464 lines
82 KiB
Plaintext
464 lines
82 KiB
Plaintext
20x12WE (20x12WE.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 0.0984 0.0390 0.010 0.633 0.502 7.487 0.071 2.231 30.384 0.08 39956. 0.6313
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0.49 0.0258 0.0633 0.0970 0.0395 0.010 0.641 0.495 7.588 0.072 2.200 29.560 0.08 39985. 0.6099
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0.98 0.0516 0.1231 0.0955 0.0400 0.010 0.649 0.487 7.683 0.073 2.165 28.739 0.08 40016. 0.5883
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1.47 0.0774 0.1794 0.0938 0.0405 0.010 0.657 0.478 7.772 0.074 2.128 27.925 0.08 40050. 0.5667
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1.95 0.1031 0.2322 0.0921 0.0409 0.011 0.664 0.469 7.851 0.075 2.088 27.119 0.08 40087. 0.5451
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2.44 0.1289 0.2818 0.0901 0.0412 0.011 0.669 0.460 7.919 0.076 2.044 26.324 0.08 40127. 0.5236
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2.93 0.1547 0.3281 0.0880 0.0415 0.011 0.674 0.449 7.973 0.076 1.997 25.541 0.08 40170. 0.5021
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3.42 0.1805 0.3712 0.0858 0.0417 0.011 0.677 0.437 8.011 0.076 1.946 24.771 0.08 40216. 0.4807
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3.91 0.2063 0.4113 0.0834 0.0418 0.011 0.679 0.425 8.031 0.077 1.891 24.014 0.08 40265. 0.4594
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4.40 0.2321 0.4484 0.0808 0.0418 0.011 0.679 0.412 8.030 0.077 1.832 23.270 0.08 40318. 0.4382
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4.88 0.2578 0.4825 0.0780 0.0417 0.011 0.677 0.398 8.006 0.076 1.770 22.539 0.08 40374. 0.4171
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5.37 0.2836 0.5138 0.0751 0.0414 0.011 0.672 0.383 7.956 0.076 1.702 21.820 0.08 40434. 0.3960
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5.86 0.3094 0.5423 0.0719 0.0410 0.011 0.666 0.367 7.879 0.075 1.631 21.110 0.08 40497. 0.3750
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6.35 0.3352 0.5680 0.0686 0.0405 0.010 0.657 0.350 7.772 0.074 1.555 20.407 0.08 40564. 0.3540
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6.84 0.3610 0.5907 0.0650 0.0398 0.010 0.645 0.332 7.633 0.073 1.475 19.709 0.08 40634. 0.3330
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7.33 0.3868 0.6105 0.0613 0.0389 0.010 0.631 0.313 7.461 0.071 1.391 19.010 0.08 40708. 0.3119
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7.81 0.4126 0.6271 0.0574 0.0378 0.010 0.613 0.293 7.256 0.069 1.303 18.307 0.08 40786. 0.2907
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8.30 0.4383 0.6403 0.0534 0.0366 0.009 0.593 0.272 7.021 0.067 1.211 17.593 0.08 40867. 0.2693
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8.79 0.4641 0.6497 0.0492 0.0352 0.009 0.571 0.251 6.754 0.065 1.117 16.860 0.08 40952. 0.2479
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9.28 0.4899 0.6549 0.0450 0.0336 0.009 0.546 0.229 6.459 0.062 1.020 16.100 0.08 41041. 0.2262
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9.77 0.5157 0.6551 0.0406 0.0320 0.008 0.519 0.207 6.135 0.059 0.921 15.301 0.08 41134. 0.2042
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10.26 0.5415 0.6496 0.0361 0.0301 0.008 0.489 0.184 5.784 0.055 0.820 14.449 0.08 41230. 0.1820
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10.74 0.5673 0.6370 0.0316 0.0282 0.007 0.457 0.161 5.407 0.052 0.717 13.525 0.08 41329. 0.1593
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11.23 0.5930 0.6157 0.0271 0.0261 0.007 0.423 0.138 5.004 0.048 0.614 12.504 0.08 41433. 0.1363
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11.72 0.6188 0.5831 0.0225 0.0238 0.006 0.387 0.115 4.579 0.044 0.510 11.348 0.08 41540. 0.1127
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12.21 0.6446 0.5355 0.0179 0.0215 0.006 0.349 0.091 4.131 0.039 0.405 10.004 0.08 41651. 0.0886
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12.70 0.6704 0.4670 0.0133 0.0191 0.005 0.310 0.068 3.665 0.035 0.302 8.389 0.08 41765. 0.0641
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13.19 0.6962 0.3680 0.0088 0.0166 0.004 0.269 0.045 3.182 0.030 0.199 6.366 0.08 41883. 0.0395
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13.67 0.7220 0.2217 0.0043 0.0140 0.004 0.227 0.022 2.685 0.026 0.097 3.698 0.08 42005. 0.0161
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14.16 0.7478 -0.0051 -0.0001 0.0113 0.003 0.184 0.000 2.178 0.021 -0.002 -0.083 0.08 42130. 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 0.0987 0.0364 0.075 2.365 2.014 55.956 0.267 8.958 16.325 0.16 79911. 0.6797
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0.98 0.0259 0.0681 0.0974 0.0370 0.076 2.401 1.986 56.820 0.271 8.833 15.852 0.16 79969. 0.6554
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1.96 0.0518 0.1322 0.0959 0.0375 0.077 2.436 1.955 57.646 0.275 8.697 15.384 0.16 80031. 0.6311
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2.94 0.0776 0.1924 0.0942 0.0380 0.078 2.469 1.922 58.415 0.279 8.548 14.921 0.16 80100. 0.6069
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3.92 0.1035 0.2487 0.0924 0.0385 0.079 2.498 1.885 59.113 0.282 8.386 14.466 0.16 80174. 0.5828
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4.90 0.1294 0.3013 0.0905 0.0389 0.080 2.524 1.846 59.719 0.285 8.211 14.020 0.16 80254. 0.5589
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5.88 0.1553 0.3503 0.0884 0.0392 0.081 2.545 1.803 60.216 0.288 8.021 13.583 0.16 80340. 0.5352
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6.86 0.1812 0.3958 0.0862 0.0394 0.081 2.560 1.757 60.582 0.289 7.816 13.157 0.16 80433. 0.5117
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7.84 0.2071 0.4381 0.0837 0.0396 0.082 2.569 1.708 60.799 0.290 7.596 12.740 0.16 80532. 0.4885
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8.82 0.2329 0.4771 0.0811 0.0396 0.082 2.571 1.655 60.846 0.291 7.360 12.334 0.16 80638. 0.4655
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9.80 0.2588 0.5131 0.0783 0.0395 0.081 2.565 1.598 60.703 0.290 7.107 11.938 0.16 80752. 0.4427
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10.78 0.2847 0.5461 0.0754 0.0393 0.081 2.550 1.537 60.350 0.288 6.837 11.552 0.16 80872. 0.4202
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11.76 0.3106 0.5763 0.0722 0.0389 0.080 2.526 1.472 59.769 0.285 6.549 11.174 0.16 80999. 0.3978
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12.74 0.3365 0.6036 0.0688 0.0384 0.079 2.491 1.404 58.940 0.281 6.244 10.803 0.16 81134. 0.3755
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13.73 0.3623 0.6281 0.0653 0.0377 0.078 2.444 1.331 57.841 0.276 5.921 10.439 0.16 81275. 0.3534
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14.71 0.3882 0.6498 0.0615 0.0368 0.076 2.386 1.255 56.466 0.270 5.581 10.079 0.16 81425. 0.3312
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15.69 0.4141 0.6685 0.0576 0.0357 0.074 2.317 1.175 54.818 0.262 5.226 9.721 0.16 81581. 0.3091
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16.67 0.4400 0.6840 0.0535 0.0344 0.071 2.236 1.092 52.906 0.253 4.857 9.362 0.16 81745. 0.2870
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17.65 0.4659 0.6961 0.0493 0.0330 0.068 2.144 1.007 50.736 0.242 4.477 8.998 0.16 81916. 0.2648
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18.63 0.4918 0.7043 0.0450 0.0315 0.065 2.042 0.919 48.314 0.231 4.087 8.625 0.16 82095. 0.2425
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19.61 0.5176 0.7081 0.0406 0.0297 0.061 1.929 0.829 45.648 0.218 3.688 8.238 0.16 82281. 0.2201
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20.59 0.5435 0.7066 0.0362 0.0278 0.057 1.806 0.738 42.746 0.204 3.282 7.828 0.16 82475. 0.1973
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21.57 0.5694 0.6986 0.0316 0.0258 0.053 1.674 0.645 39.617 0.189 2.870 7.388 0.16 82675. 0.1741
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22.55 0.5953 0.6823 0.0271 0.0236 0.049 1.533 0.552 36.271 0.173 2.455 6.902 0.16 82884. 0.1504
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23.53 0.6212 0.6550 0.0225 0.0213 0.044 1.383 0.458 32.723 0.156 2.038 6.350 0.16 83099. 0.1261
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24.51 0.6471 0.6125 0.0179 0.0189 0.039 1.225 0.364 28.987 0.138 1.620 5.701 0.16 83323. 0.1009
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25.49 0.6729 0.5475 0.0133 0.0163 0.034 1.060 0.271 25.084 0.120 1.205 4.899 0.16 83553. 0.0748
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26.47 0.6988 0.4468 0.0088 0.0137 0.028 0.889 0.179 21.037 0.100 0.794 3.851 0.16 83791. 0.0477
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27.45 0.7247 0.2840 0.0043 0.0110 0.023 0.713 0.088 16.873 0.081 0.390 2.360 0.16 84037. 0.0205
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28.43 0.7506 -0.0046 -0.0001 0.0082 0.017 0.533 -0.001 12.616 0.060 -0.005 -0.037 0.16 84287. 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 0.0992 0.0354 0.246 5.174 4.551 183.635 0.585 20.243 11.241 0.24 119863. 0.7035
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1.47 0.0259 0.0704 0.0978 0.0360 0.250 5.259 4.488 186.657 0.594 19.962 10.905 0.24 119950. 0.6778
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2.95 0.0518 0.1365 0.0963 0.0366 0.254 5.340 4.419 189.548 0.603 19.655 10.574 0.24 120044. 0.6521
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4.42 0.0778 0.1985 0.0947 0.0371 0.258 5.417 4.344 192.253 0.612 19.321 10.248 0.24 120147. 0.6266
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5.89 0.1037 0.2564 0.0929 0.0376 0.261 5.486 4.262 194.713 0.620 18.957 9.928 0.24 120259. 0.6013
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7.36 0.1296 0.3104 0.0909 0.0380 0.264 5.546 4.173 196.865 0.627 18.562 9.615 0.24 120379. 0.5763
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8.84 0.1555 0.3606 0.0888 0.0383 0.266 5.597 4.077 198.642 0.632 18.135 9.310 0.24 120509. 0.5515
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10.31 0.1814 0.4073 0.0866 0.0386 0.268 5.634 3.973 199.977 0.637 17.674 9.012 0.24 120648. 0.5270
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11.78 0.2074 0.4505 0.0841 0.0387 0.269 5.657 3.862 200.800 0.639 17.176 8.723 0.24 120798. 0.5029
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13.25 0.2333 0.4905 0.0815 0.0388 0.270 5.664 3.742 201.039 0.640 16.643 8.441 0.24 120958. 0.4790
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14.73 0.2592 0.5274 0.0787 0.0387 0.269 5.652 3.613 200.625 0.639 16.071 8.168 0.24 121128. 0.4555
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16.20 0.2851 0.5613 0.0757 0.0385 0.268 5.621 3.476 199.492 0.635 15.460 7.903 0.24 121309. 0.4323
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17.67 0.3110 0.5923 0.0726 0.0381 0.265 5.566 3.330 197.572 0.629 14.811 7.644 0.24 121500. 0.4092
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19.15 0.3370 0.6204 0.0692 0.0376 0.261 5.488 3.175 194.795 0.620 14.121 7.392 0.24 121703. 0.3864
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20.62 0.3629 0.6459 0.0656 0.0369 0.256 5.384 3.010 191.089 0.608 13.390 7.145 0.24 121916. 0.3637
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22.09 0.3888 0.6685 0.0618 0.0360 0.250 5.252 2.837 186.426 0.593 12.620 6.903 0.24 122141. 0.3411
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23.56 0.4147 0.6883 0.0579 0.0349 0.242 5.094 2.656 180.820 0.576 11.816 6.663 0.24 122377. 0.3186
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25.04 0.4406 0.7052 0.0538 0.0336 0.234 4.911 2.469 174.293 0.555 10.981 6.425 0.24 122623. 0.2962
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26.51 0.4666 0.7187 0.0496 0.0322 0.224 4.701 2.275 166.865 0.531 10.120 6.185 0.24 122881. 0.2737
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27.98 0.4925 0.7287 0.0453 0.0306 0.213 4.467 2.077 158.560 0.505 9.237 5.940 0.24 123150. 0.2511
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29.45 0.5184 0.7345 0.0408 0.0288 0.200 4.209 1.874 149.401 0.476 8.334 5.688 0.24 123430. 0.2284
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30.93 0.5443 0.7354 0.0363 0.0269 0.187 3.928 1.667 139.414 0.444 7.415 5.424 0.24 123721. 0.2055
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32.40 0.5702 0.7302 0.0318 0.0248 0.172 3.624 1.458 128.630 0.409 6.485 5.141 0.24 124023. 0.1821
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33.87 0.5962 0.7172 0.0272 0.0226 0.157 3.299 1.247 117.088 0.373 5.546 4.830 0.24 124336. 0.1582
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35.35 0.6221 0.6937 0.0225 0.0202 0.141 2.954 1.035 104.833 0.334 4.603 4.477 0.24 124661. 0.1336
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36.82 0.6480 0.6553 0.0179 0.0177 0.123 2.590 0.823 91.922 0.293 3.659 4.060 0.24 124996. 0.1080
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38.29 0.6739 0.5940 0.0133 0.0151 0.105 2.209 0.612 78.422 0.250 2.721 3.539 0.24 125343. 0.0812
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39.76 0.6998 0.4950 0.0088 0.0124 0.086 1.815 0.403 64.419 0.205 1.794 2.840 0.24 125702. 0.0529
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41.24 0.7258 0.3254 0.0043 0.0096 0.067 1.409 0.198 50.009 0.159 0.883 1.800 0.24 126071. 0.0235
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42.71 0.7517 -0.0046 0.0000 0.0068 0.047 0.994 -0.002 35.265 0.112 -0.008 -0.024 0.24 126445. 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 0.0997 0.0350 0.576 9.081 8.135 429.761 1.026 36.182 8.585 0.32 159811. 0.7184
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1.96 0.0259 0.0717 0.0983 0.0356 0.586 9.236 8.023 437.107 1.044 35.686 8.325 0.32 159927. 0.6918
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3.93 0.0519 0.1390 0.0968 0.0361 0.596 9.385 7.901 444.148 1.060 35.142 8.068 0.32 160053. 0.6653
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5.89 0.0778 0.2020 0.0952 0.0367 0.604 9.525 7.767 450.744 1.076 34.549 7.816 0.32 160191. 0.6391
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7.86 0.1037 0.2608 0.0934 0.0372 0.613 9.652 7.622 456.756 1.090 33.904 7.569 0.32 160340. 0.6131
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9.82 0.1297 0.3156 0.0915 0.0376 0.620 9.763 7.465 462.031 1.103 33.202 7.328 0.32 160501. 0.5874
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11.79 0.1556 0.3666 0.0894 0.0380 0.625 9.855 7.294 466.409 1.113 32.442 7.093 0.32 160674. 0.5620
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13.75 0.1816 0.4139 0.0871 0.0382 0.630 9.926 7.109 469.724 1.121 31.620 6.864 0.32 160861. 0.5370
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15.72 0.2075 0.4578 0.0847 0.0384 0.633 9.970 6.910 471.808 1.126 30.734 6.643 0.32 161061. 0.5123
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17.68 0.2334 0.4983 0.0821 0.0384 0.634 9.984 6.696 472.488 1.128 29.782 6.428 0.32 161274. 0.4879
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19.65 0.2594 0.5357 0.0793 0.0384 0.632 9.965 6.466 471.597 1.126 28.762 6.219 0.32 161502. 0.4640
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21.61 0.2853 0.5701 0.0763 0.0382 0.629 9.910 6.221 468.971 1.120 27.672 6.017 0.32 161743. 0.4403
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23.58 0.3112 0.6017 0.0731 0.0378 0.623 9.814 5.960 464.449 1.109 26.511 5.821 0.32 162000. 0.4169
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25.54 0.3372 0.6304 0.0697 0.0373 0.614 9.675 5.683 457.860 1.093 25.278 5.630 0.32 162270. 0.3937
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27.51 0.3631 0.6565 0.0661 0.0365 0.602 9.488 5.389 449.029 1.072 23.970 5.443 0.32 162555. 0.3707
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29.47 0.3891 0.6798 0.0623 0.0356 0.587 9.253 5.079 437.884 1.045 22.593 5.261 0.32 162855. 0.3479
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31.44 0.4150 0.7004 0.0583 0.0345 0.569 8.969 4.756 424.454 1.013 21.153 5.082 0.32 163170. 0.3251
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33.40 0.4409 0.7181 0.0542 0.0333 0.548 8.638 4.420 408.787 0.976 19.659 4.904 0.32 163500. 0.3025
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35.37 0.4669 0.7328 0.0499 0.0318 0.524 8.261 4.073 390.934 0.933 18.118 4.726 0.32 163844. 0.2798
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37.33 0.4928 0.7440 0.0456 0.0302 0.497 7.838 3.718 370.948 0.886 16.536 4.546 0.32 164203. 0.2571
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39.30 0.5187 0.7512 0.0411 0.0284 0.468 7.372 3.354 348.883 0.833 14.919 4.361 0.32 164577. 0.2343
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41.26 0.5447 0.7539 0.0366 0.0264 0.436 6.863 2.984 324.802 0.775 13.274 4.167 0.32 164966. 0.2112
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43.23 0.5706 0.7507 0.0320 0.0243 0.401 6.313 2.610 298.782 0.713 11.607 3.961 0.32 165369. 0.1877
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45.19 0.5965 0.7402 0.0274 0.0220 0.363 5.725 2.231 270.912 0.647 9.926 3.736 0.32 165788. 0.1637
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47.16 0.6225 0.7196 0.0227 0.0196 0.324 5.099 1.852 241.304 0.576 8.236 3.481 0.32 166221. 0.1390
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49.12 0.6484 0.6844 0.0180 0.0171 0.282 4.439 1.472 210.097 0.502 6.548 3.178 0.32 166669. 0.1131
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51.09 0.6744 0.6266 0.0134 0.0144 0.238 3.750 1.095 177.459 0.424 4.869 2.798 0.32 167132. 0.0859
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53.05 0.7003 0.5300 0.0088 0.0117 0.193 3.034 0.721 143.594 0.343 3.209 2.279 0.33 167610. 0.0568
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55.02 0.7262 0.3570 0.0044 0.0088 0.146 2.298 0.355 108.743 0.260 1.579 1.480 0.33 168103. 0.0259
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56.98 0.7522 -0.0056 0.0000 0.0059 0.098 1.544 -0.004 73.064 0.174 -0.016 -0.023 0.33 168602. 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 0.1004 0.0348 1.121 14.132 12.797 836.012 1.597 56.922 6.943 0.40 199754. 0.7287
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2.46 0.0259 0.0725 0.0990 0.0354 1.141 14.380 12.624 850.686 1.625 56.151 6.731 0.40 199899. 0.7016
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4.91 0.0519 0.1404 0.0975 0.0360 1.160 14.618 12.434 864.763 1.652 55.307 6.522 0.40 200057. 0.6747
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|
7.37 0.0778 0.2040 0.0959 0.0366 1.177 14.842 12.227 877.968 1.677 54.385 6.317 0.40 200229. 0.6480
|
|
9.82 0.1037 0.2633 0.0941 0.0371 1.194 15.045 12.001 890.019 1.700 53.379 6.116 0.40 200415. 0.6216
|
|
12.28 0.1297 0.3186 0.0922 0.0375 1.208 15.224 11.755 900.615 1.720 52.285 5.920 0.40 200617. 0.5955
|
|
14.73 0.1556 0.3701 0.0901 0.0379 1.220 15.374 11.488 909.436 1.737 51.098 5.729 0.40 200834. 0.5697
|
|
17.19 0.1815 0.4178 0.0879 0.0382 1.229 15.487 11.199 916.154 1.750 49.813 5.544 0.40 201068. 0.5443
|
|
19.64 0.2074 0.4620 0.0854 0.0383 1.234 15.559 10.887 920.429 1.758 48.426 5.365 0.40 201318. 0.5193
|
|
22.10 0.2334 0.5030 0.0828 0.0384 1.236 15.585 10.552 921.922 1.761 46.934 5.191 0.40 201585. 0.4947
|
|
24.56 0.2593 0.5408 0.0800 0.0383 1.234 15.557 10.192 920.298 1.758 45.334 5.023 0.40 201870. 0.4705
|
|
27.01 0.2852 0.5756 0.0769 0.0381 1.227 15.471 9.808 915.229 1.748 43.624 4.860 0.40 202173. 0.4466
|
|
29.47 0.3112 0.6075 0.0737 0.0378 1.215 15.322 9.398 906.397 1.731 41.801 4.703 0.40 202493. 0.4230
|
|
31.92 0.3371 0.6367 0.0703 0.0372 1.198 15.104 8.962 893.464 1.706 39.863 4.550 0.40 202832. 0.3996
|
|
34.38 0.3630 0.6632 0.0667 0.0365 1.175 14.810 8.500 876.081 1.673 37.808 4.401 0.40 203189. 0.3764
|
|
36.83 0.3890 0.6871 0.0629 0.0356 1.145 14.438 8.013 854.092 1.631 35.641 4.255 0.40 203564. 0.3534
|
|
39.29 0.4149 0.7084 0.0589 0.0345 1.110 13.989 7.503 827.546 1.580 33.376 4.113 0.40 203958. 0.3305
|
|
41.74 0.4408 0.7268 0.0547 0.0332 1.068 13.465 6.975 796.537 1.521 31.023 3.972 0.40 204370. 0.3077
|
|
44.20 0.4668 0.7423 0.0504 0.0317 1.021 12.867 6.429 761.165 1.454 28.595 3.831 0.40 204801. 0.2850
|
|
46.66 0.4927 0.7545 0.0460 0.0301 0.968 12.197 5.868 721.531 1.378 26.102 3.689 0.40 205250. 0.2622
|
|
49.11 0.5186 0.7630 0.0415 0.0282 0.909 11.457 5.295 677.744 1.294 23.553 3.544 0.40 205717. 0.2392
|
|
51.57 0.5445 0.7670 0.0370 0.0262 0.845 10.649 4.712 629.929 1.203 20.960 3.393 0.40 206203. 0.2161
|
|
54.02 0.5705 0.7656 0.0323 0.0241 0.775 9.775 4.121 578.233 1.104 18.332 3.233 0.40 206708. 0.1925
|
|
56.48 0.5964 0.7572 0.0277 0.0218 0.701 8.838 3.525 522.839 0.999 15.680 3.058 0.40 207231. 0.1684
|
|
58.93 0.6223 0.7391 0.0230 0.0193 0.622 7.843 2.926 463.969 0.886 13.016 2.861 0.40 207773. 0.1436
|
|
61.39 0.6483 0.7069 0.0183 0.0167 0.539 6.794 2.327 401.898 0.768 10.352 2.627 0.41 208333. 0.1176
|
|
63.84 0.6742 0.6525 0.0136 0.0140 0.452 5.696 1.732 336.964 0.644 7.703 2.331 0.41 208912. 0.0900
|
|
66.30 0.7001 0.5591 0.0090 0.0112 0.362 4.557 1.143 269.578 0.515 5.085 1.923 0.41 209509. 0.0603
|
|
68.76 0.7261 0.3858 0.0044 0.0083 0.269 3.385 0.565 200.223 0.382 2.513 1.280 0.41 210125. 0.0282
|
|
71.21 0.7520 -0.0006 0.0000 0.0054 0.173 2.184 -0.001 129.205 0.247 -0.002 -0.002 0.41 210748. 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 0.1012 0.0349 1.942 20.397 18.583 1447.957 2.304 82.657 5.821 0.48 239689. 0.7362
|
|
2.95 0.0259 0.0729 0.0999 0.0355 1.977 20.763 18.336 1473.929 2.346 81.559 5.643 0.48 239863. 0.7089
|
|
5.89 0.0519 0.1412 0.0984 0.0361 2.010 21.115 18.065 1498.859 2.386 80.353 5.467 0.48 240053. 0.6817
|
|
8.84 0.0778 0.2052 0.0968 0.0367 2.041 21.444 17.768 1522.264 2.423 79.032 5.294 0.48 240260. 0.6547
|
|
11.79 0.1037 0.2649 0.0950 0.0372 2.070 21.745 17.444 1543.643 2.457 77.589 5.125 0.48 240484. 0.6280
|
|
14.73 0.1297 0.3205 0.0931 0.0377 2.095 22.011 17.090 1562.465 2.487 76.017 4.961 0.48 240727. 0.6017
|
|
17.68 0.1556 0.3722 0.0910 0.0380 2.116 22.232 16.706 1578.163 2.512 74.308 4.801 0.48 240988. 0.5757
|
|
20.63 0.1815 0.4202 0.0887 0.0383 2.132 22.401 16.289 1590.156 2.531 72.456 4.646 0.48 241269. 0.5502
|
|
23.58 0.2075 0.4647 0.0863 0.0385 2.143 22.509 15.839 1597.845 2.543 70.454 4.496 0.48 241570. 0.5250
|
|
26.52 0.2334 0.5059 0.0836 0.0386 2.146 22.548 15.355 1600.630 2.547 68.297 4.351 0.48 241892. 0.5002
|
|
29.47 0.2593 0.5440 0.0808 0.0385 2.143 22.510 14.834 1597.918 2.543 65.982 4.211 0.48 242235. 0.4758
|
|
32.42 0.2853 0.5791 0.0778 0.0383 2.131 22.386 14.277 1589.134 2.529 63.504 4.075 0.48 242599. 0.4517
|
|
35.36 0.3112 0.6114 0.0745 0.0379 2.110 22.169 13.683 1573.715 2.505 60.861 3.944 0.48 242984. 0.4280
|
|
38.31 0.3371 0.6409 0.0711 0.0374 2.080 21.850 13.051 1551.074 2.469 58.049 3.816 0.48 243392. 0.4045
|
|
41.26 0.3631 0.6679 0.0674 0.0367 2.039 21.421 12.380 1520.592 2.420 55.064 3.693 0.48 243821. 0.3812
|
|
44.20 0.3890 0.6922 0.0636 0.0357 1.987 20.877 11.672 1481.975 2.359 51.915 3.572 0.48 244272. 0.3580
|
|
47.15 0.4149 0.7140 0.0595 0.0346 1.925 20.219 10.931 1435.298 2.284 48.620 3.454 0.48 244746. 0.3351
|
|
50.10 0.4409 0.7331 0.0554 0.0333 1.852 19.450 10.161 1380.728 2.197 45.196 3.338 0.48 245241. 0.3122
|
|
53.04 0.4668 0.7493 0.0510 0.0318 1.768 18.573 9.366 1318.439 2.098 41.661 3.222 0.48 245758. 0.2893
|
|
55.99 0.4927 0.7624 0.0466 0.0301 1.674 17.589 8.550 1248.609 1.987 38.029 3.106 0.48 246298. 0.2664
|
|
58.94 0.5187 0.7718 0.0420 0.0282 1.571 16.502 7.715 1171.430 1.864 34.316 2.987 0.48 246860. 0.2434
|
|
61.89 0.5446 0.7771 0.0374 0.0262 1.458 15.314 6.865 1087.123 1.730 30.535 2.864 0.48 247443. 0.2202
|
|
64.83 0.5705 0.7771 0.0327 0.0240 1.336 14.030 6.003 995.951 1.585 26.703 2.734 0.48 248049. 0.1965
|
|
67.78 0.5965 0.7703 0.0280 0.0217 1.205 12.653 5.134 898.233 1.430 22.836 2.592 0.48 248678. 0.1723
|
|
70.73 0.6224 0.7543 0.0232 0.0192 1.065 11.190 4.260 794.364 1.264 18.950 2.433 0.49 249328. 0.1473
|
|
73.67 0.6483 0.7245 0.0185 0.0165 0.918 9.647 3.387 684.832 1.090 15.064 2.243 0.49 250001. 0.1211
|
|
76.62 0.6743 0.6727 0.0137 0.0137 0.765 8.033 2.518 570.241 0.908 11.200 2.003 0.49 250696. 0.0932
|
|
79.57 0.7002 0.5816 0.0090 0.0109 0.605 6.358 1.659 451.321 0.718 7.379 1.667 0.49 251413. 0.0630
|
|
82.51 0.7261 0.4068 0.0044 0.0079 0.441 4.634 0.815 328.936 0.524 3.627 1.124 0.49 252152. 0.0298
|
|
85.46 0.7521 -0.0083 -0.0001 0.0049 0.273 2.868 -0.010 203.559 0.324 -0.044 -0.022 0.49 252897. 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 0.1023 0.0352 3.107 27.976 25.551 2316.916 3.161 113.653 5.002 0.56 279613. 0.7418
|
|
3.46 0.0261 0.0736 0.1009 0.0358 3.164 28.491 25.217 2359.564 3.219 112.167 4.847 0.56 279818. 0.7142
|
|
6.92 0.0522 0.1425 0.0995 0.0364 3.219 28.985 24.850 2400.526 3.275 110.531 4.695 0.56 280042. 0.6867
|
|
10.39 0.0783 0.2070 0.0978 0.0370 3.271 29.450 24.445 2438.976 3.327 108.733 4.546 0.56 280287. 0.6594
|
|
13.85 0.1044 0.2671 0.0961 0.0376 3.318 29.874 24.003 2474.082 3.375 106.763 4.400 0.56 280551. 0.6325
|
|
17.31 0.1306 0.3231 0.0941 0.0380 3.359 30.246 23.518 2504.951 3.417 104.610 4.258 0.56 280838. 0.6059
|
|
20.77 0.1567 0.3752 0.0920 0.0384 3.394 30.557 22.991 2530.641 3.452 102.264 4.121 0.56 281147. 0.5797
|
|
24.23 0.1828 0.4236 0.0897 0.0387 3.420 30.792 22.418 2550.179 3.479 99.714 3.987 0.56 281479. 0.5539
|
|
27.69 0.2089 0.4684 0.0872 0.0389 3.436 30.942 21.797 2562.569 3.496 96.952 3.858 0.56 281836. 0.5284
|
|
31.16 0.2350 0.5099 0.0846 0.0390 3.442 30.993 21.127 2566.815 3.502 93.972 3.733 0.56 282216. 0.5034
|
|
34.62 0.2611 0.5483 0.0817 0.0389 3.436 30.934 20.406 2561.931 3.495 90.765 3.613 0.56 282621. 0.4788
|
|
38.08 0.2872 0.5837 0.0786 0.0387 3.416 30.754 19.633 2546.969 3.475 87.329 3.496 0.56 283052. 0.4545
|
|
41.54 0.3133 0.6163 0.0753 0.0383 3.381 30.440 18.808 2521.000 3.439 83.658 3.384 0.56 283508. 0.4305
|
|
45.00 0.3395 0.6461 0.0718 0.0377 3.330 29.982 17.929 2483.056 3.387 79.747 3.275 0.56 283990. 0.4068
|
|
48.47 0.3656 0.6734 0.0680 0.0369 3.262 29.367 16.995 2432.124 3.318 75.592 3.169 0.56 284498. 0.3833
|
|
51.93 0.3917 0.6981 0.0641 0.0359 3.175 28.590 16.009 2367.753 3.230 71.206 3.067 0.56 285032. 0.3600
|
|
55.39 0.4178 0.7203 0.0599 0.0348 3.071 27.652 14.976 2290.087 3.124 66.614 2.966 0.56 285592. 0.3368
|
|
58.85 0.4439 0.7397 0.0556 0.0334 2.949 26.557 13.903 2199.406 3.000 61.841 2.867 0.56 286178. 0.3136
|
|
62.31 0.4700 0.7564 0.0512 0.0318 2.811 25.308 12.795 2096.004 2.859 56.912 2.769 0.56 286790. 0.2906
|
|
65.77 0.4961 0.7699 0.0467 0.0301 2.655 23.910 11.656 1980.181 2.701 51.847 2.670 0.56 287428. 0.2674
|
|
69.24 0.5222 0.7798 0.0420 0.0281 2.484 22.365 10.492 1852.267 2.527 46.668 2.569 0.56 288092. 0.2441
|
|
72.70 0.5484 0.7855 0.0372 0.0260 2.297 20.679 9.307 1712.635 2.336 41.396 2.465 0.56 288782. 0.2206
|
|
76.16 0.5745 0.7860 0.0324 0.0237 2.094 18.857 8.105 1561.734 2.130 36.053 2.354 0.56 289499. 0.1966
|
|
79.62 0.6006 0.7795 0.0276 0.0213 1.878 16.906 6.893 1400.116 1.910 30.661 2.233 0.57 290241. 0.1720
|
|
83.08 0.6267 0.7633 0.0227 0.0187 1.647 14.833 5.676 1228.462 1.676 25.246 2.096 0.57 291010. 0.1465
|
|
86.55 0.6528 0.7325 0.0178 0.0159 1.405 12.650 4.459 1047.616 1.429 19.835 1.931 0.57 291805. 0.1196
|
|
90.01 0.6789 0.6775 0.0130 0.0130 1.151 10.368 3.250 858.622 1.171 14.458 1.717 0.57 292626. 0.0908
|
|
93.47 0.7050 0.5768 0.0082 0.0101 0.889 8.002 2.057 662.748 0.904 9.148 1.408 0.57 293474. 0.0592
|
|
96.93 0.7311 0.3700 0.0035 0.0070 0.619 5.572 0.886 461.479 0.630 3.941 0.871 0.57 294346. 0.0240
|
|
100.39 0.7573
|
|
|
|
|
|
|
|
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 0.1035 0.0356 4.697 37.007 33.779 3502.704 4.181 150.251 4.374 0.63 319525. 0.7459
|
|
3.94 0.0260 0.0733 0.1022 0.0363 4.785 37.699 33.354 3568.185 4.259 148.357 4.240 0.63 319759. 0.7184
|
|
7.88 0.0520 0.1419 0.1008 0.0369 4.869 38.364 32.883 3631.137 4.334 146.263 4.107 0.63 320015. 0.6910
|
|
11.82 0.0780 0.2062 0.0992 0.0375 4.949 38.989 32.364 3690.312 4.405 143.956 3.978 0.63 320293. 0.6639
|
|
15.77 0.1040 0.2662 0.0974 0.0381 5.021 39.561 31.794 3744.426 4.470 141.419 3.851 0.64 320596. 0.6371
|
|
19.71 0.1301 0.3221 0.0955 0.0386 5.085 40.065 31.169 3792.106 4.526 138.639 3.728 0.64 320923. 0.6106
|
|
23.65 0.1561 0.3741 0.0934 0.0390 5.139 40.485 30.486 3831.916 4.574 135.600 3.608 0.64 321275. 0.5845
|
|
27.59 0.1821 0.4224 0.0911 0.0393 5.180 40.807 29.742 3862.369 4.610 132.290 3.493 0.64 321654. 0.5588
|
|
31.53 0.2081 0.4673 0.0887 0.0395 5.206 41.014 28.934 3881.949 4.634 128.698 3.381 0.64 322061. 0.5335
|
|
35.47 0.2341 0.5089 0.0860 0.0396 5.215 41.090 28.060 3889.133 4.642 124.811 3.273 0.64 322495. 0.5086
|
|
39.41 0.2601 0.5474 0.0831 0.0395 5.206 41.019 27.119 3882.440 4.634 120.624 3.168 0.64 322957. 0.4840
|
|
43.35 0.2861 0.5830 0.0800 0.0393 5.177 40.787 26.108 3860.422 4.608 116.127 3.067 0.64 323448. 0.4598
|
|
47.30 0.3121 0.6158 0.0767 0.0389 5.125 40.377 25.026 3821.679 4.562 111.318 2.970 0.64 323967. 0.4359
|
|
51.24 0.3382 0.6460 0.0732 0.0383 5.049 39.776 23.873 3764.779 4.494 106.188 2.876 0.64 324516. 0.4123
|
|
55.18 0.3642 0.6737 0.0694 0.0375 4.946 38.967 22.647 3688.185 4.402 100.732 2.785 0.64 325095. 0.3888
|
|
59.12 0.3902 0.6989 0.0654 0.0365 4.816 37.941 21.349 3591.087 4.287 94.962 2.697 0.64 325703. 0.3655
|
|
63.06 0.4162 0.7216 0.0613 0.0353 4.658 36.700 19.989 3473.652 4.146 88.912 2.610 0.64 326340. 0.3424
|
|
67.00 0.4422 0.7417 0.0569 0.0339 4.474 35.249 18.574 3336.310 3.982 82.617 2.525 0.64 327007. 0.3193
|
|
70.94 0.4682 0.7591 0.0524 0.0323 4.264 33.593 17.110 3179.522 3.795 76.107 2.441 0.64 327703. 0.2962
|
|
74.88 0.4942 0.7736 0.0478 0.0306 4.028 31.736 15.605 3003.751 3.585 69.412 2.356 0.64 328429. 0.2731
|
|
78.83 0.5202 0.7847 0.0431 0.0286 3.768 29.683 14.065 2809.502 3.354 62.560 2.271 0.64 329184. 0.2498
|
|
82.77 0.5463 0.7917 0.0383 0.0264 3.483 27.442 12.495 2597.340 3.100 55.579 2.182 0.64 329969. 0.2263
|
|
86.71 0.5723 0.7939 0.0334 0.0241 3.175 25.018 10.903 2367.944 2.827 48.498 2.088 0.65 330783. 0.2023
|
|
90.65 0.5983 0.7895 0.0285 0.0216 2.846 22.421 9.296 2122.137 2.533 41.347 1.987 0.65 331626. 0.1777
|
|
94.59 0.6243 0.7762 0.0235 0.0189 2.496 19.661 7.679 1860.943 2.221 34.158 1.872 0.65 332500. 0.1522
|
|
98.53 0.6503 0.7492 0.0186 0.0161 2.126 16.753 6.063 1585.630 1.893 26.969 1.734 0.65 333402. 0.1253
|
|
102.47 0.6763 0.6995 0.0137 0.0132 1.740 13.711 4.455 1297.762 1.549 19.818 1.557 0.65 334335. 0.0964
|
|
106.41 0.7023 0.6070 0.0088 0.0102 1.340 10.557 2.866 999.256 1.193 12.750 1.301 0.65 335297. 0.0646
|
|
110.36 0.7283 0.4142 0.0040 0.0070 0.928 7.315 1.307 692.372 0.826 5.814 0.856 0.65 336288. 0.0287
|
|
114.30 0.7544
|
|
|
|
|
|
|
|
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 0.1050 0.0364 6.831 47.841 43.367 5094.149 5.405 192.894 3.861 0.71 359421. 0.7460
|
|
4.41 0.0259 0.0724 0.1037 0.0371 6.956 48.714 42.847 5187.057 5.504 190.584 3.747 0.71 359683. 0.7195
|
|
8.81 0.0517 0.1404 0.1023 0.0377 7.076 49.556 42.270 5276.798 5.599 188.019 3.633 0.71 359969. 0.6930
|
|
13.22 0.0776 0.2041 0.1008 0.0383 7.190 50.353 41.632 5361.589 5.689 185.179 3.522 0.71 360281. 0.6667
|
|
17.63 0.1034 0.2637 0.0991 0.0389 7.295 51.085 40.927 5439.559 5.772 182.043 3.413 0.71 360620. 0.6405
|
|
22.03 0.1293 0.3193 0.0972 0.0394 7.387 51.734 40.151 5508.712 5.845 178.592 3.306 0.71 360986. 0.6146
|
|
26.44 0.1551 0.3711 0.0952 0.0398 7.465 52.281 39.300 5566.903 5.907 174.806 3.202 0.71 361381. 0.5889
|
|
30.85 0.1810 0.4194 0.0929 0.0401 7.526 52.704 38.370 5611.916 5.954 170.668 3.101 0.72 361805. 0.5636
|
|
35.25 0.2068 0.4642 0.0904 0.0403 7.565 52.981 37.357 5641.460 5.986 166.162 3.003 0.72 362260. 0.5386
|
|
39.66 0.2327 0.5058 0.0878 0.0404 7.581 53.092 36.258 5653.227 5.998 161.275 2.909 0.72 362746. 0.5139
|
|
44.07 0.2585 0.5444 0.0849 0.0403 7.570 53.014 35.071 5644.962 5.989 155.995 2.818 0.72 363263. 0.4896
|
|
48.47 0.2844 0.5801 0.0818 0.0401 7.529 52.728 33.793 5614.489 5.957 150.313 2.730 0.72 363812. 0.4656
|
|
52.88 0.3102 0.6132 0.0785 0.0397 7.456 52.214 32.424 5559.801 5.899 144.224 2.645 0.72 364394. 0.4419
|
|
57.29 0.3361 0.6437 0.0750 0.0391 7.347 51.454 30.962 5478.868 5.813 137.720 2.563 0.72 365007. 0.4184
|
|
61.69 0.3619 0.6718 0.0712 0.0384 7.201 50.427 29.404 5369.501 5.697 130.791 2.484 0.72 365654. 0.3952
|
|
66.10 0.3878 0.6974 0.0672 0.0374 7.014 49.120 27.754 5230.284 5.550 123.448 2.407 0.72 366333. 0.3720
|
|
70.51 0.4136 0.7207 0.0630 0.0362 6.787 47.533 26.019 5061.347 5.370 115.733 2.332 0.72 367045. 0.3489
|
|
74.91 0.4395 0.7416 0.0586 0.0347 6.522 45.673 24.211 4863.311 5.160 107.691 2.258 0.72 367790. 0.3260
|
|
79.32 0.4653 0.7598 0.0541 0.0331 6.218 43.547 22.339 4636.859 4.920 99.362 2.185 0.72 368567. 0.3030
|
|
83.73 0.4912 0.7753 0.0494 0.0313 5.877 41.160 20.410 4382.702 4.650 90.785 2.112 0.72 369376. 0.2800
|
|
88.13 0.5170 0.7876 0.0446 0.0293 5.500 38.519 18.434 4101.568 4.352 81.994 2.039 0.72 370218. 0.2568
|
|
92.54 0.5429 0.7962 0.0398 0.0271 5.088 35.634 16.418 3794.296 4.026 73.028 1.963 0.72 371093. 0.2333
|
|
96.95 0.5687 0.8002 0.0348 0.0247 4.643 32.512 14.371 3461.916 3.673 63.921 1.883 0.73 372000. 0.2094
|
|
101.35 0.5946 0.7982 0.0298 0.0222 4.165 29.167 12.301 3105.694 3.295 54.713 1.796 0.73 372940. 0.1848
|
|
105.76 0.6205 0.7878 0.0247 0.0195 3.657 25.612 10.217 2727.223 2.894 45.445 1.699 0.73 373913. 0.1593
|
|
110.17 0.6463 0.7649 0.0197 0.0166 3.123 21.868 8.130 2328.516 2.471 36.164 1.584 0.73 374918. 0.1325
|
|
114.57 0.6722 0.7210 0.0147 0.0137 2.564 17.957 6.052 1912.112 2.029 26.918 1.436 0.73 375956. 0.1036
|
|
118.98 0.6980 0.6380 0.0097 0.0106 1.986 13.910 3.994 1481.169 1.572 17.766 1.223 0.73 377027. 0.0717
|
|
123.39 0.7239 0.4653 0.0048 0.0074 1.394 9.762 1.971 1039.486 1.103 8.768 0.860 0.73 378129. 0.0354
|
|
127.79 0.7497 -0.0045 0.0000 0.0042 0.790 5.535 -0.011 589.348 0.625 -0.047 -0.008 0.73 379239. 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 0.1067 0.0388 9.994 62.990 54.417 7452.430 7.117 242.047 3.312 0.79 399294. 0.7168
|
|
4.89 0.0258 0.0692 0.1055 0.0394 10.138 63.901 53.808 7560.233 7.219 239.338 3.228 0.79 399585. 0.6947
|
|
9.77 0.0516 0.1347 0.1042 0.0399 10.276 64.770 53.127 7662.999 7.318 236.308 3.145 0.79 399903. 0.6724
|
|
14.66 0.0774 0.1967 0.1027 0.0404 10.404 65.577 52.367 7758.490 7.409 232.931 3.061 0.79 400250. 0.6500
|
|
19.54 0.1032 0.2553 0.1010 0.0409 10.520 66.303 51.524 7844.419 7.491 229.177 2.979 0.79 400627. 0.6274
|
|
24.43 0.1290 0.3104 0.0992 0.0412 10.619 66.927 50.589 7918.312 7.561 225.020 2.898 0.79 401034. 0.6047
|
|
29.32 0.1548 0.3621 0.0972 0.0415 10.698 67.428 49.558 7977.561 7.618 220.432 2.818 0.79 401474. 0.5819
|
|
34.20 0.1806 0.4107 0.0950 0.0418 10.754 67.782 48.424 8019.390 7.658 215.389 2.739 0.79 401947. 0.5591
|
|
39.09 0.2064 0.4561 0.0925 0.0419 10.783 67.965 47.183 8041.013 7.679 209.869 2.661 0.80 402453. 0.5363
|
|
43.98 0.2322 0.4985 0.0899 0.0419 10.781 67.952 45.830 8039.554 7.677 203.853 2.586 0.80 402994. 0.5135
|
|
48.86 0.2580 0.5380 0.0870 0.0417 10.744 67.720 44.363 8012.133 7.651 197.327 2.511 0.80 403570. 0.4908
|
|
53.75 0.2838 0.5747 0.0839 0.0414 10.669 67.245 42.779 7955.873 7.597 190.280 2.439 0.80 404181. 0.4680
|
|
58.63 0.3096 0.6087 0.0806 0.0410 10.551 66.501 41.075 7867.895 7.513 182.702 2.368 0.80 404829. 0.4452
|
|
63.52 0.3354 0.6401 0.0770 0.0403 10.387 65.465 39.251 7745.246 7.396 174.587 2.299 0.80 405512. 0.4225
|
|
68.41 0.3612 0.6690 0.0732 0.0395 10.171 64.107 37.303 7584.600 7.243 165.922 2.231 0.80 406231. 0.3997
|
|
73.29 0.3870 0.6955 0.0691 0.0385 9.901 62.406 35.233 7383.387 7.051 156.716 2.164 0.80 406986. 0.3769
|
|
78.18 0.4128 0.7195 0.0648 0.0372 9.577 60.362 33.053 7141.513 6.820 147.021 2.099 0.80 407778. 0.3541
|
|
83.07 0.4386 0.7410 0.0604 0.0357 9.199 57.980 30.776 6859.708 6.551 136.892 2.035 0.80 408606. 0.3312
|
|
87.95 0.4644 0.7600 0.0557 0.0341 8.769 55.267 28.414 6538.785 6.244 126.384 1.971 0.80 409469. 0.3082
|
|
92.84 0.4902 0.7760 0.0509 0.0322 8.287 52.231 25.977 6179.589 5.901 115.545 1.907 0.80 410368. 0.2851
|
|
97.72 0.5160 0.7888 0.0460 0.0301 7.756 48.883 23.476 5783.402 5.523 104.423 1.841 0.80 411303. 0.2617
|
|
102.61 0.5418 0.7976 0.0410 0.0279 7.177 45.237 20.922 5352.099 5.111 93.061 1.773 0.81 412274. 0.2379
|
|
107.50 0.5676 0.8014 0.0359 0.0255 6.555 41.312 18.324 4887.754 4.667 81.507 1.700 0.81 413281. 0.2136
|
|
112.38 0.5934 0.7983 0.0308 0.0229 5.891 37.132 15.695 4393.150 4.195 69.810 1.620 0.81 414323. 0.1883
|
|
117.27 0.6192 0.7856 0.0256 0.0202 5.192 32.724 13.044 3871.666 3.697 58.021 1.528 0.81 415401. 0.1619
|
|
122.16 0.6450 0.7582 0.0204 0.0173 4.462 28.124 10.386 3327.379 3.177 46.197 1.416 0.81 416515. 0.1339
|
|
127.04 0.6708 0.7065 0.0152 0.0144 3.708 23.373 7.734 2765.286 2.641 34.401 1.269 0.81 417665. 0.1035
|
|
131.93 0.6966 0.6111 0.0100 0.0114 2.939 18.521 5.104 2191.264 2.093 22.705 1.057 0.81 418851. 0.0700
|
|
136.81 0.7224 0.4245 0.0049 0.0084 2.162 13.625 2.515 1612.050 1.539 11.189 0.708 0.81 420072. 0.0329
|
|
141.70 0.7482 -0.0065 0.0000 0.0054 1.383 8.720 -0.024 1031.629 0.985 -0.106 -0.010 0.82 421305. 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 0.1084 0.0453 15.533 89.000 66.878 11582.682 10.055 297.473 2.619 0.87 439148. 0.6283
|
|
5.38 0.0258 0.0607 0.1073 0.0457 15.663 89.749 66.202 11680.207 10.140 294.468 2.571 0.87 439468. 0.6137
|
|
10.77 0.0517 0.1191 0.1061 0.0460 15.777 90.400 65.438 11764.943 10.213 291.068 2.523 0.87 439818. 0.5987
|
|
16.15 0.0775 0.1752 0.1047 0.0463 15.869 90.930 64.576 11833.849 10.273 287.235 2.475 0.87 440200. 0.5835
|
|
21.53 0.1034 0.2292 0.1031 0.0465 15.937 91.315 63.608 11884.007 10.317 282.929 2.428 0.87 440615. 0.5680
|
|
26.92 0.1292 0.2809 0.1013 0.0466 15.975 91.534 62.525 11912.542 10.341 278.112 2.381 0.87 441066. 0.5523
|
|
32.30 0.1550 0.3305 0.0994 0.0466 15.980 91.566 61.319 11916.658 10.345 272.746 2.334 0.87 441552. 0.5362
|
|
37.68 0.1809 0.3779 0.0972 0.0465 15.950 91.389 59.981 11893.657 10.325 266.797 2.287 0.87 442075. 0.5197
|
|
43.07 0.2067 0.4231 0.0948 0.0463 15.879 90.984 58.507 11840.876 10.279 260.237 2.241 0.87 442637. 0.5029
|
|
48.45 0.2326 0.4662 0.0922 0.0460 15.765 90.329 56.888 11755.683 10.205 253.038 2.195 0.88 443236. 0.4857
|
|
53.83 0.2584 0.5071 0.0893 0.0455 15.603 89.405 55.121 11635.437 10.101 245.179 2.149 0.88 443875. 0.4680
|
|
59.22 0.2842 0.5458 0.0862 0.0449 15.391 88.191 53.202 11477.416 9.964 236.643 2.102 0.88 444554. 0.4499
|
|
64.60 0.3101 0.5823 0.0829 0.0441 15.125 86.663 51.128 11278.605 9.791 227.416 2.056 0.88 445272. 0.4313
|
|
69.98 0.3359 0.6165 0.0793 0.0432 14.800 84.802 48.896 11036.354 9.581 217.489 2.010 0.88 446029. 0.4122
|
|
75.37 0.3618 0.6485 0.0754 0.0421 14.412 82.581 46.504 10747.310 9.330 206.849 1.963 0.88 446827. 0.3927
|
|
80.75 0.3876 0.6780 0.0712 0.0407 13.958 79.979 43.953 10408.682 9.036 195.505 1.915 0.88 447665. 0.3725
|
|
86.13 0.4134 0.7052 0.0669 0.0392 13.438 76.995 41.259 10020.411 8.699 183.520 1.868 0.88 448543. 0.3519
|
|
91.52 0.4393 0.7295 0.0623 0.0375 12.858 73.673 38.437 9588.057 8.324 170.967 1.818 0.88 449460. 0.3307
|
|
96.90 0.4651 0.7503 0.0575 0.0357 12.226 70.052 35.502 9116.808 7.914 157.911 1.766 0.88 450417. 0.3087
|
|
102.28 0.4910 0.7671 0.0526 0.0337 11.543 66.142 32.467 8607.958 7.473 144.415 1.711 0.88 451413. 0.2860
|
|
107.67 0.5168 0.7787 0.0476 0.0316 10.820 62.000 29.347 8068.806 7.005 130.537 1.650 0.88 452448. 0.2622
|
|
113.05 0.5426 0.7833 0.0424 0.0294 10.065 57.671 26.154 7505.535 6.516 116.332 1.581 0.89 453522. 0.2371
|
|
118.43 0.5685 0.7807 0.0371 0.0270 9.265 53.088 22.903 6909.008 5.998 101.872 1.504 0.89 454635. 0.2111
|
|
123.82 0.5943 0.7682 0.0318 0.0246 8.427 48.287 19.609 6284.195 5.455 87.220 1.415 0.89 455787. 0.1839
|
|
129.20 0.6202 0.7421 0.0264 0.0221 7.561 43.325 16.287 5638.427 4.895 72.447 1.310 0.89 456978. 0.1551
|
|
134.58 0.6460 0.6962 0.0210 0.0195 6.678 38.265 12.956 4979.907 4.323 57.628 1.180 0.89 458209. 0.1246
|
|
139.97 0.6718 0.6211 0.0156 0.0169 5.789 33.170 9.633 4316.786 3.747 42.849 1.012 0.89 459479. 0.0922
|
|
145.35 0.6977 0.5010 0.0103 0.0143 4.906 28.111 6.342 3658.394 3.176 28.210 0.786 0.89 460788. 0.0581
|
|
150.73 0.7235 0.3089 0.0050 0.0118 4.042 23.159 3.107 3014.034 2.617 13.818 0.467 0.90 462135. 0.0242
|
|
156.12 0.7494 -0.0080 -0.0001 0.0093 3.197 18.320 -0.062 2384.227 2.070 -0.275 -0.012 0.90 463505. 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 0.1075 0.0533 23.739 124.685 78.928 17702.100 14.087 351.074 2.022 0.95 479101. 0.5271
|
|
5.94 0.0261 0.0518 0.1066 0.0538 23.954 125.816 78.285 17862.559 14.215 348.211 1.988 0.95 479442. 0.5160
|
|
11.89 0.0523 0.1018 0.1056 0.0543 24.144 126.811 77.545 18003.951 14.327 344.919 1.954 0.95 479819. 0.5047
|
|
17.83 0.0784 0.1501 0.1045 0.0546 24.298 127.623 76.695 18119.197 14.419 341.141 1.920 0.95 480230. 0.4933
|
|
23.77 0.1046 0.1967 0.1031 0.0549 24.408 128.199 75.722 18200.875 14.484 336.812 1.887 0.95 480681. 0.4817
|
|
29.71 0.1307 0.2417 0.1016 0.0550 24.462 128.483 74.611 18241.320 14.516 331.869 1.855 0.95 481170. 0.4701
|
|
35.66 0.1569 0.2852 0.0999 0.0549 24.451 128.425 73.347 18233.076 14.509 326.247 1.825 0.95 481701. 0.4584
|
|
41.60 0.1830 0.3274 0.0979 0.0548 24.366 127.977 71.916 18169.361 14.459 319.884 1.795 0.95 482275. 0.4467
|
|
47.54 0.2092 0.3683 0.0958 0.0544 24.198 127.097 70.307 18044.539 14.359 312.724 1.767 0.95 482892. 0.4347
|
|
53.49 0.2353 0.4081 0.0933 0.0538 23.943 125.758 68.507 17854.357 14.208 304.720 1.740 0.95 483554. 0.4226
|
|
59.43 0.2615 0.4467 0.0906 0.0530 23.597 123.938 66.509 17595.945 14.002 295.832 1.714 0.96 484262. 0.4102
|
|
65.37 0.2876 0.4841 0.0876 0.0520 23.156 121.625 64.305 17267.635 13.741 286.031 1.689 0.96 485014. 0.3974
|
|
71.32 0.3138 0.5203 0.0843 0.0508 22.621 118.814 61.892 16868.498 13.424 275.295 1.664 0.96 485813. 0.3841
|
|
77.26 0.3399 0.5552 0.0807 0.0494 21.990 115.500 59.265 16397.998 13.049 263.609 1.639 0.96 486657. 0.3702
|
|
83.20 0.3661 0.5887 0.0768 0.0478 21.262 111.677 56.419 15855.294 12.617 250.954 1.614 0.96 487547. 0.3557
|
|
89.14 0.3922 0.6206 0.0727 0.0459 20.438 107.346 53.359 15240.354 12.128 237.341 1.588 0.96 488482. 0.3403
|
|
95.09 0.4184 0.6507 0.0682 0.0439 19.523 102.542 50.105 14558.354 11.585 222.865 1.561 0.96 489463. 0.3242
|
|
101.03 0.4445 0.6788 0.0636 0.0416 18.526 97.306 46.680 13815.003 10.994 207.631 1.533 0.96 490488. 0.3072
|
|
106.97 0.4707 0.7033 0.0587 0.0393 17.481 91.819 43.103 13035.873 10.374 191.720 1.500 0.96 491557. 0.2889
|
|
112.92 0.4968 0.7229 0.0537 0.0369 16.407 86.175 39.392 12234.619 9.736 175.217 1.460 0.96 492669. 0.2689
|
|
118.86 0.5230 0.7361 0.0484 0.0344 15.314 80.434 35.568 11419.596 9.087 158.208 1.413 0.97 493826. 0.2472
|
|
124.80 0.5491 0.7343 0.0431 0.0322 14.338 75.308 31.635 10691.812 8.508 140.712 1.342 0.97 495025. 0.2214
|
|
130.75 0.5753 0.7164 0.0376 0.0302 13.440 70.594 27.619 10022.564 7.976 122.848 1.250 0.97 496268. 0.1927
|
|
136.69 0.6014 0.6850 0.0321 0.0282 12.535 65.837 23.558 9347.155 7.438 104.786 1.143 0.97 497554. 0.1628
|
|
142.63 0.6276 0.6371 0.0265 0.0261 11.630 61.087 19.481 8672.826 6.902 86.652 1.019 0.97 498884. 0.1319
|
|
148.57 0.6537 0.5687 0.0210 0.0241 10.741 56.418 15.420 8009.836 6.374 68.588 0.873 0.97 500256. 0.1006
|
|
154.52 0.6799 0.4759 0.0155 0.0222 9.880 51.896 11.411 7367.851 5.863 50.757 0.702 0.97 501673. 0.0696
|
|
160.46 0.7060 0.3540 0.0102 0.0204 9.057 47.573 7.494 6754.073 5.375 33.334 0.503 0.98 503135. 0.0404
|
|
166.40 0.7322 0.1985 0.0050 0.0186 8.277 43.474 3.702 6172.160 4.912 16.466 0.272 0.98 504647. 0.0154
|
|
172.35 0.7583 -0.0001 0.0000 0.0169 7.500 39.394 -0.002 5592.947 4.451 -0.008 0.000 0.98 506259. 0.0000
|
|
|
|
|
|
|