427 lines
76 KiB
Plaintext
427 lines
76 KiB
Plaintext
21.5x13EPN (215x13EPN.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 0.0919 0.0353 0.013 0.823 0.626 9.732 0.093 2.783 29.158 0.09 42722. 0.6294
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0.53 0.0259 0.0656 0.0906 0.0358 0.013 0.835 0.617 9.878 0.094 2.746 28.345 0.09 42752. 0.6078
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1.06 0.0519 0.1275 0.0893 0.0363 0.013 0.847 0.608 10.018 0.096 2.705 27.533 0.09 42784. 0.5860
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1.58 0.0778 0.1857 0.0878 0.0368 0.014 0.858 0.598 10.151 0.097 2.661 26.727 0.09 42819. 0.5641
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2.11 0.1038 0.2402 0.0862 0.0373 0.014 0.868 0.587 10.273 0.098 2.612 25.929 0.09 42858. 0.5423
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2.64 0.1297 0.2911 0.0845 0.0377 0.014 0.877 0.575 10.382 0.099 2.560 25.141 0.09 42899. 0.5205
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3.17 0.1557 0.3386 0.0826 0.0380 0.014 0.885 0.563 10.473 0.100 2.502 24.366 0.09 42944. 0.4988
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3.70 0.1816 0.3827 0.0806 0.0382 0.014 0.891 0.549 10.544 0.101 2.441 23.604 0.09 42993. 0.4772
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4.23 0.2076 0.4235 0.0784 0.0384 0.014 0.895 0.534 10.591 0.101 2.374 22.856 0.09 43045. 0.4557
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4.75 0.2335 0.4611 0.0760 0.0385 0.014 0.897 0.518 10.610 0.101 2.302 22.123 0.09 43101. 0.4343
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5.28 0.2595 0.4957 0.0735 0.0384 0.014 0.896 0.500 10.599 0.101 2.225 21.405 0.09 43161. 0.4131
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5.81 0.2854 0.5273 0.0707 0.0383 0.014 0.892 0.482 10.553 0.101 2.142 20.700 0.09 43224. 0.3920
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6.34 0.3114 0.5560 0.0678 0.0380 0.014 0.885 0.462 10.470 0.100 2.054 20.007 0.09 43292. 0.3711
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6.87 0.3373 0.5818 0.0647 0.0375 0.014 0.874 0.441 10.346 0.099 1.961 19.324 0.09 43363. 0.3501
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7.40 0.3633 0.6046 0.0615 0.0369 0.014 0.860 0.418 10.178 0.097 1.861 18.649 0.09 43439. 0.3292
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7.92 0.3892 0.6245 0.0580 0.0361 0.013 0.842 0.395 9.964 0.095 1.756 17.976 0.09 43518. 0.3083
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8.45 0.4152 0.6412 0.0544 0.0352 0.013 0.820 0.370 9.702 0.093 1.646 17.303 0.09 43602. 0.2873
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8.98 0.4411 0.6545 0.0506 0.0341 0.013 0.794 0.344 9.393 0.090 1.531 16.623 0.09 43689. 0.2662
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9.51 0.4670 0.6640 0.0466 0.0328 0.012 0.764 0.317 9.040 0.086 1.412 15.929 0.09 43781. 0.2450
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10.04 0.4930 0.6694 0.0426 0.0314 0.012 0.731 0.290 8.644 0.083 1.290 15.213 0.09 43877. 0.2236
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10.57 0.5189 0.6700 0.0384 0.0298 0.011 0.694 0.262 8.206 0.078 1.164 14.465 0.09 43977. 0.2019
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11.09 0.5449 0.6648 0.0342 0.0280 0.010 0.653 0.233 7.730 0.074 1.036 13.670 0.09 44081. 0.1801
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11.62 0.5708 0.6527 0.0299 0.0262 0.010 0.610 0.204 7.216 0.069 0.906 12.810 0.09 44189. 0.1578
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12.15 0.5968 0.6319 0.0256 0.0242 0.009 0.563 0.174 6.666 0.064 0.775 11.863 0.09 44301. 0.1352
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12.68 0.6227 0.5998 0.0213 0.0221 0.008 0.514 0.145 6.083 0.058 0.644 10.792 0.09 44417. 0.1121
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13.21 0.6487 0.5527 0.0169 0.0198 0.007 0.462 0.115 5.470 0.052 0.512 9.546 0.09 44537. 0.0884
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13.74 0.6746 0.4844 0.0126 0.0175 0.006 0.408 0.086 4.831 0.046 0.381 8.045 0.09 44661. 0.0643
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14.26 0.7006 0.3848 0.0083 0.0151 0.006 0.352 0.057 4.169 0.040 0.252 6.155 0.09 44790. 0.0399
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14.79 0.7265 0.2358 0.0041 0.0127 0.005 0.295 0.028 3.489 0.033 0.124 3.637 0.09 44922. 0.0166
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15.32 0.7525 0.0008 0.0000 0.0101 0.004 0.236 0.000 2.796 0.027 0.000 0.012 0.09 45057. 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 0.0922 0.0330 0.098 3.074 2.513 72.728 0.347 11.176 15.670 0.17 85443. 0.6779
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1.08 0.0264 0.0716 0.0910 0.0336 0.099 3.127 2.479 73.992 0.353 11.026 15.195 0.17 85503. 0.6529
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2.15 0.0528 0.1389 0.0896 0.0341 0.101 3.179 2.442 75.216 0.359 10.861 14.725 0.17 85569. 0.6280
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3.23 0.0792 0.2017 0.0882 0.0346 0.102 3.228 2.401 76.377 0.365 10.681 14.260 0.17 85641. 0.6031
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4.30 0.1057 0.2603 0.0865 0.0351 0.104 3.273 2.357 77.451 0.370 10.483 13.802 0.17 85720. 0.5783
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5.38 0.1321 0.3148 0.0848 0.0356 0.105 3.314 2.309 78.410 0.374 10.268 13.354 0.17 85805. 0.5537
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6.45 0.1585 0.3654 0.0828 0.0359 0.106 3.348 2.256 79.225 0.378 10.034 12.915 0.17 85898. 0.5294
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7.53 0.1849 0.4122 0.0807 0.0362 0.107 3.375 2.199 79.869 0.381 9.781 12.487 0.17 85998. 0.5054
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8.60 0.2113 0.4553 0.0785 0.0364 0.108 3.394 2.137 80.309 0.383 9.506 12.070 0.17 86105. 0.4816
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9.68 0.2377 0.4950 0.0760 0.0365 0.108 3.403 2.071 80.515 0.384 9.210 11.665 0.17 86220. 0.4581
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10.76 0.2641 0.5314 0.0734 0.0365 0.108 3.400 1.999 80.456 0.384 8.893 11.271 0.17 86343. 0.4349
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11.83 0.2906 0.5647 0.0706 0.0363 0.107 3.385 1.923 80.102 0.382 8.552 10.887 0.17 86474. 0.4120
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12.91 0.3170 0.5949 0.0676 0.0360 0.107 3.357 1.841 79.424 0.379 8.189 10.513 0.17 86613. 0.3893
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13.98 0.3434 0.6221 0.0644 0.0355 0.105 3.313 1.754 78.395 0.374 7.802 10.148 0.17 86760. 0.3668
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15.06 0.3698 0.6463 0.0610 0.0349 0.103 3.253 1.662 76.985 0.368 7.392 9.791 0.17 86916. 0.3445
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16.13 0.3962 0.6676 0.0574 0.0341 0.101 3.177 1.564 75.170 0.359 6.958 9.439 0.17 87080. 0.3222
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17.21 0.4226 0.6858 0.0537 0.0331 0.098 3.083 1.462 72.945 0.348 6.502 9.090 0.17 87253. 0.2999
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18.28 0.4490 0.7007 0.0498 0.0319 0.094 2.972 1.355 70.321 0.336 6.028 8.742 0.17 87434. 0.2777
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19.36 0.4754 0.7121 0.0457 0.0305 0.090 2.845 1.245 67.311 0.321 5.538 8.390 0.17 87623. 0.2555
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20.44 0.5019 0.7194 0.0416 0.0290 0.086 2.702 1.132 63.928 0.305 5.034 8.030 0.17 87821. 0.2331
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21.51 0.5283 0.7220 0.0373 0.0273 0.081 2.544 1.016 60.187 0.287 4.519 7.656 0.17 88027. 0.2106
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22.59 0.5547 0.7190 0.0330 0.0254 0.075 2.371 0.898 56.101 0.268 3.995 7.261 0.17 88242. 0.1878
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23.66 0.5811 0.7090 0.0286 0.0234 0.069 2.184 0.779 51.687 0.247 3.464 6.835 0.17 88465. 0.1646
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24.74 0.6075 0.6899 0.0242 0.0213 0.063 1.985 0.659 46.963 0.224 2.930 6.362 0.17 88696. 0.1409
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25.81 0.6339 0.6585 0.0198 0.0190 0.056 1.773 0.538 41.954 0.200 2.394 5.819 0.17 88936. 0.1165
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26.89 0.6603 0.6094 0.0154 0.0166 0.049 1.550 0.418 36.686 0.175 1.860 5.169 0.17 89185. 0.0912
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27.96 0.6868 0.5331 0.0110 0.0141 0.042 1.318 0.299 31.192 0.149 1.330 4.348 0.17 89441. 0.0649
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29.04 0.7132 0.4114 0.0067 0.0116 0.034 1.078 0.182 25.514 0.122 0.809 3.232 0.17 89707. 0.0376
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30.12 0.7396 0.2042 0.0025 0.0089 0.026 0.832 0.067 19.696 0.094 0.299 1.547 0.18 89980. 0.0109
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31.19 0.7660
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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 0.0927 0.0321 0.320 6.729 5.680 238.837 0.760 25.265 10.787 0.26 128161. 0.7016
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1.59 0.0261 0.0730 0.0915 0.0327 0.326 6.851 5.606 243.183 0.774 24.934 10.455 0.26 128250. 0.6756
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3.19 0.0522 0.1415 0.0901 0.0332 0.332 6.970 5.524 247.408 0.788 24.571 10.127 0.26 128348. 0.6496
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4.78 0.0783 0.2054 0.0887 0.0338 0.337 7.084 5.434 251.429 0.800 24.173 9.804 0.26 128454. 0.6237
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6.37 0.1043 0.2650 0.0871 0.0343 0.342 7.189 5.337 255.167 0.812 23.737 9.486 0.26 128570. 0.5981
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7.97 0.1304 0.3204 0.0853 0.0347 0.347 7.284 5.230 258.533 0.823 23.263 9.175 0.26 128697. 0.5727
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9.56 0.1565 0.3718 0.0834 0.0351 0.351 7.366 5.114 261.432 0.832 22.747 8.872 0.26 128833. 0.5476
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11.15 0.1826 0.4194 0.0814 0.0354 0.354 7.431 4.988 263.767 0.840 22.187 8.577 0.26 128980. 0.5228
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12.75 0.2087 0.4633 0.0792 0.0357 0.356 7.478 4.852 265.435 0.845 21.581 8.291 0.26 129138. 0.4984
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14.34 0.2348 0.5037 0.0768 0.0358 0.357 7.504 4.705 266.335 0.848 20.929 8.013 0.26 129308. 0.4744
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15.93 0.2608 0.5409 0.0742 0.0358 0.357 7.505 4.547 266.362 0.848 20.227 7.743 0.26 129488. 0.4507
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17.53 0.2869 0.5749 0.0714 0.0357 0.356 7.478 4.378 265.417 0.845 19.475 7.482 0.26 129681. 0.4273
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19.12 0.3130 0.6059 0.0685 0.0354 0.353 7.421 4.198 263.401 0.838 18.673 7.229 0.26 129886. 0.4042
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20.71 0.3391 0.6340 0.0654 0.0350 0.349 7.332 4.006 260.222 0.828 17.819 6.983 0.26 130102. 0.3814
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22.31 0.3652 0.6593 0.0620 0.0344 0.343 7.207 3.802 255.785 0.814 16.913 6.743 0.26 130331. 0.3588
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23.90 0.3913 0.6818 0.0585 0.0336 0.335 7.043 3.587 249.996 0.796 15.955 6.508 0.26 130572. 0.3364
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25.49 0.4174 0.7015 0.0548 0.0326 0.326 6.841 3.360 242.823 0.773 14.947 6.277 0.26 130826. 0.3140
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27.09 0.4434 0.7182 0.0510 0.0315 0.314 6.601 3.124 234.294 0.746 13.896 6.048 0.26 131091. 0.2918
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28.68 0.4695 0.7317 0.0470 0.0302 0.301 6.324 2.880 224.448 0.714 12.809 5.819 0.26 131369. 0.2695
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30.27 0.4956 0.7416 0.0429 0.0287 0.286 6.010 2.628 213.327 0.679 11.690 5.588 0.26 131659. 0.2472
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31.87 0.5217 0.7475 0.0387 0.0270 0.270 5.662 2.371 200.973 0.640 10.546 5.351 0.26 131962. 0.2249
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33.46 0.5478 0.7486 0.0344 0.0252 0.251 5.281 2.109 187.432 0.597 9.381 5.104 0.26 132277. 0.2023
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35.05 0.5739 0.7438 0.0301 0.0232 0.232 4.867 1.843 172.755 0.550 8.200 4.840 0.26 132604. 0.1793
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36.64 0.6000 0.7313 0.0257 0.0211 0.211 4.423 1.576 157.003 0.500 7.009 4.552 0.26 132943. 0.1559
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38.24 0.6260 0.7085 0.0213 0.0188 0.188 3.951 1.307 140.247 0.446 5.813 4.227 0.26 133295. 0.1319
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39.83 0.6521 0.6710 0.0169 0.0165 0.164 3.453 1.038 122.575 0.390 4.619 3.843 0.26 133660. 0.1069
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41.42 0.6782 0.6108 0.0126 0.0140 0.140 2.933 0.772 104.094 0.331 3.433 3.363 0.26 134036. 0.0806
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43.02 0.7043 0.5125 0.0083 0.0114 0.114 2.393 0.509 84.932 0.270 2.264 2.718 0.26 134425. 0.0529
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44.61 0.7304 0.3415 0.0041 0.0088 0.087 1.838 0.251 65.238 0.208 1.117 1.746 0.26 134826. 0.0239
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46.20 0.7565 0.0001 0.0000 0.0061 0.061 1.272 0.000 45.135 0.144 0.000 0.001 0.26 135234. 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 0.0933 0.0317 0.750 11.825 10.160 559.601 1.336 45.193 8.235 0.34 170874. 0.7164
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2.13 0.0261 0.0743 0.0920 0.0323 0.765 12.048 10.029 570.169 1.361 44.608 7.978 0.34 170993. 0.6895
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4.25 0.0522 0.1439 0.0907 0.0329 0.778 12.265 9.884 580.450 1.386 43.966 7.724 0.34 171124. 0.6627
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6.38 0.0783 0.2089 0.0893 0.0335 0.792 12.472 9.726 590.253 1.409 43.261 7.474 0.34 171266. 0.6361
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8.50 0.1044 0.2694 0.0877 0.0340 0.804 12.665 9.553 599.381 1.431 42.490 7.229 0.34 171421. 0.6097
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10.63 0.1305 0.3257 0.0859 0.0344 0.815 12.839 9.363 607.618 1.451 41.648 6.989 0.34 171590. 0.5837
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12.75 0.1566 0.3778 0.0840 0.0348 0.824 12.990 9.157 614.737 1.468 40.731 6.756 0.34 171772. 0.5580
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14.88 0.1827 0.4259 0.0820 0.0352 0.832 13.112 8.933 620.499 1.481 39.734 6.530 0.34 171969. 0.5326
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17.00 0.2088 0.4704 0.0798 0.0354 0.838 13.199 8.691 624.659 1.491 38.656 6.310 0.34 172180. 0.5077
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19.13 0.2349 0.5114 0.0774 0.0355 0.841 13.248 8.429 626.968 1.497 37.492 6.098 0.34 172407. 0.4831
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21.26 0.2610 0.5491 0.0748 0.0355 0.841 13.253 8.147 627.173 1.497 36.239 5.892 0.34 172648. 0.4590
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23.38 0.2871 0.5836 0.0720 0.0354 0.838 13.207 7.846 625.030 1.492 34.897 5.693 0.34 172906. 0.4352
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25.51 0.3132 0.6151 0.0690 0.0352 0.832 13.107 7.523 620.303 1.481 33.463 5.501 0.34 173179. 0.4118
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27.63 0.3393 0.6438 0.0659 0.0347 0.822 12.948 7.180 612.767 1.463 31.936 5.314 0.34 173469. 0.3886
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29.76 0.3654 0.6697 0.0626 0.0341 0.808 12.725 6.815 602.193 1.438 30.315 5.133 0.34 173775. 0.3657
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31.88 0.3915 0.6928 0.0590 0.0333 0.789 12.432 6.429 588.351 1.405 28.598 4.957 0.34 174097. 0.3430
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34.01 0.4176 0.7132 0.0553 0.0324 0.766 12.069 6.024 571.156 1.364 26.793 4.784 0.34 174435. 0.3204
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36.13 0.4437 0.7307 0.0514 0.0312 0.738 11.636 5.600 550.669 1.315 24.911 4.613 0.34 174790. 0.2979
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38.26 0.4698 0.7452 0.0474 0.0299 0.707 11.135 5.162 526.982 1.258 22.961 4.443 0.34 175161. 0.2755
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40.39 0.4959 0.7564 0.0432 0.0284 0.671 10.569 4.711 500.193 1.194 20.956 4.272 0.35 175549. 0.2531
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42.51 0.5220 0.7637 0.0390 0.0267 0.631 9.940 4.250 470.402 1.123 18.904 4.098 0.35 175953. 0.2306
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44.64 0.5481 0.7665 0.0347 0.0248 0.587 9.249 3.780 437.718 1.045 16.814 3.917 0.35 176374. 0.2078
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46.76 0.5742 0.7637 0.0303 0.0228 0.539 8.500 3.304 402.264 0.960 14.696 3.725 0.35 176810. 0.1848
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48.89 0.6003 0.7537 0.0259 0.0206 0.488 7.695 2.824 364.186 0.869 12.560 3.517 0.35 177264. 0.1613
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51.01 0.6264 0.7339 0.0215 0.0183 0.434 6.839 2.342 323.659 0.773 10.415 3.281 0.35 177733. 0.1370
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53.14 0.6525 0.6997 0.0171 0.0159 0.377 5.936 1.860 280.900 0.671 8.274 3.004 0.35 178220. 0.1118
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55.27 0.6786 0.6432 0.0127 0.0134 0.317 4.990 1.382 236.169 0.564 6.148 2.655 0.35 178722. 0.0852
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57.39 0.7047 0.5476 0.0084 0.0108 0.254 4.010 0.911 189.779 0.453 4.051 2.177 0.35 179241. 0.0567
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59.52 0.7308 0.3739 0.0041 0.0081 0.191 3.003 0.449 142.097 0.339 1.997 1.433 0.35 179776. 0.0262
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61.64 0.7569 -0.0014 0.0000 0.0053 0.125 1.974 -0.001 93.408 0.223 -0.005 -0.005 0.35 180320. 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 0.0940 0.0316 1.462 18.433 15.999 1090.409 2.083 71.166 6.655 0.43 213581. 0.7265
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2.66 0.0261 0.0751 0.0928 0.0323 1.491 18.790 15.796 1111.556 2.123 70.262 6.446 0.43 213730. 0.6992
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5.32 0.0522 0.1454 0.0915 0.0329 1.518 19.138 15.573 1132.149 2.162 69.267 6.239 0.43 213893. 0.6719
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7.97 0.0783 0.2110 0.0900 0.0334 1.545 19.471 15.327 1151.806 2.200 68.173 6.036 0.43 214072. 0.6449
|
|
10.63 0.1044 0.2720 0.0884 0.0340 1.569 19.780 15.057 1170.128 2.235 66.974 5.837 0.43 214266. 0.6181
|
|
13.29 0.1305 0.3287 0.0867 0.0344 1.591 20.060 14.762 1186.687 2.266 65.662 5.642 0.43 214477. 0.5916
|
|
15.95 0.1566 0.3812 0.0848 0.0349 1.611 20.303 14.440 1201.026 2.294 64.231 5.453 0.43 214706. 0.5656
|
|
18.60 0.1828 0.4298 0.0828 0.0352 1.626 20.500 14.090 1212.669 2.316 62.673 5.270 0.43 214952. 0.5399
|
|
21.26 0.2089 0.4747 0.0805 0.0354 1.638 20.642 13.711 1221.125 2.332 60.985 5.093 0.43 215217. 0.5146
|
|
23.92 0.2350 0.5160 0.0781 0.0356 1.644 20.723 13.300 1225.893 2.341 59.160 4.921 0.43 215501. 0.4898
|
|
26.58 0.2611 0.5541 0.0755 0.0356 1.645 20.733 12.859 1226.473 2.342 57.195 4.755 0.43 215804. 0.4654
|
|
29.24 0.2872 0.5890 0.0727 0.0355 1.639 20.664 12.384 1222.376 2.335 55.086 4.595 0.43 216127. 0.4413
|
|
31.89 0.3133 0.6209 0.0698 0.0352 1.627 20.507 11.877 1213.130 2.317 52.830 4.441 0.43 216469. 0.4177
|
|
34.55 0.3394 0.6500 0.0666 0.0348 1.607 20.256 11.337 1198.283 2.289 50.427 4.291 0.43 216832. 0.3943
|
|
37.21 0.3655 0.6763 0.0632 0.0342 1.579 19.903 10.763 1177.385 2.249 47.873 4.146 0.43 217215. 0.3712
|
|
39.87 0.3916 0.7000 0.0597 0.0334 1.542 19.440 10.155 1149.972 2.196 45.168 4.005 0.43 217619. 0.3483
|
|
42.52 0.4177 0.7210 0.0559 0.0324 1.496 18.863 9.515 1115.862 2.131 42.321 3.867 0.43 218043. 0.3256
|
|
45.18 0.4438 0.7392 0.0520 0.0312 1.442 18.175 8.847 1075.166 2.053 39.350 3.732 0.43 218487. 0.3029
|
|
47.84 0.4699 0.7545 0.0479 0.0298 1.379 17.379 8.155 1028.067 1.963 36.272 3.598 0.43 218952. 0.2804
|
|
50.50 0.4961 0.7667 0.0437 0.0283 1.307 16.478 7.442 974.754 1.862 33.104 3.463 0.43 219437. 0.2578
|
|
53.16 0.5222 0.7751 0.0394 0.0266 1.228 15.475 6.713 915.427 1.748 29.861 3.326 0.43 219943. 0.2352
|
|
55.81 0.5483 0.7793 0.0351 0.0247 1.140 14.374 5.971 850.300 1.624 26.557 3.185 0.43 220469. 0.2124
|
|
58.47 0.5744 0.7781 0.0307 0.0226 1.045 13.179 5.218 779.620 1.489 23.209 3.036 0.43 221016. 0.1892
|
|
61.13 0.6005 0.7701 0.0262 0.0204 0.944 11.895 4.458 703.679 1.344 19.831 2.874 0.43 221583. 0.1656
|
|
63.79 0.6266 0.7526 0.0217 0.0181 0.835 10.529 3.696 622.830 1.190 16.439 2.692 0.43 222171. 0.1412
|
|
66.44 0.6527 0.7213 0.0172 0.0156 0.721 9.086 2.935 537.505 1.027 13.053 2.476 0.44 222779. 0.1158
|
|
69.10 0.6788 0.6678 0.0128 0.0130 0.601 7.577 2.179 448.229 0.856 9.690 2.205 0.44 223408. 0.0888
|
|
71.76 0.7049 0.5749 0.0084 0.0103 0.477 6.012 1.433 355.637 0.679 6.373 1.827 0.44 224057. 0.0597
|
|
74.42 0.7310 0.3991 0.0041 0.0076 0.349 4.403 0.703 260.473 0.497 3.125 1.223 0.44 224726. 0.0280
|
|
77.08 0.7571 -0.0086 -0.0001 0.0047 0.219 2.760 -0.009 163.256 0.312 -0.041 -0.026 0.44 225404. 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 0.0949 0.0318 2.538 26.664 23.262 1892.802 3.012 103.471 5.574 0.51 256279. 0.7337
|
|
3.19 0.0261 0.0754 0.0937 0.0324 2.589 27.192 22.975 1930.274 3.072 102.192 5.399 0.51 256457. 0.7062
|
|
6.37 0.0522 0.1460 0.0924 0.0330 2.638 27.707 22.657 1966.808 3.130 100.778 5.225 0.51 256653. 0.6788
|
|
9.56 0.0782 0.2118 0.0910 0.0336 2.684 28.198 22.307 2001.710 3.186 99.221 5.055 0.51 256868. 0.6515
|
|
12.75 0.1043 0.2731 0.0894 0.0342 2.728 28.657 21.922 2034.278 3.238 97.509 4.888 0.51 257102. 0.6246
|
|
15.93 0.1304 0.3300 0.0877 0.0347 2.768 29.072 21.500 2063.754 3.285 95.632 4.725 0.51 257355. 0.5980
|
|
19.12 0.1565 0.3828 0.0858 0.0351 2.802 29.433 21.038 2089.328 3.325 93.579 4.567 0.51 257630. 0.5717
|
|
22.30 0.1826 0.4316 0.0838 0.0354 2.830 29.726 20.535 2110.153 3.358 91.342 4.414 0.51 257926. 0.5459
|
|
25.49 0.2087 0.4767 0.0815 0.0357 2.850 29.940 19.989 2125.359 3.383 88.911 4.266 0.51 258245. 0.5205
|
|
28.68 0.2347 0.5183 0.0791 0.0358 2.862 30.063 19.397 2134.063 3.396 86.280 4.123 0.51 258586. 0.4955
|
|
31.86 0.2608 0.5566 0.0765 0.0359 2.864 30.081 18.759 2135.382 3.399 83.441 3.985 0.51 258950. 0.4710
|
|
35.05 0.2869 0.5918 0.0737 0.0357 2.854 29.984 18.073 2128.450 3.388 80.390 3.851 0.51 259337. 0.4469
|
|
38.24 0.3130 0.6240 0.0707 0.0355 2.833 29.758 17.339 2112.437 3.362 77.123 3.723 0.51 259749. 0.4231
|
|
41.42 0.3391 0.6535 0.0675 0.0350 2.798 29.393 16.555 2086.550 3.321 73.638 3.599 0.51 260184. 0.3996
|
|
44.61 0.3652 0.6803 0.0641 0.0344 2.749 28.878 15.722 2049.997 3.263 69.932 3.479 0.52 260644. 0.3764
|
|
47.79 0.3912 0.7044 0.0605 0.0336 2.685 28.202 14.839 2001.965 3.186 66.003 3.362 0.52 261129. 0.3534
|
|
50.98 0.4173 0.7260 0.0567 0.0326 2.604 27.358 13.908 1942.092 3.091 61.863 3.248 0.52 261637. 0.3306
|
|
54.17 0.4434 0.7448 0.0528 0.0314 2.508 26.351 12.936 1870.553 2.977 57.538 3.137 0.52 262171. 0.3079
|
|
57.35 0.4695 0.7609 0.0487 0.0300 2.397 25.183 11.928 1787.666 2.845 53.055 3.026 0.52 262728. 0.2852
|
|
60.54 0.4956 0.7739 0.0444 0.0284 2.271 23.860 10.889 1693.770 2.696 48.436 2.916 0.52 263310. 0.2626
|
|
63.73 0.5217 0.7835 0.0401 0.0267 2.131 22.387 9.826 1589.211 2.529 43.706 2.804 0.52 263917. 0.2399
|
|
66.91 0.5477 0.7889 0.0357 0.0248 1.977 20.770 8.742 1474.372 2.347 38.886 2.689 0.52 264548. 0.2170
|
|
70.10 0.5738 0.7893 0.0312 0.0227 1.810 19.013 7.643 1349.684 2.148 33.997 2.569 0.52 265203. 0.1938
|
|
73.28 0.5999 0.7832 0.0267 0.0204 1.630 17.125 6.534 1215.662 1.935 29.063 2.438 0.52 265883. 0.1701
|
|
76.47 0.6260 0.7681 0.0221 0.0180 1.439 15.114 5.420 1072.931 1.708 24.107 2.291 0.52 266588. 0.1456
|
|
79.66 0.6521 0.7397 0.0176 0.0155 1.237 12.992 4.307 922.254 1.468 19.157 2.118 0.52 267317. 0.1200
|
|
82.84 0.6782 0.6898 0.0131 0.0128 1.025 10.770 3.201 764.561 1.217 14.240 1.899 0.52 268070. 0.0927
|
|
86.03 0.7042 0.6008 0.0086 0.0101 0.806 8.466 2.111 600.980 0.956 9.388 1.593 0.52 268848. 0.0632
|
|
89.22 0.7303 0.4272 0.0043 0.0073 0.580 6.097 1.042 432.838 0.689 4.637 1.092 0.53 269650. 0.0304
|
|
92.40 0.7564 0.0008 0.0000 0.0044 0.350 3.678 0.001 261.078 0.416 0.005 0.002 0.53 270462. 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 0.0960 0.0321 4.073 36.677 32.036 3037.556 4.144 142.494 4.784 0.60 298964. 0.7389
|
|
3.72 0.0261 0.0755 0.0949 0.0328 4.156 37.418 31.653 3098.902 4.227 140.792 4.633 0.60 299173. 0.7114
|
|
7.43 0.0521 0.1461 0.0936 0.0334 4.236 38.141 31.229 3158.761 4.309 138.905 4.484 0.60 299402. 0.6839
|
|
11.15 0.0782 0.2120 0.0922 0.0340 4.313 38.832 30.760 3216.010 4.387 136.819 4.338 0.60 299653. 0.6566
|
|
14.86 0.1043 0.2733 0.0906 0.0346 4.384 39.478 30.242 3269.488 4.460 134.517 4.195 0.60 299927. 0.6297
|
|
18.58 0.1303 0.3303 0.0889 0.0351 4.449 40.063 29.673 3317.942 4.526 131.984 4.056 0.60 300223. 0.6030
|
|
22.29 0.1564 0.3832 0.0871 0.0355 4.506 40.571 29.048 3360.047 4.584 129.206 3.921 0.60 300545. 0.5768
|
|
26.01 0.1825 0.4321 0.0850 0.0359 4.552 40.986 28.365 3394.405 4.631 126.169 3.790 0.60 300891. 0.5509
|
|
29.72 0.2086 0.4774 0.0828 0.0362 4.586 41.290 27.622 3419.597 4.665 122.861 3.664 0.60 301263. 0.5255
|
|
33.44 0.2346 0.5192 0.0804 0.0363 4.605 41.466 26.815 3434.172 4.685 119.272 3.542 0.60 301662. 0.5005
|
|
37.15 0.2607 0.5577 0.0777 0.0363 4.609 41.497 25.942 3436.692 4.688 115.391 3.424 0.60 302088. 0.4759
|
|
40.87 0.2868 0.5931 0.0749 0.0362 4.594 41.365 25.003 3425.745 4.673 111.213 3.310 0.60 302541. 0.4517
|
|
44.58 0.3128 0.6257 0.0719 0.0360 4.559 41.053 23.995 3399.978 4.638 106.730 3.201 0.60 303023. 0.4279
|
|
48.30 0.3389 0.6555 0.0687 0.0355 4.503 40.548 22.918 3358.106 4.581 101.941 3.096 0.60 303532. 0.4044
|
|
52.01 0.3650 0.6826 0.0653 0.0349 4.424 39.832 21.772 3298.856 4.500 96.843 2.994 0.60 304069. 0.3812
|
|
55.73 0.3910 0.7072 0.0616 0.0341 4.319 38.891 20.555 3220.916 4.394 91.430 2.895 0.60 304635. 0.3582
|
|
59.45 0.4171 0.7293 0.0578 0.0330 4.189 37.717 19.271 3123.631 4.261 85.720 2.798 0.60 305230. 0.3353
|
|
63.16 0.4432 0.7488 0.0537 0.0318 4.033 36.312 17.929 3007.259 4.102 79.747 2.704 0.60 305852. 0.3125
|
|
66.88 0.4692 0.7655 0.0496 0.0304 3.852 34.682 16.535 2872.321 3.918 73.550 2.611 0.60 306504. 0.2898
|
|
70.59 0.4953 0.7794 0.0453 0.0288 3.647 32.835 15.099 2719.374 3.710 67.160 2.518 0.60 307183. 0.2671
|
|
74.31 0.5214 0.7899 0.0408 0.0270 3.418 30.778 13.626 2548.990 3.477 60.611 2.425 0.61 307891. 0.2443
|
|
78.02 0.5474 0.7965 0.0363 0.0250 3.167 28.518 12.125 2361.792 3.222 53.932 2.329 0.61 308627. 0.2213
|
|
81.74 0.5735 0.7982 0.0318 0.0228 2.895 26.063 10.601 2158.488 2.945 47.154 2.228 0.61 309392. 0.1979
|
|
85.45 0.5996 0.7938 0.0272 0.0205 2.601 23.424 9.062 1939.920 2.646 40.310 2.119 0.61 310185. 0.1741
|
|
89.17 0.6257 0.7807 0.0225 0.0181 2.289 20.613 7.516 1707.113 2.329 33.432 1.997 0.61 311007. 0.1494
|
|
92.88 0.6517 0.7547 0.0179 0.0155 1.960 17.645 5.971 1461.310 1.993 26.559 1.853 0.61 311857. 0.1236
|
|
96.60 0.6778 0.7076 0.0133 0.0127 1.615 14.538 4.436 1204.042 1.643 19.730 1.671 0.61 312736. 0.0960
|
|
100.31 0.7039 0.6216 0.0088 0.0099 1.257 11.316 2.920 937.167 1.278 12.990 1.413 0.61 313642. 0.0659
|
|
104.03 0.7299 0.4481 0.0043 0.0070 0.889 8.004 1.436 662.878 0.904 6.387 0.983 0.61 314577. 0.0321
|
|
107.74 0.7560 -0.0064 0.0000 0.0040 0.513 4.620 -0.011 382.620 0.522 -0.051 -0.014 0.61 315521. 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 0.0974 0.0327 6.186 48.740 42.433 4613.210 5.507 188.742 4.172 0.68 341634. 0.7417
|
|
4.24 0.0260 0.0752 0.0963 0.0334 6.313 49.734 41.950 4707.302 5.619 186.595 4.042 0.68 341873. 0.7145
|
|
8.48 0.0521 0.1455 0.0950 0.0340 6.436 50.707 41.412 4799.405 5.729 184.202 3.914 0.68 342136. 0.6873
|
|
12.72 0.0781 0.2113 0.0937 0.0346 6.555 51.641 40.814 4887.777 5.834 181.542 3.787 0.68 342423. 0.6604
|
|
16.97 0.1042 0.2725 0.0921 0.0352 6.666 52.516 40.151 4970.579 5.933 178.594 3.664 0.68 342736. 0.6336
|
|
21.21 0.1302 0.3294 0.0905 0.0357 6.767 53.311 39.419 5045.812 6.023 175.335 3.543 0.68 343076. 0.6071
|
|
25.45 0.1562 0.3822 0.0886 0.0362 6.854 54.003 38.612 5111.353 6.101 171.744 3.426 0.68 343444. 0.5810
|
|
29.69 0.1823 0.4312 0.0866 0.0366 6.926 54.570 37.726 5165.002 6.165 167.804 3.313 0.68 343841. 0.5553
|
|
33.93 0.2083 0.4765 0.0843 0.0369 6.979 54.987 36.757 5204.519 6.212 163.496 3.203 0.68 344267. 0.5300
|
|
38.17 0.2344 0.5184 0.0819 0.0370 7.010 55.232 35.703 5227.654 6.240 158.806 3.098 0.68 344724. 0.5051
|
|
42.41 0.2604 0.5571 0.0793 0.0371 7.016 55.280 34.560 5232.192 6.245 153.721 2.996 0.68 345212. 0.4807
|
|
46.65 0.2864 0.5927 0.0765 0.0370 6.995 55.108 33.325 5215.961 6.226 148.230 2.898 0.69 345731. 0.4566
|
|
50.90 0.3125 0.6255 0.0734 0.0367 6.942 54.695 31.998 5176.879 6.179 142.327 2.803 0.69 346282. 0.4328
|
|
55.14 0.3385 0.6557 0.0702 0.0362 6.857 54.020 30.577 5112.984 6.103 136.007 2.712 0.69 346865. 0.4093
|
|
59.38 0.3646 0.6832 0.0667 0.0356 6.735 53.063 29.062 5022.355 5.995 129.266 2.625 0.69 347480. 0.3861
|
|
63.62 0.3906 0.7083 0.0630 0.0347 6.575 51.802 27.450 4902.995 5.853 122.099 2.539 0.69 348128. 0.3631
|
|
67.86 0.4166 0.7308 0.0591 0.0337 6.375 50.225 25.747 4753.789 5.674 114.525 2.457 0.69 348808. 0.3402
|
|
72.10 0.4427 0.7510 0.0550 0.0324 6.135 48.337 23.964 4575.088 5.461 106.590 2.376 0.69 349520. 0.3174
|
|
76.34 0.4687 0.7685 0.0507 0.0309 5.857 46.146 22.110 4367.688 5.214 98.345 2.296 0.69 350265. 0.2946
|
|
80.59 0.4948 0.7831 0.0463 0.0293 5.542 43.661 20.197 4132.467 4.933 89.834 2.217 0.69 351042. 0.2719
|
|
84.83 0.5208 0.7946 0.0418 0.0274 5.190 40.891 18.233 3870.319 4.620 81.101 2.137 0.69 351851. 0.2490
|
|
89.07 0.5468 0.8024 0.0372 0.0254 4.804 37.847 16.229 3582.212 4.276 72.187 2.055 0.69 352692. 0.2259
|
|
93.31 0.5729 0.8055 0.0326 0.0232 4.384 34.540 14.194 3269.237 3.902 63.134 1.969 0.69 353565. 0.2025
|
|
97.55 0.5989 0.8027 0.0278 0.0208 3.933 30.985 12.137 2932.700 3.501 53.984 1.877 0.69 354471. 0.1785
|
|
101.79 0.6250 0.7917 0.0231 0.0182 3.452 27.197 10.068 2574.177 3.073 44.783 1.774 0.70 355409. 0.1536
|
|
106.03 0.6510 0.7681 0.0184 0.0156 2.944 23.198 7.999 2195.646 2.621 35.581 1.652 0.70 356379. 0.1276
|
|
110.27 0.6770 0.7241 0.0136 0.0127 2.413 19.013 5.943 1799.583 2.148 26.433 1.498 0.70 357382. 0.0996
|
|
114.52 0.7031 0.6412 0.0090 0.0098 1.863 14.676 3.912 1389.038 1.658 17.399 1.277 0.70 358416. 0.0689
|
|
118.76 0.7291 0.4688 0.0044 0.0069 1.298 10.224 1.921 967.678 1.155 8.545 0.900 0.70 359482. 0.0341
|
|
123.00 0.7552 -0.0095 0.0000 0.0038 0.721 5.684 -0.021 537.997 0.642 -0.093 -0.018 0.70 360558. 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 0.0990 0.0343 9.253 64.801 54.587 6900.008 7.321 242.803 3.588 0.77 384284. 0.7235
|
|
4.76 0.0260 0.0728 0.0979 0.0349 9.416 65.942 54.010 7021.498 7.450 240.236 3.489 0.77 384553. 0.6998
|
|
9.52 0.0520 0.1415 0.0967 0.0355 9.575 67.055 53.362 7140.089 7.576 237.352 3.390 0.77 384848. 0.6758
|
|
14.29 0.0780 0.2061 0.0954 0.0361 9.727 68.120 52.636 7253.461 7.696 234.123 3.291 0.77 385171. 0.6517
|
|
19.05 0.1039 0.2667 0.0940 0.0366 9.869 69.113 51.825 7359.237 7.808 230.518 3.194 0.77 385523. 0.6275
|
|
23.81 0.1299 0.3234 0.0923 0.0371 9.997 70.011 50.923 7454.796 7.910 226.505 3.098 0.77 385906. 0.6034
|
|
28.57 0.1559 0.3763 0.0905 0.0375 10.108 70.786 49.923 7537.352 7.997 222.056 3.004 0.77 386321. 0.5793
|
|
33.33 0.1819 0.4255 0.0885 0.0378 10.197 71.411 48.818 7603.917 8.068 217.144 2.912 0.77 386768. 0.5553
|
|
38.09 0.2079 0.4713 0.0863 0.0381 10.261 71.857 47.605 7651.381 8.118 211.745 2.822 0.77 387249. 0.5314
|
|
42.86 0.2339 0.5137 0.0839 0.0382 10.294 72.093 46.276 7676.530 8.145 205.837 2.734 0.77 387764. 0.5076
|
|
47.62 0.2599 0.5530 0.0813 0.0382 10.294 72.089 44.829 7676.094 8.145 199.402 2.649 0.77 388313. 0.4840
|
|
52.38 0.2859 0.5892 0.0784 0.0380 10.255 71.814 43.261 7646.802 8.114 192.426 2.566 0.77 388899. 0.4606
|
|
57.14 0.3118 0.6227 0.0754 0.0377 10.172 71.238 41.569 7585.431 8.048 184.900 2.486 0.77 389519. 0.4374
|
|
61.90 0.3378 0.6534 0.0721 0.0373 10.043 70.331 39.752 7488.885 7.946 176.818 2.408 0.77 390176. 0.4143
|
|
66.66 0.3638 0.6815 0.0685 0.0366 9.862 69.065 37.810 7354.093 7.803 168.177 2.332 0.77 390869. 0.3913
|
|
71.43 0.3898 0.7072 0.0648 0.0357 9.626 67.410 35.739 7177.814 7.616 158.969 2.258 0.77 391598. 0.3685
|
|
76.19 0.4158 0.7304 0.0608 0.0346 9.331 65.344 33.546 6957.904 7.383 149.214 2.187 0.77 392363. 0.3457
|
|
80.95 0.4418 0.7512 0.0566 0.0333 8.977 62.870 31.244 6694.474 7.103 138.972 2.117 0.78 393164. 0.3229
|
|
85.71 0.4678 0.7695 0.0523 0.0318 8.567 59.999 28.846 6388.700 6.779 128.308 2.048 0.78 394002. 0.3002
|
|
90.47 0.4937 0.7851 0.0478 0.0301 8.102 56.743 26.367 6042.022 6.411 117.282 1.979 0.78 394875. 0.2774
|
|
95.23 0.5197 0.7975 0.0432 0.0281 7.585 53.118 23.820 5656.029 6.001 105.952 1.910 0.78 395784. 0.2544
|
|
100.00 0.5457 0.8062 0.0385 0.0260 7.017 49.140 21.216 5232.467 5.552 94.370 1.839 0.78 396729. 0.2312
|
|
104.76 0.5717 0.8103 0.0337 0.0238 6.401 44.829 18.568 4773.438 5.065 82.591 1.764 0.78 397710. 0.2075
|
|
109.52 0.5977 0.8081 0.0288 0.0213 5.742 40.209 15.888 4281.485 4.543 70.671 1.683 0.78 398727. 0.1831
|
|
114.28 0.6237 0.7972 0.0239 0.0187 5.042 35.310 13.190 3759.814 3.989 58.669 1.591 0.78 399780. 0.1577
|
|
119.04 0.6497 0.7728 0.0190 0.0160 4.308 30.169 10.488 3212.371 3.408 46.648 1.481 0.78 400868. 0.1309
|
|
123.81 0.6757 0.7260 0.0141 0.0132 3.546 24.831 7.797 2644.020 2.805 34.681 1.338 0.79 401993. 0.1019
|
|
128.57 0.7016 0.6372 0.0093 0.0103 2.763 19.352 5.136 2060.604 2.186 22.844 1.130 0.79 403153. 0.0699
|
|
133.33 0.7276 0.4555 0.0046 0.0073 1.970 13.795 2.524 1468.913 1.559 11.225 0.779 0.79 404348. 0.0338
|
|
138.09 0.7536 -0.0087 -0.0001 0.0043 1.172 8.206 -0.028 873.801 0.927 -0.123 -0.014 0.79 405556. 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 0.1007 0.0397 14.675 92.491 68.541 10942.829 10.450 304.870 2.841 0.85 426910. 0.6419
|
|
5.29 0.0260 0.0646 0.0997 0.0401 14.838 93.524 67.892 11065.023 10.566 301.982 2.783 0.85 427207. 0.6258
|
|
10.58 0.0520 0.1264 0.0986 0.0405 14.991 94.484 67.154 11178.557 10.675 298.702 2.725 0.85 427535. 0.6094
|
|
15.87 0.0780 0.1856 0.0974 0.0409 15.127 95.343 66.319 11280.148 10.772 294.988 2.667 0.85 427894. 0.5927
|
|
21.17 0.1040 0.2421 0.0960 0.0412 15.243 96.073 65.377 11366.534 10.854 290.796 2.609 0.85 428286. 0.5757
|
|
26.46 0.1299 0.2959 0.0945 0.0415 15.334 96.646 64.317 11434.359 10.919 286.080 2.551 0.85 428713. 0.5584
|
|
31.75 0.1559 0.3471 0.0927 0.0416 15.395 97.034 63.129 11480.283 10.963 280.799 2.494 0.85 429176. 0.5408
|
|
37.04 0.1819 0.3958 0.0908 0.0417 15.423 97.209 61.806 11501.023 10.983 274.913 2.437 0.85 429675. 0.5230
|
|
42.33 0.2079 0.4419 0.0886 0.0417 15.413 97.145 60.339 11493.362 10.975 268.388 2.381 0.85 430212. 0.5048
|
|
47.62 0.2339 0.4855 0.0862 0.0415 15.360 96.812 58.721 11454.024 10.938 261.192 2.325 0.86 430788. 0.4863
|
|
52.91 0.2599 0.5265 0.0836 0.0413 15.260 96.184 56.947 11379.730 10.867 253.300 2.270 0.86 431402. 0.4675
|
|
58.21 0.2859 0.5651 0.0808 0.0409 15.110 95.234 55.012 11267.291 10.759 244.693 2.215 0.86 432057. 0.4483
|
|
63.50 0.3119 0.6011 0.0777 0.0403 14.903 93.933 52.913 11113.340 10.612 235.355 2.160 0.86 432751. 0.4287
|
|
68.79 0.3379 0.6347 0.0744 0.0396 14.637 92.252 50.647 10914.474 10.423 225.279 2.105 0.86 433485. 0.4088
|
|
74.08 0.3639 0.6658 0.0708 0.0387 14.305 90.162 48.215 10667.208 10.186 214.460 2.050 0.86 434259. 0.3885
|
|
79.37 0.3898 0.6944 0.0670 0.0376 13.903 87.630 45.614 10367.678 9.900 202.889 1.996 0.86 435074. 0.3678
|
|
84.66 0.4158 0.7204 0.0629 0.0363 13.428 84.632 42.848 10012.942 9.562 190.588 1.941 0.86 435928. 0.3467
|
|
89.95 0.4418 0.7439 0.0586 0.0348 12.878 81.166 39.935 9602.921 9.170 177.633 1.886 0.86 436823. 0.3253
|
|
95.25 0.4678 0.7640 0.0542 0.0332 12.264 77.298 36.894 9145.286 8.733 164.104 1.830 0.86 437758. 0.3033
|
|
100.54 0.4938 0.7804 0.0496 0.0314 11.591 73.053 33.741 8643.037 8.253 150.080 1.771 0.86 438732. 0.2807
|
|
105.83 0.5198 0.7924 0.0448 0.0294 10.859 68.443 30.493 8097.644 7.733 135.634 1.708 0.86 439746. 0.2574
|
|
111.12 0.5458 0.7987 0.0399 0.0273 10.078 63.520 27.167 7515.150 7.176 120.837 1.640 0.87 440799. 0.2332
|
|
116.41 0.5718 0.7987 0.0349 0.0250 9.242 58.252 23.779 6891.859 6.581 105.768 1.565 0.87 441892. 0.2083
|
|
121.70 0.5978 0.7897 0.0299 0.0226 8.361 52.696 20.346 6234.552 5.954 90.498 1.480 0.87 443025. 0.1822
|
|
126.99 0.6238 0.7683 0.0248 0.0201 7.442 46.907 16.886 5549.640 5.300 75.109 1.380 0.87 444196. 0.1548
|
|
132.29 0.6497 0.7284 0.0197 0.0176 6.498 40.956 13.418 4845.627 4.627 59.681 1.256 0.87 445408. 0.1256
|
|
137.58 0.6757 0.6596 0.0146 0.0150 5.540 34.920 9.962 4131.406 3.945 44.311 1.094 0.87 446658. 0.0942
|
|
142.87 0.7017 0.5440 0.0096 0.0124 4.583 28.883 6.543 3417.198 3.263 29.105 0.869 0.87 447949. 0.0606
|
|
148.16 0.7277 0.3461 0.0047 0.0098 3.639 22.937 3.188 2713.729 2.591 14.180 0.533 0.88 449278. 0.0260
|
|
153.45 0.7537 -0.0133 -0.0001 0.0073 2.716 17.120 -0.088 2025.493 1.934 -0.393 -0.020 0.88 450627. 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 0.1004 0.0479 23.592 135.179 82.687 17592.609 15.272 367.792 2.132 0.94 469606. 0.5290
|
|
5.88 0.0262 0.0540 0.0996 0.0484 23.830 136.545 82.061 17770.393 15.427 365.009 2.095 0.94 469927. 0.5178
|
|
11.75 0.0525 0.1060 0.0987 0.0489 24.045 137.777 81.337 17930.680 15.566 361.787 2.057 0.94 470282. 0.5064
|
|
17.63 0.0787 0.1562 0.0977 0.0492 24.227 138.818 80.500 18066.236 15.684 358.063 2.021 0.94 470674. 0.4949
|
|
23.50 0.1049 0.2046 0.0965 0.0495 24.366 139.613 79.534 18169.625 15.773 353.769 1.985 0.94 471102. 0.4832
|
|
29.38 0.1312 0.2513 0.0952 0.0497 24.451 140.102 78.425 18233.271 15.829 348.834 1.951 0.94 471571. 0.4715
|
|
35.26 0.1574 0.2964 0.0936 0.0497 24.474 140.230 77.155 18249.898 15.843 343.187 1.918 0.94 472080. 0.4597
|
|
41.13 0.1837 0.3400 0.0919 0.0496 24.424 139.945 75.711 18212.867 15.811 336.762 1.885 0.94 472632. 0.4477
|
|
47.01 0.2099 0.3822 0.0899 0.0494 24.295 139.205 74.078 18116.523 15.727 329.498 1.855 0.94 473228. 0.4356
|
|
52.88 0.2361 0.4231 0.0877 0.0489 24.080 137.974 72.244 17956.385 15.588 321.341 1.825 0.94 473868. 0.4233
|
|
58.76 0.2624 0.4626 0.0852 0.0483 23.774 136.223 70.198 17728.523 15.390 312.241 1.796 0.94 474553. 0.4107
|
|
64.64 0.2886 0.5009 0.0824 0.0475 23.375 133.938 67.933 17431.023 15.132 302.165 1.768 0.94 475284. 0.3976
|
|
70.51 0.3148 0.5377 0.0794 0.0465 22.883 131.115 65.444 17063.672 14.813 291.094 1.740 0.94 476061. 0.3841
|
|
76.39 0.3411 0.5731 0.0761 0.0453 22.295 127.749 62.729 16625.639 14.433 279.017 1.711 0.94 476883. 0.3699
|
|
82.26 0.3673 0.6068 0.0726 0.0439 21.612 123.832 59.785 16115.885 13.990 265.925 1.683 0.94 477752. 0.3551
|
|
88.14 0.3936 0.6388 0.0687 0.0423 20.829 119.350 56.611 15532.556 13.484 251.806 1.653 0.95 478666. 0.3395
|
|
94.02 0.4198 0.6688 0.0646 0.0405 19.948 114.301 53.214 14875.413 12.914 236.694 1.623 0.95 479625. 0.3230
|
|
99.89 0.4460 0.6966 0.0602 0.0386 18.973 108.713 49.616 14148.173 12.282 220.692 1.591 0.95 480630. 0.3058
|
|
105.77 0.4723 0.7219 0.0556 0.0364 17.910 102.623 45.845 13355.662 11.594 203.920 1.557 0.95 481679. 0.2877
|
|
111.64 0.4985 0.7423 0.0509 0.0342 16.813 96.338 41.921 12537.772 10.884 186.465 1.517 0.95 482773. 0.2680
|
|
117.52 0.5247 0.7560 0.0460 0.0319 15.696 89.934 37.866 11704.217 10.161 168.427 1.467 0.95 483911. 0.2464
|
|
123.40 0.5510 0.7583 0.0409 0.0297 14.621 83.777 33.696 10902.938 9.465 149.879 1.402 0.95 485092. 0.2221
|
|
129.27 0.5772 0.7441 0.0357 0.0277 13.633 78.118 29.430 10166.484 8.826 130.905 1.313 0.95 486318. 0.1944
|
|
135.15 0.6035 0.7170 0.0305 0.0257 12.621 72.318 25.111 9411.651 8.170 111.694 1.210 0.96 487588. 0.1655
|
|
141.02 0.6297 0.6728 0.0252 0.0236 11.607 66.507 20.767 8655.420 7.514 92.370 1.088 0.96 488901. 0.1353
|
|
146.90 0.6559 0.6070 0.0199 0.0215 10.603 60.753 16.431 7906.592 6.864 73.084 0.943 0.96 490258. 0.1043
|
|
152.78 0.6822 0.5138 0.0147 0.0196 9.626 55.157 12.141 7178.252 6.232 54.005 0.767 0.96 491659. 0.0730
|
|
158.65 0.7084 0.3866 0.0096 0.0177 8.691 49.798 7.943 6480.809 5.626 35.329 0.556 0.96 493105. 0.0428
|
|
164.53 0.7346 0.2180 0.0047 0.0159 7.806 44.730 3.880 5821.237 5.054 17.257 0.302 0.96 494597. 0.0162
|
|
170.40 0.7609 -0.0033 -0.0001 0.0141 6.948 39.810 -0.051 5180.964 4.498 -0.226 -0.004 0.97 496162. 0.0000
|
|
|
|
|
|
|