ファイルインデックス名　: File Index Name        : 1124        .A  
翼型整理番号　　　　　　: Airfoil Serial No.     : N04-0029-1
翼型名　　　　　　　　　: Airfoil Name           : N.A.C.A. 64-008
翼型ファイル番号　　　　: Airfoil File No.       : 1124
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, 0.00038
 0.97362, 0.00087
 0.96072, 0.00148
 0.94801, 0.00217
 0.93549, 0.00295
 0.92315, 0.00378
 0.91099, 0.00466
 0.89900, 0.00558
 0.88719, 0.00650
 0.87554, 0.00745
 0.86406, 0.00841
 0.85274, 0.00937
 0.84158, 0.01034
 0.83058, 0.01131
 0.81973, 0.01227
 0.80903, 0.01323
 0.79848, 0.01418
 0.78808, 0.01511
 0.77781, 0.01604
 0.76769, 0.01695
 0.75770, 0.01785
 0.74785, 0.01873
 0.73814, 0.01959
 0.72855, 0.02044
 0.71909, 0.02126
 0.70976, 0.02207
 0.70055, 0.02286
 0.69146, 0.02364
 0.68249, 0.02439
 0.67363, 0.02513
 0.66490, 0.02584
 0.65627, 0.02654
 0.64776, 0.02722
 0.63935, 0.02788
 0.63106, 0.02852
 0.62287, 0.02914
 0.61478, 0.02974
 0.60680, 0.03032
 0.59891, 0.03089
 0.59112, 0.03143
 0.58344, 0.03196
 0.57584, 0.03247
 0.56834, 0.03296
 0.56094, 0.03343
 0.55362, 0.03389
 0.54639, 0.03433
 0.53925, 0.03475
 0.53220, 0.03516
 0.52523, 0.03554
 0.51835, 0.03591
 0.51155, 0.03627
 0.50483, 0.03661
 0.49819, 0.03693
 0.49163, 0.03723
 0.48514, 0.03752
 0.47874, 0.03778
 0.47240, 0.03804
 0.46614, 0.03828
 0.45996, 0.03850
 0.45384, 0.03871
 0.44780, 0.03890
 0.44182, 0.03908
 0.43591, 0.03924
 0.43007, 0.03939
 0.42430, 0.03952
 0.41859, 0.03964
 0.41295, 0.03974
 0.40737, 0.03983
 0.40185, 0.03990
 0.39639, 0.03995
 0.39099, 0.03998
 0.38566, 0.03999
 0.38038, 0.04000
 0.37516, 0.03999
 0.37000, 0.03997
 0.36489, 0.03994
 0.35984, 0.03989
 0.35484, 0.03985
 0.34990, 0.03979
 0.34501, 0.03973
 0.34017, 0.03967
 0.33538, 0.03960
 0.33065, 0.03952
 0.32596, 0.03944
 0.32133, 0.03935
 0.31674, 0.03925
 0.31220, 0.03915
 0.30771, 0.03904
 0.30326, 0.03893
 0.29887, 0.03881
 0.29451, 0.03868
 0.29020, 0.03855
 0.28594, 0.03842
 0.28172, 0.03828
 0.27754, 0.03814
 0.27340, 0.03799
 0.26931, 0.03784
 0.26526, 0.03768
 0.26125, 0.03752
 0.25728, 0.03736
 0.25334, 0.03719
 0.24945, 0.03702
 0.24560, 0.03684
 0.24178, 0.03666
 0.23800, 0.03648
 0.23426, 0.03630
 0.23056, 0.03611
 0.22689, 0.03592
 0.22326, 0.03573
 0.21966, 0.03553
 0.21610, 0.03533
 0.21257, 0.03513
 0.20907, 0.03492
 0.20561, 0.03472
 0.20218, 0.03451
 0.19879, 0.03429
 0.19542, 0.03408
 0.19209, 0.03386
 0.18879, 0.03364
 0.18552, 0.03342
 0.18228, 0.03319
 0.17908, 0.03296
 0.17590, 0.03273
 0.17275, 0.03250
 0.16963, 0.03227
 0.16654, 0.03203
 0.16348, 0.03179
 0.16044, 0.03155
 0.15743, 0.03131
 0.15445, 0.03106
 0.15150, 0.03082
 0.14858, 0.03057
 0.14568, 0.03032
 0.14280, 0.03007
 0.13996, 0.02981
 0.13713, 0.02956
 0.13434, 0.02930
 0.13157, 0.02904
 0.12882, 0.02878
 0.12610, 0.02851
 0.12340, 0.02825
 0.12072, 0.02798
 0.11807, 0.02771
 0.11544, 0.02743
 0.11283, 0.02716
 0.11025, 0.02688
 0.10769, 0.02660
 0.10515, 0.02632
 0.10264, 0.02604
 0.10014, 0.02576
 0.09767, 0.02547
 0.09521, 0.02518
 0.09278, 0.02489
 0.09037, 0.02459
 0.08798, 0.02430
 0.08561, 0.02400
 0.08326, 0.02369
 0.08093, 0.02339
 0.07862, 0.02308
 0.07633, 0.02277
 0.07405, 0.02246
 0.07180, 0.02214
 0.06956, 0.02182
 0.06735, 0.02150
 0.06515, 0.02118
 0.06297, 0.02085
 0.06081, 0.02052
 0.05866, 0.02018
 0.05653, 0.01984
 0.05442, 0.01950
 0.05233, 0.01915
 0.05026, 0.01879
 0.04820, 0.01844
 0.04615, 0.01807
 0.04413, 0.01770
 0.04212, 0.01732
 0.04012, 0.01694
 0.03815, 0.01655
 0.03618, 0.01615
 0.03424, 0.01575
 0.03231, 0.01534
 0.03039, 0.01492
 0.02849, 0.01448
 0.02660, 0.01404
 0.02473, 0.01359
 0.02287, 0.01313
 0.02103, 0.01265
 0.01920, 0.01216
 0.01739, 0.01164
 0.01559, 0.01109
 0.01380, 0.01051
 0.01203, 0.00988
 0.01027, 0.00918
 0.00853, 0.00843
 0.00680, 0.00759
 0.00508, 0.00663
 0.00337, 0.00547
 0.00168, 0.00393
 0.00056, 0.00232
 0.00000, 0.00000
 0.00000, 0.00000
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 0.02849,-0.01448
 0.03039,-0.01492
 0.03231,-0.01534
 0.03424,-0.01575
 0.03618,-0.01615
 0.03815,-0.01655
 0.04012,-0.01694
 0.04212,-0.01732
 0.04413,-0.01770
 0.04615,-0.01807
 0.04820,-0.01844
 0.05026,-0.01879
 0.05233,-0.01915
 0.05442,-0.01950
 0.05653,-0.01984
 0.05866,-0.02018
 0.06081,-0.02052
 0.06297,-0.02085
 0.06515,-0.02118
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 0.07405,-0.02246
 0.07633,-0.02277
 0.07862,-0.02308
 0.08093,-0.02339
 0.08326,-0.02369
 0.08561,-0.02400
 0.08798,-0.02430
 0.09037,-0.02459
 0.09278,-0.02489
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 0.09767,-0.02547
 0.10014,-0.02576
 0.10264,-0.02604
 0.10515,-0.02632
 0.10769,-0.02660
 0.11025,-0.02688
 0.11283,-0.02716
 0.11544,-0.02743
 0.11807,-0.02771
 0.12072,-0.02798
 0.12340,-0.02825
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 0.13157,-0.02904
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 0.13996,-0.02981
 0.14280,-0.03007
 0.14568,-0.03032
 0.14858,-0.03057
 0.15150,-0.03082
 0.15445,-0.03106
 0.15743,-0.03131
 0.16044,-0.03155
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 0.16654,-0.03203
 0.16963,-0.03227
 0.17275,-0.03250
 0.17590,-0.03273
 0.17908,-0.03296
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 0.24945,-0.03702
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 0.26526,-0.03768
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 1.00000, 0.00000