ファイルインデックス名　: File Index Name        : 1143        .A  
翼型整理番号　　　　　　: Airfoil Serial No.     : N04-0048-1
翼型名　　　　　　　　　: Airfoil Name           : N.A.C.A. 64>>1<<-212
翼型ファイル番号　　　　: Airfoil File No.       : 1143
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

 1.00000, 0.00000
 0.98658, 0.00151
 0.97336, 0.00309
 0.96032, 0.00472
 0.94747, 0.00640
 0.93481, 0.00811
 0.92232, 0.00985
 0.91001, 0.01161
 0.89787, 0.01338
 0.88591, 0.01515
 0.87412, 0.01692
 0.86249, 0.01869
 0.85102, 0.02044
 0.83971, 0.02218
 0.82857, 0.02390
 0.81757, 0.02559
 0.80673, 0.02728
 0.79604, 0.02893
 0.78551, 0.03055
 0.77510, 0.03215
 0.76485, 0.03372
 0.75473, 0.03526
 0.74476, 0.03675
 0.73492, 0.03821
 0.72521, 0.03964
 0.71563, 0.04105
 0.70619, 0.04240
 0.69687, 0.04373
 0.68767, 0.04501
 0.67859, 0.04627
 0.66963, 0.04749
 0.66080, 0.04867
 0.65207, 0.04982
 0.64347, 0.05094
 0.63497, 0.05201
 0.62659, 0.05306
 0.61832, 0.05407
 0.61015, 0.05504
 0.60209, 0.05598
 0.59412, 0.05690
 0.58626, 0.05777
 0.57850, 0.05861
 0.57084, 0.05942
 0.56327, 0.06021
 0.55581, 0.06096
 0.54843, 0.06168
 0.54114, 0.06237
 0.53394, 0.06303
 0.52684, 0.06366
 0.51982, 0.06426
 0.51289, 0.06483
 0.50605, 0.06537
 0.49928, 0.06588
 0.49260, 0.06637
 0.48600, 0.06683
 0.47948, 0.06726
 0.47304, 0.06767
 0.46667, 0.06804
 0.46038, 0.06840
 0.45417, 0.06872
 0.44803, 0.06901
 0.44197, 0.06929
 0.43596, 0.06954
 0.43004, 0.06977
 0.42418, 0.06996
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 0.31552, 0.06894
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 0.23643, 0.06359
 0.23268, 0.06324
 0.22896, 0.06289
 0.22529, 0.06253
 0.22166, 0.06217
 0.21806, 0.06179
 0.21449, 0.06142
 0.21096, 0.06104
 0.20746, 0.06066
 0.20400, 0.06027
 0.20057, 0.05988
 0.19717, 0.05948
 0.19381, 0.05909
 0.19048, 0.05868
 0.18718, 0.05827
 0.18392, 0.05786
 0.18068, 0.05745
 0.17748, 0.05703
 0.17431, 0.05661
 0.17117, 0.05619
 0.16806, 0.05576
 0.16497, 0.05533
 0.16192, 0.05489
 0.15890, 0.05444
 0.15589, 0.05400
 0.15292, 0.05356
 0.14998, 0.05311
 0.14707, 0.05265
 0.14418, 0.05220
 0.14132, 0.05174
 0.13848, 0.05127
 0.13568, 0.05080
 0.13289, 0.05034
 0.13014, 0.04986
 0.12741, 0.04938
 0.12470, 0.04890
 0.12202, 0.04842
 0.11936, 0.04793
 0.11673, 0.04744
 0.11412, 0.04695
 0.11153, 0.04645
 0.10896, 0.04595
 0.10642, 0.04545
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 0.10141, 0.04443
 0.09894, 0.04392
 0.09649, 0.04341
 0.09406, 0.04288
 0.09164, 0.04236
 0.08926, 0.04184
 0.08689, 0.04129
 0.08455, 0.04077
 0.08222, 0.04022
 0.07992, 0.03968
 0.07764, 0.03913
 0.07537, 0.03858
 0.07313, 0.03802
 0.07090, 0.03746
 0.06869, 0.03689
 0.06650, 0.03632
 0.06434, 0.03574
 0.06219, 0.03516
 0.06006, 0.03457
 0.05795, 0.03398
 0.05585, 0.03338
 0.05377, 0.03277
 0.05171, 0.03216
 0.04967, 0.03154
 0.04766, 0.03091
 0.04565, 0.03028
 0.04366, 0.02963
 0.04169, 0.02897
 0.03974, 0.02830
 0.03779, 0.02763
 0.03588, 0.02694
 0.03397, 0.02625
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 0.02290, 0.02178
 0.02110, 0.02098
 0.01933, 0.02016
 0.01757, 0.01930
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 0.01412, 0.01748
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 0.00581, 0.01179
 0.00421, 0.01029
 0.00266, 0.00848
 0.00117, 0.00611
 0.00026, 0.00360
 0.00000, 0.00000
 0.00000, 0.00000
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 0.08353,-0.03085
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 0.11321,-0.03511
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 1.00000, 0.00000