ファイルインデックス名　: File Index Name        : 1002        .A00
翼型整理番号　　　　　　: Airfoil Serial No.     : N01-0002-0
翼型名　　　　　　　　　: Airfoil Name           : N.A.C.A. 0008
翼型ファイル番号　　　　: Airfoil File No.       : 1002
翼型情報　　　　　　　　: Airfoil Information    : Computed

算出前縁半径　　　　　　: Computed L.E.R.        : 0.705 %
算出前縁傾斜　　　　　　: Computed Slope of L.E. : 0
算出プログラム番号　　　: Computed Program No.   : ウハク-40


座標　　　　　　　　　　: Plot Ordinates         :

 X             Y

 1.00000, 0.00084
 0.98671, 0.00207
 0.97362, 0.00327
 0.96072, 0.00443
 0.94801, 0.00555
 0.93549, 0.00664
 0.92315, 0.00770
 0.91099, 0.00873
 0.89900, 0.00973
 0.88719, 0.01071
 0.87554, 0.01165
 0.86406, 0.01257
 0.85274, 0.01347
 0.84158, 0.01434
 0.83058, 0.01519
 0.81973, 0.01601
 0.80903, 0.01682
 0.79848, 0.01760
 0.78808, 0.01836
 0.77781, 0.01910
 0.76769, 0.01983
 0.75770, 0.02053
 0.74785, 0.02122
 0.73814, 0.02189
 0.72855, 0.02254
 0.71909, 0.02317
 0.70976, 0.02379
 0.70055, 0.02439
 0.69146, 0.02498
 0.68249, 0.02555
 0.67363, 0.02610
 0.66490, 0.02664
 0.65627, 0.02717
 0.64776, 0.02768
 0.63935, 0.02818
 0.63106, 0.02867
 0.62287, 0.02914
 0.61478, 0.02960
 0.60680, 0.03005
 0.59891, 0.03048
 0.59112, 0.03090
 0.58344, 0.03131
 0.57584, 0.03171
 0.56834, 0.03210
 0.56094, 0.03247
 0.55362, 0.03284
 0.54639, 0.03319
 0.53925, 0.03353
 0.53220, 0.03387
 0.52523, 0.03419
 0.51835, 0.03450
 0.51155, 0.03480
 0.50483, 0.03509
 0.49819, 0.03537
 0.49163, 0.03564
 0.48514, 0.03590
 0.47874, 0.03615
 0.47240, 0.03640
 0.46614, 0.03663
 0.45996, 0.03686
 0.45384, 0.03707
 0.44780, 0.03728
 0.44182, 0.03748
 0.43591, 0.03767
 0.43007, 0.03785
 0.42430, 0.03802
 0.41859, 0.03819
 0.41295, 0.03835
 0.40737, 0.03850
 0.40185, 0.03864
 0.39639, 0.03878
 0.39099, 0.03890
 0.38566, 0.03902
 0.38038, 0.03913
 0.37516, 0.03924
 0.37000, 0.03934
 0.36489, 0.03943
 0.35984, 0.03951
 0.35484, 0.03959
 0.34990, 0.03966
 0.34501, 0.03972
 0.34017, 0.03978
 0.33538, 0.03983
 0.33065, 0.03987
 0.32596, 0.03991
 0.32133, 0.03994
 0.31674, 0.03997
 0.31220, 0.03999
 0.30771, 0.04000
 0.30326, 0.04001
 0.29887, 0.04001
 0.29451, 0.04001
 0.29020, 0.04000
 0.28594, 0.03998
 0.28172, 0.03996
 0.27754, 0.03993
 0.27340, 0.03990
 0.26931, 0.03986
 0.26526, 0.03982
 0.26125, 0.03977
 0.25728, 0.03972
 0.25334, 0.03966
 0.24945, 0.03960
 0.24560, 0.03953
 0.24178, 0.03946
 0.23800, 0.03938
 0.23426, 0.03930
 0.23056, 0.03921
 0.22689, 0.03911
 0.22326, 0.03902
 0.21966, 0.03891
 0.21610, 0.03881
 0.21257, 0.03870
 0.20907, 0.03858
 0.20561, 0.03846
 0.20218, 0.03833
 0.19879, 0.03820
 0.19542, 0.03807
 0.19209, 0.03793
 0.18879, 0.03779
 0.18552, 0.03764
 0.18228, 0.03749
 0.17908, 0.03733
 0.17590, 0.03717
 0.17275, 0.03701
 0.16963, 0.03684
 0.16654, 0.03666
 0.16348, 0.03649
 0.16044, 0.03631
 0.15743, 0.03612
 0.15445, 0.03593
 0.15150, 0.03574
 0.14858, 0.03554
 0.14568, 0.03533
 0.14280, 0.03513
 0.13996, 0.03492
 0.13713, 0.03470
 0.13434, 0.03448
 0.13157, 0.03426
 0.12882, 0.03403
 0.12610, 0.03380
 0.12340, 0.03356
 0.12072, 0.03332
 0.11807, 0.03308
 0.11544, 0.03283
 0.11283, 0.03257
 0.11025, 0.03231
 0.10769, 0.03205
 0.10515, 0.03178
 0.10264, 0.03151
 0.10014, 0.03123
 0.09767, 0.03095
 0.09521, 0.03067
 0.09278, 0.03038
 0.09037, 0.03008
 0.08798, 0.02978
 0.08561, 0.02947
 0.08326, 0.02916
 0.08093, 0.02884
 0.07862, 0.02852
 0.07633, 0.02819
 0.07405, 0.02786
 0.07180, 0.02752
 0.06956, 0.02717
 0.06735, 0.02682
 0.06515, 0.02646
 0.06297, 0.02610
 0.06081, 0.02573
 0.05866, 0.02535
 0.05653, 0.02496
 0.05442, 0.02456
 0.05233, 0.02416
 0.05026, 0.02375
 0.04820, 0.02333
 0.04615, 0.02290
 0.04413, 0.02246
 0.04212, 0.02201
 0.04012, 0.02155
 0.03815, 0.02107
 0.03618, 0.02059
 0.03424, 0.02009
 0.03231, 0.01957
 0.03039, 0.01904
 0.02849, 0.01850
 0.02660, 0.01793
 0.02473, 0.01735
 0.02287, 0.01674
 0.02103, 0.01610
 0.01920, 0.01544
 0.01739, 0.01474
 0.01559, 0.01401
 0.01380, 0.01323
 0.01203, 0.01240
 0.01027, 0.01150
 0.00853, 0.01053
 0.00680, 0.00944
 0.00508, 0.00820
 0.00337, 0.00673
 0.00168, 0.00478
 0.00056, 0.00278
 0.00000, 0.00000
 0.00000, 0.00000
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 0.00168,-0.00478
 0.00337,-0.00673
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 0.00680,-0.00944
 0.00853,-0.01053
 0.01027,-0.01150
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 0.01559,-0.01401
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 0.02473,-0.01735
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 0.02849,-0.01850
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 0.03231,-0.01957
 0.03424,-0.02009
 0.03618,-0.02059
 0.03815,-0.02107
 0.04012,-0.02155
 0.04212,-0.02201
 0.04413,-0.02246
 0.04615,-0.02290
 0.04820,-0.02333
 0.05026,-0.02375
 0.05233,-0.02416
 0.05442,-0.02456
 0.05653,-0.02496
 0.05866,-0.02535
 0.06081,-0.02573
 0.06297,-0.02610
 0.06515,-0.02646
 0.06735,-0.02682
 0.06956,-0.02717
 0.07180,-0.02752
 0.07405,-0.02786
 0.07633,-0.02819
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 0.08093,-0.02884
 0.08326,-0.02916
 0.08561,-0.02947
 0.08798,-0.02978
 0.09037,-0.03008
 0.09278,-0.03038
 0.09521,-0.03067
 0.09767,-0.03095
 0.10014,-0.03123
 0.10264,-0.03151
 0.10515,-0.03178
 0.10769,-0.03205
 0.11025,-0.03231
 0.11283,-0.03257
 0.11544,-0.03283
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 0.12072,-0.03332
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 0.12882,-0.03403
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 0.13434,-0.03448
 0.13713,-0.03470
 0.13996,-0.03492
 0.14280,-0.03513
 0.14568,-0.03533
 0.14858,-0.03554
 0.15150,-0.03574
 0.15445,-0.03593
 0.15743,-0.03612
 0.16044,-0.03631
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 0.16654,-0.03666
 0.16963,-0.03684
 0.17275,-0.03701
 0.17590,-0.03717
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