464 lines
82 KiB
Plaintext
464 lines
82 KiB
Plaintext
19x12E (19x12E.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 0.0952 0.0384 0.008 0.483 0.395 5.712 0.055 1.759 31.396 0.08 33270. 0.6097
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0.48 0.0268 0.0646 0.0941 0.0390 0.008 0.490 0.391 5.800 0.055 1.738 30.546 0.08 33294. 0.5896
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0.96 0.0536 0.1256 0.0928 0.0396 0.008 0.498 0.385 5.887 0.056 1.714 29.695 0.08 33320. 0.5693
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1.45 0.0804 0.1830 0.0914 0.0402 0.008 0.505 0.380 5.970 0.057 1.689 28.846 0.08 33349. 0.5489
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1.93 0.1072 0.2368 0.0899 0.0407 0.008 0.511 0.373 6.048 0.058 1.661 28.003 0.08 33380. 0.5284
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2.41 0.1340 0.2872 0.0882 0.0412 0.008 0.517 0.366 6.118 0.058 1.630 27.168 0.08 33414. 0.5079
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2.89 0.1608 0.3342 0.0864 0.0416 0.008 0.522 0.359 6.179 0.059 1.596 26.344 0.08 33451. 0.4874
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3.38 0.1876 0.3779 0.0844 0.0419 0.008 0.527 0.351 6.229 0.059 1.560 25.534 0.08 33492. 0.4670
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3.86 0.2144 0.4184 0.0823 0.0422 0.008 0.530 0.342 6.265 0.060 1.520 24.737 0.08 33535. 0.4466
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4.34 0.2412 0.4558 0.0799 0.0423 0.008 0.531 0.332 6.286 0.060 1.477 23.956 0.08 33581. 0.4263
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4.82 0.2680 0.4903 0.0774 0.0423 0.008 0.531 0.321 6.287 0.060 1.430 23.190 0.08 33631. 0.4060
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5.30 0.2948 0.5218 0.0747 0.0422 0.008 0.530 0.310 6.268 0.060 1.379 22.438 0.08 33684. 0.3859
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5.79 0.3216 0.5505 0.0717 0.0419 0.008 0.526 0.298 6.227 0.059 1.325 21.700 0.08 33740. 0.3658
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6.27 0.3484 0.5764 0.0686 0.0415 0.008 0.521 0.285 6.160 0.059 1.267 20.972 0.08 33800. 0.3457
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6.75 0.3752 0.5994 0.0652 0.0408 0.008 0.513 0.271 6.068 0.058 1.205 20.251 0.08 33863. 0.3255
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7.23 0.4020 0.6194 0.0617 0.0400 0.008 0.503 0.256 5.948 0.057 1.139 19.533 0.08 33930. 0.3053
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7.72 0.4288 0.6363 0.0579 0.0390 0.008 0.490 0.241 5.800 0.055 1.070 18.812 0.08 34000. 0.2849
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8.20 0.4556 0.6499 0.0540 0.0378 0.008 0.475 0.224 5.622 0.054 0.997 18.082 0.08 34073. 0.2643
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8.68 0.4824 0.6596 0.0498 0.0364 0.007 0.458 0.207 5.416 0.052 0.921 17.334 0.08 34150. 0.2435
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9.16 0.5092 0.6652 0.0456 0.0349 0.007 0.438 0.189 5.184 0.050 0.842 16.560 0.08 34230. 0.2225
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9.64 0.5360 0.6658 0.0412 0.0332 0.007 0.416 0.171 4.927 0.047 0.761 15.746 0.08 34314. 0.2011
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10.13 0.5628 0.6605 0.0367 0.0313 0.006 0.393 0.152 4.647 0.044 0.678 14.878 0.08 34401. 0.1794
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10.61 0.5897 0.6482 0.0321 0.0292 0.006 0.367 0.133 4.344 0.041 0.594 13.936 0.08 34491. 0.1572
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11.09 0.6165 0.6269 0.0275 0.0271 0.005 0.340 0.114 4.021 0.038 0.508 12.892 0.08 34585. 0.1346
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11.57 0.6433 0.5941 0.0229 0.0248 0.005 0.311 0.095 3.679 0.035 0.422 11.709 0.08 34682. 0.1114
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12.06 0.6701 0.5460 0.0182 0.0223 0.004 0.281 0.076 3.319 0.032 0.336 10.331 0.08 34783. 0.0877
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12.54 0.6969 0.4767 0.0136 0.0198 0.004 0.249 0.056 2.944 0.028 0.250 8.673 0.08 34887. 0.0635
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13.02 0.7237 0.3765 0.0089 0.0172 0.003 0.216 0.037 2.555 0.024 0.165 6.596 0.08 34994. 0.0393
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13.50 0.7505 0.2284 0.0044 0.0145 0.003 0.182 0.018 2.157 0.021 0.082 3.858 0.08 35105. 0.0161
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13.98 0.7773 -0.0003 0.0000 0.0118 0.002 0.148 0.000 1.752 0.017 0.000 -0.005 0.08 35219. 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 0.0955 0.0357 0.057 1.795 1.587 42.472 0.203 7.060 16.950 0.15 66539. 0.6595
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0.97 0.0269 0.0699 0.0944 0.0364 0.058 1.827 1.568 43.228 0.206 6.976 16.456 0.15 66587. 0.6364
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1.94 0.0539 0.1356 0.0932 0.0370 0.059 1.858 1.547 43.971 0.210 6.883 15.962 0.15 66639. 0.6132
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2.91 0.0808 0.1972 0.0918 0.0376 0.060 1.889 1.525 44.689 0.213 6.781 15.473 0.15 66697. 0.5900
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3.88 0.1077 0.2547 0.0903 0.0382 0.061 1.917 1.499 45.365 0.217 6.669 14.991 0.15 66761. 0.5669
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4.84 0.1346 0.3083 0.0886 0.0387 0.062 1.943 1.472 45.985 0.220 6.546 14.516 0.15 66830. 0.5438
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5.81 0.1616 0.3581 0.0868 0.0391 0.062 1.966 1.441 46.532 0.222 6.411 14.050 0.15 66904. 0.5209
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6.78 0.1885 0.4043 0.0848 0.0395 0.063 1.986 1.408 46.986 0.224 6.264 13.595 0.15 66985. 0.4982
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7.75 0.2154 0.4469 0.0826 0.0398 0.063 2.000 1.372 47.329 0.226 6.104 13.151 0.15 67072. 0.4758
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8.72 0.2424 0.4863 0.0802 0.0400 0.064 2.009 1.333 47.541 0.227 5.930 12.719 0.15 67166. 0.4535
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9.69 0.2693 0.5224 0.0777 0.0400 0.064 2.012 1.291 47.603 0.227 5.741 12.298 0.15 67266. 0.4315
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10.66 0.2962 0.5556 0.0749 0.0400 0.064 2.007 1.245 47.494 0.227 5.537 11.889 0.15 67373. 0.4097
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11.63 0.3231 0.5858 0.0720 0.0397 0.063 1.995 1.196 47.198 0.225 5.319 11.491 0.15 67487. 0.3880
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12.60 0.3501 0.6131 0.0688 0.0393 0.063 1.974 1.143 46.698 0.223 5.084 11.102 0.15 67607. 0.3666
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13.57 0.3770 0.6376 0.0654 0.0387 0.062 1.943 1.087 45.980 0.220 4.834 10.721 0.15 67734. 0.3452
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14.53 0.4039 0.6593 0.0618 0.0379 0.060 1.903 1.027 45.032 0.215 4.569 10.347 0.15 67869. 0.3239
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15.50 0.4308 0.6780 0.0580 0.0369 0.059 1.853 0.964 43.841 0.209 4.289 9.975 0.15 68010. 0.3025
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16.47 0.4578 0.6936 0.0540 0.0357 0.057 1.792 0.898 42.402 0.202 3.994 9.604 0.15 68158. 0.2810
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17.44 0.4847 0.7057 0.0499 0.0343 0.055 1.721 0.829 40.727 0.194 3.686 9.229 0.15 68313. 0.2595
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18.41 0.5116 0.7140 0.0456 0.0327 0.052 1.641 0.757 38.827 0.185 3.368 8.846 0.15 68475. 0.2377
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19.38 0.5386 0.7179 0.0412 0.0309 0.049 1.552 0.684 36.713 0.175 3.042 8.449 0.15 68643. 0.2158
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20.35 0.5655 0.7164 0.0367 0.0289 0.046 1.454 0.609 34.397 0.164 2.709 8.030 0.15 68819. 0.1935
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21.32 0.5924 0.7083 0.0321 0.0268 0.043 1.348 0.533 31.887 0.152 2.370 7.579 0.15 69001. 0.1709
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22.29 0.6193 0.6919 0.0274 0.0246 0.039 1.234 0.456 29.196 0.139 2.028 7.082 0.15 69191. 0.1477
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23.26 0.6463 0.6644 0.0228 0.0222 0.035 1.113 0.378 26.336 0.126 1.683 6.516 0.15 69387. 0.1238
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24.22 0.6732 0.6213 0.0181 0.0196 0.031 0.986 0.301 23.323 0.111 1.338 5.850 0.15 69590. 0.0991
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25.19 0.7001 0.5554 0.0135 0.0170 0.027 0.853 0.224 20.174 0.096 0.995 5.028 0.15 69800. 0.0734
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26.16 0.7271 0.4532 0.0089 0.0142 0.023 0.715 0.147 16.912 0.081 0.655 3.952 0.15 70016. 0.0468
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27.13 0.7540 0.2882 0.0044 0.0114 0.018 0.573 0.072 13.561 0.065 0.322 2.423 0.16 70240. 0.0201
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28.10 0.7809 -0.0031 0.0000 0.0085 0.014 0.429 -0.001 10.148 0.048 -0.003 -0.025 0.16 70468. 0.0000
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PROP RPM = 3000
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V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
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(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
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0.00 0.0000 0.0000 0.0959 0.0346 0.186 3.915 3.584 138.952 0.442 15.944 11.701 0.23 99806. 0.6841
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1.46 0.0270 0.0724 0.0948 0.0353 0.190 3.989 3.542 141.586 0.451 15.756 11.348 0.23 99878. 0.6596
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2.91 0.0540 0.1404 0.0935 0.0359 0.193 4.062 3.496 144.183 0.459 15.548 10.996 0.23 99957. 0.6349
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4.37 0.0809 0.2039 0.0921 0.0366 0.197 4.133 3.444 146.694 0.467 15.320 10.649 0.23 100045. 0.6103
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5.82 0.1079 0.2632 0.0906 0.0372 0.200 4.200 3.388 149.070 0.475 15.068 10.307 0.23 100140. 0.5859
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7.28 0.1349 0.3183 0.0890 0.0377 0.203 4.262 3.325 151.257 0.481 14.792 9.972 0.23 100244. 0.5616
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8.74 0.1619 0.3694 0.0871 0.0382 0.205 4.316 3.257 153.194 0.488 14.489 9.644 0.23 100356. 0.5375
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10.19 0.1888 0.4167 0.0852 0.0386 0.208 4.362 3.183 154.819 0.493 14.157 9.325 0.23 100478. 0.5138
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11.65 0.2158 0.4603 0.0830 0.0389 0.209 4.397 3.102 156.064 0.497 13.796 9.014 0.23 100609. 0.4903
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13.10 0.2428 0.5006 0.0806 0.0391 0.210 4.419 3.013 156.862 0.499 13.403 8.713 0.23 100750. 0.4671
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14.56 0.2698 0.5375 0.0781 0.0392 0.211 4.427 2.917 157.144 0.500 12.977 8.421 0.23 100901. 0.4442
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16.02 0.2967 0.5714 0.0753 0.0391 0.210 4.419 2.814 156.842 0.499 12.517 8.138 0.23 101062. 0.4216
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17.47 0.3237 0.6024 0.0723 0.0389 0.209 4.392 2.703 155.896 0.496 12.022 7.864 0.23 101233. 0.3992
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18.93 0.3507 0.6304 0.0691 0.0384 0.207 4.346 2.584 154.247 0.491 11.492 7.597 0.23 101414. 0.3771
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20.38 0.3777 0.6558 0.0657 0.0379 0.204 4.278 2.457 151.846 0.483 10.927 7.338 0.23 101606. 0.3552
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21.84 0.4046 0.6783 0.0621 0.0371 0.199 4.188 2.322 148.650 0.473 10.326 7.084 0.23 101808. 0.3333
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23.30 0.4316 0.6980 0.0583 0.0360 0.194 4.074 2.179 144.610 0.460 9.691 6.834 0.23 102020. 0.3115
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24.75 0.4586 0.7146 0.0543 0.0348 0.187 3.936 2.029 139.714 0.445 9.023 6.586 0.23 102243. 0.2897
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26.21 0.4856 0.7281 0.0501 0.0334 0.180 3.775 1.872 133.993 0.427 8.327 6.337 0.23 102476. 0.2678
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27.67 0.5125 0.7380 0.0458 0.0318 0.171 3.592 1.710 127.488 0.406 7.608 6.085 0.23 102720. 0.2458
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29.12 0.5395 0.7438 0.0413 0.0300 0.161 3.387 1.544 120.234 0.383 6.869 5.826 0.23 102974. 0.2236
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30.58 0.5665 0.7446 0.0368 0.0280 0.151 3.163 1.375 112.267 0.357 6.115 5.554 0.23 103238. 0.2011
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32.03 0.5935 0.7393 0.0322 0.0258 0.139 2.919 1.203 103.621 0.330 5.349 5.264 0.23 103513. 0.1783
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33.49 0.6204 0.7261 0.0275 0.0235 0.127 2.658 1.029 94.336 0.300 4.575 4.945 0.23 103798. 0.1549
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34.95 0.6474 0.7022 0.0228 0.0211 0.113 2.379 0.854 84.457 0.269 3.796 4.584 0.23 104093. 0.1308
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36.40 0.6744 0.6632 0.0181 0.0185 0.099 2.086 0.678 74.036 0.236 3.017 4.156 0.23 104398. 0.1057
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37.86 0.7014 0.6012 0.0135 0.0157 0.085 1.779 0.504 63.139 0.201 2.243 3.622 0.23 104714. 0.0794
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39.31 0.7283 0.5008 0.0089 0.0129 0.070 1.461 0.332 51.842 0.165 1.477 2.906 0.23 105040. 0.0517
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40.77 0.7553 0.3291 0.0044 0.0100 0.054 1.134 0.163 40.236 0.128 0.727 1.841 0.23 105377. 0.0230
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42.23 0.7823 -0.0032 0.0000 0.0071 0.038 0.800 -0.001 28.406 0.090 -0.005 -0.017 0.23 105720. 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 0.0963 0.0341 0.435 6.853 6.402 324.326 0.774 28.474 8.953 0.30 133070. 0.6995
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1.94 0.0270 0.0739 0.0952 0.0348 0.444 6.988 6.327 330.719 0.790 28.143 8.677 0.30 133167. 0.6741
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3.89 0.0540 0.1432 0.0940 0.0354 0.452 7.122 6.245 337.028 0.805 27.777 8.404 0.30 133273. 0.6486
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5.83 0.0810 0.2079 0.0926 0.0361 0.460 7.251 6.154 343.139 0.819 27.372 8.134 0.30 133389. 0.6232
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7.77 0.1080 0.2681 0.0911 0.0367 0.468 7.373 6.054 348.932 0.833 26.927 7.869 0.30 133516. 0.5979
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9.72 0.1350 0.3241 0.0894 0.0373 0.475 7.486 5.944 354.276 0.846 26.437 7.609 0.30 133655. 0.5729
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11.66 0.1620 0.3760 0.0876 0.0378 0.481 7.586 5.823 359.026 0.857 25.899 7.356 0.30 133806. 0.5482
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13.60 0.1890 0.4239 0.0856 0.0382 0.487 7.671 5.690 363.028 0.867 25.310 7.109 0.30 133968. 0.5237
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15.55 0.2160 0.4682 0.0835 0.0385 0.491 7.736 5.546 366.121 0.874 24.667 6.870 0.30 134144. 0.4996
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17.49 0.2430 0.5090 0.0811 0.0387 0.494 7.779 5.388 368.141 0.879 23.967 6.639 0.30 134332. 0.4759
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19.43 0.2700 0.5465 0.0785 0.0388 0.495 7.796 5.218 368.921 0.881 23.208 6.415 0.30 134534. 0.4525
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21.37 0.2970 0.5808 0.0757 0.0387 0.494 7.782 5.033 368.298 0.879 22.387 6.198 0.30 134749. 0.4294
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23.32 0.3240 0.6122 0.0728 0.0385 0.491 7.736 4.834 366.120 0.874 21.504 5.989 0.30 134977. 0.4067
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25.26 0.3510 0.6408 0.0695 0.0381 0.486 7.655 4.622 362.248 0.865 20.557 5.787 0.30 135220. 0.3842
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27.20 0.3780 0.6667 0.0661 0.0375 0.478 7.534 4.394 356.563 0.851 19.546 5.590 0.30 135476. 0.3619
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29.15 0.4050 0.6898 0.0625 0.0367 0.468 7.374 4.153 348.954 0.833 18.473 5.398 0.30 135746. 0.3397
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31.09 0.4320 0.7101 0.0587 0.0357 0.455 7.170 3.898 339.306 0.810 17.336 5.210 0.30 136030. 0.3177
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33.03 0.4590 0.7276 0.0546 0.0344 0.439 6.922 3.629 327.583 0.782 16.141 5.024 0.30 136327. 0.2956
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34.98 0.4860 0.7421 0.0504 0.0330 0.421 6.632 3.349 313.861 0.749 14.895 4.839 0.31 136639. 0.2735
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36.92 0.5130 0.7531 0.0460 0.0314 0.400 6.302 3.059 298.230 0.712 13.608 4.653 0.31 136965. 0.2513
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38.86 0.5400 0.7602 0.0416 0.0295 0.377 5.933 2.762 280.777 0.670 12.286 4.462 0.31 137304. 0.2290
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40.81 0.5670 0.7626 0.0370 0.0275 0.351 5.527 2.459 261.584 0.624 10.936 4.263 0.31 137657. 0.2064
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42.75 0.5940 0.7593 0.0324 0.0253 0.323 5.087 2.150 240.735 0.575 9.565 4.051 0.31 138024. 0.1835
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44.69 0.6210 0.7485 0.0277 0.0230 0.293 4.613 1.839 218.325 0.521 8.179 3.820 0.31 138405. 0.1600
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46.64 0.6480 0.7275 0.0230 0.0204 0.261 4.109 1.526 194.462 0.464 6.786 3.558 0.31 138799. 0.1357
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48.58 0.6750 0.6918 0.0182 0.0178 0.227 3.577 1.212 169.278 0.404 5.392 3.248 0.31 139207. 0.1104
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50.52 0.7020 0.6331 0.0136 0.0150 0.192 3.020 0.901 142.929 0.341 4.007 2.858 0.31 139629. 0.0838
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52.47 0.7290 0.5352 0.0089 0.0122 0.155 2.443 0.593 115.606 0.276 2.638 2.327 0.31 140064. 0.0553
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54.41 0.7560 0.3602 0.0044 0.0092 0.117 1.850 0.291 87.532 0.209 1.296 1.510 0.31 140513. 0.0252
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56.35 0.7830 -0.0044 0.0000 0.0062 0.079 1.245 -0.002 58.908 0.141 -0.010 -0.018 0.31 140971. 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 0.0969 0.0339 0.844 10.637 10.059 629.228 1.202 44.743 7.251 0.38 166331. 0.7102
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2.43 0.0270 0.0748 0.0958 0.0346 0.861 10.852 9.944 641.977 1.226 44.231 7.026 0.38 166452. 0.6842
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4.86 0.0540 0.1449 0.0945 0.0352 0.878 11.065 9.817 654.571 1.250 43.665 6.802 0.38 166584. 0.6582
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7.29 0.0810 0.2103 0.0932 0.0359 0.894 11.272 9.676 666.783 1.273 43.038 6.582 0.38 166730. 0.6323
|
|
9.72 0.1080 0.2711 0.0917 0.0365 0.910 11.468 9.520 678.377 1.296 42.347 6.365 0.38 166889. 0.6065
|
|
12.15 0.1350 0.3276 0.0900 0.0371 0.924 11.649 9.349 689.090 1.316 41.585 6.154 0.38 167063. 0.5811
|
|
14.57 0.1620 0.3800 0.0882 0.0376 0.937 11.810 9.161 698.635 1.334 40.747 5.947 0.38 167251. 0.5559
|
|
17.00 0.1890 0.4284 0.0862 0.0381 0.948 11.946 8.954 706.706 1.350 39.829 5.747 0.38 167455. 0.5311
|
|
19.43 0.2160 0.4730 0.0841 0.0384 0.956 12.053 8.729 712.983 1.362 38.825 5.553 0.38 167674. 0.5066
|
|
21.86 0.2430 0.5142 0.0817 0.0386 0.962 12.123 8.483 717.136 1.370 37.731 5.365 0.38 167910. 0.4826
|
|
24.29 0.2700 0.5520 0.0791 0.0387 0.964 12.152 8.216 718.834 1.373 36.543 5.184 0.38 168163. 0.4589
|
|
26.72 0.2970 0.5867 0.0763 0.0386 0.963 12.133 7.926 717.753 1.371 35.257 5.009 0.38 168432. 0.4355
|
|
29.15 0.3240 0.6185 0.0733 0.0384 0.957 12.063 7.615 713.588 1.363 33.872 4.840 0.38 168718. 0.4125
|
|
31.58 0.3510 0.6475 0.0701 0.0380 0.947 11.936 7.281 706.061 1.348 32.385 4.677 0.38 169021. 0.3898
|
|
34.01 0.3780 0.6737 0.0667 0.0374 0.932 11.747 6.924 694.932 1.327 30.799 4.519 0.38 169342. 0.3672
|
|
36.44 0.4050 0.6973 0.0630 0.0366 0.912 11.495 6.545 679.980 1.299 29.112 4.366 0.38 169680. 0.3449
|
|
38.86 0.4320 0.7182 0.0592 0.0356 0.886 11.173 6.143 660.976 1.262 27.324 4.215 0.38 170035. 0.3227
|
|
41.29 0.4590 0.7364 0.0551 0.0343 0.855 10.782 5.720 637.841 1.218 25.443 4.068 0.38 170408. 0.3004
|
|
43.72 0.4860 0.7516 0.0508 0.0329 0.819 10.324 5.279 610.716 1.166 23.483 3.921 0.38 170798. 0.2782
|
|
46.15 0.5130 0.7635 0.0465 0.0312 0.777 9.801 4.824 579.779 1.107 21.456 3.774 0.38 171205. 0.2560
|
|
48.58 0.5400 0.7717 0.0419 0.0294 0.731 9.216 4.356 545.197 1.041 19.373 3.624 0.38 171629. 0.2335
|
|
51.01 0.5670 0.7755 0.0373 0.0273 0.680 8.573 3.878 507.134 0.969 17.247 3.468 0.38 172071. 0.2109
|
|
53.44 0.5940 0.7738 0.0327 0.0251 0.625 7.873 3.392 465.757 0.890 15.087 3.303 0.38 172530. 0.1879
|
|
55.87 0.6210 0.7650 0.0279 0.0227 0.565 7.121 2.901 421.252 0.805 12.904 3.124 0.38 173006. 0.1643
|
|
58.30 0.6480 0.7465 0.0232 0.0201 0.501 6.320 2.407 373.837 0.714 10.708 2.921 0.38 173499. 0.1400
|
|
60.73 0.6750 0.7137 0.0184 0.0174 0.434 5.473 1.914 323.772 0.618 8.512 2.681 0.39 174009. 0.1145
|
|
63.15 0.7020 0.6584 0.0137 0.0146 0.364 4.587 1.423 271.374 0.518 6.329 2.378 0.39 174537. 0.0876
|
|
65.58 0.7290 0.5637 0.0090 0.0117 0.291 3.669 0.938 217.025 0.414 4.173 1.961 0.39 175081. 0.0586
|
|
68.01 0.7560 0.3884 0.0045 0.0087 0.216 2.725 0.463 161.175 0.308 2.059 1.303 0.39 175642. 0.0274
|
|
70.44 0.7830 0.0002 0.0000 0.0056 0.140 1.762 0.000 104.217 0.199 0.001 0.001 0.39 176214. 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 0.0976 0.0339 1.457 15.308 14.585 1086.636 1.729 64.874 6.088 0.45 199587. 0.7180
|
|
2.92 0.0270 0.0754 0.0965 0.0346 1.487 15.625 14.422 1109.151 1.765 64.148 5.898 0.45 199732. 0.6917
|
|
5.83 0.0540 0.1459 0.0952 0.0353 1.517 15.938 14.241 1131.409 1.801 63.343 5.709 0.45 199891. 0.6653
|
|
8.75 0.0810 0.2118 0.0939 0.0359 1.546 16.243 14.040 1153.018 1.835 62.450 5.523 0.45 200066. 0.6391
|
|
11.66 0.1080 0.2731 0.0924 0.0366 1.574 16.532 13.818 1173.558 1.868 61.463 5.341 0.45 200258. 0.6131
|
|
14.58 0.1350 0.3299 0.0908 0.0372 1.599 16.800 13.573 1192.559 1.898 60.373 5.162 0.45 200467. 0.5873
|
|
17.49 0.1621 0.3826 0.0890 0.0377 1.622 17.039 13.303 1209.520 1.925 59.172 4.989 0.45 200693. 0.5619
|
|
20.41 0.1891 0.4313 0.0870 0.0381 1.641 17.241 13.007 1223.898 1.948 57.853 4.820 0.45 200938. 0.5368
|
|
23.33 0.2161 0.4762 0.0848 0.0385 1.656 17.399 12.682 1235.127 1.966 56.408 4.657 0.45 201202. 0.5122
|
|
26.24 0.2431 0.5176 0.0824 0.0387 1.666 17.505 12.327 1242.625 1.978 54.831 4.500 0.45 201486. 0.4879
|
|
29.16 0.2701 0.5557 0.0799 0.0388 1.671 17.550 11.941 1245.805 1.983 53.116 4.348 0.45 201789. 0.4640
|
|
32.07 0.2971 0.5907 0.0771 0.0388 1.668 17.526 11.524 1244.094 1.980 51.257 4.201 0.45 202113. 0.4404
|
|
34.99 0.3241 0.6228 0.0741 0.0385 1.659 17.425 11.073 1236.951 1.969 49.252 4.060 0.45 202457. 0.4172
|
|
37.90 0.3511 0.6521 0.0708 0.0381 1.641 17.241 10.589 1223.887 1.948 47.099 3.924 0.46 202822. 0.3943
|
|
40.82 0.3781 0.6787 0.0674 0.0375 1.615 16.967 10.071 1204.473 1.917 44.798 3.793 0.46 203207. 0.3717
|
|
43.74 0.4051 0.7027 0.0637 0.0367 1.580 16.599 9.521 1178.322 1.875 42.349 3.665 0.46 203613. 0.3492
|
|
46.65 0.4321 0.7241 0.0598 0.0357 1.536 16.130 8.937 1145.030 1.822 39.754 3.540 0.46 204041. 0.3269
|
|
49.57 0.4591 0.7427 0.0557 0.0344 1.481 15.558 8.323 1104.445 1.758 37.020 3.418 0.46 204488. 0.3045
|
|
52.48 0.4862 0.7586 0.0514 0.0329 1.417 14.887 7.682 1056.806 1.682 34.169 3.297 0.46 204957. 0.2822
|
|
55.40 0.5132 0.7713 0.0469 0.0312 1.344 14.121 7.019 1002.424 1.595 31.219 3.176 0.46 205446. 0.2598
|
|
58.31 0.5402 0.7804 0.0424 0.0293 1.263 13.264 6.337 941.593 1.499 28.189 3.053 0.46 205957. 0.2373
|
|
61.23 0.5672 0.7853 0.0377 0.0273 1.173 12.321 5.642 874.599 1.392 25.093 2.926 0.46 206487. 0.2146
|
|
64.15 0.5942 0.7850 0.0330 0.0250 1.075 11.294 4.934 801.735 1.276 21.948 2.792 0.46 207038. 0.1915
|
|
67.06 0.6212 0.7779 0.0282 0.0225 0.970 10.190 4.219 723.332 1.151 18.768 2.646 0.46 207610. 0.1678
|
|
69.98 0.6482 0.7613 0.0234 0.0199 0.858 9.013 3.500 639.775 1.018 15.569 2.482 0.46 208202. 0.1434
|
|
72.89 0.6752 0.7309 0.0186 0.0172 0.740 7.769 2.781 551.528 0.878 12.370 2.287 0.46 208815. 0.1178
|
|
75.81 0.7022 0.6782 0.0138 0.0143 0.616 6.468 2.066 459.151 0.731 9.189 2.041 0.46 209449. 0.0906
|
|
78.72 0.7292 0.5858 0.0091 0.0113 0.487 5.118 1.360 363.326 0.578 6.047 1.697 0.46 210103. 0.0611
|
|
81.64 0.7562 0.4091 0.0045 0.0083 0.355 3.731 0.667 264.861 0.422 2.969 1.143 0.47 210776. 0.0288
|
|
84.56 0.7833 -0.0069 0.0000 0.0051 0.220 2.316 -0.007 164.417 0.262 -0.030 -0.019 0.47 211461. 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 0.0984 0.0340 2.324 20.924 20.015 1732.917 2.364 89.027 5.239 0.53 232836. 0.7238
|
|
3.40 0.0270 0.0757 0.0973 0.0347 2.373 21.366 19.798 1769.533 2.414 88.060 5.075 0.53 233005. 0.6973
|
|
6.80 0.0540 0.1465 0.0961 0.0354 2.422 21.804 19.555 1805.777 2.463 86.983 4.912 0.53 233192. 0.6708
|
|
10.21 0.0810 0.2126 0.0948 0.0361 2.469 22.229 19.286 1840.998 2.511 85.786 4.752 0.53 233397. 0.6444
|
|
13.61 0.1081 0.2741 0.0933 0.0368 2.514 22.634 18.988 1874.512 2.557 84.458 4.594 0.53 233620. 0.6183
|
|
17.01 0.1351 0.3312 0.0917 0.0374 2.555 23.009 18.657 1905.560 2.600 82.988 4.441 0.53 233864. 0.5924
|
|
20.41 0.1621 0.3841 0.0899 0.0379 2.593 23.344 18.292 1933.314 2.637 81.364 4.291 0.53 234129. 0.5668
|
|
23.82 0.1891 0.4329 0.0879 0.0384 2.624 23.629 17.890 1956.894 2.670 79.576 4.147 0.53 234416. 0.5416
|
|
27.22 0.2161 0.4781 0.0857 0.0388 2.649 23.852 17.449 1975.376 2.695 77.612 4.006 0.53 234725. 0.5168
|
|
30.62 0.2431 0.5197 0.0834 0.0390 2.666 24.002 16.966 1987.813 2.712 75.465 3.871 0.53 235056. 0.4924
|
|
34.02 0.2701 0.5580 0.0808 0.0391 2.673 24.068 16.440 1993.247 2.719 73.124 3.741 0.53 235411. 0.4684
|
|
37.43 0.2972 0.5932 0.0780 0.0391 2.670 24.038 15.869 1990.744 2.716 70.584 3.616 0.53 235790. 0.4448
|
|
40.83 0.3242 0.6255 0.0749 0.0388 2.654 23.901 15.252 1979.424 2.700 67.839 3.495 0.53 236192. 0.4215
|
|
44.23 0.3512 0.6551 0.0717 0.0384 2.626 23.648 14.588 1958.485 2.672 64.888 3.378 0.53 236619. 0.3985
|
|
47.63 0.3782 0.6820 0.0682 0.0378 2.584 23.271 13.878 1927.232 2.629 61.730 3.266 0.53 237069. 0.3758
|
|
51.03 0.4052 0.7064 0.0645 0.0370 2.528 22.761 13.122 1885.039 2.572 58.366 3.157 0.53 237544. 0.3532
|
|
54.44 0.4322 0.7282 0.0605 0.0359 2.456 22.112 12.319 1831.255 2.498 54.797 3.051 0.53 238044. 0.3307
|
|
57.84 0.4592 0.7474 0.0564 0.0346 2.368 21.319 11.474 1765.612 2.409 51.035 2.947 0.53 238567. 0.3083
|
|
61.24 0.4862 0.7638 0.0520 0.0331 2.264 20.388 10.591 1688.483 2.303 47.108 2.845 0.53 239115. 0.2859
|
|
64.64 0.5133 0.7772 0.0476 0.0314 2.146 19.324 9.677 1600.372 2.183 43.043 2.743 0.53 239687. 0.2635
|
|
68.05 0.5403 0.7872 0.0429 0.0295 2.014 18.133 8.737 1501.757 2.049 38.864 2.639 0.54 240282. 0.2409
|
|
71.45 0.5673 0.7931 0.0382 0.0273 1.868 16.821 7.777 1393.098 1.900 34.593 2.532 0.54 240902. 0.2181
|
|
74.85 0.5943 0.7940 0.0334 0.0250 1.710 15.394 6.801 1274.879 1.739 30.252 2.420 0.54 241546. 0.1949
|
|
78.25 0.6213 0.7883 0.0286 0.0225 1.539 13.857 5.814 1147.635 1.566 25.861 2.298 0.54 242214. 0.1711
|
|
81.66 0.6483 0.7735 0.0237 0.0199 1.357 12.219 4.821 1011.997 1.381 21.444 2.161 0.54 242905. 0.1465
|
|
85.06 0.6753 0.7452 0.0188 0.0170 1.165 10.489 3.828 868.719 1.185 17.025 1.998 0.54 243621. 0.1207
|
|
88.46 0.7024 0.6949 0.0140 0.0141 0.964 8.678 2.839 718.723 0.980 12.630 1.792 0.54 244360. 0.0932
|
|
91.86 0.7294 0.6045 0.0092 0.0110 0.755 6.800 1.864 563.128 0.768 8.289 1.501 0.54 245124. 0.0633
|
|
95.26 0.7564 0.4262 0.0045 0.0079 0.541 4.869 0.907 403.264 0.550 4.036 1.021 0.54 245910. 0.0300
|
|
98.67 0.7834 -0.0199 -0.0001 0.0047 0.322 2.900 -0.024 240.132 0.328 -0.108 -0.046 0.54 246707. 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 0.0993 0.0343 3.499 27.567 26.395 2609.232 3.115 117.406 4.588 0.60 266078. 0.7280
|
|
3.88 0.0270 0.0757 0.0983 0.0350 3.574 28.160 26.120 2665.332 3.182 116.181 4.445 0.60 266271. 0.7016
|
|
7.76 0.0539 0.1465 0.0971 0.0358 3.649 28.747 25.812 2720.932 3.248 114.812 4.303 0.60 266484. 0.6751
|
|
11.65 0.0809 0.2126 0.0958 0.0365 3.721 29.319 25.468 2775.041 3.312 113.284 4.163 0.60 266718. 0.6488
|
|
15.53 0.1079 0.2741 0.0944 0.0372 3.791 29.864 25.086 2826.605 3.374 111.582 4.025 0.60 266974. 0.6226
|
|
19.41 0.1349 0.3312 0.0928 0.0378 3.855 30.369 24.661 2874.454 3.431 109.692 3.891 0.60 267253. 0.5968
|
|
23.29 0.1618 0.3841 0.0910 0.0383 3.912 30.822 24.190 2917.324 3.482 107.596 3.761 0.60 267555. 0.5712
|
|
27.18 0.1888 0.4330 0.0890 0.0388 3.961 31.208 23.669 2953.859 3.526 105.281 3.634 0.60 267883. 0.5461
|
|
31.06 0.2158 0.4782 0.0869 0.0392 4.000 31.513 23.096 2982.648 3.560 102.732 3.512 0.60 268236. 0.5213
|
|
34.94 0.2428 0.5200 0.0845 0.0395 4.026 31.719 22.468 3002.233 3.584 99.936 3.394 0.60 268615. 0.4969
|
|
38.82 0.2697 0.5584 0.0819 0.0396 4.038 31.814 21.781 3011.149 3.594 96.883 3.281 0.61 269021. 0.4729
|
|
42.71 0.2967 0.5938 0.0791 0.0395 4.034 31.780 21.034 3007.971 3.590 93.561 3.172 0.61 269453. 0.4492
|
|
46.59 0.3237 0.6264 0.0761 0.0393 4.011 31.604 20.226 2991.343 3.571 89.965 3.067 0.61 269913. 0.4259
|
|
50.47 0.3506 0.6562 0.0728 0.0389 3.969 31.274 19.355 2960.042 3.533 86.091 2.966 0.61 270400. 0.4029
|
|
54.35 0.3776 0.6835 0.0693 0.0383 3.906 30.777 18.422 2912.999 3.477 81.939 2.868 0.61 270915. 0.3802
|
|
58.24 0.4046 0.7082 0.0656 0.0375 3.821 30.103 17.426 2849.270 3.401 77.512 2.774 0.61 271458. 0.3576
|
|
62.12 0.4316 0.7305 0.0616 0.0364 3.712 29.243 16.369 2767.880 3.304 72.809 2.682 0.61 272028. 0.3351
|
|
66.00 0.4585 0.7502 0.0574 0.0351 3.578 28.192 15.253 2668.352 3.185 67.845 2.593 0.61 272626. 0.3127
|
|
69.88 0.4855 0.7672 0.0530 0.0335 3.421 26.954 14.086 2551.219 3.045 62.656 2.504 0.61 273251. 0.2903
|
|
73.77 0.5125 0.7814 0.0484 0.0318 3.242 25.539 12.878 2417.251 2.885 57.280 2.416 0.61 273904. 0.2678
|
|
77.65 0.5394 0.7923 0.0438 0.0298 3.040 23.953 11.634 2267.182 2.706 51.749 2.328 0.61 274584. 0.2452
|
|
81.53 0.5664 0.7993 0.0390 0.0276 2.818 22.205 10.362 2101.718 2.509 46.091 2.236 0.61 275291. 0.2223
|
|
85.41 0.5934 0.8015 0.0341 0.0253 2.577 20.302 9.068 1921.595 2.294 40.336 2.140 0.61 276025. 0.1991
|
|
89.29 0.6204 0.7974 0.0292 0.0227 2.317 18.253 7.759 1727.633 2.062 34.512 2.037 0.61 276787. 0.1752
|
|
93.18 0.6473 0.7847 0.0242 0.0200 2.039 16.068 6.441 1520.790 1.815 28.649 1.921 0.62 277575. 0.1506
|
|
97.06 0.6743 0.7590 0.0193 0.0171 1.746 13.758 5.121 1302.217 1.554 22.780 1.784 0.62 278391. 0.1247
|
|
100.94 0.7013 0.7122 0.0143 0.0141 1.439 11.340 3.808 1073.318 1.281 16.940 1.609 0.62 279234. 0.0970
|
|
104.82 0.7283 0.6262 0.0094 0.0110 1.121 8.831 2.511 835.803 0.998 11.169 1.363 0.62 280104. 0.0667
|
|
108.71 0.7552 0.4527 0.0047 0.0078 0.794 6.252 1.239 591.717 0.706 5.513 0.950 0.62 281001. 0.0327
|
|
112.59 0.7822 0.0002 0.0000 0.0045 0.460 3.621 0.000 342.723 0.409 0.001 0.000 0.62 281911. 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 0.1004 0.0348 5.051 35.374 33.783 3766.674 3.997 150.266 4.068 0.68 299309. 0.7302
|
|
4.36 0.0270 0.0754 0.0994 0.0355 5.161 36.141 33.448 3848.293 4.083 148.779 3.942 0.68 299527. 0.7041
|
|
8.73 0.0539 0.1461 0.0983 0.0363 5.270 36.903 33.073 3929.500 4.169 147.107 3.817 0.68 299766. 0.6780
|
|
13.09 0.0809 0.2121 0.0971 0.0370 5.376 37.648 32.651 4008.811 4.253 145.232 3.694 0.68 300030. 0.6519
|
|
17.46 0.1078 0.2735 0.0957 0.0377 5.478 38.361 32.179 4084.656 4.334 143.133 3.573 0.68 300318. 0.6260
|
|
21.82 0.1348 0.3306 0.0941 0.0384 5.572 39.024 31.652 4155.302 4.409 140.788 3.455 0.68 300632. 0.6003
|
|
26.19 0.1617 0.3834 0.0923 0.0389 5.658 39.620 31.065 4218.814 4.476 138.177 3.340 0.68 300973. 0.5749
|
|
30.55 0.1887 0.4324 0.0904 0.0395 5.730 40.131 30.414 4273.153 4.534 135.280 3.228 0.68 301342. 0.5498
|
|
34.92 0.2156 0.4777 0.0883 0.0398 5.788 40.535 29.694 4316.179 4.580 132.078 3.120 0.68 301740. 0.5251
|
|
39.28 0.2426 0.5195 0.0859 0.0401 5.828 40.812 28.901 4345.736 4.611 128.552 3.016 0.68 302167. 0.5008
|
|
43.65 0.2695 0.5581 0.0833 0.0402 5.846 40.943 28.032 4359.660 4.626 124.688 2.916 0.68 302625. 0.4769
|
|
48.01 0.2965 0.5936 0.0805 0.0402 5.841 40.907 27.085 4355.851 4.622 120.473 2.820 0.68 303112. 0.4533
|
|
52.38 0.3234 0.6264 0.0775 0.0400 5.810 40.686 26.056 4332.315 4.597 115.899 2.728 0.68 303631. 0.4300
|
|
56.74 0.3504 0.6565 0.0742 0.0396 5.749 40.263 24.946 4287.251 4.549 110.959 2.639 0.68 304180. 0.4071
|
|
61.11 0.3774 0.6841 0.0706 0.0390 5.658 39.623 23.753 4219.092 4.477 105.654 2.554 0.68 304760. 0.3843
|
|
65.47 0.4043 0.7092 0.0668 0.0381 5.534 38.753 22.479 4126.466 4.378 99.986 2.471 0.68 305371. 0.3618
|
|
69.84 0.4313 0.7319 0.0628 0.0370 5.375 37.640 21.124 4007.976 4.253 93.958 2.390 0.68 306014. 0.3393
|
|
74.20 0.4582 0.7521 0.0585 0.0357 5.180 36.278 19.691 3862.863 4.099 87.584 2.312 0.69 306687. 0.3168
|
|
78.57 0.4852 0.7698 0.0541 0.0341 4.951 34.672 18.191 3691.858 3.917 80.914 2.235 0.69 307391. 0.2944
|
|
82.93 0.5121 0.7846 0.0495 0.0323 4.688 32.833 16.635 3496.099 3.709 73.993 2.158 0.69 308126. 0.2718
|
|
87.29 0.5391 0.7963 0.0447 0.0303 4.394 30.772 15.033 3276.669 3.477 66.865 2.081 0.69 308891. 0.2492
|
|
91.66 0.5660 0.8043 0.0398 0.0280 4.069 28.499 13.392 3034.617 3.220 59.569 2.002 0.69 309687. 0.2262
|
|
96.02 0.5930 0.8077 0.0348 0.0256 3.716 26.024 11.722 2771.025 2.940 52.140 1.919 0.69 310513. 0.2029
|
|
100.39 0.6199 0.8051 0.0298 0.0230 3.335 23.357 10.031 2487.103 2.639 44.617 1.829 0.69 311369. 0.1789
|
|
104.75 0.6469 0.7941 0.0248 0.0202 2.929 20.513 8.327 2184.252 2.318 37.039 1.729 0.69 312256. 0.1541
|
|
109.12 0.6739 0.7706 0.0197 0.0172 2.500 17.507 6.620 1864.193 1.978 29.447 1.611 0.69 313174. 0.1280
|
|
113.48 0.7008 0.7263 0.0146 0.0141 2.051 14.360 4.921 1529.059 1.622 21.890 1.460 0.69 314121. 0.1000
|
|
117.85 0.7278 0.6430 0.0096 0.0109 1.584 11.096 3.242 1181.496 1.254 14.419 1.245 0.70 315099. 0.0692
|
|
122.21 0.7547 0.4699 0.0047 0.0076 1.106 7.745 1.595 824.712 0.875 7.093 0.877 0.70 316107. 0.0342
|
|
126.58 0.7817 -0.0059 0.0000 0.0043 0.619 4.333 -0.011 461.354 0.490 -0.048 -0.011 0.70 317128. 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 0.1017 0.0361 7.198 45.370 42.237 5367.825 5.126 187.871 3.569 0.75 332529. 0.7163
|
|
4.84 0.0269 0.0736 0.1008 0.0368 7.339 46.257 41.849 5472.800 5.226 186.146 3.468 0.75 332770. 0.6929
|
|
9.69 0.0538 0.1430 0.0997 0.0375 7.479 47.140 41.410 5577.199 5.326 184.193 3.368 0.75 333035. 0.6693
|
|
14.53 0.0807 0.2081 0.0985 0.0382 7.616 48.001 40.914 5679.112 5.423 181.987 3.268 0.75 333328. 0.6455
|
|
19.37 0.1077 0.2691 0.0972 0.0389 7.746 48.824 40.355 5776.510 5.516 179.498 3.169 0.75 333648. 0.6216
|
|
24.21 0.1346 0.3260 0.0957 0.0395 7.868 49.590 39.726 5867.120 5.603 176.699 3.071 0.75 333997. 0.5978
|
|
29.06 0.1615 0.3790 0.0940 0.0400 7.977 50.278 39.020 5948.456 5.680 173.561 2.975 0.75 334376. 0.5740
|
|
33.90 0.1884 0.4282 0.0921 0.0405 8.070 50.864 38.232 6017.849 5.747 170.056 2.882 0.76 334787. 0.5502
|
|
38.74 0.2153 0.4739 0.0899 0.0409 8.143 51.326 37.356 6072.458 5.799 166.159 2.790 0.76 335229. 0.5267
|
|
43.59 0.2422 0.5162 0.0876 0.0411 8.193 51.637 36.386 6109.320 5.834 161.846 2.701 0.76 335705. 0.5032
|
|
48.43 0.2692 0.5552 0.0850 0.0412 8.214 51.773 35.319 6125.387 5.849 157.097 2.615 0.76 336213. 0.4800
|
|
53.27 0.2961 0.5913 0.0822 0.0412 8.204 51.708 34.149 6117.625 5.842 151.895 2.532 0.76 336756. 0.4569
|
|
58.11 0.3230 0.6245 0.0792 0.0409 8.158 51.416 32.875 6083.065 5.809 146.227 2.451 0.76 337333. 0.4340
|
|
62.96 0.3499 0.6550 0.0758 0.0405 8.072 50.874 31.495 6018.956 5.748 140.088 2.373 0.76 337944. 0.4113
|
|
67.80 0.3768 0.6830 0.0723 0.0399 7.943 50.061 30.008 5922.826 5.656 133.476 2.298 0.76 338589. 0.3888
|
|
72.64 0.4037 0.7086 0.0684 0.0390 7.768 48.960 28.416 5792.491 5.531 126.396 2.225 0.76 339269. 0.3663
|
|
77.48 0.4307 0.7318 0.0643 0.0379 7.544 47.550 26.720 5625.770 5.372 118.850 2.154 0.76 339983. 0.3439
|
|
82.33 0.4576 0.7526 0.0600 0.0365 7.270 45.822 24.923 5421.283 5.177 110.855 2.085 0.76 340731. 0.3215
|
|
87.17 0.4845 0.7709 0.0555 0.0349 6.946 43.782 23.038 5179.938 4.946 102.472 2.017 0.76 341514. 0.2990
|
|
92.01 0.5114 0.7865 0.0508 0.0330 6.576 41.445 21.079 4903.395 4.682 93.760 1.950 0.76 342330. 0.2765
|
|
96.86 0.5383 0.7991 0.0459 0.0309 6.160 38.824 19.059 4593.333 4.386 84.774 1.882 0.76 343180. 0.2537
|
|
101.70 0.5652 0.8081 0.0409 0.0286 5.701 35.934 16.988 4251.416 4.060 75.563 1.812 0.77 344063. 0.2307
|
|
106.54 0.5921 0.8124 0.0358 0.0261 5.202 32.790 14.878 3879.452 3.705 66.176 1.739 0.77 344980. 0.2072
|
|
111.38 0.6191 0.8108 0.0307 0.0234 4.666 29.410 12.738 3479.494 3.323 56.658 1.660 0.77 345931. 0.1830
|
|
116.23 0.6460 0.8006 0.0255 0.0206 4.096 25.814 10.580 3054.048 2.916 47.059 1.571 0.77 346915. 0.1578
|
|
121.07 0.6729 0.7774 0.0203 0.0175 3.495 22.028 8.416 2606.202 2.489 37.434 1.465 0.77 347932. 0.1312
|
|
125.91 0.6998 0.7323 0.0151 0.0144 2.869 18.086 6.259 2139.781 2.043 27.839 1.327 0.77 348983. 0.1025
|
|
130.76 0.7267 0.6461 0.0099 0.0112 2.225 14.026 4.124 1659.463 1.585 18.344 1.127 0.77 350068. 0.0707
|
|
135.60 0.7536 0.4670 0.0049 0.0079 1.570 9.896 2.028 1170.807 1.118 9.019 0.786 0.78 351185. 0.0345
|
|
140.44 0.7806 -0.0073 0.0000 0.0046 0.910 5.734 -0.018 678.427 0.648 -0.079 -0.012 0.78 352317. 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 0.1031 0.0402 10.659 61.074 51.794 7948.369 6.900 230.378 2.956 0.83 365732. 0.6569
|
|
5.32 0.0269 0.0674 0.1022 0.0408 10.815 61.966 51.366 8064.481 7.001 228.475 2.889 0.83 365996. 0.6394
|
|
10.64 0.0538 0.1317 0.1012 0.0413 10.966 62.834 50.877 8177.384 7.099 226.300 2.822 0.83 366288. 0.6216
|
|
15.96 0.0807 0.1928 0.1001 0.0419 11.110 63.656 50.319 8284.435 7.192 223.819 2.755 0.83 366609. 0.6035
|
|
21.28 0.1075 0.2508 0.0989 0.0424 11.242 64.414 49.684 8383.014 7.277 220.993 2.688 0.83 366960. 0.5852
|
|
26.60 0.1344 0.3058 0.0974 0.0428 11.359 65.084 48.962 8470.185 7.353 217.782 2.622 0.83 367344. 0.5666
|
|
31.93 0.1613 0.3578 0.0958 0.0432 11.456 65.642 48.145 8542.877 7.416 214.149 2.556 0.83 367762. 0.5477
|
|
37.25 0.1882 0.4068 0.0940 0.0435 11.530 66.065 47.225 8597.918 7.464 210.056 2.491 0.83 368214. 0.5287
|
|
42.57 0.2151 0.4530 0.0919 0.0436 11.576 66.327 46.193 8632.031 7.494 205.466 2.427 0.83 368702. 0.5095
|
|
47.89 0.2420 0.4963 0.0896 0.0437 11.589 66.403 45.042 8641.920 7.502 200.347 2.364 0.83 369226. 0.4900
|
|
53.21 0.2688 0.5369 0.0871 0.0436 11.565 66.268 43.766 8624.261 7.487 194.671 2.302 0.83 369787. 0.4703
|
|
58.53 0.2957 0.5749 0.0843 0.0434 11.500 65.895 42.360 8575.710 7.445 188.415 2.240 0.83 370385. 0.4503
|
|
63.85 0.3226 0.6102 0.0812 0.0429 11.389 65.259 40.819 8493.008 7.373 181.562 2.180 0.83 371021. 0.4301
|
|
69.17 0.3495 0.6430 0.0779 0.0423 11.229 64.338 39.142 8373.124 7.269 174.102 2.120 0.83 371695. 0.4097
|
|
74.49 0.3764 0.6732 0.0743 0.0415 11.014 63.109 37.328 8213.188 7.130 166.035 2.061 0.83 372407. 0.3889
|
|
79.81 0.4033 0.7009 0.0704 0.0405 10.742 61.552 35.379 8010.567 6.954 157.365 2.003 0.84 373156. 0.3680
|
|
85.14 0.4302 0.7261 0.0663 0.0393 10.410 59.645 33.295 7762.437 6.739 148.097 1.945 0.84 373943. 0.3467
|
|
90.46 0.4570 0.7487 0.0619 0.0378 10.013 57.372 31.081 7466.513 6.482 138.250 1.888 0.84 374768. 0.3251
|
|
95.78 0.4839 0.7686 0.0572 0.0360 9.554 54.742 28.753 7124.309 6.185 127.894 1.831 0.84 375629. 0.3031
|
|
101.10 0.5108 0.7852 0.0524 0.0341 9.039 51.794 26.328 6740.652 5.852 117.105 1.772 0.84 376528. 0.2807
|
|
106.42 0.5377 0.7979 0.0474 0.0319 8.471 48.538 23.820 6316.901 5.484 105.953 1.710 0.84 377464. 0.2578
|
|
111.74 0.5646 0.8062 0.0423 0.0296 7.852 44.992 21.246 5855.338 5.083 94.501 1.646 0.84 378436. 0.2343
|
|
117.06 0.5915 0.8089 0.0370 0.0271 7.184 41.164 18.618 5357.187 4.651 82.812 1.576 0.84 379445. 0.2100
|
|
122.38 0.6184 0.8042 0.0317 0.0244 6.472 37.086 15.950 4826.474 4.190 70.944 1.499 0.84 380490. 0.1849
|
|
127.70 0.6452 0.7885 0.0264 0.0216 5.724 32.799 13.255 4268.584 3.706 58.959 1.408 0.85 381572. 0.1584
|
|
133.02 0.6721 0.7563 0.0210 0.0187 4.947 28.348 10.549 3689.345 3.203 46.924 1.297 0.85 382690. 0.1301
|
|
138.34 0.6990 0.6974 0.0156 0.0157 4.152 23.788 7.849 3095.810 2.688 34.912 1.150 0.85 383844. 0.0995
|
|
143.67 0.7259 0.5920 0.0103 0.0126 3.347 19.179 5.173 2496.051 2.167 23.008 0.940 0.85 385035. 0.0660
|
|
148.99 0.7528 0.3966 0.0051 0.0096 2.546 14.591 2.542 1898.899 1.648 11.306 0.607 0.85 386262. 0.0299
|
|
154.31 0.7797 -0.0061 -0.0001 0.0066 1.758 10.073 -0.026 1310.889 1.138 -0.116 -0.009 0.85 387509. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 12000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1035 0.0475 16.342 85.834 61.926 12186.192 9.697 275.447 2.305 0.90 398959. 0.5601
|
|
5.88 0.0272 0.0583 0.1028 0.0480 16.539 86.870 61.497 12333.323 9.815 273.540 2.262 0.90 399246. 0.5477
|
|
11.76 0.0545 0.1144 0.1020 0.0486 16.723 87.835 60.998 12470.328 9.924 271.320 2.219 0.90 399564. 0.5351
|
|
17.65 0.0817 0.1684 0.1010 0.0490 16.887 88.694 60.417 12592.269 10.021 268.737 2.176 0.90 399916. 0.5224
|
|
23.53 0.1090 0.2202 0.0999 0.0494 17.023 89.411 59.743 12694.061 10.102 265.736 2.135 0.90 400302. 0.5095
|
|
29.41 0.1362 0.2700 0.0986 0.0497 17.126 89.950 58.962 12770.544 10.162 262.261 2.094 0.91 400726. 0.4966
|
|
35.29 0.1635 0.3179 0.0971 0.0499 17.187 90.275 58.061 12816.694 10.199 258.255 2.055 0.91 401188. 0.4835
|
|
41.18 0.1907 0.3640 0.0954 0.0500 17.202 90.353 57.028 12827.811 10.208 253.662 2.016 0.91 401689. 0.4703
|
|
47.06 0.2180 0.4083 0.0934 0.0499 17.165 90.155 55.852 12799.729 10.186 248.429 1.979 0.91 402231. 0.4568
|
|
52.94 0.2452 0.4509 0.0912 0.0496 17.069 89.654 54.521 12728.617 10.129 242.507 1.943 0.91 402815. 0.4430
|
|
58.82 0.2724 0.4918 0.0887 0.0491 16.911 88.824 53.024 12610.765 10.035 235.851 1.907 0.91 403441. 0.4289
|
|
64.70 0.2997 0.5310 0.0859 0.0485 16.688 87.654 51.356 12444.550 9.903 228.432 1.872 0.91 404110. 0.4143
|
|
70.59 0.3269 0.5683 0.0828 0.0476 16.398 86.126 49.511 12227.689 9.730 220.227 1.837 0.91 404822. 0.3991
|
|
76.47 0.3542 0.6038 0.0794 0.0466 16.036 84.228 47.487 11958.174 9.516 211.221 1.801 0.91 405576. 0.3833
|
|
82.35 0.3814 0.6373 0.0757 0.0453 15.602 81.947 45.282 11634.287 9.258 201.412 1.765 0.91 406373. 0.3669
|
|
88.23 0.4087 0.6687 0.0717 0.0438 15.092 79.271 42.897 11254.446 8.956 190.807 1.729 0.91 407213. 0.3497
|
|
94.12 0.4359 0.6979 0.0674 0.0421 14.505 76.188 40.335 10816.701 8.608 179.411 1.691 0.91 408095. 0.3317
|
|
100.00 0.4631 0.7245 0.0629 0.0402 13.840 72.691 37.604 10320.174 8.213 167.263 1.653 0.91 409019. 0.3130
|
|
105.88 0.4904 0.7485 0.0581 0.0380 13.098 68.797 34.726 9767.452 7.773 154.461 1.613 0.92 409985. 0.2935
|
|
111.76 0.5176 0.7685 0.0530 0.0357 12.302 64.615 31.722 9173.721 7.300 141.101 1.568 0.92 410992. 0.2728
|
|
117.64 0.5449 0.7822 0.0478 0.0333 11.475 60.272 28.611 8557.086 6.810 127.264 1.517 0.92 412040. 0.2505
|
|
123.53 0.5721 0.7871 0.0425 0.0309 10.634 55.851 25.410 7929.462 6.310 113.026 1.453 0.92 413129. 0.2263
|
|
129.41 0.5994 0.7798 0.0370 0.0284 9.795 51.449 22.135 7304.482 5.813 98.457 1.374 0.92 414258. 0.1997
|
|
135.29 0.6266 0.7606 0.0315 0.0259 8.923 46.866 18.812 6653.786 5.295 83.678 1.282 0.92 415428. 0.1718
|
|
141.17 0.6539 0.7249 0.0259 0.0233 8.030 42.175 15.463 5987.746 4.765 68.778 1.171 0.92 416638. 0.1422
|
|
147.06 0.6811 0.6658 0.0202 0.0207 7.131 37.455 12.108 5317.666 4.232 53.856 1.033 0.93 417888. 0.1110
|
|
152.94 0.7083 0.5734 0.0147 0.0181 6.241 32.780 8.775 4653.861 3.703 39.030 0.855 0.93 419179. 0.0782
|
|
158.82 0.7356 0.4329 0.0092 0.0156 5.374 28.226 5.493 4007.380 3.189 24.432 0.622 0.93 420511. 0.0450
|
|
164.70 0.7628 0.2218 0.0038 0.0132 4.544 23.866 2.295 3388.295 2.696 10.208 0.307 0.93 421882. 0.0144
|
|
170.59 0.7901
|
|
|
|
|
|
|