ファイルインデックス名　: File Index Name        : 3220        .A90
翼型整理番号　　　　　　: Airfoil Serial No.     : S04-0002-1
翼型名　　　　　　　　　: Airfoil Name           : S4053-089-84
翼型ファイル番号　　　　: Airfoil File No.       : 3220
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.   : X68eB03-C01G2


座標　　　　　　　　　　: Plot Ordinates         :

 X             Y

 1.00000, 0.00000
 0.98671, 0.00266
 0.97362, 0.00519
 0.96072, 0.00761
 0.94801, 0.00992
 0.93549, 0.01214
 0.92315, 0.01427
 0.91099, 0.01632
 0.89900, 0.01830
 0.88719, 0.02023
 0.87554, 0.02212
 0.86406, 0.02395
 0.85274, 0.02574
 0.84158, 0.02747
 0.83058, 0.02917
 0.81973, 0.03081
 0.80903, 0.03242
 0.79848, 0.03399
 0.78808, 0.03553
 0.77781, 0.03704
 0.76769, 0.03853
 0.75770, 0.03999
 0.74785, 0.04141
 0.73814, 0.04280
 0.72855, 0.04416
 0.71909, 0.04548
 0.70976, 0.04678
 0.70055, 0.04804
 0.69146, 0.04926
 0.68249, 0.05047
 0.67363, 0.05164
 0.66490, 0.05278
 0.65627, 0.05389
 0.64776, 0.05497
 0.63935, 0.05601
 0.63106, 0.05702
 0.62287, 0.05800
 0.61478, 0.05895
 0.60680, 0.05987
 0.59891, 0.06075
 0.59112, 0.06159
 0.58344, 0.06240
 0.57584, 0.06318
 0.56834, 0.06392
 0.56094, 0.06463
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 0.54639, 0.06597
 0.53925, 0.06660
 0.53220, 0.06719
 0.52523, 0.06776
 0.51835, 0.06830
 0.51155, 0.06881
 0.50483, 0.06930
 0.49819, 0.06975
 0.49163, 0.07017
 0.48514, 0.07056
 0.47874, 0.07092
 0.47240, 0.07126
 0.46614, 0.07158
 0.45996, 0.07187
 0.45384, 0.07214
 0.44780, 0.07239
 0.44182, 0.07262
 0.43591, 0.07283
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 0.32596, 0.07333
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 0.16963, 0.06145
 0.16654, 0.06103
 0.16348, 0.06059
 0.16044, 0.06016
 0.15743, 0.05971
 0.15445, 0.05926
 0.15150, 0.05881
 0.14858, 0.05835
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 0.14280, 0.05742
 0.13996, 0.05694
 0.13713, 0.05646
 0.13434, 0.05597
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 0.12340, 0.05397
 0.12072, 0.05346
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 0.10769, 0.05080
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 0.10264, 0.04970
 0.10014, 0.04914
 0.09767, 0.04857
 0.09521, 0.04800
 0.09278, 0.04742
 0.09037, 0.04683
 0.08798, 0.04624
 0.08561, 0.04564
 0.08326, 0.04504
 0.08093, 0.04442
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 0.07633, 0.04318
 0.07405, 0.04254
 0.07180, 0.04190
 0.06956, 0.04125
 0.06735, 0.04060
 0.06515, 0.03993
 0.06297, 0.03926
 0.06081, 0.03857
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 0.05653, 0.03718
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 0.04820, 0.03426
 0.04615, 0.03350
 0.04413, 0.03273
 0.04212, 0.03195
 0.04012, 0.03114
 0.03815, 0.03033
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 0.02473, 0.02405
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 0.00337, 0.00803
 0.00168, 0.00554
 0.00056, 0.00311
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 1.00000, 0.00000