ファイルインデックス名　: File Index Name        : 0753        .A  
翼型整理番号　　　　　　: Airfoil Serial No.     : N09-0026-1
翼型名　　　　　　　　　: Airfoil Name           : Naylor & Griffiths 26
翼型ファイル番号　　　　: Airfoil File No.       : 0753
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-A01E


座標　　　　　　　　　　: Plot Ordinates         :

 X             Y

 1.00000, 0.00000
 0.98671, 0.00508
 0.97362, 0.00920
 0.96072, 0.01249
 0.94801, 0.01506
 0.93549, 0.01705
 0.92315, 0.01856
 0.91099, 0.01970
 0.89900, 0.02061
 0.88719, 0.02187
 0.87554, 0.02308
 0.86406, 0.02423
 0.85274, 0.02534
 0.84158, 0.02640
 0.83058, 0.02741
 0.81973, 0.02839
 0.80903, 0.02933
 0.79848, 0.03023
 0.78808, 0.03112
 0.77781, 0.03197
 0.76769, 0.03280
 0.75770, 0.03359
 0.74785, 0.03435
 0.73814, 0.03509
 0.72855, 0.03580
 0.71909, 0.03648
 0.70976, 0.03713
 0.70055, 0.03776
 0.69146, 0.03838
 0.68249, 0.03898
 0.67363, 0.03955
 0.66490, 0.04010
 0.65627, 0.04063
 0.64776, 0.04113
 0.63935, 0.04161
 0.63106, 0.04206
 0.62287, 0.04250
 0.61478, 0.04290
 0.60680, 0.04329
 0.59891, 0.04364
 0.59112, 0.04392
 0.58344, 0.04419
 0.57584, 0.04443
 0.56834, 0.04466
 0.56094, 0.04487
 0.55362, 0.04506
 0.54639, 0.04525
 0.53925, 0.04542
 0.53220, 0.04559
 0.52523, 0.04575
 0.51835, 0.04590
 0.51155, 0.04605
 0.50483, 0.04620
 0.49819, 0.04636
 0.49163, 0.04658
 0.48514, 0.04680
 0.47874, 0.04701
 0.47240, 0.04722
 0.46614, 0.04743
 0.45996, 0.04764
 0.45384, 0.04784
 0.44780, 0.04804
 0.44182, 0.04823
 0.43591, 0.04841
 0.43007, 0.04859
 0.42430, 0.04876
 0.41859, 0.04892
 0.41295, 0.04907
 0.40737, 0.04922
 0.40185, 0.04936
 0.39639, 0.04946
 0.39099, 0.04955
 0.38566, 0.04963
 0.38038, 0.04970
 0.37516, 0.04976
 0.37000, 0.04982
 0.36489, 0.04986
 0.35984, 0.04990
 0.35484, 0.04994
 0.34990, 0.04997
 0.34501, 0.04999
 0.34017, 0.05000
 0.33538, 0.05001
 0.33065, 0.05001
 0.32596, 0.05001
 0.32133, 0.05000
 0.31674, 0.04999
 0.31220, 0.04997
 0.30771, 0.04995
 0.30326, 0.04992
 0.29887, 0.04989
 0.29451, 0.04985
 0.29020, 0.04981
 0.28594, 0.04976
 0.28172, 0.04970
 0.27754, 0.04964
 0.27340, 0.04958
 0.26931, 0.04951
 0.26526, 0.04944
 0.26125, 0.04936
 0.25728, 0.04928
 0.25334, 0.04919
 0.24945, 0.04909
 0.24560, 0.04900
 0.24178, 0.04890
 0.23800, 0.04879
 0.23426, 0.04868
 0.23056, 0.04856
 0.22689, 0.04845
 0.22326, 0.04832
 0.21966, 0.04819
 0.21610, 0.04806
 0.21257, 0.04793
 0.20907, 0.04779
 0.20561, 0.04764
 0.20218, 0.04750
 0.19879, 0.04735
 0.19542, 0.04720
 0.19209, 0.04704
 0.18879, 0.04688
 0.18552, 0.04672
 0.18228, 0.04655
 0.17908, 0.04638
 0.17590, 0.04620
 0.17275, 0.04602
 0.16963, 0.04583
 0.16654, 0.04564
 0.16348, 0.04545
 0.16044, 0.04525
 0.15743, 0.04504
 0.15445, 0.04483
 0.15150, 0.04461
 0.14858, 0.04439
 0.14568, 0.04416
 0.14280, 0.04392
 0.13996, 0.04368
 0.13713, 0.04344
 0.13434, 0.04319
 0.13157, 0.04293
 0.12882, 0.04267
 0.12610, 0.04240
 0.12340, 0.04213
 0.12072, 0.04185
 0.11807, 0.04156
 0.11544, 0.04127
 0.11283, 0.04098
 0.11025, 0.04068
 0.10769, 0.04037
 0.10515, 0.04006
 0.10264, 0.03974
 0.10014, 0.03942
 0.09767, 0.03910
 0.09521, 0.03878
 0.09278, 0.03845
 0.09037, 0.03811
 0.08798, 0.03777
 0.08561, 0.03741
 0.08326, 0.03703
 0.08093, 0.03665
 0.07862, 0.03626
 0.07633, 0.03585
 0.07405, 0.03541
 0.07180, 0.03495
 0.06956, 0.03447
 0.06735, 0.03398
 0.06515, 0.03347
 0.06297, 0.03294
 0.06081, 0.03240
 0.05866, 0.03185
 0.05653, 0.03128
 0.05442, 0.03069
 0.05233, 0.03009
 0.05026, 0.02948
 0.04820, 0.02883
 0.04615, 0.02817
 0.04413, 0.02749
 0.04212, 0.02679
 0.04012, 0.02608
 0.03815, 0.02537
 0.03618, 0.02463
 0.03424, 0.02388
 0.03231, 0.02313
 0.03039, 0.02236
 0.02849, 0.02158
 0.02660, 0.02078
 0.02473, 0.01999
 0.02287, 0.01923
 0.02103, 0.01846
 0.01920, 0.01766
 0.01739, 0.01684
 0.01559, 0.01598
 0.01380, 0.01509
 0.01203, 0.01414
 0.01027, 0.01313
 0.00853, 0.01204
 0.00680, 0.01083
 0.00508, 0.00944
 0.00337, 0.00778
 0.00168, 0.00558
 0.00056, 0.00328
 0.00000, 0.00000
 0.00000, 0.00000
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 0.00680,-0.00221
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 0.01203,-0.00285
 0.01380,-0.00303
 0.01559,-0.00320
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 0.02473,-0.00398
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 0.03039,-0.00443
 0.03231,-0.00458
 0.03424,-0.00473
 0.03618,-0.00488
 0.03815,-0.00503
 0.04012,-0.00518
 0.04212,-0.00533
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 0.04615,-0.00562
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 0.05026,-0.00592
 0.05233,-0.00610
 0.05442,-0.00627
 0.05653,-0.00644
 0.05866,-0.00660
 0.06081,-0.00676
 0.06297,-0.00691
 0.06515,-0.00706
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 0.07405,-0.00756
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 0.08093,-0.00773
 0.08326,-0.00777
 0.08561,-0.00780
 0.08798,-0.00783
 0.09037,-0.00785
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 0.10769,-0.00804
 0.11025,-0.00809
 0.11283,-0.00815
 0.11544,-0.00820
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 0.14280,-0.00876
 0.14568,-0.00882
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 0.15150,-0.00892
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 0.15743,-0.00901
 0.16044,-0.00905
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 0.16963,-0.00917
 0.17275,-0.00921
 0.17590,-0.00925
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 1.00000, 0.00000