ファイルインデックス名　: File Index Name        : 1149        .A  
翼型整理番号　　　　　　: Airfoil Serial No.     : N04-0054-1
翼型名　　　　　　　　　: Airfoil Name           : N.A.C.A. 64A410
翼型ファイル番号　　　　: Airfoil File No.       : 1149
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

 0.99996, 0.00022
 0.98613, 0.00301
 0.97251, 0.00578
 0.95908, 0.00853
 0.94585, 0.01124
 0.93281, 0.01391
 0.91997, 0.01653
 0.90731, 0.01911
 0.89484, 0.02163
 0.88256, 0.02407
 0.87045, 0.02647
 0.85852, 0.02881
 0.84676, 0.03111
 0.83516, 0.03337
 0.82374, 0.03555
 0.81249, 0.03766
 0.80140, 0.03969
 0.79049, 0.04156
 0.77974, 0.04334
 0.76915, 0.04504
 0.75871, 0.04667
 0.74843, 0.04823
 0.73829, 0.04973
 0.72830, 0.05117
 0.71844, 0.05255
 0.70873, 0.05388
 0.69915, 0.05515
 0.68971, 0.05638
 0.68039, 0.05755
 0.67120, 0.05868
 0.66214, 0.05976
 0.65321, 0.06079
 0.64439, 0.06178
 0.63570, 0.06273
 0.62711, 0.06363
 0.61866, 0.06449
 0.61031, 0.06532
 0.60207, 0.06610
 0.59394, 0.06685
 0.58592, 0.06756
 0.57800, 0.06824
 0.57019, 0.06888
 0.56248, 0.06949
 0.55487, 0.07006
 0.54736, 0.07061
 0.53994, 0.07111
 0.53262, 0.07160
 0.52539, 0.07205
 0.51826, 0.07247
 0.51122, 0.07286
 0.50427, 0.07322
 0.49740, 0.07356
 0.49062, 0.07387
 0.48393, 0.07415
 0.47732, 0.07441
 0.47079, 0.07464
 0.46435, 0.07483
 0.45797, 0.07501
 0.45168, 0.07517
 0.44548, 0.07530
 0.43934, 0.07540
 0.43328, 0.07549
 0.42729, 0.07555
 0.42137, 0.07558
 0.41553, 0.07560
 0.40976, 0.07559
 0.40406, 0.07556
 0.39843, 0.07552
 0.39286, 0.07543
 0.38736, 0.07534
 0.38192, 0.07522
 0.37655, 0.07510
 0.37125, 0.07495
 0.36600, 0.07479
 0.36081, 0.07462
 0.35569, 0.07443
 0.35062, 0.07422
 0.34561, 0.07400
 0.34065, 0.07378
 0.33575, 0.07355
 0.33091, 0.07331
 0.32612, 0.07305
 0.32138, 0.07279
 0.31671, 0.07251
 0.31207, 0.07223
 0.30750, 0.07193
 0.30296, 0.07163
 0.29848, 0.07132
 0.29405, 0.07100
 0.28967, 0.07068
 0.28534, 0.07035
 0.28105, 0.07001
 0.27680, 0.06967
 0.27261, 0.06931
 0.26846, 0.06896
 0.26435, 0.06860
 0.26028, 0.06822
 0.25626, 0.06785
 0.25228, 0.06747
 0.24835, 0.06708
 0.24445, 0.06670
 0.24059, 0.06630
 0.23678, 0.06589
 0.23300, 0.06549
 0.22926, 0.06508
 0.22556, 0.06467
 0.22190, 0.06426
 0.21828, 0.06383
 0.21470, 0.06340
 0.21115, 0.06297
 0.20763, 0.06254
 0.20416, 0.06210
 0.20071, 0.06166
 0.19730, 0.06120
 0.19392, 0.06076
 0.19058, 0.06030
 0.18728, 0.05985
 0.18400, 0.05938
 0.18076, 0.05892
 0.17755, 0.05844
 0.17437, 0.05798
 0.17122, 0.05750
 0.16811, 0.05703
 0.16503, 0.05655
 0.16197, 0.05606
 0.15894, 0.05557
 0.15595, 0.05508
 0.15298, 0.05460
 0.15004, 0.05410
 0.14712, 0.05360
 0.14424, 0.05308
 0.14139, 0.05256
 0.13857, 0.05204
 0.13577, 0.05151
 0.13299, 0.05099
 0.13026, 0.05046
 0.12753, 0.04992
 0.12484, 0.04940
 0.12217, 0.04887
 0.11952, 0.04834
 0.11690, 0.04782
 0.11431, 0.04729
 0.11173, 0.04676
 0.10918, 0.04624
 0.10665, 0.04573
 0.10414, 0.04520
 0.10165, 0.04469
 0.09919, 0.04418
 0.09675, 0.04369
 0.09432, 0.04324
 0.09191, 0.04279
 0.08953, 0.04234
 0.08716, 0.04187
 0.08482, 0.04141
 0.08250, 0.04094
 0.08020, 0.04046
 0.07793, 0.03996
 0.07567, 0.03945
 0.07344, 0.03892
 0.07124, 0.03836
 0.06907, 0.03773
 0.06692, 0.03709
 0.06480, 0.03642
 0.06268, 0.03575
 0.06061, 0.03507
 0.05854, 0.03437
 0.05650, 0.03366
 0.05448, 0.03293
 0.05247, 0.03220
 0.05048, 0.03147
 0.04851, 0.03073
 0.04656, 0.03001
 0.04462, 0.02935
 0.04269, 0.02867
 0.04077, 0.02799
 0.03888, 0.02731
 0.03700, 0.02663
 0.03513, 0.02594
 0.03329, 0.02525
 0.03146, 0.02454
 0.02965, 0.02384
 0.02786, 0.02312
 0.02609, 0.02238
 0.02433, 0.02164
 0.02259, 0.02087
 0.02087, 0.02007
 0.01917, 0.01925
 0.01749, 0.01841
 0.01583, 0.01754
 0.01419, 0.01665
 0.01257, 0.01572
 0.01096, 0.01475
 0.00939, 0.01373
 0.00784, 0.01266
 0.00631, 0.01152
 0.00482, 0.01028
 0.00337, 0.00889
 0.00197, 0.00725
 0.00069, 0.00514
-0.00002, 0.00299
 0.00000, 0.00000
 0.00000, 0.00000
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 0.03692,-0.01396
 0.03892,-0.01423
 0.04094,-0.01449
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 0.04500,-0.01500
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 0.05763,-0.01671
 0.05981,-0.01703
 0.06200,-0.01734
 0.06420,-0.01765
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 0.06865,-0.01822
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 0.08469,-0.01953
 0.08703,-0.01961
 0.08939,-0.01968
 0.09178,-0.01974
 0.09418,-0.01980
 0.09660,-0.01984
 0.09904,-0.01989
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 0.10399,-0.02002
 0.10651,-0.02014
 0.10905,-0.02026
 0.11161,-0.02038
 0.11419,-0.02050
 0.11680,-0.02063
 0.11943,-0.02077
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 0.14420,-0.02204
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 0.15290,-0.02246
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 1.00000, 0.00000