ファイルインデックス名　: File Index Name        : 1261        .A00
翼型整理番号　　　　　　: Airfoil Serial No.     : N01-0096-0
翼型名　　　　　　　　　: Airfoil Name           : N.A.C.A. 4212
翼型ファイル番号　　　　: Airfoil File No.       : 1261
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. : 0.4
算出プログラム番号　　　: Computed Program No.   : ウハク-40C


座標　　　　　　　　　　: Plot Ordinates         :

 X             Y

 1.00013, 0.00125
 0.98702, 0.00441
 0.97409, 0.00747
 0.96135, 0.01044
 0.94879, 0.01332
 0.93640, 0.01611
 0.92419, 0.01882
 0.91215, 0.02145
 0.90027, 0.02401
 0.88856, 0.02649
 0.87701, 0.02890
 0.86562, 0.03123
 0.85438, 0.03351
 0.84330, 0.03571
 0.83237, 0.03786
 0.82158, 0.03994
 0.81095, 0.04197
 0.80045, 0.04394
 0.79009, 0.04585
 0.77988, 0.04771
 0.76979, 0.04952
 0.75985, 0.05128
 0.75003, 0.05299
 0.74034, 0.05466
 0.73078, 0.05627
 0.72134, 0.05784
 0.71203, 0.05937
 0.70283, 0.06086
 0.69375, 0.06230
 0.68479, 0.06370
 0.67595, 0.06507
 0.66722, 0.06639
 0.65859, 0.06768
 0.65008, 0.06893
 0.64167, 0.07015
 0.63337, 0.07133
 0.62517, 0.07248
 0.61708, 0.07359
 0.60908, 0.07467
 0.60119, 0.07572
 0.59339, 0.07674
 0.58568, 0.07773
 0.57807, 0.07869
 0.57056, 0.07962
 0.56313, 0.08052
 0.55579, 0.08139
 0.54855, 0.08224
 0.54139, 0.08306
 0.53431, 0.08386
 0.52732, 0.08463
 0.52041, 0.08537
 0.51358, 0.08609
 0.50683, 0.08679
 0.50017, 0.08746
 0.49358, 0.08811
 0.48706, 0.08874
 0.48062, 0.08934
 0.47426, 0.08993
 0.46797, 0.09049
 0.46175, 0.09103
 0.45560, 0.09155
 0.44953, 0.09206
 0.44352, 0.09254
 0.43758, 0.09300
 0.43171, 0.09344
 0.42590, 0.09387
 0.42016, 0.09428
 0.41448, 0.09467
 0.40886, 0.09504
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 0.39782, 0.09573
 0.39239, 0.09606
 0.38702, 0.09636
 0.38170, 0.09665
 0.37645, 0.09693
 0.37125, 0.09719
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 0.36102, 0.09766
 0.35599, 0.09787
 0.35101, 0.09807
 0.34609, 0.09826
 0.34122, 0.09843
 0.33639, 0.09859
 0.33162, 0.09874
 0.32691, 0.09887
 0.32224, 0.09899
 0.31761, 0.09910
 0.31304, 0.09919
 0.30852, 0.09927
 0.30404, 0.09934
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 0.28658, 0.09951
 0.28233, 0.09952
 0.27812, 0.09952
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 0.26170, 0.09942
 0.25770, 0.09937
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 0.24982, 0.09924
 0.24594, 0.09916
 0.24209, 0.09908
 0.23828, 0.09898
 0.23451, 0.09887
 0.23078, 0.09875
 0.22709, 0.09863
 0.22343, 0.09849
 0.21980, 0.09835
 0.21621, 0.09819
 0.21266, 0.09803
 0.20914, 0.09786
 0.20565, 0.09769
 0.20220, 0.09750
 0.19865, 0.09730
 0.19490, 0.09708
 0.19119, 0.09683
 0.18752, 0.09654
 0.18389, 0.09623
 0.18029, 0.09588
 0.17674, 0.09551
 0.17321, 0.09511
 0.16973, 0.09469
 0.16628, 0.09423
 0.16287, 0.09375
 0.15949, 0.09325
 0.15615, 0.09272
 0.15284, 0.09217
 0.14957, 0.09160
 0.14633, 0.09100
 0.14312, 0.09038
 0.13995, 0.08974
 0.13682, 0.08908
 0.13371, 0.08840
 0.13064, 0.08769
 0.12760, 0.08697
 0.12460, 0.08623
 0.12162, 0.08547
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 0.11577, 0.08389
 0.11289, 0.08308
 0.11005, 0.08225
 0.10723, 0.08140
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 0.10169, 0.07965
 0.09896, 0.07876
 0.09627, 0.07784
 0.09360, 0.07692
 0.09096, 0.07597
 0.08836, 0.07501
 0.08578, 0.07404
 0.08323, 0.07305
 0.08071, 0.07205
 0.07822, 0.07104
 0.07575, 0.07001
 0.07331, 0.06897
 0.07091, 0.06791
 0.06853, 0.06684
 0.06617, 0.06576
 0.06385, 0.06466
 0.06155, 0.06355
 0.05928, 0.06243
 0.05703, 0.06129
 0.05481, 0.06014
 0.05262, 0.05898
 0.05046, 0.05780
 0.04832, 0.05661
 0.04621, 0.05540
 0.04412, 0.05418
 0.04207, 0.05295
 0.04004, 0.05170
 0.03803, 0.05044
 0.03605, 0.04916
 0.03410, 0.04787
 0.03218, 0.04655
 0.03028, 0.04523
 0.02841, 0.04388
 0.02657, 0.04251
 0.02475, 0.04112
 0.02297, 0.03972
 0.02121, 0.03829
 0.01949, 0.03683
 0.01779, 0.03535
 0.01612, 0.03383
 0.01449, 0.03229
 0.01289, 0.03071
 0.01133, 0.02909
 0.00980, 0.02743
 0.00832, 0.02571
 0.00688, 0.02393
 0.00549, 0.02208
 0.00415, 0.02014
 0.00288, 0.01809
 0.00169, 0.01588
 0.00061, 0.01347
-0.00032, 0.01073
-0.00097, 0.00734
-0.00099, 0.00410
 0.00000, 0.00000
 0.00000, 0.00000
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 0.09547,-0.01618
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 0.11881,-0.01576
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