649 lines
115 KiB
Plaintext
649 lines
115 KiB
Plaintext
13x6 (13x6.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 0.0836 0.0391 0.001 0.073 0.075 0.859 0.008 0.334 39.713 0.05 16354. 0.4930
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0.26 0.0215 0.0448 0.0821 0.0393 0.001 0.073 0.074 0.863 0.008 0.328 38.800 0.05 16364. 0.4773
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0.53 0.0429 0.0874 0.0805 0.0395 0.001 0.073 0.072 0.867 0.008 0.322 37.879 0.05 16374. 0.4614
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0.79 0.0644 0.1279 0.0788 0.0396 0.001 0.074 0.071 0.870 0.008 0.315 36.950 0.05 16385. 0.4453
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1.05 0.0858 0.1663 0.0770 0.0397 0.001 0.074 0.069 0.872 0.008 0.308 36.014 0.05 16397. 0.4289
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1.32 0.1073 0.2024 0.0750 0.0398 0.001 0.074 0.067 0.872 0.008 0.300 35.072 0.05 16409. 0.4124
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1.58 0.1287 0.2363 0.0730 0.0398 0.001 0.074 0.066 0.872 0.008 0.292 34.123 0.05 16422. 0.3958
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1.84 0.1502 0.2680 0.0708 0.0397 0.001 0.074 0.064 0.871 0.008 0.283 33.167 0.05 16436. 0.3789
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2.11 0.1716 0.2973 0.0685 0.0396 0.001 0.073 0.062 0.868 0.008 0.274 32.203 0.05 16451. 0.3619
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2.37 0.1931 0.3244 0.0661 0.0394 0.001 0.073 0.059 0.863 0.008 0.264 31.230 0.05 16467. 0.3448
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2.63 0.2145 0.3491 0.0636 0.0391 0.001 0.072 0.057 0.857 0.008 0.254 30.246 0.05 16484. 0.3275
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2.90 0.2360 0.3713 0.0610 0.0387 0.001 0.072 0.055 0.850 0.008 0.244 29.250 0.05 16502. 0.3100
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3.16 0.2574 0.3911 0.0582 0.0383 0.001 0.071 0.052 0.841 0.008 0.233 28.239 0.05 16520. 0.2925
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3.42 0.2789 0.4083 0.0554 0.0378 0.001 0.070 0.050 0.830 0.008 0.221 27.211 0.05 16540. 0.2749
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3.69 0.3003 0.4227 0.0524 0.0373 0.001 0.069 0.047 0.817 0.008 0.210 26.162 0.05 16560. 0.2572
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3.95 0.3218 0.4343 0.0494 0.0366 0.001 0.068 0.044 0.803 0.008 0.198 25.088 0.05 16582. 0.2394
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4.21 0.3432 0.4429 0.0463 0.0359 0.001 0.067 0.042 0.787 0.008 0.185 23.983 0.05 16604. 0.2215
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4.48 0.3647 0.4482 0.0431 0.0351 0.001 0.065 0.039 0.769 0.007 0.172 22.842 0.05 16628. 0.2036
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4.74 0.3861 0.4499 0.0398 0.0342 0.001 0.063 0.036 0.750 0.007 0.159 21.657 0.05 16652. 0.1855
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5.00 0.4076 0.4478 0.0365 0.0332 0.001 0.062 0.033 0.728 0.007 0.146 20.420 0.05 16678. 0.1674
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5.27 0.4290 0.4413 0.0330 0.0321 0.001 0.060 0.030 0.705 0.007 0.132 19.119 0.05 16705. 0.1492
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5.53 0.4505 0.4300 0.0296 0.0310 0.001 0.057 0.027 0.680 0.006 0.118 17.741 0.05 16732. 0.1310
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5.79 0.4719 0.4131 0.0260 0.0297 0.001 0.055 0.023 0.652 0.006 0.104 16.268 0.05 16761. 0.1127
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6.06 0.4934 0.3896 0.0224 0.0284 0.001 0.053 0.020 0.623 0.006 0.090 14.678 0.05 16791. 0.0944
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6.32 0.5148 0.3585 0.0188 0.0270 0.001 0.050 0.017 0.592 0.006 0.075 12.944 0.05 16821. 0.0762
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6.58 0.5363 0.3182 0.0151 0.0255 0.001 0.047 0.014 0.560 0.005 0.061 11.029 0.05 16853. 0.0582
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6.84 0.5577 0.2666 0.0114 0.0239 0.001 0.044 0.010 0.525 0.005 0.046 8.884 0.05 16886. 0.0408
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7.11 0.5792 0.2008 0.0077 0.0223 0.001 0.041 0.007 0.488 0.005 0.031 6.444 0.05 16920. 0.0243
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7.37 0.6006 0.1169 0.0040 0.0205 0.001 0.038 0.004 0.450 0.004 0.016 3.618 0.05 16955. 0.0098
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7.63 0.6221 0.0088 0.0003 0.0187 0.001 0.035 0.000 0.410 0.004 0.001 0.264 0.05 16991. 0.0002
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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 0.0841 0.0335 0.008 0.248 0.302 5.876 0.028 1.345 23.335 0.10 32709. 0.5809
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0.53 0.0217 0.0530 0.0826 0.0337 0.008 0.250 0.297 5.921 0.028 1.321 22.742 0.10 32728. 0.5610
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1.06 0.0433 0.1032 0.0809 0.0340 0.008 0.252 0.291 5.961 0.028 1.295 22.150 0.10 32748. 0.5411
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1.59 0.0650 0.1507 0.0792 0.0341 0.008 0.253 0.285 5.993 0.029 1.267 21.560 0.10 32770. 0.5210
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2.13 0.0866 0.1955 0.0774 0.0343 0.008 0.254 0.278 6.019 0.029 1.238 20.972 0.10 32794. 0.5009
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2.66 0.1083 0.2375 0.0754 0.0344 0.008 0.255 0.271 6.035 0.029 1.207 20.387 0.10 32819. 0.4807
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3.19 0.1299 0.2769 0.0734 0.0344 0.008 0.255 0.264 6.042 0.029 1.174 19.804 0.10 32846. 0.4606
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3.72 0.1516 0.3136 0.0712 0.0344 0.008 0.255 0.256 6.039 0.029 1.139 19.225 0.10 32875. 0.4404
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4.25 0.1732 0.3476 0.0689 0.0343 0.008 0.255 0.248 6.024 0.029 1.102 18.648 0.10 32905. 0.4202
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4.78 0.1949 0.3790 0.0664 0.0342 0.008 0.253 0.239 5.996 0.029 1.063 18.073 0.10 32937. 0.4000
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5.32 0.2166 0.4078 0.0639 0.0339 0.008 0.252 0.230 5.955 0.028 1.022 17.499 0.10 32971. 0.3797
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5.85 0.2382 0.4338 0.0612 0.0336 0.008 0.249 0.220 5.900 0.028 0.979 16.925 0.10 33007. 0.3596
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6.38 0.2599 0.4572 0.0585 0.0332 0.008 0.246 0.210 5.831 0.028 0.935 16.351 0.10 33045. 0.3394
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6.91 0.2815 0.4778 0.0556 0.0327 0.008 0.243 0.200 5.747 0.027 0.889 15.774 0.10 33085. 0.3193
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7.44 0.3032 0.4956 0.0526 0.0322 0.008 0.239 0.189 5.648 0.027 0.841 15.192 0.10 33126. 0.2991
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7.97 0.3248 0.5104 0.0495 0.0315 0.007 0.234 0.178 5.533 0.026 0.792 14.602 0.10 33170. 0.2790
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8.50 0.3465 0.5221 0.0464 0.0308 0.007 0.228 0.167 5.403 0.026 0.742 14.003 0.10 33216. 0.2589
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9.04 0.3681 0.5304 0.0432 0.0300 0.007 0.222 0.155 5.257 0.025 0.690 13.390 0.10 33264. 0.2388
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9.57 0.3898 0.5351 0.0398 0.0290 0.007 0.215 0.143 5.094 0.024 0.637 12.758 0.10 33313. 0.2186
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10.10 0.4115 0.5358 0.0365 0.0280 0.007 0.208 0.131 4.915 0.023 0.583 12.102 0.10 33365. 0.1984
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10.63 0.4331 0.5319 0.0330 0.0269 0.006 0.199 0.119 4.718 0.023 0.528 11.414 0.10 33419. 0.1781
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11.16 0.4548 0.5229 0.0295 0.0257 0.006 0.190 0.106 4.504 0.022 0.472 10.685 0.10 33476. 0.1576
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11.69 0.4764 0.5077 0.0259 0.0243 0.006 0.181 0.093 4.273 0.020 0.415 9.903 0.10 33534. 0.1369
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12.23 0.4981 0.4851 0.0223 0.0229 0.005 0.170 0.080 4.025 0.019 0.357 9.050 0.10 33595. 0.1161
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12.76 0.5197 0.4533 0.0187 0.0214 0.005 0.159 0.067 3.759 0.018 0.299 8.105 0.10 33657. 0.0951
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13.29 0.5414 0.4099 0.0150 0.0198 0.005 0.147 0.054 3.476 0.017 0.240 7.036 0.10 33722. 0.0740
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13.82 0.5630 0.3511 0.0113 0.0181 0.004 0.134 0.041 3.177 0.015 0.181 5.795 0.10 33789. 0.0529
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14.35 0.5847 0.2713 0.0076 0.0163 0.004 0.121 0.027 2.861 0.014 0.121 4.312 0.10 33858. 0.0322
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14.88 0.6064 0.1615 0.0038 0.0144 0.003 0.107 0.014 2.529 0.012 0.061 2.475 0.10 33929. 0.0132
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15.41 0.6280 0.0053 0.0001 0.0124 0.003 0.092 0.000 2.181 0.010 0.002 0.079 0.10 34001. 0.0001
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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 0.0844 0.0312 0.025 0.520 0.683 18.461 0.059 3.037 16.772 0.15 49062. 0.6274
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0.80 0.0218 0.0573 0.0829 0.0314 0.025 0.525 0.670 18.627 0.059 2.982 16.325 0.15 49091. 0.6052
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1.60 0.0435 0.1115 0.0812 0.0317 0.025 0.529 0.657 18.775 0.060 2.924 15.880 0.15 49122. 0.5829
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2.40 0.0653 0.1627 0.0795 0.0319 0.025 0.532 0.643 18.900 0.060 2.862 15.439 0.15 49155. 0.5607
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3.20 0.0870 0.2107 0.0777 0.0321 0.025 0.535 0.628 18.999 0.060 2.795 15.003 0.15 49191. 0.5385
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4.01 0.1088 0.2558 0.0757 0.0322 0.026 0.537 0.613 19.069 0.061 2.725 14.571 0.15 49229. 0.5163
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4.81 0.1305 0.2980 0.0736 0.0323 0.026 0.538 0.596 19.105 0.061 2.650 14.143 0.15 49270. 0.4942
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5.61 0.1523 0.3373 0.0714 0.0323 0.026 0.538 0.578 19.105 0.061 2.571 13.720 0.15 49313. 0.4722
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6.41 0.1741 0.3737 0.0691 0.0322 0.026 0.537 0.559 19.065 0.061 2.487 13.302 0.15 49359. 0.4503
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7.21 0.1958 0.4073 0.0667 0.0320 0.025 0.535 0.539 18.980 0.060 2.399 12.888 0.15 49408. 0.4285
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8.01 0.2176 0.4382 0.0641 0.0318 0.025 0.531 0.519 18.849 0.060 2.306 12.477 0.15 49459. 0.4068
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8.81 0.2393 0.4663 0.0614 0.0315 0.025 0.526 0.497 18.670 0.059 2.210 12.070 0.15 49513. 0.3852
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9.61 0.2611 0.4916 0.0586 0.0311 0.025 0.520 0.474 18.441 0.059 2.109 11.664 0.15 49570. 0.3637
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10.41 0.2829 0.5141 0.0557 0.0307 0.024 0.512 0.451 18.159 0.058 2.005 11.260 0.15 49630. 0.3423
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11.21 0.3046 0.5337 0.0527 0.0301 0.024 0.502 0.427 17.825 0.057 1.897 10.855 0.15 49693. 0.3210
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12.02 0.3264 0.5503 0.0496 0.0294 0.023 0.491 0.402 17.436 0.056 1.786 10.447 0.16 49760. 0.2998
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12.82 0.3481 0.5639 0.0465 0.0287 0.023 0.479 0.376 16.992 0.054 1.672 10.036 0.16 49829. 0.2786
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13.62 0.3699 0.5741 0.0432 0.0278 0.022 0.465 0.350 16.490 0.052 1.555 9.617 0.16 49901. 0.2575
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14.42 0.3916 0.5808 0.0399 0.0269 0.021 0.449 0.323 15.930 0.051 1.435 9.188 0.16 49976. 0.2363
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15.22 0.4134 0.5835 0.0365 0.0258 0.021 0.431 0.295 15.310 0.049 1.313 8.744 0.16 50055. 0.2151
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16.02 0.4352 0.5816 0.0330 0.0247 0.020 0.412 0.267 14.629 0.047 1.188 8.281 0.16 50137. 0.1938
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16.82 0.4569 0.5746 0.0295 0.0234 0.019 0.391 0.239 13.887 0.044 1.061 7.791 0.16 50222. 0.1723
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17.62 0.4787 0.5613 0.0259 0.0221 0.018 0.369 0.210 13.084 0.042 0.932 7.265 0.16 50310. 0.1506
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18.42 0.5004 0.5403 0.0223 0.0206 0.016 0.344 0.180 12.218 0.039 0.801 6.689 0.16 50402. 0.1286
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19.23 0.5222 0.5096 0.0186 0.0191 0.015 0.318 0.151 11.291 0.036 0.669 6.046 0.16 50497. 0.1062
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20.03 0.5439 0.4660 0.0149 0.0174 0.014 0.290 0.121 10.303 0.033 0.536 5.307 0.16 50595. 0.0834
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20.83 0.5657 0.4047 0.0112 0.0156 0.012 0.261 0.090 9.255 0.029 0.402 4.432 0.16 50696. 0.0603
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21.63 0.5875 0.3178 0.0074 0.0138 0.011 0.230 0.060 8.149 0.026 0.268 3.352 0.16 50801. 0.0372
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22.43 0.6092 0.1916 0.0037 0.0118 0.009 0.197 0.030 6.988 0.022 0.134 1.948 0.16 50908. 0.0153
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23.23 0.6310 -0.0027 0.0000 0.0097 0.008 0.162 0.000 5.763 0.018 -0.002 -0.027 0.16 51015. 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 0.0847 0.0299 0.056 0.887 1.218 41.975 0.100 5.418 13.162 0.21 65415. 0.6577
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1.07 0.0218 0.0600 0.0832 0.0302 0.057 0.896 1.196 42.388 0.101 5.321 12.801 0.21 65454. 0.6339
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2.14 0.0436 0.1167 0.0815 0.0305 0.057 0.903 1.173 42.758 0.102 5.217 12.443 0.21 65495. 0.6101
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3.21 0.0654 0.1701 0.0798 0.0307 0.058 0.910 1.148 43.074 0.103 5.107 12.089 0.21 65540. 0.5865
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4.28 0.0872 0.2203 0.0780 0.0309 0.058 0.916 1.121 43.328 0.103 4.988 11.740 0.21 65588. 0.5629
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5.35 0.1090 0.2673 0.0760 0.0310 0.058 0.919 1.093 43.512 0.104 4.863 11.396 0.21 65639. 0.5395
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6.42 0.1308 0.3112 0.0739 0.0311 0.058 0.922 1.063 43.616 0.104 4.729 11.057 0.21 65693. 0.5162
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7.49 0.1526 0.3521 0.0717 0.0311 0.059 0.922 1.031 43.632 0.104 4.588 10.722 0.21 65751. 0.4930
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8.56 0.1744 0.3900 0.0694 0.0310 0.058 0.920 0.998 43.551 0.104 4.439 10.393 0.21 65812. 0.4701
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9.63 0.1962 0.4251 0.0669 0.0309 0.058 0.916 0.963 43.363 0.104 4.281 10.068 0.21 65877. 0.4472
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10.70 0.2180 0.4573 0.0643 0.0307 0.058 0.910 0.925 43.063 0.103 4.117 9.748 0.21 65946. 0.4246
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11.77 0.2398 0.4866 0.0616 0.0304 0.057 0.901 0.887 42.646 0.102 3.944 9.431 0.21 66018. 0.4021
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12.84 0.2616 0.5132 0.0588 0.0300 0.056 0.890 0.846 42.107 0.101 3.765 9.117 0.21 66095. 0.3798
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13.91 0.2834 0.5370 0.0559 0.0295 0.056 0.876 0.805 41.443 0.099 3.579 8.806 0.21 66175. 0.3576
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14.98 0.3052 0.5579 0.0529 0.0290 0.055 0.859 0.761 40.650 0.097 3.386 8.495 0.21 66260. 0.3356
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16.05 0.3270 0.5759 0.0498 0.0283 0.053 0.839 0.717 39.725 0.095 3.188 8.184 0.21 66348. 0.3137
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17.12 0.3488 0.5908 0.0466 0.0275 0.052 0.817 0.671 38.663 0.092 2.984 7.871 0.21 66441. 0.2919
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18.19 0.3705 0.6024 0.0434 0.0267 0.050 0.792 0.624 37.461 0.089 2.775 7.555 0.21 66537. 0.2702
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19.26 0.3923 0.6106 0.0400 0.0257 0.048 0.763 0.576 36.117 0.086 2.561 7.232 0.21 66638. 0.2485
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20.33 0.4141 0.6149 0.0366 0.0247 0.046 0.732 0.527 34.628 0.083 2.343 6.899 0.21 66744. 0.2267
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21.40 0.4359 0.6148 0.0331 0.0235 0.044 0.697 0.477 32.990 0.079 2.120 6.553 0.21 66853. 0.2048
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22.47 0.4577 0.6095 0.0296 0.0222 0.042 0.659 0.426 31.203 0.074 1.893 6.188 0.21 66967. 0.1828
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23.54 0.4795 0.5981 0.0260 0.0208 0.039 0.618 0.374 29.265 0.070 1.663 5.796 0.21 67085. 0.1605
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24.61 0.5013 0.5791 0.0224 0.0194 0.036 0.574 0.322 27.176 0.065 1.430 5.367 0.21 67208. 0.1378
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25.68 0.5231 0.5501 0.0187 0.0178 0.033 0.527 0.269 24.935 0.060 1.195 4.886 0.21 67334. 0.1146
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26.75 0.5449 0.5077 0.0150 0.0161 0.030 0.476 0.215 22.546 0.054 0.957 4.329 0.21 67466. 0.0909
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27.82 0.5667 0.4464 0.0112 0.0143 0.027 0.423 0.162 20.011 0.048 0.718 3.661 0.21 67601. 0.0666
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28.89 0.5885 0.3567 0.0075 0.0123 0.023 0.366 0.108 17.336 0.041 0.479 2.817 0.21 67741. 0.0418
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29.96 0.6103 0.2208 0.0037 0.0103 0.019 0.307 0.054 14.524 0.035 0.239 1.681 0.21 67885. 0.0177
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31.03 0.6321 -0.0020 0.0000 0.0082 0.015 0.244 0.000 11.551 0.028 -0.002 -0.015 0.21 68026. 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 0.0850 0.0291 0.107 1.350 1.911 79.840 0.152 8.501 10.857 0.26 81767. 0.6796
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1.36 0.0221 0.0627 0.0835 0.0294 0.108 1.364 1.877 80.685 0.154 8.347 10.550 0.26 81816. 0.6543
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2.71 0.0442 0.1217 0.0819 0.0297 0.109 1.377 1.840 81.441 0.156 8.183 10.246 0.26 81869. 0.6292
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4.07 0.0663 0.1773 0.0801 0.0299 0.110 1.388 1.800 82.089 0.157 8.007 9.946 0.26 81926. 0.6042
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5.42 0.0883 0.2294 0.0782 0.0301 0.111 1.397 1.758 82.612 0.158 7.819 9.651 0.26 81986. 0.5794
|
|
6.78 0.1104 0.2781 0.0762 0.0303 0.111 1.403 1.713 82.991 0.159 7.619 9.362 0.26 82051. 0.5547
|
|
8.13 0.1325 0.3236 0.0741 0.0303 0.112 1.407 1.665 83.208 0.159 7.407 9.077 0.26 82120. 0.5303
|
|
9.49 0.1546 0.3659 0.0718 0.0304 0.112 1.407 1.615 83.245 0.159 7.181 8.797 0.26 82194. 0.5061
|
|
10.84 0.1767 0.4051 0.0695 0.0303 0.111 1.404 1.561 83.082 0.159 6.943 8.522 0.26 82272. 0.4821
|
|
12.20 0.1988 0.4413 0.0669 0.0302 0.111 1.398 1.505 82.703 0.158 6.692 8.252 0.26 82355. 0.4583
|
|
13.55 0.2209 0.4745 0.0643 0.0299 0.110 1.388 1.445 82.095 0.157 6.429 7.986 0.26 82443. 0.4347
|
|
14.91 0.2430 0.5048 0.0616 0.0296 0.109 1.373 1.384 81.247 0.155 6.154 7.724 0.26 82536. 0.4113
|
|
16.26 0.2650 0.5323 0.0587 0.0292 0.107 1.355 1.319 80.150 0.153 5.868 7.465 0.26 82634. 0.3882
|
|
17.62 0.2871 0.5568 0.0557 0.0287 0.106 1.332 1.252 78.797 0.150 5.571 7.209 0.26 82736. 0.3653
|
|
18.97 0.3092 0.5785 0.0527 0.0281 0.103 1.305 1.183 77.180 0.147 5.264 6.954 0.26 82844. 0.3425
|
|
20.33 0.3313 0.5971 0.0495 0.0275 0.101 1.273 1.112 75.290 0.144 4.947 6.700 0.26 82957. 0.3199
|
|
21.68 0.3534 0.6127 0.0462 0.0267 0.098 1.236 1.039 73.121 0.140 4.622 6.445 0.26 83076. 0.2975
|
|
23.04 0.3755 0.6250 0.0429 0.0258 0.095 1.195 0.964 70.667 0.135 4.288 6.188 0.26 83199. 0.2751
|
|
24.40 0.3976 0.6337 0.0395 0.0248 0.091 1.148 0.887 67.919 0.130 3.947 5.925 0.26 83329. 0.2527
|
|
25.75 0.4196 0.6384 0.0360 0.0237 0.087 1.097 0.809 64.873 0.124 3.598 5.655 0.26 83463. 0.2303
|
|
27.11 0.4417 0.6386 0.0324 0.0224 0.083 1.040 0.729 61.524 0.118 3.242 5.374 0.26 83603. 0.2077
|
|
28.46 0.4638 0.6335 0.0288 0.0211 0.078 0.978 0.648 57.869 0.111 2.881 5.077 0.26 83749. 0.1850
|
|
29.82 0.4859 0.6218 0.0252 0.0197 0.072 0.911 0.565 53.904 0.103 2.514 4.757 0.26 83900. 0.1619
|
|
31.17 0.5080 0.6018 0.0214 0.0181 0.067 0.839 0.482 49.630 0.095 2.143 4.404 0.26 84057. 0.1384
|
|
32.53 0.5301 0.5707 0.0177 0.0164 0.060 0.762 0.398 45.049 0.086 1.768 4.002 0.26 84220. 0.1143
|
|
33.88 0.5522 0.5243 0.0139 0.0146 0.054 0.679 0.313 40.165 0.077 1.390 3.530 0.26 84388. 0.0893
|
|
35.24 0.5742 0.4550 0.0101 0.0128 0.047 0.591 0.227 34.986 0.067 1.011 2.946 0.26 84562. 0.0636
|
|
36.59 0.5963 0.3493 0.0063 0.0108 0.040 0.499 0.142 29.523 0.056 0.630 2.177 0.26 84741. 0.0371
|
|
37.95 0.6184 0.1786 0.0025 0.0087 0.032 0.402 0.056 23.782 0.045 0.250 1.074 0.26 84924. 0.0115
|
|
39.30 0.6405
|
|
|
|
|
|
|
|
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 0.0854 0.0286 0.182 1.910 2.765 135.611 0.216 12.299 9.249 0.31 98118. 0.6963
|
|
1.62 0.0220 0.0638 0.0839 0.0289 0.184 1.931 2.716 137.105 0.218 12.079 8.984 0.31 98176. 0.6703
|
|
3.24 0.0440 0.1240 0.0823 0.0292 0.186 1.950 2.663 138.444 0.220 11.843 8.723 0.31 98240. 0.6445
|
|
4.86 0.0660 0.1805 0.0805 0.0295 0.187 1.967 2.606 139.596 0.222 11.591 8.467 0.31 98308. 0.6188
|
|
6.48 0.0881 0.2335 0.0786 0.0297 0.188 1.980 2.545 140.532 0.224 11.321 8.214 0.31 98380. 0.5933
|
|
8.10 0.1101 0.2831 0.0766 0.0298 0.189 1.989 2.481 141.219 0.225 11.034 7.967 0.31 98458. 0.5681
|
|
9.73 0.1321 0.3293 0.0745 0.0299 0.190 1.995 2.412 141.626 0.225 10.728 7.724 0.31 98541. 0.5431
|
|
11.35 0.1541 0.3724 0.0723 0.0299 0.190 1.996 2.339 141.721 0.226 10.405 7.486 0.31 98629. 0.5184
|
|
12.97 0.1761 0.4123 0.0699 0.0299 0.190 1.993 2.262 141.470 0.225 10.063 7.253 0.31 98723. 0.4939
|
|
14.59 0.1981 0.4492 0.0674 0.0297 0.189 1.984 2.181 140.845 0.224 9.702 7.024 0.31 98822. 0.4697
|
|
16.21 0.2201 0.4832 0.0648 0.0295 0.188 1.970 2.096 139.822 0.223 9.324 6.800 0.31 98927. 0.4457
|
|
17.83 0.2421 0.5142 0.0620 0.0292 0.186 1.949 2.007 138.382 0.220 8.928 6.579 0.31 99037. 0.4220
|
|
19.45 0.2642 0.5424 0.0592 0.0288 0.183 1.923 1.915 136.511 0.217 8.516 6.361 0.31 99154. 0.3985
|
|
21.07 0.2862 0.5678 0.0562 0.0283 0.180 1.890 1.819 134.194 0.214 8.089 6.147 0.31 99277. 0.3753
|
|
22.69 0.3082 0.5903 0.0531 0.0277 0.176 1.851 1.719 131.418 0.209 7.647 5.934 0.31 99406. 0.3523
|
|
24.31 0.3302 0.6099 0.0500 0.0270 0.172 1.806 1.617 128.168 0.204 7.192 5.722 0.31 99541. 0.3294
|
|
25.93 0.3522 0.6265 0.0467 0.0263 0.167 1.753 1.512 124.433 0.198 6.724 5.510 0.31 99682. 0.3067
|
|
27.56 0.3742 0.6398 0.0434 0.0254 0.161 1.693 1.404 120.201 0.191 6.244 5.297 0.31 99830. 0.2841
|
|
29.18 0.3962 0.6498 0.0400 0.0244 0.155 1.626 1.293 115.459 0.184 5.752 5.080 0.31 99984. 0.2616
|
|
30.80 0.4182 0.6560 0.0365 0.0233 0.148 1.552 1.180 110.198 0.175 5.250 4.858 0.31 100145. 0.2390
|
|
32.42 0.4403 0.6578 0.0329 0.0220 0.140 1.471 1.065 104.409 0.166 4.739 4.628 0.31 100312. 0.2163
|
|
34.04 0.4623 0.6545 0.0293 0.0207 0.132 1.382 0.948 98.086 0.156 4.219 4.386 0.31 100486. 0.1934
|
|
35.66 0.4843 0.6450 0.0256 0.0193 0.122 1.285 0.830 91.224 0.145 3.691 4.126 0.31 100666. 0.1702
|
|
37.28 0.5063 0.6276 0.0219 0.0177 0.112 1.181 0.710 83.823 0.133 3.156 3.840 0.31 100854. 0.1465
|
|
38.90 0.5283 0.5996 0.0182 0.0160 0.102 1.069 0.588 75.886 0.121 2.616 3.516 0.31 101048. 0.1221
|
|
40.52 0.5503 0.5567 0.0144 0.0142 0.090 0.950 0.466 67.421 0.107 2.072 3.134 0.31 101248. 0.0968
|
|
42.14 0.5723 0.4917 0.0106 0.0123 0.078 0.823 0.343 58.439 0.093 1.525 2.661 0.31 101455. 0.0706
|
|
43.76 0.5943 0.3905 0.0068 0.0103 0.066 0.690 0.220 48.960 0.078 0.977 2.035 0.31 101669. 0.0432
|
|
45.39 0.6164 0.2236 0.0030 0.0082 0.052 0.549 0.097 38.999 0.062 0.430 1.124 0.31 101888. 0.0158
|
|
47.01 0.6384
|
|
|
|
|
|
|
|
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 0.0859 0.0283 0.286 2.572 3.785 213.039 0.291 16.834 8.057 0.36 114467. 0.7097
|
|
1.88 0.0219 0.0645 0.0844 0.0286 0.289 2.601 3.718 215.447 0.294 16.536 7.827 0.36 114535. 0.6832
|
|
3.76 0.0437 0.1252 0.0828 0.0289 0.292 2.628 3.646 217.610 0.297 16.216 7.599 0.36 114608. 0.6569
|
|
5.64 0.0656 0.1822 0.0810 0.0292 0.294 2.650 3.569 219.480 0.299 15.875 7.375 0.36 114687. 0.6308
|
|
7.51 0.0875 0.2358 0.0792 0.0294 0.296 2.669 3.487 221.005 0.301 15.510 7.156 0.36 114771. 0.6050
|
|
9.39 0.1093 0.2858 0.0772 0.0295 0.298 2.682 3.400 222.139 0.303 15.121 6.941 0.36 114861. 0.5794
|
|
11.27 0.1312 0.3326 0.0751 0.0296 0.299 2.691 3.307 222.830 0.304 14.708 6.731 0.36 114957. 0.5541
|
|
13.15 0.1531 0.3762 0.0728 0.0296 0.299 2.693 3.208 223.027 0.304 14.270 6.525 0.36 115059. 0.5291
|
|
15.03 0.1749 0.4166 0.0705 0.0296 0.299 2.689 3.104 222.681 0.304 13.807 6.323 0.36 115168. 0.5044
|
|
16.91 0.1968 0.4540 0.0680 0.0295 0.297 2.677 2.994 221.742 0.302 13.319 6.125 0.36 115283. 0.4799
|
|
18.79 0.2187 0.4885 0.0654 0.0293 0.295 2.659 2.879 220.173 0.300 12.807 5.932 0.36 115404. 0.4557
|
|
20.67 0.2405 0.5202 0.0626 0.0290 0.292 2.632 2.759 217.945 0.297 12.271 5.742 0.36 115532. 0.4318
|
|
22.54 0.2624 0.5490 0.0598 0.0286 0.288 2.596 2.633 215.034 0.293 11.714 5.555 0.36 115667. 0.4081
|
|
24.42 0.2843 0.5750 0.0568 0.0281 0.284 2.553 2.503 211.416 0.288 11.135 5.371 0.36 115809. 0.3847
|
|
26.30 0.3062 0.5983 0.0538 0.0275 0.278 2.500 2.369 207.071 0.282 10.537 5.189 0.36 115958. 0.3616
|
|
28.18 0.3280 0.6187 0.0506 0.0268 0.271 2.439 2.230 201.977 0.276 9.920 5.008 0.36 116114. 0.3386
|
|
30.06 0.3499 0.6362 0.0474 0.0261 0.263 2.368 2.088 196.114 0.268 9.286 4.828 0.36 116277. 0.3158
|
|
31.94 0.3718 0.6507 0.0441 0.0252 0.254 2.288 1.941 189.462 0.258 8.635 4.647 0.36 116448. 0.2932
|
|
33.82 0.3936 0.6619 0.0407 0.0242 0.244 2.198 1.792 182.004 0.248 7.969 4.465 0.36 116626. 0.2706
|
|
35.69 0.4155 0.6694 0.0372 0.0231 0.233 2.098 1.639 173.722 0.237 7.288 4.278 0.36 116811. 0.2479
|
|
37.57 0.4374 0.6730 0.0337 0.0219 0.221 1.988 1.483 164.604 0.225 6.595 4.085 0.36 117004. 0.2252
|
|
39.45 0.4592 0.6717 0.0301 0.0206 0.207 1.867 1.324 154.638 0.211 5.889 3.884 0.36 117205. 0.2023
|
|
41.33 0.4811 0.6646 0.0264 0.0191 0.193 1.737 1.163 143.818 0.196 5.173 3.668 0.36 117413. 0.1791
|
|
43.21 0.5030 0.6502 0.0227 0.0176 0.177 1.596 1.000 132.141 0.180 4.448 3.432 0.36 117629. 0.1554
|
|
45.09 0.5248 0.6260 0.0190 0.0159 0.160 1.444 0.835 119.610 0.163 3.715 3.167 0.36 117852. 0.1310
|
|
46.97 0.5467 0.5881 0.0152 0.0141 0.142 1.283 0.669 106.237 0.145 2.976 2.856 0.37 118084. 0.1058
|
|
48.84 0.5686 0.5297 0.0114 0.0122 0.123 1.111 0.502 92.040 0.126 2.233 2.474 0.37 118323. 0.0793
|
|
50.72 0.5904 0.4379 0.0076 0.0102 0.103 0.930 0.335 77.048 0.105 1.488 1.969 0.37 118569. 0.0516
|
|
52.60 0.6123 0.2852 0.0038 0.0081 0.082 0.740 0.167 61.288 0.084 0.743 1.237 0.37 118822. 0.0229
|
|
54.48 0.6342 -0.0062 -0.0001 0.0059 0.060 0.537 -0.003 44.493 0.061 -0.011 -0.026 0.37 119061. 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 0.0865 0.0281 0.424 3.340 4.974 316.140 0.377 22.127 7.137 0.41 130814. 0.7207
|
|
2.15 0.0219 0.0653 0.0849 0.0285 0.429 3.379 4.887 319.811 0.382 21.737 6.931 0.41 130892. 0.6937
|
|
4.30 0.0438 0.1269 0.0833 0.0288 0.433 3.414 4.793 323.111 0.386 21.319 6.728 0.41 130976. 0.6669
|
|
6.45 0.0657 0.1846 0.0816 0.0290 0.437 3.444 4.692 325.963 0.389 20.871 6.529 0.41 131067. 0.6403
|
|
8.60 0.0876 0.2388 0.0797 0.0292 0.440 3.469 4.585 328.295 0.392 20.392 6.334 0.41 131163. 0.6140
|
|
10.75 0.1095 0.2896 0.0777 0.0294 0.443 3.487 4.470 330.030 0.394 19.882 6.143 0.41 131267. 0.5880
|
|
12.90 0.1314 0.3369 0.0756 0.0295 0.444 3.498 4.348 331.094 0.395 19.340 5.956 0.41 131377. 0.5623
|
|
15.05 0.1533 0.3810 0.0733 0.0295 0.444 3.501 4.219 331.409 0.396 18.765 5.774 0.41 131494. 0.5369
|
|
17.20 0.1752 0.4220 0.0709 0.0295 0.444 3.496 4.082 330.897 0.395 18.156 5.595 0.41 131619. 0.5118
|
|
19.35 0.1971 0.4599 0.0684 0.0293 0.442 3.481 3.938 329.486 0.393 17.514 5.420 0.41 131750. 0.4870
|
|
21.50 0.2190 0.4949 0.0658 0.0291 0.439 3.456 3.786 327.119 0.390 16.841 5.250 0.41 131890. 0.4625
|
|
23.65 0.2409 0.5270 0.0631 0.0288 0.434 3.421 3.628 323.751 0.386 16.136 5.082 0.41 132037. 0.4383
|
|
25.80 0.2628 0.5563 0.0602 0.0284 0.428 3.374 3.463 319.345 0.381 15.402 4.918 0.41 132192. 0.4143
|
|
27.95 0.2847 0.5829 0.0572 0.0279 0.421 3.316 3.291 313.867 0.375 14.640 4.756 0.41 132354. 0.3907
|
|
30.10 0.3066 0.6067 0.0541 0.0274 0.412 3.247 3.114 307.285 0.367 13.853 4.597 0.41 132525. 0.3673
|
|
32.26 0.3285 0.6277 0.0510 0.0267 0.402 3.165 2.932 299.567 0.358 13.040 4.439 0.41 132704. 0.3441
|
|
34.41 0.3504 0.6458 0.0477 0.0259 0.390 3.071 2.744 290.681 0.347 12.205 4.282 0.41 132892. 0.3211
|
|
36.56 0.3723 0.6609 0.0443 0.0250 0.376 2.965 2.551 280.598 0.335 11.348 4.124 0.41 133087. 0.2982
|
|
38.71 0.3942 0.6728 0.0409 0.0240 0.361 2.845 2.354 269.292 0.321 10.471 3.965 0.41 133291. 0.2754
|
|
40.86 0.4161 0.6812 0.0374 0.0229 0.344 2.712 2.153 256.736 0.306 9.575 3.803 0.41 133504. 0.2526
|
|
43.01 0.4380 0.6856 0.0338 0.0216 0.326 2.566 1.947 242.912 0.290 8.662 3.636 0.42 133725. 0.2297
|
|
45.16 0.4599 0.6853 0.0302 0.0203 0.305 2.407 1.738 227.801 0.272 7.733 3.461 0.42 133955. 0.2066
|
|
47.31 0.4818 0.6792 0.0265 0.0188 0.283 2.233 1.526 211.394 0.252 6.790 3.275 0.42 134194. 0.1832
|
|
49.46 0.5037 0.6660 0.0228 0.0172 0.260 2.046 1.312 193.687 0.231 5.834 3.072 0.42 134442. 0.1593
|
|
51.61 0.5256 0.6430 0.0190 0.0156 0.234 1.846 1.095 174.686 0.209 4.868 2.842 0.42 134698. 0.1346
|
|
53.76 0.5475 0.6062 0.0152 0.0137 0.207 1.631 0.876 154.408 0.184 3.895 2.572 0.42 134963. 0.1090
|
|
55.91 0.5694 0.5485 0.0114 0.0118 0.178 1.404 0.656 132.882 0.159 2.916 2.238 0.42 135237. 0.0820
|
|
58.06 0.5914 0.4560 0.0076 0.0098 0.148 1.164 0.435 110.151 0.131 1.935 1.791 0.42 135519. 0.0535
|
|
60.21 0.6133 0.2979 0.0037 0.0077 0.116 0.911 0.215 86.256 0.103 0.955 1.129 0.42 135809. 0.0237
|
|
62.36 0.6352 -0.0212 -0.0002 0.0054 0.081 0.640 -0.010 60.606 0.072 -0.046 -0.077 0.42 136072. 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 0.0871 0.0281 0.602 4.219 6.342 449.283 0.477 28.208 6.402 0.46 147159. 0.7299
|
|
2.45 0.0222 0.0667 0.0855 0.0284 0.610 4.270 6.229 454.671 0.482 27.708 6.214 0.46 147248. 0.7022
|
|
4.90 0.0443 0.1294 0.0839 0.0287 0.616 4.315 6.109 459.509 0.488 27.171 6.030 0.46 147344. 0.6747
|
|
7.35 0.0665 0.1883 0.0821 0.0290 0.622 4.355 5.979 463.681 0.492 26.595 5.849 0.46 147448. 0.6475
|
|
9.79 0.0887 0.2435 0.0802 0.0292 0.626 4.386 5.840 467.076 0.496 25.978 5.672 0.46 147558. 0.6206
|
|
12.24 0.1108 0.2951 0.0782 0.0294 0.630 4.410 5.693 469.583 0.498 25.320 5.498 0.46 147677. 0.5940
|
|
14.69 0.1330 0.3432 0.0760 0.0295 0.632 4.424 5.535 471.087 0.500 24.620 5.329 0.46 147803. 0.5677
|
|
17.14 0.1552 0.3880 0.0737 0.0295 0.632 4.428 5.368 471.475 0.500 23.877 5.164 0.46 147938. 0.5417
|
|
19.59 0.1773 0.4296 0.0713 0.0294 0.631 4.420 5.191 470.630 0.499 23.090 5.003 0.46 148080. 0.5161
|
|
22.04 0.1995 0.4681 0.0687 0.0293 0.628 4.399 5.004 468.445 0.497 22.259 4.845 0.46 148232. 0.4908
|
|
24.49 0.2217 0.5036 0.0660 0.0291 0.623 4.365 4.808 464.837 0.493 21.386 4.692 0.46 148392. 0.4658
|
|
26.93 0.2439 0.5362 0.0632 0.0287 0.617 4.318 4.603 459.741 0.488 20.473 4.541 0.46 148561. 0.4411
|
|
29.38 0.2660 0.5659 0.0603 0.0283 0.608 4.255 4.389 453.103 0.481 19.522 4.393 0.46 148739. 0.4167
|
|
31.83 0.2882 0.5929 0.0572 0.0278 0.597 4.178 4.167 444.872 0.472 18.535 4.248 0.46 148926. 0.3927
|
|
34.28 0.3104 0.6170 0.0541 0.0272 0.583 4.085 3.937 435.001 0.462 17.514 4.106 0.46 149122. 0.3688
|
|
36.73 0.3325 0.6383 0.0508 0.0265 0.568 3.977 3.701 423.442 0.449 16.461 3.964 0.47 149328. 0.3453
|
|
39.18 0.3547 0.6567 0.0475 0.0256 0.550 3.852 3.457 410.151 0.435 15.378 3.823 0.47 149543. 0.3219
|
|
41.63 0.3769 0.6720 0.0440 0.0247 0.530 3.710 3.208 395.082 0.419 14.267 3.682 0.47 149768. 0.2986
|
|
44.07 0.3990 0.6840 0.0405 0.0236 0.507 3.552 2.952 378.198 0.401 13.130 3.540 0.47 150003. 0.2754
|
|
46.52 0.4212 0.6925 0.0370 0.0225 0.482 3.376 2.691 359.462 0.381 11.969 3.395 0.47 150247. 0.2522
|
|
48.97 0.4434 0.6968 0.0333 0.0212 0.454 3.182 2.425 338.845 0.360 10.785 3.246 0.47 150502. 0.2288
|
|
51.42 0.4655 0.6962 0.0296 0.0198 0.424 2.971 2.154 316.323 0.336 9.581 3.089 0.47 150767. 0.2052
|
|
53.87 0.4877 0.6897 0.0258 0.0183 0.391 2.741 1.879 291.883 0.310 8.359 2.920 0.47 151041. 0.1813
|
|
56.32 0.5099 0.6753 0.0220 0.0166 0.356 2.494 1.601 265.524 0.282 7.122 2.735 0.47 151326. 0.1567
|
|
58.77 0.5320 0.6501 0.0181 0.0148 0.318 2.228 1.320 237.258 0.252 5.872 2.524 0.47 151621. 0.1313
|
|
61.21 0.5542 0.6094 0.0142 0.0130 0.278 1.945 1.037 207.115 0.220 4.612 2.271 0.47 151926. 0.1047
|
|
63.66 0.5764 0.5439 0.0103 0.0110 0.235 1.645 0.752 175.146 0.186 3.347 1.949 0.47 152241. 0.0765
|
|
66.11 0.5985 0.4347 0.0064 0.0088 0.190 1.328 0.468 141.420 0.150 2.080 1.500 0.47 152566. 0.0464
|
|
68.56 0.6207 0.2353 0.0025 0.0066 0.142 0.995 0.183 105.969 0.112 0.814 0.783 0.47 152897. 0.0152
|
|
71.01 0.6429
|
|
|
|
|
|
|
|
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 0.0878 0.0281 0.828 5.217 7.894 617.292 0.589 35.112 5.800 0.51 163500. 0.7378
|
|
2.69 0.0219 0.0664 0.0863 0.0285 0.838 5.281 7.757 624.750 0.597 34.503 5.632 0.51 163599. 0.7101
|
|
5.38 0.0439 0.1290 0.0846 0.0288 0.847 5.337 7.609 631.457 0.603 33.847 5.466 0.51 163705. 0.6826
|
|
8.07 0.0658 0.1877 0.0829 0.0290 0.855 5.386 7.451 637.256 0.609 33.143 5.303 0.51 163819. 0.6554
|
|
10.76 0.0877 0.2428 0.0810 0.0293 0.861 5.426 7.282 641.998 0.613 32.390 5.145 0.51 163940. 0.6286
|
|
13.45 0.1096 0.2943 0.0790 0.0294 0.866 5.456 7.101 645.534 0.616 31.587 4.990 0.51 164071. 0.6020
|
|
16.14 0.1316 0.3424 0.0769 0.0295 0.869 5.475 6.909 647.709 0.619 30.731 4.838 0.51 164209. 0.5758
|
|
18.84 0.1535 0.3873 0.0746 0.0296 0.869 5.480 6.705 648.370 0.619 29.823 4.690 0.51 164357. 0.5499
|
|
21.53 0.1754 0.4290 0.0722 0.0295 0.868 5.472 6.489 647.362 0.618 28.861 4.546 0.51 164514. 0.5243
|
|
24.22 0.1973 0.4677 0.0696 0.0294 0.864 5.448 6.260 644.539 0.615 27.846 4.405 0.52 164680. 0.4991
|
|
26.91 0.2193 0.5035 0.0670 0.0292 0.858 5.408 6.020 639.785 0.611 26.778 4.268 0.52 164855. 0.4741
|
|
29.60 0.2412 0.5364 0.0642 0.0289 0.849 5.350 5.769 633.009 0.604 25.661 4.134 0.52 165040. 0.4495
|
|
32.29 0.2631 0.5666 0.0613 0.0284 0.837 5.275 5.507 624.141 0.596 24.497 4.002 0.52 165234. 0.4253
|
|
34.98 0.2850 0.5940 0.0582 0.0279 0.822 5.182 5.236 613.112 0.585 23.288 3.873 0.52 165439. 0.4013
|
|
37.67 0.3070 0.6187 0.0551 0.0273 0.804 5.070 4.955 599.860 0.573 22.038 3.746 0.52 165654. 0.3775
|
|
40.36 0.3289 0.6407 0.0519 0.0266 0.784 4.939 4.665 584.321 0.558 20.748 3.621 0.52 165879. 0.3541
|
|
43.05 0.3508 0.6599 0.0486 0.0258 0.760 4.788 4.366 566.436 0.541 19.422 3.496 0.52 166114. 0.3308
|
|
45.74 0.3727 0.6762 0.0452 0.0249 0.732 4.616 4.060 546.144 0.522 18.060 3.372 0.52 166359. 0.3076
|
|
48.43 0.3947 0.6894 0.0417 0.0239 0.702 4.424 3.747 523.394 0.500 16.666 3.247 0.52 166616. 0.2846
|
|
51.13 0.4166 0.6993 0.0381 0.0227 0.668 4.210 3.427 498.135 0.476 15.241 3.120 0.52 166883. 0.2615
|
|
53.82 0.4385 0.7053 0.0345 0.0214 0.631 3.975 3.100 470.326 0.449 13.789 2.990 0.52 167160. 0.2383
|
|
56.51 0.4604 0.7069 0.0308 0.0201 0.590 3.718 2.768 439.933 0.420 12.311 2.854 0.52 167449. 0.2150
|
|
59.20 0.4824 0.7031 0.0270 0.0185 0.546 3.440 2.431 406.936 0.389 10.811 2.709 0.52 167748. 0.1912
|
|
61.89 0.5043 0.6922 0.0232 0.0169 0.498 3.139 2.089 371.330 0.355 9.291 2.551 0.52 168058. 0.1669
|
|
64.58 0.5262 0.6720 0.0194 0.0152 0.447 2.816 1.743 333.124 0.318 7.754 2.374 0.52 168380. 0.1419
|
|
67.27 0.5481 0.6382 0.0155 0.0133 0.392 2.471 1.395 292.354 0.279 6.205 2.164 0.52 168712. 0.1157
|
|
69.96 0.5701 0.5834 0.0116 0.0114 0.334 2.105 1.045 249.079 0.238 4.646 1.902 0.52 169055. 0.0880
|
|
72.65 0.5920 0.4926 0.0077 0.0093 0.273 1.719 0.693 203.385 0.194 3.085 1.547 0.52 169409. 0.0583
|
|
75.34 0.6139 0.3303 0.0038 0.0071 0.208 1.313 0.342 155.359 0.148 1.523 1.000 0.52 169772. 0.0265
|
|
78.03 0.6358 -0.0277 -0.0002 0.0047 0.139 0.874 -0.018 103.401 0.099 -0.082 -0.081 0.52 170086. 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 0.0886 0.0283 1.107 6.344 9.641 825.587 0.717 42.884 5.297 0.57 179839. 0.7446
|
|
2.97 0.0220 0.0670 0.0871 0.0286 1.121 6.422 9.475 835.758 0.726 42.144 5.142 0.57 179948. 0.7166
|
|
5.94 0.0440 0.1300 0.0855 0.0289 1.133 6.492 9.296 844.896 0.733 41.346 4.990 0.57 180065. 0.6888
|
|
8.91 0.0660 0.1891 0.0837 0.0292 1.144 6.553 9.103 852.791 0.740 40.490 4.842 0.57 180192. 0.6614
|
|
11.88 0.0880 0.2446 0.0818 0.0294 1.152 6.602 8.897 859.235 0.746 39.572 4.696 0.57 180327. 0.6342
|
|
14.85 0.1100 0.2966 0.0798 0.0296 1.159 6.639 8.676 864.023 0.750 38.591 4.555 0.57 180471. 0.6074
|
|
17.82 0.1320 0.3451 0.0776 0.0297 1.163 6.662 8.441 866.948 0.753 37.546 4.416 0.57 180625. 0.5809
|
|
20.79 0.1540 0.3903 0.0753 0.0297 1.164 6.668 8.192 867.797 0.753 36.436 4.281 0.57 180789. 0.5548
|
|
23.76 0.1760 0.4323 0.0729 0.0297 1.162 6.657 7.927 866.362 0.752 35.259 4.150 0.57 180962. 0.5290
|
|
26.73 0.1980 0.4714 0.0703 0.0295 1.157 6.627 7.647 862.444 0.749 34.016 4.022 0.57 181146. 0.5036
|
|
29.70 0.2200 0.5075 0.0676 0.0293 1.148 6.576 7.353 855.885 0.743 32.708 3.897 0.57 181341. 0.4784
|
|
32.67 0.2420 0.5407 0.0648 0.0290 1.135 6.505 7.046 846.565 0.735 31.338 3.775 0.57 181546. 0.4536
|
|
35.65 0.2640 0.5712 0.0618 0.0286 1.119 6.411 6.725 834.387 0.724 29.911 3.655 0.57 181762. 0.4292
|
|
38.62 0.2860 0.5990 0.0588 0.0281 1.099 6.295 6.391 819.261 0.711 28.428 3.538 0.57 181989. 0.4050
|
|
41.59 0.3080 0.6241 0.0556 0.0274 1.074 6.156 6.046 801.103 0.695 26.894 3.423 0.57 182227. 0.3811
|
|
44.56 0.3301 0.6465 0.0523 0.0267 1.046 5.992 5.691 779.831 0.677 25.311 3.310 0.57 182476. 0.3575
|
|
47.53 0.3521 0.6661 0.0489 0.0259 1.013 5.804 5.324 755.362 0.656 23.683 3.197 0.57 182737. 0.3340
|
|
50.50 0.3741 0.6829 0.0455 0.0249 0.976 5.591 4.949 727.619 0.632 22.011 3.085 0.57 183009. 0.3107
|
|
53.47 0.3961 0.6966 0.0420 0.0239 0.934 5.352 4.564 696.528 0.605 20.300 2.972 0.57 183293. 0.2874
|
|
56.44 0.4181 0.7070 0.0383 0.0227 0.888 5.087 4.171 662.024 0.575 18.551 2.857 0.57 183589. 0.2642
|
|
59.41 0.4401 0.7136 0.0347 0.0214 0.837 4.795 3.770 624.051 0.542 16.767 2.740 0.57 183897. 0.2408
|
|
62.38 0.4621 0.7157 0.0309 0.0200 0.781 4.476 3.362 582.565 0.506 14.952 2.617 0.57 184216. 0.2173
|
|
65.35 0.4841 0.7125 0.0271 0.0184 0.721 4.130 2.947 537.540 0.467 13.110 2.487 0.57 184548. 0.1933
|
|
68.32 0.5061 0.7022 0.0232 0.0167 0.656 3.757 2.527 488.969 0.424 11.242 2.345 0.57 184892. 0.1688
|
|
71.29 0.5281 0.6824 0.0193 0.0150 0.586 3.357 2.103 436.868 0.379 9.355 2.184 0.57 185248. 0.1434
|
|
74.26 0.5501 0.6488 0.0154 0.0131 0.511 2.930 1.675 381.287 0.331 7.452 1.993 0.57 185616. 0.1168
|
|
77.23 0.5721 0.5932 0.0114 0.0110 0.432 2.477 1.245 322.311 0.280 5.538 1.752 0.57 185996. 0.0885
|
|
80.20 0.5941 0.4991 0.0075 0.0089 0.349 1.998 0.814 260.062 0.226 3.620 1.419 0.58 186388. 0.0580
|
|
83.17 0.6161 0.3253 0.0035 0.0067 0.261 1.496 0.383 194.646 0.169 1.703 0.892 0.58 186789. 0.0250
|
|
86.14 0.6381
|
|
|
|
|
|
|
|
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 0.0896 0.0285 1.449 7.610 11.595 1080.394 0.860 51.575 4.868 0.62 196173. 0.7505
|
|
3.24 0.0220 0.0671 0.0880 0.0289 1.467 7.705 11.397 1093.905 0.871 50.696 4.726 0.62 196292. 0.7223
|
|
6.48 0.0440 0.1303 0.0864 0.0292 1.483 7.790 11.184 1106.042 0.880 49.746 4.586 0.62 196421. 0.6944
|
|
9.72 0.0660 0.1896 0.0846 0.0295 1.497 7.864 10.954 1116.520 0.888 48.725 4.450 0.62 196560. 0.6668
|
|
12.96 0.0880 0.2453 0.0827 0.0297 1.509 7.924 10.708 1125.067 0.895 47.630 4.317 0.62 196708. 0.6396
|
|
16.20 0.1100 0.2974 0.0807 0.0298 1.517 7.969 10.445 1131.410 0.900 46.458 4.187 0.62 196866. 0.6127
|
|
19.44 0.1320 0.3461 0.0785 0.0299 1.522 7.996 10.164 1135.276 0.903 45.208 4.061 0.62 197034. 0.5861
|
|
22.68 0.1540 0.3915 0.0762 0.0300 1.524 8.004 9.865 1136.387 0.904 43.879 3.937 0.62 197214. 0.5599
|
|
25.92 0.1760 0.4338 0.0738 0.0299 1.521 7.991 9.548 1134.467 0.903 42.468 3.817 0.62 197404. 0.5340
|
|
29.16 0.1980 0.4731 0.0712 0.0298 1.514 7.954 9.213 1129.258 0.899 40.978 3.700 0.62 197605. 0.5085
|
|
32.40 0.2200 0.5094 0.0684 0.0296 1.503 7.893 8.860 1120.549 0.892 39.408 3.586 0.62 197818. 0.4833
|
|
35.64 0.2420 0.5430 0.0656 0.0292 1.486 7.806 8.490 1108.182 0.882 37.764 3.475 0.62 198043. 0.4584
|
|
38.88 0.2640 0.5738 0.0626 0.0288 1.464 7.692 8.105 1092.034 0.869 36.049 3.366 0.62 198279. 0.4339
|
|
42.12 0.2860 0.6020 0.0595 0.0283 1.438 7.551 7.704 1071.989 0.853 34.268 3.260 0.62 198527. 0.4096
|
|
45.37 0.3080 0.6275 0.0563 0.0276 1.405 7.381 7.289 1047.938 0.834 32.423 3.155 0.62 198787. 0.3857
|
|
48.61 0.3300 0.6503 0.0530 0.0269 1.368 7.183 6.862 1019.776 0.812 30.520 3.052 0.62 199060. 0.3619
|
|
51.85 0.3520 0.6704 0.0496 0.0260 1.324 6.955 6.421 987.398 0.786 28.561 2.950 0.62 199345. 0.3384
|
|
55.09 0.3740 0.6877 0.0461 0.0251 1.275 6.696 5.969 950.705 0.757 26.550 2.848 0.62 199643. 0.3150
|
|
58.33 0.3961 0.7021 0.0425 0.0240 1.220 6.407 5.506 909.599 0.724 24.491 2.746 0.62 199953. 0.2917
|
|
61.57 0.4181 0.7131 0.0389 0.0228 1.159 6.086 5.033 863.997 0.688 22.386 2.642 0.62 200276. 0.2684
|
|
64.81 0.4401 0.7205 0.0351 0.0215 1.091 5.732 4.550 813.826 0.648 20.239 2.536 0.62 200612. 0.2449
|
|
68.05 0.4621 0.7236 0.0314 0.0200 1.018 5.346 4.059 759.028 0.604 18.054 2.425 0.62 200961. 0.2212
|
|
71.29 0.4841 0.7214 0.0275 0.0185 0.938 4.927 3.560 699.568 0.557 15.835 2.308 0.62 201323. 0.1972
|
|
74.53 0.5061 0.7123 0.0236 0.0168 0.852 4.476 3.054 635.435 0.506 13.586 2.180 0.62 201699. 0.1725
|
|
77.77 0.5281 0.6940 0.0196 0.0149 0.760 3.991 2.543 566.655 0.451 11.312 2.036 0.63 202087. 0.1470
|
|
81.01 0.5501 0.6621 0.0157 0.0130 0.662 3.474 2.028 493.289 0.393 9.018 1.864 0.63 202489. 0.1202
|
|
84.25 0.5721 0.6085 0.0117 0.0110 0.557 2.926 1.509 415.451 0.331 6.712 1.648 0.63 202904. 0.0916
|
|
87.49 0.5941 0.5164 0.0076 0.0088 0.447 2.348 0.989 333.302 0.265 4.400 1.346 0.63 203332. 0.0606
|
|
90.73 0.6161 0.3430 0.0036 0.0065 0.331 1.740 0.470 246.984 0.197 2.089 0.862 0.63 203770. 0.0268
|
|
93.97 0.6381
|
|
|
|
|
|
|
|
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 0.0906 0.0288 1.863 9.032 13.770 1389.156 1.020 61.250 4.496 0.67 212502. 0.7554
|
|
3.50 0.0219 0.0669 0.0891 0.0292 1.886 9.146 13.540 1406.683 1.033 60.225 4.366 0.67 212632. 0.7273
|
|
6.99 0.0438 0.1299 0.0875 0.0295 1.908 9.248 13.290 1422.437 1.045 59.116 4.238 0.67 212771. 0.6995
|
|
10.49 0.0657 0.1891 0.0857 0.0298 1.926 9.337 13.022 1436.050 1.055 57.922 4.113 0.67 212921. 0.6720
|
|
13.99 0.0877 0.2447 0.0838 0.0300 1.941 9.409 12.734 1447.162 1.063 56.639 3.991 0.67 213081. 0.6448
|
|
17.48 0.1096 0.2968 0.0818 0.0302 1.952 9.463 12.425 1455.423 1.069 55.266 3.872 0.67 213253. 0.6180
|
|
20.98 0.1315 0.3455 0.0796 0.0303 1.959 9.496 12.095 1460.479 1.073 53.799 3.756 0.67 213435. 0.5915
|
|
24.48 0.1534 0.3910 0.0773 0.0303 1.961 9.505 11.744 1461.977 1.074 52.237 3.644 0.67 213629. 0.5653
|
|
27.97 0.1753 0.4333 0.0748 0.0303 1.957 9.490 11.371 1459.566 1.072 50.579 3.534 0.67 213835. 0.5395
|
|
31.47 0.1972 0.4728 0.0722 0.0301 1.948 9.446 10.977 1452.914 1.067 48.825 3.427 0.67 214053. 0.5140
|
|
34.97 0.2192 0.5093 0.0695 0.0299 1.933 9.374 10.561 1441.749 1.059 46.977 3.323 0.67 214283. 0.4889
|
|
38.46 0.2411 0.5431 0.0666 0.0296 1.912 9.271 10.126 1425.873 1.047 45.040 3.221 0.67 214526. 0.4641
|
|
41.96 0.2630 0.5743 0.0637 0.0292 1.884 9.136 9.671 1405.127 1.032 43.017 3.122 0.67 214781. 0.4396
|
|
45.46 0.2849 0.6028 0.0605 0.0286 1.850 8.968 9.199 1379.370 1.013 40.915 3.025 0.67 215049. 0.4153
|
|
48.95 0.3068 0.6287 0.0573 0.0280 1.808 8.767 8.709 1348.469 0.991 38.738 2.929 0.67 215330. 0.3914
|
|
52.45 0.3287 0.6520 0.0540 0.0272 1.760 8.532 8.204 1312.295 0.964 36.491 2.836 0.67 215624. 0.3677
|
|
55.95 0.3507 0.6727 0.0506 0.0264 1.704 8.262 7.684 1270.716 0.933 34.177 2.743 0.67 215932. 0.3442
|
|
59.44 0.3726 0.6906 0.0471 0.0254 1.641 7.956 7.149 1223.610 0.899 31.801 2.650 0.67 216253. 0.3208
|
|
62.94 0.3945 0.7057 0.0435 0.0243 1.570 7.613 6.602 1170.856 0.860 29.366 2.558 0.67 216587. 0.2975
|
|
66.44 0.4164 0.7176 0.0398 0.0231 1.492 7.232 6.043 1112.347 0.817 26.878 2.464 0.67 216935. 0.2742
|
|
69.93 0.4383 0.7260 0.0360 0.0217 1.405 6.814 5.472 1047.982 0.770 24.338 2.368 0.67 217298. 0.2508
|
|
73.43 0.4602 0.7304 0.0322 0.0203 1.311 6.357 4.891 977.694 0.718 21.753 2.269 0.68 217674. 0.2272
|
|
76.93 0.4822 0.7297 0.0283 0.0187 1.209 5.861 4.300 901.435 0.662 19.127 2.164 0.68 218064. 0.2031
|
|
80.42 0.5041 0.7226 0.0244 0.0170 1.099 5.326 3.701 819.189 0.602 16.464 2.049 0.68 218468. 0.1785
|
|
83.92 0.5260 0.7067 0.0204 0.0152 0.980 4.753 3.096 730.982 0.537 13.771 1.921 0.68 218886. 0.1530
|
|
87.41 0.5479 0.6782 0.0164 0.0132 0.854 4.141 2.485 636.889 0.468 11.053 1.770 0.68 219319. 0.1263
|
|
90.91 0.5698 0.6295 0.0123 0.0111 0.720 3.492 1.870 537.048 0.394 8.319 1.580 0.68 219765. 0.0978
|
|
94.41 0.5917 0.5452 0.0083 0.0090 0.579 2.807 1.254 431.658 0.317 5.576 1.317 0.68 220225. 0.0668
|
|
97.90 0.6137 0.3864 0.0042 0.0067 0.430 2.087 0.637 320.924 0.236 2.833 0.900 0.68 220697. 0.0325
|
|
101.40 0.6356 0.0072 0.0000 0.0042 0.271 1.314 0.007 202.143 0.148 0.032 0.016 0.68 221125. 0.0001
|
|
|
|
|
|
|
|
PROP RPM = 14000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.0918 0.0294 2.370 10.669 16.184 1767.228 1.205 71.985 4.154 0.72 228826. 0.7565
|
|
3.77 0.0220 0.0668 0.0903 0.0297 2.398 10.797 15.917 1788.378 1.220 70.800 4.037 0.72 228966. 0.7292
|
|
7.54 0.0439 0.1297 0.0887 0.0300 2.424 10.912 15.628 1807.407 1.233 69.515 3.922 0.72 229117. 0.7020
|
|
11.32 0.0659 0.1890 0.0869 0.0303 2.446 11.011 15.317 1823.849 1.244 68.129 3.809 0.72 229280. 0.6749
|
|
15.09 0.0878 0.2446 0.0850 0.0305 2.464 11.092 14.981 1837.254 1.253 66.636 3.698 0.72 229454. 0.6481
|
|
18.86 0.1098 0.2968 0.0830 0.0307 2.477 11.152 14.621 1847.159 1.260 65.034 3.590 0.72 229639. 0.6215
|
|
22.63 0.1317 0.3457 0.0808 0.0308 2.485 11.188 14.236 1853.088 1.264 63.320 3.484 0.72 229838. 0.5952
|
|
26.40 0.1537 0.3914 0.0785 0.0308 2.487 11.197 13.825 1854.570 1.265 61.492 3.381 0.72 230048. 0.5692
|
|
30.18 0.1756 0.4340 0.0760 0.0308 2.482 11.176 13.388 1851.126 1.263 59.550 3.280 0.72 230271. 0.5434
|
|
33.95 0.1976 0.4736 0.0734 0.0306 2.471 11.123 12.925 1842.298 1.257 57.492 3.182 0.72 230508. 0.5180
|
|
37.72 0.2195 0.5104 0.0706 0.0304 2.451 11.034 12.437 1827.709 1.247 55.321 3.086 0.72 230757. 0.4928
|
|
41.49 0.2415 0.5444 0.0677 0.0300 2.423 10.910 11.925 1807.081 1.233 53.043 2.993 0.72 231020. 0.4680
|
|
45.26 0.2634 0.5759 0.0646 0.0296 2.387 10.748 11.390 1780.202 1.214 50.664 2.902 0.72 231297. 0.4434
|
|
49.03 0.2854 0.6047 0.0615 0.0290 2.343 10.547 10.834 1746.897 1.192 48.189 2.813 0.72 231588. 0.4192
|
|
52.81 0.3073 0.6310 0.0582 0.0284 2.289 10.306 10.257 1707.002 1.164 45.625 2.726 0.72 231892. 0.3952
|
|
56.58 0.3293 0.6547 0.0548 0.0276 2.227 10.024 9.662 1660.361 1.133 42.976 2.639 0.72 232211. 0.3715
|
|
60.35 0.3513 0.6758 0.0514 0.0267 2.155 9.701 9.049 1606.813 1.096 40.249 2.554 0.72 232544. 0.3479
|
|
64.12 0.3732 0.6942 0.0478 0.0257 2.073 9.335 8.419 1546.207 1.055 37.447 2.470 0.72 232891. 0.3244
|
|
67.89 0.3952 0.7098 0.0441 0.0246 1.983 8.926 7.773 1478.393 1.008 34.576 2.385 0.73 233253. 0.3010
|
|
71.67 0.4171 0.7224 0.0404 0.0233 1.882 8.472 7.113 1403.235 0.957 31.640 2.299 0.73 233630. 0.2776
|
|
75.44 0.4391 0.7315 0.0365 0.0219 1.771 7.973 6.440 1320.612 0.901 28.644 2.212 0.73 234022. 0.2541
|
|
79.21 0.4610 0.7365 0.0327 0.0204 1.650 7.429 5.754 1230.432 0.839 25.593 2.121 0.73 234429. 0.2303
|
|
82.98 0.4830 0.7367 0.0287 0.0188 1.519 6.838 5.057 1132.635 0.773 22.492 2.025 0.73 234851. 0.2062
|
|
86.75 0.5049 0.7305 0.0247 0.0171 1.378 6.202 4.350 1027.210 0.701 19.347 1.921 0.73 235288. 0.1814
|
|
90.53 0.5269 0.7156 0.0206 0.0152 1.226 5.519 3.634 914.208 0.624 16.166 1.803 0.73 235740. 0.1556
|
|
94.30 0.5488 0.6880 0.0165 0.0132 1.064 4.792 2.913 793.758 0.541 12.955 1.664 0.73 236208. 0.1286
|
|
98.07 0.5708 0.6401 0.0124 0.0111 0.893 4.021 2.186 666.088 0.454 9.725 1.489 0.73 236691. 0.0997
|
|
101.84 0.5927 0.5553 0.0083 0.0088 0.713 3.209 1.458 531.533 0.363 6.483 1.244 0.73 237188. 0.0680
|
|
105.61 0.6147 0.3918 0.0041 0.0065 0.524 2.357 0.729 390.458 0.266 3.241 0.846 0.73 237698. 0.0327
|
|
109.39 0.6366 -0.0253 -0.0002 0.0039 0.318 1.430 -0.028 236.887 0.162 -0.123 -0.053 0.73 238114. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 15000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.0932 0.0306 3.034 12.751 18.854 2262.825 1.441 83.861 3.779 0.77 245142. 0.7429
|
|
4.04 0.0220 0.0653 0.0917 0.0309 3.063 12.871 18.551 2284.229 1.454 82.514 3.684 0.77 245293. 0.7183
|
|
8.09 0.0439 0.1272 0.0901 0.0311 3.088 12.977 18.221 2303.007 1.466 81.049 3.589 0.77 245456. 0.6936
|
|
12.13 0.0659 0.1858 0.0883 0.0313 3.109 13.065 17.865 2318.652 1.476 79.461 3.495 0.77 245631. 0.6687
|
|
16.17 0.0879 0.2412 0.0864 0.0315 3.125 13.133 17.479 2330.663 1.484 77.748 3.402 0.77 245818. 0.6439
|
|
20.22 0.1098 0.2933 0.0844 0.0316 3.136 13.177 17.065 2338.531 1.489 75.904 3.310 0.77 246019. 0.6190
|
|
24.26 0.1318 0.3424 0.0822 0.0316 3.140 13.195 16.620 2341.721 1.491 73.928 3.219 0.77 246232. 0.5942
|
|
28.30 0.1537 0.3884 0.0798 0.0316 3.138 13.184 16.146 2339.684 1.489 71.816 3.130 0.77 246459. 0.5694
|
|
32.35 0.1757 0.4314 0.0773 0.0315 3.127 13.140 15.640 2331.856 1.485 69.568 3.042 0.77 246700. 0.5447
|
|
36.39 0.1977 0.4715 0.0747 0.0313 3.108 13.060 15.104 2317.681 1.475 67.182 2.956 0.77 246955. 0.5201
|
|
40.43 0.2196 0.5089 0.0719 0.0310 3.080 12.941 14.537 2296.686 1.462 64.662 2.871 0.77 247224. 0.4956
|
|
44.48 0.2416 0.5435 0.0689 0.0306 3.042 12.783 13.942 2268.509 1.444 62.013 2.788 0.77 247507. 0.4712
|
|
48.52 0.2636 0.5755 0.0658 0.0302 2.994 12.582 13.319 2232.855 1.421 59.244 2.706 0.77 247806. 0.4471
|
|
52.56 0.2855 0.6049 0.0626 0.0296 2.936 12.337 12.671 2189.453 1.394 56.361 2.625 0.77 248118. 0.4231
|
|
56.61 0.3075 0.6317 0.0593 0.0289 2.867 12.048 11.999 2138.047 1.361 53.372 2.545 0.77 248446. 0.3992
|
|
60.65 0.3295 0.6559 0.0559 0.0281 2.787 11.711 11.304 2078.375 1.323 50.282 2.467 0.78 248789. 0.3755
|
|
64.69 0.3514 0.6776 0.0523 0.0271 2.696 11.327 10.589 2010.182 1.280 47.099 2.389 0.78 249148. 0.3520
|
|
68.74 0.3734 0.6966 0.0487 0.0261 2.592 10.893 9.853 1933.223 1.231 43.828 2.312 0.78 249521. 0.3286
|
|
72.78 0.3954 0.7129 0.0450 0.0249 2.477 10.409 9.099 1847.292 1.176 40.474 2.234 0.78 249911. 0.3051
|
|
76.82 0.4173 0.7261 0.0412 0.0237 2.350 9.873 8.328 1752.203 1.115 37.044 2.156 0.78 250316. 0.2817
|
|
80.87 0.4393 0.7359 0.0373 0.0223 2.210 9.285 7.541 1647.832 1.049 33.542 2.076 0.78 250737. 0.2581
|
|
84.91 0.4612 0.7417 0.0333 0.0207 2.057 8.644 6.739 1534.089 0.977 29.975 1.992 0.78 251174. 0.2342
|
|
88.95 0.4832 0.7426 0.0293 0.0191 1.892 7.951 5.924 1410.984 0.898 26.349 1.904 0.78 251628. 0.2098
|
|
93.00 0.5052 0.7371 0.0252 0.0173 1.715 7.205 5.097 1278.597 0.814 22.669 1.808 0.78 252097. 0.1848
|
|
97.04 0.5271 0.7228 0.0211 0.0154 1.525 6.408 4.259 1137.128 0.724 18.946 1.699 0.78 252583. 0.1587
|
|
101.08 0.5491 0.6953 0.0169 0.0133 1.323 5.561 3.414 986.917 0.628 15.186 1.569 0.78 253085. 0.1313
|
|
105.13 0.5711 0.6467 0.0127 0.0112 1.111 4.668 2.563 828.451 0.527 11.400 1.403 0.78 253603. 0.1017
|
|
109.17 0.5930 0.5599 0.0084 0.0089 0.888 3.732 1.709 662.380 0.422 7.600 1.170 0.78 254136. 0.0692
|
|
113.21 0.6150 0.3926 0.0042 0.0066 0.656 2.758 0.853 489.396 0.312 3.796 0.791 0.79 254683. 0.0331
|
|
117.26 0.6370 -0.0289 -0.0002 0.0041 0.403 1.694 -0.037 300.561 0.191 -0.166 -0.056 0.79 255116. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 16000
|
|
|
|
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 0.0947 0.0332 3.995 15.738 21.798 2979.234 1.778 96.956 3.319 0.82 261448. 0.7015
|
|
4.32 0.0220 0.0615 0.0932 0.0333 4.015 15.817 21.459 2994.139 1.787 95.449 3.251 0.82 261610. 0.6818
|
|
8.63 0.0440 0.1204 0.0916 0.0334 4.030 15.876 21.088 3005.347 1.794 93.802 3.183 0.82 261785. 0.6617
|
|
12.95 0.0659 0.1768 0.0899 0.0335 4.040 15.913 20.686 3012.368 1.798 92.010 3.115 0.82 261973. 0.6414
|
|
17.26 0.0879 0.2306 0.0880 0.0335 4.043 15.926 20.249 3014.730 1.799 90.068 3.046 0.82 262175. 0.6207
|
|
21.58 0.1099 0.2818 0.0859 0.0335 4.039 15.911 19.778 3011.951 1.798 87.971 2.978 0.82 262390. 0.5997
|
|
25.90 0.1319 0.3304 0.0837 0.0334 4.028 15.867 19.271 3003.542 1.793 85.717 2.910 0.82 262620. 0.5784
|
|
30.21 0.1539 0.3764 0.0814 0.0333 4.008 15.790 18.728 2988.971 1.784 83.302 2.842 0.82 262864. 0.5568
|
|
34.53 0.1758 0.4199 0.0789 0.0330 3.980 15.677 18.149 2967.701 1.771 80.725 2.774 0.82 263122. 0.5350
|
|
38.84 0.1978 0.4608 0.0762 0.0327 3.941 15.527 17.533 2939.149 1.754 77.986 2.706 0.82 263396. 0.5129
|
|
43.16 0.2198 0.4991 0.0733 0.0323 3.893 15.334 16.881 2902.792 1.732 75.086 2.638 0.82 263685. 0.4907
|
|
47.48 0.2418 0.5349 0.0704 0.0318 3.833 15.099 16.195 2858.249 1.706 72.034 2.570 0.82 263990. 0.4682
|
|
51.79 0.2638 0.5682 0.0672 0.0312 3.762 14.819 15.476 2805.228 1.674 68.837 2.502 0.83 264310. 0.4457
|
|
56.11 0.2857 0.5989 0.0640 0.0305 3.679 14.493 14.727 2743.458 1.637 65.505 2.435 0.83 264646. 0.4230
|
|
60.42 0.3077 0.6271 0.0606 0.0297 3.584 14.119 13.949 2672.653 1.595 62.047 2.367 0.83 264997. 0.4003
|
|
64.74 0.3297 0.6527 0.0571 0.0289 3.477 13.695 13.145 2592.494 1.547 58.469 2.300 0.83 265365. 0.3775
|
|
69.06 0.3517 0.6757 0.0535 0.0279 3.356 13.221 12.316 2502.639 1.494 54.780 2.232 0.83 265750. 0.3546
|
|
73.37 0.3737 0.6960 0.0498 0.0267 3.222 12.693 11.463 2402.740 1.434 50.987 2.164 0.83 266150. 0.3317
|
|
77.69 0.3956 0.7135 0.0460 0.0255 3.074 12.110 10.588 2292.441 1.368 47.097 2.095 0.83 266568. 0.3086
|
|
82.00 0.4176 0.7276 0.0421 0.0242 2.913 11.476 9.693 2172.348 1.297 43.115 2.024 0.83 267002. 0.2853
|
|
86.32 0.4396 0.7378 0.0381 0.0227 2.739 10.788 8.779 2042.209 1.219 39.048 1.950 0.83 267453. 0.2616
|
|
90.64 0.4616 0.7436 0.0341 0.0212 2.551 10.047 7.847 1901.949 1.135 34.903 1.871 0.83 267921. 0.2373
|
|
94.95 0.4836 0.7439 0.0300 0.0195 2.348 9.250 6.899 1751.025 1.045 30.687 1.787 0.83 268406. 0.2125
|
|
99.27 0.5055 0.7371 0.0258 0.0177 2.132 8.399 5.937 1589.846 0.949 26.407 1.694 0.83 268908. 0.1868
|
|
103.58 0.5275 0.7204 0.0216 0.0158 1.903 7.495 4.962 1418.868 0.847 22.073 1.586 0.83 269428. 0.1600
|
|
107.90 0.5495 0.6889 0.0173 0.0138 1.661 6.545 3.978 1238.873 0.739 17.694 1.456 0.84 269964. 0.1315
|
|
112.22 0.5715 0.6341 0.0130 0.0117 1.409 5.551 2.986 1050.823 0.627 13.283 1.289 0.84 270518. 0.1008
|
|
116.53 0.5935 0.5388 0.0086 0.0095 1.148 4.521 1.990 855.844 0.511 8.852 1.055 0.84 271089. 0.0674
|
|
120.85 0.6154 0.3640 0.0043 0.0073 0.878 3.461 0.992 655.094 0.391 4.413 0.687 0.84 271673. 0.0310
|
|
125.17 0.6374 -0.0268 -0.0002 0.0048 0.584 2.302 -0.047 435.751 0.260 -0.209 -0.049 0.84 272143. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 17000
|
|
|
|
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 0.0961 0.0377 5.452 20.214 24.977 4065.650 2.284 111.099 2.786 0.87 277750. 0.6305
|
|
4.59 0.0220 0.0553 0.0947 0.0377 5.455 20.225 24.609 4067.771 2.285 109.462 2.744 0.87 277923. 0.6163
|
|
9.19 0.0440 0.1088 0.0932 0.0377 5.449 20.204 24.204 4063.535 2.283 107.659 2.702 0.87 278109. 0.6018
|
|
13.78 0.0661 0.1607 0.0915 0.0376 5.435 20.149 23.760 4052.574 2.276 105.683 2.659 0.87 278310. 0.5869
|
|
18.37 0.0881 0.2108 0.0896 0.0374 5.410 20.059 23.275 4034.445 2.266 103.528 2.617 0.87 278525. 0.5716
|
|
22.97 0.1101 0.2592 0.0876 0.0372 5.376 19.931 22.749 4008.768 2.252 101.188 2.574 0.87 278755. 0.5558
|
|
27.56 0.1321 0.3058 0.0854 0.0369 5.331 19.764 22.180 3975.212 2.233 98.658 2.531 0.87 279001. 0.5396
|
|
32.16 0.1541 0.3506 0.0830 0.0365 5.275 19.557 21.568 3933.494 2.210 95.935 2.487 0.87 279262. 0.5229
|
|
36.75 0.1761 0.3935 0.0805 0.0360 5.208 19.307 20.912 3883.316 2.181 93.019 2.443 0.88 279540. 0.5057
|
|
41.34 0.1982 0.4345 0.0778 0.0355 5.129 19.014 20.213 3824.350 2.148 89.907 2.397 0.88 279833. 0.4880
|
|
45.94 0.2202 0.4735 0.0749 0.0349 5.037 18.676 19.471 3756.311 2.110 86.606 2.351 0.88 280143. 0.4697
|
|
50.53 0.2422 0.5104 0.0719 0.0341 4.934 18.292 18.688 3679.050 2.067 83.123 2.304 0.88 280469. 0.4509
|
|
55.12 0.2642 0.5451 0.0688 0.0333 4.818 17.861 17.866 3592.443 2.018 79.468 2.256 0.88 280812. 0.4317
|
|
59.72 0.2862 0.5777 0.0655 0.0324 4.689 17.383 17.008 3496.333 1.964 75.653 2.206 0.88 281172. 0.4120
|
|
64.31 0.3083 0.6079 0.0620 0.0315 4.547 16.857 16.117 3390.464 1.905 71.687 2.156 0.88 281549. 0.3919
|
|
68.91 0.3303 0.6357 0.0585 0.0304 4.391 16.280 15.193 3274.473 1.839 67.578 2.104 0.88 281943. 0.3714
|
|
73.50 0.3523 0.6611 0.0548 0.0292 4.221 15.651 14.239 3147.970 1.768 63.336 2.052 0.88 282354. 0.3505
|
|
78.09 0.3743 0.6838 0.0510 0.0279 4.037 14.968 13.257 3010.595 1.691 58.968 1.997 0.88 282783. 0.3293
|
|
82.69 0.3963 0.7037 0.0471 0.0266 3.838 14.229 12.249 2861.975 1.608 54.484 1.941 0.88 283230. 0.3076
|
|
87.28 0.4183 0.7203 0.0432 0.0251 3.624 13.436 11.217 2702.452 1.518 49.891 1.883 0.88 283694. 0.2855
|
|
91.87 0.4404 0.7322 0.0391 0.0235 3.400 12.604 10.161 2535.019 1.424 45.196 1.818 0.88 284176. 0.2624
|
|
96.47 0.4624 0.7369 0.0350 0.0219 3.171 11.755 9.083 2364.305 1.328 40.402 1.743 0.88 284676. 0.2378
|
|
101.06 0.4844 0.7339 0.0307 0.0203 2.932 10.872 7.986 2186.689 1.228 35.522 1.656 0.88 285194. 0.2119
|
|
105.66 0.5064 0.7221 0.0265 0.0186 2.681 9.941 6.872 1999.450 1.123 30.567 1.559 0.89 285731. 0.1850
|
|
110.25 0.5284 0.6981 0.0221 0.0167 2.418 8.967 5.743 1803.473 1.013 25.546 1.444 0.89 286285. 0.1567
|
|
114.84 0.5505 0.6569 0.0177 0.0148 2.146 7.955 4.603 1599.964 0.899 20.472 1.305 0.89 286858. 0.1267
|
|
119.44 0.5725 0.5897 0.0133 0.0129 1.865 6.915 3.453 1390.753 0.781 15.359 1.126 0.89 287449. 0.0947
|
|
124.03 0.5945 0.4814 0.0088 0.0109 1.579 5.854 2.298 1177.512 0.661 10.223 0.885 0.89 288058. 0.0608
|
|
128.62 0.6165 0.3036 0.0044 0.0089 1.290 4.782 1.142 961.833 0.540 5.079 0.538 0.89 288681. 0.0261
|
|
133.22 0.6385 -0.0204 -0.0002 0.0067 0.974 3.613 -0.056 726.637 0.408 -0.249 -0.035 0.89 289217. 0.0000
|
|
|
|
|
|
|