ファイルインデックス名　: File Index Name        : 0736        .A01
翼型整理番号　　　　　　: Airfoil Serial No.     : N09-0009-1
翼型名　　　　　　　　　: Airfoil Name           : Naylor & Griffiths 9
翼型ファイル番号　　　　: Airfoil File No.       : 0736
翼型情報　　　　　　　　: Airfoil Information    : (B.1)

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-A01E


座標　　　　　　　　　　: Plot Ordinates         :

 X             Y

 1.00000, 0.00000
 0.98671, 0.00574
 0.97362, 0.01036
 0.96072, 0.01404
 0.94801, 0.01690
 0.93549, 0.01909
 0.92315, 0.02073
 0.91099, 0.02195
 0.89900, 0.02292
 0.88719, 0.02430
 0.87554, 0.02562
 0.86406, 0.02689
 0.85274, 0.02811
 0.84158, 0.02928
 0.83058, 0.03041
 0.81973, 0.03149
 0.80903, 0.03254
 0.79848, 0.03355
 0.78808, 0.03454
 0.77781, 0.03551
 0.76769, 0.03644
 0.75770, 0.03733
 0.74785, 0.03820
 0.73814, 0.03903
 0.72855, 0.03983
 0.71909, 0.04060
 0.70976, 0.04134
 0.70055, 0.04206
 0.69146, 0.04274
 0.68249, 0.04338
 0.67363, 0.04401
 0.66490, 0.04460
 0.65627, 0.04518
 0.64776, 0.04572
 0.63935, 0.04625
 0.63106, 0.04675
 0.62287, 0.04723
 0.61478, 0.04770
 0.60680, 0.04814
 0.59891, 0.04856
 0.59112, 0.04895
 0.58344, 0.04932
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 0.56094, 0.05034
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 0.54639, 0.05096
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 0.53220, 0.05152
 0.52523, 0.05179
 0.51835, 0.05204
 0.51155, 0.05229
 0.50483, 0.05253
 0.49819, 0.05277
 0.49163, 0.05301
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 0.47874, 0.05348
 0.47240, 0.05371
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 0.44780, 0.05454
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 0.43591, 0.05493
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 0.16963, 0.05667
 0.16654, 0.05649
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 0.15743, 0.05592
 0.15445, 0.05572
 0.15150, 0.05551
 0.14858, 0.05531
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 0.14280, 0.05494
 0.13996, 0.05475
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 0.13434, 0.05434
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 0.12340, 0.05344
 0.12072, 0.05319
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 0.10769, 0.05180
 0.10515, 0.05149
 0.10264, 0.05116
 0.10014, 0.05082
 0.09767, 0.05045
 0.09521, 0.05006
 0.09278, 0.04966
 0.09037, 0.04925
 0.08798, 0.04882
 0.08561, 0.04838
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 0.08093, 0.04747
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 0.07633, 0.04649
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 0.06735, 0.04439
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 0.06297, 0.04325
 0.06081, 0.04266
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 0.04615, 0.03788
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 0.00337, 0.00923
 0.00168, 0.00635
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 0.00000, 0.00000
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 1.00000, 0.00000