ファイルインデックス名　: File Index Name        : 1196        .A  
翼型整理番号　　　　　　: Airfoil Serial No.     : N04-0101-1
翼型名　　　　　　　　　: Airfoil Name           : N.A.C.A. 66-210
翼型ファイル番号　　　　: Airfoil File No.       : 1196
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-A01C


座標　　　　　　　　　　: Plot Ordinates         :

 X             Y

 1.00000, 0.00000
 0.98656, 0.00179
 0.97331, 0.00367
 0.96024, 0.00565
 0.94736, 0.00770
 0.93467, 0.00978
 0.92215, 0.01191
 0.90981, 0.01404
 0.89764, 0.01618
 0.88565, 0.01828
 0.87383, 0.02036
 0.86217, 0.02241
 0.85068, 0.02442
 0.83936, 0.02637
 0.82820, 0.02828
 0.81719, 0.03013
 0.80634, 0.03193
 0.79564, 0.03369
 0.78510, 0.03538
 0.77469, 0.03704
 0.76444, 0.03862
 0.75432, 0.04015
 0.74435, 0.04162
 0.73452, 0.04303
 0.72481, 0.04438
 0.71524, 0.04567
 0.70581, 0.04691
 0.69650, 0.04810
 0.68732, 0.04923
 0.67825, 0.05031
 0.66931, 0.05133
 0.66050, 0.05228
 0.65179, 0.05318
 0.64321, 0.05401
 0.63474, 0.05477
 0.62639, 0.05548
 0.61814, 0.05612
 0.61000, 0.05672
 0.60198, 0.05726
 0.59405, 0.05772
 0.58622, 0.05814
 0.57851, 0.05851
 0.57088, 0.05885
 0.56336, 0.05914
 0.55594, 0.05941
 0.54860, 0.05965
 0.54135, 0.05988
 0.53419, 0.06008
 0.52713, 0.06025
 0.52014, 0.06040
 0.51325, 0.06053
 0.50644, 0.06065
 0.49972, 0.06074
 0.49307, 0.06082
 0.48650, 0.06089
 0.48001, 0.06094
 0.47361, 0.06097
 0.46727, 0.06098
 0.46101, 0.06098
 0.45483, 0.06097
 0.44871, 0.06094
 0.44267, 0.06090
 0.43670, 0.06085
 0.43079, 0.06079
 0.42496, 0.06071
 0.41920, 0.06062
 0.41349, 0.06052
 0.40786, 0.06042
 0.40229, 0.06030
 0.39678, 0.06017
 0.39134, 0.06003
 0.38595, 0.05989
 0.38063, 0.05973
 0.37536, 0.05957
 0.37016, 0.05939
 0.36501, 0.05922
 0.35992, 0.05903
 0.35489, 0.05884
 0.34990, 0.05863
 0.34498, 0.05843
 0.34011, 0.05822
 0.33529, 0.05799
 0.33052, 0.05777
 0.32581, 0.05754
 0.32114, 0.05729
 0.31653, 0.05706
 0.31196, 0.05680
 0.30744, 0.05655
 0.30297, 0.05630
 0.29854, 0.05603
 0.29417, 0.05577
 0.28984, 0.05549
 0.28555, 0.05521
 0.28131, 0.05494
 0.27712, 0.05465
 0.27296, 0.05436
 0.26885, 0.05407
 0.26478, 0.05376
 0.26076, 0.05347
 0.25677, 0.05316
 0.25283, 0.05286
 0.24892, 0.05255
 0.24505, 0.05223
 0.24123, 0.05191
 0.23744, 0.05159
 0.23368, 0.05127
 0.22997, 0.05093
 0.22630, 0.05060
 0.22266, 0.05028
 0.21906, 0.04993
 0.21548, 0.04959
 0.21195, 0.04926
 0.20845, 0.04891
 0.20498, 0.04856
 0.20155, 0.04821
 0.19815, 0.04786
 0.19479, 0.04750
 0.19145, 0.04715
 0.18815, 0.04678
 0.18488, 0.04642
 0.18164, 0.04605
 0.17843, 0.04569
 0.17526, 0.04531
 0.17212, 0.04495
 0.16900, 0.04457
 0.16591, 0.04419
 0.16285, 0.04381
 0.15982, 0.04343
 0.15682, 0.04305
 0.15384, 0.04266
 0.15089, 0.04227
 0.14797, 0.04188
 0.14509, 0.04149
 0.14222, 0.04109
 0.13937, 0.04069
 0.13657, 0.04029
 0.13377, 0.03988
 0.13102, 0.03948
 0.12828, 0.03907
 0.12556, 0.03866
 0.12288, 0.03825
 0.12021, 0.03784
 0.11757, 0.03742
 0.11495, 0.03700
 0.11236, 0.03658
 0.10979, 0.03616
 0.10724, 0.03574
 0.10472, 0.03531
 0.10221, 0.03489
 0.09974, 0.03445
 0.09728, 0.03402
 0.09484, 0.03358
 0.09242, 0.03314
 0.09003, 0.03270
 0.08765, 0.03226
 0.08530, 0.03182
 0.08297, 0.03136
 0.08066, 0.03091
 0.07837, 0.03046
 0.07609, 0.03001
 0.07384, 0.02955
 0.07160, 0.02909
 0.06939, 0.02863
 0.06719, 0.02817
 0.06502, 0.02769
 0.06286, 0.02722
 0.06072, 0.02675
 0.05860, 0.02627
 0.05649, 0.02579
 0.05440, 0.02530
 0.05233, 0.02481
 0.05028, 0.02432
 0.04825, 0.02382
 0.04624, 0.02331
 0.04423, 0.02280
 0.04225, 0.02228
 0.04029, 0.02176
 0.03833, 0.02123
 0.03641, 0.02070
 0.03448, 0.02015
 0.03259, 0.01960
 0.03071, 0.01904
 0.02883, 0.01848
 0.02698, 0.01791
 0.02514, 0.01732
 0.02332, 0.01674
 0.02151, 0.01616
 0.01972, 0.01557
 0.01794, 0.01495
 0.01619, 0.01431
 0.01444, 0.01362
 0.01271, 0.01290
 0.01101, 0.01212
 0.00932, 0.01127
 0.00766, 0.01034
 0.00602, 0.00929
 0.00440, 0.00810
 0.00281, 0.00665
 0.00128, 0.00474
 0.00033, 0.00277
 0.00000, 0.00000
 0.00000, 0.00000
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 0.02967,-0.01403
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 0.03355,-0.01477
 0.03551,-0.01512
 0.03748,-0.01548
 0.03948,-0.01582
 0.04148,-0.01617
 0.04351,-0.01651
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 0.04760,-0.01717
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 0.05176,-0.01781
 0.05386,-0.01812
 0.05597,-0.01843
 0.05811,-0.01874
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 0.06244,-0.01934
 0.06462,-0.01964
 0.06683,-0.01993
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 0.07355,-0.02079
 0.07582,-0.02107
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 0.08044,-0.02163
 0.08277,-0.02190
 0.08513,-0.02217
 0.08750,-0.02244
 0.08989,-0.02270
 0.09230,-0.02297
 0.09474,-0.02322
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 0.09967,-0.02375
 0.10216,-0.02401
 0.10468,-0.02427
 0.10722,-0.02453
 0.10978,-0.02480
 0.11236,-0.02505
 0.11496,-0.02532
 0.11759,-0.02558
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 0.12292,-0.02608
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 0.14230,-0.02784
 0.14516,-0.02808
 0.14806,-0.02832
 0.15099,-0.02856
 0.15392,-0.02880
 0.15689,-0.02903
 0.15989,-0.02926
 0.16292,-0.02949
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 0.16906,-0.02993
 0.17217,-0.03016
 0.17531,-0.03038
 0.17848,-0.03059
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 0.31532,-0.03711
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 0.33856,-0.03774
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 0.36306,-0.03827
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 1.00000, 0.00000