ファイルインデックス名　: File Index Name        : 1024        .A00
翼型整理番号　　　　　　: Airfoil Serial No.     : N01-0024-0
翼型名　　　　　　　　　: Airfoil Name           : N.A.C.A. 2408
翼型ファイル番号　　　　: Airfoil File No.       : 1024
翼型情報　　　　　　　　: Airfoil Information    : Computed

算出前縁半径　　　　　　: Computed L.E.R.        : 0.71 %
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

 1.00006, 0.00084
 0.98685, 0.00294
 0.97383, 0.00498
 0.96100, 0.00695
 0.94835, 0.00886
 0.93589, 0.01070
 0.92360, 0.01249
 0.91148, 0.01421
 0.89954, 0.01589
 0.88776, 0.01751
 0.87615, 0.01907
 0.86471, 0.02059
 0.85342, 0.02206
 0.84228, 0.02349
 0.83130, 0.02487
 0.82048, 0.02621
 0.80979, 0.02750
 0.79926, 0.02876
 0.78887, 0.02998
 0.77861, 0.03116
 0.76850, 0.03230
 0.75852, 0.03341
 0.74867, 0.03448
 0.73896, 0.03552
 0.72937, 0.03652
 0.71991, 0.03750
 0.71057, 0.03844
 0.70136, 0.03936
 0.69226, 0.04024
 0.68329, 0.04110
 0.67443, 0.04193
 0.66568, 0.04273
 0.65705, 0.04351
 0.64852, 0.04426
 0.64010, 0.04499
 0.63179, 0.04569
 0.62359, 0.04637
 0.61549, 0.04703
 0.60749, 0.04766
 0.59958, 0.04828
 0.59178, 0.04887
 0.58407, 0.04944
 0.57646, 0.04999
 0.56894, 0.05052
 0.56152, 0.05103
 0.55418, 0.05152
 0.54693, 0.05200
 0.53977, 0.05245
 0.53270, 0.05289
 0.52571, 0.05331
 0.51880, 0.05372
 0.51198, 0.05410
 0.50524, 0.05448
 0.49858, 0.05483
 0.49199, 0.05517
 0.48548, 0.05550
 0.47905, 0.05581
 0.47270, 0.05611
 0.46641, 0.05639
 0.46020, 0.05666
 0.45406, 0.05691
 0.44799, 0.05715
 0.44199, 0.05738
 0.43606, 0.05760
 0.43020, 0.05780
 0.42440, 0.05799
 0.41867, 0.05817
 0.41300, 0.05834
 0.40740, 0.05850
 0.40186, 0.05864
 0.39636, 0.05877
 0.39091, 0.05889
 0.38552, 0.05900
 0.38019, 0.05909
 0.37492, 0.05916
 0.36970, 0.05922
 0.36454, 0.05927
 0.35944, 0.05931
 0.35439, 0.05933
 0.34940, 0.05934
 0.34446, 0.05934
 0.33957, 0.05933
 0.33474, 0.05930
 0.32996, 0.05927
 0.32522, 0.05922
 0.32054, 0.05916
 0.31591, 0.05909
 0.31132, 0.05902
 0.30679, 0.05893
 0.30230, 0.05883
 0.29785, 0.05872
 0.29346, 0.05860
 0.28911, 0.05848
 0.28480, 0.05834
 0.28054, 0.05819
 0.27632, 0.05804
 0.27214, 0.05788
 0.26801, 0.05771
 0.26392, 0.05753
 0.25987, 0.05734
 0.25586, 0.05715
 0.25189, 0.05695
 0.24796, 0.05674
 0.24407, 0.05652
 0.24022, 0.05630
 0.23641, 0.05607
 0.23263, 0.05583
 0.22890, 0.05558
 0.22520, 0.05533
 0.22153, 0.05507
 0.21791, 0.05481
 0.21431, 0.05454
 0.21076, 0.05426
 0.20723, 0.05398
 0.20374, 0.05369
 0.20029, 0.05339
 0.19687, 0.05309
 0.19348, 0.05279
 0.19012, 0.05248
 0.18680, 0.05216
 0.18351, 0.05184
 0.18025, 0.05151
 0.17702, 0.05117
 0.17382, 0.05084
 0.17065, 0.05049
 0.16751, 0.05014
 0.16440, 0.04979
 0.16132, 0.04943
 0.15827, 0.04907
 0.15525, 0.04870
 0.15225, 0.04833
 0.14929, 0.04795
 0.14635, 0.04757
 0.14343, 0.04718
 0.14055, 0.04679
 0.13769, 0.04639
 0.13486, 0.04599
 0.13205, 0.04558
 0.12927, 0.04517
 0.12652, 0.04476
 0.12379, 0.04434
 0.12108, 0.04392
 0.11840, 0.04349
 0.11574, 0.04306
 0.11311, 0.04262
 0.11050, 0.04218
 0.10792, 0.04173
 0.10535, 0.04128
 0.10282, 0.04083
 0.10030, 0.04037
 0.09781, 0.03991
 0.09533, 0.03944
 0.09288, 0.03897
 0.09046, 0.03849
 0.08805, 0.03801
 0.08566, 0.03752
 0.08330, 0.03703
 0.08096, 0.03653
 0.07864, 0.03603
 0.07633, 0.03552
 0.07405, 0.03501
 0.07179, 0.03449
 0.06955, 0.03396
 0.06733, 0.03343
 0.06512, 0.03290
 0.06294, 0.03236
 0.06078, 0.03181
 0.05863, 0.03125
 0.05651, 0.03069
 0.05440, 0.03012
 0.05231, 0.02955
 0.05024, 0.02896
 0.04819, 0.02837
 0.04615, 0.02777
 0.04414, 0.02716
 0.04214, 0.02654
 0.04016, 0.02591
 0.03819, 0.02527
 0.03625, 0.02462
 0.03432, 0.02396
 0.03241, 0.02328
 0.03051, 0.02259
 0.02864, 0.02189
 0.02678, 0.02117
 0.02494, 0.02043
 0.02311, 0.01967
 0.02130, 0.01888
 0.01951, 0.01808
 0.01774, 0.01724
 0.01599, 0.01638
 0.01425, 0.01547
 0.01253, 0.01453
 0.01084, 0.01353
 0.00916, 0.01246
 0.00750, 0.01132
 0.00587, 0.01007
 0.00427, 0.00867
 0.00271, 0.00703
 0.00121, 0.00493
 0.00028, 0.00282
 0.00000, 0.00000
 0.00000, 0.00000
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 0.04408,-0.01793
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 0.08792,-0.02174
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 0.11259,-0.02272
 0.11517,-0.02280
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