ファイルインデックス名　: File Index Name        : 1159        .A  
翼型整理番号　　　　　　: Airfoil Serial No.     : N04-0064-1
翼型名　　　　　　　　　: Airfoil Name           : N.A.C.A. 65-009
翼型ファイル番号　　　　: Airfoil File No.       : 1159
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, 0.00051
 0.97362, 0.00119
 0.96072, 0.00201
 0.94801, 0.00296
 0.93549, 0.00399
 0.92315, 0.00511
 0.91099, 0.00628
 0.89900, 0.00748
 0.88719, 0.00867
 0.87554, 0.00988
 0.86406, 0.01109
 0.85274, 0.01230
 0.84158, 0.01351
 0.83058, 0.01471
 0.81973, 0.01589
 0.80903, 0.01706
 0.79848, 0.01822
 0.78808, 0.01934
 0.77781, 0.02045
 0.76769, 0.02154
 0.75770, 0.02260
 0.74785, 0.02365
 0.73814, 0.02467
 0.72855, 0.02566
 0.71909, 0.02664
 0.70976, 0.02758
 0.70055, 0.02851
 0.69146, 0.02940
 0.68249, 0.03027
 0.67363, 0.03111
 0.66490, 0.03193
 0.65627, 0.03272
 0.64776, 0.03348
 0.63935, 0.03422
 0.63106, 0.03493
 0.62287, 0.03561
 0.61478, 0.03627
 0.60680, 0.03690
 0.59891, 0.03751
 0.59112, 0.03810
 0.58344, 0.03866
 0.57584, 0.03919
 0.56834, 0.03970
 0.56094, 0.04018
 0.55362, 0.04064
 0.54639, 0.04107
 0.53925, 0.04148
 0.53220, 0.04187
 0.52523, 0.04223
 0.51835, 0.04256
 0.51155, 0.04288
 0.50483, 0.04317
 0.49819, 0.04343
 0.49163, 0.04366
 0.48514, 0.04387
 0.47874, 0.04406
 0.47240, 0.04423
 0.46614, 0.04438
 0.45996, 0.04451
 0.45384, 0.04463
 0.44780, 0.04472
 0.44182, 0.04480
 0.43591, 0.04487
 0.43007, 0.04492
 0.42430, 0.04495
 0.41859, 0.04498
 0.41295, 0.04498
 0.40737, 0.04498
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 0.39099, 0.04491
 0.38566, 0.04486
 0.38038, 0.04481
 0.37516, 0.04475
 0.37000, 0.04468
 0.36489, 0.04460
 0.35984, 0.04451
 0.35484, 0.04441
 0.34990, 0.04431
 0.34501, 0.04420
 0.34017, 0.04408
 0.33538, 0.04396
 0.33065, 0.04383
 0.32596, 0.04370
 0.32133, 0.04356
 0.31674, 0.04341
 0.31220, 0.04326
 0.30771, 0.04310
 0.30326, 0.04294
 0.29887, 0.04278
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 0.29020, 0.04243
 0.28594, 0.04225
 0.28172, 0.04207
 0.27754, 0.04188
 0.27340, 0.04169
 0.26931, 0.04150
 0.26526, 0.04130
 0.26125, 0.04110
 0.25728, 0.04089
 0.25334, 0.04068
 0.24945, 0.04047
 0.24560, 0.04025
 0.24178, 0.04003
 0.23800, 0.03981
 0.23426, 0.03959
 0.23056, 0.03936
 0.22689, 0.03913
 0.22326, 0.03889
 0.21966, 0.03866
 0.21610, 0.03842
 0.21257, 0.03817
 0.20907, 0.03793
 0.20561, 0.03768
 0.20218, 0.03743
 0.19879, 0.03718
 0.19542, 0.03692
 0.19209, 0.03667
 0.18879, 0.03641
 0.18552, 0.03615
 0.18228, 0.03588
 0.17908, 0.03562
 0.17590, 0.03535
 0.17275, 0.03508
 0.16963, 0.03481
 0.16654, 0.03454
 0.16348, 0.03426
 0.16044, 0.03398
 0.15743, 0.03370
 0.15445, 0.03342
 0.15150, 0.03314
 0.14858, 0.03285
 0.14568, 0.03256
 0.14280, 0.03227
 0.13996, 0.03198
 0.13713, 0.03169
 0.13434, 0.03139
 0.13157, 0.03110
 0.12882, 0.03080
 0.12610, 0.03050
 0.12340, 0.03019
 0.12072, 0.02989
 0.11807, 0.02958
 0.11544, 0.02927
 0.11283, 0.02896
 0.11025, 0.02865
 0.10769, 0.02834
 0.10515, 0.02802
 0.10264, 0.02770
 0.10014, 0.02738
 0.09767, 0.02705
 0.09521, 0.02673
 0.09278, 0.02640
 0.09037, 0.02607
 0.08798, 0.02573
 0.08561, 0.02540
 0.08326, 0.02506
 0.08093, 0.02472
 0.07862, 0.02438
 0.07633, 0.02403
 0.07405, 0.02368
 0.07180, 0.02333
 0.06956, 0.02298
 0.06735, 0.02263
 0.06515, 0.02227
 0.06297, 0.02190
 0.06081, 0.02154
 0.05866, 0.02117
 0.05653, 0.02080
 0.05442, 0.02042
 0.05233, 0.02004
 0.05026, 0.01966
 0.04820, 0.01927
 0.04615, 0.01887
 0.04413, 0.01848
 0.04212, 0.01807
 0.04012, 0.01766
 0.03815, 0.01725
 0.03618, 0.01683
 0.03424, 0.01640
 0.03231, 0.01597
 0.03039, 0.01552
 0.02849, 0.01507
 0.02660, 0.01461
 0.02473, 0.01414
 0.02287, 0.01368
 0.02103, 0.01320
 0.01920, 0.01270
 0.01739, 0.01218
 0.01559, 0.01163
 0.01380, 0.01104
 0.01203, 0.01041
 0.01027, 0.00972
 0.00853, 0.00895
 0.00680, 0.00808
 0.00508, 0.00705
 0.00337, 0.00580
 0.00168, 0.00414
 0.00056, 0.00241
 0.00000, 0.00000
 0.00000, 0.00000
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 0.03618,-0.01683
 0.03815,-0.01725
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 0.05442,-0.02042
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 0.10264,-0.02770
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 0.10769,-0.02834
 0.11025,-0.02865
 0.11283,-0.02896
 0.11544,-0.02927
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 0.14568,-0.03256
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 1.00000, 0.00000