464 lines
82 KiB
Plaintext
464 lines
82 KiB
Plaintext
20x11E (20x11E.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 0.0874 0.0331 0.009 0.537 0.446 6.357 0.061 1.983 31.812 0.08 36675. 0.6232
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0.45 0.0240 0.0617 0.0861 0.0335 0.009 0.544 0.439 6.433 0.061 1.953 30.958 0.08 36698. 0.6018
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0.91 0.0480 0.1200 0.0847 0.0339 0.009 0.550 0.432 6.505 0.062 1.921 30.107 0.08 36723. 0.5804
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1.36 0.0720 0.1750 0.0831 0.0342 0.009 0.555 0.424 6.570 0.063 1.885 29.263 0.08 36751. 0.5589
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1.82 0.0960 0.2266 0.0815 0.0345 0.009 0.560 0.415 6.627 0.063 1.847 28.426 0.08 36780. 0.5375
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2.27 0.1200 0.2750 0.0797 0.0348 0.009 0.564 0.406 6.675 0.064 1.807 27.598 0.08 36812. 0.5160
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2.73 0.1440 0.3203 0.0777 0.0350 0.009 0.567 0.396 6.712 0.064 1.763 26.781 0.08 36847. 0.4946
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3.18 0.1680 0.3624 0.0756 0.0351 0.009 0.569 0.386 6.735 0.064 1.716 25.975 0.08 36884. 0.4733
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3.64 0.1920 0.4015 0.0734 0.0351 0.009 0.570 0.374 6.744 0.064 1.665 25.181 0.08 36923. 0.4520
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4.09 0.2160 0.4376 0.0711 0.0351 0.009 0.569 0.362 6.736 0.064 1.612 24.397 0.08 36965. 0.4308
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4.55 0.2400 0.4709 0.0685 0.0349 0.009 0.567 0.349 6.709 0.064 1.554 23.624 0.08 37010. 0.4097
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5.00 0.2641 0.5012 0.0659 0.0347 0.009 0.563 0.336 6.663 0.064 1.494 22.860 0.08 37058. 0.3887
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5.46 0.2881 0.5286 0.0630 0.0343 0.009 0.557 0.321 6.595 0.063 1.429 22.103 0.08 37108. 0.3676
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5.91 0.3121 0.5532 0.0600 0.0339 0.009 0.550 0.306 6.503 0.062 1.361 21.349 0.08 37161. 0.3465
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6.36 0.3361 0.5747 0.0569 0.0333 0.009 0.540 0.290 6.386 0.061 1.290 20.597 0.08 37217. 0.3254
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6.82 0.3601 0.5932 0.0536 0.0325 0.008 0.528 0.273 6.244 0.060 1.215 19.840 0.08 37276. 0.3042
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7.27 0.3841 0.6083 0.0501 0.0317 0.008 0.514 0.256 6.078 0.058 1.137 19.075 0.08 37338. 0.2829
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7.73 0.4081 0.6198 0.0466 0.0307 0.008 0.498 0.237 5.888 0.056 1.056 18.293 0.08 37403. 0.2615
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8.18 0.4321 0.6274 0.0429 0.0296 0.008 0.480 0.219 5.675 0.054 0.973 17.489 0.08 37470. 0.2400
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8.64 0.4561 0.6306 0.0392 0.0283 0.007 0.460 0.200 5.439 0.052 0.888 16.652 0.08 37541. 0.2183
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9.09 0.4801 0.6287 0.0353 0.0270 0.007 0.438 0.180 5.181 0.049 0.801 15.771 0.08 37614. 0.1964
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9.55 0.5041 0.6208 0.0314 0.0255 0.007 0.414 0.160 4.902 0.047 0.713 14.832 0.08 37691. 0.1742
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10.00 0.5281 0.6058 0.0275 0.0240 0.006 0.389 0.140 4.602 0.044 0.624 13.815 0.08 37770. 0.1518
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10.46 0.5521 0.5820 0.0235 0.0223 0.006 0.362 0.120 4.283 0.041 0.533 12.695 0.08 37853. 0.1289
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10.91 0.5761 0.5470 0.0195 0.0205 0.005 0.333 0.099 3.945 0.038 0.442 11.435 0.08 37938. 0.1058
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11.37 0.6001 0.4975 0.0155 0.0187 0.005 0.303 0.079 3.589 0.034 0.351 9.985 0.08 38026. 0.0824
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11.82 0.6241 0.4285 0.0115 0.0168 0.004 0.272 0.059 3.219 0.031 0.261 8.268 0.08 38118. 0.0588
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12.28 0.6481 0.3318 0.0076 0.0148 0.004 0.240 0.039 2.835 0.027 0.171 6.165 0.08 38212. 0.0355
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12.73 0.6721 0.1941 0.0037 0.0127 0.003 0.206 0.019 2.440 0.023 0.083 3.478 0.08 38310. 0.0140
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13.18 0.6961 -0.0090 -0.0001 0.0106 0.003 0.172 -0.001 2.036 0.019 -0.003 -0.157 0.08 38409. 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 0.0878 0.0307 0.063 1.994 1.790 47.174 0.225 7.964 17.215 0.16 73348. 0.6758
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0.91 0.0241 0.0669 0.0865 0.0311 0.064 2.022 1.763 47.837 0.228 7.844 16.720 0.16 73395. 0.6514
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1.82 0.0482 0.1298 0.0850 0.0315 0.065 2.048 1.734 48.464 0.231 7.714 16.230 0.16 73446. 0.6271
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2.74 0.0723 0.1889 0.0835 0.0319 0.066 2.073 1.703 49.041 0.234 7.573 15.747 0.16 73501. 0.6028
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3.65 0.0963 0.2443 0.0818 0.0323 0.066 2.094 1.668 49.555 0.237 7.421 15.270 0.16 73561. 0.5787
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4.56 0.1204 0.2960 0.0800 0.0325 0.067 2.113 1.632 49.992 0.239 7.257 14.803 0.16 73625. 0.5547
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5.47 0.1445 0.3442 0.0781 0.0328 0.068 2.127 1.592 50.338 0.240 7.081 14.344 0.16 73694. 0.5310
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6.39 0.1686 0.3890 0.0760 0.0329 0.068 2.137 1.549 50.577 0.241 6.892 13.895 0.16 73769. 0.5074
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7.30 0.1927 0.4305 0.0737 0.0330 0.068 2.142 1.504 50.695 0.242 6.690 13.456 0.16 73848. 0.4841
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8.21 0.2168 0.4689 0.0714 0.0330 0.068 2.142 1.455 50.677 0.242 6.474 13.026 0.16 73933. 0.4611
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9.12 0.2408 0.5042 0.0688 0.0329 0.068 2.134 1.404 50.506 0.241 6.244 12.606 0.16 74023. 0.4382
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10.03 0.2649 0.5365 0.0661 0.0327 0.067 2.120 1.349 50.170 0.240 6.000 12.194 0.16 74118. 0.4155
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10.95 0.2890 0.5658 0.0633 0.0323 0.067 2.098 1.291 49.652 0.237 5.741 11.790 0.16 74220. 0.3930
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11.86 0.3131 0.5923 0.0603 0.0319 0.066 2.068 1.229 48.936 0.234 5.467 11.392 0.16 74327. 0.3705
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12.77 0.3372 0.6159 0.0571 0.0313 0.064 2.029 1.164 48.012 0.229 5.179 10.999 0.16 74439. 0.3482
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13.68 0.3613 0.6364 0.0538 0.0305 0.063 1.981 1.096 46.878 0.224 4.877 10.609 0.16 74558. 0.3259
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14.60 0.3853 0.6539 0.0503 0.0296 0.061 1.924 1.026 45.538 0.217 4.563 10.219 0.16 74682. 0.3037
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15.51 0.4094 0.6680 0.0467 0.0286 0.059 1.859 0.953 43.995 0.210 4.239 9.825 0.16 74813. 0.2814
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16.42 0.4335 0.6785 0.0430 0.0275 0.057 1.786 0.878 42.252 0.202 3.905 9.425 0.16 74949. 0.2591
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17.33 0.4576 0.6848 0.0393 0.0262 0.054 1.704 0.801 40.313 0.192 3.563 9.013 0.16 75091. 0.2367
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18.25 0.4817 0.6865 0.0354 0.0249 0.051 1.614 0.723 38.183 0.182 3.214 8.583 0.16 75239. 0.2141
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19.16 0.5058 0.6827 0.0315 0.0233 0.048 1.516 0.643 35.866 0.171 2.859 8.129 0.16 75392. 0.1912
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20.07 0.5298 0.6721 0.0276 0.0217 0.045 1.410 0.562 33.370 0.159 2.500 7.639 0.16 75552. 0.1680
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20.98 0.5539 0.6531 0.0236 0.0200 0.041 1.298 0.481 30.703 0.147 2.138 7.100 0.16 75718. 0.1444
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21.89 0.5780 0.6229 0.0196 0.0181 0.037 1.178 0.399 27.873 0.133 1.774 6.490 0.16 75890. 0.1202
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22.81 0.6021 0.5776 0.0155 0.0162 0.033 1.052 0.317 24.894 0.119 1.410 5.777 0.16 76068. 0.0954
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23.72 0.6262 0.5104 0.0116 0.0142 0.029 0.920 0.236 21.781 0.104 1.049 4.909 0.16 76252. 0.0699
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24.63 0.6503 0.4100 0.0076 0.0121 0.025 0.784 0.155 18.551 0.089 0.691 3.797 0.16 76442. 0.0439
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25.54 0.6743 0.2544 0.0037 0.0099 0.020 0.643 0.076 15.226 0.073 0.339 2.272 0.16 76637. 0.0184
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26.46 0.6984 -0.0049 -0.0001 0.0077 0.016 0.500 -0.001 11.822 0.056 -0.005 -0.042 0.16 76836. 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 0.0882 0.0298 0.207 4.347 4.047 154.299 0.491 18.000 11.896 0.24 110020. 0.7021
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1.37 0.0241 0.0694 0.0869 0.0302 0.210 4.413 3.986 156.627 0.499 17.730 11.543 0.24 110090. 0.6761
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2.74 0.0482 0.1345 0.0854 0.0306 0.213 4.475 3.920 158.832 0.506 17.437 11.195 0.24 110167. 0.6503
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4.11 0.0724 0.1956 0.0839 0.0310 0.216 4.532 3.849 160.869 0.512 17.120 10.852 0.24 110250. 0.6246
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5.48 0.0965 0.2528 0.0822 0.0314 0.218 4.584 3.772 162.693 0.518 16.778 10.516 0.24 110340. 0.5992
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6.85 0.1206 0.3061 0.0804 0.0317 0.220 4.628 3.689 164.255 0.523 16.409 10.187 0.24 110436. 0.5740
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8.22 0.1447 0.3557 0.0784 0.0319 0.222 4.663 3.600 165.505 0.527 16.011 9.865 0.24 110541. 0.5491
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9.59 0.1689 0.4017 0.0764 0.0321 0.223 4.688 3.504 166.391 0.530 15.585 9.551 0.24 110652. 0.5245
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10.97 0.1930 0.4444 0.0741 0.0322 0.224 4.701 3.401 166.861 0.531 15.128 9.245 0.24 110772. 0.5002
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12.34 0.2171 0.4838 0.0717 0.0322 0.224 4.701 3.291 166.861 0.531 14.640 8.947 0.24 110899. 0.4762
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13.71 0.2412 0.5201 0.0692 0.0321 0.223 4.686 3.174 166.338 0.529 14.120 8.656 0.24 111035. 0.4525
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15.08 0.2654 0.5534 0.0665 0.0319 0.222 4.656 3.050 165.243 0.526 13.568 8.373 0.24 111179. 0.4290
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16.45 0.2895 0.5837 0.0636 0.0315 0.219 4.607 2.919 163.521 0.521 12.982 8.096 0.24 111331. 0.4058
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17.82 0.3136 0.6112 0.0606 0.0311 0.216 4.539 2.779 161.115 0.513 12.363 7.824 0.24 111492. 0.3827
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19.19 0.3377 0.6358 0.0574 0.0305 0.212 4.451 2.633 157.989 0.503 11.710 7.558 0.24 111662. 0.3598
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20.56 0.3618 0.6575 0.0540 0.0297 0.207 4.343 2.479 154.137 0.491 11.027 7.295 0.24 111841. 0.3370
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21.93 0.3860 0.6762 0.0505 0.0288 0.201 4.214 2.319 149.564 0.476 10.316 7.034 0.24 112028. 0.3143
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23.30 0.4101 0.6917 0.0469 0.0278 0.193 4.065 2.154 144.283 0.459 9.582 6.772 0.24 112224. 0.2916
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24.67 0.4342 0.7038 0.0432 0.0267 0.185 3.897 1.984 138.302 0.440 8.826 6.507 0.24 112429. 0.2689
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26.04 0.4583 0.7121 0.0394 0.0254 0.177 3.709 1.810 131.636 0.419 8.051 6.237 0.24 112642. 0.2462
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27.41 0.4825 0.7159 0.0356 0.0240 0.167 3.502 1.632 124.298 0.396 7.261 5.957 0.24 112865. 0.2233
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28.78 0.5066 0.7145 0.0316 0.0224 0.156 3.277 1.452 116.307 0.370 6.458 5.662 0.24 113096. 0.2002
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30.15 0.5307 0.7067 0.0277 0.0208 0.144 3.034 1.269 107.683 0.343 5.646 5.346 0.24 113337. 0.1767
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31.52 0.5548 0.6908 0.0236 0.0190 0.132 2.774 1.085 98.455 0.313 4.826 4.999 0.24 113586. 0.1528
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32.90 0.5790 0.6641 0.0196 0.0171 0.119 2.498 0.900 88.658 0.282 4.004 4.605 0.24 113845. 0.1282
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34.27 0.6031 0.6222 0.0156 0.0151 0.105 2.207 0.715 78.334 0.249 3.182 4.142 0.24 114113. 0.1028
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35.64 0.6272 0.5578 0.0116 0.0130 0.091 1.903 0.532 67.538 0.215 2.365 3.570 0.24 114389. 0.0764
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37.01 0.6513 0.4573 0.0076 0.0109 0.076 1.587 0.350 56.334 0.179 1.557 2.818 0.24 114675. 0.0489
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38.38 0.6755 0.2925 0.0037 0.0086 0.060 1.262 0.172 44.798 0.143 0.764 1.739 0.24 114970. 0.0211
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39.75 0.6996 -0.0068 -0.0001 0.0064 0.044 0.929 -0.003 32.976 0.105 -0.013 -0.039 0.24 115268. 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 0.0887 0.0293 0.483 7.616 7.236 360.413 0.860 32.186 9.106 0.32 146688. 0.7187
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1.85 0.0244 0.0715 0.0874 0.0298 0.491 7.737 7.127 366.136 0.874 31.702 8.829 0.32 146783. 0.6916
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3.69 0.0487 0.1385 0.0859 0.0302 0.498 7.851 7.009 371.560 0.887 31.177 8.556 0.32 146886. 0.6646
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5.54 0.0731 0.2013 0.0843 0.0306 0.505 7.957 6.881 376.572 0.899 30.607 8.288 0.32 146999. 0.6378
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7.39 0.0975 0.2599 0.0826 0.0310 0.511 8.052 6.742 381.062 0.910 29.990 8.025 0.32 147120. 0.6114
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9.23 0.1219 0.3144 0.0808 0.0313 0.516 8.133 6.593 384.907 0.919 29.324 7.769 0.32 147251. 0.5852
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11.08 0.1462 0.3652 0.0788 0.0316 0.520 8.198 6.431 387.984 0.926 28.606 7.518 0.32 147392. 0.5594
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12.93 0.1706 0.4122 0.0767 0.0317 0.523 8.244 6.258 390.160 0.931 27.835 7.275 0.32 147544. 0.5339
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14.77 0.1950 0.4558 0.0744 0.0318 0.525 8.269 6.072 391.305 0.934 27.007 7.038 0.32 147706. 0.5088
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16.62 0.2194 0.4960 0.0720 0.0318 0.525 8.268 5.873 391.286 0.934 26.123 6.808 0.32 147879. 0.4840
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18.47 0.2437 0.5330 0.0694 0.0317 0.523 8.240 5.661 389.972 0.931 25.180 6.584 0.32 148063. 0.4596
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20.31 0.2681 0.5669 0.0666 0.0315 0.519 8.183 5.436 387.236 0.924 24.177 6.367 0.32 148259. 0.4355
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22.16 0.2925 0.5979 0.0637 0.0312 0.514 8.092 5.196 382.943 0.914 23.114 6.155 0.32 148466. 0.4116
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24.01 0.3169 0.6259 0.0606 0.0307 0.506 7.965 4.943 376.954 0.900 21.987 5.948 0.32 148684. 0.3880
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25.85 0.3412 0.6511 0.0573 0.0300 0.495 7.801 4.676 369.182 0.881 20.800 5.745 0.32 148915. 0.3645
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27.70 0.3656 0.6734 0.0539 0.0293 0.482 7.599 4.397 359.615 0.859 19.558 5.546 0.32 149157. 0.3412
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29.54 0.3900 0.6928 0.0503 0.0283 0.467 7.359 4.107 348.270 0.831 18.267 5.349 0.32 149412. 0.3180
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31.39 0.4144 0.7089 0.0467 0.0273 0.449 7.082 3.807 335.172 0.800 16.933 5.152 0.32 149678. 0.2949
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33.24 0.4387 0.7217 0.0429 0.0261 0.430 6.769 3.498 320.346 0.765 15.560 4.953 0.32 149956. 0.2718
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35.08 0.4631 0.7307 0.0390 0.0247 0.407 6.420 3.182 303.822 0.725 14.154 4.750 0.32 150247. 0.2486
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36.93 0.4875 0.7352 0.0351 0.0232 0.383 6.036 2.860 285.637 0.682 12.720 4.541 0.32 150549. 0.2253
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38.78 0.5119 0.7345 0.0310 0.0216 0.356 5.617 2.532 265.836 0.635 11.264 4.321 0.32 150864. 0.2017
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40.62 0.5362 0.7273 0.0270 0.0199 0.328 5.166 2.201 244.476 0.584 9.791 4.084 0.32 151191. 0.1778
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42.47 0.5606 0.7117 0.0229 0.0180 0.297 4.683 1.868 221.629 0.529 8.308 3.822 0.32 151530. 0.1533
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44.32 0.5850 0.6845 0.0188 0.0161 0.265 4.171 1.533 197.388 0.471 6.820 3.523 0.32 151881. 0.1280
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46.16 0.6094 0.6407 0.0147 0.0140 0.230 3.632 1.200 171.867 0.410 5.335 3.166 0.32 152245. 0.1017
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48.01 0.6337 0.5708 0.0106 0.0118 0.195 3.068 0.868 145.207 0.347 3.862 2.712 0.32 152621. 0.0741
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49.86 0.6581 0.4565 0.0066 0.0096 0.158 2.485 0.541 117.582 0.281 2.408 2.089 0.32 153009. 0.0451
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51.70 0.6825 0.2550 0.0027 0.0073 0.120 1.885 0.221 89.186 0.213 0.984 1.125 0.32 153409. 0.0155
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53.55 0.7069
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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 0.0893 0.0292 0.939 11.838 11.389 700.310 1.337 50.660 7.377 0.40 183351. 0.7304
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2.29 0.0241 0.0717 0.0880 0.0296 0.954 12.030 11.222 711.640 1.359 49.915 7.152 0.40 183469. 0.7029
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4.57 0.0483 0.1389 0.0866 0.0301 0.969 12.212 11.040 722.395 1.380 49.104 6.931 0.40 183597. 0.6757
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6.86 0.0724 0.2018 0.0851 0.0305 0.982 12.380 10.842 732.357 1.399 48.225 6.715 0.40 183736. 0.6487
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9.14 0.0965 0.2606 0.0834 0.0309 0.994 12.531 10.628 741.310 1.416 47.273 6.503 0.40 183886. 0.6220
|
|
11.43 0.1207 0.3154 0.0816 0.0312 1.004 12.662 10.397 749.023 1.431 46.245 6.296 0.40 184049. 0.5956
|
|
13.71 0.1448 0.3664 0.0796 0.0315 1.013 12.767 10.148 755.252 1.442 45.137 6.094 0.40 184223. 0.5696
|
|
16.00 0.1690 0.4137 0.0775 0.0317 1.019 12.843 9.880 759.745 1.451 43.946 5.898 0.40 184410. 0.5439
|
|
18.28 0.1931 0.4576 0.0753 0.0318 1.022 12.885 9.593 762.248 1.456 42.668 5.708 0.40 184610. 0.5187
|
|
20.57 0.2172 0.4981 0.0728 0.0318 1.023 12.890 9.285 762.504 1.456 41.301 5.523 0.40 184824. 0.4938
|
|
22.86 0.2414 0.5355 0.0703 0.0317 1.020 12.852 8.958 760.261 1.452 39.844 5.344 0.40 185051. 0.4693
|
|
25.14 0.2655 0.5698 0.0675 0.0315 1.013 12.767 8.609 755.270 1.442 38.293 5.170 0.40 185292. 0.4451
|
|
27.43 0.2896 0.6013 0.0646 0.0311 1.002 12.632 8.239 747.278 1.427 36.648 5.001 0.40 185547. 0.4211
|
|
29.71 0.3138 0.6299 0.0616 0.0307 0.987 12.442 7.848 736.011 1.406 34.906 4.836 0.40 185816. 0.3975
|
|
32.00 0.3379 0.6558 0.0583 0.0300 0.967 12.193 7.434 721.273 1.378 33.068 4.675 0.40 186100. 0.3740
|
|
34.28 0.3620 0.6789 0.0549 0.0293 0.943 11.884 7.002 703.026 1.343 31.143 4.517 0.40 186399. 0.3507
|
|
36.57 0.3862 0.6993 0.0514 0.0284 0.914 11.517 6.551 681.293 1.301 29.141 4.362 0.40 186712. 0.3275
|
|
38.86 0.4103 0.7166 0.0477 0.0273 0.880 11.091 6.086 656.118 1.253 27.068 4.207 0.40 187039. 0.3045
|
|
41.14 0.4344 0.7308 0.0440 0.0261 0.842 10.608 5.606 627.549 1.199 24.935 4.052 0.40 187381. 0.2814
|
|
43.43 0.4586 0.7414 0.0401 0.0248 0.799 10.069 5.114 595.641 1.138 22.749 3.895 0.40 187738. 0.2584
|
|
45.71 0.4827 0.7481 0.0362 0.0233 0.752 9.474 4.613 560.460 1.070 20.518 3.733 0.40 188110. 0.2352
|
|
48.00 0.5069 0.7500 0.0322 0.0218 0.700 8.826 4.103 522.090 0.997 18.250 3.564 0.40 188497. 0.2118
|
|
50.28 0.5310 0.7462 0.0281 0.0200 0.645 8.125 3.587 480.635 0.918 15.954 3.385 0.40 188899. 0.1881
|
|
52.57 0.5551 0.7348 0.0241 0.0182 0.585 7.374 3.066 436.230 0.833 13.640 3.188 0.40 189315. 0.1638
|
|
54.85 0.5793 0.7133 0.0200 0.0162 0.522 6.577 2.544 389.042 0.743 11.316 2.966 0.40 189747. 0.1388
|
|
57.14 0.6034 0.6772 0.0159 0.0141 0.455 5.735 2.022 339.285 0.648 8.994 2.703 0.40 190194. 0.1128
|
|
59.43 0.6275 0.6185 0.0118 0.0120 0.385 4.855 1.503 287.221 0.549 6.687 2.374 0.40 190655. 0.0854
|
|
61.71 0.6517 0.5214 0.0078 0.0097 0.313 3.942 0.991 233.173 0.445 4.407 1.927 0.41 191132. 0.0563
|
|
64.00 0.6758 0.3494 0.0038 0.0074 0.238 3.001 0.487 177.516 0.339 2.168 1.245 0.41 191623. 0.0255
|
|
66.28 0.6999 -0.0059 0.0000 0.0050 0.161 2.036 -0.005 120.418 0.230 -0.024 -0.020 0.41 192118. 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 0.0902 0.0292 1.626 17.077 16.550 1212.218 1.929 73.613 6.192 0.48 220007. 0.7391
|
|
2.74 0.0241 0.0721 0.0889 0.0297 1.652 17.359 16.310 1232.244 1.961 72.546 6.003 0.48 220149. 0.7113
|
|
5.48 0.0482 0.1398 0.0874 0.0302 1.678 17.627 16.049 1251.261 1.991 71.384 5.817 0.48 220303. 0.6837
|
|
8.22 0.0724 0.2031 0.0859 0.0306 1.702 17.875 15.765 1268.890 2.020 70.122 5.635 0.48 220471. 0.6564
|
|
10.96 0.0965 0.2623 0.0842 0.0310 1.723 18.098 15.457 1284.744 2.045 68.754 5.457 0.48 220651. 0.6294
|
|
13.70 0.1206 0.3174 0.0824 0.0313 1.741 18.291 15.124 1298.421 2.067 67.274 5.283 0.48 220846. 0.6028
|
|
16.45 0.1447 0.3687 0.0804 0.0316 1.756 18.447 14.765 1309.489 2.084 65.676 5.114 0.48 221056. 0.5766
|
|
19.19 0.1688 0.4164 0.0783 0.0318 1.767 18.560 14.379 1317.503 2.097 63.957 4.950 0.48 221281. 0.5507
|
|
21.93 0.1930 0.4605 0.0761 0.0319 1.773 18.623 13.964 1322.015 2.104 62.111 4.791 0.48 221522. 0.5252
|
|
24.67 0.2171 0.5014 0.0737 0.0319 1.774 18.631 13.519 1322.573 2.105 60.134 4.636 0.48 221778. 0.5001
|
|
27.41 0.2412 0.5391 0.0711 0.0318 1.768 18.577 13.045 1318.733 2.099 58.024 4.487 0.48 222051. 0.4754
|
|
30.15 0.2653 0.5738 0.0683 0.0316 1.757 18.455 12.540 1310.058 2.085 55.778 4.342 0.48 222341. 0.4511
|
|
32.89 0.2894 0.6057 0.0654 0.0312 1.738 18.258 12.004 1296.105 2.063 53.393 4.201 0.48 222647. 0.4270
|
|
35.63 0.3136 0.6348 0.0623 0.0308 1.712 17.981 11.436 1276.398 2.031 50.866 4.064 0.48 222971. 0.4032
|
|
38.37 0.3377 0.6611 0.0590 0.0302 1.677 17.617 10.836 1250.574 1.990 48.199 3.930 0.48 223312. 0.3796
|
|
41.11 0.3618 0.6848 0.0556 0.0294 1.634 17.166 10.208 1218.556 1.939 45.403 3.799 0.48 223670. 0.3561
|
|
43.85 0.3859 0.7057 0.0520 0.0285 1.583 16.628 9.553 1180.383 1.879 42.492 3.671 0.48 224046. 0.3329
|
|
46.59 0.4100 0.7238 0.0484 0.0274 1.524 16.005 8.876 1136.127 1.808 39.478 3.543 0.48 224439. 0.3097
|
|
49.34 0.4342 0.7388 0.0446 0.0262 1.456 15.297 8.178 1085.875 1.728 36.375 3.416 0.48 224850. 0.2866
|
|
52.08 0.4583 0.7504 0.0407 0.0248 1.381 14.506 7.462 1029.722 1.639 33.193 3.287 0.48 225278. 0.2634
|
|
54.82 0.4824 0.7582 0.0367 0.0233 1.298 13.633 6.732 967.784 1.540 29.944 3.155 0.48 225724. 0.2402
|
|
57.56 0.5065 0.7615 0.0326 0.0217 1.207 12.681 5.990 900.208 1.433 26.642 3.018 0.48 226188. 0.2167
|
|
60.30 0.5306 0.7592 0.0285 0.0199 1.109 11.652 5.238 827.176 1.316 23.297 2.872 0.48 226670. 0.1928
|
|
63.04 0.5547 0.7497 0.0244 0.0181 1.004 10.550 4.479 748.926 1.192 19.924 2.713 0.48 227170. 0.1684
|
|
65.78 0.5789 0.7305 0.0203 0.0161 0.893 9.379 3.718 665.753 1.060 16.537 2.533 0.48 227687. 0.1433
|
|
68.52 0.6030 0.6970 0.0161 0.0139 0.775 8.143 2.957 578.034 0.920 13.153 2.320 0.48 228223. 0.1171
|
|
71.26 0.6271 0.6413 0.0120 0.0117 0.652 6.850 2.201 486.235 0.774 9.788 2.053 0.49 228776. 0.0893
|
|
74.00 0.6512 0.5469 0.0079 0.0094 0.524 5.507 1.453 390.925 0.622 6.463 1.686 0.49 229348. 0.0596
|
|
76.74 0.6753 0.3747 0.0039 0.0071 0.393 4.124 0.719 292.776 0.466 3.198 1.114 0.49 229936. 0.0277
|
|
79.48 0.6995 0.0001 0.0000 0.0046 0.258 2.706 0.000 192.081 0.306 0.000 0.000 0.49 230529. 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 0.0912 0.0294 2.601 23.418 22.775 1939.470 2.646 101.303 5.326 0.56 256655. 0.7457
|
|
3.20 0.0241 0.0724 0.0899 0.0299 2.645 23.812 22.451 1972.095 2.690 99.863 5.164 0.56 256821. 0.7178
|
|
6.39 0.0482 0.1403 0.0884 0.0304 2.686 24.187 22.098 2003.088 2.733 98.290 5.004 0.56 257002. 0.6901
|
|
9.59 0.0723 0.2038 0.0869 0.0308 2.725 24.534 21.713 2031.827 2.772 96.578 4.847 0.56 257198. 0.6626
|
|
12.79 0.0965 0.2632 0.0852 0.0312 2.759 24.846 21.295 2057.685 2.807 94.719 4.694 0.56 257409. 0.6355
|
|
15.99 0.1206 0.3185 0.0834 0.0316 2.789 25.115 20.842 2079.997 2.838 92.705 4.545 0.56 257638. 0.6087
|
|
19.18 0.1447 0.3700 0.0815 0.0319 2.814 25.333 20.352 2098.065 2.862 90.527 4.400 0.56 257883. 0.5823
|
|
22.38 0.1688 0.4179 0.0793 0.0321 2.831 25.492 19.824 2111.166 2.880 88.179 4.259 0.56 258146. 0.5564
|
|
25.58 0.1929 0.4623 0.0771 0.0322 2.841 25.581 19.257 2118.569 2.890 85.654 4.123 0.56 258428. 0.5308
|
|
28.77 0.2170 0.5034 0.0746 0.0322 2.842 25.593 18.648 2119.540 2.891 82.947 3.991 0.56 258728. 0.5056
|
|
31.97 0.2411 0.5414 0.0720 0.0321 2.834 25.518 17.998 2113.358 2.883 80.054 3.863 0.56 259048. 0.4808
|
|
35.17 0.2653 0.5764 0.0693 0.0319 2.815 25.348 17.305 2099.318 2.864 76.972 3.739 0.56 259386. 0.4563
|
|
38.36 0.2894 0.6086 0.0663 0.0315 2.785 25.075 16.568 2076.703 2.833 73.696 3.619 0.56 259745. 0.4321
|
|
41.56 0.3135 0.6381 0.0632 0.0310 2.742 24.690 15.787 2044.750 2.789 70.222 3.502 0.56 260123. 0.4082
|
|
44.76 0.3376 0.6649 0.0599 0.0304 2.686 24.184 14.962 2002.852 2.732 66.551 3.388 0.56 260522. 0.3845
|
|
47.96 0.3617 0.6890 0.0564 0.0296 2.616 23.556 14.096 1950.865 2.661 62.701 3.277 0.56 260941. 0.3610
|
|
51.15 0.3858 0.7105 0.0528 0.0287 2.533 22.807 13.194 1888.848 2.577 58.688 3.168 0.56 261380. 0.3376
|
|
54.35 0.4100 0.7292 0.0491 0.0276 2.437 21.939 12.260 1816.922 2.479 54.531 3.060 0.56 261839. 0.3144
|
|
57.55 0.4341 0.7450 0.0452 0.0263 2.327 20.952 11.297 1735.229 2.367 50.248 2.953 0.56 262319. 0.2912
|
|
60.74 0.4582 0.7574 0.0413 0.0250 2.205 19.850 10.309 1643.925 2.243 45.855 2.844 0.56 262820. 0.2679
|
|
63.94 0.4823 0.7662 0.0372 0.0234 2.069 18.634 9.300 1543.203 2.105 41.367 2.733 0.56 263340. 0.2446
|
|
67.14 0.5064 0.7707 0.0331 0.0218 1.922 17.307 8.274 1433.299 1.955 36.803 2.618 0.56 263882. 0.2210
|
|
70.33 0.5305 0.7697 0.0290 0.0200 1.763 15.872 7.235 1314.512 1.793 32.180 2.496 0.56 264444. 0.1970
|
|
73.53 0.5546 0.7618 0.0248 0.0180 1.592 14.335 6.186 1187.228 1.620 27.516 2.363 0.56 265027. 0.1725
|
|
76.73 0.5788 0.7445 0.0205 0.0160 1.411 12.702 5.133 1051.933 1.435 22.831 2.213 0.56 265631. 0.1471
|
|
79.93 0.6029 0.7132 0.0163 0.0138 1.219 10.979 4.080 909.240 1.240 18.148 2.035 0.57 266256. 0.1206
|
|
83.12 0.6270 0.6597 0.0121 0.0115 1.019 9.176 3.033 759.913 1.037 13.492 1.810 0.57 266902. 0.0925
|
|
86.32 0.6511 0.5671 0.0080 0.0092 0.811 7.304 1.999 604.887 0.825 8.889 1.499 0.57 267568. 0.0622
|
|
89.52 0.6752 0.3928 0.0039 0.0068 0.597 5.376 0.983 445.269 0.607 4.371 1.001 0.57 268255. 0.0291
|
|
92.71 0.6993 -0.0084 -0.0001 0.0043 0.377 3.398 -0.013 281.409 0.384 -0.057 -0.021 0.57 268944. 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 0.0924 0.0298 3.933 30.989 30.142 2933.049 3.501 134.073 4.661 0.63 293292. 0.7508
|
|
3.65 0.0241 0.0723 0.0911 0.0303 4.001 31.519 29.725 2983.212 3.561 132.215 4.519 0.63 293482. 0.7229
|
|
7.30 0.0482 0.1402 0.0897 0.0308 4.064 32.022 29.267 3030.882 3.618 130.181 4.380 0.63 293689. 0.6952
|
|
10.95 0.0723 0.2037 0.0882 0.0313 4.124 32.489 28.768 3075.099 3.671 127.961 4.243 0.63 293914. 0.6677
|
|
14.60 0.0964 0.2631 0.0865 0.0317 4.177 32.910 28.225 3114.896 3.718 125.543 4.110 0.63 294157. 0.6406
|
|
18.25 0.1205 0.3185 0.0847 0.0320 4.223 33.273 27.634 3149.247 3.759 122.917 3.980 0.64 294418. 0.6138
|
|
21.91 0.1446 0.3701 0.0827 0.0323 4.261 33.567 26.995 3177.078 3.792 120.072 3.854 0.64 294700. 0.5874
|
|
25.56 0.1687 0.4181 0.0806 0.0325 4.288 33.780 26.303 3197.273 3.816 116.997 3.731 0.64 295002. 0.5615
|
|
29.21 0.1928 0.4626 0.0783 0.0326 4.303 33.901 25.559 3208.721 3.830 113.686 3.613 0.64 295325. 0.5359
|
|
32.86 0.2169 0.5039 0.0759 0.0327 4.305 33.918 24.759 3210.293 3.832 110.130 3.498 0.64 295669. 0.5107
|
|
36.51 0.2410 0.5421 0.0732 0.0326 4.292 33.818 23.903 3200.890 3.821 106.323 3.387 0.64 296035. 0.4858
|
|
40.16 0.2651 0.5774 0.0705 0.0323 4.264 33.592 22.990 3179.430 3.795 102.260 3.280 0.64 296423. 0.4614
|
|
43.81 0.2892 0.6099 0.0675 0.0320 4.217 33.226 22.018 3144.839 3.754 97.938 3.176 0.64 296834. 0.4372
|
|
47.46 0.3132 0.6397 0.0643 0.0315 4.152 32.710 20.987 3095.963 3.696 93.349 3.075 0.64 297267. 0.4132
|
|
51.11 0.3373 0.6670 0.0610 0.0308 4.066 32.032 19.896 3031.846 3.619 88.496 2.976 0.64 297723. 0.3895
|
|
54.76 0.3614 0.6916 0.0575 0.0300 3.959 31.191 18.749 2952.219 3.524 83.398 2.881 0.64 298203. 0.3659
|
|
58.41 0.3855 0.7136 0.0538 0.0291 3.832 30.187 17.554 2857.188 3.411 78.080 2.787 0.64 298705. 0.3425
|
|
62.07 0.4096 0.7330 0.0500 0.0279 3.684 29.022 16.314 2746.938 3.279 72.566 2.694 0.64 299231. 0.3192
|
|
65.72 0.4337 0.7494 0.0461 0.0267 3.516 27.699 15.036 2621.690 3.129 66.880 2.601 0.64 299780. 0.2959
|
|
69.37 0.4578 0.7628 0.0421 0.0252 3.328 26.220 13.724 2481.697 2.962 61.044 2.508 0.64 300352. 0.2726
|
|
73.02 0.4819 0.7726 0.0379 0.0237 3.121 24.588 12.383 2327.251 2.778 55.080 2.413 0.64 300947. 0.2492
|
|
76.67 0.5060 0.7781 0.0338 0.0220 2.895 22.808 11.018 2158.723 2.577 49.010 2.315 0.64 301566. 0.2255
|
|
80.32 0.5301 0.7786 0.0295 0.0201 2.651 20.883 9.635 1976.573 2.359 42.858 2.211 0.64 302209. 0.2014
|
|
83.97 0.5542 0.7723 0.0252 0.0181 2.389 18.821 8.239 1781.387 2.126 36.648 2.098 0.64 302875. 0.1767
|
|
87.62 0.5783 0.7568 0.0209 0.0160 2.111 16.629 6.836 1573.917 1.879 30.408 1.970 0.65 303564. 0.1511
|
|
91.27 0.6024 0.7277 0.0167 0.0138 1.817 14.317 5.434 1355.104 1.618 24.169 1.819 0.65 304278. 0.1244
|
|
94.92 0.6265 0.6769 0.0124 0.0115 1.510 11.898 4.038 1126.123 1.344 17.962 1.626 0.65 305015. 0.0959
|
|
98.58 0.6506 0.5866 0.0081 0.0090 1.191 9.386 2.659 888.423 1.060 11.826 1.357 0.65 305776. 0.0649
|
|
102.23 0.6747 0.4118 0.0040 0.0065 0.863 6.801 1.304 643.714 0.768 5.800 0.919 0.65 306560. 0.0308
|
|
105.88 0.6988 -0.0131 -0.0001 0.0040 0.526 4.146 -0.024 392.429 0.468 -0.109 -0.028 0.65 307344. 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 0.0938 0.0305 5.720 40.057 38.754 4265.270 4.526 172.377 4.121 0.71 329914. 0.7527
|
|
4.12 0.0242 0.0722 0.0926 0.0310 5.816 40.733 38.234 4337.265 4.602 170.065 3.998 0.71 330130. 0.7253
|
|
8.23 0.0483 0.1400 0.0912 0.0315 5.908 41.378 37.662 4405.952 4.675 167.521 3.877 0.71 330364. 0.6981
|
|
12.35 0.0725 0.2035 0.0897 0.0319 5.994 41.978 37.035 4469.883 4.743 164.733 3.758 0.71 330619. 0.6710
|
|
16.47 0.0966 0.2629 0.0880 0.0323 6.072 42.521 36.350 4527.611 4.804 161.686 3.642 0.71 330894. 0.6441
|
|
20.59 0.1208 0.3184 0.0862 0.0327 6.139 42.990 35.603 4577.576 4.857 158.363 3.528 0.71 331191. 0.6176
|
|
24.70 0.1449 0.3701 0.0842 0.0330 6.193 43.370 34.791 4618.117 4.900 154.750 3.417 0.71 331511. 0.5913
|
|
28.82 0.1691 0.4182 0.0821 0.0332 6.232 43.647 33.911 4647.526 4.931 150.834 3.309 0.72 331853. 0.5654
|
|
32.94 0.1932 0.4628 0.0798 0.0333 6.255 43.802 32.960 4664.046 4.949 146.605 3.205 0.72 332220. 0.5399
|
|
37.06 0.2174 0.5043 0.0773 0.0333 6.257 43.820 31.936 4665.950 4.951 142.051 3.104 0.72 332610. 0.5147
|
|
41.17 0.2415 0.5428 0.0747 0.0332 6.238 43.684 30.838 4651.538 4.935 137.165 3.007 0.72 333026. 0.4899
|
|
45.29 0.2657 0.5783 0.0718 0.0330 6.194 43.381 29.663 4619.219 4.901 131.941 2.913 0.72 333466. 0.4654
|
|
49.41 0.2899 0.6111 0.0688 0.0326 6.125 42.894 28.411 4567.417 4.846 126.374 2.821 0.72 333932. 0.4412
|
|
53.52 0.3140 0.6413 0.0656 0.0321 6.027 42.209 27.081 4494.447 4.769 120.454 2.733 0.72 334423. 0.4172
|
|
57.64 0.3382 0.6689 0.0622 0.0314 5.899 41.312 25.671 4398.890 4.667 114.184 2.647 0.72 334941. 0.3935
|
|
61.76 0.3623 0.6940 0.0586 0.0306 5.740 40.198 24.188 4280.329 4.542 107.588 2.563 0.72 335484. 0.3698
|
|
65.88 0.3865 0.7165 0.0548 0.0296 5.550 38.870 22.639 4138.923 4.392 100.700 2.481 0.72 336054. 0.3463
|
|
69.99 0.4106 0.7364 0.0509 0.0284 5.331 37.331 21.032 3974.979 4.218 93.552 2.400 0.72 336649. 0.3229
|
|
74.11 0.4348 0.7535 0.0469 0.0271 5.081 35.582 19.374 3788.838 4.020 86.174 2.319 0.72 337271. 0.2995
|
|
78.23 0.4589 0.7676 0.0428 0.0256 4.802 33.630 17.670 3580.894 3.799 78.596 2.238 0.72 337919. 0.2760
|
|
82.35 0.4831 0.7781 0.0386 0.0239 4.495 31.476 15.928 3351.603 3.556 70.847 2.155 0.72 338593. 0.2524
|
|
86.46 0.5072 0.7846 0.0343 0.0222 4.159 29.128 14.154 3101.557 3.291 62.956 2.070 0.72 339294. 0.2285
|
|
90.58 0.5314 0.7859 0.0299 0.0202 3.797 26.592 12.355 2831.510 3.004 54.954 1.979 0.72 340021. 0.2041
|
|
94.70 0.5556 0.7805 0.0255 0.0182 3.409 23.877 10.539 2542.435 2.698 46.875 1.880 0.73 340774. 0.1791
|
|
98.81 0.5797 0.7658 0.0211 0.0160 2.998 20.995 8.713 2235.588 2.372 38.755 1.768 0.73 341555. 0.1531
|
|
102.93 0.6039 0.7370 0.0167 0.0137 2.565 17.962 6.887 1912.574 2.029 30.632 1.633 0.73 342361. 0.1257
|
|
107.05 0.6280 0.6850 0.0123 0.0113 2.113 14.796 5.070 1575.438 1.672 22.552 1.460 0.73 343195. 0.0964
|
|
111.17 0.6522 0.5900 0.0079 0.0088 1.645 11.521 3.274 1226.714 1.302 14.565 1.211 0.73 344055. 0.0643
|
|
115.28 0.6763 0.3985 0.0037 0.0062 1.166 8.165 1.511 869.419 0.922 6.722 0.788 0.73 344941. 0.0284
|
|
119.40 0.7005
|
|
|
|
|
|
|
|
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 0.0956 0.0324 8.354 52.657 48.728 6229.929 5.949 216.743 3.548 0.79 366517. 0.7266
|
|
4.54 0.0240 0.0689 0.0944 0.0329 8.462 53.336 48.112 6310.292 6.026 214.001 3.458 0.79 366756. 0.7037
|
|
9.09 0.0480 0.1342 0.0930 0.0333 8.564 53.975 47.430 6385.887 6.098 210.969 3.369 0.79 367016. 0.6807
|
|
13.63 0.0720 0.1960 0.0915 0.0336 8.656 54.559 46.679 6454.980 6.164 207.629 3.280 0.79 367297. 0.6575
|
|
18.18 0.0960 0.2544 0.0899 0.0339 8.738 55.073 45.854 6515.792 6.222 203.958 3.192 0.79 367602. 0.6341
|
|
22.72 0.1200 0.3093 0.0882 0.0342 8.806 55.502 44.950 6566.494 6.271 199.938 3.105 0.79 367932. 0.6107
|
|
27.27 0.1440 0.3609 0.0862 0.0344 8.858 55.828 43.963 6605.083 6.307 195.547 3.019 0.79 368285. 0.5873
|
|
31.81 0.1680 0.4092 0.0841 0.0345 8.890 56.034 42.889 6629.502 6.331 190.769 2.934 0.79 368665. 0.5638
|
|
36.36 0.1920 0.4544 0.0818 0.0346 8.901 56.103 41.724 6637.623 6.338 185.589 2.851 0.79 369070. 0.5403
|
|
40.90 0.2160 0.4966 0.0794 0.0345 8.887 56.015 40.466 6627.251 6.329 179.992 2.769 0.80 369503. 0.5169
|
|
45.45 0.2400 0.5358 0.0767 0.0344 8.846 55.752 39.112 6596.158 6.299 173.969 2.689 0.80 369962. 0.4935
|
|
49.99 0.2639 0.5722 0.0739 0.0341 8.773 55.296 37.660 6542.113 6.247 167.512 2.611 0.80 370449. 0.4701
|
|
54.53 0.2879 0.6059 0.0708 0.0337 8.667 54.626 36.109 6462.842 6.172 160.614 2.534 0.80 370964. 0.4468
|
|
59.08 0.3119 0.6369 0.0676 0.0331 8.523 53.721 34.457 6355.867 6.069 153.266 2.459 0.80 371507. 0.4235
|
|
63.62 0.3359 0.6653 0.0641 0.0324 8.340 52.563 32.703 6218.799 5.939 145.465 2.385 0.80 372079. 0.4002
|
|
68.17 0.3599 0.6912 0.0605 0.0315 8.114 51.142 30.854 6050.693 5.778 137.238 2.313 0.80 372679. 0.3769
|
|
72.71 0.3839 0.7145 0.0567 0.0305 7.847 49.460 28.918 5851.659 5.588 128.628 2.241 0.80 373307. 0.3536
|
|
77.26 0.4079 0.7352 0.0528 0.0293 7.539 47.518 26.905 5621.912 5.369 119.676 2.171 0.80 373964. 0.3303
|
|
81.80 0.4319 0.7531 0.0487 0.0279 7.190 45.319 24.825 5361.774 5.120 110.420 2.100 0.80 374649. 0.3070
|
|
86.35 0.4559 0.7679 0.0445 0.0264 6.801 42.868 22.684 5071.793 4.843 100.898 2.029 0.80 375363. 0.2835
|
|
90.89 0.4799 0.7792 0.0402 0.0248 6.374 40.174 20.491 4753.023 4.539 91.146 1.955 0.80 376106. 0.2597
|
|
95.44 0.5039 0.7862 0.0358 0.0229 5.909 37.246 18.256 4406.648 4.208 81.202 1.879 0.80 376877. 0.2355
|
|
99.98 0.5279 0.7877 0.0314 0.0210 5.410 34.099 15.985 4034.280 3.852 71.103 1.797 0.80 377677. 0.2108
|
|
104.53 0.5519 0.7821 0.0268 0.0189 4.879 30.749 13.689 3638.021 3.474 60.889 1.707 0.81 378505. 0.1853
|
|
109.07 0.5759 0.7662 0.0223 0.0168 4.319 27.220 11.377 3220.448 3.075 50.607 1.602 0.81 379363. 0.1586
|
|
113.61 0.5999 0.7351 0.0178 0.0145 3.734 23.537 9.061 2784.713 2.659 40.303 1.476 0.81 380250. 0.1303
|
|
118.16 0.6239 0.6795 0.0132 0.0122 3.131 19.733 6.752 2334.650 2.229 30.032 1.312 0.81 381166. 0.1000
|
|
122.70 0.6479 0.5810 0.0088 0.0098 2.514 15.846 4.464 1874.755 1.790 19.856 1.080 0.81 382111. 0.0669
|
|
127.25 0.6719 0.3969 0.0043 0.0073 1.891 11.919 2.212 1410.152 1.347 9.840 0.712 0.81 383084. 0.0310
|
|
131.79 0.6959 0.0009 0.0000 0.0049 1.265 7.974 0.003 943.380 0.901 0.014 0.002 0.81 384064. 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 0.0974 0.0380 13.034 74.684 60.065 9719.603 8.438 267.170 2.803 0.87 403101. 0.6373
|
|
5.01 0.0240 0.0605 0.0962 0.0383 13.113 75.133 59.365 9778.066 8.489 264.055 2.754 0.87 403363. 0.6225
|
|
10.02 0.0481 0.1188 0.0950 0.0384 13.176 75.497 58.583 9825.406 8.530 260.577 2.704 0.87 403650. 0.6073
|
|
15.02 0.0721 0.1749 0.0935 0.0386 13.222 75.759 57.714 9859.558 8.559 256.711 2.655 0.87 403962. 0.5918
|
|
20.03 0.0962 0.2288 0.0920 0.0387 13.247 75.906 56.751 9878.604 8.576 252.427 2.606 0.87 404299. 0.5759
|
|
25.04 0.1202 0.2806 0.0903 0.0387 13.250 75.921 55.687 9880.608 8.578 247.697 2.556 0.87 404664. 0.5597
|
|
30.05 0.1442 0.3303 0.0884 0.0386 13.227 75.791 54.518 9863.611 8.563 242.494 2.507 0.87 405056. 0.5431
|
|
35.06 0.1683 0.3777 0.0863 0.0384 13.176 75.499 53.236 9825.665 8.530 236.794 2.457 0.87 405477. 0.5260
|
|
40.07 0.1923 0.4229 0.0840 0.0382 13.095 75.031 51.838 9764.766 8.477 230.575 2.408 0.87 405927. 0.5086
|
|
45.07 0.2164 0.4660 0.0816 0.0379 12.980 74.371 50.319 9678.871 8.402 223.818 2.358 0.87 406407. 0.4907
|
|
50.08 0.2404 0.5067 0.0789 0.0374 12.828 73.503 48.675 9565.876 8.304 216.508 2.308 0.88 406917. 0.4724
|
|
55.09 0.2644 0.5452 0.0760 0.0369 12.637 72.410 46.905 9423.641 8.181 208.633 2.258 0.88 407458. 0.4536
|
|
60.10 0.2885 0.5814 0.0729 0.0362 12.404 71.075 45.006 9249.933 8.030 200.185 2.207 0.88 408030. 0.4343
|
|
65.11 0.3125 0.6153 0.0697 0.0354 12.126 69.479 42.975 9042.242 7.850 191.152 2.156 0.88 408633. 0.4146
|
|
70.11 0.3366 0.6467 0.0661 0.0344 11.799 67.604 40.812 8798.169 7.638 181.531 2.104 0.88 409267. 0.3943
|
|
75.12 0.3606 0.6757 0.0624 0.0333 11.421 65.441 38.524 8516.642 7.393 171.357 2.052 0.88 409933. 0.3736
|
|
80.13 0.3846 0.7020 0.0586 0.0321 10.996 63.004 36.124 8199.563 7.118 160.681 1.998 0.88 410630. 0.3524
|
|
85.14 0.4087 0.7249 0.0545 0.0307 10.530 60.336 33.623 7852.309 6.817 149.554 1.942 0.88 411358. 0.3304
|
|
90.15 0.4327 0.7441 0.0503 0.0292 10.024 57.439 31.031 7475.233 6.489 138.026 1.883 0.88 412118. 0.3077
|
|
95.16 0.4567 0.7591 0.0460 0.0277 9.480 54.318 28.360 7069.060 6.137 126.145 1.820 0.88 412909. 0.2843
|
|
100.16 0.4808 0.7680 0.0415 0.0260 8.909 51.048 25.619 6643.542 5.767 113.954 1.749 0.88 413731. 0.2597
|
|
105.17 0.5048 0.7704 0.0370 0.0242 8.307 47.599 22.820 6194.741 5.378 101.504 1.671 0.88 414585. 0.2342
|
|
110.18 0.5289 0.7651 0.0324 0.0224 7.670 43.950 19.976 5719.817 4.965 88.852 1.584 0.88 415470. 0.2077
|
|
115.19 0.5529 0.7498 0.0277 0.0204 7.004 40.134 17.098 5223.150 4.534 76.051 1.485 0.89 416386. 0.1801
|
|
120.20 0.5769 0.7205 0.0230 0.0184 6.317 36.194 14.199 4710.444 4.089 63.158 1.367 0.89 417335. 0.1512
|
|
125.20 0.6010 0.6715 0.0183 0.0164 5.616 32.177 11.295 4187.556 3.635 50.239 1.223 0.89 418314. 0.1206
|
|
130.21 0.6250 0.5942 0.0136 0.0143 4.909 28.130 8.401 3660.890 3.178 37.367 1.041 0.89 419326. 0.0885
|
|
135.22 0.6491 0.4744 0.0090 0.0123 4.208 24.109 5.536 3137.593 2.724 24.625 0.800 0.89 420370. 0.0552
|
|
140.23 0.6731 0.2891 0.0044 0.0103 3.520 20.168 2.722 2624.672 2.279 12.106 0.470 0.89 421445. 0.0228
|
|
145.24 0.6971 -0.0051 -0.0001 0.0083 2.844 16.297 -0.037 2120.902 1.841 -0.166 -0.008 0.89 422533. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 12000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.0970 0.0455 20.240 106.306 71.189 15092.655 12.010 316.647 2.139 0.95 439754. 0.5296
|
|
5.58 0.0246 0.0515 0.0960 0.0458 20.370 106.990 70.497 15189.873 12.088 313.570 2.105 0.95 440039. 0.5185
|
|
11.16 0.0491 0.1013 0.0949 0.0460 20.473 107.531 69.711 15266.578 12.149 310.073 2.071 0.95 440351. 0.5073
|
|
16.74 0.0737 0.1496 0.0937 0.0462 20.541 107.888 68.819 15317.301 12.189 306.109 2.038 0.95 440692. 0.4960
|
|
22.32 0.0982 0.1962 0.0924 0.0462 20.567 108.023 67.812 15336.521 12.204 301.628 2.006 0.95 441063. 0.4845
|
|
27.90 0.1228 0.2415 0.0908 0.0462 20.543 107.900 66.677 15318.953 12.190 296.578 1.974 0.95 441465. 0.4729
|
|
33.48 0.1473 0.2853 0.0891 0.0460 20.464 107.482 65.403 15259.724 12.143 290.911 1.944 0.95 441901. 0.4612
|
|
39.06 0.1719 0.3279 0.0871 0.0457 20.323 106.742 63.980 15154.674 12.060 284.583 1.915 0.95 442370. 0.4494
|
|
44.64 0.1964 0.3693 0.0850 0.0452 20.116 105.657 62.399 15000.569 11.937 277.552 1.887 0.95 442873. 0.4373
|
|
50.22 0.2210 0.4094 0.0826 0.0446 19.840 104.209 60.653 14795.019 11.773 269.786 1.859 0.95 443412. 0.4249
|
|
55.80 0.2455 0.4483 0.0800 0.0438 19.494 102.388 58.736 14536.509 11.568 261.258 1.833 0.95 443987. 0.4121
|
|
61.38 0.2701 0.4860 0.0771 0.0429 19.075 100.188 56.643 14224.099 11.319 251.948 1.806 0.96 444597. 0.3988
|
|
66.96 0.2946 0.5224 0.0741 0.0418 18.583 97.605 54.371 13857.316 11.027 241.842 1.780 0.96 445244. 0.3850
|
|
72.54 0.3192 0.5574 0.0707 0.0405 18.018 94.636 51.917 13435.801 10.692 230.927 1.753 0.96 445926. 0.3705
|
|
78.12 0.3437 0.5907 0.0671 0.0391 17.379 91.281 49.281 12959.590 10.313 219.204 1.725 0.96 446645. 0.3552
|
|
83.70 0.3683 0.6223 0.0633 0.0375 16.670 87.558 46.476 12430.962 9.892 206.727 1.696 0.96 447401. 0.3392
|
|
89.28 0.3929 0.6518 0.0593 0.0357 15.895 83.489 43.518 11853.221 9.432 193.570 1.665 0.96 448192. 0.3223
|
|
94.86 0.4174 0.6783 0.0551 0.0339 15.076 79.187 40.424 11242.446 8.946 179.808 1.631 0.96 449019. 0.3042
|
|
100.44 0.4420 0.7003 0.0507 0.0320 14.232 74.751 37.209 10612.764 8.445 165.505 1.590 0.96 449882. 0.2846
|
|
106.02 0.4665 0.7168 0.0462 0.0300 13.366 70.202 33.888 9966.830 7.931 150.733 1.542 0.96 450780. 0.2634
|
|
111.61 0.4911 0.7248 0.0415 0.0281 12.513 65.722 30.475 9330.859 7.425 135.551 1.481 0.96 451713. 0.2399
|
|
117.19 0.5156 0.7137 0.0367 0.0265 11.809 62.026 26.971 8806.037 7.008 119.966 1.389 0.96 452682. 0.2117
|
|
122.77 0.5402 0.6904 0.0319 0.0250 11.103 58.316 23.415 8279.377 6.589 104.150 1.283 0.97 453687. 0.1821
|
|
128.35 0.5647 0.6532 0.0270 0.0234 10.390 54.574 19.830 7748.074 6.166 88.205 1.161 0.97 454727. 0.1517
|
|
133.93 0.5893 0.5990 0.0221 0.0218 9.682 50.853 16.240 7219.746 5.745 72.237 1.020 0.97 455803. 0.1206
|
|
139.51 0.6138 0.5245 0.0173 0.0202 8.988 47.206 12.673 6702.077 5.333 56.369 0.858 0.97 456915. 0.0896
|
|
145.09 0.6384 0.4260 0.0125 0.0187 8.318 43.690 9.160 6202.797 4.936 40.742 0.670 0.97 458063. 0.0595
|
|
150.67 0.6629 0.3000 0.0078 0.0173 7.678 40.329 5.733 5725.717 4.556 25.500 0.454 0.97 459249. 0.0319
|
|
156.25 0.6875 0.1424 0.0033 0.0159 7.070 37.135 2.417 5272.233 4.196 10.751 0.208 0.97 460478. 0.0095
|
|
161.83 0.7120
|
|
|
|
|
|
|