ファイルインデックス名　: File Index Name        : 3113        .A  
翼型整理番号　　　　　　: Airfoil Serial No.     : H06-0010-1
翼型名　　　　　　　　　: Airfoil Name           : HQ-2.5/9
翼型ファイル番号　　　　: Airfoil File No.       : 3113
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, 0.00201
 0.97362, 0.00410
 0.96072, 0.00626
 0.94801, 0.00845
 0.93549, 0.01064
 0.92315, 0.01283
 0.91099, 0.01498
 0.89900, 0.01707
 0.88719, 0.01900
 0.87554, 0.02087
 0.86406, 0.02269
 0.85274, 0.02447
 0.84158, 0.02626
 0.83058, 0.02803
 0.81973, 0.02977
 0.80903, 0.03147
 0.79848, 0.03314
 0.78808, 0.03473
 0.77781, 0.03628
 0.76769, 0.03779
 0.75770, 0.03925
 0.74785, 0.04067
 0.73814, 0.04205
 0.72855, 0.04338
 0.71909, 0.04467
 0.70976, 0.04592
 0.70055, 0.04713
 0.69146, 0.04829
 0.68249, 0.04942
 0.67363, 0.05051
 0.66490, 0.05155
 0.65627, 0.05256
 0.64776, 0.05353
 0.63935, 0.05447
 0.63106, 0.05536
 0.62287, 0.05623
 0.61478, 0.05705
 0.60680, 0.05784
 0.59891, 0.05860
 0.59112, 0.05932
 0.58344, 0.06000
 0.57584, 0.06065
 0.56834, 0.06126
 0.56094, 0.06185
 0.55362, 0.06241
 0.54639, 0.06294
 0.53925, 0.06344
 0.53220, 0.06391
 0.52523, 0.06436
 0.51835, 0.06478
 0.51155, 0.06518
 0.50483, 0.06555
 0.49819, 0.06589
 0.49163, 0.06618
 0.48514, 0.06646
 0.47874, 0.06671
 0.47240, 0.06694
 0.46614, 0.06716
 0.45996, 0.06736
 0.45384, 0.06754
 0.44780, 0.06770
 0.44182, 0.06785
 0.43591, 0.06799
 0.43007, 0.06812
 0.42430, 0.06823
 0.41859, 0.06833
 0.41295, 0.06842
 0.40737, 0.06850
 0.40185, 0.06858
 0.39639, 0.06867
 0.39099, 0.06876
 0.38566, 0.06884
 0.38038, 0.06891
 0.37516, 0.06896
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 0.34990, 0.06900
 0.34501, 0.06893
 0.34017, 0.06884
 0.33538, 0.06874
 0.33065, 0.06863
 0.32596, 0.06850
 0.32133, 0.06837
 0.31674, 0.06822
 0.31220, 0.06807
 0.30771, 0.06790
 0.30326, 0.06773
 0.29887, 0.06756
 0.29451, 0.06740
 0.29020, 0.06723
 0.28594, 0.06706
 0.28172, 0.06688
 0.27754, 0.06670
 0.27340, 0.06651
 0.26931, 0.06632
 0.26526, 0.06612
 0.26125, 0.06591
 0.25728, 0.06570
 0.25334, 0.06549
 0.24945, 0.06527
 0.24560, 0.06504
 0.24178, 0.06481
 0.23800, 0.06458
 0.23426, 0.06434
 0.23056, 0.06409
 0.22689, 0.06384
 0.22326, 0.06358
 0.21966, 0.06331
 0.21610, 0.06304
 0.21257, 0.06276
 0.20907, 0.06248
 0.20561, 0.06219
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 0.19879, 0.06159
 0.19542, 0.06127
 0.19209, 0.06095
 0.18879, 0.06062
 0.18552, 0.06029
 0.18228, 0.05995
 0.17908, 0.05960
 0.17590, 0.05925
 0.17275, 0.05889
 0.16963, 0.05852
 0.16654, 0.05815
 0.16348, 0.05777
 0.16044, 0.05739
 0.15743, 0.05700
 0.15445, 0.05661
 0.15150, 0.05621
 0.14858, 0.05580
 0.14568, 0.05539
 0.14280, 0.05498
 0.13996, 0.05456
 0.13713, 0.05413
 0.13434, 0.05370
 0.13157, 0.05326
 0.12882, 0.05282
 0.12610, 0.05237
 0.12340, 0.05192
 0.12072, 0.05145
 0.11807, 0.05099
 0.11544, 0.05051
 0.11283, 0.05003
 0.11025, 0.04954
 0.10769, 0.04905
 0.10515, 0.04855
 0.10264, 0.04804
 0.10014, 0.04753
 0.09767, 0.04700
 0.09521, 0.04647
 0.09278, 0.04593
 0.09037, 0.04538
 0.08798, 0.04482
 0.08561, 0.04425
 0.08326, 0.04368
 0.08093, 0.04310
 0.07862, 0.04251
 0.07633, 0.04191
 0.07405, 0.04131
 0.07180, 0.04069
 0.06956, 0.04007
 0.06735, 0.03944
 0.06515, 0.03879
 0.06297, 0.03814
 0.06081, 0.03748
 0.05866, 0.03680
 0.05653, 0.03611
 0.05442, 0.03542
 0.05233, 0.03471
 0.05026, 0.03399
 0.04820, 0.03327
 0.04615, 0.03253
 0.04413, 0.03179
 0.04212, 0.03102
 0.04012, 0.03023
 0.03815, 0.02943
 0.03618, 0.02860
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 0.03231, 0.02687
 0.03039, 0.02597
 0.02849, 0.02503
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 0.02473, 0.02304
 0.02287, 0.02190
 0.02103, 0.02073
 0.01920, 0.01953
 0.01739, 0.01830
 0.01559, 0.01704
 0.01380, 0.01575
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 0.01027, 0.01325
 0.00853, 0.01199
 0.00680, 0.01064
 0.00508, 0.00917
 0.00337, 0.00748
 0.00168, 0.00531
 0.00056, 0.00310
 0.00000, 0.00000
 0.00000, 0.00000
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 0.03231,-0.01220
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 0.03618,-0.01275
 0.03815,-0.01300
 0.04012,-0.01324
 0.04212,-0.01348
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 0.04615,-0.01392
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 0.05442,-0.01470
 0.05653,-0.01487
 0.05866,-0.01504
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 0.08093,-0.01651
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 0.09037,-0.01702
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 0.10769,-0.01794
 0.11025,-0.01807
 0.11283,-0.01821
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 0.14280,-0.01955
 0.14568,-0.01966
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 0.15150,-0.01984
 0.15445,-0.01990
 0.15743,-0.01997
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 0.16654,-0.02014
 0.16963,-0.02019
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 0.98671, 0.00073
 1.00000, 0.00000