ファイルインデックス名　: File Index Name        : 1316        .A  
翼型整理番号　　　　　　: Airfoil Serial No.     : N06-0038-1
翼型名　　　　　　　　　: Airfoil Name           : N.A.C.A. 15
翼型ファイル番号　　　　: Airfoil File No.       : 1316
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

 0.99987, 0.00132
 0.98629, 0.00414
 0.97293, 0.00685
 0.95977, 0.00948
 0.94680, 0.01202
 0.93404, 0.01448
 0.92146, 0.01685
 0.90907, 0.01915
 0.89686, 0.02137
 0.88483, 0.02351
 0.87297, 0.02558
 0.86129, 0.02758
 0.84978, 0.02952
 0.83843, 0.03140
 0.82725, 0.03321
 0.81622, 0.03497
 0.80535, 0.03667
 0.79463, 0.03833
 0.78407, 0.03994
 0.77365, 0.04151
 0.76337, 0.04302
 0.75324, 0.04449
 0.74324, 0.04592
 0.73339, 0.04730
 0.72367, 0.04864
 0.71408, 0.04994
 0.70462, 0.05120
 0.69529, 0.05241
 0.68608, 0.05360
 0.67700, 0.05475
 0.66802, 0.05587
 0.65919, 0.05694
 0.65045, 0.05798
 0.64184, 0.05900
 0.63333, 0.05997
 0.62495, 0.06091
 0.61667, 0.06183
 0.60849, 0.06271
 0.60042, 0.06356
 0.59245, 0.06437
 0.58458, 0.06515
 0.57683, 0.06591
 0.56915, 0.06664
 0.56158, 0.06735
 0.55412, 0.06802
 0.54673, 0.06867
 0.53944, 0.06930
 0.53224, 0.06990
 0.52513, 0.07048
 0.51810, 0.07104
 0.51117, 0.07158
 0.50432, 0.07208
 0.49755, 0.07258
 0.49086, 0.07307
 0.48425, 0.07353
 0.47772, 0.07397
 0.47128, 0.07439
 0.46490, 0.07479
 0.45860, 0.07518
 0.45238, 0.07555
 0.44623, 0.07589
 0.44015, 0.07622
 0.43414, 0.07653
 0.42820, 0.07682
 0.42233, 0.07709
 0.41654, 0.07735
 0.41081, 0.07759
 0.40514, 0.07781
 0.39954, 0.07801
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 0.38853, 0.07838
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 0.37247, 0.07880
 0.36724, 0.07890
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 0.35190, 0.07913
 0.34690, 0.07917
 0.34195, 0.07920
 0.33706, 0.07921
 0.33222, 0.07922
 0.32743, 0.07920
 0.32271, 0.07917
 0.31802, 0.07912
 0.31340, 0.07906
 0.30881, 0.07899
 0.30428, 0.07890
 0.29980, 0.07879
 0.29537, 0.07868
 0.29099, 0.07854
 0.28664, 0.07839
 0.28235, 0.07824
 0.27811, 0.07806
 0.27391, 0.07788
 0.26975, 0.07767
 0.26563, 0.07746
 0.26156, 0.07723
 0.25754, 0.07699
 0.25355, 0.07674
 0.24961, 0.07647
 0.24570, 0.07619
 0.24184, 0.07589
 0.23802, 0.07558
 0.23423, 0.07526
 0.23048, 0.07492
 0.22678, 0.07457
 0.22311, 0.07421
 0.21948, 0.07385
 0.21589, 0.07347
 0.21233, 0.07307
 0.20881, 0.07267
 0.20532, 0.07226
 0.20186, 0.07184
 0.19845, 0.07140
 0.19506, 0.07095
 0.19172, 0.07051
 0.18839, 0.07004
 0.18511, 0.06957
 0.18186, 0.06909
 0.17864, 0.06860
 0.17545, 0.06810
 0.17230, 0.06760
 0.16917, 0.06708
 0.16607, 0.06655
 0.16301, 0.06602
 0.15997, 0.06547
 0.15697, 0.06493
 0.15398, 0.06437
 0.15103, 0.06380
 0.14811, 0.06322
 0.14522, 0.06264
 0.14236, 0.06204
 0.13952, 0.06144
 0.13670, 0.06083
 0.13392, 0.06021
 0.13115, 0.05959
 0.12843, 0.05895
 0.12572, 0.05832
 0.12303, 0.05767
 0.12038, 0.05702
 0.11774, 0.05636
 0.11513, 0.05570
 0.11255, 0.05503
 0.10999, 0.05436
 0.10744, 0.05367
 0.10493, 0.05299
 0.10244, 0.05230
 0.09997, 0.05160
 0.09753, 0.05090
 0.09511, 0.05018
 0.09271, 0.04947
 0.09032, 0.04876
 0.08796, 0.04803
 0.08562, 0.04730
 0.08331, 0.04656
 0.08101, 0.04581
 0.07874, 0.04506
 0.07648, 0.04430
 0.07425, 0.04354
 0.07204, 0.04276
 0.06984, 0.04198
 0.06767, 0.04119
 0.06551, 0.04039
 0.06338, 0.03958
 0.06126, 0.03877
 0.05916, 0.03795
 0.05708, 0.03713
 0.05502, 0.03629
 0.05297, 0.03545
 0.05095, 0.03461
 0.04894, 0.03375
 0.04696, 0.03289
 0.04499, 0.03203
 0.04302, 0.03115
 0.04109, 0.03027
 0.03917, 0.02938
 0.03726, 0.02848
 0.03538, 0.02757
 0.03351, 0.02664
 0.03166, 0.02573
 0.02982, 0.02478
 0.02800, 0.02382
 0.02620, 0.02286
 0.02441, 0.02187
 0.02264, 0.02087
 0.02088, 0.01985
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 0.01742, 0.01774
 0.01572, 0.01666
 0.01403, 0.01554
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 0.01070, 0.01321
 0.00907, 0.01197
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 0.00587, 0.00931
 0.00430, 0.00781
 0.00275, 0.00614
 0.00127, 0.00413
 0.00033, 0.00226
 0.00000, 0.00000
 0.00000, 0.00000
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