ファイルインデックス名　: File Index Name        : 1157        .A  
翼型整理番号　　　　　　: Airfoil Serial No.     : N04-0062-1
翼型名　　　　　　　　　: Airfoil Name           : N.A.C.A. 65-008
翼型ファイル番号　　　　: Airfoil File No.       : 1157
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, 0.00046
 0.97362, 0.00107
 0.96072, 0.00181
 0.94801, 0.00266
 0.93549, 0.00359
 0.92315, 0.00460
 0.91099, 0.00565
 0.89900, 0.00673
 0.88719, 0.00780
 0.87554, 0.00888
 0.86406, 0.00996
 0.85274, 0.01105
 0.84158, 0.01212
 0.83058, 0.01319
 0.81973, 0.01425
 0.80903, 0.01529
 0.79848, 0.01632
 0.78808, 0.01732
 0.77781, 0.01831
 0.76769, 0.01928
 0.75770, 0.02023
 0.74785, 0.02116
 0.73814, 0.02207
 0.72855, 0.02296
 0.71909, 0.02382
 0.70976, 0.02466
 0.70055, 0.02548
 0.69146, 0.02627
 0.68249, 0.02704
 0.67363, 0.02779
 0.66490, 0.02851
 0.65627, 0.02921
 0.64776, 0.02989
 0.63935, 0.03054
 0.63106, 0.03116
 0.62287, 0.03177
 0.61478, 0.03235
 0.60680, 0.03291
 0.59891, 0.03344
 0.59112, 0.03396
 0.58344, 0.03445
 0.57584, 0.03492
 0.56834, 0.03536
 0.56094, 0.03579
 0.55362, 0.03619
 0.54639, 0.03657
 0.53925, 0.03693
 0.53220, 0.03726
 0.52523, 0.03758
 0.51835, 0.03787
 0.51155, 0.03815
 0.50483, 0.03840
 0.49819, 0.03863
 0.49163, 0.03883
 0.48514, 0.03902
 0.47874, 0.03919
 0.47240, 0.03934
 0.46614, 0.03947
 0.45996, 0.03958
 0.45384, 0.03968
 0.44780, 0.03977
 0.44182, 0.03984
 0.43591, 0.03990
 0.43007, 0.03994
 0.42430, 0.03997
 0.41859, 0.03999
 0.41295, 0.04000
 0.40737, 0.04000
 0.40185, 0.03999
 0.39639, 0.03996
 0.39099, 0.03993
 0.38566, 0.03989
 0.38038, 0.03984
 0.37516, 0.03978
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 0.36489, 0.03964
 0.35984, 0.03956
 0.35484, 0.03947
 0.34990, 0.03938
 0.34501, 0.03928
 0.34017, 0.03918
 0.33538, 0.03907
 0.33065, 0.03895
 0.32596, 0.03883
 0.32133, 0.03871
 0.31674, 0.03858
 0.31220, 0.03844
 0.30771, 0.03830
 0.30326, 0.03816
 0.29887, 0.03801
 0.29451, 0.03786
 0.29020, 0.03771
 0.28594, 0.03755
 0.28172, 0.03738
 0.27754, 0.03722
 0.27340, 0.03705
 0.26931, 0.03688
 0.26526, 0.03670
 0.26125, 0.03652
 0.25728, 0.03634
 0.25334, 0.03615
 0.24945, 0.03596
 0.24560, 0.03577
 0.24178, 0.03558
 0.23800, 0.03538
 0.23426, 0.03518
 0.23056, 0.03498
 0.22689, 0.03477
 0.22326, 0.03456
 0.21966, 0.03435
 0.21610, 0.03414
 0.21257, 0.03392
 0.20907, 0.03371
 0.20561, 0.03349
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 0.19879, 0.03304
 0.19542, 0.03281
 0.19209, 0.03258
 0.18879, 0.03235
 0.18552, 0.03212
 0.18228, 0.03189
 0.17908, 0.03165
 0.17590, 0.03141
 0.17275, 0.03117
 0.16963, 0.03093
 0.16654, 0.03069
 0.16348, 0.03044
 0.16044, 0.03019
 0.15743, 0.02994
 0.15445, 0.02969
 0.15150, 0.02944
 0.14858, 0.02919
 0.14568, 0.02893
 0.14280, 0.02867
 0.13996, 0.02842
 0.13713, 0.02816
 0.13434, 0.02790
 0.13157, 0.02763
 0.12882, 0.02737
 0.12610, 0.02710
 0.12340, 0.02683
 0.12072, 0.02656
 0.11807, 0.02629
 0.11544, 0.02602
 0.11283, 0.02574
 0.11025, 0.02546
 0.10769, 0.02519
 0.10515, 0.02490
 0.10264, 0.02462
 0.10014, 0.02434
 0.09767, 0.02405
 0.09521, 0.02376
 0.09278, 0.02346
 0.09037, 0.02317
 0.08798, 0.02287
 0.08561, 0.02257
 0.08326, 0.02227
 0.08093, 0.02197
 0.07862, 0.02167
 0.07633, 0.02136
 0.07405, 0.02105
 0.07180, 0.02074
 0.06956, 0.02043
 0.06735, 0.02011
 0.06515, 0.01980
 0.06297, 0.01948
 0.06081, 0.01915
 0.05866, 0.01883
 0.05653, 0.01850
 0.05442, 0.01817
 0.05233, 0.01783
 0.05026, 0.01749
 0.04820, 0.01715
 0.04615, 0.01680
 0.04413, 0.01645
 0.04212, 0.01609
 0.04012, 0.01573
 0.03815, 0.01536
 0.03618, 0.01499
 0.03424, 0.01461
 0.03231, 0.01423
 0.03039, 0.01383
 0.02849, 0.01343
 0.02660, 0.01303
 0.02473, 0.01261
 0.02287, 0.01220
 0.02103, 0.01178
 0.01920, 0.01133
 0.01739, 0.01087
 0.01559, 0.01038
 0.01380, 0.00986
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 0.00853, 0.00801
 0.00680, 0.00723
 0.00508, 0.00632
 0.00337, 0.00520
 0.00168, 0.00372
 0.00056, 0.00217
 0.00000, 0.00000
 0.00000, 0.00000
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 0.03618,-0.01499
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 0.04012,-0.01573
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 0.05233,-0.01783
 0.05442,-0.01817
 0.05653,-0.01850
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 0.08093,-0.02197
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 0.09767,-0.02405
 0.10014,-0.02434
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 0.10515,-0.02490
 0.10769,-0.02519
 0.11025,-0.02546
 0.11283,-0.02574
 0.11544,-0.02602
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 0.14280,-0.02867
 0.14568,-0.02893
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 0.15743,-0.02994
 0.16044,-0.03019
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 0.16963,-0.03093
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 1.00000, 0.00000