ファイルインデックス名　: File Index Name        : 1127        .A  
翼型整理番号　　　　　　: Airfoil Serial No.     : N04-0032-1
翼型名　　　　　　　　　: Airfoil Name           : N.A.C.A. 64-010
翼型ファイル番号　　　　: Airfoil File No.       : 1127
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, 0.00044
 0.97362, 0.00104
 0.96072, 0.00177
 0.94801, 0.00262
 0.93549, 0.00357
 0.92315, 0.00459
 0.91099, 0.00568
 0.89900, 0.00680
 0.88719, 0.00794
 0.87554, 0.00910
 0.86406, 0.01028
 0.85274, 0.01147
 0.84158, 0.01266
 0.83058, 0.01385
 0.81973, 0.01503
 0.80903, 0.01622
 0.79848, 0.01739
 0.78808, 0.01855
 0.77781, 0.01970
 0.76769, 0.02083
 0.75770, 0.02195
 0.74785, 0.02305
 0.73814, 0.02412
 0.72855, 0.02518
 0.71909, 0.02621
 0.70976, 0.02722
 0.70055, 0.02821
 0.69146, 0.02918
 0.68249, 0.03012
 0.67363, 0.03105
 0.66490, 0.03194
 0.65627, 0.03282
 0.64776, 0.03367
 0.63935, 0.03450
 0.63106, 0.03531
 0.62287, 0.03609
 0.61478, 0.03685
 0.60680, 0.03758
 0.59891, 0.03830
 0.59112, 0.03899
 0.58344, 0.03965
 0.57584, 0.04030
 0.56834, 0.04092
 0.56094, 0.04152
 0.55362, 0.04210
 0.54639, 0.04266
 0.53925, 0.04319
 0.53220, 0.04371
 0.52523, 0.04420
 0.51835, 0.04468
 0.51155, 0.04513
 0.50483, 0.04556
 0.49819, 0.04597
 0.49163, 0.04636
 0.48514, 0.04673
 0.47874, 0.04707
 0.47240, 0.04740
 0.46614, 0.04771
 0.45996, 0.04800
 0.45384, 0.04827
 0.44780, 0.04852
 0.44182, 0.04875
 0.43591, 0.04897
 0.43007, 0.04916
 0.42430, 0.04934
 0.41859, 0.04950
 0.41295, 0.04963
 0.40737, 0.04975
 0.40185, 0.04985
 0.39639, 0.04992
 0.39099, 0.04997
 0.38566, 0.05000
 0.38038, 0.05001
 0.37516, 0.05001
 0.37000, 0.04999
 0.36489, 0.04996
 0.35984, 0.04992
 0.35484, 0.04986
 0.34990, 0.04980
 0.34501, 0.04973
 0.34017, 0.04966
 0.33538, 0.04957
 0.33065, 0.04948
 0.32596, 0.04938
 0.32133, 0.04927
 0.31674, 0.04915
 0.31220, 0.04902
 0.30771, 0.04889
 0.30326, 0.04875
 0.29887, 0.04860
 0.29451, 0.04845
 0.29020, 0.04829
 0.28594, 0.04812
 0.28172, 0.04795
 0.27754, 0.04777
 0.27340, 0.04758
 0.26931, 0.04739
 0.26526, 0.04719
 0.26125, 0.04699
 0.25728, 0.04679
 0.25334, 0.04657
 0.24945, 0.04636
 0.24560, 0.04614
 0.24178, 0.04592
 0.23800, 0.04569
 0.23426, 0.04545
 0.23056, 0.04522
 0.22689, 0.04498
 0.22326, 0.04473
 0.21966, 0.04448
 0.21610, 0.04423
 0.21257, 0.04398
 0.20907, 0.04372
 0.20561, 0.04346
 0.20218, 0.04319
 0.19879, 0.04292
 0.19542, 0.04265
 0.19209, 0.04238
 0.18879, 0.04211
 0.18552, 0.04183
 0.18228, 0.04154
 0.17908, 0.04126
 0.17590, 0.04097
 0.17275, 0.04068
 0.16963, 0.04039
 0.16654, 0.04010
 0.16348, 0.03980
 0.16044, 0.03950
 0.15743, 0.03919
 0.15445, 0.03889
 0.15150, 0.03858
 0.14858, 0.03827
 0.14568, 0.03795
 0.14280, 0.03764
 0.13996, 0.03732
 0.13713, 0.03700
 0.13434, 0.03667
 0.13157, 0.03635
 0.12882, 0.03602
 0.12610, 0.03569
 0.12340, 0.03535
 0.12072, 0.03502
 0.11807, 0.03468
 0.11544, 0.03434
 0.11283, 0.03399
 0.11025, 0.03364
 0.10769, 0.03330
 0.10515, 0.03294
 0.10264, 0.03259
 0.10014, 0.03223
 0.09767, 0.03187
 0.09521, 0.03151
 0.09278, 0.03114
 0.09037, 0.03077
 0.08798, 0.03040
 0.08561, 0.03002
 0.08326, 0.02964
 0.08093, 0.02926
 0.07862, 0.02888
 0.07633, 0.02849
 0.07405, 0.02810
 0.07180, 0.02770
 0.06956, 0.02730
 0.06735, 0.02689
 0.06515, 0.02649
 0.06297, 0.02607
 0.06081, 0.02565
 0.05866, 0.02523
 0.05653, 0.02480
 0.05442, 0.02437
 0.05233, 0.02393
 0.05026, 0.02349
 0.04820, 0.02303
 0.04615, 0.02257
 0.04413, 0.02211
 0.04212, 0.02163
 0.04012, 0.02115
 0.03815, 0.02066
 0.03618, 0.02016
 0.03424, 0.01965
 0.03231, 0.01913
 0.03039, 0.01860
 0.02849, 0.01806
 0.02660, 0.01750
 0.02473, 0.01693
 0.02287, 0.01635
 0.02103, 0.01576
 0.01920, 0.01514
 0.01739, 0.01449
 0.01559, 0.01380
 0.01380, 0.01307
 0.01203, 0.01228
 0.01027, 0.01143
 0.00853, 0.01049
 0.00680, 0.00945
 0.00508, 0.00826
 0.00337, 0.00682
 0.00168, 0.00490
 0.00056, 0.00289
 0.00000, 0.00000
 0.00000, 0.00000
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 0.03618,-0.02016
 0.03815,-0.02066
 0.04012,-0.02115
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 0.05442,-0.02437
 0.05653,-0.02480
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 0.08093,-0.02926
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 0.08561,-0.03002
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 0.09767,-0.03187
 0.10014,-0.03223
 0.10264,-0.03259
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 0.10769,-0.03330
 0.11025,-0.03364
 0.11283,-0.03399
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 0.14568,-0.03795
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 0.16654,-0.04010
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 1.00000, 0.00000