ファイルインデックス名　: File Index Name        : 9026        .A00
翼型整理番号　　　　　　: Airfoil Serial No.     : B09-0010-0
翼型名　　　　　　　　　: Airfoil Name           : Bw 3A0614
翼型ファイル番号　　　　: Airfoil File No.       : 9026
翼型情報　　　　　　　　: Airfoil Information    : Computed

算出前縁半径　　　　　　: Computed L.E.R.        : 1.80 %
算出前縁傾斜　　　　　　: Computed Slope of L.E. : ?
算出プログラム番号　　　: Computed Program No.   : Bw 3/3A


座標　　　　　　　　　　: Plot Ordinates         :

 X             Y

 1.00000, 0.00000
 0.98685, 0.00286
 0.97392, 0.00574
 0.96119, 0.00863
 0.94865, 0.01152
 0.93631, 0.01440
 0.92415, 0.01726
 0.91217, 0.02011
 0.90036, 0.02293
 0.88873, 0.02573
 0.87726, 0.02850
 0.86596, 0.03124
 0.85481, 0.03395
 0.84382, 0.03662
 0.83298, 0.03926
 0.82229, 0.04186
 0.81175, 0.04442
 0.80135, 0.04695
 0.79109, 0.04943
 0.78096, 0.05188
 0.77098, 0.05428
 0.76111, 0.05664
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 0.74179, 0.06124
 0.73230, 0.06348
 0.72294, 0.06567
 0.71371, 0.06782
 0.70458, 0.06992
 0.69557, 0.07199
 0.68668, 0.07401
 0.67788, 0.07598
 0.66921, 0.07792
 0.66063, 0.07981
 0.65217, 0.08165
 0.64380, 0.08346
 0.63554, 0.08521
 0.62737, 0.08693
 0.61930, 0.08861
 0.61133, 0.09024
 0.60345, 0.09183
 0.59565, 0.09337
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 0.56540, 0.09915
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 0.52945, 0.10546
 0.52250, 0.10660
 0.51563, 0.10771
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 0.48239, 0.11266
 0.47594, 0.11355
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 0.17751, 0.11015
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 0.14538, 0.10241
 0.14234, 0.10158
 0.13933, 0.10073
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 0.08235, 0.08042
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 0.05685, 0.06784
 0.05466, 0.06662
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 0.00185, 0.02045
 0.00059, 0.01789
-0.00055, 0.01506
-0.00150, 0.01183
-0.00208, 0.00788
-0.00188, 0.00418
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