ファイルインデックス名　: File Index Name        : 1211        .A00
翼型整理番号　　　　　　: Airfoil Serial No.     : N02-0024-0
翼型名　　　　　　　　　: Airfoil Name           : N.A.C.A. 34012
翼型ファイル番号　　　　: Airfoil File No.       : 1211
翼型情報　　　　　　　　: Airfoil Information    : Computed

算出前縁半径　　　　　　: Computed L.E.R.        : 1.59 %
算出前縁傾斜　　　　　　: Computed Slope of L.E. : 0.379
算出プログラム番号　　　: Computed Program No.   : ウハク-40D


座標　　　　　　　　　　: Plot Ordinates         :

 X             Y

 1.00005, 0.00126
 0.98684, 0.00364
 0.97382, 0.00597
 0.96099, 0.00823
 0.94835, 0.01043
 0.93589, 0.01257
 0.92362, 0.01466
 0.91152, 0.01669
 0.89959, 0.01868
 0.88784, 0.02062
 0.87625, 0.02251
 0.86482, 0.02435
 0.85356, 0.02615
 0.84245, 0.02791
 0.83150, 0.02963
 0.82070, 0.03130
 0.81005, 0.03294
 0.79955, 0.03454
 0.78919, 0.03610
 0.77897, 0.03763
 0.76889, 0.03913
 0.75895, 0.04059
 0.74914, 0.04201
 0.73947, 0.04341
 0.72992, 0.04477
 0.72050, 0.04611
 0.71120, 0.04741
 0.70203, 0.04869
 0.69297, 0.04993
 0.68404, 0.05115
 0.67522, 0.05234
 0.66651, 0.05351
 0.65792, 0.05465
 0.64944, 0.05576
 0.64107, 0.05685
 0.63280, 0.05791
 0.62464, 0.05895
 0.61658, 0.05997
 0.60862, 0.06096
 0.60076, 0.06193
 0.59300, 0.06288
 0.58534, 0.06381
 0.57777, 0.06471
 0.57029, 0.06559
 0.56291, 0.06646
 0.55561, 0.06730
 0.54841, 0.06812
 0.54129, 0.06892
 0.53426, 0.06970
 0.52731, 0.07047
 0.52044, 0.07121
 0.51366, 0.07194
 0.50696, 0.07265
 0.50034, 0.07334
 0.49379, 0.07401
 0.48732, 0.07466
 0.48093, 0.07530
 0.47461, 0.07592
 0.46837, 0.07653
 0.46219, 0.07711
 0.45609, 0.07768
 0.45006, 0.07824
 0.44410, 0.07878
 0.43820, 0.07930
 0.43237, 0.07981
 0.42661, 0.08031
 0.42091, 0.08079
 0.41528, 0.08125
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 0.38803, 0.08337
 0.38276, 0.08375
 0.37754, 0.08412
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 0.36224, 0.08515
 0.35724, 0.08547
 0.35231, 0.08577
 0.34742, 0.08606
 0.34258, 0.08635
 0.33780, 0.08662
 0.33307, 0.08687
 0.32839, 0.08712
 0.32375, 0.08736
 0.31917, 0.08758
 0.31463, 0.08779
 0.31014, 0.08799
 0.30569, 0.08819
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 0.29263, 0.08870
 0.28836, 0.08885
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 0.27992, 0.08911
 0.27575, 0.08923
 0.27160, 0.08933
 0.26749, 0.08943
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 0.25137, 0.08966
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 0.23960, 0.08968
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 0.23190, 0.08961
 0.22810, 0.08956
 0.22433, 0.08948
 0.22058, 0.08939
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 0.21318, 0.08916
 0.20953, 0.08902
 0.20590, 0.08886
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 0.19873, 0.08850
 0.19519, 0.08829
 0.19168, 0.08806
 0.18820, 0.08781
 0.18474, 0.08755
 0.18131, 0.08727
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 0.17120, 0.08632
 0.16788, 0.08597
 0.16459, 0.08560
 0.16133, 0.08521
 0.15809, 0.08480
 0.15489, 0.08438
 0.15171, 0.08394
 0.14855, 0.08348
 0.14543, 0.08300
 0.14233, 0.08251
 0.13926, 0.08200
 0.13621, 0.08147
 0.13319, 0.08092
 0.13020, 0.08036
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 0.12430, 0.07918
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 0.11850, 0.07793
 0.11564, 0.07728
 0.11280, 0.07661
 0.10999, 0.07593
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 0.10445, 0.07452
 0.10172, 0.07378
 0.09902, 0.07303
 0.09634, 0.07227
 0.09369, 0.07149
 0.09106, 0.07069
 0.08846, 0.06987
 0.08588, 0.06904
 0.08333, 0.06820
 0.08080, 0.06733
 0.07830, 0.06646
 0.07583, 0.06556
 0.07338, 0.06465
 0.07095, 0.06372
 0.06855, 0.06278
 0.06618, 0.06182
 0.06383, 0.06085
 0.06151, 0.05985
 0.05921, 0.05885
 0.05694, 0.05782
 0.05469, 0.05678
 0.05247, 0.05572
 0.05028, 0.05465
 0.04811, 0.05356
 0.04596, 0.05245
 0.04384, 0.05132
 0.04175, 0.05018
 0.03968, 0.04901
 0.03764, 0.04783
 0.03563, 0.04663
 0.03364, 0.04541
 0.03168, 0.04417
 0.02975, 0.04290
 0.02784, 0.04162
 0.02597, 0.04031
 0.02412, 0.03897
 0.02230, 0.03761
 0.02051, 0.03622
 0.01875, 0.03480
 0.01703, 0.03335
 0.01533, 0.03187
 0.01367, 0.03034
 0.01205, 0.02877
 0.01046, 0.02716
 0.00892, 0.02548
 0.00742, 0.02375
 0.00597, 0.02193
 0.00458, 0.02003
 0.00326, 0.01801
 0.00201, 0.01584
 0.00087, 0.01345
-0.00012, 0.01072
-0.00083, 0.00735
-0.00091, 0.00412
 0.00000, 0.00000
 0.00000, 0.00000
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