ファイルインデックス名　: File Index Name        : 0929        .A  
翼型整理番号　　　　　　: Airfoil Serial No.     : W02-0001-1
翼型名　　　　　　　　　: Airfoil Name           : W-1
翼型ファイル番号　　　　: Airfoil File No.       : 0929
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-C01G3


座標　　　　　　　　　　: Plot Ordinates         :

 X             Y

 1.00000, 0.00000
 0.98671, 0.00461
 0.97362, 0.00828
 0.96072, 0.01113
 0.94801, 0.01330
 0.93549, 0.01491
 0.92315, 0.01609
 0.91099, 0.01693
 0.89900, 0.01760
 0.88719, 0.01874
 0.87554, 0.01989
 0.86406, 0.02104
 0.85274, 0.02218
 0.84158, 0.02331
 0.83058, 0.02443
 0.81973, 0.02553
 0.80903, 0.02660
 0.79848, 0.02764
 0.78808, 0.02856
 0.77781, 0.02946
 0.76769, 0.03033
 0.75770, 0.03118
 0.74785, 0.03201
 0.73814, 0.03282
 0.72855, 0.03362
 0.71909, 0.03441
 0.70976, 0.03519
 0.70055, 0.03595
 0.69146, 0.03678
 0.68249, 0.03760
 0.67363, 0.03841
 0.66490, 0.03921
 0.65627, 0.04000
 0.64776, 0.04077
 0.63935, 0.04154
 0.63106, 0.04228
 0.62287, 0.04301
 0.61478, 0.04372
 0.60680, 0.04442
 0.59891, 0.04509
 0.59112, 0.04570
 0.58344, 0.04630
 0.57584, 0.04687
 0.56834, 0.04743
 0.56094, 0.04797
 0.55362, 0.04850
 0.54639, 0.04900
 0.53925, 0.04949
 0.53220, 0.04996
 0.52523, 0.05042
 0.51835, 0.05087
 0.51155, 0.05129
 0.50483, 0.05171
 0.49819, 0.05211
 0.49163, 0.05252
 0.48514, 0.05291
 0.47874, 0.05328
 0.47240, 0.05364
 0.46614, 0.05399
 0.45996, 0.05433
 0.45384, 0.05465
 0.44780, 0.05496
 0.44182, 0.05525
 0.43591, 0.05554
 0.43007, 0.05580
 0.42430, 0.05606
 0.41859, 0.05630
 0.41295, 0.05652
 0.40737, 0.05674
 0.40185, 0.05694
 0.39639, 0.05710
 0.39099, 0.05723
 0.38566, 0.05736
 0.38038, 0.05747
 0.37516, 0.05757
 0.37000, 0.05766
 0.36489, 0.05773
 0.35984, 0.05780
 0.35484, 0.05786
 0.34990, 0.05791
 0.34501, 0.05795
 0.34017, 0.05798
 0.33538, 0.05801
 0.33065, 0.05803
 0.32596, 0.05804
 0.32133, 0.05805
 0.31674, 0.05805
 0.31220, 0.05804
 0.30771, 0.05803
 0.30326, 0.05801
 0.29887, 0.05801
 0.29451, 0.05804
 0.29020, 0.05807
 0.28594, 0.05809
 0.28172, 0.05811
 0.27754, 0.05813
 0.27340, 0.05814
 0.26931, 0.05814
 0.26526, 0.05814
 0.26125, 0.05814
 0.25728, 0.05813
 0.25334, 0.05811
 0.24945, 0.05808
 0.24560, 0.05805
 0.24178, 0.05801
 0.23800, 0.05797
 0.23426, 0.05792
 0.23056, 0.05786
 0.22689, 0.05779
 0.22326, 0.05771
 0.21966, 0.05763
 0.21610, 0.05754
 0.21257, 0.05744
 0.20907, 0.05733
 0.20561, 0.05721
 0.20218, 0.05709
 0.19879, 0.05695
 0.19542, 0.05681
 0.19209, 0.05665
 0.18879, 0.05649
 0.18552, 0.05632
 0.18228, 0.05613
 0.17908, 0.05594
 0.17590, 0.05573
 0.17275, 0.05551
 0.16963, 0.05529
 0.16654, 0.05505
 0.16348, 0.05479
 0.16044, 0.05453
 0.15743, 0.05425
 0.15445, 0.05396
 0.15150, 0.05366
 0.14858, 0.05333
 0.14568, 0.05296
 0.14280, 0.05258
 0.13996, 0.05219
 0.13713, 0.05178
 0.13434, 0.05136
 0.13157, 0.05093
 0.12882, 0.05049
 0.12610, 0.05004
 0.12340, 0.04958
 0.12072, 0.04911
 0.11807, 0.04863
 0.11544, 0.04814
 0.11283, 0.04764
 0.11025, 0.04713
 0.10769, 0.04662
 0.10515, 0.04610
 0.10264, 0.04557
 0.10014, 0.04503
 0.09767, 0.04452
 0.09521, 0.04399
 0.09278, 0.04346
 0.09037, 0.04292
 0.08798, 0.04236
 0.08561, 0.04180
 0.08326, 0.04121
 0.08093, 0.04062
 0.07862, 0.04000
 0.07633, 0.03938
 0.07405, 0.03871
 0.07180, 0.03800
 0.06956, 0.03727
 0.06735, 0.03652
 0.06515, 0.03576
 0.06297, 0.03499
 0.06081, 0.03420
 0.05866, 0.03340
 0.05653, 0.03259
 0.05442, 0.03177
 0.05233, 0.03094
 0.05026, 0.03011
 0.04820, 0.02932
 0.04615, 0.02853
 0.04413, 0.02774
 0.04212, 0.02695
 0.04012, 0.02614
 0.03815, 0.02534
 0.03618, 0.02452
 0.03424, 0.02370
 0.03231, 0.02286
 0.03039, 0.02201
 0.02849, 0.02115
 0.02660, 0.02027
 0.02473, 0.01936
 0.02287, 0.01842
 0.02103, 0.01745
 0.01920, 0.01646
 0.01739, 0.01544
 0.01559, 0.01440
 0.01380, 0.01332
 0.01203, 0.01220
 0.01027, 0.01103
 0.00853, 0.00981
 0.00680, 0.00852
 0.00508, 0.00712
 0.00337, 0.00556
 0.00168, 0.00370
 0.00056, 0.00200
 0.00000, 0.00000
 0.00000, 0.00000
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 0.00168,-0.00495
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 0.00680,-0.00881
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 0.01559,-0.01188
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 0.03039,-0.01524
 0.03231,-0.01567
 0.03424,-0.01609
 0.03618,-0.01649
 0.03815,-0.01689
 0.04012,-0.01728
 0.04212,-0.01766
 0.04413,-0.01802
 0.04615,-0.01838
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 0.05026,-0.01903
 0.05233,-0.01925
 0.05442,-0.01947
 0.05653,-0.01968
 0.05866,-0.01989
 0.06081,-0.02010
 0.06297,-0.02030
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 0.07405,-0.02140
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 0.08093,-0.02233
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 0.08561,-0.02300
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 0.09037,-0.02368
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 0.09767,-0.02469
 0.10014,-0.02502
 0.10264,-0.02528
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 0.10769,-0.02577
 0.11025,-0.02601
 0.11283,-0.02623
 0.11544,-0.02645
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 0.12072,-0.02685
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 0.13996,-0.02803
 0.14280,-0.02817
 0.14568,-0.02831
 0.14858,-0.02844
 0.15150,-0.02857
 0.15445,-0.02870
 0.15743,-0.02882
 0.16044,-0.02894
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 0.16654,-0.02916
 0.16963,-0.02927
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 0.17590,-0.02946
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 0.26526,-0.03018
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 1.00000, 0.00000