ファイルインデックス名　: File Index Name        : 0737        .A01
翼型整理番号　　　　　　: Airfoil Serial No.     : N09-0010-1
翼型名　　　　　　　　　: Airfoil Name           : Naylor & Griffiths 10
翼型ファイル番号　　　　: Airfoil File No.       : 0737
翼型情報　　　　　　　　: Airfoil Information    : (B.1)

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, 0.00574
 0.97362, 0.01036
 0.96072, 0.01404
 0.94801, 0.01690
 0.93549, 0.01909
 0.92315, 0.02073
 0.91099, 0.02195
 0.89900, 0.02292
 0.88719, 0.02430
 0.87554, 0.02562
 0.86406, 0.02689
 0.85274, 0.02811
 0.84158, 0.02928
 0.83058, 0.03041
 0.81973, 0.03149
 0.80903, 0.03254
 0.79848, 0.03355
 0.78808, 0.03454
 0.77781, 0.03551
 0.76769, 0.03644
 0.75770, 0.03733
 0.74785, 0.03820
 0.73814, 0.03903
 0.72855, 0.03983
 0.71909, 0.04060
 0.70976, 0.04134
 0.70055, 0.04206
 0.69146, 0.04274
 0.68249, 0.04338
 0.67363, 0.04401
 0.66490, 0.04460
 0.65627, 0.04518
 0.64776, 0.04572
 0.63935, 0.04625
 0.63106, 0.04675
 0.62287, 0.04723
 0.61478, 0.04770
 0.60680, 0.04814
 0.59891, 0.04856
 0.59112, 0.04895
 0.58344, 0.04932
 0.57584, 0.04968
 0.56834, 0.05002
 0.56094, 0.05034
 0.55362, 0.05066
 0.54639, 0.05096
 0.53925, 0.05124
 0.53220, 0.05152
 0.52523, 0.05179
 0.51835, 0.05204
 0.51155, 0.05229
 0.50483, 0.05253
 0.49819, 0.05277
 0.49163, 0.05301
 0.48514, 0.05325
 0.47874, 0.05348
 0.47240, 0.05371
 0.46614, 0.05393
 0.45996, 0.05414
 0.45384, 0.05434
 0.44780, 0.05454
 0.44182, 0.05474
 0.43591, 0.05493
 0.43007, 0.05511
 0.42430, 0.05529
 0.41859, 0.05546
 0.41295, 0.05563
 0.40737, 0.05579
 0.40185, 0.05595
 0.39639, 0.05610
 0.39099, 0.05626
 0.38566, 0.05640
 0.38038, 0.05655
 0.37516, 0.05668
 0.37000, 0.05682
 0.36489, 0.05695
 0.35984, 0.05707
 0.35484, 0.05719
 0.34990, 0.05730
 0.34501, 0.05741
 0.34017, 0.05751
 0.33538, 0.05761
 0.33065, 0.05770
 0.32596, 0.05779
 0.32133, 0.05787
 0.31674, 0.05795
 0.31220, 0.05802
 0.30771, 0.05809
 0.30326, 0.05816
 0.29887, 0.05821
 0.29451, 0.05827
 0.29020, 0.05832
 0.28594, 0.05836
 0.28172, 0.05840
 0.27754, 0.05843
 0.27340, 0.05846
 0.26931, 0.05848
 0.26526, 0.05850
 0.26125, 0.05851
 0.25728, 0.05852
 0.25334, 0.05853
 0.24945, 0.05853
 0.24560, 0.05852
 0.24178, 0.05851
 0.23800, 0.05849
 0.23426, 0.05848
 0.23056, 0.05846
 0.22689, 0.05843
 0.22326, 0.05840
 0.21966, 0.05836
 0.21610, 0.05831
 0.21257, 0.05826
 0.20907, 0.05820
 0.20561, 0.05813
 0.20218, 0.05805
 0.19879, 0.05796
 0.19542, 0.05785
 0.19209, 0.05773
 0.18879, 0.05760
 0.18552, 0.05747
 0.18228, 0.05732
 0.17908, 0.05717
 0.17590, 0.05701
 0.17275, 0.05685
 0.16963, 0.05667
 0.16654, 0.05649
 0.16348, 0.05631
 0.16044, 0.05612
 0.15743, 0.05592
 0.15445, 0.05572
 0.15150, 0.05551
 0.14858, 0.05531
 0.14568, 0.05513
 0.14280, 0.05494
 0.13996, 0.05475
 0.13713, 0.05455
 0.13434, 0.05434
 0.13157, 0.05413
 0.12882, 0.05391
 0.12610, 0.05368
 0.12340, 0.05344
 0.12072, 0.05319
 0.11807, 0.05294
 0.11544, 0.05267
 0.11283, 0.05239
 0.11025, 0.05210
 0.10769, 0.05180
 0.10515, 0.05149
 0.10264, 0.05116
 0.10014, 0.05082
 0.09767, 0.05045
 0.09521, 0.05006
 0.09278, 0.04966
 0.09037, 0.04925
 0.08798, 0.04882
 0.08561, 0.04838
 0.08326, 0.04793
 0.08093, 0.04747
 0.07862, 0.04699
 0.07633, 0.04649
 0.07405, 0.04599
 0.07180, 0.04547
 0.06956, 0.04494
 0.06735, 0.04439
 0.06515, 0.04383
 0.06297, 0.04325
 0.06081, 0.04266
 0.05866, 0.04204
 0.05653, 0.04141
 0.05442, 0.04075
 0.05233, 0.04008
 0.05026, 0.03939
 0.04820, 0.03865
 0.04615, 0.03788
 0.04413, 0.03709
 0.04212, 0.03628
 0.04012, 0.03543
 0.03815, 0.03457
 0.03618, 0.03367
 0.03424, 0.03275
 0.03231, 0.03179
 0.03039, 0.03080
 0.02849, 0.02979
 0.02660, 0.02873
 0.02473, 0.02764
 0.02287, 0.02650
 0.02103, 0.02532
 0.01920, 0.02409
 0.01739, 0.02281
 0.01559, 0.02148
 0.01380, 0.02007
 0.01203, 0.01860
 0.01027, 0.01704
 0.00853, 0.01537
 0.00680, 0.01356
 0.00508, 0.01155
 0.00337, 0.00923
 0.00168, 0.00635
 0.00056, 0.00357
 0.00000, 0.00000
 0.00000, 0.00000
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 0.03039,-0.00526
 0.03231,-0.00543
 0.03424,-0.00559
 0.03618,-0.00574
 0.03815,-0.00590
 0.04012,-0.00604
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 0.05233,-0.00684
 0.05442,-0.00695
 0.05653,-0.00706
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 0.08561,-0.00828
 0.08798,-0.00836
 0.09037,-0.00843
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 0.09767,-0.00864
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 0.10264,-0.00876
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 0.11025,-0.00892
 0.11283,-0.00897
 0.11544,-0.00901
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 0.14280,-0.00938
 0.14568,-0.00941
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 1.00000, 0.00000