Tip_Airfoil.txt

(3 KB) Pobierz
E205  (10.48%)
     1.000000   -0.000222
     0.992988    0.000466
     0.979837    0.002115
     0.964505    0.004292
     0.948400    0.006594
     0.932217    0.008826
     0.915924    0.010985
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     0.849898    0.019336
     0.833346    0.021408
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     0.800244    0.025537
     0.783687    0.027594
     0.767128    0.029649
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     0.503137    0.060037
     0.486776    0.061560
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     0.454144    0.064308
     0.437865    0.065511
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     0.180615    0.061872
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     0.011669    0.015215
     0.007531    0.011794
     0.004468    0.008693
     0.002412    0.006171
     0.001092    0.004107
     0.000325    0.002291
     0.000025    0.000575
     0.000196   -0.001157
     0.000842   -0.002980
     0.002030   -0.004936
     0.003912   -0.006978
     0.006770   -0.009044
     0.010894   -0.011171
     0.016428   -0.013610
     0.023831   -0.016380
     0.033623   -0.019228
     0.045986   -0.021977
     0.060079   -0.024504
     0.074876   -0.026643
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     0.153836   -0.033058
     0.170040   -0.033741
     0.186318   -0.034285
     0.202642   -0.034702
     0.218996   -0.035004
     0.235376   -0.035200
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     0.268197   -0.035301
     0.284635   -0.035217
     0.301090   -0.035052
     0.317561   -0.034811
     0.334049   -0.034500
     0.350551   -0.034123
     0.367067   -0.033686
     0.383593   -0.033193
     0.400130   -0.032649
     0.416676   -0.032056
     0.433232   -0.031419
     0.449798   -0.030742
     0.466374   -0.030028
     0.482961   -0.029281
     0.499560   -0.028505
     0.516168   -0.027705
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     0.549416   -0.026044
     0.566052   -0.025190
     0.582695   -0.024325
     0.599344   -0.023450
     0.615997   -0.022567
     0.632654   -0.021679
     0.649313   -0.020786
     0.665975   -0.019888
     0.682638   -0.018988
     0.699302   -0.018085
     0.715967   -0.017180
     0.732634   -0.016273
     0.749302   -0.015365
     0.765970   -0.014457
     0.782637   -0.013550
     0.799299   -0.012643
     0.815959   -0.011733
     0.832618   -0.010819
     0.849277   -0.009902
     0.865927   -0.008981
     0.882551   -0.008050
     0.899121   -0.007100
     0.915596   -0.006107
     0.931927   -0.005037
     0.948119   -0.003863
     0.964268   -0.002575
     0.979726   -0.001337
     0.992967   -0.000479
     1.000000   -0.000222
Zgłoś jeśli naruszono regulamin