ファイルインデックス名　: File Index Name        : 3168        .A  
翼型整理番号　　　　　　: Airfoil Serial No.     : C08-0004-1
翼型名　　　　　　　　　: Airfoil Name           : CJ-5
翼型ファイル番号　　　　: Airfoil File No.       : 3168
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, 0.00043
 0.97362, 0.00093
 0.96072, 0.00149
 0.94801, 0.00210
 0.93549, 0.00277
 0.92315, 0.00349
 0.91099, 0.00425
 0.89900, 0.00507
 0.88719, 0.00591
 0.87554, 0.00678
 0.86406, 0.00770
 0.85274, 0.00867
 0.84158, 0.00968
 0.83058, 0.01073
 0.81973, 0.01183
 0.80903, 0.01298
 0.79848, 0.01420
 0.78808, 0.01561
 0.77781, 0.01705
 0.76769, 0.01852
 0.75770, 0.02002
 0.74785, 0.02152
 0.73814, 0.02302
 0.72855, 0.02452
 0.71909, 0.02601
 0.70976, 0.02747
 0.70055, 0.02891
 0.69146, 0.03019
 0.68249, 0.03142
 0.67363, 0.03262
 0.66490, 0.03379
 0.65627, 0.03493
 0.64776, 0.03604
 0.63935, 0.03712
 0.63106, 0.03818
 0.62287, 0.03920
 0.61478, 0.04020
 0.60680, 0.04118
 0.59891, 0.04213
 0.59112, 0.04305
 0.58344, 0.04394
 0.57584, 0.04481
 0.56834, 0.04566
 0.56094, 0.04649
 0.55362, 0.04730
 0.54639, 0.04809
 0.53925, 0.04887
 0.53220, 0.04962
 0.52523, 0.05037
 0.51835, 0.05109
 0.51155, 0.05180
 0.50483, 0.05250
 0.49819, 0.05320
 0.49163, 0.05391
 0.48514, 0.05460
 0.47874, 0.05529
 0.47240, 0.05596
 0.46614, 0.05661
 0.45996, 0.05725
 0.45384, 0.05788
 0.44780, 0.05850
 0.44182, 0.05909
 0.43591, 0.05968
 0.43007, 0.06024
 0.42430, 0.06079
 0.41859, 0.06133
 0.41295, 0.06185
 0.40737, 0.06235
 0.40185, 0.06284
 0.39639, 0.06330
 0.39099, 0.06375
 0.38566, 0.06417
 0.38038, 0.06458
 0.37516, 0.06497
 0.37000, 0.06535
 0.36489, 0.06571
 0.35984, 0.06605
 0.35484, 0.06638
 0.34990, 0.06669
 0.34501, 0.06698
 0.34017, 0.06726
 0.33538, 0.06752
 0.33065, 0.06777
 0.32596, 0.06800
 0.32133, 0.06821
 0.31674, 0.06841
 0.31220, 0.06859
 0.30771, 0.06875
 0.30326, 0.06890
 0.29887, 0.06902
 0.29451, 0.06910
 0.29020, 0.06916
 0.28594, 0.06920
 0.28172, 0.06923
 0.27754, 0.06925
 0.27340, 0.06925
 0.26931, 0.06924
 0.26526, 0.06921
 0.26125, 0.06917
 0.25728, 0.06912
 0.25334, 0.06906
 0.24945, 0.06899
 0.24560, 0.06890
 0.24178, 0.06881
 0.23800, 0.06870
 0.23426, 0.06859
 0.23056, 0.06846
 0.22689, 0.06832
 0.22326, 0.06818
 0.21966, 0.06802
 0.21610, 0.06786
 0.21257, 0.06769
 0.20907, 0.06751
 0.20561, 0.06732
 0.20218, 0.06713
 0.19879, 0.06694
 0.19542, 0.06676
 0.19209, 0.06657
 0.18879, 0.06638
 0.18552, 0.06617
 0.18228, 0.06596
 0.17908, 0.06573
 0.17590, 0.06549
 0.17275, 0.06524
 0.16963, 0.06498
 0.16654, 0.06471
 0.16348, 0.06443
 0.16044, 0.06413
 0.15743, 0.06383
 0.15445, 0.06351
 0.15150, 0.06317
 0.14858, 0.06282
 0.14568, 0.06244
 0.14280, 0.06204
 0.13996, 0.06164
 0.13713, 0.06122
 0.13434, 0.06079
 0.13157, 0.06034
 0.12882, 0.05988
 0.12610, 0.05941
 0.12340, 0.05893
 0.12072, 0.05843
 0.11807, 0.05793
 0.11544, 0.05741
 0.11283, 0.05687
 0.11025, 0.05633
 0.10769, 0.05577
 0.10515, 0.05521
 0.10264, 0.05463
 0.10014, 0.05403
 0.09767, 0.05342
 0.09521, 0.05280
 0.09278, 0.05216
 0.09037, 0.05152
 0.08798, 0.05086
 0.08561, 0.05019
 0.08326, 0.04952
 0.08093, 0.04883
 0.07862, 0.04813
 0.07633, 0.04742
 0.07405, 0.04669
 0.07180, 0.04596
 0.06956, 0.04521
 0.06735, 0.04446
 0.06515, 0.04369
 0.06297, 0.04292
 0.06081, 0.04214
 0.05866, 0.04134
 0.05653, 0.04054
 0.05442, 0.03974
 0.05233, 0.03892
 0.05026, 0.03810
 0.04820, 0.03731
 0.04615, 0.03651
 0.04413, 0.03570
 0.04212, 0.03489
 0.04012, 0.03406
 0.03815, 0.03323
 0.03618, 0.03237
 0.03424, 0.03151
 0.03231, 0.03063
 0.03039, 0.02972
 0.02849, 0.02879
 0.02660, 0.02784
 0.02473, 0.02685
 0.02287, 0.02582
 0.02103, 0.02474
 0.01920, 0.02363
 0.01739, 0.02247
 0.01559, 0.02126
 0.01380, 0.01998
 0.01203, 0.01863
 0.01027, 0.01719
 0.00853, 0.01564
 0.00680, 0.01394
 0.00508, 0.01201
 0.00337, 0.00975
 0.00168, 0.00686
 0.00056, 0.00394
 0.00000, 0.00000
 0.00000, 0.00000
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 0.00168,-0.00541
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 0.00680,-0.01057
 0.00853,-0.01175
 0.01027,-0.01280
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 0.01559,-0.01546
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 0.02849,-0.02012
 0.03039,-0.02068
 0.03231,-0.02123
 0.03424,-0.02174
 0.03618,-0.02224
 0.03815,-0.02271
 0.04012,-0.02315
 0.04212,-0.02358
 0.04413,-0.02398
 0.04615,-0.02436
 0.04820,-0.02471
 0.05026,-0.02503
 0.05233,-0.02526
 0.05442,-0.02547
 0.05653,-0.02567
 0.05866,-0.02585
 0.06081,-0.02602
 0.06297,-0.02619
 0.06515,-0.02634
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 0.07180,-0.02679
 0.07405,-0.02694
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 0.07862,-0.02734
 0.08093,-0.02755
 0.08326,-0.02775
 0.08561,-0.02796
 0.08798,-0.02815
 0.09037,-0.02834
 0.09278,-0.02852
 0.09521,-0.02870
 0.09767,-0.02886
 0.10014,-0.02900
 0.10264,-0.02906
 0.10515,-0.02911
 0.10769,-0.02913
 0.11025,-0.02914
 0.11283,-0.02914
 0.11544,-0.02912
 0.11807,-0.02909
 0.12072,-0.02904
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 0.13713,-0.02855
 0.13996,-0.02843
 0.14280,-0.02832
 0.14568,-0.02819
 0.14858,-0.02806
 0.15150,-0.02795
 0.15445,-0.02785
 0.15743,-0.02775
 0.16044,-0.02764
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 0.16654,-0.02741
 0.16963,-0.02729
 0.17275,-0.02717
 0.17590,-0.02704
 0.17908,-0.02691
 0.18228,-0.02678
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 0.26526,-0.02252
 0.26931,-0.02232
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 0.32133,-0.02068
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 0.33538,-0.02053
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 0.49163,-0.01812
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 1.00000, 0.00000