ファイルインデックス名　: File Index Name        : 0257        .A  
翼型整理番号　　　　　　: Airfoil Serial No.     : D03-0002-1
翼型名　　　　　　　　　: Airfoil Name           : D.G.A. 1182
翼型ファイル番号　　　　: Airfoil File No.       : 0257
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, 0.00300
 0.98671, 0.00411
 0.97362, 0.00527
 0.96072, 0.00647
 0.94801, 0.00769
 0.93549, 0.00893
 0.92315, 0.01017
 0.91099, 0.01139
 0.89900, 0.01259
 0.88719, 0.01368
 0.87554, 0.01473
 0.86406, 0.01573
 0.85274, 0.01670
 0.84158, 0.01764
 0.83058, 0.01854
 0.81973, 0.01943
 0.80903, 0.02028
 0.79848, 0.02113
 0.78808, 0.02200
 0.77781, 0.02286
 0.76769, 0.02370
 0.75770, 0.02452
 0.74785, 0.02532
 0.73814, 0.02609
 0.72855, 0.02684
 0.71909, 0.02757
 0.70976, 0.02828
 0.70055, 0.02896
 0.69146, 0.02958
 0.68249, 0.03017
 0.67363, 0.03074
 0.66490, 0.03129
 0.65627, 0.03182
 0.64776, 0.03233
 0.63935, 0.03282
 0.63106, 0.03330
 0.62287, 0.03376
 0.61478, 0.03420
 0.60680, 0.03464
 0.59891, 0.03506
 0.59112, 0.03550
 0.58344, 0.03592
 0.57584, 0.03633
 0.56834, 0.03673
 0.56094, 0.03712
 0.55362, 0.03749
 0.54639, 0.03786
 0.53925, 0.03821
 0.53220, 0.03855
 0.52523, 0.03888
 0.51835, 0.03920
 0.51155, 0.03950
 0.50483, 0.03979
 0.49819, 0.04007
 0.49163, 0.04034
 0.48514, 0.04059
 0.47874, 0.04083
 0.47240, 0.04106
 0.46614, 0.04128
 0.45996, 0.04148
 0.45384, 0.04168
 0.44780, 0.04187
 0.44182, 0.04204
 0.43591, 0.04220
 0.43007, 0.04236
 0.42430, 0.04250
 0.41859, 0.04263
 0.41295, 0.04275
 0.40737, 0.04287
 0.40185, 0.04297
 0.39639, 0.04305
 0.39099, 0.04312
 0.38566, 0.04318
 0.38038, 0.04324
 0.37516, 0.04328
 0.37000, 0.04332
 0.36489, 0.04334
 0.35984, 0.04336
 0.35484, 0.04337
 0.34990, 0.04337
 0.34501, 0.04337
 0.34017, 0.04336
 0.33538, 0.04334
 0.33065, 0.04332
 0.32596, 0.04329
 0.32133, 0.04325
 0.31674, 0.04321
 0.31220, 0.04316
 0.30771, 0.04311
 0.30326, 0.04305
 0.29887, 0.04303
 0.29451, 0.04313
 0.29020, 0.04322
 0.28594, 0.04331
 0.28172, 0.04339
 0.27754, 0.04345
 0.27340, 0.04351
 0.26931, 0.04355
 0.26526, 0.04358
 0.26125, 0.04358
 0.25728, 0.04357
 0.25334, 0.04354
 0.24945, 0.04349
 0.24560, 0.04342
 0.24178, 0.04332
 0.23800, 0.04320
 0.23426, 0.04305
 0.23056, 0.04287
 0.22689, 0.04267
 0.22326, 0.04243
 0.21966, 0.04216
 0.21610, 0.04186
 0.21257, 0.04153
 0.20907, 0.04115
 0.20561, 0.04075
 0.20218, 0.04030
 0.19879, 0.03966
 0.19542, 0.03871
 0.19209, 0.03775
 0.18879, 0.03679
 0.18552, 0.03583
 0.18228, 0.03488
 0.17908, 0.03395
 0.17590, 0.03303
 0.17275, 0.03212
 0.16963, 0.03125
 0.16654, 0.03041
 0.16348, 0.02960
 0.16044, 0.02883
 0.15743, 0.02810
 0.15445, 0.02742
 0.15150, 0.02680
 0.14858, 0.02650
 0.14568, 0.02655
 0.14280, 0.02666
 0.13996, 0.02682
 0.13713, 0.02702
 0.13434, 0.02727
 0.13157, 0.02754
 0.12882, 0.02784
 0.12610, 0.02816
 0.12340, 0.02849
 0.12072, 0.02883
 0.11807, 0.02917
 0.11544, 0.02950
 0.11283, 0.02982
 0.11025, 0.03012
 0.10769, 0.03039
 0.10515, 0.03063
 0.10264, 0.03084
 0.10014, 0.03099
 0.09767, 0.03082
 0.09521, 0.03059
 0.09278, 0.03035
 0.09037, 0.03008
 0.08798, 0.02980
 0.08561, 0.02950
 0.08326, 0.02918
 0.08093, 0.02886
 0.07862, 0.02853
 0.07633, 0.02820
 0.07405, 0.02790
 0.07180, 0.02765
 0.06956, 0.02741
 0.06735, 0.02716
 0.06515, 0.02692
 0.06297, 0.02667
 0.06081, 0.02642
 0.05866, 0.02616
 0.05653, 0.02589
 0.05442, 0.02562
 0.05233, 0.02533
 0.05026, 0.02504
 0.04820, 0.02468
 0.04615, 0.02431
 0.04413, 0.02391
 0.04212, 0.02350
 0.04012, 0.02307
 0.03815, 0.02263
 0.03618, 0.02216
 0.03424, 0.02167
 0.03231, 0.02117
 0.03039, 0.02064
 0.02849, 0.02009
 0.02660, 0.01951
 0.02473, 0.01891
 0.02287, 0.01829
 0.02103, 0.01764
 0.01920, 0.01696
 0.01739, 0.01623
 0.01559, 0.01546
 0.01380, 0.01464
 0.01203, 0.01376
 0.01027, 0.01280
 0.00853, 0.01175
 0.00680, 0.01057
 0.00508, 0.00921
 0.00337, 0.00758
 0.00168, 0.00541
 0.00056, 0.00316
 0.00000, 0.00000
 0.00000, 0.00000
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 0.00168,-0.00196
 0.00337,-0.00279
 0.00508,-0.00344
 0.00680,-0.00400
 0.00853,-0.00450
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 0.01380,-0.00580
 0.01559,-0.00619
 0.01739,-0.00656
 0.01920,-0.00692
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 0.02287,-0.00761
 0.02473,-0.00795
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 0.02849,-0.00863
 0.03039,-0.00896
 0.03231,-0.00929
 0.03424,-0.00961
 0.03618,-0.00993
 0.03815,-0.01024
 0.04012,-0.01055
 0.04212,-0.01086
 0.04413,-0.01116
 0.04615,-0.01145
 0.04820,-0.01175
 0.05026,-0.01204
 0.05233,-0.01232
 0.05442,-0.01260
 0.05653,-0.01288
 0.05866,-0.01315
 0.06081,-0.01342
 0.06297,-0.01368
 0.06515,-0.01394
 0.06735,-0.01419
 0.06956,-0.01443
 0.07180,-0.01467
 0.07405,-0.01490
 0.07633,-0.01513
 0.07862,-0.01534
 0.08093,-0.01554
 0.08326,-0.01574
 0.08561,-0.01594
 0.08798,-0.01613
 0.09037,-0.01631
 0.09278,-0.01649
 0.09521,-0.01667
 0.09767,-0.01684
 0.10014,-0.01701
 0.10264,-0.01717
 0.10515,-0.01733
 0.10769,-0.01749
 0.11025,-0.01764
 0.11283,-0.01779
 0.11544,-0.01794
 0.11807,-0.01808
 0.12072,-0.01822
 0.12340,-0.01835
 0.12610,-0.01848
 0.12882,-0.01861
 0.13157,-0.01874
 0.13434,-0.01886
 0.13713,-0.01899
 0.13996,-0.01911
 0.14280,-0.01922
 0.14568,-0.01934
 0.14858,-0.01945
 0.15150,-0.01956
 0.15445,-0.01966
 0.15743,-0.01977
 0.16044,-0.01987
 0.16348,-0.01997
 0.16654,-0.02007
 0.16963,-0.02017
 0.17275,-0.02026
 0.17590,-0.02036
 0.17908,-0.02045
 0.18228,-0.02054
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 0.26526,-0.02243
 0.26931,-0.02251
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 0.31674,-0.02327
 0.32133,-0.02334
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 0.35984,-0.02380
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 1.00000, 0.00000