ファイルインデックス名　: File Index Name        : 0152        .A  
翼型整理番号　　　　　　: Airfoil Serial No.     : G01-0780-1
翼型名　　　　　　　　　: Airfoil Name           : Go 780
翼型ファイル番号　　　　: Airfoil File No.       : 0152
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, 0.00212
 0.97362, 0.00430
 0.96072, 0.00651
 0.94801, 0.00875
 0.93549, 0.01100
 0.92315, 0.01325
 0.91099, 0.01548
 0.89900, 0.01767
 0.88719, 0.01971
 0.87554, 0.02170
 0.86406, 0.02362
 0.85274, 0.02551
 0.84158, 0.02735
 0.83058, 0.02916
 0.81973, 0.03095
 0.80903, 0.03271
 0.79848, 0.03447
 0.78808, 0.03636
 0.77781, 0.03823
 0.76769, 0.04008
 0.75770, 0.04189
 0.74785, 0.04367
 0.73814, 0.04541
 0.72855, 0.04711
 0.71909, 0.04876
 0.70976, 0.05036
 0.70055, 0.05191
 0.69146, 0.05333
 0.68249, 0.05470
 0.67363, 0.05600
 0.66490, 0.05725
 0.65627, 0.05844
 0.64776, 0.05956
 0.63935, 0.06063
 0.63106, 0.06164
 0.62287, 0.06260
 0.61478, 0.06349
 0.60680, 0.06433
 0.59891, 0.06510
 0.59112, 0.06576
 0.58344, 0.06636
 0.57584, 0.06692
 0.56834, 0.06742
 0.56094, 0.06787
 0.55362, 0.06827
 0.54639, 0.06863
 0.53925, 0.06895
 0.53220, 0.06922
 0.52523, 0.06946
 0.51835, 0.06965
 0.51155, 0.06981
 0.50483, 0.06993
 0.49819, 0.07002
 0.49163, 0.07006
 0.48514, 0.07008
 0.47874, 0.07007
 0.47240, 0.07002
 0.46614, 0.06996
 0.45996, 0.06987
 0.45384, 0.06975
 0.44780, 0.06961
 0.44182, 0.06946
 0.43591, 0.06928
 0.43007, 0.06909
 0.42430, 0.06888
 0.41859, 0.06865
 0.41295, 0.06841
 0.40737, 0.06816
 0.40185, 0.06789
 0.39639, 0.06764
 0.39099, 0.06739
 0.38566, 0.06713
 0.38038, 0.06686
 0.37516, 0.06659
 0.37000, 0.06630
 0.36489, 0.06600
 0.35984, 0.06569
 0.35484, 0.06538
 0.34990, 0.06506
 0.34501, 0.06472
 0.34017, 0.06438
 0.33538, 0.06404
 0.33065, 0.06368
 0.32596, 0.06332
 0.32133, 0.06295
 0.31674, 0.06257
 0.31220, 0.06219
 0.30771, 0.06180
 0.30326, 0.06140
 0.29887, 0.06099
 0.29451, 0.06056
 0.29020, 0.06013
 0.28594, 0.05969
 0.28172, 0.05925
 0.27754, 0.05880
 0.27340, 0.05834
 0.26931, 0.05788
 0.26526, 0.05742
 0.26125, 0.05695
 0.25728, 0.05648
 0.25334, 0.05601
 0.24945, 0.05553
 0.24560, 0.05505
 0.24178, 0.05457
 0.23800, 0.05408
 0.23426, 0.05359
 0.23056, 0.05310
 0.22689, 0.05261
 0.22326, 0.05211
 0.21966, 0.05162
 0.21610, 0.05112
 0.21257, 0.05062
 0.20907, 0.05012
 0.20561, 0.04962
 0.20218, 0.04912
 0.19879, 0.04863
 0.19542, 0.04816
 0.19209, 0.04768
 0.18879, 0.04720
 0.18552, 0.04672
 0.18228, 0.04623
 0.17908, 0.04574
 0.17590, 0.04525
 0.17275, 0.04476
 0.16963, 0.04426
 0.16654, 0.04376
 0.16348, 0.04325
 0.16044, 0.04274
 0.15743, 0.04222
 0.15445, 0.04170
 0.15150, 0.04117
 0.14858, 0.04061
 0.14568, 0.04002
 0.14280, 0.03942
 0.13996, 0.03882
 0.13713, 0.03821
 0.13434, 0.03760
 0.13157, 0.03699
 0.12882, 0.03638
 0.12610, 0.03577
 0.12340, 0.03516
 0.12072, 0.03455
 0.11807, 0.03394
 0.11544, 0.03334
 0.11283, 0.03273
 0.11025, 0.03214
 0.10769, 0.03155
 0.10515, 0.03097
 0.10264, 0.03040
 0.10014, 0.02983
 0.09767, 0.02930
 0.09521, 0.02877
 0.09278, 0.02826
 0.09037, 0.02775
 0.08798, 0.02725
 0.08561, 0.02676
 0.08326, 0.02627
 0.08093, 0.02579
 0.07862, 0.02533
 0.07633, 0.02487
 0.07405, 0.02443
 0.07180, 0.02402
 0.06956, 0.02361
 0.06735, 0.02322
 0.06515, 0.02282
 0.06297, 0.02243
 0.06081, 0.02205
 0.05866, 0.02166
 0.05653, 0.02126
 0.05442, 0.02087
 0.05233, 0.02046
 0.05026, 0.02005
 0.04820, 0.01957
 0.04615, 0.01905
 0.04413, 0.01853
 0.04212, 0.01799
 0.04012, 0.01744
 0.03815, 0.01688
 0.03618, 0.01630
 0.03424, 0.01572
 0.03231, 0.01512
 0.03039, 0.01451
 0.02849, 0.01388
 0.02660, 0.01325
 0.02473, 0.01261
 0.02287, 0.01197
 0.02103, 0.01131
 0.01920, 0.01064
 0.01739, 0.00996
 0.01559, 0.00926
 0.01380, 0.00854
 0.01203, 0.00780
 0.01027, 0.00703
 0.00853, 0.00623
 0.00680, 0.00538
 0.00508, 0.00448
 0.00337, 0.00347
 0.00168, 0.00229
 0.00056, 0.00122
 0.00000, 0.00000
 0.00000, 0.00000
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 0.00168,-0.00317
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 0.00680,-0.00654
 0.00853,-0.00736
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 0.01559,-0.01012
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 0.03039,-0.01439
 0.03231,-0.01485
 0.03424,-0.01531
 0.03618,-0.01576
 0.03815,-0.01621
 0.04012,-0.01666
 0.04212,-0.01710
 0.04413,-0.01754
 0.04615,-0.01798
 0.04820,-0.01842
 0.05026,-0.01886
 0.05233,-0.01937
 0.05442,-0.01987
 0.05653,-0.02037
 0.05866,-0.02086
 0.06081,-0.02134
 0.06297,-0.02181
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 0.07405,-0.02394
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 0.08093,-0.02482
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 0.08561,-0.02531
 0.08798,-0.02554
 0.09037,-0.02576
 0.09278,-0.02598
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 0.09767,-0.02640
 0.10014,-0.02662
 0.10264,-0.02689
 0.10515,-0.02718
 0.10769,-0.02747
 0.11025,-0.02776
 0.11283,-0.02806
 0.11544,-0.02836
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 0.12072,-0.02897
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 0.13996,-0.03118
 0.14280,-0.03150
 0.14568,-0.03182
 0.14858,-0.03214
 0.15150,-0.03245
 0.15445,-0.03275
 0.15743,-0.03305
 0.16044,-0.03335
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 0.16654,-0.03395
 0.16963,-0.03425
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 0.17590,-0.03484
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 0.26526,-0.04210
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 1.00000, 0.00000