ファイルインデックス名　: File Index Name        : 3114        .A  
翼型整理番号　　　　　　: Airfoil Serial No.     : H06-0011-1
翼型名　　　　　　　　　: Airfoil Name           : HQ-2.5/10
翼型ファイル番号　　　　: Airfoil File No.       : 3114
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.   : X68eB03-C01G2


座標　　　　　　　　　　: Plot Ordinates         :

 X             Y

 1.00000, 0.00000
 0.98671, 0.00211
 0.97362, 0.00431
 0.96072, 0.00657
 0.94801, 0.00886
 0.93549, 0.01116
 0.92315, 0.01344
 0.91099, 0.01569
 0.89900, 0.01787
 0.88719, 0.01989
 0.87554, 0.02185
 0.86406, 0.02376
 0.85274, 0.02564
 0.84158, 0.02755
 0.83058, 0.02945
 0.81973, 0.03132
 0.80903, 0.03316
 0.79848, 0.03495
 0.78808, 0.03665
 0.77781, 0.03831
 0.76769, 0.03991
 0.75770, 0.04146
 0.74785, 0.04297
 0.73814, 0.04442
 0.72855, 0.04584
 0.71909, 0.04721
 0.70976, 0.04854
 0.70055, 0.04982
 0.69146, 0.05109
 0.68249, 0.05231
 0.67363, 0.05349
 0.66490, 0.05464
 0.65627, 0.05574
 0.64776, 0.05681
 0.63935, 0.05784
 0.63106, 0.05883
 0.62287, 0.05978
 0.61478, 0.06070
 0.60680, 0.06157
 0.59891, 0.06241
 0.59112, 0.06320
 0.58344, 0.06395
 0.57584, 0.06467
 0.56834, 0.06536
 0.56094, 0.06601
 0.55362, 0.06663
 0.54639, 0.06721
 0.53925, 0.06777
 0.53220, 0.06830
 0.52523, 0.06879
 0.51835, 0.06926
 0.51155, 0.06970
 0.50483, 0.07012
 0.49819, 0.07049
 0.49163, 0.07082
 0.48514, 0.07112
 0.47874, 0.07140
 0.47240, 0.07166
 0.46614, 0.07190
 0.45996, 0.07212
 0.45384, 0.07232
 0.44780, 0.07250
 0.44182, 0.07266
 0.43591, 0.07282
 0.43007, 0.07295
 0.42430, 0.07308
 0.41859, 0.07319
 0.41295, 0.07330
 0.40737, 0.07339
 0.40185, 0.07347
 0.39639, 0.07358
 0.39099, 0.07369
 0.38566, 0.07378
 0.38038, 0.07386
 0.37516, 0.07392
 0.37000, 0.07397
 0.36489, 0.07401
 0.35984, 0.07402
 0.35484, 0.07402
 0.34990, 0.07400
 0.34501, 0.07393
 0.34017, 0.07383
 0.33538, 0.07373
 0.33065, 0.07361
 0.32596, 0.07347
 0.32133, 0.07332
 0.31674, 0.07317
 0.31220, 0.07300
 0.30771, 0.07282
 0.30326, 0.07264
 0.29887, 0.07246
 0.29451, 0.07229
 0.29020, 0.07211
 0.28594, 0.07193
 0.28172, 0.07175
 0.27754, 0.07156
 0.27340, 0.07136
 0.26931, 0.07116
 0.26526, 0.07095
 0.26125, 0.07074
 0.25728, 0.07052
 0.25334, 0.07030
 0.24945, 0.07007
 0.24560, 0.06983
 0.24178, 0.06959
 0.23800, 0.06934
 0.23426, 0.06909
 0.23056, 0.06883
 0.22689, 0.06856
 0.22326, 0.06829
 0.21966, 0.06801
 0.21610, 0.06772
 0.21257, 0.06743
 0.20907, 0.06713
 0.20561, 0.06682
 0.20218, 0.06651
 0.19879, 0.06618
 0.19542, 0.06584
 0.19209, 0.06550
 0.18879, 0.06515
 0.18552, 0.06479
 0.18228, 0.06443
 0.17908, 0.06406
 0.17590, 0.06368
 0.17275, 0.06329
 0.16963, 0.06290
 0.16654, 0.06250
 0.16348, 0.06210
 0.16044, 0.06169
 0.15743, 0.06127
 0.15445, 0.06085
 0.15150, 0.06042
 0.14858, 0.05999
 0.14568, 0.05955
 0.14280, 0.05911
 0.13996, 0.05866
 0.13713, 0.05820
 0.13434, 0.05774
 0.13157, 0.05727
 0.12882, 0.05679
 0.12610, 0.05631
 0.12340, 0.05583
 0.12072, 0.05533
 0.11807, 0.05483
 0.11544, 0.05432
 0.11283, 0.05381
 0.11025, 0.05329
 0.10769, 0.05276
 0.10515, 0.05222
 0.10264, 0.05168
 0.10014, 0.05113
 0.09767, 0.05057
 0.09521, 0.05000
 0.09278, 0.04942
 0.09037, 0.04884
 0.08798, 0.04824
 0.08561, 0.04764
 0.08326, 0.04703
 0.08093, 0.04641
 0.07862, 0.04579
 0.07633, 0.04515
 0.07405, 0.04450
 0.07180, 0.04385
 0.06956, 0.04318
 0.06735, 0.04251
 0.06515, 0.04182
 0.06297, 0.04113
 0.06081, 0.04042
 0.05866, 0.03970
 0.05653, 0.03897
 0.05442, 0.03822
 0.05233, 0.03747
 0.05026, 0.03670
 0.04820, 0.03592
 0.04615, 0.03513
 0.04413, 0.03433
 0.04212, 0.03350
 0.04012, 0.03266
 0.03815, 0.03179
 0.03618, 0.03090
 0.03424, 0.02999
 0.03231, 0.02905
 0.03039, 0.02807
 0.02849, 0.02707
 0.02660, 0.02602
 0.02473, 0.02493
 0.02287, 0.02371
 0.02103, 0.02247
 0.01920, 0.02118
 0.01739, 0.01987
 0.01559, 0.01851
 0.01380, 0.01713
 0.01203, 0.01575
 0.01027, 0.01440
 0.00853, 0.01300
 0.00680, 0.01151
 0.00508, 0.00988
 0.00337, 0.00801
 0.00168, 0.00564
 0.00056, 0.00326
 0.00000, 0.00000
 0.00000, 0.00000
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 0.00680,-0.00643
 0.00853,-0.00741
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 0.01559,-0.01040
 0.01739,-0.01096
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 0.02473,-0.01284
 0.02660,-0.01325
 0.02849,-0.01364
 0.03039,-0.01402
 0.03231,-0.01438
 0.03424,-0.01472
 0.03618,-0.01505
 0.03815,-0.01536
 0.04012,-0.01567
 0.04212,-0.01596
 0.04413,-0.01624
 0.04615,-0.01651
 0.04820,-0.01678
 0.05026,-0.01703
 0.05233,-0.01727
 0.05442,-0.01750
 0.05653,-0.01772
 0.05866,-0.01794
 0.06081,-0.01815
 0.06297,-0.01835
 0.06515,-0.01855
 0.06735,-0.01874
 0.06956,-0.01893
 0.07180,-0.01912
 0.07405,-0.01930
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 0.07862,-0.01965
 0.08093,-0.01982
 0.08326,-0.01999
 0.08561,-0.02015
 0.08798,-0.02032
 0.09037,-0.02048
 0.09278,-0.02064
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 0.09767,-0.02095
 0.10014,-0.02111
 0.10264,-0.02130
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 0.10769,-0.02166
 0.11025,-0.02184
 0.11283,-0.02202
 0.11544,-0.02220
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 0.12072,-0.02254
 0.12340,-0.02271
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 0.13996,-0.02364
 0.14280,-0.02377
 0.14568,-0.02391
 0.14858,-0.02404
 0.15150,-0.02415
 0.15445,-0.02424
 0.15743,-0.02433
 0.16044,-0.02441
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 0.16654,-0.02456
 0.16963,-0.02464
 0.17275,-0.02470
 0.17590,-0.02477
 0.17908,-0.02483
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 0.97362, 0.00112
 0.98671, 0.00062
 1.00000, 0.00000