ファイルインデックス名　: File Index Name        : 1023        .A00
翼型整理番号　　　　　　: Airfoil Serial No.     : N01-0023-0
翼型名　　　　　　　　　: Airfoil Name           : N.A.C.A. 2406
翼型ファイル番号　　　　: Airfoil File No.       : 1023
翼型情報　　　　　　　　: Airfoil Information    : Computed

算出前縁半径　　　　　　: Computed L.E.R.        : 0.4 %
算出前縁傾斜　　　　　　: Computed Slope of L.E. : 0.1
算出プログラム番号　　　: Computed Program No.   : ウハク-40B


座標　　　　　　　　　　: Plot Ordinates         :

 X             Y

 1.00004, 0.00063
 0.98681, 0.00243
 0.97378, 0.00417
 0.96093, 0.00585
 0.94827, 0.00747
 0.93579, 0.00904
 0.92349, 0.01056
 0.91136, 0.01203
 0.89941, 0.01346
 0.88762, 0.01483
 0.87600, 0.01616
 0.86454, 0.01745
 0.85325, 0.01870
 0.84211, 0.01991
 0.83112, 0.02108
 0.82029, 0.02221
 0.80960, 0.02330
 0.79906, 0.02437
 0.78867, 0.02539
 0.77841, 0.02639
 0.76830, 0.02735
 0.75832, 0.02828
 0.74847, 0.02918
 0.73875, 0.03005
 0.72917, 0.03089
 0.71971, 0.03171
 0.71037, 0.03250
 0.70116, 0.03326
 0.69206, 0.03400
 0.68309, 0.03472
 0.67423, 0.03541
 0.66548, 0.03608
 0.65685, 0.03672
 0.64833, 0.03735
 0.63992, 0.03795
 0.63161, 0.03853
 0.62341, 0.03909
 0.61531, 0.03963
 0.60731, 0.04015
 0.59942, 0.04066
 0.59162, 0.04114
 0.58391, 0.04161
 0.57631, 0.04206
 0.56879, 0.04250
 0.56137, 0.04291
 0.55404, 0.04331
 0.54680, 0.04370
 0.53964, 0.04407
 0.53257, 0.04443
 0.52559, 0.04477
 0.51869, 0.04509
 0.51187, 0.04541
 0.50514, 0.04570
 0.49848, 0.04599
 0.49190, 0.04626
 0.48540, 0.04652
 0.47897, 0.04677
 0.47262, 0.04701
 0.46634, 0.04723
 0.46014, 0.04744
 0.45401, 0.04764
 0.44794, 0.04783
 0.44195, 0.04801
 0.43603, 0.04818
 0.43017, 0.04834
 0.42438, 0.04849
 0.41865, 0.04862
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 0.40185, 0.04898
 0.39636, 0.04908
 0.39093, 0.04917
 0.38555, 0.04924
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 0.34460, 0.04941
 0.33972, 0.04938
 0.33490, 0.04935
 0.33013, 0.04930
 0.32541, 0.04924
 0.32074, 0.04918
 0.31612, 0.04910
 0.31154, 0.04902
 0.30702, 0.04893
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 0.29372, 0.04860
 0.28938, 0.04848
 0.28508, 0.04835
 0.28083, 0.04821
 0.27662, 0.04806
 0.27246, 0.04791
 0.26833, 0.04775
 0.26425, 0.04758
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 0.25621, 0.04723
 0.25225, 0.04704
 0.24833, 0.04685
 0.24445, 0.04665
 0.24061, 0.04644
 0.23681, 0.04623
 0.23304, 0.04601
 0.22931, 0.04579
 0.22562, 0.04556
 0.22196, 0.04533
 0.21834, 0.04509
 0.21476, 0.04485
 0.21121, 0.04460
 0.20769, 0.04434
 0.20421, 0.04409
 0.20076, 0.04382
 0.19735, 0.04356
 0.19397, 0.04328
 0.19062, 0.04301
 0.18730, 0.04272
 0.18401, 0.04244
 0.18076, 0.04215
 0.17753, 0.04186
 0.17434, 0.04156
 0.17117, 0.04126
 0.16804, 0.04095
 0.16494, 0.04064
 0.16186, 0.04032
 0.15881, 0.04001
 0.15579, 0.03969
 0.15280, 0.03936
 0.14984, 0.03903
 0.14690, 0.03870
 0.14400, 0.03836
 0.14111, 0.03802
 0.13826, 0.03768
 0.13543, 0.03733
 0.13262, 0.03698
 0.12985, 0.03663
 0.12709, 0.03627
 0.12436, 0.03591
 0.12166, 0.03555
 0.11898, 0.03518
 0.11633, 0.03481
 0.11369, 0.03444
 0.11109, 0.03406
 0.10850, 0.03368
 0.10594, 0.03329
 0.10340, 0.03291
 0.10088, 0.03251
 0.09839, 0.03212
 0.09592, 0.03172
 0.09347, 0.03132
 0.09104, 0.03092
 0.08863, 0.03051
 0.08624, 0.03010
 0.08388, 0.02968
 0.08153, 0.02926
 0.07921, 0.02884
 0.07690, 0.02841
 0.07462, 0.02798
 0.07236, 0.02755
 0.07011, 0.02711
 0.06789, 0.02666
 0.06568, 0.02621
 0.06349, 0.02576
 0.06133, 0.02531
 0.05918, 0.02484
 0.05705, 0.02438
 0.05493, 0.02390
 0.05284, 0.02343
 0.05076, 0.02294
 0.04870, 0.02245
 0.04666, 0.02196
 0.04464, 0.02146
 0.04264, 0.02095
 0.04065, 0.02043
 0.03868, 0.01991
 0.03672, 0.01937
 0.03479, 0.01883
 0.03287, 0.01828
 0.03096, 0.01772
 0.02908, 0.01715
 0.02721, 0.01656
 0.02535, 0.01596
 0.02352, 0.01535
 0.02170, 0.01472
 0.01989, 0.01407
 0.01811, 0.01340
 0.01634, 0.01271
 0.01459, 0.01199
 0.01285, 0.01123
 0.01113, 0.01044
 0.00944, 0.00960
 0.00776, 0.00870
 0.00610, 0.00772
 0.00447, 0.00663
 0.00287, 0.00536
 0.00132, 0.00374
 0.00035, 0.00213
 0.00000, 0.00000
 0.00000, 0.00000
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