427 lines
76 KiB
Plaintext
427 lines
76 KiB
Plaintext
22x12E (22x12E.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 0.0869 0.0320 0.013 0.836 0.649 9.894 0.094 2.885 29.737 0.09 44301. 0.6388
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0.50 0.0239 0.0631 0.0856 0.0324 0.013 0.847 0.639 10.017 0.096 2.841 28.923 0.09 44329. 0.6165
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0.99 0.0477 0.1226 0.0841 0.0328 0.014 0.856 0.628 10.132 0.097 2.793 28.114 0.09 44360. 0.5942
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1.49 0.0716 0.1786 0.0826 0.0331 0.014 0.865 0.616 10.237 0.098 2.742 27.312 0.09 44393. 0.5719
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1.99 0.0955 0.2312 0.0809 0.0334 0.014 0.873 0.604 10.329 0.099 2.686 26.519 0.09 44428. 0.5497
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2.49 0.1193 0.2805 0.0791 0.0337 0.014 0.880 0.590 10.407 0.099 2.626 25.737 0.09 44466. 0.5275
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2.98 0.1432 0.3265 0.0772 0.0338 0.014 0.885 0.576 10.466 0.100 2.562 24.965 0.09 44508. 0.5054
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3.48 0.1671 0.3694 0.0751 0.0340 0.014 0.888 0.561 10.504 0.100 2.493 24.206 0.09 44552. 0.4834
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3.98 0.1909 0.4091 0.0729 0.0340 0.014 0.889 0.544 10.519 0.100 2.420 23.459 0.09 44599. 0.4615
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4.48 0.2148 0.4458 0.0705 0.0340 0.014 0.888 0.526 10.507 0.100 2.341 22.724 0.09 44649. 0.4397
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4.97 0.2387 0.4796 0.0680 0.0338 0.014 0.885 0.508 10.466 0.100 2.258 22.000 0.09 44703. 0.4181
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5.47 0.2625 0.5104 0.0653 0.0336 0.014 0.878 0.488 10.393 0.099 2.169 21.286 0.09 44760. 0.3965
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5.97 0.2864 0.5384 0.0625 0.0333 0.014 0.869 0.467 10.284 0.098 2.076 20.580 0.09 44820. 0.3750
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6.46 0.3103 0.5634 0.0595 0.0328 0.014 0.857 0.444 10.138 0.097 1.977 19.880 0.09 44883. 0.3534
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6.96 0.3342 0.5854 0.0564 0.0322 0.013 0.841 0.421 9.953 0.095 1.872 19.182 0.09 44950. 0.3319
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7.46 0.3580 0.6043 0.0531 0.0315 0.013 0.822 0.396 9.727 0.093 1.763 18.482 0.09 45021. 0.3103
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7.96 0.3819 0.6200 0.0497 0.0306 0.013 0.800 0.371 9.463 0.090 1.650 17.776 0.09 45095. 0.2887
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8.45 0.4058 0.6322 0.0462 0.0296 0.012 0.774 0.345 9.161 0.087 1.532 17.058 0.09 45172. 0.2671
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8.95 0.4296 0.6404 0.0425 0.0285 0.012 0.746 0.317 8.821 0.084 1.412 16.321 0.09 45253. 0.2453
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9.45 0.4535 0.6443 0.0388 0.0273 0.011 0.714 0.290 8.445 0.081 1.288 15.556 0.09 45337. 0.2233
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9.94 0.4774 0.6432 0.0350 0.0260 0.011 0.679 0.261 8.033 0.077 1.162 14.753 0.09 45425. 0.2011
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10.44 0.5012 0.6362 0.0311 0.0245 0.010 0.641 0.232 7.586 0.072 1.034 13.898 0.09 45516. 0.1787
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10.94 0.5251 0.6221 0.0272 0.0230 0.010 0.601 0.203 7.106 0.068 0.904 12.972 0.09 45611. 0.1560
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11.44 0.5490 0.5993 0.0233 0.0213 0.009 0.557 0.174 6.594 0.063 0.773 11.953 0.09 45709. 0.1329
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11.93 0.5728 0.5653 0.0193 0.0196 0.008 0.512 0.144 6.052 0.058 0.641 10.805 0.09 45811. 0.1094
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12.43 0.5967 0.5165 0.0153 0.0177 0.007 0.463 0.115 5.482 0.052 0.510 9.478 0.09 45917. 0.0856
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12.93 0.6206 0.4475 0.0114 0.0158 0.007 0.413 0.085 4.887 0.047 0.378 7.895 0.09 46026. 0.0614
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13.43 0.6444 0.3494 0.0075 0.0138 0.006 0.361 0.056 4.271 0.041 0.249 5.936 0.09 46139. 0.0374
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13.92 0.6683 0.2069 0.0036 0.0118 0.005 0.307 0.027 3.636 0.035 0.121 3.390 0.09 46255. 0.0149
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14.42 0.6922 -0.0090 -0.0001 0.0097 0.004 0.252 -0.001 2.987 0.029 -0.004 -0.142 0.09 46374. 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 0.0873 0.0299 0.099 3.121 2.606 73.855 0.353 11.590 16.003 0.17 88601. 0.6890
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1.01 0.0241 0.0685 0.0859 0.0303 0.100 3.166 2.566 74.925 0.358 11.413 15.532 0.17 88658. 0.6636
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2.01 0.0483 0.1329 0.0845 0.0307 0.102 3.209 2.522 75.934 0.363 11.220 15.067 0.17 88720. 0.6382
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3.02 0.0724 0.1933 0.0829 0.0311 0.103 3.248 2.476 76.861 0.367 11.011 14.609 0.17 88786. 0.6130
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4.02 0.0966 0.2498 0.0812 0.0314 0.104 3.283 2.425 77.685 0.371 10.786 14.158 0.17 88858. 0.5880
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5.03 0.1207 0.3025 0.0794 0.0317 0.105 3.313 2.370 78.384 0.374 10.544 13.717 0.17 88936. 0.5633
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6.04 0.1449 0.3516 0.0774 0.0319 0.106 3.336 2.312 78.932 0.377 10.283 13.284 0.17 89020. 0.5387
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7.04 0.1690 0.3971 0.0753 0.0321 0.106 3.352 2.249 79.307 0.379 10.003 12.862 0.17 89110. 0.5144
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8.05 0.1932 0.4393 0.0731 0.0321 0.107 3.359 2.182 79.483 0.380 9.704 12.449 0.17 89206. 0.4904
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9.06 0.2173 0.4782 0.0706 0.0321 0.107 3.357 2.110 79.436 0.379 9.384 12.046 0.17 89309. 0.4667
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10.06 0.2415 0.5140 0.0681 0.0320 0.106 3.345 2.033 79.140 0.378 9.044 11.653 0.18 89418. 0.4432
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11.07 0.2656 0.5467 0.0654 0.0318 0.105 3.321 1.952 78.573 0.375 8.682 11.268 0.18 89534. 0.4199
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12.07 0.2898 0.5764 0.0625 0.0314 0.104 3.284 1.866 77.708 0.371 8.299 10.891 0.18 89657. 0.3968
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13.08 0.3139 0.6032 0.0594 0.0309 0.103 3.234 1.775 76.520 0.365 7.894 10.520 0.18 89786. 0.3738
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14.09 0.3381 0.6271 0.0562 0.0303 0.101 3.169 1.679 74.994 0.358 7.468 10.155 0.18 89923. 0.3509
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15.09 0.3622 0.6479 0.0529 0.0296 0.098 3.091 1.579 73.130 0.349 7.023 9.793 0.18 90066. 0.3282
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16.10 0.3864 0.6656 0.0494 0.0287 0.095 2.998 1.475 70.932 0.339 6.560 9.431 0.18 90217. 0.3055
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17.10 0.4105 0.6799 0.0458 0.0276 0.092 2.891 1.367 68.405 0.327 6.082 9.067 0.18 90375. 0.2828
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18.11 0.4346 0.6905 0.0421 0.0265 0.088 2.770 1.257 65.554 0.313 5.591 8.697 0.18 90540. 0.2601
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19.12 0.4588 0.6970 0.0383 0.0252 0.084 2.636 1.144 62.384 0.298 5.088 8.316 0.18 90712. 0.2372
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20.12 0.4829 0.6987 0.0344 0.0238 0.079 2.489 1.029 58.903 0.281 4.575 7.920 0.18 90891. 0.2142
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21.13 0.5071 0.6947 0.0305 0.0223 0.074 2.329 0.911 55.120 0.263 4.054 7.500 0.18 91078. 0.1910
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22.13 0.5312 0.6837 0.0266 0.0206 0.068 2.157 0.793 51.044 0.244 3.527 7.045 0.18 91272. 0.1673
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23.14 0.5554 0.6638 0.0226 0.0189 0.063 1.973 0.673 46.690 0.223 2.996 6.543 0.18 91473. 0.1432
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24.15 0.5795 0.6319 0.0185 0.0170 0.056 1.778 0.554 42.073 0.201 2.463 5.970 0.18 91681. 0.1185
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25.15 0.6037 0.5835 0.0145 0.0150 0.050 1.573 0.434 37.216 0.178 1.931 5.291 0.18 91897. 0.0930
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26.16 0.6278 0.5104 0.0106 0.0130 0.043 1.358 0.315 32.144 0.153 1.403 4.451 0.18 92120. 0.0667
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27.17 0.6520 0.3981 0.0066 0.0109 0.036 1.136 0.198 26.889 0.128 0.881 3.343 0.18 92350. 0.0397
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28.17 0.6761 0.2168 0.0028 0.0087 0.029 0.908 0.083 21.485 0.103 0.370 1.755 0.18 92587. 0.0135
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29.18 0.7003
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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 0.0877 0.0290 0.325 6.832 5.894 242.497 0.772 26.216 11.024 0.26 132898. 0.7138
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1.50 0.0240 0.0702 0.0864 0.0295 0.330 6.937 5.805 246.211 0.784 25.821 10.694 0.26 132982. 0.6872
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3.00 0.0479 0.1362 0.0850 0.0299 0.335 7.036 5.708 249.726 0.795 25.391 10.368 0.26 133074. 0.6607
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4.49 0.0719 0.1980 0.0834 0.0303 0.339 7.127 5.604 252.969 0.805 24.927 10.048 0.26 133174. 0.6344
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5.99 0.0959 0.2557 0.0817 0.0306 0.343 7.209 5.491 255.870 0.814 24.425 9.734 0.26 133281. 0.6084
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7.49 0.1198 0.3096 0.0799 0.0309 0.346 7.279 5.370 258.353 0.822 23.885 9.427 0.26 133397. 0.5826
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8.99 0.1438 0.3597 0.0780 0.0312 0.349 7.335 5.239 260.336 0.829 23.303 9.128 0.26 133521. 0.5572
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10.49 0.1678 0.4062 0.0759 0.0313 0.351 7.374 5.099 261.737 0.833 22.679 8.836 0.26 133655. 0.5321
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11.98 0.1918 0.4493 0.0737 0.0314 0.352 7.395 4.949 262.474 0.835 22.011 8.552 0.26 133798. 0.5074
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13.48 0.2157 0.4891 0.0713 0.0314 0.352 7.395 4.788 262.460 0.835 21.299 8.275 0.26 133950. 0.4829
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14.98 0.2397 0.5258 0.0687 0.0313 0.351 7.371 4.618 261.615 0.833 20.539 8.006 0.26 134112. 0.4588
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16.48 0.2637 0.5594 0.0660 0.0311 0.348 7.321 4.436 259.855 0.827 19.733 7.744 0.26 134284. 0.4350
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17.98 0.2876 0.5901 0.0632 0.0308 0.345 7.243 4.244 257.095 0.818 18.879 7.488 0.26 134466. 0.4115
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19.48 0.3116 0.6180 0.0601 0.0303 0.340 7.135 4.041 253.246 0.806 17.976 7.238 0.26 134659. 0.3881
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20.97 0.3356 0.6430 0.0570 0.0297 0.333 6.994 3.827 248.252 0.790 17.024 6.993 0.26 134861. 0.3649
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22.47 0.3595 0.6651 0.0536 0.0290 0.325 6.821 3.604 242.104 0.771 16.029 6.751 0.26 135074. 0.3418
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23.97 0.3835 0.6843 0.0502 0.0281 0.315 6.616 3.371 234.811 0.747 14.995 6.512 0.26 135298. 0.3189
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25.47 0.4075 0.7004 0.0466 0.0271 0.304 6.378 3.131 226.388 0.721 13.926 6.273 0.26 135531. 0.2960
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26.97 0.4315 0.7131 0.0429 0.0260 0.291 6.110 2.884 216.850 0.690 12.827 6.032 0.26 135776. 0.2732
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28.46 0.4554 0.7220 0.0392 0.0247 0.277 5.810 2.631 206.214 0.656 11.701 5.786 0.26 136031. 0.2503
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29.96 0.4794 0.7267 0.0353 0.0233 0.261 5.480 2.372 194.502 0.619 10.552 5.532 0.26 136296. 0.2273
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31.46 0.5034 0.7263 0.0314 0.0218 0.244 5.120 2.110 181.741 0.579 9.385 5.266 0.27 136573. 0.2040
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32.96 0.5273 0.7197 0.0275 0.0201 0.225 4.732 1.845 167.966 0.535 8.204 4.981 0.27 136860. 0.1804
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34.46 0.5513 0.7051 0.0235 0.0183 0.205 4.317 1.577 153.220 0.488 7.014 4.668 0.27 137157. 0.1563
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35.95 0.5753 0.6799 0.0195 0.0165 0.184 3.876 1.308 137.557 0.438 5.819 4.314 0.27 137466. 0.1316
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37.45 0.5992 0.6397 0.0155 0.0145 0.162 3.410 1.040 121.048 0.385 4.625 3.896 0.27 137785. 0.1060
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38.95 0.6232 0.5769 0.0115 0.0124 0.139 2.924 0.773 103.777 0.330 3.438 3.378 0.27 138115. 0.0792
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40.45 0.6472 0.4772 0.0076 0.0103 0.115 2.419 0.509 85.848 0.273 2.265 2.691 0.27 138456. 0.0512
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41.95 0.6711 0.3099 0.0037 0.0081 0.090 1.898 0.250 67.383 0.214 1.113 1.685 0.27 138807. 0.0225
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43.44 0.6951 -0.0057 0.0000 0.0058 0.065 1.365 -0.003 48.445 0.154 -0.014 -0.030 0.27 139162. 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 0.0883 0.0287 0.762 12.011 10.551 568.399 1.357 46.932 8.420 0.35 177190. 0.7294
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2.00 0.0240 0.0715 0.0870 0.0292 0.774 12.202 10.393 577.442 1.379 46.230 8.164 0.35 177302. 0.7020
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4.00 0.0480 0.1386 0.0856 0.0296 0.786 12.383 10.222 586.010 1.399 45.468 7.912 0.35 177425. 0.6747
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6.00 0.0719 0.2014 0.0840 0.0300 0.796 12.550 10.037 593.929 1.418 44.643 7.665 0.35 177558. 0.6476
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7.99 0.0959 0.2601 0.0823 0.0304 0.806 12.700 9.836 601.026 1.435 43.750 7.423 0.35 177702. 0.6209
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9.99 0.1199 0.3148 0.0805 0.0307 0.814 12.829 9.619 607.117 1.449 42.788 7.187 0.35 177857. 0.5945
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11.99 0.1439 0.3657 0.0786 0.0309 0.821 12.932 9.387 612.006 1.461 41.751 6.957 0.35 178023. 0.5684
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13.99 0.1679 0.4129 0.0765 0.0311 0.825 13.006 9.136 615.495 1.469 40.639 6.733 0.35 178202. 0.5428
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15.99 0.1918 0.4566 0.0742 0.0312 0.828 13.046 8.868 617.379 1.474 39.447 6.515 0.35 178393. 0.5175
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17.99 0.2158 0.4971 0.0718 0.0312 0.828 13.047 8.582 617.455 1.474 38.173 6.304 0.35 178596. 0.4926
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19.98 0.2398 0.5344 0.0693 0.0311 0.825 13.006 8.277 615.522 1.469 36.816 6.099 0.35 178813. 0.4680
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21.98 0.2638 0.5686 0.0666 0.0309 0.820 12.919 7.953 611.380 1.460 35.374 5.900 0.35 179043. 0.4438
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23.98 0.2878 0.5999 0.0637 0.0306 0.811 12.780 7.609 604.824 1.444 33.846 5.706 0.35 179286. 0.4198
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25.98 0.3118 0.6284 0.0607 0.0301 0.799 12.586 7.246 595.635 1.422 32.229 5.517 0.35 179543. 0.3961
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27.98 0.3357 0.6541 0.0575 0.0295 0.783 12.333 6.863 583.672 1.393 30.525 5.333 0.35 179814. 0.3726
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29.98 0.3597 0.6770 0.0541 0.0287 0.763 12.021 6.462 568.911 1.358 28.742 5.152 0.35 180099. 0.3493
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31.97 0.3837 0.6971 0.0506 0.0279 0.739 11.651 6.045 551.370 1.316 26.889 4.973 0.35 180397. 0.3261
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33.97 0.4077 0.7141 0.0470 0.0268 0.712 11.222 5.614 531.080 1.268 24.973 4.795 0.35 180709. 0.3030
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35.97 0.4317 0.7280 0.0433 0.0257 0.681 10.736 5.171 508.075 1.213 23.001 4.616 0.35 181036. 0.2800
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37.97 0.4556 0.7383 0.0395 0.0244 0.647 10.193 4.717 482.398 1.152 20.982 4.435 0.35 181376. 0.2569
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39.97 0.4796 0.7445 0.0356 0.0229 0.609 9.595 4.254 454.100 1.084 18.922 4.249 0.35 181731. 0.2337
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41.97 0.5036 0.7459 0.0317 0.0214 0.568 8.943 3.783 423.244 1.010 16.828 4.054 0.35 182100. 0.2103
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43.97 0.5276 0.7415 0.0277 0.0197 0.523 8.239 3.307 389.914 0.931 14.710 3.847 0.35 182483. 0.1866
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45.96 0.5516 0.7294 0.0237 0.0179 0.475 7.485 2.827 354.214 0.846 12.574 3.620 0.35 182880. 0.1623
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47.96 0.5755 0.7071 0.0196 0.0160 0.424 6.683 2.345 316.280 0.755 10.430 3.363 0.35 183292. 0.1373
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49.96 0.5995 0.6701 0.0156 0.0140 0.370 5.838 1.864 276.280 0.660 8.289 3.059 0.36 183718. 0.1114
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51.96 0.6235 0.6104 0.0116 0.0118 0.314 4.954 1.385 234.423 0.560 6.161 2.680 0.36 184159. 0.0841
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53.96 0.6475 0.5125 0.0076 0.0096 0.256 4.035 0.912 190.966 0.456 4.057 2.167 0.36 184614. 0.0552
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55.96 0.6715 0.3409 0.0038 0.0074 0.196 3.089 0.448 146.208 0.349 1.993 1.390 0.36 185082. 0.0248
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57.95 0.6954 -0.0078 -0.0001 0.0051 0.134 2.119 -0.007 100.269 0.239 -0.030 -0.031 0.36 185554. 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 0.0891 0.0287 1.487 18.739 16.634 1108.533 2.117 73.989 6.806 0.44 221474. 0.7404
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2.50 0.0240 0.0722 0.0878 0.0291 1.511 19.045 16.389 1126.628 2.152 72.898 6.598 0.44 221615. 0.7124
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4.99 0.0479 0.1400 0.0864 0.0296 1.534 19.335 16.122 1143.782 2.184 71.710 6.393 0.44 221769. 0.6846
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7.49 0.0719 0.2034 0.0848 0.0300 1.555 19.603 15.832 1159.650 2.215 70.423 6.192 0.44 221935. 0.6572
|
|
9.99 0.0959 0.2626 0.0832 0.0304 1.574 19.844 15.519 1173.888 2.242 69.029 5.996 0.44 222115. 0.6300
|
|
12.48 0.1199 0.3177 0.0813 0.0307 1.591 20.051 15.181 1186.125 2.265 67.524 5.805 0.44 222310. 0.6032
|
|
14.98 0.1438 0.3690 0.0794 0.0309 1.604 20.217 14.816 1195.978 2.284 65.902 5.619 0.44 222518. 0.5768
|
|
17.48 0.1678 0.4167 0.0773 0.0311 1.613 20.337 14.424 1203.042 2.298 64.158 5.438 0.44 222742. 0.5509
|
|
19.98 0.1918 0.4609 0.0750 0.0312 1.618 20.402 14.004 1206.915 2.305 62.288 5.263 0.44 222981. 0.5253
|
|
22.47 0.2157 0.5017 0.0726 0.0312 1.619 20.407 13.554 1207.188 2.306 60.289 5.093 0.44 223236. 0.5001
|
|
24.97 0.2397 0.5394 0.0701 0.0311 1.614 20.344 13.075 1203.463 2.298 58.157 4.928 0.44 223508. 0.4752
|
|
27.47 0.2637 0.5741 0.0673 0.0309 1.603 20.207 12.565 1195.345 2.283 55.890 4.768 0.44 223796. 0.4508
|
|
29.96 0.2876 0.6059 0.0644 0.0306 1.586 19.988 12.025 1182.424 2.258 53.485 4.613 0.44 224100. 0.4266
|
|
32.46 0.3116 0.6349 0.0614 0.0301 1.561 19.681 11.452 1164.265 2.224 50.939 4.461 0.44 224422. 0.4027
|
|
34.96 0.3356 0.6611 0.0581 0.0295 1.530 19.281 10.849 1140.575 2.178 48.254 4.314 0.44 224761. 0.3790
|
|
37.45 0.3596 0.6847 0.0547 0.0287 1.490 18.786 10.217 1111.296 2.122 45.444 4.170 0.44 225117. 0.3555
|
|
39.95 0.3835 0.7055 0.0512 0.0278 1.444 18.197 9.560 1076.459 2.056 42.521 4.028 0.44 225490. 0.3322
|
|
42.45 0.4075 0.7234 0.0476 0.0268 1.389 17.515 8.880 1036.125 1.979 39.497 3.887 0.44 225881. 0.3089
|
|
44.95 0.4315 0.7382 0.0438 0.0256 1.328 16.742 8.180 990.362 1.891 36.385 3.746 0.44 226289. 0.2858
|
|
47.44 0.4554 0.7496 0.0400 0.0243 1.260 15.878 7.463 939.249 1.794 33.196 3.604 0.44 226715. 0.2626
|
|
49.94 0.4794 0.7571 0.0361 0.0228 1.184 14.925 6.731 882.890 1.686 29.942 3.458 0.44 227158. 0.2393
|
|
52.44 0.5034 0.7601 0.0321 0.0212 1.102 13.886 5.988 821.410 1.569 26.634 3.306 0.44 227619. 0.2158
|
|
54.93 0.5274 0.7574 0.0281 0.0195 1.012 12.762 5.235 754.973 1.442 23.286 3.145 0.44 228098. 0.1919
|
|
57.43 0.5513 0.7475 0.0240 0.0177 0.917 11.559 4.476 683.791 1.306 19.910 2.969 0.44 228595. 0.1675
|
|
59.93 0.5753 0.7278 0.0199 0.0157 0.816 10.280 3.714 608.130 1.161 16.521 2.770 0.44 229109. 0.1424
|
|
62.42 0.5993 0.6938 0.0158 0.0137 0.709 8.931 2.953 528.330 1.009 13.135 2.535 0.44 229642. 0.1162
|
|
64.92 0.6232 0.6374 0.0118 0.0115 0.597 7.519 2.196 444.812 0.850 9.769 2.239 0.44 230192. 0.0885
|
|
67.42 0.6472 0.5423 0.0078 0.0093 0.480 6.053 1.449 358.090 0.684 6.443 1.835 0.45 230760. 0.0589
|
|
69.91 0.6712 0.3695 0.0038 0.0070 0.360 4.543 0.714 268.768 0.513 3.177 1.206 0.45 231346. 0.0272
|
|
72.41 0.6952 -0.0040 0.0000 0.0046 0.237 2.993 -0.005 177.064 0.338 -0.022 -0.013 0.45 231934. 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 0.0901 0.0288 2.584 27.146 24.223 1927.013 3.067 107.743 5.701 0.52 265748. 0.7484
|
|
3.00 0.0240 0.0726 0.0888 0.0293 2.627 27.598 23.872 1959.107 3.118 106.181 5.527 0.52 265918. 0.7202
|
|
5.99 0.0479 0.1406 0.0874 0.0298 2.668 28.027 23.489 1989.542 3.166 104.479 5.355 0.52 266103. 0.6922
|
|
8.99 0.0719 0.2043 0.0859 0.0302 2.706 28.424 23.073 2017.706 3.211 102.630 5.187 0.52 266304. 0.6645
|
|
11.98 0.0959 0.2638 0.0842 0.0306 2.740 28.780 22.622 2042.990 3.252 100.625 5.022 0.52 266521. 0.6371
|
|
14.98 0.1198 0.3193 0.0824 0.0309 2.769 29.086 22.135 2064.735 3.286 98.456 4.862 0.52 266755. 0.6101
|
|
17.97 0.1438 0.3709 0.0804 0.0312 2.792 29.333 21.608 2082.255 3.314 96.114 4.707 0.52 267006. 0.5836
|
|
20.97 0.1678 0.4188 0.0783 0.0314 2.809 29.510 21.042 2094.846 3.334 93.594 4.556 0.52 267275. 0.5574
|
|
23.96 0.1917 0.4633 0.0760 0.0315 2.819 29.608 20.433 2101.781 3.345 90.887 4.410 0.52 267563. 0.5316
|
|
26.96 0.2157 0.5044 0.0736 0.0315 2.819 29.616 19.782 2102.351 3.346 87.990 4.268 0.52 267870. 0.5063
|
|
29.96 0.2396 0.5425 0.0710 0.0314 2.811 29.524 19.087 2095.844 3.336 84.897 4.131 0.53 268197. 0.4813
|
|
32.95 0.2636 0.5775 0.0683 0.0312 2.791 29.323 18.346 2081.565 3.313 81.604 3.998 0.53 268543. 0.4567
|
|
35.95 0.2876 0.6097 0.0653 0.0308 2.761 29.002 17.560 2058.799 3.277 78.109 3.869 0.53 268910. 0.4324
|
|
38.94 0.3115 0.6391 0.0622 0.0303 2.718 28.551 16.728 2026.783 3.226 74.405 3.743 0.53 269296. 0.4084
|
|
41.94 0.3355 0.6658 0.0590 0.0297 2.662 27.962 15.849 1984.972 3.159 70.497 3.622 0.53 269704. 0.3845
|
|
44.93 0.3595 0.6899 0.0555 0.0289 2.593 27.234 14.928 1933.247 3.077 66.401 3.502 0.53 270132. 0.3609
|
|
47.93 0.3834 0.7113 0.0520 0.0280 2.510 26.366 13.970 1871.667 2.979 62.138 3.385 0.53 270581. 0.3375
|
|
50.93 0.4074 0.7300 0.0483 0.0270 2.414 25.361 12.978 1800.333 2.865 57.726 3.270 0.53 271050. 0.3142
|
|
53.92 0.4314 0.7456 0.0445 0.0257 2.306 24.221 11.957 1719.370 2.736 53.183 3.154 0.53 271541. 0.2909
|
|
56.92 0.4553 0.7580 0.0406 0.0244 2.184 22.947 10.909 1628.920 2.593 48.525 3.038 0.53 272052. 0.2676
|
|
59.91 0.4793 0.7666 0.0366 0.0229 2.051 21.541 9.840 1529.161 2.434 43.769 2.919 0.53 272585. 0.2442
|
|
62.91 0.5033 0.7709 0.0326 0.0213 1.905 20.008 8.753 1420.320 2.261 38.934 2.795 0.53 273138. 0.2206
|
|
65.90 0.5272 0.7698 0.0285 0.0195 1.747 18.351 7.652 1302.689 2.073 34.038 2.664 0.53 273713. 0.1966
|
|
68.90 0.5512 0.7617 0.0243 0.0176 1.578 16.575 6.542 1176.638 1.873 29.100 2.522 0.53 274309. 0.1720
|
|
71.89 0.5752 0.7441 0.0202 0.0156 1.398 14.688 5.427 1042.646 1.659 24.141 2.361 0.53 274927. 0.1467
|
|
74.89 0.5991 0.7126 0.0160 0.0135 1.209 12.697 4.313 901.315 1.434 19.186 2.171 0.53 275566. 0.1202
|
|
77.89 0.6231 0.6590 0.0119 0.0113 1.010 10.613 3.206 753.395 1.199 14.259 1.930 0.53 276226. 0.0922
|
|
80.88 0.6470 0.5660 0.0079 0.0090 0.804 8.450 2.111 599.808 0.955 9.390 1.596 0.53 276908. 0.0619
|
|
83.88 0.6710 0.3914 0.0039 0.0066 0.592 6.221 1.036 441.637 0.703 4.610 1.064 0.54 277610. 0.0289
|
|
86.87 0.6950 -0.0107 -0.0001 0.0042 0.374 3.932 -0.017 279.137 0.444 -0.077 -0.028 0.54 278313. 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 0.0914 0.0292 4.156 37.419 33.427 3098.959 4.228 148.681 4.892 0.61 310009. 0.7544
|
|
3.51 0.0240 0.0729 0.0901 0.0297 4.227 38.056 32.952 3151.703 4.300 146.569 4.742 0.61 310209. 0.7260
|
|
7.01 0.0481 0.1413 0.0887 0.0302 4.294 38.660 32.433 3201.719 4.368 144.260 4.595 0.61 310427. 0.6979
|
|
10.52 0.0721 0.2053 0.0871 0.0306 4.356 39.218 31.867 3247.995 4.431 141.744 4.450 0.61 310663. 0.6700
|
|
14.03 0.0962 0.2650 0.0854 0.0310 4.411 39.720 31.252 3289.500 4.487 139.008 4.309 0.61 310918. 0.6425
|
|
17.54 0.1202 0.3207 0.0836 0.0313 4.459 40.150 30.585 3325.155 4.536 136.041 4.172 0.61 311194. 0.6154
|
|
21.04 0.1443 0.3726 0.0816 0.0316 4.498 40.496 29.863 3353.814 4.575 132.831 4.039 0.61 311490. 0.5886
|
|
24.55 0.1683 0.4208 0.0795 0.0318 4.525 40.744 29.084 3374.313 4.603 129.367 3.909 0.61 311807. 0.5623
|
|
28.06 0.1924 0.4655 0.0772 0.0319 4.540 40.878 28.246 3385.458 4.618 125.640 3.784 0.61 312146. 0.5364
|
|
31.56 0.2164 0.5069 0.0748 0.0319 4.541 40.886 27.348 3386.067 4.619 121.642 3.663 0.61 312508. 0.5109
|
|
35.07 0.2405 0.5452 0.0721 0.0318 4.526 40.752 26.387 3374.971 4.604 117.368 3.546 0.61 312893. 0.4858
|
|
38.58 0.2645 0.5806 0.0693 0.0316 4.494 40.462 25.362 3351.024 4.571 112.811 3.433 0.61 313300. 0.4611
|
|
42.09 0.2886 0.6131 0.0664 0.0312 4.443 40.004 24.273 3313.070 4.520 107.967 3.323 0.61 313732. 0.4367
|
|
45.59 0.3126 0.6429 0.0632 0.0307 4.372 39.362 23.118 3259.862 4.447 102.828 3.217 0.61 314187. 0.4125
|
|
49.10 0.3367 0.6701 0.0599 0.0301 4.279 38.524 21.898 3190.498 4.352 97.400 3.113 0.61 314667. 0.3885
|
|
52.61 0.3607 0.6946 0.0564 0.0293 4.164 37.489 20.618 3104.777 4.235 91.707 3.012 0.61 315171. 0.3648
|
|
56.11 0.3848 0.7166 0.0527 0.0283 4.027 36.258 19.284 3002.802 4.096 85.776 2.913 0.62 315699. 0.3412
|
|
59.62 0.4088 0.7358 0.0489 0.0272 3.869 34.832 17.903 2884.756 3.935 79.634 2.815 0.62 316251. 0.3177
|
|
63.13 0.4329 0.7520 0.0451 0.0259 3.689 33.215 16.480 2750.846 3.753 73.305 2.717 0.62 316828. 0.2942
|
|
66.64 0.4569 0.7651 0.0411 0.0245 3.488 31.410 15.021 2601.321 3.549 66.814 2.619 0.62 317430. 0.2707
|
|
70.14 0.4810 0.7746 0.0370 0.0230 3.267 29.420 13.531 2436.486 3.324 60.185 2.519 0.62 318056. 0.2471
|
|
73.65 0.5050 0.7797 0.0328 0.0213 3.026 27.249 12.015 2256.721 3.079 53.444 2.415 0.62 318707. 0.2233
|
|
77.16 0.5291 0.7796 0.0286 0.0194 2.766 24.904 10.480 2062.524 2.814 46.615 2.305 0.62 319382. 0.1990
|
|
80.66 0.5531 0.7725 0.0244 0.0175 2.487 22.393 8.931 1854.524 2.530 39.727 2.184 0.62 320083. 0.1741
|
|
84.17 0.5772 0.7558 0.0202 0.0154 2.191 19.724 7.377 1633.528 2.228 32.811 2.048 0.62 320808. 0.1484
|
|
87.68 0.6012 0.7248 0.0159 0.0132 1.878 16.911 5.823 1400.561 1.911 25.900 1.886 0.62 321559. 0.1214
|
|
91.19 0.6253 0.6706 0.0117 0.0109 1.551 13.969 4.279 1156.897 1.578 19.031 1.677 0.62 322335. 0.0925
|
|
94.69 0.6493 0.5734 0.0075 0.0085 1.212 10.917 2.753 904.105 1.233 12.246 1.381 0.62 323136. 0.0611
|
|
98.20 0.6734 0.3810 0.0034 0.0061 0.864 7.776 1.257 644.019 0.879 5.590 0.885 0.62 323960. 0.0265
|
|
101.71 0.6974
|
|
|
|
|
|
|
|
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 0.0929 0.0298 6.331 49.875 44.397 4720.655 5.635 197.477 4.266 0.70 354252. 0.7581
|
|
3.98 0.0239 0.0722 0.0917 0.0303 6.438 50.722 43.791 4800.807 5.731 194.783 4.137 0.70 354480. 0.7302
|
|
7.97 0.0478 0.1401 0.0903 0.0308 6.540 51.528 43.127 4877.104 5.822 191.827 4.011 0.70 354729. 0.7025
|
|
11.95 0.0717 0.2036 0.0887 0.0312 6.635 52.277 42.400 4947.943 5.906 188.596 3.887 0.70 354998. 0.6750
|
|
15.93 0.0956 0.2630 0.0871 0.0317 6.721 52.951 41.608 5011.739 5.982 185.071 3.766 0.70 355289. 0.6478
|
|
19.91 0.1195 0.3184 0.0853 0.0320 6.795 53.532 40.746 5066.771 6.048 181.237 3.647 0.70 355603. 0.6210
|
|
23.90 0.1434 0.3701 0.0833 0.0323 6.854 54.002 39.811 5111.245 6.101 177.077 3.533 0.70 355940. 0.5945
|
|
27.88 0.1673 0.4182 0.0812 0.0325 6.897 54.341 38.799 5143.307 6.139 172.578 3.422 0.70 356301. 0.5684
|
|
31.86 0.1912 0.4629 0.0789 0.0326 6.921 54.529 37.708 5161.124 6.161 167.726 3.314 0.70 356687. 0.5427
|
|
35.84 0.2151 0.5044 0.0765 0.0326 6.924 54.547 36.536 5162.887 6.163 162.512 3.210 0.70 357099. 0.5175
|
|
39.83 0.2390 0.5428 0.0738 0.0325 6.902 54.378 35.280 5146.834 6.144 156.925 3.109 0.70 357536. 0.4925
|
|
43.81 0.2629 0.5784 0.0710 0.0323 6.854 54.002 33.939 5111.233 6.101 150.960 3.012 0.70 358000. 0.4680
|
|
47.79 0.2868 0.6113 0.0680 0.0319 6.778 53.401 32.511 5054.364 6.033 144.610 2.917 0.70 358490. 0.4437
|
|
51.77 0.3106 0.6415 0.0649 0.0314 6.671 52.556 30.995 4974.379 5.938 137.864 2.826 0.70 359008. 0.4196
|
|
55.76 0.3345 0.6691 0.0615 0.0308 6.530 51.451 29.390 4869.782 5.813 130.728 2.737 0.70 359552. 0.3958
|
|
59.74 0.3584 0.6943 0.0580 0.0299 6.357 50.081 27.704 4740.144 5.658 123.229 2.651 0.70 360124. 0.3721
|
|
63.72 0.3823 0.7169 0.0543 0.0290 6.149 48.448 25.945 4585.611 5.474 115.403 2.566 0.70 360723. 0.3486
|
|
67.70 0.4062 0.7369 0.0505 0.0278 5.909 46.556 24.120 4406.470 5.260 107.288 2.483 0.70 361349. 0.3252
|
|
71.69 0.4301 0.7542 0.0465 0.0265 5.636 44.407 22.238 4203.059 5.017 98.915 2.400 0.70 362003. 0.3018
|
|
75.67 0.4540 0.7685 0.0425 0.0251 5.332 42.005 20.305 3975.760 4.746 90.318 2.317 0.71 362684. 0.2784
|
|
79.65 0.4779 0.7793 0.0384 0.0235 4.995 39.356 18.329 3725.036 4.446 81.528 2.232 0.71 363394. 0.2548
|
|
83.64 0.5018 0.7862 0.0342 0.0218 4.628 36.466 16.317 3451.463 4.120 72.578 2.144 0.71 364130. 0.2310
|
|
87.62 0.5257 0.7882 0.0299 0.0199 4.232 33.342 14.277 3155.777 3.767 63.503 2.052 0.71 364895. 0.2068
|
|
91.60 0.5496 0.7838 0.0256 0.0179 3.807 29.994 12.217 2838.943 3.389 54.339 1.952 0.71 365687. 0.1820
|
|
95.58 0.5735 0.7706 0.0212 0.0158 3.356 26.437 10.145 2502.228 2.987 45.127 1.839 0.71 366508. 0.1562
|
|
99.57 0.5974 0.7444 0.0169 0.0136 2.880 22.686 8.073 2147.256 2.563 35.909 1.705 0.71 367357. 0.1292
|
|
103.55 0.6213 0.6968 0.0126 0.0112 2.382 18.765 6.011 1776.081 2.120 26.736 1.535 0.71 368233. 0.1004
|
|
107.53 0.6452 0.6103 0.0083 0.0088 1.866 14.699 3.971 1391.276 1.661 17.662 1.295 0.71 369138. 0.0688
|
|
111.51 0.6691 0.4378 0.0041 0.0063 1.336 10.522 1.966 995.925 1.189 8.747 0.896 0.71 370071. 0.0335
|
|
115.50 0.6930 0.0002 0.0000 0.0037 0.793 6.246 0.001 591.189 0.706 0.003 0.000 0.71 371003. 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 0.0948 0.0316 9.563 66.972 57.323 7131.209 7.566 254.974 3.646 0.79 398471. 0.7362
|
|
4.47 0.0238 0.0696 0.0936 0.0321 9.691 67.865 56.582 7226.298 7.667 251.679 3.551 0.79 398729. 0.7125
|
|
8.94 0.0477 0.1356 0.0922 0.0325 9.811 68.706 55.765 7315.840 7.762 248.042 3.457 0.79 399009. 0.6886
|
|
13.42 0.0715 0.1978 0.0907 0.0328 9.921 69.476 54.866 7397.825 7.849 244.042 3.364 0.79 399312. 0.6646
|
|
17.89 0.0954 0.2565 0.0891 0.0331 10.018 70.156 53.879 7470.269 7.926 239.656 3.271 0.79 399641. 0.6404
|
|
22.36 0.1192 0.3117 0.0873 0.0334 10.099 70.726 52.801 7530.989 7.991 234.860 3.180 0.79 399995. 0.6163
|
|
26.83 0.1431 0.3635 0.0854 0.0336 10.162 71.165 51.626 7577.693 8.040 229.632 3.090 0.79 400376. 0.5922
|
|
31.30 0.1669 0.4119 0.0833 0.0337 10.202 71.449 50.349 7607.974 8.072 223.952 3.002 0.79 400784. 0.5681
|
|
35.77 0.1908 0.4572 0.0810 0.0338 10.218 71.556 48.967 7619.316 8.084 217.803 2.915 0.79 401220. 0.5440
|
|
40.25 0.2146 0.4993 0.0785 0.0338 10.204 71.460 47.475 7609.142 8.074 211.171 2.830 0.79 401685. 0.5201
|
|
44.72 0.2385 0.5385 0.0759 0.0336 10.158 71.138 45.873 7574.854 8.037 204.043 2.747 0.79 402179. 0.4962
|
|
49.19 0.2623 0.5748 0.0730 0.0333 10.076 70.565 44.157 7513.816 7.972 196.410 2.666 0.79 402702. 0.4724
|
|
53.66 0.2862 0.6084 0.0700 0.0329 9.955 69.716 42.326 7423.366 7.876 188.265 2.586 0.79 403255. 0.4487
|
|
58.13 0.3100 0.6393 0.0668 0.0324 9.790 68.562 40.377 7300.569 7.746 179.595 2.509 0.79 403839. 0.4251
|
|
62.60 0.3339 0.6677 0.0634 0.0317 9.579 67.081 38.310 7142.811 7.579 170.401 2.433 0.79 404452. 0.4016
|
|
67.08 0.3577 0.6935 0.0598 0.0308 9.319 65.260 36.133 6948.978 7.373 160.719 2.358 0.79 405097. 0.3781
|
|
71.55 0.3816 0.7169 0.0560 0.0298 9.011 63.102 33.857 6719.132 7.129 150.596 2.285 0.79 405771. 0.3547
|
|
76.02 0.4054 0.7376 0.0521 0.0286 8.655 60.609 31.493 6453.674 6.848 140.080 2.213 0.79 406477. 0.3313
|
|
80.49 0.4293 0.7557 0.0480 0.0273 8.251 57.784 29.050 6152.905 6.528 129.214 2.141 0.79 407212. 0.3078
|
|
84.96 0.4531 0.7707 0.0439 0.0258 7.802 54.635 26.538 5817.584 6.173 118.043 2.069 0.79 407979. 0.2843
|
|
89.44 0.4770 0.7822 0.0396 0.0242 7.307 51.172 23.967 5448.778 5.781 106.607 1.995 0.79 408776. 0.2605
|
|
93.91 0.5008 0.7896 0.0353 0.0224 6.769 47.406 21.346 5047.801 5.356 94.949 1.918 0.80 409604. 0.2364
|
|
98.38 0.5247 0.7918 0.0309 0.0205 6.191 43.355 18.686 4616.431 4.898 83.114 1.836 0.80 410463. 0.2117
|
|
102.85 0.5485 0.7870 0.0265 0.0184 5.575 39.039 15.996 4156.914 4.411 71.150 1.745 0.80 411354. 0.1862
|
|
107.32 0.5724 0.7723 0.0220 0.0163 4.924 34.485 13.288 3672.032 3.896 59.106 1.641 0.80 412275. 0.1596
|
|
111.79 0.5962 0.7427 0.0175 0.0140 4.245 29.727 10.576 3165.297 3.358 47.041 1.515 0.80 413227. 0.1314
|
|
116.27 0.6201 0.6892 0.0130 0.0117 3.542 24.802 7.873 2640.984 2.802 35.018 1.352 0.80 414211. 0.1012
|
|
120.74 0.6439 0.5928 0.0086 0.0093 2.822 19.761 5.195 2104.160 2.233 23.109 1.120 0.80 415226. 0.0681
|
|
125.21 0.6678 0.4085 0.0042 0.0069 2.093 14.656 2.561 1560.573 1.656 11.390 0.744 0.80 416272. 0.0318
|
|
129.68 0.6916 -0.0066 0.0000 0.0045 1.358 9.508 -0.026 1012.449 1.074 -0.115 -0.012 0.80 417318. 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 0.0968 0.0375 15.547 97.992 72.256 11593.646 11.071 321.396 2.827 0.87 442664. 0.6409
|
|
4.98 0.0239 0.0606 0.0956 0.0377 15.637 98.557 71.400 11660.432 11.135 317.586 2.777 0.87 442950. 0.6259
|
|
9.95 0.0478 0.1190 0.0944 0.0379 15.709 99.009 70.445 11713.876 11.186 313.339 2.728 0.87 443263. 0.6106
|
|
14.93 0.0716 0.1752 0.0929 0.0380 15.759 99.327 69.385 11751.578 11.222 308.626 2.678 0.87 443602. 0.5950
|
|
19.90 0.0955 0.2293 0.0914 0.0381 15.786 99.494 68.213 11771.278 11.241 303.410 2.628 0.87 443969. 0.5790
|
|
24.88 0.1194 0.2812 0.0896 0.0381 15.785 99.489 66.920 11770.668 11.240 297.659 2.579 0.87 444365. 0.5626
|
|
29.85 0.1433 0.3310 0.0877 0.0380 15.754 99.292 65.499 11747.427 11.218 291.341 2.529 0.87 444792. 0.5459
|
|
34.83 0.1672 0.3785 0.0857 0.0378 15.689 98.884 63.945 11699.158 11.172 284.427 2.479 0.87 445249. 0.5287
|
|
39.80 0.1911 0.4239 0.0834 0.0376 15.587 98.244 62.251 11623.425 11.100 276.891 2.429 0.87 445738. 0.5112
|
|
44.78 0.2149 0.4670 0.0809 0.0372 15.446 97.352 60.412 11517.849 10.999 268.711 2.379 0.87 446259. 0.4932
|
|
49.76 0.2388 0.5079 0.0783 0.0368 15.261 96.187 58.424 11380.043 10.867 259.871 2.329 0.88 446813. 0.4747
|
|
54.73 0.2627 0.5465 0.0754 0.0362 15.030 94.730 56.286 11207.621 10.702 250.359 2.278 0.88 447400. 0.4558
|
|
59.71 0.2866 0.5829 0.0723 0.0356 14.749 92.958 53.994 10997.999 10.502 240.164 2.227 0.88 448021. 0.4364
|
|
64.68 0.3105 0.6168 0.0690 0.0348 14.413 90.846 51.545 10748.123 10.264 229.272 2.175 0.88 448675. 0.4165
|
|
69.66 0.3344 0.6483 0.0656 0.0338 14.021 88.370 48.940 10455.238 9.984 217.683 2.123 0.88 449363. 0.3961
|
|
74.63 0.3582 0.6774 0.0619 0.0327 13.569 85.521 46.187 10118.157 9.662 205.441 2.070 0.88 450085. 0.3753
|
|
79.61 0.3821 0.7040 0.0580 0.0315 13.058 82.299 43.302 9736.986 9.298 192.608 2.017 0.88 450841. 0.3540
|
|
84.58 0.4060 0.7276 0.0540 0.0301 12.492 78.737 40.298 9315.542 8.896 179.246 1.962 0.88 451631. 0.3322
|
|
89.56 0.4299 0.7472 0.0498 0.0287 11.885 74.912 37.187 8862.932 8.463 165.407 1.903 0.88 452454. 0.3095
|
|
94.53 0.4538 0.7622 0.0455 0.0271 11.238 70.833 33.981 8380.326 8.003 151.147 1.839 0.88 453312. 0.2859
|
|
99.51 0.4776 0.7713 0.0411 0.0255 10.559 66.552 30.692 7873.852 7.519 136.520 1.768 0.88 454203. 0.2612
|
|
104.49 0.5015 0.7739 0.0366 0.0237 9.841 62.027 27.335 7338.492 7.008 121.588 1.690 0.88 455129. 0.2356
|
|
109.46 0.5254 0.7690 0.0320 0.0219 9.081 57.237 23.925 6771.849 6.467 106.418 1.602 0.88 456088. 0.2091
|
|
114.44 0.5493 0.7539 0.0274 0.0200 8.287 52.231 20.475 6179.550 5.901 91.071 1.503 0.89 457082. 0.1814
|
|
119.41 0.5732 0.7249 0.0228 0.0180 7.467 47.064 17.000 5568.191 5.317 75.617 1.385 0.89 458110. 0.1523
|
|
124.39 0.5971 0.6763 0.0181 0.0160 6.631 41.791 13.519 4944.388 4.722 60.132 1.240 0.89 459172. 0.1216
|
|
129.36 0.6209 0.5990 0.0135 0.0140 5.788 36.480 10.051 4315.957 4.121 44.706 1.056 0.89 460269. 0.0893
|
|
134.34 0.6448 0.4789 0.0089 0.0119 4.950 31.200 6.618 3691.370 3.525 29.438 0.813 0.89 461400. 0.0558
|
|
139.31 0.6687 0.2920 0.0043 0.0100 4.129 26.023 3.246 3078.838 2.940 14.436 0.478 0.89 462566. 0.0230
|
|
144.29 0.6926 -0.0072 -0.0001 0.0080 3.321 20.929 -0.062 2476.125 2.365 -0.278 -0.011 0.89 463743. 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 0.0962 0.0454 25.081 143.713 86.854 18703.221 16.237 386.326 2.106 0.96 486949. 0.5235
|
|
5.55 0.0242 0.0504 0.0952 0.0457 25.248 144.665 86.022 18827.072 16.344 382.625 2.072 0.96 487258. 0.5126
|
|
11.10 0.0484 0.0992 0.0942 0.0460 25.382 145.433 85.078 18927.143 16.431 378.425 2.039 0.96 487597. 0.5016
|
|
16.65 0.0727 0.1464 0.0930 0.0462 25.475 145.969 84.009 18996.775 16.491 373.674 2.006 0.96 487966. 0.4903
|
|
22.20 0.0969 0.1921 0.0917 0.0462 25.519 146.217 82.803 19029.164 16.520 368.309 1.974 0.96 488368. 0.4790
|
|
27.75 0.1211 0.2363 0.0902 0.0462 25.503 146.127 81.445 19017.359 16.509 362.268 1.942 0.96 488804. 0.4676
|
|
33.30 0.1453 0.2792 0.0885 0.0460 25.419 145.646 79.922 18954.803 16.455 355.492 1.912 0.96 489275. 0.4560
|
|
38.85 0.1695 0.3208 0.0866 0.0458 25.259 144.730 78.220 18835.621 16.352 347.925 1.884 0.96 489782. 0.4443
|
|
44.40 0.1937 0.3612 0.0845 0.0453 25.016 143.340 76.329 18654.742 16.195 339.512 1.856 0.96 490327. 0.4324
|
|
49.95 0.2180 0.4006 0.0822 0.0447 24.685 141.443 74.237 18407.854 15.980 330.204 1.829 0.96 490909. 0.4203
|
|
55.50 0.2422 0.4388 0.0796 0.0440 24.264 139.031 71.937 18093.869 15.708 319.977 1.803 0.96 491530. 0.4079
|
|
61.05 0.2664 0.4758 0.0769 0.0430 23.752 136.093 69.425 17711.496 15.376 308.804 1.778 0.96 492189. 0.3951
|
|
66.60 0.2906 0.5117 0.0738 0.0419 23.146 132.626 66.697 17260.301 14.984 296.668 1.753 0.96 492888. 0.3818
|
|
72.15 0.3148 0.5463 0.0706 0.0407 22.449 128.628 63.748 16740.033 14.532 283.550 1.727 0.96 493626. 0.3678
|
|
77.70 0.3391 0.5795 0.0671 0.0392 21.659 124.103 60.578 16151.196 14.021 269.451 1.701 0.97 494403. 0.3531
|
|
83.25 0.3633 0.6110 0.0633 0.0376 20.782 119.078 57.202 15497.192 13.453 254.436 1.674 0.97 495219. 0.3377
|
|
88.80 0.3875 0.6407 0.0594 0.0359 19.824 113.590 53.641 14782.941 12.833 238.595 1.646 0.97 496074. 0.3215
|
|
94.35 0.4117 0.6683 0.0553 0.0340 18.792 107.674 49.915 14013.078 12.165 222.022 1.616 0.97 496967. 0.3044
|
|
99.90 0.4359 0.6928 0.0510 0.0321 17.703 101.435 46.043 13201.062 11.460 204.798 1.582 0.97 497899. 0.2863
|
|
105.45 0.4601 0.7113 0.0465 0.0301 16.617 95.215 42.038 12391.558 10.757 186.984 1.539 0.97 498869. 0.2661
|
|
111.00 0.4844 0.7213 0.0420 0.0282 15.559 89.150 37.918 11602.199 10.072 168.659 1.482 0.97 499877. 0.2435
|
|
116.55 0.5086 0.7125 0.0373 0.0266 14.693 84.190 33.686 10956.784 9.512 149.833 1.394 0.97 500923. 0.2159
|
|
122.10 0.5328 0.6899 0.0325 0.0251 13.866 79.449 29.383 10339.722 8.976 130.695 1.289 0.97 502008. 0.1863
|
|
127.65 0.5570 0.6541 0.0277 0.0236 13.031 74.666 25.043 9717.281 8.436 111.389 1.169 0.97 503131. 0.1560
|
|
133.20 0.5812 0.6024 0.0229 0.0221 12.202 69.916 20.694 9099.017 7.899 92.048 1.032 0.98 504292. 0.1252
|
|
138.75 0.6055 0.5317 0.0181 0.0206 11.391 65.268 16.371 8494.148 7.374 72.819 0.874 0.98 505492. 0.0943
|
|
144.30 0.6297 0.4394 0.0134 0.0192 10.608 60.780 12.112 7910.110 6.867 53.874 0.695 0.98 506731. 0.0645
|
|
149.85 0.6539 0.3225 0.0088 0.0179 9.858 56.487 7.956 7351.415 6.382 35.388 0.491 0.98 508011. 0.0369
|
|
155.40 0.6781 0.1782 0.0044 0.0166 9.147 52.410 3.934 6820.768 5.921 17.497 0.262 0.98 509338. 0.0138
|
|
160.95 0.7023 -0.0004 0.0000 0.0153 8.424 48.268 -0.007 6281.714 5.453 -0.031 -0.001 0.98 510765. 0.0000
|
|
|
|
|
|
|