.4569 0.7678 0.0483 0.0288 6.107 48.112 23.092 4553.814 5.436 102.712 2.300 0.71 356854. 0.2948
|
|
80.38 0.4823 0.7823 0.0441 0.0272 5.777 45.515 21.085 4307.974 5.142 93.785 2.220 0.71 357609. 0.2719
|
|
84.61 0.5077 0.7936 0.0398 0.0255 5.411 42.633 19.033 4035.144 4.817 84.658 2.139 0.71 358394. 0.2489
|
|
88.84 0.5331 0.8012 0.0355 0.0236 5.010 39.471 16.943 3735.917 4.459 75.364 2.057 0.71 359211. 0.2258
|
|
93.07 0.5584 0.8043 0.0310 0.0215 4.574 36.039 14.824 3411.055 4.072 65.939 1.971 0.71 360060. 0.2024
|
|
97.30 0.5838 0.8016 0.0265 0.0193 4.106 32.347 12.685 3061.586 3.654 56.422 1.879 0.71 360940. 0.1785
|
|
101.54 0.6092 0.7909 0.0220 0.0170 3.606 28.409 10.533 2688.888 3.210 46.852 1.777 0.71 361852. 0.1538
|
|
105.77 0.6346 0.7680 0.0175 0.0145 3.077 24.245 8.380 2294.738 2.739 37.274 1.656 0.71 362795. 0.1279
|
|
110.00 0.6600 0.7249 0.0131 0.0119 2.523 19.878 6.236 1881.416 2.246 27.736 1.503 0.71 363770. 0.1001
|
|
114.23 0.6854 0.6435 0.0086 0.0092 1.947 15.338 4.113 1451.777 1.733 18.295 1.285 0.71 364776. 0.0695
|
|
118.46 0.7107 0.4726 0.0042 0.0064 1.354 10.664 2.025 1009.312 1.205 9.008 0.910 0.72 365813. 0.0345
|
|
122.69 0.7361 -0.0115 -0.0001 0.0035 0.744 5.864 -0.026 555.007 0.662 -0.117 -0.021 0.72 366846. 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 0.0962 0.0329 9.953 69.700 58.176 7421.665 7.875 258.767 3.555 0.79 391933. 0.7233
|
|
4.75 0.0253 0.0720 0.0952 0.0335 10.117 70.849 57.544 7544.092 8.005 255.954 3.460 0.79 392197. 0.7000
|
|
9.50 0.0507 0.1401 0.0940 0.0340 10.276 71.962 56.834 7662.560 8.130 252.796 3.364 0.79 392487. 0.6764
|
|
14.25 0.0760 0.2042 0.0927 0.0345 10.426 73.014 56.039 7774.585 8.249 249.261 3.269 0.79 392804. 0.6527
|
|
18.99 0.1013 0.2644 0.0912 0.0349 10.564 73.981 55.151 7877.560 8.358 245.313 3.175 0.79 393150. 0.6290
|
|
23.74 0.1266 0.3209 0.0896 0.0353 10.686 74.837 54.163 7968.654 8.455 240.917 3.083 0.79 393525. 0.6051
|
|
28.49 0.1520 0.3737 0.0878 0.0357 10.788 75.552 53.066 8044.794 8.536 236.038 2.992 0.79 393931. 0.5813
|
|
33.24 0.1773 0.4230 0.0858 0.0359 10.866 76.096 51.854 8102.741 8.597 230.646 2.903 0.79 394368. 0.5575
|
|
37.99 0.2026 0.4689 0.0835 0.0361 10.915 76.438 50.520 8139.156 8.636 224.713 2.815 0.79 394838. 0.5337
|
|
42.74 0.2279 0.5115 0.0811 0.0362 10.930 76.546 49.060 8150.712 8.648 218.217 2.730 0.79 395341. 0.5100
|
|
47.49 0.2533 0.5510 0.0785 0.0361 10.908 76.391 47.469 8134.154 8.631 211.142 2.647 0.79 395878. 0.4864
|
|
52.23 0.2786 0.5876 0.0757 0.0359 10.844 75.943 45.747 8086.441 8.580 203.481 2.566 0.79 396449. 0.4629
|
|
56.98 0.3039 0.6213 0.0726 0.0355 10.734 75.175 43.892 8004.703 8.493 195.232 2.487 0.79 397054. 0.4395
|
|
61.73 0.3292 0.6523 0.0693 0.0350 10.575 74.062 41.906 7886.150 8.367 186.399 2.410 0.79 397693. 0.4161
|
|
66.48 0.3546 0.6806 0.0658 0.0343 10.363 72.574 39.788 7727.726 8.199 176.977 2.335 0.79 398367. 0.3929
|
|
71.23 0.3799 0.7064 0.0621 0.0334 10.095 70.694 37.545 7527.569 7.987 166.999 2.262 0.79 399076. 0.3697
|
|
75.98 0.4052 0.7297 0.0582 0.0323 9.770 68.424 35.191 7285.850 7.731 156.531 2.191 0.79 399820. 0.3466
|
|
80.73 0.4305 0.7505 0.0541 0.0311 9.392 65.770 32.742 7003.275 7.431 145.637 2.121 0.79 400598. 0.3236
|
|
85.48 0.4559 0.7686 0.0500 0.0296 8.958 62.738 30.209 6680.332 7.088 134.371 2.051 0.79 401411. 0.3007
|
|
90.22 0.4812 0.7839 0.0456 0.0280 8.472 59.330 27.603 6317.543 6.703 122.779 1.982 0.79 402259. 0.2777
|
|
94.97 0.5065 0.7959 0.0412 0.0262 7.933 55.559 24.934 5915.979 6.277 110.908 1.912 0.80 403142. 0.2546
|
|
99.72 0.5318 0.8042 0.0367 0.0243 7.345 51.436 22.213 5476.981 5.811 98.802 1.840 0.80 404060. 0.2312
|
|
104.47 0.5572 0.8076 0.0322 0.0222 6.708 46.980 19.449 5002.484 5.308 86.509 1.763 0.80 405013. 0.2074
|
|
109.22 0.5825 0.8047 0.0275 0.0199 6.028 42.213 16.654 4494.854 4.769 74.077 1.681 0.80 406000. 0.1829
|
|
113.97 0.6078 0.7925 0.0229 0.0176 5.307 37.164 13.840 3957.284 4.199 61.559 1.586 0.80 407023. 0.1574
|
|
118.72 0.6331 0.7664 0.0182 0.0151 4.551 31.872 11.019 3393.707 3.601 49.012 1.473 0.80 408081. 0.1304
|
|
123.46 0.6585 0.7172 0.0136 0.0125 3.767 26.380 8.206 2808.955 2.980 36.499 1.325 0.80 409174. 0.1012
|
|
128.21 0.6838 0.6252 0.0090 0.0098 2.962 20.744 5.416 2208.783 2.344 24.092 1.112 0.80 410302. 0.0690
|
|
132.96 0.7091 0.4409 0.0044 0.0071 2.145 15.025 2.668 1599.827 1.697 11.868 0.756 0.81 411464. 0.0330
|
|
137.71 0.7345 -0.0093 -0.0001 0.0044 1.321 9.249 -0.034 984.874 1.045 -0.149 -0.015 0.81 412627. 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 0.0979 0.0392 16.256 102.460 73.063 12122.267 11.576 324.982 2.734 0.87 435407. 0.6232
|
|
5.33 0.0256 0.0627 0.0969 0.0396 16.412 103.441 72.350 12238.328 11.687 321.815 2.681 0.87 435702. 0.6083
|
|
10.66 0.0512 0.1229 0.0958 0.0399 16.551 104.319 71.540 12342.201 11.786 318.211 2.629 0.87 436028. 0.5931
|
|
15.99 0.0767 0.1806 0.0946 0.0402 16.669 105.064 70.622 12430.320 11.870 314.125 2.577 0.87 436385. 0.5776
|
|
21.32 0.1023 0.2360 0.0932 0.0404 16.761 105.644 69.582 12498.980 11.936 309.502 2.525 0.87 436774. 0.5618
|
|
26.65 0.1279 0.2890 0.0916 0.0406 16.822 106.028 68.411 12544.395 11.979 304.292 2.474 0.87 437198. 0.5457
|
|
31.98 0.1535 0.3396 0.0899 0.0406 16.847 106.183 67.096 12562.747 11.997 298.441 2.422 0.87 437657. 0.5292
|
|
37.31 0.1791 0.3879 0.0879 0.0406 16.830 106.078 65.626 12550.249 11.985 291.904 2.372 0.87 438152. 0.5124
|
|
42.64 0.2047 0.4339 0.0857 0.0404 16.767 105.682 63.992 12503.370 11.940 284.638 2.321 0.87 438685. 0.4953
|
|
47.97 0.2302 0.4776 0.0833 0.0402 16.654 104.967 62.188 12418.825 11.859 276.611 2.271 0.88 439256. 0.4777
|
|
53.30 0.2558 0.5190 0.0806 0.0398 16.486 103.909 60.207 12293.653 11.740 267.799 2.221 0.88 439866. 0.4597
|
|
58.63 0.2814 0.5581 0.0778 0.0392 16.260 102.485 58.046 12125.222 11.579 258.189 2.171 0.88 440515. 0.4412
|
|
63.96 0.3070 0.5948 0.0746 0.0385 15.973 100.674 55.706 11910.889 11.374 247.778 2.121 0.88 441203. 0.4223
|
|
69.29 0.3326 0.6291 0.0712 0.0377 15.620 98.451 53.185 11647.973 11.123 236.568 2.071 0.88 441930. 0.4028
|
|
74.61 0.3582 0.6609 0.0676 0.0366 15.199 95.794 50.485 11333.562 10.823 224.559 2.020 0.88 442696. 0.3829
|
|
79.94 0.3837 0.6902 0.0638 0.0355 14.706 92.688 47.615 10966.032 10.472 211.792 1.969 0.88 443502. 0.3625
|
|
85.27 0.4093 0.7170 0.0597 0.0341 14.143 89.141 44.596 10546.420 10.071 198.362 1.918 0.88 444348. 0.3416
|
|
90.60 0.4349 0.7410 0.0555 0.0326 13.513 85.167 41.446 10076.302 9.622 184.353 1.866 0.88 445232. 0.3203
|
|
95.93 0.4605 0.7612 0.0511 0.0309 12.831 80.870 38.181 9567.864 9.137 169.828 1.810 0.88 446156. 0.2983
|
|
101.26 0.4861 0.7770 0.0466 0.0292 12.098 76.251 34.814 9021.428 8.615 154.853 1.750 0.88 447119. 0.2755
|
|
106.59 0.5116 0.7874 0.0420 0.0273 11.320 71.351 31.360 8441.607 8.061 139.490 1.685 0.88 448121. 0.2517
|
|
111.92 0.5372 0.7904 0.0373 0.0253 10.509 66.235 27.832 7836.406 7.483 123.798 1.611 0.89 449162. 0.2267
|
|
117.25 0.5628 0.7858 0.0325 0.0233 9.648 60.808 24.248 7194.298 6.870 107.855 1.529 0.89 450243. 0.2008
|
|
122.58 0.5884 0.7707 0.0276 0.0211 8.747 55.128 20.622 6522.330 6.228 91.729 1.434 0.89 451363. 0.1737
|
|
127.91 0.6140 0.7408 0.0227 0.0188 7.815 49.254 16.973 5827.383 5.565 75.494 1.321 0.89 452522. 0.1452
|
|
133.24 0.6396 0.6893 0.0178 0.0166 6.864 43.263 13.317 5118.558 4.888 59.236 1.180 0.89 453720. 0.1149
|
|
138.57 0.6651 0.6054 0.0130 0.0142 5.907 37.231 9.678 4404.830 4.206 43.048 0.997 0.89 454958. 0.0827
|
|
143.90 0.6907 0.4706 0.0081 0.0120 4.957 31.242 6.079 3696.266 3.530 27.037 0.746 0.89 456236. 0.0490
|
|
149.23 0.7163 0.2515 0.0034 0.0097 4.026 25.378 2.545 3002.516 2.867 11.320 0.384 0.90 457551. 0.0164
|
|
154.56 0.7419
|
|
|
|
|
|
|
|
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 0.0967 0.0470 25.962 148.758 87.329 19359.867 16.807 388.439 2.046 0.96 478990. 0.5099
|
|
5.90 0.0257 0.0520 0.0959 0.0475 26.222 150.247 86.668 19553.604 16.975 385.497 2.010 0.96 479306. 0.4992
|
|
11.79 0.0515 0.1021 0.0951 0.0479 26.459 151.607 85.903 19730.648 17.129 382.097 1.975 0.96 479655. 0.4882
|
|
17.69 0.0772 0.1504 0.0941 0.0483 26.664 152.780 85.020 19883.188 17.261 378.171 1.939 0.96 480039. 0.4770
|
|
23.58 0.1029 0.1969 0.0930 0.0486 26.824 153.698 84.002 20002.688 17.365 373.642 1.905 0.96 480460. 0.4656
|
|
29.48 0.1286 0.2418 0.0917 0.0488 26.928 154.292 82.830 20079.975 17.432 368.428 1.871 0.96 480919. 0.4542
|
|
35.37 0.1544 0.2851 0.0902 0.0488 26.962 154.487 81.485 20105.453 17.454 362.446 1.838 0.96 481419. 0.4426
|
|
41.27 0.1801 0.3269 0.0885 0.0488 26.914 154.213 79.949 20069.746 17.423 355.612 1.807 0.96 481960. 0.4309
|
|
47.16 0.2058 0.3674 0.0866 0.0485 26.773 153.402 78.203 19964.256 17.331 347.847 1.777 0.96 482544. 0.4191
|
|
53.06 0.2315 0.4066 0.0844 0.0481 26.528 152.001 76.233 19781.822 17.173 339.085 1.748 0.96 483173. 0.4070
|
|
58.96 0.2573 0.4447 0.0819 0.0474 26.171 149.957 74.025 19515.799 16.942 329.263 1.720 0.96 483845. 0.3948
|
|
64.85 0.2830 0.4816 0.0792 0.0466 25.700 147.256 71.572 19164.303 16.637 318.352 1.694 0.96 484563. 0.3822
|
|
70.75 0.3087 0.5174 0.0762 0.0455 25.113 143.893 68.871 18726.684 16.257 306.340 1.668 0.96 485325. 0.3692
|
|
76.64 0.3344 0.5519 0.0730 0.0442 24.411 139.874 65.923 18203.570 15.803 293.224 1.643 0.97 486133. 0.3557
|
|
82.54 0.3602 0.5851 0.0694 0.0427 23.597 135.205 62.725 17595.939 15.275 279.002 1.617 0.97 486986. 0.3415
|
|
88.43 0.3859 0.6167 0.0656 0.0411 22.673 129.911 59.290 16906.969 14.677 263.724 1.591 0.97 487883. 0.3267
|
|
94.33 0.4116 0.6465 0.0616 0.0392 21.648 124.042 55.646 16143.175 14.014 247.511 1.563 0.97 488824. 0.3111
|
|
100.22 0.4373 0.6745 0.0574 0.0372 20.532 117.644 51.816 15310.563 13.291 230.476 1.535 0.97 489810. 0.2947
|
|
106.12 0.4631 0.7001 0.0529 0.0350 19.330 110.761 47.825 14414.744 12.514 212.725 1.505 0.97 490839. 0.2776
|
|
112.02 0.4888 0.7205 0.0484 0.0328 18.112 103.780 43.688 13506.189 11.725 194.326 1.467 0.97 491913. 0.2586
|
|
117.91 0.5145 0.7339 0.0436 0.0306 16.892 96.791 39.428 12596.710 10.935 175.375 1.420 0.97 493030. 0.2378
|
|
123.81 0.5402 0.7344 0.0388 0.0285 15.759 90.294 35.056 11751.143 10.201 155.928 1.353 0.97 494190. 0.2137
|
|
129.70 0.5660 0.7142 0.0339 0.0268 14.811 84.866 30.583 11044.731 9.588 136.035 1.256 0.98 495393. 0.1853
|
|
135.60 0.5917 0.6805 0.0289 0.0251 13.850 79.361 26.066 10328.245 8.966 115.941 1.145 0.98 496640. 0.1559
|
|
141.49 0.6174 0.6299 0.0238 0.0234 12.899 73.907 21.534 9618.486 8.350 95.784 1.015 0.98 497930. 0.1257
|
|
147.39 0.6432 0.5593 0.0188 0.0217 11.965 68.559 17.027 8922.462 7.746 75.736 0.866 0.98 499264. 0.0953
|
|
153.29 0.6689 0.4651 0.0139 0.0200 11.061 63.376 12.586 8247.975 7.160 55.985 0.692 0.98 500642. 0.0655
|
|
159.18 0.6946 0.3437 0.0091 0.0185 10.196 58.421 8.256 7603.088 6.600 36.721 0.493 0.98 502065. 0.0377
|
|
165.08 0.7203 0.1910 0.0045 0.0170 9.373 53.709 4.068 6989.788 6.068 18.096 0.264 0.98 503539. 0.0142
|
|
170.97 0.7461 -0.0013 0.0000 0.0155 8.544 48.954 -0.024 6370.986 5.531 -0.106 -0.002 0.99 505125. 0.0000
|
|
|
|
|
|
|