ファイルインデックス名　: File Index Name        : 1004        .A00
翼型整理番号　　　　　　: Airfoil Serial No.     : N01-0004-0
翼型名　　　　　　　　　: Airfoil Name           : N.A.C.A. 0009
翼型ファイル番号　　　　: Airfoil File No.       : 1004
翼型情報　　　　　　　　: Airfoil Information    : Computed

算出前縁半径　　　　　　: Computed L.E.R.        : 0.893 %
算出前縁傾斜　　　　　　: Computed Slope of L.E. : 0
算出プログラム番号　　　: Computed Program No.   : ウハク-40


座標　　　　　　　　　　: Plot Ordinates         :

 X             Y

 1.00000, 0.00094
 0.98671, 0.00233
 0.97362, 0.00368
 0.96072, 0.00498
 0.94801, 0.00625
 0.93549, 0.00747
 0.92315, 0.00867
 0.91099, 0.00983
 0.89900, 0.01095
 0.88719, 0.01205
 0.87554, 0.01311
 0.86406, 0.01415
 0.85274, 0.01515
 0.84158, 0.01613
 0.83058, 0.01709
 0.81973, 0.01801
 0.80903, 0.01892
 0.79848, 0.01980
 0.78808, 0.02066
 0.77781, 0.02149
 0.76769, 0.02231
 0.75770, 0.02310
 0.74785, 0.02387
 0.73814, 0.02462
 0.72855, 0.02535
 0.71909, 0.02607
 0.70976, 0.02676
 0.70055, 0.02744
 0.69146, 0.02810
 0.68249, 0.02874
 0.67363, 0.02937
 0.66490, 0.02998
 0.65627, 0.03057
 0.64776, 0.03114
 0.63935, 0.03171
 0.63106, 0.03225
 0.62287, 0.03278
 0.61478, 0.03330
 0.60680, 0.03380
 0.59891, 0.03429
 0.59112, 0.03477
 0.58344, 0.03523
 0.57584, 0.03568
 0.56834, 0.03611
 0.56094, 0.03653
 0.55362, 0.03694
 0.54639, 0.03734
 0.53925, 0.03773
 0.53220, 0.03810
 0.52523, 0.03846
 0.51835, 0.03881
 0.51155, 0.03915
 0.50483, 0.03947
 0.49819, 0.03979
 0.49163, 0.04010
 0.48514, 0.04039
 0.47874, 0.04067
 0.47240, 0.04095
 0.46614, 0.04121
 0.45996, 0.04146
 0.45384, 0.04171
 0.44780, 0.04194
 0.44182, 0.04216
 0.43591, 0.04238
 0.43007, 0.04258
 0.42430, 0.04278
 0.41859, 0.04296
 0.41295, 0.04314
 0.40737, 0.04331
 0.40185, 0.04347
 0.39639, 0.04362
 0.39099, 0.04376
 0.38566, 0.04390
 0.38038, 0.04403
 0.37516, 0.04414
 0.37000, 0.04425
 0.36489, 0.04436
 0.35984, 0.04445
 0.35484, 0.04454
 0.34990, 0.04462
 0.34501, 0.04469
 0.34017, 0.04475
 0.33538, 0.04481
 0.33065, 0.04486
 0.32596, 0.04490
 0.32133, 0.04494
 0.31674, 0.04497
 0.31220, 0.04499
 0.30771, 0.04500
 0.30326, 0.04501
 0.29887, 0.04501
 0.29451, 0.04501
 0.29020, 0.04500
 0.28594, 0.04498
 0.28172, 0.04496
 0.27754, 0.04493
 0.27340, 0.04489
 0.26931, 0.04485
 0.26526, 0.04480
 0.26125, 0.04475
 0.25728, 0.04469
 0.25334, 0.04462
 0.24945, 0.04455
 0.24560, 0.04447
 0.24178, 0.04439
 0.23800, 0.04430
 0.23426, 0.04421
 0.23056, 0.04411
 0.22689, 0.04400
 0.22326, 0.04389
 0.21966, 0.04378
 0.21610, 0.04366
 0.21257, 0.04353
 0.20907, 0.04340
 0.20561, 0.04327
 0.20218, 0.04312
 0.19879, 0.04298
 0.19542, 0.04283
 0.19209, 0.04267
 0.18879, 0.04251
 0.18552, 0.04234
 0.18228, 0.04217
 0.17908, 0.04200
 0.17590, 0.04182
 0.17275, 0.04163
 0.16963, 0.04144
 0.16654, 0.04125
 0.16348, 0.04105
 0.16044, 0.04084
 0.15743, 0.04063
 0.15445, 0.04042
 0.15150, 0.04020
 0.14858, 0.03998
 0.14568, 0.03975
 0.14280, 0.03952
 0.13996, 0.03928
 0.13713, 0.03904
 0.13434, 0.03879
 0.13157, 0.03854
 0.12882, 0.03828
 0.12610, 0.03802
 0.12340, 0.03776
 0.12072, 0.03749
 0.11807, 0.03721
 0.11544, 0.03693
 0.11283, 0.03664
 0.11025, 0.03635
 0.10769, 0.03606
 0.10515, 0.03576
 0.10264, 0.03545
 0.10014, 0.03514
 0.09767, 0.03482
 0.09521, 0.03450
 0.09278, 0.03417
 0.09037, 0.03384
 0.08798, 0.03350
 0.08561, 0.03316
 0.08326, 0.03281
 0.08093, 0.03245
 0.07862, 0.03209
 0.07633, 0.03172
 0.07405, 0.03134
 0.07180, 0.03096
 0.06956, 0.03057
 0.06735, 0.03017
 0.06515, 0.02977
 0.06297, 0.02936
 0.06081, 0.02894
 0.05866, 0.02851
 0.05653, 0.02808
 0.05442, 0.02763
 0.05233, 0.02718
 0.05026, 0.02672
 0.04820, 0.02625
 0.04615, 0.02576
 0.04413, 0.02527
 0.04212, 0.02476
 0.04012, 0.02424
 0.03815, 0.02371
 0.03618, 0.02316
 0.03424, 0.02260
 0.03231, 0.02202
 0.03039, 0.02143
 0.02849, 0.02081
 0.02660, 0.02017
 0.02473, 0.01951
 0.02287, 0.01883
 0.02103, 0.01811
 0.01920, 0.01737
 0.01739, 0.01659
 0.01559, 0.01576
 0.01380, 0.01489
 0.01203, 0.01395
 0.01027, 0.01294
 0.00853, 0.01184
 0.00680, 0.01062
 0.00508, 0.00923
 0.00337, 0.00757
 0.00168, 0.00538
 0.00056, 0.00313
 0.00000, 0.00000
 0.00000, 0.00000
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 0.03231,-0.02202
 0.03424,-0.02260
 0.03618,-0.02316
 0.03815,-0.02371
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 0.05442,-0.02763
 0.05653,-0.02808
 0.05866,-0.02851
 0.06081,-0.02894
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 0.06515,-0.02977
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 0.08093,-0.03245
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 0.08561,-0.03316
 0.08798,-0.03350
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 0.10264,-0.03545
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 0.10769,-0.03606
 0.11025,-0.03635
 0.11283,-0.03664
 0.11544,-0.03693
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 0.14280,-0.03952
 0.14568,-0.03975
 0.14858,-0.03998
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