ファイルインデックス名　: File Index Name        : 1177        .A  
翼型整理番号　　　　　　: Airfoil Serial No.     : N04-0082-1
翼型名　　　　　　　　　: Airfoil Name           : N.A.C.A. 65>>1<<-412
翼型ファイル番号　　　　: Airfoil File No.       : 1177
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
 0.98625, 0.00272
 0.97270, 0.00540
 0.95935, 0.00807
 0.94620, 0.01068
 0.93324, 0.01327
 0.92047, 0.01582
 0.90788, 0.01834
 0.89547, 0.02083
 0.88324, 0.02329
 0.87118, 0.02570
 0.85930, 0.02808
 0.84759, 0.03039
 0.83604, 0.03264
 0.82467, 0.03484
 0.81346, 0.03700
 0.80240, 0.03909
 0.79150, 0.04114
 0.78077, 0.04312
 0.77017, 0.04505
 0.75973, 0.04694
 0.74943, 0.04876
 0.73928, 0.05052
 0.72928, 0.05222
 0.71941, 0.05387
 0.70968, 0.05547
 0.70009, 0.05700
 0.69063, 0.05850
 0.68129, 0.05994
 0.67209, 0.06132
 0.66300, 0.06266
 0.65405, 0.06395
 0.64521, 0.06518
 0.63650, 0.06636
 0.62790, 0.06749
 0.61943, 0.06858
 0.61106, 0.06961
 0.60281, 0.07060
 0.59467, 0.07154
 0.58663, 0.07243
 0.57869, 0.07328
 0.57088, 0.07408
 0.56315, 0.07484
 0.55553, 0.07555
 0.54801, 0.07623
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 0.53326, 0.07744
 0.52603, 0.07797
 0.51889, 0.07848
 0.51184, 0.07894
 0.50489, 0.07936
 0.49803, 0.07974
 0.49125, 0.08007
 0.48456, 0.08036
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 0.47143, 0.08086
 0.46500, 0.08104
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 0.21895, 0.06848
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 0.21180, 0.06756
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 0.17816, 0.06266
 0.17498, 0.06215
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 0.15953, 0.05956
 0.15653, 0.05903
 0.15356, 0.05850
 0.15061, 0.05797
 0.14769, 0.05743
 0.14480, 0.05689
 0.14194, 0.05635
 0.13912, 0.05581
 0.13631, 0.05525
 0.13352, 0.05470
 0.13078, 0.05415
 0.12804, 0.05358
 0.12535, 0.05303
 0.12267, 0.05246
 0.12002, 0.05190
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 0.11479, 0.05076
 0.11221, 0.05018
 0.10966, 0.04960
 0.10713, 0.04902
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 0.09724, 0.04667
 0.09483, 0.04607
 0.09243, 0.04546
 0.09006, 0.04487
 0.08770, 0.04426
 0.08538, 0.04365
 0.08307, 0.04304
 0.08079, 0.04241
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 0.07628, 0.04117
 0.07405, 0.04055
 0.07185, 0.03993
 0.06967, 0.03929
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 0.06535, 0.03801
 0.06322, 0.03737
 0.06112, 0.03672
 0.05903, 0.03607
 0.05697, 0.03540
 0.05492, 0.03474
 0.05288, 0.03407
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 0.04300, 0.03063
 0.04108, 0.02992
 0.03918, 0.02920
 0.03729, 0.02848
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 0.03357, 0.02700
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 0.00485, 0.01150
 0.00338, 0.01001
 0.00198, 0.00822
 0.00069, 0.00587
-0.00002, 0.00342
 0.00000, 0.00000
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 1.00000, 0.00000