ファイルインデックス名　: File Index Name        : 0751        .A  
翼型整理番号　　　　　　: Airfoil Serial No.     : N09-0024-1
翼型名　　　　　　　　　: Airfoil Name           : Naylor & Griffiths 24
翼型ファイル番号　　　　: Airfoil File No.       : 0751
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, 0.00796
 0.97362, 0.01441
 0.96072, 0.01954
 0.94801, 0.02357
 0.93549, 0.02666
 0.92315, 0.02900
 0.91099, 0.03076
 0.89900, 0.03217
 0.88719, 0.03413
 0.87554, 0.03601
 0.86406, 0.03782
 0.85274, 0.03954
 0.84158, 0.04120
 0.83058, 0.04279
 0.81973, 0.04432
 0.80903, 0.04579
 0.79848, 0.04720
 0.78808, 0.04859
 0.77781, 0.04992
 0.76769, 0.05121
 0.75770, 0.05244
 0.74785, 0.05363
 0.73814, 0.05478
 0.72855, 0.05588
 0.71909, 0.05694
 0.70976, 0.05796
 0.70055, 0.05894
 0.69146, 0.05990
 0.68249, 0.06082
 0.67363, 0.06170
 0.66490, 0.06254
 0.65627, 0.06335
 0.64776, 0.06413
 0.63935, 0.06487
 0.63106, 0.06558
 0.62287, 0.06625
 0.61478, 0.06689
 0.60680, 0.06750
 0.59891, 0.06807
 0.59112, 0.06857
 0.58344, 0.06904
 0.57584, 0.06948
 0.56834, 0.06990
 0.56094, 0.07029
 0.55362, 0.07067
 0.54639, 0.07102
 0.53925, 0.07135
 0.53220, 0.07167
 0.52523, 0.07198
 0.51835, 0.07227
 0.51155, 0.07254
 0.50483, 0.07281
 0.49819, 0.07309
 0.49163, 0.07340
 0.48514, 0.07370
 0.47874, 0.07399
 0.47240, 0.07428
 0.46614, 0.07455
 0.45996, 0.07482
 0.45384, 0.07508
 0.44780, 0.07533
 0.44182, 0.07557
 0.43591, 0.07579
 0.43007, 0.07601
 0.42430, 0.07622
 0.41859, 0.07642
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 0.40737, 0.07678
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 0.38566, 0.07736
 0.38038, 0.07747
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 0.34017, 0.07800
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 0.33065, 0.07802
 0.32596, 0.07802
 0.32133, 0.07801
 0.31674, 0.07798
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 0.24178, 0.07626
 0.23800, 0.07610
 0.23426, 0.07594
 0.23056, 0.07577
 0.22689, 0.07559
 0.22326, 0.07540
 0.21966, 0.07521
 0.21610, 0.07501
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 0.19879, 0.07392
 0.19542, 0.07368
 0.19209, 0.07343
 0.18879, 0.07318
 0.18552, 0.07292
 0.18228, 0.07265
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 0.17590, 0.07210
 0.17275, 0.07181
 0.16963, 0.07151
 0.16654, 0.07121
 0.16348, 0.07090
 0.16044, 0.07058
 0.15743, 0.07025
 0.15445, 0.06992
 0.15150, 0.06958
 0.14858, 0.06923
 0.14568, 0.06886
 0.14280, 0.06849
 0.13996, 0.06811
 0.13713, 0.06772
 0.13434, 0.06733
 0.13157, 0.06692
 0.12882, 0.06651
 0.12610, 0.06609
 0.12340, 0.06566
 0.12072, 0.06523
 0.11807, 0.06478
 0.11544, 0.06433
 0.11283, 0.06387
 0.11025, 0.06340
 0.10769, 0.06292
 0.10515, 0.06243
 0.10264, 0.06193
 0.10014, 0.06143
 0.09767, 0.06094
 0.09521, 0.06044
 0.09278, 0.05993
 0.09037, 0.05941
 0.08798, 0.05886
 0.08561, 0.05831
 0.08326, 0.05773
 0.08093, 0.05714
 0.07862, 0.05652
 0.07633, 0.05588
 0.07405, 0.05520
 0.07180, 0.05448
 0.06956, 0.05373
 0.06735, 0.05296
 0.06515, 0.05216
 0.06297, 0.05134
 0.06081, 0.05050
 0.05866, 0.04963
 0.05653, 0.04873
 0.05442, 0.04782
 0.05233, 0.04688
 0.05026, 0.04592
 0.04820, 0.04492
 0.04615, 0.04389
 0.04413, 0.04284
 0.04212, 0.04176
 0.04012, 0.04066
 0.03815, 0.03955
 0.03618, 0.03841
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 0.03231, 0.03609
 0.03039, 0.03490
 0.02849, 0.03369
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 0.02473, 0.03123
 0.02287, 0.03004
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 0.01920, 0.02759
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 0.01559, 0.02497
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 0.00853, 0.01881
 0.00680, 0.01691
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 0.00337, 0.01214
 0.00168, 0.00871
 0.00056, 0.00511
 0.00000, 0.00000
 0.00000, 0.00000
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 1.00000, 0.00000