ファイルインデックス名　: File Index Name        : 3215        .A  
翼型整理番号　　　　　　: Airfoil Serial No.     : 900-0019-1
翼型名　　　　　　　　　: Airfoil Name           : 77A
翼型ファイル番号　　　　: Airfoil File No.       : 3215
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, 0.00179
 0.97362, 0.00341
 0.96072, 0.00487
 0.94801, 0.00620
 0.93549, 0.00742
 0.92315, 0.00854
 0.91099, 0.00959
 0.89900, 0.01059
 0.88719, 0.01163
 0.87554, 0.01265
 0.86406, 0.01364
 0.85274, 0.01461
 0.84158, 0.01556
 0.83058, 0.01649
 0.81973, 0.01739
 0.80903, 0.01827
 0.79848, 0.01912
 0.78808, 0.01993
 0.77781, 0.02072
 0.76769, 0.02149
 0.75770, 0.02224
 0.74785, 0.02298
 0.73814, 0.02370
 0.72855, 0.02441
 0.71909, 0.02510
 0.70976, 0.02579
 0.70055, 0.02646
 0.69146, 0.02716
 0.68249, 0.02785
 0.67363, 0.02853
 0.66490, 0.02920
 0.65627, 0.02985
 0.64776, 0.03050
 0.63935, 0.03113
 0.63106, 0.03175
 0.62287, 0.03235
 0.61478, 0.03294
 0.60680, 0.03352
 0.59891, 0.03407
 0.59112, 0.03459
 0.58344, 0.03509
 0.57584, 0.03557
 0.56834, 0.03604
 0.56094, 0.03650
 0.55362, 0.03694
 0.54639, 0.03738
 0.53925, 0.03780
 0.53220, 0.03821
 0.52523, 0.03860
 0.51835, 0.03899
 0.51155, 0.03937
 0.50483, 0.03974
 0.49819, 0.04010
 0.49163, 0.04047
 0.48514, 0.04083
 0.47874, 0.04119
 0.47240, 0.04153
 0.46614, 0.04186
 0.45996, 0.04219
 0.45384, 0.04250
 0.44780, 0.04281
 0.44182, 0.04311
 0.43591, 0.04340
 0.43007, 0.04367
 0.42430, 0.04394
 0.41859, 0.04420
 0.41295, 0.04445
 0.40737, 0.04469
 0.40185, 0.04492
 0.39639, 0.04516
 0.39099, 0.04539
 0.38566, 0.04562
 0.38038, 0.04583
 0.37516, 0.04603
 0.37000, 0.04622
 0.36489, 0.04640
 0.35984, 0.04657
 0.35484, 0.04672
 0.34990, 0.04686
 0.34501, 0.04699
 0.34017, 0.04711
 0.33538, 0.04721
 0.33065, 0.04730
 0.32596, 0.04737
 0.32133, 0.04743
 0.31674, 0.04747
 0.31220, 0.04750
 0.30771, 0.04751
 0.30326, 0.04751
 0.29887, 0.04748
 0.29451, 0.04740
 0.29020, 0.04730
 0.28594, 0.04720
 0.28172, 0.04709
 0.27754, 0.04697
 0.27340, 0.04684
 0.26931, 0.04671
 0.26526, 0.04657
 0.26125, 0.04643
 0.25728, 0.04628
 0.25334, 0.04613
 0.24945, 0.04598
 0.24560, 0.04586
 0.24178, 0.04574
 0.23800, 0.04561
 0.23426, 0.04548
 0.23056, 0.04535
 0.22689, 0.04521
 0.22326, 0.04507
 0.21966, 0.04492
 0.21610, 0.04477
 0.21257, 0.04462
 0.20907, 0.04446
 0.20561, 0.04429
 0.20218, 0.04411
 0.19879, 0.04392
 0.19542, 0.04368
 0.19209, 0.04343
 0.18879, 0.04318
 0.18552, 0.04292
 0.18228, 0.04266
 0.17908, 0.04240
 0.17590, 0.04214
 0.17275, 0.04188
 0.16963, 0.04162
 0.16654, 0.04136
 0.16348, 0.04110
 0.16044, 0.04085
 0.15743, 0.04060
 0.15445, 0.04036
 0.15150, 0.04012
 0.14858, 0.03993
 0.14568, 0.03980
 0.14280, 0.03968
 0.13996, 0.03957
 0.13713, 0.03946
 0.13434, 0.03935
 0.13157, 0.03925
 0.12882, 0.03915
 0.12610, 0.03906
 0.12340, 0.03896
 0.12072, 0.03887
 0.11807, 0.03877
 0.11544, 0.03867
 0.11283, 0.03857
 0.11025, 0.03847
 0.10769, 0.03836
 0.10515, 0.03825
 0.10264, 0.03813
 0.10014, 0.03801
 0.09767, 0.03782
 0.09521, 0.03761
 0.09278, 0.03740
 0.09037, 0.03717
 0.08798, 0.03694
 0.08561, 0.03669
 0.08326, 0.03643
 0.08093, 0.03617
 0.07862, 0.03589
 0.07633, 0.03560
 0.07405, 0.03529
 0.07180, 0.03498
 0.06956, 0.03465
 0.06735, 0.03431
 0.06515, 0.03396
 0.06297, 0.03359
 0.06081, 0.03321
 0.05866, 0.03281
 0.05653, 0.03240
 0.05442, 0.03197
 0.05233, 0.03152
 0.05026, 0.03106
 0.04820, 0.03060
 0.04615, 0.03012
 0.04413, 0.02962
 0.04212, 0.02909
 0.04012, 0.02854
 0.03815, 0.02796
 0.03618, 0.02735
 0.03424, 0.02671
 0.03231, 0.02603
 0.03039, 0.02531
 0.02849, 0.02455
 0.02660, 0.02374
 0.02473, 0.02286
 0.02287, 0.02185
 0.02103, 0.02080
 0.01920, 0.01968
 0.01739, 0.01851
 0.01559, 0.01728
 0.01380, 0.01599
 0.01203, 0.01463
 0.01027, 0.01320
 0.00853, 0.01168
 0.00680, 0.01007
 0.00508, 0.00832
 0.00337, 0.00638
 0.00168, 0.00412
 0.00056, 0.00215
 0.00000, 0.00000
 0.00000, 0.00000
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 0.00680,-0.01007
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 0.03231,-0.02603
 0.03424,-0.02671
 0.03618,-0.02735
 0.03815,-0.02796
 0.04012,-0.02854
 0.04212,-0.02909
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 0.04615,-0.03012
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 0.05233,-0.03152
 0.05442,-0.03197
 0.05653,-0.03240
 0.05866,-0.03281
 0.06081,-0.03321
 0.06297,-0.03359
 0.06515,-0.03396
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 0.07405,-0.03529
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 0.07862,-0.03589
 0.08093,-0.03617
 0.08326,-0.03643
 0.08561,-0.03669
 0.08798,-0.03694
 0.09037,-0.03717
 0.09278,-0.03740
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 0.09767,-0.03782
 0.10014,-0.03801
 0.10264,-0.03813
 0.10515,-0.03825
 0.10769,-0.03836
 0.11025,-0.03847
 0.11283,-0.03857
 0.11544,-0.03867
 0.11807,-0.03877
 0.12072,-0.03887
 0.12340,-0.03896
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 0.13996,-0.03957
 0.14280,-0.03968
 0.14568,-0.03980
 0.14858,-0.03993
 0.15150,-0.04012
 0.15445,-0.04036
 0.15743,-0.04060
 0.16044,-0.04085
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 0.16654,-0.04136
 0.16963,-0.04162
 0.17275,-0.04188
 0.17590,-0.04214
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 0.18228,-0.04266
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 0.26526,-0.04657
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 1.00000, 0.00000