575 lines
102 KiB
Plaintext
575 lines
102 KiB
Plaintext
16x10E (16x10E.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 0.0955 0.0403 0.003 0.214 0.199 2.536 0.024 0.887 35.670 0.06 23803. 0.5842
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0.40 0.0265 0.0611 0.0943 0.0408 0.003 0.217 0.197 2.570 0.025 0.876 34.761 0.06 23820. 0.5658
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0.80 0.0529 0.1190 0.0930 0.0414 0.003 0.220 0.194 2.604 0.025 0.864 33.846 0.06 23839. 0.5471
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1.20 0.0794 0.1737 0.0916 0.0419 0.004 0.223 0.191 2.636 0.025 0.851 32.929 0.06 23860. 0.5283
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1.60 0.1059 0.2251 0.0901 0.0424 0.004 0.225 0.188 2.666 0.025 0.837 32.014 0.06 23882. 0.5092
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2.01 0.1323 0.2734 0.0884 0.0428 0.004 0.228 0.185 2.692 0.026 0.821 31.104 0.06 23906. 0.4901
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2.41 0.1588 0.3186 0.0866 0.0432 0.004 0.230 0.181 2.715 0.026 0.804 30.201 0.06 23933. 0.4709
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2.81 0.1853 0.3607 0.0846 0.0434 0.004 0.231 0.177 2.734 0.026 0.786 29.308 0.06 23961. 0.4517
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3.21 0.2117 0.3998 0.0824 0.0436 0.004 0.232 0.172 2.746 0.026 0.766 28.426 0.06 23992. 0.4325
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3.61 0.2382 0.4360 0.0801 0.0437 0.004 0.233 0.167 2.752 0.026 0.744 27.555 0.06 24025. 0.4132
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4.01 0.2647 0.4693 0.0775 0.0437 0.004 0.232 0.162 2.751 0.026 0.720 26.696 0.06 24060. 0.3939
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4.41 0.2911 0.4998 0.0748 0.0436 0.004 0.232 0.156 2.741 0.026 0.695 25.847 0.06 24098. 0.3746
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4.81 0.3176 0.5276 0.0718 0.0433 0.004 0.230 0.150 2.721 0.026 0.667 25.008 0.06 24138. 0.3552
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5.21 0.3441 0.5525 0.0687 0.0428 0.004 0.228 0.143 2.692 0.026 0.638 24.174 0.06 24180. 0.3358
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5.61 0.3705 0.5745 0.0654 0.0422 0.004 0.224 0.137 2.652 0.025 0.607 23.344 0.06 24225. 0.3163
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6.02 0.3970 0.5936 0.0618 0.0413 0.003 0.220 0.129 2.601 0.025 0.574 22.510 0.06 24272. 0.2966
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6.42 0.4235 0.6095 0.0581 0.0403 0.003 0.215 0.121 2.539 0.024 0.539 21.667 0.06 24322. 0.2767
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6.82 0.4499 0.6218 0.0541 0.0392 0.003 0.208 0.113 2.464 0.024 0.503 20.805 0.06 24374. 0.2565
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7.22 0.4764 0.6303 0.0500 0.0378 0.003 0.201 0.104 2.378 0.023 0.465 19.917 0.06 24428. 0.2360
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7.62 0.5029 0.6343 0.0457 0.0363 0.003 0.193 0.096 2.282 0.022 0.425 18.988 0.06 24485. 0.2152
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8.02 0.5293 0.6331 0.0413 0.0346 0.003 0.184 0.086 2.175 0.021 0.384 18.006 0.06 24544. 0.1940
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8.42 0.5558 0.6259 0.0368 0.0327 0.003 0.174 0.077 2.058 0.020 0.342 16.953 0.06 24606. 0.1724
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8.82 0.5823 0.6113 0.0323 0.0307 0.003 0.163 0.067 1.933 0.018 0.300 15.805 0.06 24670. 0.1504
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9.22 0.6087 0.5876 0.0276 0.0286 0.002 0.152 0.058 1.800 0.017 0.257 14.532 0.06 24737. 0.1280
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9.62 0.6352 0.5524 0.0229 0.0264 0.002 0.140 0.048 1.659 0.016 0.213 13.092 0.06 24805. 0.1051
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10.03 0.6617 0.5022 0.0182 0.0240 0.002 0.128 0.038 1.511 0.014 0.169 11.427 0.06 24877. 0.0818
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10.43 0.6881 0.4319 0.0135 0.0216 0.002 0.115 0.028 1.357 0.013 0.126 9.450 0.06 24950. 0.0583
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10.83 0.7146 0.3336 0.0089 0.0190 0.002 0.101 0.019 1.198 0.011 0.083 7.027 0.07 25026. 0.0351
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11.23 0.7411 0.1941 0.0043 0.0164 0.001 0.087 0.009 1.035 0.010 0.040 3.943 0.07 25105. 0.0137
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11.63 0.7675 -0.0092 -0.0002 0.0138 0.001 0.073 0.000 0.869 0.008 -0.002 -0.181 0.07 25185. 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 0.0958 0.0370 0.025 0.788 0.800 18.645 0.089 3.560 19.472 0.13 47606. 0.6389
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0.81 0.0266 0.0668 0.0947 0.0376 0.025 0.801 0.791 18.944 0.090 3.517 18.933 0.13 47640. 0.6174
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1.61 0.0531 0.1299 0.0934 0.0382 0.026 0.813 0.780 19.236 0.092 3.470 18.393 0.13 47678. 0.5957
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2.42 0.0797 0.1891 0.0920 0.0388 0.026 0.825 0.768 19.518 0.093 3.418 17.855 0.13 47719. 0.5739
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3.22 0.1063 0.2446 0.0904 0.0393 0.027 0.836 0.755 19.782 0.094 3.360 17.322 0.13 47764. 0.5521
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4.03 0.1329 0.2964 0.0888 0.0398 0.027 0.846 0.741 20.024 0.096 3.298 16.795 0.13 47813. 0.5304
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4.83 0.1594 0.3447 0.0869 0.0402 0.027 0.855 0.726 20.235 0.097 3.230 16.276 0.13 47867. 0.5086
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5.64 0.1860 0.3896 0.0849 0.0405 0.027 0.862 0.709 20.407 0.097 3.155 15.767 0.13 47924. 0.4870
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6.44 0.2126 0.4312 0.0827 0.0408 0.028 0.868 0.691 20.535 0.098 3.075 15.268 0.13 47986. 0.4655
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7.25 0.2392 0.4695 0.0804 0.0409 0.028 0.871 0.672 20.608 0.098 2.987 14.779 0.13 48052. 0.4441
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8.05 0.2657 0.5049 0.0778 0.0410 0.028 0.871 0.650 20.621 0.098 2.892 14.301 0.13 48123. 0.4229
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8.86 0.2923 0.5372 0.0751 0.0409 0.028 0.869 0.627 20.563 0.098 2.790 13.834 0.13 48199. 0.4018
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9.66 0.3189 0.5667 0.0721 0.0406 0.027 0.863 0.603 20.429 0.098 2.680 13.377 0.13 48280. 0.3808
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10.47 0.3454 0.5933 0.0690 0.0402 0.027 0.854 0.576 20.212 0.097 2.562 12.928 0.13 48365. 0.3599
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11.27 0.3720 0.6171 0.0656 0.0395 0.027 0.841 0.548 19.905 0.095 2.437 12.486 0.13 48455. 0.3390
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12.08 0.3986 0.6380 0.0620 0.0387 0.026 0.824 0.518 19.505 0.093 2.305 12.048 0.13 48550. 0.3180
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12.88 0.4252 0.6558 0.0582 0.0378 0.025 0.803 0.487 19.008 0.091 2.164 11.611 0.13 48650. 0.2970
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13.69 0.4517 0.6704 0.0543 0.0366 0.025 0.778 0.453 18.410 0.088 2.017 11.171 0.13 48755. 0.2759
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14.49 0.4783 0.6814 0.0501 0.0352 0.024 0.749 0.419 17.713 0.085 1.863 10.723 0.13 48864. 0.2545
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15.30 0.5049 0.6883 0.0458 0.0336 0.023 0.715 0.383 16.923 0.081 1.703 10.262 0.13 48979. 0.2329
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16.10 0.5315 0.6905 0.0414 0.0319 0.022 0.678 0.346 16.045 0.077 1.539 9.781 0.13 49098. 0.2110
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16.91 0.5580 0.6872 0.0369 0.0300 0.020 0.637 0.308 15.085 0.072 1.371 9.270 0.13 49223. 0.1887
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17.72 0.5846 0.6769 0.0323 0.0279 0.019 0.594 0.270 14.046 0.067 1.201 8.716 0.13 49352. 0.1661
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18.52 0.6112 0.6580 0.0277 0.0257 0.017 0.547 0.231 12.933 0.062 1.028 8.104 0.13 49485. 0.1429
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19.33 0.6377 0.6277 0.0230 0.0233 0.016 0.497 0.192 11.753 0.056 0.854 7.409 0.13 49624. 0.1190
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20.13 0.6643 0.5819 0.0183 0.0209 0.014 0.444 0.153 10.510 0.050 0.680 6.594 0.13 49768. 0.0945
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20.94 0.6909 0.5140 0.0136 0.0183 0.012 0.389 0.114 9.213 0.044 0.506 5.600 0.13 49916. 0.0693
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21.74 0.7175 0.4127 0.0090 0.0156 0.011 0.333 0.075 7.870 0.038 0.334 4.330 0.13 50069. 0.0435
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22.55 0.7440 0.2567 0.0044 0.0129 0.009 0.274 0.037 6.492 0.031 0.165 2.597 0.13 50227. 0.0184
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23.35 0.7706 0.0014 0.0000 0.0101 0.007 0.215 0.000 5.088 0.024 0.001 0.013 0.13 50389. 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 0.0961 0.0357 0.081 1.707 1.807 60.602 0.193 8.036 13.521 0.19 71408. 0.6665
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1.21 0.0266 0.0697 0.0949 0.0363 0.083 1.737 1.785 61.647 0.196 7.939 13.131 0.19 71459. 0.6433
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2.42 0.0533 0.1353 0.0937 0.0369 0.084 1.766 1.761 62.675 0.200 7.832 12.742 0.19 71516. 0.6201
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3.63 0.0799 0.1968 0.0923 0.0375 0.085 1.794 1.734 63.667 0.203 7.715 12.356 0.19 71578. 0.5968
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4.84 0.1066 0.2543 0.0907 0.0380 0.087 1.820 1.706 64.604 0.206 7.586 11.974 0.19 71646. 0.5735
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6.06 0.1332 0.3079 0.0891 0.0385 0.088 1.844 1.674 65.461 0.208 7.446 11.599 0.19 71720. 0.5503
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7.27 0.1599 0.3577 0.0872 0.0390 0.089 1.866 1.639 66.216 0.211 7.292 11.230 0.19 71800. 0.5273
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8.48 0.1865 0.4040 0.0852 0.0393 0.090 1.883 1.602 66.842 0.213 7.124 10.869 0.19 71887. 0.5044
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9.69 0.2132 0.4467 0.0830 0.0396 0.090 1.896 1.561 67.312 0.214 6.942 10.516 0.19 71980. 0.4818
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10.90 0.2398 0.4861 0.0807 0.0398 0.091 1.905 1.516 67.599 0.215 6.744 10.173 0.19 72080. 0.4594
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12.11 0.2664 0.5224 0.0781 0.0398 0.091 1.907 1.468 67.674 0.215 6.529 9.839 0.19 72187. 0.4372
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13.32 0.2931 0.5556 0.0753 0.0397 0.091 1.902 1.416 67.511 0.215 6.298 9.513 0.19 72302. 0.4151
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14.53 0.3197 0.5859 0.0724 0.0395 0.090 1.890 1.360 67.083 0.214 6.050 9.196 0.19 72423. 0.3933
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15.74 0.3464 0.6134 0.0692 0.0391 0.089 1.870 1.300 66.367 0.211 5.784 8.887 0.19 72552. 0.3716
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16.96 0.3730 0.6380 0.0658 0.0385 0.088 1.841 1.237 65.343 0.208 5.500 8.584 0.19 72688. 0.3500
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18.17 0.3997 0.6599 0.0622 0.0377 0.086 1.803 1.169 63.994 0.204 5.200 8.285 0.19 72831. 0.3285
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19.38 0.4263 0.6788 0.0584 0.0367 0.084 1.755 1.098 62.306 0.198 4.882 7.990 0.19 72981. 0.3070
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20.59 0.4530 0.6945 0.0544 0.0355 0.081 1.698 1.022 60.269 0.192 4.548 7.694 0.19 73139. 0.2853
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21.80 0.4796 0.7069 0.0502 0.0341 0.078 1.631 0.944 57.886 0.184 4.199 7.396 0.19 73305. 0.2635
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23.01 0.5062 0.7154 0.0459 0.0325 0.074 1.555 0.863 55.178 0.176 3.838 7.092 0.19 73477. 0.2416
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24.22 0.5329 0.7196 0.0415 0.0307 0.070 1.470 0.779 52.160 0.166 3.466 6.776 0.19 73657. 0.2194
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25.43 0.5595 0.7184 0.0369 0.0288 0.066 1.376 0.694 48.851 0.155 3.087 6.443 0.19 73845. 0.1968
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26.64 0.5862 0.7108 0.0323 0.0266 0.061 1.275 0.607 45.264 0.144 2.701 6.085 0.19 74039. 0.1739
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27.86 0.6128 0.6948 0.0276 0.0244 0.056 1.167 0.520 41.418 0.132 2.311 5.689 0.19 74241. 0.1504
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29.07 0.6395 0.6677 0.0229 0.0220 0.050 1.052 0.431 37.329 0.119 1.918 5.240 0.19 74450. 0.1262
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30.28 0.6661 0.6251 0.0182 0.0194 0.044 0.930 0.343 33.021 0.105 1.525 4.710 0.19 74667. 0.1011
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31.49 0.6928 0.5597 0.0136 0.0168 0.038 0.804 0.255 28.520 0.091 1.134 4.054 0.19 74890. 0.0751
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32.70 0.7194 0.4578 0.0089 0.0140 0.032 0.672 0.168 23.857 0.076 0.747 3.193 0.20 75121. 0.0480
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33.91 0.7461 0.2922 0.0044 0.0112 0.026 0.537 0.083 19.068 0.061 0.368 1.965 0.20 75359. 0.0207
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35.12 0.7727 -0.0027 0.0000 0.0084 0.019 0.400 -0.001 14.191 0.045 -0.002 -0.017 0.20 75603. 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 0.0964 0.0349 0.189 2.973 3.223 140.707 0.336 14.335 10.389 0.25 95208. 0.6840
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1.62 0.0267 0.0715 0.0953 0.0356 0.192 3.027 3.184 143.248 0.342 14.164 10.082 0.25 95277. 0.6598
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3.24 0.0534 0.1387 0.0940 0.0362 0.195 3.080 3.142 145.753 0.348 13.975 9.777 0.25 95353. 0.6355
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4.85 0.0801 0.2016 0.0926 0.0368 0.199 3.131 3.095 148.173 0.354 13.767 9.474 0.25 95436. 0.6113
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6.47 0.1068 0.2603 0.0911 0.0374 0.202 3.179 3.044 150.462 0.359 13.539 9.176 0.25 95527. 0.5871
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8.09 0.1335 0.3150 0.0894 0.0379 0.205 3.224 2.988 152.564 0.364 13.289 8.882 0.25 95626. 0.5631
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9.71 0.1601 0.3657 0.0876 0.0383 0.207 3.263 2.926 154.421 0.369 13.016 8.595 0.25 95733. 0.5392
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11.32 0.1868 0.4128 0.0856 0.0387 0.209 3.296 2.859 155.970 0.372 12.718 8.315 0.25 95849. 0.5156
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12.94 0.2135 0.4562 0.0834 0.0390 0.211 3.321 2.786 157.147 0.375 12.392 8.041 0.25 95974. 0.4922
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14.56 0.2402 0.4963 0.0810 0.0392 0.212 3.336 2.707 157.882 0.377 12.039 7.776 0.25 96108. 0.4691
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16.18 0.2669 0.5332 0.0784 0.0393 0.212 3.341 2.621 158.109 0.377 11.657 7.518 0.25 96251. 0.4463
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17.79 0.2936 0.5669 0.0756 0.0392 0.212 3.334 2.528 157.762 0.377 11.244 7.268 0.25 96404. 0.4238
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19.41 0.3203 0.5978 0.0727 0.0389 0.210 3.313 2.428 156.776 0.374 10.800 7.025 0.26 96566. 0.4014
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21.03 0.3470 0.6258 0.0695 0.0385 0.208 3.277 2.321 155.096 0.370 10.325 6.788 0.26 96738. 0.3793
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22.65 0.3737 0.6511 0.0661 0.0379 0.205 3.226 2.207 152.670 0.364 9.818 6.558 0.26 96920. 0.3573
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24.26 0.4004 0.6735 0.0624 0.0371 0.200 3.158 2.086 149.459 0.357 9.280 6.331 0.26 97112. 0.3354
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25.88 0.4271 0.6931 0.0586 0.0361 0.195 3.073 1.959 145.429 0.347 8.712 6.108 0.26 97314. 0.3135
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27.50 0.4538 0.7097 0.0546 0.0349 0.188 2.970 1.824 140.549 0.336 8.114 5.887 0.26 97525. 0.2916
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29.12 0.4804 0.7230 0.0504 0.0335 0.181 2.849 1.684 134.833 0.322 7.489 5.664 0.26 97746. 0.2695
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30.74 0.5071 0.7327 0.0460 0.0319 0.172 2.712 1.538 128.323 0.306 6.843 5.438 0.26 97977. 0.2473
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32.35 0.5338 0.7382 0.0416 0.0301 0.162 2.558 1.389 121.061 0.289 6.179 5.204 0.26 98218. 0.2249
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33.97 0.5605 0.7386 0.0370 0.0281 0.152 2.390 1.237 113.085 0.270 5.500 4.960 0.26 98468. 0.2023
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35.59 0.5872 0.7329 0.0324 0.0259 0.140 2.207 1.082 104.433 0.249 4.811 4.697 0.26 98729. 0.1791
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37.21 0.6139 0.7191 0.0277 0.0236 0.128 2.010 0.925 95.143 0.227 4.113 4.409 0.26 98999. 0.1555
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38.82 0.6406 0.6945 0.0230 0.0212 0.114 1.802 0.767 85.263 0.204 3.412 4.081 0.26 99279. 0.1311
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40.44 0.6673 0.6546 0.0182 0.0186 0.100 1.582 0.609 74.845 0.179 2.710 3.692 0.26 99568. 0.1057
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42.06 0.6940 0.5915 0.0135 0.0159 0.086 1.351 0.452 63.954 0.153 2.012 3.208 0.26 99868. 0.0791
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43.68 0.7207 0.4901 0.0089 0.0131 0.071 1.113 0.297 52.669 0.126 1.322 2.559 0.26 100176. 0.0512
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45.29 0.7474 0.3181 0.0043 0.0102 0.055 0.868 0.145 41.081 0.098 0.645 1.602 0.26 100495. 0.0224
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46.91 0.7741 -0.0098 -0.0001 0.0073 0.039 0.619 -0.003 29.272 0.070 -0.014 -0.048 0.26 100820. 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 0.0968 0.0345 0.364 4.592 5.057 271.637 0.519 22.493 8.444 0.32 119007. 0.6963
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2.02 0.0267 0.0726 0.0957 0.0352 0.371 4.677 4.997 276.700 0.528 22.226 8.191 0.32 119093. 0.6715
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4.05 0.0534 0.1408 0.0944 0.0358 0.378 4.762 4.931 281.695 0.538 21.933 7.939 0.32 119188. 0.6465
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6.07 0.0801 0.2046 0.0930 0.0364 0.384 4.844 4.858 286.530 0.547 21.610 7.691 0.32 119292. 0.6217
|
|
8.09 0.1068 0.2641 0.0915 0.0370 0.390 4.921 4.779 291.108 0.556 21.255 7.445 0.32 119406. 0.5969
|
|
10.11 0.1335 0.3195 0.0898 0.0375 0.396 4.992 4.691 295.321 0.564 20.866 7.205 0.32 119530. 0.5723
|
|
12.14 0.1602 0.3708 0.0880 0.0380 0.401 5.055 4.595 299.053 0.571 20.440 6.970 0.32 119664. 0.5479
|
|
14.16 0.1869 0.4184 0.0860 0.0384 0.405 5.108 4.490 302.180 0.577 19.974 6.740 0.32 119809. 0.5238
|
|
16.18 0.2136 0.4624 0.0838 0.0387 0.408 5.149 4.376 304.572 0.582 19.466 6.517 0.32 119965. 0.5000
|
|
18.21 0.2403 0.5029 0.0814 0.0389 0.410 5.174 4.252 306.094 0.585 18.913 6.301 0.32 120133. 0.4765
|
|
20.23 0.2670 0.5401 0.0789 0.0390 0.411 5.183 4.117 306.611 0.586 18.314 6.091 0.32 120312. 0.4532
|
|
22.25 0.2937 0.5743 0.0761 0.0389 0.410 5.173 3.972 305.992 0.584 17.668 5.888 0.32 120504. 0.4303
|
|
24.27 0.3204 0.6056 0.0731 0.0387 0.408 5.141 3.816 304.111 0.581 16.972 5.691 0.32 120707. 0.4077
|
|
26.30 0.3471 0.6340 0.0699 0.0383 0.403 5.086 3.648 300.853 0.575 16.226 5.500 0.32 120923. 0.3852
|
|
28.32 0.3738 0.6597 0.0664 0.0376 0.397 5.006 3.469 296.119 0.566 15.431 5.314 0.32 121150. 0.3630
|
|
30.34 0.4005 0.6827 0.0628 0.0368 0.389 4.899 3.279 289.825 0.554 14.586 5.132 0.32 121390. 0.3408
|
|
32.37 0.4272 0.7028 0.0590 0.0358 0.378 4.765 3.079 281.905 0.538 13.694 4.953 0.32 121643. 0.3187
|
|
34.39 0.4539 0.7201 0.0549 0.0346 0.365 4.603 2.867 272.297 0.520 12.755 4.776 0.32 121907. 0.2966
|
|
36.41 0.4806 0.7342 0.0507 0.0332 0.350 4.412 2.647 261.025 0.499 11.774 4.599 0.32 122184. 0.2744
|
|
38.43 0.5073 0.7448 0.0463 0.0316 0.333 4.195 2.419 248.171 0.474 10.758 4.420 0.32 122473. 0.2521
|
|
40.46 0.5340 0.7514 0.0418 0.0297 0.314 3.953 2.184 233.815 0.447 9.714 4.237 0.32 122774. 0.2296
|
|
42.48 0.5607 0.7532 0.0372 0.0277 0.292 3.686 1.944 218.033 0.416 8.648 4.045 0.32 123088. 0.2068
|
|
44.50 0.5874 0.7491 0.0326 0.0255 0.269 3.396 1.701 200.897 0.384 7.564 3.840 0.32 123414. 0.1836
|
|
46.53 0.6141 0.7373 0.0279 0.0232 0.245 3.085 1.454 182.486 0.349 6.469 3.615 0.32 123751. 0.1599
|
|
48.55 0.6408 0.7150 0.0231 0.0207 0.218 2.754 1.207 162.891 0.311 5.367 3.360 0.32 124101. 0.1353
|
|
50.57 0.6675 0.6778 0.0184 0.0181 0.191 2.404 0.959 142.221 0.272 4.264 3.057 0.32 124464. 0.1098
|
|
52.59 0.6942 0.6175 0.0136 0.0153 0.162 2.039 0.712 120.603 0.230 3.167 2.678 0.32 124838. 0.0829
|
|
54.62 0.7209 0.5182 0.0090 0.0125 0.132 1.660 0.469 98.195 0.188 2.084 2.164 0.33 125225. 0.0543
|
|
56.64 0.7476 0.3442 0.0044 0.0096 0.101 1.271 0.230 75.182 0.144 1.022 1.386 0.33 125623. 0.0244
|
|
58.66 0.7744 -0.0063 -0.0001 0.0066 0.069 0.874 -0.003 51.726 0.099 -0.013 -0.025 0.33 126029. 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 0.0973 0.0343 0.626 6.574 7.318 466.697 0.743 32.550 7.112 0.38 142803. 0.7056
|
|
2.43 0.0267 0.0734 0.0962 0.0350 0.638 6.700 7.233 475.611 0.757 32.170 6.897 0.38 142907. 0.6803
|
|
4.86 0.0534 0.1423 0.0949 0.0356 0.650 6.824 7.138 484.412 0.771 31.751 6.684 0.38 143021. 0.6549
|
|
7.28 0.0801 0.2067 0.0936 0.0363 0.661 6.944 7.034 492.939 0.785 31.289 6.473 0.38 143146. 0.6296
|
|
9.71 0.1068 0.2667 0.0920 0.0369 0.672 7.058 6.920 501.022 0.797 30.781 6.265 0.38 143282. 0.6044
|
|
12.14 0.1335 0.3225 0.0904 0.0374 0.682 7.163 6.795 508.473 0.809 30.223 6.061 0.38 143431. 0.5794
|
|
14.57 0.1602 0.3743 0.0885 0.0379 0.691 7.256 6.657 515.085 0.820 29.611 5.862 0.38 143592. 0.5547
|
|
16.99 0.1869 0.4223 0.0865 0.0383 0.698 7.334 6.506 520.643 0.829 28.940 5.668 0.38 143767. 0.5302
|
|
19.42 0.2136 0.4666 0.0843 0.0386 0.704 7.395 6.342 524.915 0.835 28.209 5.480 0.38 143954. 0.5061
|
|
21.85 0.2403 0.5074 0.0820 0.0388 0.708 7.433 6.163 527.668 0.840 27.412 5.297 0.38 144156. 0.4823
|
|
24.28 0.2670 0.5450 0.0794 0.0389 0.709 7.447 5.969 528.664 0.841 26.549 5.121 0.38 144372. 0.4588
|
|
26.70 0.2938 0.5795 0.0766 0.0388 0.708 7.433 5.759 527.670 0.840 25.615 4.950 0.38 144602. 0.4356
|
|
29.13 0.3205 0.6111 0.0736 0.0386 0.703 7.388 5.533 524.464 0.835 24.609 4.785 0.38 144846. 0.4127
|
|
31.56 0.3472 0.6399 0.0704 0.0382 0.696 7.309 5.290 518.846 0.826 23.531 4.625 0.38 145105. 0.3901
|
|
33.99 0.3739 0.6659 0.0669 0.0376 0.685 7.193 5.032 510.638 0.813 22.381 4.469 0.38 145379. 0.3677
|
|
36.42 0.4006 0.6893 0.0633 0.0368 0.670 7.039 4.757 499.695 0.795 21.158 4.318 0.38 145667. 0.3453
|
|
38.84 0.4273 0.7099 0.0594 0.0358 0.652 6.845 4.466 485.895 0.773 19.866 4.169 0.38 145970. 0.3231
|
|
41.27 0.4540 0.7277 0.0553 0.0345 0.629 6.609 4.160 469.133 0.747 18.505 4.022 0.38 146288. 0.3009
|
|
43.70 0.4807 0.7425 0.0511 0.0331 0.603 6.331 3.841 449.442 0.715 17.083 3.876 0.39 146620. 0.2786
|
|
46.13 0.5074 0.7539 0.0467 0.0314 0.573 6.015 3.510 426.965 0.680 15.611 3.728 0.39 146967. 0.2561
|
|
48.55 0.5341 0.7615 0.0422 0.0296 0.539 5.661 3.169 401.841 0.640 14.097 3.577 0.39 147329. 0.2336
|
|
50.98 0.5608 0.7644 0.0375 0.0275 0.502 5.271 2.822 374.199 0.596 12.551 3.420 0.39 147706. 0.2107
|
|
53.41 0.5875 0.7617 0.0328 0.0253 0.462 4.848 2.468 344.169 0.548 10.979 3.253 0.39 148097. 0.1874
|
|
55.84 0.6142 0.7515 0.0281 0.0229 0.418 4.394 2.111 311.887 0.496 9.390 3.070 0.39 148503. 0.1636
|
|
58.27 0.6409 0.7313 0.0233 0.0204 0.372 3.909 1.752 277.514 0.442 7.792 2.863 0.39 148923. 0.1390
|
|
60.69 0.6676 0.6964 0.0185 0.0177 0.324 3.398 1.392 241.239 0.384 6.192 2.617 0.39 149358. 0.1133
|
|
63.12 0.6943 0.6387 0.0138 0.0150 0.273 2.864 1.035 203.292 0.324 4.602 2.308 0.39 149807. 0.0861
|
|
65.55 0.7210 0.5416 0.0091 0.0121 0.220 2.310 0.681 163.950 0.261 3.031 1.885 0.39 150271. 0.0571
|
|
67.98 0.7477 0.3666 0.0045 0.0091 0.166 1.740 0.335 123.542 0.197 1.490 1.230 0.39 150749. 0.0261
|
|
70.40 0.7744 -0.0036 0.0000 0.0061 0.110 1.160 -0.002 82.349 0.131 -0.009 -0.012 0.39 151236. 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 0.0979 0.0343 0.993 8.937 10.019 740.108 1.010 44.564 6.140 0.44 166596. 0.7127
|
|
2.83 0.0267 0.0740 0.0968 0.0350 1.012 9.111 9.904 754.537 1.029 44.052 5.953 0.44 166717. 0.6871
|
|
5.67 0.0534 0.1433 0.0955 0.0356 1.031 9.283 9.777 768.797 1.049 43.487 5.768 0.44 166850. 0.6614
|
|
8.50 0.0801 0.2081 0.0942 0.0363 1.050 9.450 9.637 782.622 1.068 42.864 5.585 0.44 166996. 0.6358
|
|
11.33 0.1069 0.2686 0.0927 0.0369 1.067 9.608 9.482 795.741 1.086 42.177 5.405 0.44 167156. 0.6103
|
|
14.17 0.1336 0.3247 0.0910 0.0374 1.083 9.754 9.312 807.845 1.102 41.420 5.228 0.44 167330. 0.5851
|
|
17.00 0.1603 0.3768 0.0892 0.0379 1.098 9.884 9.125 818.605 1.117 40.589 5.056 0.44 167519. 0.5601
|
|
19.84 0.1870 0.4251 0.0872 0.0383 1.110 9.994 8.920 827.667 1.129 39.678 4.888 0.45 167723. 0.5354
|
|
22.67 0.2137 0.4696 0.0850 0.0387 1.119 10.078 8.696 834.659 1.139 38.682 4.726 0.45 167942. 0.5111
|
|
25.50 0.2404 0.5107 0.0826 0.0389 1.125 10.133 8.452 839.201 1.145 37.596 4.568 0.45 168178. 0.4871
|
|
28.34 0.2672 0.5486 0.0800 0.0390 1.128 10.154 8.187 840.909 1.147 36.417 4.416 0.45 168430. 0.4634
|
|
31.17 0.2939 0.5833 0.0772 0.0389 1.126 10.136 7.901 839.406 1.145 35.142 4.269 0.45 168699. 0.4401
|
|
34.00 0.3206 0.6152 0.0742 0.0387 1.119 10.074 7.591 834.332 1.138 33.767 4.127 0.45 168984. 0.4170
|
|
36.84 0.3473 0.6443 0.0709 0.0382 1.107 9.966 7.260 825.361 1.126 32.291 3.989 0.45 169287. 0.3942
|
|
39.67 0.3740 0.6706 0.0675 0.0376 1.089 9.807 6.905 812.209 1.108 30.715 3.856 0.45 169607. 0.3716
|
|
42.50 0.4007 0.6944 0.0638 0.0368 1.066 9.595 6.529 794.635 1.084 29.039 3.726 0.45 169944. 0.3492
|
|
45.34 0.4275 0.7154 0.0599 0.0358 1.036 9.327 6.130 772.445 1.054 27.267 3.600 0.45 170298. 0.3268
|
|
48.17 0.4542 0.7337 0.0558 0.0345 1.000 9.001 5.710 745.466 1.017 25.399 3.474 0.45 170670. 0.3045
|
|
51.00 0.4809 0.7490 0.0515 0.0331 0.957 8.618 5.272 713.750 0.974 23.448 3.350 0.45 171058. 0.2821
|
|
53.84 0.5076 0.7611 0.0471 0.0314 0.909 8.181 4.817 677.519 0.924 21.426 3.225 0.45 171464. 0.2596
|
|
56.67 0.5343 0.7695 0.0425 0.0295 0.854 7.692 4.350 636.999 0.869 19.348 3.097 0.45 171887. 0.2369
|
|
59.51 0.5610 0.7734 0.0378 0.0274 0.794 7.153 3.872 592.398 0.808 17.224 2.965 0.45 172327. 0.2139
|
|
62.34 0.5878 0.7718 0.0331 0.0252 0.729 6.568 3.387 543.923 0.742 15.064 2.824 0.45 172783. 0.1906
|
|
65.17 0.6145 0.7631 0.0283 0.0228 0.660 5.938 2.896 491.796 0.671 12.881 2.671 0.45 173257. 0.1667
|
|
68.01 0.6412 0.7445 0.0235 0.0202 0.585 5.268 2.402 436.278 0.595 10.684 2.497 0.45 173748. 0.1419
|
|
70.84 0.6679 0.7115 0.0186 0.0175 0.506 4.560 1.908 377.676 0.515 8.486 2.291 0.45 174256. 0.1161
|
|
73.67 0.6946 0.6558 0.0138 0.0147 0.424 3.820 1.416 316.365 0.432 6.300 2.031 0.45 174781. 0.0886
|
|
76.51 0.7213 0.5602 0.0091 0.0117 0.339 3.052 0.931 252.797 0.345 4.141 1.670 0.46 175323. 0.0591
|
|
79.34 0.7481 0.3830 0.0044 0.0087 0.251 2.264 0.455 187.509 0.256 2.025 1.101 0.46 175881. 0.0272
|
|
82.17 0.7748 -0.0109 -0.0001 0.0056 0.162 1.460 -0.008 120.940 0.165 -0.036 -0.030 0.46 176449. 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 0.0986 0.0344 1.485 11.699 13.175 1107.331 1.322 58.601 5.396 0.51 190385. 0.7183
|
|
3.24 0.0267 0.0742 0.0975 0.0351 1.514 11.931 13.027 1129.292 1.348 57.944 5.232 0.51 190524. 0.6925
|
|
6.47 0.0534 0.1438 0.0962 0.0357 1.544 12.161 12.863 1151.013 1.374 57.217 5.069 0.51 190676. 0.6667
|
|
9.71 0.0801 0.2089 0.0949 0.0364 1.572 12.384 12.683 1172.095 1.399 56.412 4.908 0.51 190843. 0.6410
|
|
12.94 0.1068 0.2695 0.0934 0.0370 1.599 12.595 12.483 1192.117 1.423 55.523 4.749 0.51 191026. 0.6154
|
|
16.18 0.1335 0.3259 0.0917 0.0376 1.623 12.791 12.262 1210.616 1.445 54.542 4.594 0.51 191225. 0.5900
|
|
19.42 0.1602 0.3782 0.0899 0.0381 1.646 12.965 12.020 1227.086 1.465 53.463 4.443 0.51 191440. 0.5649
|
|
22.65 0.1869 0.4266 0.0879 0.0385 1.664 13.111 11.753 1240.990 1.481 52.277 4.296 0.51 191673. 0.5401
|
|
25.89 0.2136 0.4713 0.0857 0.0389 1.679 13.225 11.461 1251.764 1.494 50.979 4.153 0.51 191925. 0.5156
|
|
29.12 0.2403 0.5126 0.0834 0.0391 1.688 13.300 11.143 1258.828 1.503 49.563 4.015 0.51 192194. 0.4915
|
|
32.36 0.2670 0.5506 0.0808 0.0392 1.692 13.329 10.796 1261.599 1.506 48.022 3.881 0.51 192482. 0.4677
|
|
35.60 0.2937 0.5856 0.0780 0.0391 1.689 13.307 10.421 1259.504 1.503 46.352 3.753 0.51 192790. 0.4443
|
|
38.83 0.3204 0.6177 0.0749 0.0389 1.679 13.228 10.016 1251.996 1.494 44.550 3.629 0.51 193117. 0.4211
|
|
42.07 0.3471 0.6470 0.0717 0.0384 1.661 13.086 9.581 1238.580 1.478 42.615 3.508 0.51 193463. 0.3983
|
|
45.30 0.3738 0.6737 0.0682 0.0378 1.634 12.877 9.115 1218.821 1.455 40.546 3.392 0.51 193828. 0.3756
|
|
48.54 0.4004 0.6978 0.0645 0.0370 1.599 12.598 8.620 1192.355 1.423 38.344 3.279 0.51 194213. 0.3531
|
|
51.78 0.4271 0.7193 0.0606 0.0360 1.554 12.244 8.096 1158.885 1.383 36.013 3.169 0.51 194618. 0.3307
|
|
55.01 0.4538 0.7380 0.0564 0.0347 1.499 11.814 7.544 1118.151 1.335 33.556 3.060 0.51 195043. 0.3083
|
|
58.25 0.4805 0.7539 0.0521 0.0332 1.435 11.307 6.967 1070.210 1.277 30.987 2.953 0.51 195487. 0.2858
|
|
61.48 0.5072 0.7667 0.0476 0.0315 1.362 10.728 6.368 1015.396 1.212 28.324 2.844 0.51 195950. 0.2632
|
|
64.72 0.5339 0.7759 0.0430 0.0296 1.279 10.080 5.752 954.050 1.139 25.585 2.735 0.52 196433. 0.2405
|
|
67.95 0.5606 0.7808 0.0383 0.0275 1.189 9.366 5.122 886.487 1.058 22.784 2.621 0.52 196935. 0.2175
|
|
71.19 0.5873 0.7804 0.0335 0.0252 1.090 8.590 4.482 813.021 0.970 19.935 2.500 0.52 197457. 0.1941
|
|
74.43 0.6140 0.7731 0.0287 0.0228 0.984 7.755 3.834 733.989 0.876 17.054 2.369 0.52 197998. 0.1701
|
|
77.66 0.6407 0.7563 0.0238 0.0202 0.871 6.865 3.182 649.786 0.776 14.154 2.221 0.52 198559. 0.1453
|
|
80.90 0.6674 0.7256 0.0189 0.0174 0.752 5.926 2.530 560.878 0.669 11.253 2.046 0.52 199138. 0.1193
|
|
84.13 0.6941 0.6726 0.0141 0.0145 0.627 4.943 1.881 467.835 0.558 8.366 1.824 0.52 199738. 0.0917
|
|
87.37 0.7208 0.5800 0.0093 0.0115 0.498 3.923 1.240 371.348 0.443 5.515 1.514 0.52 200356. 0.0618
|
|
90.61 0.7475 0.4046 0.0046 0.0085 0.365 2.876 0.611 272.235 0.325 2.720 1.019 0.52 200993. 0.0292
|
|
93.84 0.7742 -0.0007 0.0000 0.0053 0.230 1.809 -0.001 171.178 0.204 -0.003 -0.002 0.52 201642. 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 0.0993 0.0346 2.126 14.890 16.805 1585.493 1.682 74.748 4.807 0.57 214170. 0.7227
|
|
3.64 0.0267 0.0744 0.0983 0.0353 2.169 15.190 16.622 1617.472 1.716 73.933 4.661 0.57 214326. 0.6969
|
|
7.28 0.0534 0.1441 0.0971 0.0360 2.212 15.488 16.418 1649.133 1.750 73.028 4.516 0.57 214497. 0.6710
|
|
10.92 0.0801 0.2093 0.0957 0.0366 2.253 15.776 16.192 1679.886 1.782 72.024 4.372 0.57 214685. 0.6452
|
|
14.56 0.1068 0.2701 0.0942 0.0373 2.292 16.051 15.942 1709.129 1.813 70.912 4.231 0.57 214891. 0.6195
|
|
18.20 0.1335 0.3266 0.0926 0.0378 2.328 16.305 15.666 1736.173 1.842 69.682 4.093 0.57 215115. 0.5941
|
|
21.84 0.1602 0.3790 0.0908 0.0384 2.361 16.532 15.361 1760.285 1.868 68.324 3.958 0.57 215358. 0.5689
|
|
25.48 0.1869 0.4275 0.0888 0.0388 2.388 16.723 15.025 1780.678 1.889 66.830 3.827 0.57 215621. 0.5440
|
|
29.12 0.2136 0.4724 0.0866 0.0392 2.409 16.872 14.656 1796.530 1.906 65.190 3.700 0.57 215904. 0.5195
|
|
32.76 0.2402 0.5138 0.0843 0.0394 2.423 16.970 14.253 1806.997 1.917 63.397 3.578 0.57 216208. 0.4953
|
|
36.40 0.2669 0.5520 0.0817 0.0395 2.429 17.010 13.814 1811.227 1.922 61.443 3.459 0.57 216533. 0.4715
|
|
40.04 0.2936 0.5872 0.0788 0.0394 2.425 16.983 13.337 1808.386 1.919 59.323 3.345 0.57 216880. 0.4480
|
|
43.68 0.3203 0.6195 0.0758 0.0392 2.411 16.883 12.822 1797.682 1.907 57.031 3.235 0.57 217248. 0.4248
|
|
47.32 0.3470 0.6491 0.0725 0.0388 2.385 16.702 12.268 1778.390 1.887 54.566 3.129 0.57 217638. 0.4019
|
|
50.96 0.3737 0.6760 0.0690 0.0381 2.347 16.434 11.674 1749.878 1.857 51.927 3.026 0.58 218050. 0.3792
|
|
54.60 0.4004 0.7005 0.0653 0.0373 2.295 16.074 11.043 1711.621 1.816 49.117 2.926 0.58 218484. 0.3566
|
|
58.24 0.4271 0.7223 0.0613 0.0363 2.230 15.620 10.373 1663.188 1.765 46.140 2.829 0.58 218940. 0.3341
|
|
61.88 0.4538 0.7415 0.0571 0.0350 2.151 15.066 9.667 1604.200 1.702 42.999 2.733 0.58 219418. 0.3117
|
|
65.52 0.4805 0.7579 0.0528 0.0335 2.058 14.413 8.928 1534.729 1.628 39.712 2.639 0.58 219918. 0.2891
|
|
69.16 0.5072 0.7713 0.0482 0.0317 1.952 13.667 8.162 1455.250 1.544 36.303 2.544 0.58 220440. 0.2665
|
|
72.80 0.5339 0.7812 0.0436 0.0298 1.832 12.831 7.373 1366.259 1.450 32.794 2.448 0.58 220984. 0.2437
|
|
76.44 0.5606 0.7869 0.0388 0.0276 1.701 11.910 6.566 1268.214 1.346 29.205 2.348 0.58 221549. 0.2207
|
|
80.08 0.5873 0.7876 0.0340 0.0253 1.558 10.909 5.745 1161.571 1.232 25.553 2.243 0.58 222137. 0.1972
|
|
83.72 0.6140 0.7815 0.0290 0.0228 1.404 9.831 4.914 1046.823 1.111 21.858 2.129 0.58 222746. 0.1731
|
|
87.36 0.6407 0.7662 0.0241 0.0202 1.240 8.683 4.078 924.543 0.981 18.139 2.001 0.58 223376. 0.1482
|
|
91.00 0.6674 0.7373 0.0192 0.0173 1.067 7.470 3.241 795.414 0.844 14.415 1.848 0.58 224029. 0.1220
|
|
94.64 0.6940 0.6863 0.0142 0.0144 0.885 6.201 2.408 660.268 0.701 10.711 1.654 0.58 224703. 0.0941
|
|
98.28 0.7207 0.5956 0.0094 0.0113 0.697 4.885 1.585 520.114 0.552 7.051 1.382 0.59 225399. 0.0638
|
|
101.92 0.7474 0.4194 0.0046 0.0082 0.504 3.533 0.779 376.153 0.399 3.463 0.939 0.59 226116. 0.0304
|
|
105.56 0.7741 -0.0067 0.0000 0.0050 0.308 2.154 -0.007 229.353 0.243 -0.033 -0.014 0.59 226844. 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 0.1002 0.0349 2.942 18.545 20.932 2194.058 2.095 93.106 4.327 0.63 237949. 0.7260
|
|
4.04 0.0267 0.0744 0.0992 0.0356 3.003 18.925 20.712 2239.039 2.138 92.126 4.196 0.63 238122. 0.7003
|
|
8.09 0.0534 0.1441 0.0980 0.0363 3.062 19.302 20.466 2283.620 2.181 91.034 4.065 0.63 238313. 0.6744
|
|
12.13 0.0800 0.2093 0.0967 0.0370 3.121 19.668 20.193 2326.989 2.222 89.819 3.936 0.63 238522. 0.6486
|
|
16.17 0.1067 0.2700 0.0952 0.0376 3.176 20.017 19.890 2368.267 2.262 88.469 3.809 0.64 238751. 0.6230
|
|
20.21 0.1334 0.3266 0.0936 0.0382 3.227 20.340 19.553 2406.497 2.298 86.970 3.685 0.64 239000. 0.5976
|
|
24.26 0.1601 0.3790 0.0918 0.0388 3.273 20.629 19.179 2440.637 2.331 85.310 3.564 0.64 239271. 0.5724
|
|
28.30 0.1868 0.4276 0.0899 0.0392 3.312 20.873 18.767 2469.572 2.358 83.477 3.447 0.64 239563. 0.5476
|
|
32.34 0.2134 0.4726 0.0877 0.0396 3.342 21.064 18.314 2492.145 2.380 81.461 3.333 0.64 239879. 0.5231
|
|
36.38 0.2401 0.5141 0.0853 0.0398 3.362 21.191 17.817 2507.165 2.394 79.250 3.223 0.64 240217. 0.4989
|
|
40.43 0.2668 0.5525 0.0827 0.0399 3.371 21.244 17.274 2513.435 2.400 76.835 3.117 0.64 240578. 0.4751
|
|
44.47 0.2935 0.5878 0.0799 0.0399 3.366 21.213 16.684 2509.782 2.397 74.209 3.015 0.64 240964. 0.4516
|
|
48.51 0.3202 0.6203 0.0768 0.0397 3.346 21.089 16.045 2495.091 2.383 71.366 2.917 0.64 241374. 0.4284
|
|
52.55 0.3469 0.6501 0.0735 0.0392 3.310 20.863 15.356 2468.348 2.357 68.303 2.822 0.64 241808. 0.4055
|
|
56.60 0.3735 0.6774 0.0700 0.0386 3.257 20.528 14.618 2428.668 2.319 65.020 2.730 0.64 242266. 0.3828
|
|
60.64 0.4002 0.7021 0.0662 0.0377 3.185 20.077 13.831 2375.313 2.268 61.520 2.641 0.64 242749. 0.3602
|
|
64.68 0.4269 0.7243 0.0622 0.0367 3.095 19.505 12.996 2307.685 2.204 57.807 2.554 0.64 243256. 0.3377
|
|
68.72 0.4536 0.7440 0.0580 0.0354 2.984 18.808 12.115 2225.256 2.125 53.886 2.469 0.64 243788. 0.3152
|
|
72.77 0.4803 0.7609 0.0536 0.0338 2.854 17.987 11.191 2128.099 2.032 49.779 2.385 0.64 244344. 0.2926
|
|
76.81 0.5069 0.7749 0.0490 0.0321 2.705 17.047 10.233 2016.872 1.926 45.516 2.301 0.64 244924. 0.2700
|
|
80.85 0.5336 0.7855 0.0443 0.0301 2.538 15.994 9.246 1892.272 1.807 41.125 2.216 0.64 245528. 0.2471
|
|
84.89 0.5603 0.7921 0.0394 0.0279 2.353 14.833 8.235 1754.945 1.676 36.630 2.128 0.64 246157. 0.2240
|
|
88.94 0.5870 0.7938 0.0345 0.0255 2.153 13.570 7.207 1605.530 1.533 32.055 2.036 0.65 246809. 0.2004
|
|
92.98 0.6137 0.7890 0.0295 0.0230 1.937 12.211 6.165 1444.722 1.380 27.424 1.936 0.65 247486. 0.1763
|
|
97.02 0.6403 0.7752 0.0245 0.0202 1.708 10.762 5.117 1273.325 1.216 22.759 1.823 0.65 248187. 0.1512
|
|
101.06 0.6670 0.7481 0.0195 0.0174 1.465 9.232 4.066 1092.302 1.043 18.087 1.689 0.65 248911. 0.1249
|
|
105.11 0.6937 0.6994 0.0145 0.0143 1.211 7.631 3.021 902.818 0.862 13.438 1.518 0.65 249660. 0.0967
|
|
109.15 0.7204 0.6109 0.0095 0.0112 0.947 5.970 1.988 706.302 0.674 8.843 1.277 0.65 250433. 0.0660
|
|
113.19 0.7471 0.4351 0.0047 0.0080 0.676 4.264 0.975 504.453 0.482 4.338 0.877 0.65 251229. 0.0318
|
|
117.24 0.7738 -0.0091 -0.0001 0.0047 0.400 2.524 -0.012 298.625 0.285 -0.052 -0.018 0.65 252036. 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 0.1012 0.0354 3.973 22.762 25.584 2962.320 2.572 113.796 3.917 0.70 261721. 0.7266
|
|
4.48 0.0269 0.0747 0.1002 0.0361 4.054 23.228 25.324 3023.019 2.624 112.643 3.800 0.70 261913. 0.7012
|
|
8.96 0.0538 0.1447 0.0991 0.0368 4.135 23.692 25.034 3083.406 2.677 111.351 3.682 0.70 262125. 0.6757
|
|
13.45 0.0807 0.2102 0.0978 0.0375 4.214 24.145 24.709 3142.357 2.728 109.904 3.566 0.70 262358. 0.6501
|
|
17.93 0.1076 0.2713 0.0963 0.0382 4.289 24.578 24.345 3198.661 2.777 108.287 3.452 0.70 262613. 0.6247
|
|
22.41 0.1345 0.3281 0.0947 0.0388 4.360 24.980 23.940 3250.956 2.822 106.483 3.340 0.70 262891. 0.5993
|
|
26.89 0.1614 0.3809 0.0929 0.0394 4.422 25.339 23.488 3297.748 2.863 104.476 3.231 0.70 263192. 0.5742
|
|
31.37 0.1882 0.4297 0.0910 0.0399 4.476 25.644 22.988 3337.433 2.897 102.249 3.124 0.70 263519. 0.5493
|
|
35.86 0.2151 0.4749 0.0888 0.0402 4.517 25.882 22.435 3368.325 2.924 99.789 3.021 0.70 263871. 0.5247
|
|
40.34 0.2420 0.5166 0.0864 0.0405 4.544 26.038 21.826 3388.686 2.942 97.080 2.921 0.70 264248. 0.5005
|
|
44.82 0.2689 0.5551 0.0837 0.0406 4.555 26.100 21.158 3396.784 2.949 94.113 2.825 0.70 264653. 0.4766
|
|
49.30 0.2958 0.5907 0.0808 0.0405 4.547 26.056 20.431 3390.949 2.944 90.876 2.733 0.70 265084. 0.4530
|
|
53.78 0.3227 0.6234 0.0777 0.0402 4.519 25.892 19.641 3369.623 2.925 87.362 2.644 0.70 265542. 0.4297
|
|
58.27 0.3496 0.6534 0.0743 0.0398 4.467 25.598 18.788 3331.403 2.892 83.569 2.558 0.70 266027. 0.4066
|
|
62.75 0.3765 0.6809 0.0707 0.0391 4.392 25.165 17.872 3275.077 2.843 79.496 2.475 0.70 266539. 0.3837
|
|
67.23 0.4034 0.7059 0.0669 0.0382 4.291 24.586 16.895 3199.642 2.778 75.147 2.395 0.70 267079. 0.3610
|
|
71.71 0.4303 0.7283 0.0627 0.0371 4.163 23.853 15.856 3104.285 2.695 70.528 2.317 0.70 267646. 0.3383
|
|
76.19 0.4572 0.7483 0.0584 0.0357 4.007 22.962 14.759 2988.323 2.594 65.647 2.240 0.71 268240. 0.3156
|
|
80.68 0.4841 0.7655 0.0539 0.0341 3.825 21.914 13.609 2851.972 2.476 60.533 2.164 0.71 268861. 0.2928
|
|
85.16 0.5109 0.7797 0.0491 0.0322 3.616 20.717 12.416 2696.190 2.341 55.224 2.089 0.71 269510. 0.2699
|
|
89.64 0.5378 0.7906 0.0443 0.0301 3.382 19.378 11.186 2521.941 2.189 49.756 2.012 0.71 270185. 0.2468
|
|
94.12 0.5647 0.7974 0.0393 0.0278 3.125 17.904 9.928 2330.131 2.023 44.159 1.932 0.71 270887. 0.2233
|
|
98.60 0.5916 0.7991 0.0342 0.0253 2.845 16.303 8.647 2121.671 1.842 38.462 1.849 0.71 271615. 0.1994
|
|
103.08 0.6185 0.7940 0.0291 0.0227 2.545 14.581 7.351 1897.582 1.647 32.697 1.757 0.71 272371. 0.1747
|
|
107.57 0.6454 0.7794 0.0239 0.0198 2.225 12.748 6.046 1659.079 1.440 26.892 1.653 0.71 273153. 0.1490
|
|
112.05 0.6723 0.7502 0.0188 0.0168 1.888 10.816 4.740 1407.643 1.222 21.083 1.527 0.71 273962. 0.1219
|
|
116.53 0.6992 0.6963 0.0136 0.0137 1.536 8.799 3.441 1145.116 0.994 15.307 1.363 0.72 274798. 0.0927
|
|
121.01 0.7261 0.5947 0.0085 0.0104 1.172 6.714 2.160 873.786 0.759 9.606 1.121 0.72 275660. 0.0604
|
|
125.49 0.7530 0.3787 0.0036 0.0071 0.800 4.583 0.905 596.395 0.518 4.026 0.688 0.72 276548. 0.0240
|
|
129.98 0.7799
|
|
|
|
|
|
|
|
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 0.1024 0.0367 5.355 28.125 30.785 3992.995 3.178 136.934 3.497 0.76 285485. 0.7116
|
|
4.84 0.0266 0.0722 0.1014 0.0374 5.452 28.636 30.495 4065.565 3.235 135.642 3.402 0.76 285692. 0.6890
|
|
9.68 0.0533 0.1404 0.1003 0.0381 5.549 29.143 30.168 4137.615 3.293 134.188 3.307 0.76 285921. 0.6661
|
|
14.52 0.0799 0.2045 0.0991 0.0387 5.643 29.638 29.800 4207.799 3.348 132.552 3.212 0.76 286172. 0.6431
|
|
19.36 0.1065 0.2647 0.0977 0.0393 5.732 30.109 29.387 4274.675 3.402 130.714 3.118 0.76 286447. 0.6199
|
|
24.21 0.1331 0.3210 0.0962 0.0399 5.816 30.545 28.924 4336.636 3.451 128.653 3.025 0.76 286747. 0.5967
|
|
29.05 0.1598 0.3736 0.0945 0.0404 5.890 30.935 28.406 4391.910 3.495 126.349 2.934 0.76 287072. 0.5734
|
|
33.89 0.1864 0.4225 0.0925 0.0408 5.952 31.263 27.829 4438.587 3.532 123.782 2.844 0.76 287424. 0.5501
|
|
38.73 0.2130 0.4679 0.0904 0.0412 6.001 31.517 27.188 4474.632 3.561 120.932 2.756 0.76 287803. 0.5270
|
|
43.57 0.2396 0.5101 0.0880 0.0414 6.032 31.681 26.480 4497.927 3.579 117.783 2.670 0.76 288210. 0.5039
|
|
48.41 0.2663 0.5490 0.0855 0.0414 6.043 31.740 25.701 4506.310 3.586 114.319 2.587 0.76 288645. 0.4810
|
|
53.25 0.2929 0.5850 0.0826 0.0414 6.031 31.679 24.849 4497.604 3.579 110.529 2.506 0.76 289109. 0.4581
|
|
58.09 0.3195 0.6182 0.0795 0.0411 5.994 31.483 23.922 4469.703 3.557 106.403 2.427 0.77 289602. 0.4354
|
|
62.94 0.3461 0.6488 0.0762 0.0407 5.928 31.137 22.917 4420.627 3.518 101.936 2.351 0.77 290124. 0.4128
|
|
67.78 0.3728 0.6767 0.0726 0.0400 5.832 30.630 21.836 4348.602 3.461 97.128 2.278 0.77 290676. 0.3903
|
|
72.62 0.3994 0.7023 0.0688 0.0391 5.702 29.950 20.680 4252.109 3.384 91.983 2.206 0.77 291256. 0.3679
|
|
77.46 0.4260 0.7253 0.0647 0.0380 5.538 29.089 19.449 4129.889 3.286 86.509 2.136 0.77 291866. 0.3455
|
|
82.30 0.4527 0.7460 0.0603 0.0366 5.338 28.039 18.146 3980.845 3.168 80.714 2.068 0.77 292505. 0.3230
|
|
87.14 0.4793 0.7640 0.0558 0.0350 5.102 26.800 16.778 3804.927 3.028 74.627 2.000 0.77 293172. 0.3004
|
|
91.98 0.5059 0.7793 0.0511 0.0331 4.832 25.380 15.353 3603.324 2.867 68.292 1.933 0.77 293869. 0.2777
|
|
96.82 0.5325 0.7914 0.0462 0.0311 4.529 23.789 13.883 3377.427 2.688 61.752 1.864 0.77 294594. 0.2548
|
|
101.67 0.5592 0.7997 0.0411 0.0288 4.195 22.036 12.376 3128.578 2.490 55.046 1.794 0.77 295347. 0.2315
|
|
106.51 0.5858 0.8031 0.0360 0.0263 3.833 20.132 10.838 2858.159 2.274 48.209 1.720 0.77 296129. 0.2077
|
|
111.35 0.6124 0.8001 0.0309 0.0236 3.443 18.086 9.279 2567.753 2.043 41.274 1.639 0.78 296940. 0.1831
|
|
116.19 0.6390 0.7881 0.0256 0.0208 3.030 15.913 7.707 2259.245 1.798 34.279 1.547 0.78 297779. 0.1575
|
|
121.03 0.6657 0.7623 0.0204 0.0178 2.595 13.629 6.129 1934.950 1.540 27.263 1.437 0.78 298647. 0.1304
|
|
125.87 0.6923 0.7138 0.0152 0.0147 2.143 11.254 4.557 1597.714 1.271 20.268 1.294 0.78 299543. 0.1013
|
|
130.71 0.7189 0.6233 0.0100 0.0115 1.678 8.812 3.000 1251.008 0.996 13.343 1.088 0.78 300467. 0.0691
|
|
135.55 0.7455 0.4411 0.0049 0.0083 1.205 6.332 1.471 898.915 0.715 6.543 0.742 0.78 301419. 0.0330
|
|
140.40 0.7722 -0.0108 -0.0001 0.0050 0.731 3.837 -0.021 544.783 0.434 -0.094 -0.018 0.78 302385. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 13000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1036 0.0401 7.439 36.066 36.551 5547.083 4.075 162.577 2.989 0.83 309238. 0.6626
|
|
5.24 0.0266 0.0671 0.1027 0.0407 7.543 36.572 36.234 5624.915 4.132 161.169 2.922 0.83 309462. 0.6450
|
|
10.48 0.0532 0.1311 0.1016 0.0412 7.645 37.064 35.875 5700.615 4.187 159.571 2.854 0.83 309709. 0.6270
|
|
15.71 0.0798 0.1920 0.1005 0.0418 7.741 37.531 35.468 5772.479 4.240 157.760 2.787 0.83 309981. 0.6087
|
|
20.95 0.1064 0.2498 0.0992 0.0422 7.830 37.962 35.006 5838.697 4.289 155.708 2.719 0.83 310278. 0.5901
|
|
26.19 0.1330 0.3045 0.0977 0.0427 7.908 38.343 34.485 5897.329 4.332 153.390 2.652 0.83 310603. 0.5712
|
|
31.43 0.1595 0.3562 0.0960 0.0430 7.974 38.661 33.898 5946.327 4.368 150.779 2.586 0.83 310956. 0.5521
|
|
36.66 0.1861 0.4050 0.0942 0.0433 8.024 38.903 33.239 5983.522 4.395 147.849 2.520 0.83 311337. 0.5327
|
|
41.90 0.2127 0.4508 0.0921 0.0435 8.055 39.054 32.504 6006.646 4.412 144.576 2.454 0.83 311748. 0.5132
|
|
47.14 0.2393 0.4939 0.0898 0.0435 8.064 39.097 31.685 6013.368 4.417 140.937 2.390 0.83 312190. 0.4934
|
|
52.38 0.2659 0.5342 0.0872 0.0434 8.048 39.019 30.781 6001.283 4.408 136.912 2.326 0.83 312662. 0.4733
|
|
57.61 0.2925 0.5718 0.0844 0.0432 8.003 38.802 29.785 5968.020 4.384 132.486 2.264 0.83 313166. 0.4531
|
|
62.85 0.3191 0.6067 0.0813 0.0428 7.927 38.434 28.697 5911.292 4.342 127.645 2.202 0.83 313701. 0.4326
|
|
68.09 0.3457 0.6391 0.0780 0.0422 7.817 37.898 27.515 5828.914 4.282 122.385 2.141 0.83 314268. 0.4119
|
|
73.33 0.3723 0.6689 0.0743 0.0414 7.669 37.183 26.237 5718.883 4.201 116.702 2.081 0.83 314866. 0.3909
|
|
78.56 0.3989 0.6962 0.0704 0.0404 7.482 36.276 24.866 5579.408 4.098 110.604 2.021 0.83 315495. 0.3697
|
|
83.80 0.4255 0.7210 0.0663 0.0391 7.253 35.167 23.404 5408.926 3.973 104.099 1.963 0.83 316157. 0.3482
|
|
89.04 0.4520 0.7431 0.0619 0.0377 6.982 33.851 21.852 5206.506 3.824 97.198 1.904 0.83 316849. 0.3263
|
|
94.28 0.4786 0.7622 0.0573 0.0360 6.668 32.330 20.219 4972.592 3.653 89.933 1.844 0.83 317573. 0.3041
|
|
99.51 0.5052 0.7781 0.0525 0.0341 6.314 30.614 18.516 4708.523 3.459 82.357 1.784 0.84 318327. 0.2815
|
|
104.75 0.5318 0.7903 0.0475 0.0319 5.922 28.711 16.754 4415.923 3.244 74.524 1.721 0.84 319113. 0.2583
|
|
109.99 0.5584 0.7979 0.0423 0.0296 5.493 26.634 14.946 4096.418 3.009 66.479 1.655 0.84 319929. 0.2346
|
|
115.23 0.5850 0.8000 0.0371 0.0271 5.031 24.392 13.099 3751.610 2.756 58.265 1.584 0.84 320776. 0.2102
|
|
120.46 0.6116 0.7944 0.0318 0.0245 4.538 22.003 11.224 3384.155 2.486 49.924 1.504 0.84 321653. 0.1848
|
|
125.70 0.6382 0.7780 0.0264 0.0217 4.020 19.489 9.330 2997.533 2.202 41.501 1.412 0.84 322561. 0.1581
|
|
130.94 0.6648 0.7450 0.0210 0.0188 3.481 16.878 7.428 2595.945 1.907 33.042 1.298 0.84 323499. 0.1297
|
|
136.18 0.6914 0.6857 0.0157 0.0158 2.929 14.200 5.531 2184.023 1.604 24.600 1.149 0.84 324468. 0.0991
|
|
141.41 0.7180 0.5808 0.0103 0.0128 2.370 11.490 3.650 1767.151 1.298 16.234 0.937 0.85 325468. 0.0656
|
|
146.65 0.7445 0.3886 0.0051 0.0098 1.812 8.786 1.801 1351.375 0.993 8.010 0.604 0.85 326497. 0.0297
|
|
151.89 0.7711 -0.0015 0.0000 0.0068 1.262 6.119 -0.005 941.184 0.691 -0.020 -0.002 0.85 327545. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 14000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1043 0.0462 10.689 48.121 42.697 7970.520 5.437 189.915 2.430 0.89 332998. 0.5822
|
|
5.66 0.0267 0.0592 0.1035 0.0467 10.804 48.639 42.372 8056.315 5.495 188.470 2.386 0.89 333237. 0.5695
|
|
11.32 0.0534 0.1162 0.1026 0.0471 10.910 49.119 41.999 8135.884 5.549 186.810 2.341 0.89 333502. 0.5565
|
|
16.98 0.0800 0.1710 0.1016 0.0475 11.005 49.545 41.570 8206.479 5.598 184.904 2.298 0.89 333794. 0.5433
|
|
22.63 0.1067 0.2237 0.1004 0.0479 11.084 49.900 41.079 8265.298 5.638 182.718 2.254 0.89 334115. 0.5299
|
|
28.29 0.1334 0.2743 0.0990 0.0481 11.143 50.167 40.516 8309.496 5.668 180.215 2.212 0.89 334464. 0.5162
|
|
33.95 0.1601 0.3229 0.0974 0.0483 11.179 50.329 39.874 8336.304 5.686 177.360 2.170 0.89 334845. 0.5024
|
|
39.61 0.1867 0.3696 0.0956 0.0483 11.188 50.370 39.145 8343.070 5.691 174.119 2.128 0.89 335258. 0.4883
|
|
45.27 0.2134 0.4142 0.0936 0.0482 11.167 50.275 38.323 8327.354 5.680 170.459 2.087 0.89 335703. 0.4739
|
|
50.93 0.2401 0.4570 0.0914 0.0480 11.113 50.031 37.399 8286.904 5.652 166.352 2.047 0.89 336182. 0.4591
|
|
56.59 0.2668 0.4979 0.0888 0.0476 11.023 49.624 36.369 8219.593 5.607 161.771 2.007 0.89 336695. 0.4439
|
|
62.24 0.2934 0.5367 0.0861 0.0470 10.894 49.044 35.228 8123.492 5.541 156.696 1.967 0.89 337241. 0.4281
|
|
67.90 0.3201 0.5736 0.0830 0.0463 10.723 48.277 33.972 7996.396 5.454 151.107 1.927 0.89 337823. 0.4119
|
|
73.56 0.3468 0.6084 0.0796 0.0454 10.509 47.314 32.599 7836.916 5.346 144.998 1.887 0.89 338438. 0.3950
|
|
79.22 0.3735 0.6411 0.0760 0.0443 10.250 46.146 31.108 7643.528 5.214 138.367 1.846 0.89 339088. 0.3776
|
|
84.88 0.4001 0.6715 0.0721 0.0429 9.943 44.765 29.501 7414.762 5.058 131.219 1.805 0.90 339773. 0.3595
|
|
90.54 0.4268 0.6995 0.0679 0.0414 9.587 43.163 27.780 7149.293 4.876 123.567 1.762 0.90 340491. 0.3407
|
|
96.20 0.4535 0.7251 0.0634 0.0396 9.181 41.331 25.949 6845.900 4.670 115.423 1.719 0.90 341244. 0.3212
|
|
101.86 0.4802 0.7472 0.0587 0.0377 8.729 39.300 24.017 6509.558 4.440 106.826 1.673 0.90 342030. 0.3008
|
|
107.51 0.5069 0.7654 0.0537 0.0356 8.239 37.094 21.997 6144.084 4.191 97.843 1.624 0.90 342850. 0.2793
|
|
113.17 0.5335 0.7786 0.0486 0.0333 7.715 34.732 19.905 5752.959 3.924 88.538 1.569 0.90 343702. 0.2568
|
|
118.83 0.5602 0.7845 0.0434 0.0310 7.171 32.282 17.752 5347.117 3.647 78.961 1.506 0.90 344588. 0.2327
|
|
124.49 0.5869 0.7806 0.0380 0.0286 6.613 29.770 15.550 4930.969 3.363 69.165 1.430 0.90 345507. 0.2068
|
|
130.15 0.6136 0.7665 0.0325 0.0260 6.028 27.137 13.312 4494.872 3.066 59.213 1.343 0.91 346459. 0.1797
|
|
135.81 0.6402 0.7380 0.0270 0.0234 5.423 24.416 11.053 4044.230 2.759 49.164 1.240 0.91 347444. 0.1511
|
|
141.47 0.6669 0.6892 0.0215 0.0208 4.809 21.648 8.786 3585.732 2.446 39.079 1.111 0.91 348461. 0.1208
|
|
147.12 0.6936 0.6106 0.0159 0.0181 4.193 18.876 6.526 3126.620 2.133 29.026 0.947 0.91 349512. 0.0887
|
|
152.78 0.7203 0.4876 0.0105 0.0155 3.586 16.143 4.291 2673.858 1.824 19.088 0.728 0.91 350595. 0.0553
|
|
158.44 0.7469 0.2965 0.0051 0.0129 2.997 13.492 2.103 2234.715 1.524 9.353 0.427 0.91 351710. 0.0227
|
|
164.10 0.7736 -0.0048 -0.0001 0.0105 2.428 10.933 -0.027 1810.906 1.235 -0.119 -0.007 0.92 352851. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 15000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1029 0.0517 14.733 61.907 48.356 10986.488 6.994 215.088 1.996 0.95 356826. 0.5091
|
|
6.21 0.0273 0.0534 0.1022 0.0523 14.905 62.629 48.049 11114.604 7.076 213.722 1.961 0.95 357082. 0.4984
|
|
12.42 0.0546 0.1048 0.1015 0.0529 15.070 63.322 47.693 11237.619 7.154 212.138 1.925 0.95 357367. 0.4875
|
|
18.62 0.0819 0.1543 0.1006 0.0535 15.222 63.961 47.279 11351.011 7.226 210.297 1.889 0.95 357682. 0.4764
|
|
24.83 0.1093 0.2018 0.0996 0.0539 15.354 64.517 46.797 11449.688 7.289 208.154 1.854 0.95 358029. 0.4651
|
|
31.04 0.1366 0.2476 0.0984 0.0543 15.459 64.958 46.236 11527.944 7.339 205.658 1.819 0.95 358409. 0.4536
|
|
37.25 0.1639 0.2916 0.0970 0.0545 15.529 65.249 45.584 11579.642 7.372 202.758 1.786 0.95 358825. 0.4421
|
|
43.46 0.1912 0.3340 0.0954 0.0546 15.554 65.355 44.829 11598.464 7.384 199.400 1.753 0.95 359276. 0.4305
|
|
49.67 0.2185 0.3749 0.0935 0.0545 15.527 65.242 43.959 11578.357 7.371 195.530 1.722 0.95 359766. 0.4187
|
|
55.87 0.2458 0.4146 0.0914 0.0542 15.440 64.879 42.963 11513.896 7.330 191.099 1.692 0.95 360294. 0.4068
|
|
62.08 0.2732 0.4529 0.0890 0.0537 15.289 64.241 41.831 11400.644 7.258 186.062 1.664 0.96 360860. 0.3947
|
|
68.29 0.3005 0.4901 0.0863 0.0529 15.067 63.310 40.554 11235.457 7.153 180.382 1.637 0.96 361467. 0.3823
|
|
74.50 0.3278 0.5261 0.0833 0.0519 14.773 62.075 39.126 11016.313 7.013 174.032 1.611 0.96 362113. 0.3695
|
|
80.71 0.3551 0.5609 0.0799 0.0506 14.406 60.531 37.544 10742.258 6.839 166.994 1.585 0.96 362799. 0.3562
|
|
86.92 0.3824 0.5943 0.0762 0.0490 13.964 58.677 35.806 10413.283 6.629 159.264 1.560 0.96 363525. 0.3422
|
|
93.12 0.4097 0.6261 0.0722 0.0472 13.451 56.519 33.915 10030.350 6.386 150.852 1.534 0.96 364289. 0.3275
|
|
99.33 0.4371 0.6561 0.0678 0.0452 12.867 54.066 31.874 9594.975 6.108 141.777 1.507 0.96 365093. 0.3120
|
|
105.54 0.4644 0.6841 0.0632 0.0429 12.215 51.327 29.691 9108.851 5.799 132.067 1.478 0.96 365935. 0.2954
|
|
111.75 0.4917 0.7092 0.0583 0.0404 11.505 48.342 27.381 8579.057 5.462 121.792 1.448 0.96 366815. 0.2778
|
|
117.96 0.5190 0.7294 0.0531 0.0378 10.764 45.230 24.962 8026.836 5.110 111.032 1.411 0.96 367732. 0.2584
|
|
124.17 0.5463 0.7432 0.0478 0.0351 10.003 42.032 22.454 7459.365 4.749 99.875 1.365 0.97 368687. 0.2373
|
|
130.37 0.5736 0.7464 0.0423 0.0325 9.255 38.887 19.871 6901.235 4.393 88.385 1.306 0.97 369679. 0.2135
|
|
136.58 0.6010 0.7274 0.0366 0.0303 8.620 36.220 17.217 6427.898 4.092 76.581 1.215 0.97 370707. 0.1849
|
|
142.79 0.6283 0.6934 0.0309 0.0280 7.978 33.523 14.530 5949.285 3.787 64.628 1.108 0.97 371772. 0.1548
|
|
149.00 0.6556 0.6408 0.0252 0.0258 7.337 30.829 11.833 5471.091 3.483 52.632 0.981 0.97 372874. 0.1237
|
|
155.21 0.6829 0.5647 0.0195 0.0236 6.707 28.182 9.151 5001.478 3.184 40.703 0.830 0.97 374012. 0.0921
|
|
161.41 0.7102 0.4596 0.0139 0.0214 6.099 25.626 6.513 4547.779 2.895 28.969 0.650 0.98 375188. 0.0608
|
|
167.62 0.7375 0.3197 0.0084 0.0194 5.521 23.198 3.949 4116.947 2.621 17.563 0.435 0.98 376401. 0.0317
|
|
173.83 0.7649 0.1379 0.0032 0.0175 4.977 20.912 1.481 3711.152 2.363 6.586 0.181 0.98 377659. 0.0081
|
|
180.04 0.7922
|
|
|
|
|
|
|