ファイルインデックス名　: File Index Name        : 1197        .A  
翼型整理番号　　　　　　: Airfoil Serial No.     : N04-0102-1
翼型名　　　　　　　　　: Airfoil Name           : N.A.C.A. 66>>1<<-212
翼型ファイル番号　　　　: Airfoil File No.       : 1197
翼型情報　　　　　　　　: Airfoil Information    : Original

算出前縁半径　　　　　　: Computed L.E.R.        : ?
算出前縁傾斜　　　　　　: Computed Slope of L.E. : ?
算出プログラム番号　　　: Computed Program No.   : VB6B05-A01C


座標　　　　　　　　　　: Plot Ordinates         :

 X             Y

 1.00000, 0.00000
 0.98655, 0.00190
 0.97329, 0.00394
 0.96020, 0.00613
 0.94730, 0.00842
 0.93458, 0.01078
 0.92204, 0.01320
 0.90967, 0.01565
 0.89748, 0.01809
 0.88546, 0.02050
 0.87361, 0.02289
 0.86193, 0.02526
 0.85042, 0.02758
 0.83907, 0.02985
 0.82788, 0.03207
 0.81685, 0.03424
 0.80597, 0.03637
 0.79524, 0.03843
 0.78468, 0.04042
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 0.76397, 0.04423
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 0.73397, 0.04949
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 0.71465, 0.05267
 0.70520, 0.05417
 0.69587, 0.05558
 0.68667, 0.05693
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 0.65980, 0.06055
 0.65108, 0.06162
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 0.15922, 0.05063
 0.15621, 0.05018
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 0.15030, 0.04928
 0.14739, 0.04883
 0.14451, 0.04836
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 0.13881, 0.04744
 0.13600, 0.04698
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 0.09680, 0.03970
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 0.08957, 0.03817
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 0.06899, 0.03342
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