ファイルインデックス名　: File Index Name        : 1224-2      .A  
翼型整理番号　　　　　　: Airfoil Serial No.     : N06-0006-2
翼型名　　　　　　　　　: Airfoil Name           : N.A.C.A. 6-H-10
翼型ファイル番号　　　　: Airfoil File No.       : 1224
翼型情報　　　　　　　　: Airfoil Information    : 

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.   : X68eB03-C01G2


座標　　　　　　　　　　: Plot Ordinates         :

 X             Y

 1.00000, 0.00000
 0.98671, 0.00074
 0.97362, 0.00144
 0.96072, 0.00212
 0.94801, 0.00281
 0.93549, 0.00353
 0.92315, 0.00430
 0.91099, 0.00515
 0.89900, 0.00610
 0.88719, 0.00738
 0.87554, 0.00881
 0.86406, 0.01035
 0.85274, 0.01200
 0.84158, 0.01374
 0.83058, 0.01555
 0.81973, 0.01742
 0.80903, 0.01934
 0.79848, 0.02126
 0.78808, 0.02309
 0.77781, 0.02493
 0.76769, 0.02678
 0.75770, 0.02865
 0.74785, 0.03052
 0.73814, 0.03239
 0.72855, 0.03427
 0.71909, 0.03615
 0.70976, 0.03802
 0.70055, 0.03989
 0.69146, 0.04182
 0.68249, 0.04374
 0.67363, 0.04565
 0.66490, 0.04753
 0.65627, 0.04939
 0.64776, 0.05121
 0.63935, 0.05299
 0.63106, 0.05474
 0.62287, 0.05643
 0.61478, 0.05808
 0.60680, 0.05967
 0.59891, 0.06119
 0.59112, 0.06254
 0.58344, 0.06382
 0.57584, 0.06505
 0.56834, 0.06623
 0.56094, 0.06735
 0.55362, 0.06841
 0.54639, 0.06943
 0.53925, 0.07039
 0.53220, 0.07131
 0.52523, 0.07217
 0.51835, 0.07299
 0.51155, 0.07377
 0.50483, 0.07450
 0.49819, 0.07518
 0.49163, 0.07583
 0.48514, 0.07643
 0.47874, 0.07700
 0.47240, 0.07752
 0.46614, 0.07800
 0.45996, 0.07845
 0.45384, 0.07886
 0.44780, 0.07923
 0.44182, 0.07957
 0.43591, 0.07987
 0.43007, 0.08013
 0.42430, 0.08037
 0.41859, 0.08057
 0.41295, 0.08073
 0.40737, 0.08087
 0.40185, 0.08097
 0.39639, 0.08101
 0.39099, 0.08101
 0.38566, 0.08098
 0.38038, 0.08092
 0.37516, 0.08083
 0.37000, 0.08072
 0.36489, 0.08059
 0.35984, 0.08043
 0.35484, 0.08026
 0.34990, 0.08006
 0.34501, 0.07985
 0.34017, 0.07962
 0.33538, 0.07937
 0.33065, 0.07911
 0.32596, 0.07883
 0.32133, 0.07854
 0.31674, 0.07824
 0.31220, 0.07792
 0.30771, 0.07759
 0.30326, 0.07726
 0.29887, 0.07692
 0.29451, 0.07660
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 0.28594, 0.07594
 0.28172, 0.07560
 0.27754, 0.07526
 0.27340, 0.07490
 0.26931, 0.07454
 0.26526, 0.07418
 0.26125, 0.07381
 0.25728, 0.07343
 0.25334, 0.07304
 0.24945, 0.07266
 0.24560, 0.07227
 0.24178, 0.07187
 0.23800, 0.07147
 0.23426, 0.07106
 0.23056, 0.07066
 0.22689, 0.07024
 0.22326, 0.06983
 0.21966, 0.06941
 0.21610, 0.06899
 0.21257, 0.06856
 0.20907, 0.06814
 0.20561, 0.06771
 0.20218, 0.06728
 0.19879, 0.06686
 0.19542, 0.06647
 0.19209, 0.06607
 0.18879, 0.06567
 0.18552, 0.06526
 0.18228, 0.06485
 0.17908, 0.06443
 0.17590, 0.06400
 0.17275, 0.06356
 0.16963, 0.06312
 0.16654, 0.06267
 0.16348, 0.06221
 0.16044, 0.06173
 0.15743, 0.06125
 0.15445, 0.06076
 0.15150, 0.06026
 0.14858, 0.05972
 0.14568, 0.05913
 0.14280, 0.05853
 0.13996, 0.05793
 0.13713, 0.05731
 0.13434, 0.05669
 0.13157, 0.05605
 0.12882, 0.05541
 0.12610, 0.05476
 0.12340, 0.05410
 0.12072, 0.05344
 0.11807, 0.05278
 0.11544, 0.05211
 0.11283, 0.05143
 0.11025, 0.05076
 0.10769, 0.05008
 0.10515, 0.04940
 0.10264, 0.04872
 0.10014, 0.04804
 0.09767, 0.04738
 0.09521, 0.04672
 0.09278, 0.04606
 0.09037, 0.04540
 0.08798, 0.04474
 0.08561, 0.04407
 0.08326, 0.04341
 0.08093, 0.04274
 0.07862, 0.04207
 0.07633, 0.04139
 0.07405, 0.04072
 0.07180, 0.04004
 0.06956, 0.03936
 0.06735, 0.03869
 0.06515, 0.03800
 0.06297, 0.03731
 0.06081, 0.03662
 0.05866, 0.03592
 0.05653, 0.03522
 0.05442, 0.03452
 0.05233, 0.03381
 0.05026, 0.03309
 0.04820, 0.03237
 0.04615, 0.03164
 0.04413, 0.03091
 0.04212, 0.03016
 0.04012, 0.02941
 0.03815, 0.02865
 0.03618, 0.02787
 0.03424, 0.02708
 0.03231, 0.02628
 0.03039, 0.02545
 0.02849, 0.02461
 0.02660, 0.02375
 0.02473, 0.02287
 0.02287, 0.02195
 0.02103, 0.02101
 0.01920, 0.02003
 0.01739, 0.01902
 0.01559, 0.01796
 0.01380, 0.01685
 0.01203, 0.01568
 0.01027, 0.01444
 0.00853, 0.01311
 0.00680, 0.01166
 0.00508, 0.01002
 0.00337, 0.00811
 0.00168, 0.00568
 0.00056, 0.00325
 0.00000, 0.00000
 0.00000, 0.00000
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 0.01559,-0.00793
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 0.03039,-0.00977
 0.03231,-0.00991
 0.03424,-0.01005
 0.03618,-0.01017
 0.03815,-0.01029
 0.04012,-0.01041
 0.04212,-0.01053
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 0.04615,-0.01077
 0.04820,-0.01089
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 0.05233,-0.01121
 0.05442,-0.01139
 0.05653,-0.01157
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 0.06081,-0.01194
 0.06297,-0.01211
 0.06515,-0.01229
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 0.07405,-0.01294
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 0.08093,-0.01330
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 0.08561,-0.01350
 0.08798,-0.01360
 0.09037,-0.01369
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 0.09767,-0.01393
 0.10014,-0.01400
 0.10264,-0.01407
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 0.10769,-0.01421
 0.11025,-0.01427
 0.11283,-0.01433
 0.11544,-0.01438
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 0.13996,-0.01484
 0.14280,-0.01488
 0.14568,-0.01493
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 0.15445,-0.01509
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 0.16044,-0.01521
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 0.16654,-0.01533
 0.16963,-0.01539
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 0.17590,-0.01552
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 1.00000, 0.00000