ファイルインデックス名　: File Index Name        : 1186        .A  
翼型整理番号　　　　　　: Airfoil Serial No.     : N04-0091-1
翼型名　　　　　　　　　: Airfoil Name           : N.A.C.A. 66-006
翼型ファイル番号　　　　: Airfoil File No.       : 1186
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, 0.00115
 0.96072, 0.00191
 0.94801, 0.00276
 0.93549, 0.00369
 0.92315, 0.00467
 0.91099, 0.00569
 0.89900, 0.00674
 0.88719, 0.00776
 0.87554, 0.00879
 0.86406, 0.00981
 0.85274, 0.01082
 0.84158, 0.01181
 0.83058, 0.01278
 0.81973, 0.01373
 0.80903, 0.01466
 0.79848, 0.01556
 0.78808, 0.01644
 0.77781, 0.01729
 0.76769, 0.01812
 0.75770, 0.01892
 0.74785, 0.01970
 0.73814, 0.02044
 0.72855, 0.02116
 0.71909, 0.02184
 0.70976, 0.02250
 0.70055, 0.02312
 0.69146, 0.02372
 0.68249, 0.02428
 0.67363, 0.02481
 0.66490, 0.02531
 0.65627, 0.02578
 0.64776, 0.02622
 0.63935, 0.02662
 0.63106, 0.02699
 0.62287, 0.02733
 0.61478, 0.02764
 0.60680, 0.02793
 0.59891, 0.02818
 0.59112, 0.02840
 0.58344, 0.02860
 0.57584, 0.02877
 0.56834, 0.02893
 0.56094, 0.02907
 0.55362, 0.02919
 0.54639, 0.02931
 0.53925, 0.02942
 0.53220, 0.02952
 0.52523, 0.02961
 0.51835, 0.02968
 0.51155, 0.02975
 0.50483, 0.02981
 0.49819, 0.02986
 0.49163, 0.02991
 0.48514, 0.02994
 0.47874, 0.02997
 0.47240, 0.02999
 0.46614, 0.03000
 0.45996, 0.03001
 0.45384, 0.03000
 0.44780, 0.03000
 0.44182, 0.02998
 0.43591, 0.02996
 0.43007, 0.02994
 0.42430, 0.02991
 0.41859, 0.02987
 0.41295, 0.02983
 0.40737, 0.02978
 0.40185, 0.02973
 0.39639, 0.02967
 0.39099, 0.02961
 0.38566, 0.02955
 0.38038, 0.02948
 0.37516, 0.02941
 0.37000, 0.02933
 0.36489, 0.02925
 0.35984, 0.02917
 0.35484, 0.02908
 0.34990, 0.02899
 0.34501, 0.02889
 0.34017, 0.02880
 0.33538, 0.02870
 0.33065, 0.02859
 0.32596, 0.02848
 0.32133, 0.02838
 0.31674, 0.02826
 0.31220, 0.02815
 0.30771, 0.02803
 0.30326, 0.02791
 0.29887, 0.02779
 0.29451, 0.02766
 0.29020, 0.02754
 0.28594, 0.02741
 0.28172, 0.02728
 0.27754, 0.02714
 0.27340, 0.02701
 0.26931, 0.02687
 0.26526, 0.02673
 0.26125, 0.02659
 0.25728, 0.02645
 0.25334, 0.02631
 0.24945, 0.02616
 0.24560, 0.02601
 0.24178, 0.02586
 0.23800, 0.02571
 0.23426, 0.02556
 0.23056, 0.02540
 0.22689, 0.02525
 0.22326, 0.02509
 0.21966, 0.02493
 0.21610, 0.02477
 0.21257, 0.02461
 0.20907, 0.02445
 0.20561, 0.02428
 0.20218, 0.02412
 0.19879, 0.02395
 0.19542, 0.02378
 0.19209, 0.02361
 0.18879, 0.02344
 0.18552, 0.02327
 0.18228, 0.02309
 0.17908, 0.02292
 0.17590, 0.02274
 0.17275, 0.02256
 0.16963, 0.02238
 0.16654, 0.02220
 0.16348, 0.02202
 0.16044, 0.02184
 0.15743, 0.02166
 0.15445, 0.02147
 0.15150, 0.02129
 0.14858, 0.02110
 0.14568, 0.02091
 0.14280, 0.02072
 0.13996, 0.02053
 0.13713, 0.02034
 0.13434, 0.02015
 0.13157, 0.01995
 0.12882, 0.01976
 0.12610, 0.01956
 0.12340, 0.01936
 0.12072, 0.01916
 0.11807, 0.01896
 0.11544, 0.01876
 0.11283, 0.01856
 0.11025, 0.01836
 0.10769, 0.01815
 0.10515, 0.01795
 0.10264, 0.01774
 0.10014, 0.01753
 0.09767, 0.01732
 0.09521, 0.01711
 0.09278, 0.01690
 0.09037, 0.01668
 0.08798, 0.01647
 0.08561, 0.01625
 0.08326, 0.01603
 0.08093, 0.01581
 0.07862, 0.01559
 0.07633, 0.01537
 0.07405, 0.01515
 0.07180, 0.01492
 0.06956, 0.01470
 0.06735, 0.01447
 0.06515, 0.01425
 0.06297, 0.01402
 0.06081, 0.01379
 0.05866, 0.01355
 0.05653, 0.01332
 0.05442, 0.01308
 0.05233, 0.01284
 0.05026, 0.01260
 0.04820, 0.01236
 0.04615, 0.01211
 0.04413, 0.01186
 0.04212, 0.01160
 0.04012, 0.01134
 0.03815, 0.01108
 0.03618, 0.01082
 0.03424, 0.01055
 0.03231, 0.01028
 0.03039, 0.01000
 0.02849, 0.00972
 0.02660, 0.00943
 0.02473, 0.00914
 0.02287, 0.00886
 0.02103, 0.00856
 0.01920, 0.00826
 0.01739, 0.00794
 0.01559, 0.00759
 0.01380, 0.00722
 0.01203, 0.00682
 0.01027, 0.00637
 0.00853, 0.00587
 0.00680, 0.00530
 0.00508, 0.00464
 0.00337, 0.00384
 0.00168, 0.00276
 0.00056, 0.00163
 0.00000, 0.00000
 0.00000, 0.00000
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 0.00168,-0.00276
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 0.01559,-0.00759
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 0.03039,-0.01000
 0.03231,-0.01028
 0.03424,-0.01055
 0.03618,-0.01082
 0.03815,-0.01108
 0.04012,-0.01134
 0.04212,-0.01160
 0.04413,-0.01186
 0.04615,-0.01211
 0.04820,-0.01236
 0.05026,-0.01260
 0.05233,-0.01284
 0.05442,-0.01308
 0.05653,-0.01332
 0.05866,-0.01355
 0.06081,-0.01379
 0.06297,-0.01402
 0.06515,-0.01425
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 0.06956,-0.01470
 0.07180,-0.01492
 0.07405,-0.01515
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 0.07862,-0.01559
 0.08093,-0.01581
 0.08326,-0.01603
 0.08561,-0.01625
 0.08798,-0.01647
 0.09037,-0.01668
 0.09278,-0.01690
 0.09521,-0.01711
 0.09767,-0.01732
 0.10014,-0.01753
 0.10264,-0.01774
 0.10515,-0.01795
 0.10769,-0.01815
 0.11025,-0.01836
 0.11283,-0.01856
 0.11544,-0.01876
 0.11807,-0.01896
 0.12072,-0.01916
 0.12340,-0.01936
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 0.12882,-0.01976
 0.13157,-0.01995
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 0.13713,-0.02034
 0.13996,-0.02053
 0.14280,-0.02072
 0.14568,-0.02091
 0.14858,-0.02110
 0.15150,-0.02129
 0.15445,-0.02147
 0.15743,-0.02166
 0.16044,-0.02184
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 0.16654,-0.02220
 0.16963,-0.02238
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 0.17590,-0.02274
 0.17908,-0.02292
 0.18228,-0.02309
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 1.00000, 0.00000