ファイルインデックス名　: File Index Name        : 0262        .A01
翼型整理番号　　　　　　: Airfoil Serial No.     : T02-0001-1
翼型名　　　　　　　　　: Airfoil Name           : TsAGI 8%
翼型ファイル番号　　　　: Airfoil File No.       : 0262
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-A01C


座標　　　　　　　　　　: Plot Ordinates         :

 X             Y

 1.00000, 0.00000
 0.98671, 0.00129
 0.97362, 0.00256
 0.96072, 0.00381
 0.94801, 0.00505
 0.93549, 0.00628
 0.92315, 0.00749
 0.91099, 0.00869
 0.89900, 0.00987
 0.88719, 0.01103
 0.87554, 0.01218
 0.86406, 0.01331
 0.85274, 0.01443
 0.84158, 0.01553
 0.83058, 0.01662
 0.81973, 0.01770
 0.80903, 0.01876
 0.79848, 0.01980
 0.78808, 0.02084
 0.77781, 0.02186
 0.76769, 0.02287
 0.75770, 0.02386
 0.74785, 0.02484
 0.73814, 0.02580
 0.72855, 0.02675
 0.71909, 0.02768
 0.70976, 0.02860
 0.70055, 0.02950
 0.69146, 0.03037
 0.68249, 0.03123
 0.67363, 0.03208
 0.66490, 0.03290
 0.65627, 0.03371
 0.64776, 0.03450
 0.63935, 0.03528
 0.63106, 0.03603
 0.62287, 0.03677
 0.61478, 0.03750
 0.60680, 0.03820
 0.59891, 0.03890
 0.59112, 0.03957
 0.58344, 0.04023
 0.57584, 0.04088
 0.56834, 0.04150
 0.56094, 0.04211
 0.55362, 0.04270
 0.54639, 0.04328
 0.53925, 0.04384
 0.53220, 0.04438
 0.52523, 0.04490
 0.51835, 0.04541
 0.51155, 0.04590
 0.50483, 0.04637
 0.49819, 0.04682
 0.49163, 0.04724
 0.48514, 0.04765
 0.47874, 0.04804
 0.47240, 0.04842
 0.46614, 0.04878
 0.45996, 0.04912
 0.45384, 0.04945
 0.44780, 0.04976
 0.44182, 0.05006
 0.43591, 0.05034
 0.43007, 0.05061
 0.42430, 0.05086
 0.41859, 0.05110
 0.41295, 0.05133
 0.40737, 0.05154
 0.40185, 0.05174
 0.39639, 0.05192
 0.39099, 0.05209
 0.38566, 0.05225
 0.38038, 0.05240
 0.37516, 0.05253
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 0.35984, 0.05286
 0.35484, 0.05294
 0.34990, 0.05302
 0.34501, 0.05308
 0.34017, 0.05313
 0.33538, 0.05317
 0.33065, 0.05320
 0.32596, 0.05321
 0.32133, 0.05322
 0.31674, 0.05321
 0.31220, 0.05320
 0.30771, 0.05317
 0.30326, 0.05313
 0.29887, 0.05308
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 0.28594, 0.05285
 0.28172, 0.05275
 0.27754, 0.05265
 0.27340, 0.05253
 0.26931, 0.05241
 0.26526, 0.05227
 0.26125, 0.05213
 0.25728, 0.05198
 0.25334, 0.05182
 0.24945, 0.05165
 0.24560, 0.05148
 0.24178, 0.05129
 0.23800, 0.05110
 0.23426, 0.05090
 0.23056, 0.05069
 0.22689, 0.05048
 0.22326, 0.05026
 0.21966, 0.05003
 0.21610, 0.04979
 0.21257, 0.04955
 0.20907, 0.04929
 0.20561, 0.04904
 0.20218, 0.04877
 0.19879, 0.04850
 0.19542, 0.04822
 0.19209, 0.04794
 0.18879, 0.04765
 0.18552, 0.04735
 0.18228, 0.04704
 0.17908, 0.04673
 0.17590, 0.04642
 0.17275, 0.04610
 0.16963, 0.04577
 0.16654, 0.04544
 0.16348, 0.04510
 0.16044, 0.04475
 0.15743, 0.04440
 0.15445, 0.04405
 0.15150, 0.04369
 0.14858, 0.04332
 0.14568, 0.04294
 0.14280, 0.04256
 0.13996, 0.04217
 0.13713, 0.04177
 0.13434, 0.04138
 0.13157, 0.04097
 0.12882, 0.04057
 0.12610, 0.04016
 0.12340, 0.03974
 0.12072, 0.03932
 0.11807, 0.03889
 0.11544, 0.03847
 0.11283, 0.03803
 0.11025, 0.03760
 0.10769, 0.03716
 0.10515, 0.03671
 0.10264, 0.03627
 0.10014, 0.03582
 0.09767, 0.03537
 0.09521, 0.03491
 0.09278, 0.03446
 0.09037, 0.03399
 0.08798, 0.03353
 0.08561, 0.03306
 0.08326, 0.03259
 0.08093, 0.03211
 0.07862, 0.03163
 0.07633, 0.03114
 0.07405, 0.03064
 0.07180, 0.03015
 0.06956, 0.02964
 0.06735, 0.02913
 0.06515, 0.02862
 0.06297, 0.02810
 0.06081, 0.02757
 0.05866, 0.02704
 0.05653, 0.02649
 0.05442, 0.02594
 0.05233, 0.02539
 0.05026, 0.02482
 0.04820, 0.02424
 0.04615, 0.02364
 0.04413, 0.02304
 0.04212, 0.02243
 0.04012, 0.02181
 0.03815, 0.02118
 0.03618, 0.02054
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 0.03231, 0.01924
 0.03039, 0.01857
 0.02849, 0.01789
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 0.02473, 0.01650
 0.02287, 0.01576
 0.02103, 0.01501
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 0.01739, 0.01345
 0.01559, 0.01265
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 0.00853, 0.00907
 0.00680, 0.00811
 0.00508, 0.00668
 0.00337, 0.00530
 0.00168, 0.00377
 0.00056, 0.00227
 0.00000, 0.00000
 0.00000, 0.00000
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 0.03618,-0.01410
 0.03815,-0.01442
 0.04012,-0.01474
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 0.05653,-0.01689
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 0.11025,-0.02114
 0.11283,-0.02129
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 0.14280,-0.02280
 0.14568,-0.02292
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 1.00000, 0.00000