ファイルインデックス名　: File Index Name        : 0156        .A  
翼型整理番号　　　　　　: Airfoil Serial No.     : A00-0001-1
翼型名　　　　　　　　　: Airfoil Name           : A.D.I.
翼型ファイル番号　　　　: Airfoil File No.       : 0156
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, 0.00382
 0.97362, 0.00729
 0.96072, 0.01045
 0.94801, 0.01333
 0.93549, 0.01594
 0.92315, 0.01831
 0.91099, 0.02047
 0.89900, 0.02244
 0.88719, 0.02424
 0.87554, 0.02589
 0.86406, 0.02741
 0.85274, 0.02882
 0.84158, 0.03014
 0.83058, 0.03137
 0.81973, 0.03259
 0.80903, 0.03385
 0.79848, 0.03506
 0.78808, 0.03622
 0.77781, 0.03735
 0.76769, 0.03844
 0.75770, 0.03949
 0.74785, 0.04050
 0.73814, 0.04149
 0.72855, 0.04245
 0.71909, 0.04339
 0.70976, 0.04430
 0.70055, 0.04519
 0.69146, 0.04605
 0.68249, 0.04689
 0.67363, 0.04771
 0.66490, 0.04851
 0.65627, 0.04929
 0.64776, 0.05005
 0.63935, 0.05082
 0.63106, 0.05158
 0.62287, 0.05232
 0.61478, 0.05304
 0.60680, 0.05374
 0.59891, 0.05442
 0.59112, 0.05508
 0.58344, 0.05572
 0.57584, 0.05634
 0.56834, 0.05693
 0.56094, 0.05750
 0.55362, 0.05804
 0.54639, 0.05855
 0.53925, 0.05903
 0.53220, 0.05949
 0.52523, 0.05993
 0.51835, 0.06034
 0.51155, 0.06074
 0.50483, 0.06111
 0.49819, 0.06146
 0.49163, 0.06179
 0.48514, 0.06210
 0.47874, 0.06239
 0.47240, 0.06266
 0.46614, 0.06291
 0.45996, 0.06312
 0.45384, 0.06332
 0.44780, 0.06350
 0.44182, 0.06367
 0.43591, 0.06382
 0.43007, 0.06395
 0.42430, 0.06406
 0.41859, 0.06416
 0.41295, 0.06425
 0.40737, 0.06432
 0.40185, 0.06438
 0.39639, 0.06443
 0.39099, 0.06447
 0.38566, 0.06449
 0.38038, 0.06450
 0.37516, 0.06450
 0.37000, 0.06449
 0.36489, 0.06448
 0.35984, 0.06445
 0.35484, 0.06441
 0.34990, 0.06436
 0.34501, 0.06431
 0.34017, 0.06424
 0.33538, 0.06417
 0.33065, 0.06409
 0.32596, 0.06400
 0.32133, 0.06390
 0.31674, 0.06379
 0.31220, 0.06369
 0.30771, 0.06358
 0.30326, 0.06347
 0.29887, 0.06334
 0.29451, 0.06321
 0.29020, 0.06307
 0.28594, 0.06292
 0.28172, 0.06277
 0.27754, 0.06261
 0.27340, 0.06244
 0.26931, 0.06226
 0.26526, 0.06207
 0.26125, 0.06188
 0.25728, 0.06168
 0.25334, 0.06146
 0.24945, 0.06123
 0.24560, 0.06099
 0.24178, 0.06075
 0.23800, 0.06049
 0.23426, 0.06023
 0.23056, 0.05996
 0.22689, 0.05968
 0.22326, 0.05940
 0.21966, 0.05911
 0.21610, 0.05881
 0.21257, 0.05850
 0.20907, 0.05819
 0.20561, 0.05787
 0.20218, 0.05754
 0.19879, 0.05721
 0.19542, 0.05687
 0.19209, 0.05652
 0.18879, 0.05617
 0.18552, 0.05582
 0.18228, 0.05546
 0.17908, 0.05510
 0.17590, 0.05473
 0.17275, 0.05436
 0.16963, 0.05398
 0.16654, 0.05359
 0.16348, 0.05319
 0.16044, 0.05279
 0.15743, 0.05238
 0.15445, 0.05197
 0.15150, 0.05154
 0.14858, 0.05112
 0.14568, 0.05068
 0.14280, 0.05024
 0.13996, 0.04979
 0.13713, 0.04933
 0.13434, 0.04887
 0.13157, 0.04839
 0.12882, 0.04791
 0.12610, 0.04742
 0.12340, 0.04690
 0.12072, 0.04637
 0.11807, 0.04583
 0.11544, 0.04529
 0.11283, 0.04473
 0.11025, 0.04417
 0.10769, 0.04360
 0.10515, 0.04303
 0.10264, 0.04244
 0.10014, 0.04185
 0.09767, 0.04125
 0.09521, 0.04064
 0.09278, 0.04003
 0.09037, 0.03941
 0.08798, 0.03878
 0.08561, 0.03815
 0.08326, 0.03750
 0.08093, 0.03686
 0.07862, 0.03620
 0.07633, 0.03553
 0.07405, 0.03486
 0.07180, 0.03418
 0.06956, 0.03350
 0.06735, 0.03280
 0.06515, 0.03210
 0.06297, 0.03139
 0.06081, 0.03066
 0.05866, 0.02991
 0.05653, 0.02916
 0.05442, 0.02841
 0.05233, 0.02765
 0.05026, 0.02688
 0.04820, 0.02610
 0.04615, 0.02531
 0.04413, 0.02452
 0.04212, 0.02372
 0.04012, 0.02291
 0.03815, 0.02210
 0.03618, 0.02128
 0.03424, 0.02045
 0.03231, 0.01961
 0.03039, 0.01876
 0.02849, 0.01791
 0.02660, 0.01704
 0.02473, 0.01616
 0.02287, 0.01527
 0.02103, 0.01437
 0.01920, 0.01346
 0.01739, 0.01253
 0.01559, 0.01159
 0.01380, 0.01062
 0.01203, 0.00963
 0.01027, 0.00862
 0.00853, 0.00757
 0.00680, 0.00648
 0.00508, 0.00532
 0.00337, 0.00406
 0.00168, 0.00261
 0.00056, 0.00136
 0.00000, 0.00000
 0.00000, 0.00000
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 0.00168,-0.00391
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 0.00680,-0.00702
 0.00853,-0.00764
 0.01027,-0.00816
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 0.01559,-0.00937
 0.01739,-0.00968
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 0.02287,-0.01046
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 0.03039,-0.01120
 0.03231,-0.01135
 0.03424,-0.01149
 0.03618,-0.01162
 0.03815,-0.01174
 0.04012,-0.01185
 0.04212,-0.01195
 0.04413,-0.01205
 0.04615,-0.01214
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 0.05026,-0.01230
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 0.05442,-0.01244
 0.05653,-0.01251
 0.05866,-0.01257
 0.06081,-0.01263
 0.06297,-0.01269
 0.06515,-0.01276
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 0.07405,-0.01305
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 0.07862,-0.01319
 0.08093,-0.01325
 0.08326,-0.01332
 0.08561,-0.01338
 0.08798,-0.01345
 0.09037,-0.01351
 0.09278,-0.01357
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 0.09767,-0.01369
 0.10014,-0.01375
 0.10264,-0.01381
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 0.10769,-0.01392
 0.11025,-0.01398
 0.11283,-0.01403
 0.11544,-0.01409
 0.11807,-0.01414
 0.12072,-0.01419
 0.12340,-0.01424
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 0.13996,-0.01452
 0.14280,-0.01456
 0.14568,-0.01461
 0.14858,-0.01465
 0.15150,-0.01469
 0.15445,-0.01473
 0.15743,-0.01477
 0.16044,-0.01482
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 0.16654,-0.01490
 0.16963,-0.01494
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 0.17590,-0.01502
 0.17908,-0.01506
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 0.26526,-0.01612
 0.26931,-0.01616
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 0.31220,-0.01648
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 0.32133,-0.01651
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 0.33538,-0.01653
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 0.49163,-0.01617
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 1.00000, 0.00000