ファイルインデックス名　: File Index Name        : 0322-2      .A  
翼型整理番号　　　　　　: Airfoil Serial No.     : C05-0062-2
翼型名　　　　　　　　　: Airfoil Name           : C-62
翼型ファイル番号　　　　: Airfoil File No.       : 0322
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.   : VB6B05-A01K


座標　　　　　　　　　　: Plot Ordinates         :

 X             Y

 1.00000, 0.00000
 0.98671, 0.00254
 0.97362, 0.00494
 0.96072, 0.00720
 0.94801, 0.00933
 0.93549, 0.01134
 0.92315, 0.01324
 0.91099, 0.01503
 0.89900, 0.01674
 0.88719, 0.01837
 0.87554, 0.01993
 0.86406, 0.02141
 0.85274, 0.02283
 0.84158, 0.02418
 0.83058, 0.02548
 0.81973, 0.02672
 0.80903, 0.02791
 0.79848, 0.02907
 0.78808, 0.03020
 0.77781, 0.03130
 0.76769, 0.03236
 0.75770, 0.03338
 0.74785, 0.03437
 0.73814, 0.03532
 0.72855, 0.03625
 0.71909, 0.03714
 0.70976, 0.03801
 0.70055, 0.03885
 0.69146, 0.03967
 0.68249, 0.04047
 0.67363, 0.04125
 0.66490, 0.04200
 0.65627, 0.04273
 0.64776, 0.04344
 0.63935, 0.04413
 0.63106, 0.04480
 0.62287, 0.04545
 0.61478, 0.04608
 0.60680, 0.04669
 0.59891, 0.04728
 0.59112, 0.04787
 0.58344, 0.04843
 0.57584, 0.04898
 0.56834, 0.04951
 0.56094, 0.05003
 0.55362, 0.05053
 0.54639, 0.05102
 0.53925, 0.05149
 0.53220, 0.05194
 0.52523, 0.05238
 0.51835, 0.05281
 0.51155, 0.05322
 0.50483, 0.05362
 0.49819, 0.05401
 0.49163, 0.05438
 0.48514, 0.05474
 0.47874, 0.05509
 0.47240, 0.05542
 0.46614, 0.05575
 0.45996, 0.05606
 0.45384, 0.05635
 0.44780, 0.05663
 0.44182, 0.05690
 0.43591, 0.05716
 0.43007, 0.05741
 0.42430, 0.05764
 0.41859, 0.05786
 0.41295, 0.05806
 0.40737, 0.05826
 0.40185, 0.05844
 0.39639, 0.05861
 0.39099, 0.05876
 0.38566, 0.05890
 0.38038, 0.05902
 0.37516, 0.05914
 0.37000, 0.05924
 0.36489, 0.05934
 0.35984, 0.05942
 0.35484, 0.05949
 0.34990, 0.05955
 0.34501, 0.05960
 0.34017, 0.05965
 0.33538, 0.05968
 0.33065, 0.05970
 0.32596, 0.05971
 0.32133, 0.05971
 0.31674, 0.05971
 0.31220, 0.05969
 0.30771, 0.05966
 0.30326, 0.05963
 0.29887, 0.05959
 0.29451, 0.05954
 0.29020, 0.05948
 0.28594, 0.05942
 0.28172, 0.05934
 0.27754, 0.05926
 0.27340, 0.05917
 0.26931, 0.05907
 0.26526, 0.05896
 0.26125, 0.05884
 0.25728, 0.05872
 0.25334, 0.05859
 0.24945, 0.05845
 0.24560, 0.05830
 0.24178, 0.05815
 0.23800, 0.05799
 0.23426, 0.05782
 0.23056, 0.05764
 0.22689, 0.05746
 0.22326, 0.05726
 0.21966, 0.05706
 0.21610, 0.05686
 0.21257, 0.05664
 0.20907, 0.05642
 0.20561, 0.05619
 0.20218, 0.05596
 0.19879, 0.05571
 0.19542, 0.05546
 0.19209, 0.05520
 0.18879, 0.05493
 0.18552, 0.05465
 0.18228, 0.05437
 0.17908, 0.05408
 0.17590, 0.05379
 0.17275, 0.05349
 0.16963, 0.05318
 0.16654, 0.05286
 0.16348, 0.05254
 0.16044, 0.05221
 0.15743, 0.05187
 0.15445, 0.05153
 0.15150, 0.05118
 0.14858, 0.05083
 0.14568, 0.05047
 0.14280, 0.05010
 0.13996, 0.04972
 0.13713, 0.04934
 0.13434, 0.04895
 0.13157, 0.04856
 0.12882, 0.04816
 0.12610, 0.04775
 0.12340, 0.04733
 0.12072, 0.04691
 0.11807, 0.04647
 0.11544, 0.04603
 0.11283, 0.04559
 0.11025, 0.04513
 0.10769, 0.04467
 0.10515, 0.04420
 0.10264, 0.04372
 0.10014, 0.04323
 0.09767, 0.04274
 0.09521, 0.04223
 0.09278, 0.04172
 0.09037, 0.04120
 0.08798, 0.04067
 0.08561, 0.04012
 0.08326, 0.03957
 0.08093, 0.03900
 0.07862, 0.03842
 0.07633, 0.03783
 0.07405, 0.03722
 0.07180, 0.03658
 0.06956, 0.03593
 0.06735, 0.03527
 0.06515, 0.03459
 0.06297, 0.03390
 0.06081, 0.03320
 0.05866, 0.03248
 0.05653, 0.03175
 0.05442, 0.03101
 0.05233, 0.03026
 0.05026, 0.02950
 0.04820, 0.02873
 0.04615, 0.02796
 0.04413, 0.02717
 0.04212, 0.02638
 0.04012, 0.02556
 0.03815, 0.02474
 0.03618, 0.02389
 0.03424, 0.02304
 0.03231, 0.02216
 0.03039, 0.02126
 0.02849, 0.02034
 0.02660, 0.01940
 0.02473, 0.01843
 0.02287, 0.01740
 0.02103, 0.01635
 0.01920, 0.01527
 0.01739, 0.01417
 0.01559, 0.01304
 0.01380, 0.01187
 0.01203, 0.01068
 0.01027, 0.00945
 0.00853, 0.00819
 0.00680, 0.00688
 0.00508, 0.00551
 0.00337, 0.00405
 0.00168, 0.00245
 0.00000, 0.00117
 0.00000, 0.00000
 0.00000, 0.00000
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 0.03231,-0.01233
 0.03424,-0.01272
 0.03618,-0.01309
 0.03815,-0.01346
 0.04012,-0.01380
 0.04212,-0.01413
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 0.04615,-0.01476
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 0.05233,-0.01558
 0.05442,-0.01582
 0.05653,-0.01604
 0.05866,-0.01626
 0.06081,-0.01647
 0.06297,-0.01667
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 0.07862,-0.01792
 0.08093,-0.01809
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 0.08561,-0.01840
 0.08798,-0.01855
 0.09037,-0.01869
 0.09278,-0.01883
 0.09521,-0.01896
 0.09767,-0.01909
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 0.10264,-0.01931
 0.10515,-0.01940
 0.10769,-0.01949
 0.11025,-0.01958
 0.11283,-0.01965
 0.11544,-0.01973
 0.11807,-0.01979
 0.12072,-0.01986
 0.12340,-0.01991
 0.12610,-0.01996
 0.12882,-0.02001
 0.13157,-0.02006
 0.13434,-0.02010
 0.13713,-0.02013
 0.13996,-0.02016
 0.14280,-0.02019
 0.14568,-0.02022
 0.14858,-0.02024
 0.15150,-0.02026
 0.15445,-0.02028
 0.15743,-0.02030
 0.16044,-0.02032
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 0.16654,-0.02034
 0.16963,-0.02035
 0.17275,-0.02036
 0.17590,-0.02037
 0.17908,-0.02037
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 0.18552,-0.02037
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 0.25728,-0.02028
 0.26125,-0.02026
 0.26526,-0.02025
 0.26931,-0.02024
 0.27340,-0.02022
 0.27754,-0.02021
 0.28172,-0.02019
 0.28594,-0.02017
 0.29020,-0.02015
 0.29451,-0.02013
 0.29887,-0.02011
 0.30326,-0.02008
 0.30771,-0.02006
 0.31220,-0.02004
 0.31674,-0.02001
 0.32133,-0.01999
 0.32596,-0.01996
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 0.33538,-0.01990
 0.34017,-0.01986
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 0.35984,-0.01971
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 1.00000, 0.00000