ファイルインデックス名　: File Index Name        : 0291        .A  
翼型整理番号　　　　　　: Airfoil Serial No.     : A01-0001-1
翼型名　　　　　　　　　: Airfoil Name           : A.D. No.1
翼型ファイル番号　　　　: Airfoil File No.       : 0291
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, 0.00332
 0.97362, 0.00629
 0.96072, 0.00896
 0.94801, 0.01136
 0.93549, 0.01355
 0.92315, 0.01555
 0.91099, 0.01740
 0.89900, 0.01916
 0.88719, 0.02103
 0.87554, 0.02286
 0.86406, 0.02464
 0.85274, 0.02637
 0.84158, 0.02805
 0.83058, 0.02968
 0.81973, 0.03125
 0.80903, 0.03276
 0.79848, 0.03419
 0.78808, 0.03549
 0.77781, 0.03673
 0.76769, 0.03791
 0.75770, 0.03904
 0.74785, 0.04012
 0.73814, 0.04116
 0.72855, 0.04216
 0.71909, 0.04313
 0.70976, 0.04405
 0.70055, 0.04495
 0.69146, 0.04585
 0.68249, 0.04672
 0.67363, 0.04757
 0.66490, 0.04839
 0.65627, 0.04918
 0.64776, 0.04995
 0.63935, 0.05070
 0.63106, 0.05142
 0.62287, 0.05212
 0.61478, 0.05280
 0.60680, 0.05345
 0.59891, 0.05409
 0.59112, 0.05473
 0.58344, 0.05534
 0.57584, 0.05594
 0.56834, 0.05651
 0.56094, 0.05706
 0.55362, 0.05760
 0.54639, 0.05811
 0.53925, 0.05860
 0.53220, 0.05907
 0.52523, 0.05952
 0.51835, 0.05994
 0.51155, 0.06035
 0.50483, 0.06073
 0.49819, 0.06109
 0.49163, 0.06140
 0.48514, 0.06170
 0.47874, 0.06197
 0.47240, 0.06223
 0.46614, 0.06246
 0.45996, 0.06268
 0.45384, 0.06288
 0.44780, 0.06307
 0.44182, 0.06323
 0.43591, 0.06338
 0.43007, 0.06352
 0.42430, 0.06364
 0.41859, 0.06374
 0.41295, 0.06384
 0.40737, 0.06392
 0.40185, 0.06398
 0.39639, 0.06404
 0.39099, 0.06408
 0.38566, 0.06412
 0.38038, 0.06414
 0.37516, 0.06415
 0.37000, 0.06415
 0.36489, 0.06414
 0.35984, 0.06412
 0.35484, 0.06409
 0.34990, 0.06404
 0.34501, 0.06399
 0.34017, 0.06393
 0.33538, 0.06386
 0.33065, 0.06378
 0.32596, 0.06369
 0.32133, 0.06359
 0.31674, 0.06348
 0.31220, 0.06336
 0.30771, 0.06324
 0.30326, 0.06310
 0.29887, 0.06296
 0.29451, 0.06280
 0.29020, 0.06264
 0.28594, 0.06246
 0.28172, 0.06228
 0.27754, 0.06210
 0.27340, 0.06190
 0.26931, 0.06170
 0.26526, 0.06150
 0.26125, 0.06128
 0.25728, 0.06107
 0.25334, 0.06084
 0.24945, 0.06061
 0.24560, 0.06038
 0.24178, 0.06013
 0.23800, 0.05989
 0.23426, 0.05964
 0.23056, 0.05938
 0.22689, 0.05912
 0.22326, 0.05886
 0.21966, 0.05859
 0.21610, 0.05832
 0.21257, 0.05804
 0.20907, 0.05776
 0.20561, 0.05747
 0.20218, 0.05719
 0.19879, 0.05691
 0.19542, 0.05665
 0.19209, 0.05639
 0.18879, 0.05612
 0.18552, 0.05584
 0.18228, 0.05556
 0.17908, 0.05526
 0.17590, 0.05496
 0.17275, 0.05465
 0.16963, 0.05433
 0.16654, 0.05401
 0.16348, 0.05367
 0.16044, 0.05332
 0.15743, 0.05296
 0.15445, 0.05258
 0.15150, 0.05220
 0.14858, 0.05179
 0.14568, 0.05134
 0.14280, 0.05087
 0.13996, 0.05040
 0.13713, 0.04992
 0.13434, 0.04942
 0.13157, 0.04891
 0.12882, 0.04839
 0.12610, 0.04786
 0.12340, 0.04732
 0.12072, 0.04677
 0.11807, 0.04621
 0.11544, 0.04564
 0.11283, 0.04506
 0.11025, 0.04447
 0.10769, 0.04388
 0.10515, 0.04327
 0.10264, 0.04266
 0.10014, 0.04204
 0.09767, 0.04141
 0.09521, 0.04078
 0.09278, 0.04014
 0.09037, 0.03950
 0.08798, 0.03884
 0.08561, 0.03817
 0.08326, 0.03750
 0.08093, 0.03681
 0.07862, 0.03612
 0.07633, 0.03542
 0.07405, 0.03469
 0.07180, 0.03395
 0.06956, 0.03319
 0.06735, 0.03243
 0.06515, 0.03166
 0.06297, 0.03088
 0.06081, 0.03010
 0.05866, 0.02930
 0.05653, 0.02851
 0.05442, 0.02771
 0.05233, 0.02691
 0.05026, 0.02610
 0.04820, 0.02531
 0.04615, 0.02451
 0.04413, 0.02372
 0.04212, 0.02293
 0.04012, 0.02213
 0.03815, 0.02134
 0.03618, 0.02055
 0.03424, 0.01977
 0.03231, 0.01898
 0.03039, 0.01820
 0.02849, 0.01743
 0.02660, 0.01665
 0.02473, 0.01590
 0.02287, 0.01519
 0.02103, 0.01448
 0.01920, 0.01377
 0.01739, 0.01305
 0.01559, 0.01232
 0.01380, 0.01157
 0.01203, 0.01079
 0.01027, 0.00998
 0.00853, 0.00911
 0.00680, 0.00816
 0.00508, 0.00710
 0.00337, 0.00584
 0.00168, 0.00418
 0.00056, 0.00246
 0.00000, 0.00000
 0.00000, 0.00000
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 0.00168,-0.00352
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 0.00680,-0.00637
 0.00853,-0.00696
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 0.01559,-0.00863
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 0.03424,-0.01093
 0.03618,-0.01109
 0.03815,-0.01124
 0.04012,-0.01139
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 0.04615,-0.01178
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 0.05442,-0.01221
 0.05653,-0.01230
 0.05866,-0.01239
 0.06081,-0.01247
 0.06297,-0.01256
 0.06515,-0.01264
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 0.07405,-0.01297
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 0.08093,-0.01325
 0.08326,-0.01335
 0.08561,-0.01345
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 0.09037,-0.01364
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 0.09767,-0.01392
 0.10014,-0.01400
 0.10264,-0.01408
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 0.10769,-0.01423
 0.11025,-0.01430
 0.11283,-0.01437
 0.11544,-0.01443
 0.11807,-0.01450
 0.12072,-0.01456
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 0.13996,-0.01489
 0.14280,-0.01492
 0.14568,-0.01496
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 0.15150,-0.01501
 0.15445,-0.01502
 0.15743,-0.01503
 0.16044,-0.01503
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 0.16654,-0.01504
 0.16963,-0.01504
 0.17275,-0.01504
 0.17590,-0.01503
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 0.24945,-0.01549
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 0.26526,-0.01566
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 0.33538,-0.01605
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 1.00000, 0.00000