ファイルインデックス名　: File Index Name        : 3090        .A  
翼型整理番号　　　　　　: Airfoil Serial No.     : G01-9017-1
翼型名　　　　　　　　　: Airfoil Name           : Go 477 mod.1
翼型ファイル番号　　　　: Airfoil File No.       : 3090
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, 0.00309
 0.97362, 0.00612
 0.96072, 0.00910
 0.94801, 0.01203
 0.93549, 0.01491
 0.92315, 0.01773
 0.91099, 0.02051
 0.89900, 0.02323
 0.88719, 0.02589
 0.87554, 0.02851
 0.86406, 0.03107
 0.85274, 0.03358
 0.84158, 0.03603
 0.83058, 0.03843
 0.81973, 0.04078
 0.80903, 0.04308
 0.79848, 0.04533
 0.78808, 0.04756
 0.77781, 0.04973
 0.76769, 0.05185
 0.75770, 0.05391
 0.74785, 0.05590
 0.73814, 0.05783
 0.72855, 0.05970
 0.71909, 0.06150
 0.70976, 0.06324
 0.70055, 0.06490
 0.69146, 0.06638
 0.68249, 0.06779
 0.67363, 0.06914
 0.66490, 0.07042
 0.65627, 0.07166
 0.64776, 0.07285
 0.63935, 0.07399
 0.63106, 0.07508
 0.62287, 0.07614
 0.61478, 0.07717
 0.60680, 0.07817
 0.59891, 0.07915
 0.59112, 0.08019
 0.58344, 0.08121
 0.57584, 0.08220
 0.56834, 0.08317
 0.56094, 0.08411
 0.55362, 0.08501
 0.54639, 0.08589
 0.53925, 0.08674
 0.53220, 0.08756
 0.52523, 0.08835
 0.51835, 0.08910
 0.51155, 0.08983
 0.50483, 0.09052
 0.49819, 0.09116
 0.49163, 0.09172
 0.48514, 0.09225
 0.47874, 0.09275
 0.47240, 0.09322
 0.46614, 0.09366
 0.45996, 0.09408
 0.45384, 0.09447
 0.44780, 0.09483
 0.44182, 0.09517
 0.43591, 0.09549
 0.43007, 0.09578
 0.42430, 0.09605
 0.41859, 0.09630
 0.41295, 0.09653
 0.40737, 0.09674
 0.40185, 0.09694
 0.39639, 0.09714
 0.39099, 0.09733
 0.38566, 0.09750
 0.38038, 0.09766
 0.37516, 0.09780
 0.37000, 0.09792
 0.36489, 0.09803
 0.35984, 0.09812
 0.35484, 0.09820
 0.34990, 0.09826
 0.34501, 0.09831
 0.34017, 0.09834
 0.33538, 0.09836
 0.33065, 0.09836
 0.32596, 0.09835
 0.32133, 0.09832
 0.31674, 0.09828
 0.31220, 0.09822
 0.30771, 0.09815
 0.30326, 0.09807
 0.29887, 0.09797
 0.29451, 0.09784
 0.29020, 0.09770
 0.28594, 0.09755
 0.28172, 0.09739
 0.27754, 0.09721
 0.27340, 0.09702
 0.26931, 0.09681
 0.26526, 0.09660
 0.26125, 0.09637
 0.25728, 0.09613
 0.25334, 0.09588
 0.24945, 0.09562
 0.24560, 0.09535
 0.24178, 0.09506
 0.23800, 0.09477
 0.23426, 0.09446
 0.23056, 0.09415
 0.22689, 0.09382
 0.22326, 0.09348
 0.21966, 0.09314
 0.21610, 0.09278
 0.21257, 0.09241
 0.20907, 0.09204
 0.20561, 0.09165
 0.20218, 0.09126
 0.19879, 0.09087
 0.19542, 0.09052
 0.19209, 0.09015
 0.18879, 0.08977
 0.18552, 0.08939
 0.18228, 0.08899
 0.17908, 0.08859
 0.17590, 0.08817
 0.17275, 0.08775
 0.16963, 0.08731
 0.16654, 0.08686
 0.16348, 0.08640
 0.16044, 0.08593
 0.15743, 0.08545
 0.15445, 0.08495
 0.15150, 0.08444
 0.14858, 0.08393
 0.14568, 0.08339
 0.14280, 0.08284
 0.13996, 0.08228
 0.13713, 0.08171
 0.13434, 0.08112
 0.13157, 0.08051
 0.12882, 0.07989
 0.12610, 0.07926
 0.12340, 0.07861
 0.12072, 0.07794
 0.11807, 0.07725
 0.11544, 0.07655
 0.11283, 0.07583
 0.11025, 0.07509
 0.10769, 0.07433
 0.10515, 0.07356
 0.10264, 0.07276
 0.10014, 0.07195
 0.09767, 0.07096
 0.09521, 0.06995
 0.09278, 0.06892
 0.09037, 0.06788
 0.08798, 0.06683
 0.08561, 0.06576
 0.08326, 0.06467
 0.08093, 0.06358
 0.07862, 0.06247
 0.07633, 0.06135
 0.07405, 0.06021
 0.07180, 0.05907
 0.06956, 0.05792
 0.06735, 0.05676
 0.06515, 0.05559
 0.06297, 0.05441
 0.06081, 0.05322
 0.05866, 0.05202
 0.05653, 0.05081
 0.05442, 0.04960
 0.05233, 0.04838
 0.05026, 0.04715
 0.04820, 0.04596
 0.04615, 0.04476
 0.04413, 0.04357
 0.04212, 0.04235
 0.04012, 0.04113
 0.03815, 0.03990
 0.03618, 0.03864
 0.03424, 0.03738
 0.03231, 0.03611
 0.03039, 0.03481
 0.02849, 0.03350
 0.02660, 0.03216
 0.02473, 0.03080
 0.02287, 0.02941
 0.02103, 0.02800
 0.01920, 0.02655
 0.01739, 0.02506
 0.01559, 0.02353
 0.01380, 0.02193
 0.01203, 0.02028
 0.01027, 0.01853
 0.00853, 0.01669
 0.00680, 0.01471
 0.00508, 0.01252
 0.00337, 0.01001
 0.00168, 0.00690
 0.00056, 0.00388
 0.00000, 0.00000
 0.00000, 0.00000
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 0.00168,-0.00529
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 0.00680,-0.01023
 0.00853,-0.01134
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 0.01559,-0.01481
 0.01739,-0.01551
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 0.02660,-0.01844
 0.02849,-0.01894
 0.03039,-0.01941
 0.03231,-0.01986
 0.03424,-0.02028
 0.03618,-0.02069
 0.03815,-0.02108
 0.04012,-0.02144
 0.04212,-0.02179
 0.04413,-0.02213
 0.04615,-0.02245
 0.04820,-0.02275
 0.05026,-0.02303
 0.05233,-0.02328
 0.05442,-0.02352
 0.05653,-0.02374
 0.05866,-0.02395
 0.06081,-0.02415
 0.06297,-0.02433
 0.06515,-0.02451
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 0.07180,-0.02496
 0.07405,-0.02510
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 0.07862,-0.02533
 0.08093,-0.02544
 0.08326,-0.02553
 0.08561,-0.02562
 0.08798,-0.02570
 0.09037,-0.02578
 0.09278,-0.02584
 0.09521,-0.02590
 0.09767,-0.02596
 0.10014,-0.02600
 0.10264,-0.02606
 0.10515,-0.02611
 0.10769,-0.02615
 0.11025,-0.02618
 0.11283,-0.02622
 0.11544,-0.02624
 0.11807,-0.02626
 0.12072,-0.02628
 0.12340,-0.02629
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 0.13996,-0.02625
 0.14280,-0.02622
 0.14568,-0.02619
 0.14858,-0.02616
 0.15150,-0.02612
 0.15445,-0.02608
 0.15743,-0.02603
 0.16044,-0.02598
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 0.16654,-0.02587
 0.16963,-0.02580
 0.17275,-0.02573
 0.17590,-0.02566
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 0.26526,-0.02248
 0.26931,-0.02231
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 0.33538,-0.01952
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 0.35984,-0.01853
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 1.00000, 0.00000