ファイルインデックス名　: File Index Name        : 1308        .A  
翼型整理番号　　　　　　: Airfoil Serial No.     : N06-0030-1
翼型名　　　　　　　　　: Airfoil Name           : N.A.C.A. 7-H-12
翼型ファイル番号　　　　: Airfoil File No.       : 1308
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-A01B1


座標　　　　　　　　　　: Plot Ordinates         :

 X             Y

 1.00000, 0.00000
 0.98586, 0.00179
 0.97190, 0.00363
 0.95810, 0.00551
 0.94448, 0.00744
 0.93103, 0.00940
 0.91775, 0.01138
 0.90463, 0.01339
 0.89168, 0.01542
 0.87890, 0.01747
 0.86628, 0.01951
 0.85382, 0.02157
 0.84153, 0.02362
 0.82940, 0.02567
 0.81743, 0.02771
 0.80562, 0.02973
 0.79398, 0.03172
 0.78250, 0.03368
 0.77118, 0.03561
 0.76001, 0.03752
 0.74899, 0.03941
 0.73812, 0.04126
 0.72741, 0.04309
 0.71685, 0.04488
 0.70642, 0.04665
 0.69614, 0.04837
 0.68601, 0.05005
 0.67602, 0.05170
 0.66617, 0.05331
 0.65645, 0.05488
 0.64686, 0.05642
 0.63742, 0.05793
 0.62809, 0.05940
 0.61889, 0.06084
 0.60982, 0.06224
 0.60088, 0.06361
 0.59207, 0.06493
 0.58337, 0.06621
 0.57479, 0.06747
 0.56632, 0.06868
 0.55797, 0.06987
 0.54975, 0.07101
 0.54162, 0.07213
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 0.52571, 0.07425
 0.51791, 0.07526
 0.51022, 0.07624
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 0.49515, 0.07808
 0.48777, 0.07896
 0.48049, 0.07979
 0.47331, 0.08060
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 0.45922, 0.08213
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 0.43880, 0.08419
 0.43216, 0.08481
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 0.41279, 0.08652
 0.40650, 0.08704
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 0.18914, 0.08729
 0.18565, 0.08692
 0.18221, 0.08652
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 0.14685, 0.08151
 0.14385, 0.08099
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 0.13223, 0.07882
 0.12941, 0.07825
 0.12663, 0.07768
 0.12386, 0.07709
 0.12114, 0.07650
 0.11844, 0.07589
 0.11578, 0.07529
 0.11315, 0.07467
 0.11055, 0.07403
 0.10798, 0.07340
 0.10544, 0.07276
 0.10292, 0.07210
 0.10045, 0.07144
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 0.09557, 0.07009
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 0.08846, 0.06800
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 0.06859, 0.06130
 0.06650, 0.06051
 0.06445, 0.05971
 0.06242, 0.05891
 0.06041, 0.05810
 0.05843, 0.05728
 0.05647, 0.05646
 0.05454, 0.05562
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 0.04704, 0.05219
 0.04522, 0.05130
 0.04343, 0.05042
 0.04166, 0.04951
 0.03991, 0.04860
 0.03819, 0.04767
 0.03648, 0.04674
 0.03481, 0.04579
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 0.02992, 0.04288
 0.02832, 0.04189
 0.02675, 0.04088
 0.02522, 0.03986
 0.02370, 0.03882
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 0.00107, 0.01572
 0.00022, 0.01386
-0.00052, 0.01181
-0.00112, 0.00946
-0.00141, 0.00652
-0.00118, 0.00368
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 0.00000, 0.00000
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 1.00000, 0.00000