353 lines
63 KiB
Plaintext
353 lines
63 KiB
Plaintext
27x13E (27x13E.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 0.0805 0.0271 0.031 1.975 1.364 23.372 0.223 6.066 26.464 0.11 66888. 0.6716
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0.55 0.0216 0.0624 0.0791 0.0274 0.032 1.995 1.340 23.608 0.225 5.960 25.743 0.11 66926. 0.6476
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1.11 0.0433 0.1214 0.0776 0.0277 0.032 2.013 1.314 23.821 0.227 5.846 25.028 0.11 66967. 0.6236
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1.66 0.0649 0.1770 0.0760 0.0279 0.032 2.029 1.287 24.006 0.229 5.725 24.321 0.11 67011. 0.5997
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2.21 0.0866 0.2292 0.0743 0.0281 0.032 2.042 1.258 24.158 0.231 5.596 23.623 0.11 67058. 0.5758
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2.77 0.1082 0.2782 0.0725 0.0282 0.033 2.052 1.227 24.273 0.232 5.459 22.935 0.11 67108. 0.5522
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3.32 0.1298 0.3239 0.0705 0.0283 0.033 2.058 1.195 24.344 0.232 5.313 22.256 0.11 67162. 0.5286
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3.87 0.1515 0.3666 0.0685 0.0283 0.033 2.060 1.160 24.366 0.233 5.159 21.588 0.11 67219. 0.5052
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4.43 0.1731 0.4062 0.0663 0.0283 0.033 2.057 1.123 24.335 0.232 4.995 20.930 0.11 67280. 0.4820
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4.98 0.1948 0.4428 0.0640 0.0282 0.033 2.049 1.084 24.243 0.232 4.822 20.282 0.11 67344. 0.4589
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5.53 0.2164 0.4765 0.0616 0.0280 0.032 2.036 1.043 24.086 0.230 4.639 19.642 0.11 67413. 0.4359
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6.09 0.2381 0.5072 0.0590 0.0277 0.032 2.016 1.000 23.857 0.228 4.447 19.009 0.11 67485. 0.4131
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6.64 0.2597 0.5351 0.0564 0.0274 0.032 1.991 0.954 23.551 0.225 4.245 18.381 0.11 67561. 0.3903
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7.19 0.2813 0.5600 0.0536 0.0269 0.031 1.958 0.907 23.167 0.221 4.034 17.757 0.11 67642. 0.3675
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7.75 0.3030 0.5819 0.0506 0.0264 0.030 1.919 0.858 22.703 0.217 3.815 17.134 0.11 67726. 0.3448
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8.30 0.3246 0.6007 0.0476 0.0257 0.030 1.873 0.807 22.159 0.212 3.587 16.508 0.11 67815. 0.3222
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8.85 0.3463 0.6162 0.0445 0.0250 0.029 1.820 0.754 21.536 0.206 3.353 15.876 0.11 67907. 0.2995
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9.41 0.3679 0.6281 0.0413 0.0242 0.028 1.761 0.700 20.833 0.199 3.112 15.232 0.11 68004. 0.2769
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9.96 0.3895 0.6362 0.0380 0.0233 0.027 1.695 0.644 20.050 0.191 2.865 14.570 0.11 68105. 0.2541
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10.51 0.4112 0.6399 0.0347 0.0223 0.026 1.622 0.587 19.188 0.183 2.613 13.885 0.11 68211. 0.2313
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11.07 0.4328 0.6387 0.0313 0.0212 0.024 1.542 0.530 18.248 0.174 2.356 13.165 0.11 68320. 0.2082
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11.62 0.4545 0.6317 0.0278 0.0200 0.023 1.456 0.471 17.231 0.165 2.096 12.401 0.11 68435. 0.1850
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12.17 0.4761 0.6178 0.0243 0.0187 0.022 1.364 0.412 16.140 0.154 1.832 11.576 0.11 68553. 0.1615
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12.73 0.4977 0.5952 0.0208 0.0174 0.020 1.266 0.352 14.976 0.143 1.567 10.668 0.11 68676. 0.1376
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13.28 0.5194 0.5617 0.0173 0.0160 0.018 1.162 0.292 13.743 0.131 1.300 9.648 0.11 68803. 0.1134
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13.83 0.5410 0.5137 0.0137 0.0145 0.017 1.052 0.232 12.445 0.119 1.034 8.470 0.11 68935. 0.0887
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14.39 0.5627 0.4457 0.0102 0.0129 0.015 0.937 0.173 11.088 0.106 0.768 7.066 0.11 69071. 0.0638
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14.94 0.5843 0.3488 0.0067 0.0112 0.013 0.818 0.114 9.679 0.092 0.506 5.326 0.11 69212. 0.0390
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15.49 0.6060 0.2076 0.0033 0.0096 0.011 0.695 0.055 8.224 0.079 0.247 3.057 0.11 69357. 0.0156
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16.05 0.6276 -0.0087 -0.0001 0.0078 0.009 0.569 -0.002 6.727 0.064 -0.008 -0.124 0.11 69503. 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 0.0810 0.0256 0.236 7.442 5.486 176.084 0.841 24.401 14.131 0.21 133773. 0.7193
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1.11 0.0217 0.0667 0.0796 0.0259 0.239 7.527 5.390 178.116 0.850 23.977 13.727 0.21 133849. 0.6926
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2.22 0.0434 0.1296 0.0781 0.0261 0.241 7.606 5.288 179.966 0.859 23.522 13.328 0.21 133931. 0.6661
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3.33 0.0651 0.1887 0.0765 0.0264 0.244 7.674 5.179 181.591 0.867 23.037 12.936 0.21 134019. 0.6398
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4.44 0.0867 0.2441 0.0747 0.0266 0.245 7.732 5.063 182.951 0.874 22.519 12.552 0.21 134113. 0.6137
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5.54 0.1084 0.2959 0.0729 0.0267 0.247 7.776 4.939 184.001 0.879 21.968 12.174 0.21 134214. 0.5880
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6.65 0.1301 0.3444 0.0710 0.0268 0.248 7.806 4.807 184.697 0.882 21.381 11.805 0.21 134322. 0.5625
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7.76 0.1518 0.3894 0.0689 0.0269 0.248 7.818 4.667 184.992 0.883 20.760 11.443 0.21 134437. 0.5372
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8.87 0.1735 0.4313 0.0667 0.0268 0.248 7.812 4.519 184.842 0.883 20.101 11.089 0.21 134559. 0.5123
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9.98 0.1952 0.4700 0.0644 0.0267 0.247 7.784 4.363 184.198 0.879 19.405 10.743 0.21 134689. 0.4876
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11.09 0.2169 0.5058 0.0620 0.0266 0.245 7.734 4.198 183.011 0.874 18.671 10.403 0.21 134827. 0.4632
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12.20 0.2386 0.5385 0.0594 0.0263 0.243 7.659 4.024 181.227 0.865 17.897 10.070 0.21 134972. 0.4390
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13.31 0.2602 0.5684 0.0567 0.0260 0.240 7.557 3.841 178.806 0.854 17.084 9.743 0.21 135125. 0.4149
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14.42 0.2819 0.5954 0.0539 0.0255 0.236 7.426 3.650 175.727 0.839 16.234 9.420 0.22 135286. 0.3911
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15.53 0.3036 0.6195 0.0509 0.0250 0.231 7.268 3.451 171.981 0.821 15.350 9.101 0.22 135456. 0.3674
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16.63 0.3253 0.6406 0.0479 0.0243 0.225 7.081 3.245 167.565 0.800 14.434 8.784 0.22 135634. 0.3439
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17.74 0.3470 0.6586 0.0448 0.0236 0.218 6.866 3.033 162.474 0.776 13.489 8.466 0.22 135820. 0.3204
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18.85 0.3687 0.6733 0.0415 0.0227 0.210 6.623 2.814 156.707 0.748 12.519 8.146 0.22 136015. 0.2970
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19.96 0.3904 0.6844 0.0382 0.0218 0.202 6.350 2.591 150.263 0.717 11.525 7.821 0.22 136218. 0.2736
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21.07 0.4120 0.6916 0.0349 0.0208 0.192 6.050 2.363 143.147 0.683 10.510 7.487 0.22 136430. 0.2501
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22.18 0.4337 0.6942 0.0315 0.0197 0.182 5.721 2.131 135.363 0.646 9.477 7.139 0.22 136650. 0.2265
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23.29 0.4554 0.6914 0.0280 0.0184 0.170 5.364 1.895 126.923 0.606 8.430 6.772 0.22 136879. 0.2026
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24.40 0.4771 0.6822 0.0245 0.0171 0.158 4.980 1.657 117.842 0.563 7.371 6.378 0.22 137117. 0.1784
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25.51 0.4988 0.6647 0.0209 0.0157 0.145 4.570 1.417 108.141 0.516 6.304 5.944 0.22 137364. 0.1538
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26.62 0.5205 0.6364 0.0174 0.0142 0.131 4.135 1.177 97.849 0.467 5.234 5.454 0.22 137619. 0.1286
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27.72 0.5422 0.5931 0.0138 0.0126 0.117 3.677 0.936 87.004 0.415 4.164 4.880 0.22 137884. 0.1026
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28.83 0.5639 0.5280 0.0103 0.0110 0.101 3.197 0.697 75.652 0.361 3.099 4.177 0.22 138157. 0.0758
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29.94 0.5855 0.4288 0.0068 0.0093 0.086 2.699 0.460 63.853 0.305 2.046 3.267 0.22 138440. 0.0481
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31.05 0.6072 0.2709 0.0033 0.0075 0.069 2.184 0.227 51.673 0.247 1.008 1.990 0.22 138730. 0.0206
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32.16 0.6289 -0.0047 0.0000 0.0057 0.052 1.653 -0.003 39.108 0.187 -0.013 -0.033 0.22 139021. 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 0.0816 0.0251 0.781 16.412 12.443 582.517 1.854 55.348 9.689 0.32 200650. 0.7427
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1.67 0.0217 0.0687 0.0802 0.0254 0.791 16.612 12.228 589.631 1.877 54.391 9.406 0.32 200765. 0.7148
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3.33 0.0434 0.1333 0.0787 0.0256 0.799 16.795 11.997 596.120 1.898 53.364 9.128 0.32 200888. 0.6871
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5.00 0.0652 0.1940 0.0771 0.0259 0.807 16.956 11.751 601.839 1.916 52.267 8.856 0.32 201021. 0.6597
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6.66 0.0869 0.2509 0.0754 0.0261 0.814 17.092 11.487 606.641 1.931 51.095 8.589 0.32 201163. 0.6326
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8.33 0.1086 0.3041 0.0735 0.0263 0.819 17.197 11.207 610.375 1.943 49.847 8.328 0.32 201315. 0.6058
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10.00 0.1303 0.3538 0.0716 0.0264 0.822 17.267 10.908 612.885 1.951 48.519 8.073 0.32 201478. 0.5794
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11.66 0.1520 0.4000 0.0695 0.0264 0.823 17.299 10.591 614.012 1.954 47.110 7.824 0.32 201651. 0.5533
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13.33 0.1738 0.4430 0.0673 0.0264 0.823 17.288 10.255 613.596 1.953 45.616 7.581 0.32 201836. 0.5276
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14.99 0.1955 0.4827 0.0650 0.0263 0.820 17.228 9.900 611.472 1.946 44.037 7.344 0.32 202031. 0.5022
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16.66 0.2172 0.5195 0.0625 0.0261 0.815 17.115 9.526 607.468 1.934 42.371 7.112 0.32 202238. 0.4771
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18.33 0.2389 0.5533 0.0599 0.0259 0.806 16.944 9.131 601.399 1.914 40.614 6.886 0.32 202457. 0.4522
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19.99 0.2606 0.5842 0.0572 0.0255 0.795 16.711 8.716 593.116 1.888 38.767 6.665 0.32 202688. 0.4276
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21.66 0.2824 0.6122 0.0543 0.0251 0.781 16.413 8.281 582.547 1.854 36.836 6.448 0.32 202931. 0.4033
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23.32 0.3041 0.6375 0.0514 0.0245 0.764 16.050 7.830 569.659 1.813 34.827 6.234 0.32 203187. 0.3791
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24.99 0.3258 0.6598 0.0483 0.0238 0.744 15.621 7.362 554.430 1.765 32.745 6.023 0.32 203455. 0.3551
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26.66 0.3475 0.6792 0.0451 0.0231 0.720 15.125 6.879 536.847 1.709 30.598 5.812 0.32 203735. 0.3313
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28.32 0.3692 0.6954 0.0419 0.0222 0.693 14.563 6.383 516.901 1.645 28.391 5.601 0.32 204028. 0.3075
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29.99 0.3910 0.7083 0.0385 0.0213 0.663 13.935 5.875 494.592 1.574 26.131 5.387 0.32 204334. 0.2838
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31.65 0.4127 0.7174 0.0351 0.0202 0.630 13.240 5.356 469.926 1.496 23.823 5.169 0.32 204653. 0.2600
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33.32 0.4344 0.7222 0.0317 0.0191 0.594 12.479 4.828 442.926 1.410 21.475 4.944 0.32 204984. 0.2361
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34.99 0.4561 0.7220 0.0282 0.0178 0.555 11.654 4.293 413.626 1.317 19.094 4.707 0.32 205329. 0.2119
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36.65 0.4778 0.7156 0.0246 0.0164 0.512 10.765 3.751 382.080 1.216 16.686 4.453 0.32 205687. 0.1874
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38.32 0.4996 0.7013 0.0210 0.0150 0.467 9.815 3.206 348.364 1.109 14.262 4.175 0.33 206058. 0.1625
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39.98 0.5213 0.6764 0.0174 0.0134 0.419 8.807 2.659 312.579 0.995 11.829 3.859 0.33 206443. 0.1368
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41.65 0.5430 0.6367 0.0139 0.0118 0.369 7.744 2.113 274.859 0.875 9.398 3.487 0.33 206841. 0.1101
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43.32 0.5647 0.5743 0.0103 0.0101 0.316 6.631 1.569 235.372 0.749 6.981 3.024 0.33 207252. 0.0823
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44.98 0.5864 0.4748 0.0068 0.0084 0.261 5.475 1.032 194.326 0.619 4.589 2.408 0.33 207677. 0.0531
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46.65 0.6082 0.3067 0.0033 0.0065 0.204 4.281 0.502 151.957 0.484 2.235 1.500 0.33 208114. 0.0231
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48.31 0.6299 -0.0177 -0.0001 0.0047 0.145 3.046 -0.020 108.112 0.344 -0.089 -0.084 0.33 208545. 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 0.0826 0.0250 1.846 29.095 22.372 1376.905 3.287 99.512 7.370 0.43 267516. 0.7575
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2.22 0.0217 0.0696 0.0811 0.0253 1.870 29.460 21.989 1394.204 3.328 97.807 7.154 0.43 267669. 0.7290
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4.44 0.0434 0.1351 0.0796 0.0256 1.891 29.794 21.578 1409.991 3.366 95.978 6.941 0.43 267834. 0.7007
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6.66 0.0651 0.1965 0.0780 0.0258 1.909 30.088 21.137 1423.910 3.399 94.020 6.733 0.43 268012. 0.6727
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8.88 0.0868 0.2541 0.0763 0.0261 1.925 30.335 20.667 1435.608 3.427 91.928 6.530 0.43 268202. 0.6451
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11.10 0.1085 0.3080 0.0744 0.0262 1.937 30.528 20.166 1444.717 3.449 89.697 6.331 0.43 268406. 0.6178
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13.32 0.1302 0.3583 0.0724 0.0263 1.946 30.658 19.632 1450.861 3.464 87.322 6.137 0.43 268623. 0.5910
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15.54 0.1519 0.4051 0.0704 0.0264 1.949 30.717 19.065 1453.654 3.470 84.800 5.949 0.43 268855. 0.5645
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17.76 0.1736 0.4487 0.0681 0.0264 1.948 30.697 18.464 1452.707 3.468 82.126 5.765 0.43 269101. 0.5383
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19.97 0.1953 0.4891 0.0658 0.0263 1.941 30.589 17.828 1447.626 3.456 79.297 5.586 0.43 269363. 0.5125
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22.19 0.2170 0.5265 0.0633 0.0261 1.928 30.386 17.156 1437.997 3.433 76.310 5.411 0.43 269639. 0.4871
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24.41 0.2387 0.5610 0.0607 0.0258 1.909 30.077 16.448 1423.371 3.398 73.159 5.241 0.43 269932. 0.4619
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26.63 0.2604 0.5926 0.0579 0.0255 1.882 29.654 15.703 1403.379 3.350 69.846 5.075 0.43 270240. 0.4371
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28.85 0.2821 0.6214 0.0551 0.0250 1.848 29.114 14.923 1377.833 3.289 66.379 4.913 0.43 270565. 0.4124
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31.07 0.3038 0.6475 0.0521 0.0244 1.806 28.455 14.112 1346.648 3.215 62.770 4.753 0.43 270906. 0.3880
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33.29 0.3255 0.6707 0.0490 0.0238 1.756 27.676 13.271 1309.771 3.127 59.030 4.596 0.43 271263. 0.3638
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35.51 0.3472 0.6911 0.0458 0.0230 1.699 26.776 12.403 1267.166 3.025 55.170 4.440 0.43 271637. 0.3398
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37.73 0.3689 0.7086 0.0425 0.0221 1.634 25.754 11.511 1218.810 2.910 51.202 4.284 0.43 272028. 0.3159
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39.95 0.3906 0.7228 0.0391 0.0211 1.562 24.611 10.597 1164.700 2.781 47.136 4.127 0.43 272435. 0.2920
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42.17 0.4123 0.7334 0.0357 0.0200 1.482 23.346 9.664 1104.854 2.638 42.984 3.967 0.43 272860. 0.2680
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44.39 0.4340 0.7400 0.0322 0.0189 1.394 21.961 8.714 1039.320 2.481 38.759 3.803 0.43 273302. 0.2440
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46.61 0.4557 0.7418 0.0286 0.0176 1.298 20.458 7.750 968.184 2.311 34.472 3.631 0.43 273762. 0.2197
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48.83 0.4774 0.7379 0.0250 0.0162 1.196 18.839 6.776 891.572 2.128 30.139 3.447 0.43 274239. 0.1950
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51.05 0.4991 0.7264 0.0214 0.0147 1.086 17.109 5.794 809.671 1.933 25.773 3.246 0.43 274733. 0.1698
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53.27 0.5208 0.7048 0.0177 0.0131 0.969 15.272 4.809 722.726 1.725 21.392 3.018 0.43 275246. 0.1438
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55.48 0.5425 0.6687 0.0141 0.0115 0.846 13.335 3.825 631.061 1.507 17.014 2.749 0.43 275776. 0.1168
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57.70 0.5642 0.6103 0.0105 0.0097 0.718 11.307 2.846 535.087 1.277 12.658 2.412 0.44 276323. 0.0884
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59.92 0.5859 0.5138 0.0069 0.0079 0.584 9.198 1.877 435.313 1.039 8.349 1.956 0.44 276889. 0.0582
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62.14 0.6076 0.3435 0.0034 0.0060 0.446 7.022 0.924 332.322 0.793 4.109 1.261 0.44 277471. 0.0263
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64.36 0.6293 -0.0099 -0.0001 0.0041 0.303 4.770 -0.018 225.724 0.539 -0.078 -0.035 0.44 278044. 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 0.0838 0.0252 3.639 45.871 35.487 2713.564 5.183 157.845 5.932 0.54 334363. 0.7679
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2.78 0.0218 0.0703 0.0824 0.0255 3.686 46.460 34.884 2748.359 5.249 155.163 5.757 0.54 334557. 0.7389
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5.57 0.0436 0.1364 0.0809 0.0258 3.728 46.996 34.235 2780.078 5.310 152.279 5.586 0.54 334766. 0.7102
|
|
8.35 0.0653 0.1984 0.0792 0.0261 3.766 47.468 33.541 2807.986 5.363 149.189 5.418 0.54 334990. 0.6819
|
|
11.14 0.0871 0.2565 0.0775 0.0263 3.797 47.863 32.797 2831.367 5.408 145.882 5.254 0.54 335231. 0.6539
|
|
13.92 0.1089 0.3109 0.0756 0.0265 3.821 48.169 32.003 2849.477 5.442 142.351 5.094 0.54 335488. 0.6263
|
|
16.71 0.1307 0.3617 0.0736 0.0266 3.837 48.373 31.157 2861.544 5.465 138.587 4.939 0.54 335763. 0.5991
|
|
19.49 0.1525 0.4091 0.0715 0.0266 3.844 48.462 30.257 2866.790 5.475 134.584 4.787 0.54 336055. 0.5723
|
|
22.28 0.1742 0.4531 0.0692 0.0266 3.841 48.422 29.302 2864.425 5.471 130.335 4.640 0.54 336366. 0.5458
|
|
25.06 0.1960 0.4940 0.0668 0.0265 3.827 48.240 28.291 2853.652 5.450 125.837 4.497 0.54 336697. 0.5198
|
|
27.84 0.2178 0.5319 0.0643 0.0263 3.800 47.901 27.222 2833.647 5.412 121.082 4.357 0.54 337046. 0.4940
|
|
30.63 0.2396 0.5669 0.0616 0.0260 3.760 47.392 26.093 2803.505 5.354 116.063 4.222 0.54 337415. 0.4686
|
|
33.41 0.2614 0.5990 0.0588 0.0257 3.705 46.698 24.906 2762.463 5.276 110.780 4.089 0.54 337804. 0.4435
|
|
36.20 0.2832 0.6284 0.0559 0.0252 3.634 45.814 23.662 2710.141 5.176 105.249 3.960 0.54 338214. 0.4186
|
|
38.98 0.3049 0.6551 0.0528 0.0246 3.549 44.735 22.367 2646.368 5.054 99.487 3.833 0.54 338644. 0.3940
|
|
41.77 0.3267 0.6791 0.0497 0.0239 3.448 43.462 21.024 2571.042 4.910 93.513 3.709 0.54 339095. 0.3696
|
|
44.55 0.3485 0.7003 0.0464 0.0231 3.331 41.992 19.637 2484.089 4.744 87.345 3.585 0.54 339567. 0.3453
|
|
47.34 0.3703 0.7186 0.0430 0.0222 3.199 40.325 18.211 2385.474 4.556 81.001 3.463 0.54 340060. 0.3211
|
|
50.12 0.3921 0.7337 0.0396 0.0211 3.051 38.461 16.749 2275.193 4.345 74.500 3.339 0.54 340574. 0.2970
|
|
52.91 0.4138 0.7453 0.0360 0.0200 2.888 36.400 15.256 2153.290 4.112 67.860 3.214 0.54 341109. 0.2728
|
|
55.69 0.4356 0.7531 0.0324 0.0188 2.709 34.145 13.737 2019.865 3.858 61.101 3.085 0.54 341666. 0.2485
|
|
58.47 0.4574 0.7562 0.0288 0.0174 2.515 31.698 12.195 1875.101 3.581 54.244 2.950 0.54 342245. 0.2239
|
|
61.26 0.4792 0.7536 0.0251 0.0160 2.306 29.063 10.636 1719.271 3.284 47.311 2.806 0.54 342846. 0.1989
|
|
64.04 0.5010 0.7435 0.0214 0.0144 2.082 26.249 9.066 1552.756 2.966 40.326 2.648 0.54 343469. 0.1733
|
|
66.83 0.5227 0.7233 0.0177 0.0128 1.845 23.262 7.490 1376.077 2.628 33.318 2.469 0.54 344114. 0.1468
|
|
69.61 0.5445 0.6882 0.0140 0.0111 1.596 20.115 5.916 1189.913 2.273 26.315 2.255 0.54 344781. 0.1192
|
|
72.40 0.5663 0.6294 0.0103 0.0092 1.334 16.822 4.351 995.126 1.901 19.353 1.983 0.54 345471. 0.0899
|
|
75.18 0.5881 0.5285 0.0066 0.0074 1.063 13.402 2.803 792.784 1.514 12.467 1.604 0.54 346183. 0.0583
|
|
77.97 0.6099 0.3400 0.0030 0.0054 0.783 9.874 1.281 584.096 1.116 5.697 0.995 0.55 346915. 0.0245
|
|
80.75 0.6316
|
|
|
|
|
|
|
|
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 0.0855 0.0257 6.413 67.366 52.113 4782.131 7.611 231.798 4.943 0.64 401185. 0.7754
|
|
3.32 0.0216 0.0699 0.0841 0.0260 6.496 68.234 51.248 4843.748 7.709 227.953 4.799 0.64 401418. 0.7466
|
|
6.64 0.0433 0.1356 0.0825 0.0263 6.571 69.025 50.318 4899.869 7.798 223.813 4.658 0.64 401669. 0.7180
|
|
9.96 0.0649 0.1974 0.0809 0.0266 6.637 69.720 49.318 4949.206 7.877 219.368 4.520 0.64 401938. 0.6898
|
|
13.28 0.0866 0.2553 0.0791 0.0268 6.692 70.301 48.248 4990.493 7.943 214.605 4.385 0.64 402227. 0.6619
|
|
16.60 0.1082 0.3096 0.0773 0.0270 6.735 70.751 47.102 5022.411 7.993 209.512 4.254 0.64 402535. 0.6345
|
|
19.92 0.1299 0.3603 0.0753 0.0271 6.764 71.050 45.880 5043.613 8.027 204.076 4.126 0.64 402865. 0.6074
|
|
23.24 0.1515 0.4077 0.0731 0.0272 6.776 71.178 44.579 5052.742 8.042 198.287 4.002 0.64 403215. 0.5806
|
|
26.56 0.1731 0.4519 0.0708 0.0271 6.770 71.117 43.196 5048.408 8.035 192.137 3.881 0.64 403588. 0.5543
|
|
29.88 0.1948 0.4930 0.0684 0.0270 6.744 70.847 41.731 5029.233 8.004 185.618 3.764 0.64 403983. 0.5284
|
|
33.20 0.2164 0.5312 0.0659 0.0269 6.697 70.348 40.180 4993.792 7.948 178.722 3.649 0.64 404401. 0.5027
|
|
36.52 0.2381 0.5665 0.0632 0.0266 6.625 69.598 38.543 4940.549 7.863 171.438 3.538 0.64 404842. 0.4774
|
|
39.84 0.2597 0.5992 0.0604 0.0262 6.528 68.577 36.817 4868.101 7.748 163.763 3.430 0.64 405307. 0.4523
|
|
43.16 0.2814 0.6291 0.0574 0.0257 6.404 67.275 35.008 4775.686 7.601 155.717 3.325 0.65 405796. 0.4275
|
|
46.48 0.3030 0.6565 0.0543 0.0251 6.253 65.688 33.122 4662.985 7.421 147.325 3.222 0.65 406309. 0.4029
|
|
49.80 0.3246 0.6813 0.0511 0.0244 6.075 63.812 31.163 4529.838 7.209 138.615 3.120 0.65 406846. 0.3786
|
|
53.12 0.3463 0.7034 0.0478 0.0235 5.868 61.647 29.140 4376.134 6.965 129.615 3.020 0.65 407408. 0.3543
|
|
56.44 0.3679 0.7227 0.0444 0.0226 5.635 59.191 27.057 4201.812 6.687 120.351 2.921 0.65 407995. 0.3302
|
|
59.76 0.3896 0.7391 0.0409 0.0215 5.373 56.445 24.921 4006.872 6.377 110.848 2.821 0.65 408607. 0.3060
|
|
63.08 0.4112 0.7522 0.0373 0.0204 5.084 53.410 22.737 3791.395 6.034 101.135 2.720 0.65 409244. 0.2819
|
|
66.40 0.4328 0.7617 0.0336 0.0191 4.768 50.087 20.513 3555.556 5.659 91.240 2.617 0.65 409907. 0.2576
|
|
69.72 0.4545 0.7670 0.0299 0.0177 4.425 46.483 18.254 3299.659 5.252 81.193 2.509 0.65 410595. 0.2330
|
|
73.04 0.4761 0.7669 0.0262 0.0163 4.055 42.602 15.968 3024.166 4.813 71.026 2.395 0.65 411309. 0.2080
|
|
76.36 0.4978 0.7600 0.0224 0.0147 3.661 38.454 13.663 2729.727 4.344 60.775 2.270 0.65 412049. 0.1824
|
|
79.68 0.5194 0.7439 0.0186 0.0130 3.242 34.052 11.349 2417.231 3.847 50.479 2.129 0.65 412815. 0.1559
|
|
83.00 0.5411 0.7141 0.0148 0.0112 2.800 29.411 9.034 2087.835 3.323 40.182 1.963 0.65 413607. 0.1282
|
|
86.32 0.5627 0.6627 0.0110 0.0094 2.337 24.554 6.730 1743.021 2.774 29.933 1.751 0.65 414426. 0.0987
|
|
89.64 0.5843 0.5727 0.0073 0.0074 1.857 19.505 4.448 1384.631 2.204 19.786 1.457 0.65 415271. 0.0668
|
|
92.96 0.6060 0.4012 0.0036 0.0055 1.361 14.296 2.203 1014.822 1.615 9.798 0.985 0.65 416140. 0.0318
|
|
96.28 0.6276 -0.0051 0.0000 0.0034 0.847 8.902 -0.017 631.945 1.006 -0.075 -0.012 0.66 416990. 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 0.0877 0.0267 10.567 95.145 72.752 7879.768 10.749 323.601 4.188 0.75 467969. 0.7762
|
|
3.87 0.0216 0.0690 0.0863 0.0270 10.691 96.266 71.581 7972.541 10.876 318.390 4.072 0.75 468243. 0.7488
|
|
7.73 0.0432 0.1342 0.0847 0.0273 10.805 97.287 70.315 8057.141 10.991 312.760 3.958 0.75 468538. 0.7213
|
|
11.60 0.0648 0.1956 0.0831 0.0275 10.905 98.185 68.952 8131.494 11.093 306.697 3.846 0.75 468854. 0.6941
|
|
15.46 0.0864 0.2533 0.0813 0.0277 10.988 98.933 67.487 8193.500 11.177 300.181 3.736 0.75 469194. 0.6670
|
|
19.33 0.1080 0.3074 0.0794 0.0279 11.051 99.506 65.916 8240.942 11.242 293.193 3.628 0.75 469557. 0.6401
|
|
23.20 0.1296 0.3582 0.0774 0.0280 11.092 99.876 64.235 8271.533 11.284 285.716 3.522 0.75 469944. 0.6135
|
|
27.06 0.1512 0.4057 0.0752 0.0280 11.108 100.013 62.441 8282.905 11.299 277.736 3.419 0.75 470356. 0.5872
|
|
30.93 0.1728 0.4500 0.0729 0.0280 11.094 99.889 60.531 8272.652 11.285 269.241 3.319 0.75 470793. 0.5611
|
|
34.80 0.1944 0.4913 0.0705 0.0279 11.048 99.475 58.502 8238.324 11.239 260.218 3.221 0.75 471257. 0.5354
|
|
38.66 0.2160 0.5298 0.0679 0.0277 10.966 98.740 56.353 8177.465 11.156 250.658 3.126 0.75 471747. 0.5099
|
|
42.53 0.2376 0.5655 0.0652 0.0274 10.845 97.652 54.080 8087.399 11.033 240.546 3.033 0.75 472264. 0.4847
|
|
46.39 0.2592 0.5985 0.0623 0.0270 10.682 96.182 51.681 7965.609 10.867 229.876 2.943 0.75 472809. 0.4597
|
|
50.26 0.2808 0.6290 0.0592 0.0264 10.474 94.311 49.161 7810.671 10.655 218.669 2.855 0.75 473381. 0.4350
|
|
54.13 0.3024 0.6570 0.0561 0.0258 10.221 92.034 46.530 7622.063 10.398 206.963 2.769 0.75 473982. 0.4105
|
|
57.99 0.3240 0.6825 0.0528 0.0251 9.923 89.347 43.795 7399.558 10.094 194.800 2.684 0.75 474611. 0.3861
|
|
61.86 0.3456 0.7054 0.0494 0.0242 9.579 86.250 40.966 7143.049 9.744 182.216 2.601 0.75 475268. 0.3618
|
|
65.72 0.3672 0.7257 0.0459 0.0232 9.189 82.742 38.051 6852.523 9.348 169.249 2.519 0.75 475954. 0.3376
|
|
69.59 0.3888 0.7431 0.0422 0.0221 8.754 78.825 35.058 6528.111 8.906 155.937 2.436 0.76 476668. 0.3134
|
|
73.46 0.4104 0.7574 0.0386 0.0209 8.274 74.502 31.996 6170.095 8.417 142.317 2.352 0.76 477412. 0.2891
|
|
77.32 0.4320 0.7682 0.0348 0.0196 7.750 69.779 28.874 5778.953 7.884 128.431 2.266 0.76 478185. 0.2646
|
|
81.19 0.4536 0.7748 0.0310 0.0181 7.182 64.665 25.701 5355.435 7.306 114.319 2.177 0.76 478987. 0.2398
|
|
85.06 0.4752 0.7761 0.0271 0.0166 6.572 59.173 22.488 4900.632 6.685 100.027 2.081 0.76 479819. 0.2145
|
|
88.92 0.4968 0.7706 0.0232 0.0150 5.922 53.322 19.246 4416.033 6.024 85.605 1.977 0.76 480681. 0.1885
|
|
92.79 0.5184 0.7556 0.0193 0.0132 5.235 47.135 15.987 3903.646 5.325 71.108 1.857 0.76 481573. 0.1614
|
|
96.65 0.5400 0.7265 0.0153 0.0114 4.514 40.644 12.724 3366.061 4.592 56.598 1.715 0.76 482495. 0.1329
|
|
100.52 0.5616 0.6747 0.0114 0.0095 3.764 33.888 9.474 2806.550 3.829 42.142 1.531 0.76 483448. 0.1024
|
|
104.39 0.5832 0.5823 0.0075 0.0075 2.989 26.916 6.254 2229.117 3.041 27.817 1.273 0.76 484431. 0.0692
|
|
108.25 0.6048 0.4048 0.0037 0.0055 2.197 19.783 3.081 1638.383 2.235 13.706 0.853 0.76 485442. 0.0325
|
|
112.12 0.6264 -0.0128 -0.0001 0.0035 1.383 12.452 -0.059 1031.241 1.407 -0.264 -0.026 0.76 486425. 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 0.0905 0.0310 18.327 144.392 98.055 13666.633 16.313 436.146 3.254 0.86 534695. 0.7003
|
|
4.42 0.0216 0.0618 0.0891 0.0311 18.382 144.823 96.558 13707.437 16.362 429.488 3.195 0.86 535011. 0.6823
|
|
8.83 0.0432 0.1214 0.0876 0.0312 18.417 145.099 94.930 13733.565 16.393 422.247 3.135 0.86 535352. 0.6638
|
|
13.25 0.0648 0.1786 0.0860 0.0312 18.430 145.198 93.166 13742.932 16.404 414.403 3.075 0.86 535718. 0.6450
|
|
17.66 0.0863 0.2334 0.0842 0.0312 18.417 145.097 91.260 13733.362 16.393 405.926 3.014 0.86 536110. 0.6257
|
|
22.08 0.1079 0.2858 0.0823 0.0311 18.375 144.771 89.206 13702.488 16.356 396.789 2.953 0.86 536530. 0.6061
|
|
26.49 0.1295 0.3358 0.0803 0.0310 18.302 144.195 86.998 13647.946 16.291 386.966 2.891 0.86 536977. 0.5861
|
|
30.91 0.1511 0.3834 0.0781 0.0308 18.194 143.342 84.631 13567.214 16.195 376.437 2.829 0.86 537453. 0.5656
|
|
35.32 0.1727 0.4285 0.0757 0.0305 18.047 142.185 82.101 13457.701 16.064 365.185 2.767 0.86 537959. 0.5449
|
|
39.74 0.1943 0.4712 0.0733 0.0302 17.858 140.694 79.405 13316.624 15.896 353.193 2.705 0.86 538494. 0.5237
|
|
44.15 0.2159 0.5114 0.0706 0.0298 17.622 138.839 76.540 13141.044 15.686 340.448 2.642 0.86 539060. 0.5023
|
|
48.57 0.2374 0.5491 0.0678 0.0293 17.336 136.584 73.501 12927.605 15.431 326.934 2.579 0.86 539657. 0.4805
|
|
52.98 0.2590 0.5843 0.0648 0.0287 16.994 133.890 70.287 12672.633 15.127 312.635 2.516 0.86 540285. 0.4583
|
|
57.40 0.2806 0.6171 0.0617 0.0281 16.593 130.732 66.902 12373.672 14.770 297.578 2.452 0.86 540945. 0.4359
|
|
61.82 0.3022 0.6474 0.0585 0.0273 16.132 127.095 63.357 12029.515 14.359 281.814 2.389 0.86 541636. 0.4132
|
|
66.23 0.3238 0.6750 0.0550 0.0264 15.611 122.995 59.666 11641.378 13.896 265.396 2.325 0.86 542360. 0.3902
|
|
70.65 0.3454 0.6993 0.0515 0.0254 15.043 118.519 55.839 11217.732 13.390 248.373 2.258 0.86 543116. 0.3666
|
|
75.06 0.3670 0.7201 0.0479 0.0244 14.422 113.623 51.889 10754.365 12.837 230.802 2.188 0.86 543904. 0.3426
|
|
79.48 0.3886 0.7372 0.0441 0.0233 13.750 108.328 47.827 10253.224 12.239 212.733 2.116 0.86 544724. 0.3180
|
|
83.89 0.4101 0.7495 0.0403 0.0220 13.032 102.671 43.664 9717.727 11.600 194.217 2.038 0.86 545578. 0.2927
|
|
88.31 0.4317 0.7572 0.0364 0.0207 12.258 96.575 39.415 9140.792 10.911 175.317 1.956 0.86 546464. 0.2668
|
|
92.72 0.4533 0.7589 0.0324 0.0193 11.432 90.070 35.092 8525.094 10.176 156.090 1.867 0.87 547384. 0.2404
|
|
97.14 0.4749 0.7532 0.0283 0.0179 10.561 83.204 30.710 7875.169 9.400 136.599 1.769 0.87 548337. 0.2130
|
|
101.55 0.4965 0.7376 0.0242 0.0163 9.650 76.025 26.284 7195.700 8.589 116.912 1.657 0.87 549323. 0.1846
|
|
105.97 0.5181 0.7086 0.0201 0.0147 8.706 68.593 21.832 6492.269 7.750 97.107 1.525 0.87 550344. 0.1549
|
|
110.38 0.5397 0.6607 0.0160 0.0131 7.740 60.976 17.372 5771.345 6.889 77.271 1.365 0.87 551398. 0.1237
|
|
114.80 0.5612 0.5854 0.0119 0.0114 6.759 53.253 12.926 5040.321 6.016 57.497 1.163 0.87 552487. 0.0909
|
|
119.22 0.5828 0.4689 0.0079 0.0098 5.776 45.505 8.519 4307.070 5.141 37.894 0.897 0.87 553610. 0.0569
|
|
123.63 0.6044 0.2869 0.0039 0.0081 4.800 37.820 4.177 3579.679 4.273 18.580 0.529 0.87 554765. 0.0235
|
|
128.05 0.6260 -0.0106 -0.0001 0.0065 3.819 30.089 -0.118 2847.888 3.399 -0.526 -0.019 0.87 555908. 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 0.0912 0.0406 34.174 239.324 125.070 25483.361 27.039 556.309 2.226 0.96 601485. 0.5410
|
|
5.19 0.0225 0.0499 0.0900 0.0406 34.205 239.541 123.433 25506.475 27.063 549.028 2.195 0.96 601847. 0.5300
|
|
10.38 0.0451 0.0985 0.0886 0.0406 34.175 239.329 121.610 25483.939 27.039 540.923 2.164 0.96 602239. 0.5187
|
|
15.56 0.0676 0.1457 0.0872 0.0405 34.073 238.616 119.588 25407.928 26.959 531.925 2.135 0.96 602664. 0.5073
|
|
20.75 0.0902 0.1916 0.0855 0.0403 33.892 237.353 117.352 25273.537 26.816 521.980 2.106 0.96 603123. 0.4958
|
|
25.94 0.1127 0.2363 0.0837 0.0399 33.626 235.491 114.888 25075.221 26.606 511.022 2.078 0.96 603617. 0.4841
|
|
31.13 0.1353 0.2799 0.0818 0.0395 33.269 232.985 112.185 24808.375 26.323 498.997 2.051 0.96 604148. 0.4721
|
|
36.32 0.1578 0.3224 0.0796 0.0390 32.814 229.804 109.230 24469.695 25.963 485.855 2.025 0.97 604715. 0.4599
|
|
41.50 0.1804 0.3637 0.0773 0.0383 32.261 225.929 106.016 24057.053 25.525 471.557 1.999 0.97 605320. 0.4473
|
|
46.69 0.2029 0.4039 0.0747 0.0375 31.607 221.351 102.535 23569.541 25.008 456.076 1.973 0.97 605964. 0.4342
|
|
51.88 0.2255 0.4429 0.0720 0.0367 30.853 216.067 98.783 23006.967 24.411 439.387 1.947 0.97 606646. 0.4206
|
|
57.07 0.2480 0.4807 0.0691 0.0356 29.998 210.078 94.754 22369.275 23.735 421.466 1.921 0.97 607368. 0.4064
|
|
62.26 0.2705 0.5170 0.0659 0.0345 29.042 203.386 90.448 21656.674 22.978 402.310 1.894 0.97 608129. 0.3915
|
|
67.45 0.2931 0.5518 0.0626 0.0333 27.990 196.017 85.877 20872.016 22.146 381.983 1.866 0.97 608930. 0.3758
|
|
72.63 0.3156 0.5848 0.0591 0.0319 26.847 188.010 81.065 20019.473 21.241 360.577 1.837 0.97 609771. 0.3594
|
|
77.82 0.3382 0.6159 0.0554 0.0304 25.618 179.403 76.031 19102.986 20.269 338.188 1.805 0.97 610651. 0.3421
|
|
83.01 0.3607 0.6444 0.0516 0.0289 24.319 170.308 70.797 18134.467 19.241 314.905 1.771 0.97 611571. 0.3238
|
|
88.20 0.3833 0.6676 0.0477 0.0274 23.029 161.277 65.375 17172.863 18.221 290.789 1.727 0.97 612531. 0.3034
|
|
93.39 0.4058 0.6845 0.0436 0.0258 21.751 152.329 59.789 16220.035 17.210 265.941 1.672 0.97 613531. 0.2809
|
|
98.57 0.4284 0.6891 0.0394 0.0245 20.618 144.388 54.049 15374.520 16.313 240.408 1.595 0.97 614571. 0.2548
|
|
103.76 0.4509 0.6765 0.0351 0.0234 19.703 137.984 48.171 14692.625 15.589 214.266 1.487 0.97 615651. 0.2243
|
|
108.95 0.4735 0.6534 0.0308 0.0223 18.768 131.436 42.212 13995.340 14.850 187.759 1.368 0.97 616771. 0.1932
|
|
114.14 0.4960 0.6181 0.0264 0.0212 17.826 124.836 36.202 13292.622 14.104 161.028 1.235 0.98 617932. 0.1615
|
|
119.33 0.5186 0.5686 0.0220 0.0201 16.889 118.274 30.179 12593.929 13.363 134.235 1.087 0.98 619134. 0.1298
|
|
124.51 0.5411 0.5027 0.0176 0.0190 15.971 111.848 24.182 11909.632 12.637 107.563 0.921 0.98 620377. 0.0984
|
|
129.70 0.5636 0.4188 0.0133 0.0179 15.079 105.603 18.260 11244.654 11.931 81.221 0.737 0.98 621662. 0.0684
|
|
134.89 0.5862 0.3151 0.0091 0.0169 14.220 99.588 12.459 10604.178 11.251 55.416 0.533 0.98 622991. 0.0409
|
|
140.08 0.6087 0.1900 0.0050 0.0159 13.398 93.826 6.815 9990.635 10.600 30.311 0.309 0.98 624370. 0.0176
|
|
145.27 0.6313 0.0398 0.0009 0.0149 12.572 88.041 1.292 9374.608 9.947 5.748 0.063 0.98 625833. 0.0015
|
|
150.46 0.6538
|
|
|
|
|
|
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