ファイルインデックス名　: File Index Name        : 1139        .A  
翼型整理番号　　　　　　: Airfoil Serial No.     : N04-0044-1
翼型名　　　　　　　　　: Airfoil Name           : N.A.C.A. 64-208
翼型ファイル番号　　　　: Airfoil File No.       : 1139
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.   : VB6B05-A01C


座標　　　　　　　　　　: Plot Ordinates         :

 X             Y

 1.00000, 0.00000
 0.98659, 0.00138
 0.97339, 0.00276
 0.96037, 0.00413
 0.94755, 0.00549
 0.93491, 0.00685
 0.92246, 0.00821
 0.91019, 0.00956
 0.89808, 0.01091
 0.88616, 0.01225
 0.87440, 0.01359
 0.86280, 0.01491
 0.85137, 0.01622
 0.84011, 0.01750
 0.82900, 0.01876
 0.81805, 0.02000
 0.80724, 0.02122
 0.79659, 0.02241
 0.78609, 0.02359
 0.77573, 0.02473
 0.76551, 0.02585
 0.75543, 0.02695
 0.74549, 0.02801
 0.73570, 0.02904
 0.72602, 0.03004
 0.71648, 0.03101
 0.70707, 0.03196
 0.69778, 0.03288
 0.68862, 0.03377
 0.67957, 0.03464
 0.67064, 0.03547
 0.66184, 0.03629
 0.65315, 0.03707
 0.64457, 0.03783
 0.63610, 0.03857
 0.62775, 0.03929
 0.61950, 0.03998
 0.61136, 0.04064
 0.60332, 0.04127
 0.59538, 0.04189
 0.58754, 0.04247
 0.57982, 0.04305
 0.57217, 0.04359
 0.56463, 0.04411
 0.55718, 0.04460
 0.54982, 0.04508
 0.54256, 0.04553
 0.53538, 0.04597
 0.52829, 0.04639
 0.52129, 0.04677
 0.51438, 0.04715
 0.50755, 0.04750
 0.50080, 0.04784
 0.49414, 0.04815
 0.48755, 0.04844
 0.48104, 0.04871
 0.47462, 0.04896
 0.46826, 0.04919
 0.46198, 0.04941
 0.45578, 0.04960
 0.44965, 0.04979
 0.44359, 0.04995
 0.43760, 0.05010
 0.43168, 0.05022
 0.42583, 0.05033
 0.42005, 0.05043
 0.41434, 0.05051
 0.40869, 0.05057
 0.40311, 0.05061
 0.39759, 0.05064
 0.39213, 0.05063
 0.38673, 0.05061
 0.38140, 0.05058
 0.37613, 0.05052
 0.37091, 0.05047
 0.36576, 0.05039
 0.36065, 0.05031
 0.35561, 0.05021
 0.35062, 0.05011
 0.34569, 0.05001
 0.34081, 0.04990
 0.33598, 0.04977
 0.33120, 0.04964
 0.32648, 0.04951
 0.32180, 0.04936
 0.31719, 0.04921
 0.31261, 0.04906
 0.30808, 0.04890
 0.30361, 0.04872
 0.29917, 0.04855
 0.29480, 0.04836
 0.29045, 0.04818
 0.28616, 0.04798
 0.28192, 0.04778
 0.27771, 0.04757
 0.27355, 0.04736
 0.26943, 0.04714
 0.26536, 0.04692
 0.26133, 0.04669
 0.25734, 0.04646
 0.25339, 0.04623
 0.24947, 0.04599
 0.24560, 0.04575
 0.24177, 0.04549
 0.23797, 0.04524
 0.23421, 0.04500
 0.23049, 0.04474
 0.22682, 0.04448
 0.22317, 0.04421
 0.21956, 0.04395
 0.21598, 0.04367
 0.21245, 0.04340
 0.20894, 0.04312
 0.20546, 0.04284
 0.20203, 0.04256
 0.19862, 0.04227
 0.19526, 0.04198
 0.19191, 0.04169
 0.18861, 0.04139
 0.18533, 0.04109
 0.18209, 0.04079
 0.17887, 0.04049
 0.17570, 0.04018
 0.17254, 0.03988
 0.16942, 0.03956
 0.16633, 0.03925
 0.16326, 0.03893
 0.16023, 0.03862
 0.15722, 0.03829
 0.15423, 0.03797
 0.15128, 0.03764
 0.14836, 0.03732
 0.14547, 0.03699
 0.14259, 0.03666
 0.13974, 0.03632
 0.13693, 0.03598
 0.13413, 0.03565
 0.13137, 0.03531
 0.12863, 0.03496
 0.12591, 0.03461
 0.12321, 0.03427
 0.12054, 0.03391
 0.11789, 0.03356
 0.11527, 0.03321
 0.11267, 0.03285
 0.11009, 0.03249
 0.10755, 0.03213
 0.10502, 0.03176
 0.10251, 0.03140
 0.10003, 0.03103
 0.09756, 0.03066
 0.09512, 0.03029
 0.09269, 0.02991
 0.09029, 0.02953
 0.08792, 0.02915
 0.08556, 0.02877
 0.08322, 0.02838
 0.08090, 0.02799
 0.07861, 0.02760
 0.07633, 0.02720
 0.07407, 0.02681
 0.07183, 0.02640
 0.06961, 0.02600
 0.06741, 0.02559
 0.06523, 0.02518
 0.06306, 0.02477
 0.06092, 0.02435
 0.05880, 0.02393
 0.05668, 0.02350
 0.05459, 0.02306
 0.05252, 0.02262
 0.05046, 0.02218
 0.04843, 0.02174
 0.04641, 0.02129
 0.04440, 0.02083
 0.04242, 0.02036
 0.04045, 0.01988
 0.03849, 0.01941
 0.03656, 0.01892
 0.03463, 0.01843
 0.03273, 0.01793
 0.03084, 0.01741
 0.02897, 0.01689
 0.02711, 0.01636
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 0.02345, 0.01526
 0.02163, 0.01470
 0.01984, 0.01412
 0.01806, 0.01352
 0.01630, 0.01289
 0.01456, 0.01223
 0.01283, 0.01154
 0.01112, 0.01079
 0.00943, 0.00999
 0.00776, 0.00912
 0.00611, 0.00816
 0.00448, 0.00708
 0.00288, 0.00580
 0.00133, 0.00414
 0.00036, 0.00241
 0.00000, 0.00000
 0.00000, 0.00000
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 0.03147,-0.01278
 0.03341,-0.01309
 0.03537,-0.01340
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 0.03933,-0.01400
 0.04132,-0.01429
 0.04335,-0.01458
 0.04538,-0.01486
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 0.05367,-0.01591
 0.05578,-0.01617
 0.05791,-0.01642
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 0.06223,-0.01691
 0.06441,-0.01715
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 0.07332,-0.01807
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 0.08253,-0.01896
 0.08487,-0.01918
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 0.08963,-0.01960
 0.09204,-0.01981
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 0.09691,-0.02022
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 0.10948,-0.02122
 0.11205,-0.02142
 0.11465,-0.02161
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 0.11992,-0.02198
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 0.13909,-0.02324
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 0.14479,-0.02360
 0.14768,-0.02376
 0.15059,-0.02393
 0.15353,-0.02410
 0.15649,-0.02427
 0.15949,-0.02444
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 0.17174,-0.02508
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 1.00000, 0.00000