ファイルインデックス名　: File Index Name        : 3219        .A90
翼型整理番号　　　　　　: Airfoil Serial No.     : S04-0001-1
翼型名　　　　　　　　　: Airfoil Name           : S3021-095-84
翼型ファイル番号　　　　: Airfoil File No.       : 3219
翼型情報　　　　　　　　: Airfoil Information    : (informal)

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.   : X68eB03-C01G2


座標　　　　　　　　　　: Plot Ordinates         :

 X             Y

 1.00000, 0.00000
 0.98671, 0.00199
 0.97362, 0.00399
 0.96072, 0.00600
 0.94801, 0.00800
 0.93549, 0.00999
 0.92315, 0.01196
 0.91099, 0.01390
 0.89900, 0.01581
 0.88719, 0.01765
 0.87554, 0.01943
 0.86406, 0.02117
 0.85274, 0.02287
 0.84158, 0.02453
 0.83058, 0.02615
 0.81973, 0.02774
 0.80903, 0.02932
 0.79848, 0.03088
 0.78808, 0.03241
 0.77781, 0.03391
 0.76769, 0.03538
 0.75770, 0.03682
 0.74785, 0.03824
 0.73814, 0.03963
 0.72855, 0.04099
 0.71909, 0.04232
 0.70976, 0.04363
 0.70055, 0.04491
 0.69146, 0.04616
 0.68249, 0.04739
 0.67363, 0.04860
 0.66490, 0.04978
 0.65627, 0.05094
 0.64776, 0.05206
 0.63935, 0.05316
 0.63106, 0.05423
 0.62287, 0.05528
 0.61478, 0.05629
 0.60680, 0.05728
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 0.53220, 0.06565
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 0.51835, 0.06700
 0.51155, 0.06764
 0.50483, 0.06826
 0.49819, 0.06885
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 0.47874, 0.07045
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 0.44780, 0.07262
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 0.15445, 0.06423
 0.15150, 0.06377
 0.14858, 0.06330
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 0.14280, 0.06234
 0.13996, 0.06185
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 0.12072, 0.05821
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 0.10264, 0.05419
 0.10014, 0.05358
 0.09767, 0.05297
 0.09521, 0.05235
 0.09278, 0.05172
 0.09037, 0.05108
 0.08798, 0.05043
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 0.07633, 0.04706
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 0.06956, 0.04492
 0.06735, 0.04419
 0.06515, 0.04344
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 0.06081, 0.04192
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 0.04615, 0.03617
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 0.00337, 0.00783
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