ファイルインデックス名　: File Index Name        : 1324        .A  
翼型整理番号　　　　　　: Airfoil Serial No.     : N06-0046-1
翼型名　　　　　　　　　: Airfoil Name           : N.A.C.A. 24
翼型ファイル番号　　　　: Airfoil File No.       : 1324
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
 0.98669, 0.00015
 0.97355, 0.00049
 0.96058, 0.00098
 0.94777, 0.00162
 0.93514, 0.00240
 0.92267, 0.00329
 0.91037, 0.00428
 0.89822, 0.00536
 0.88624, 0.00651
 0.87441, 0.00773
 0.86275, 0.00901
 0.85123, 0.01035
 0.83987, 0.01173
 0.82866, 0.01314
 0.81760, 0.01459
 0.80669, 0.01607
 0.79592, 0.01756
 0.78530, 0.01904
 0.77481, 0.02054
 0.76448, 0.02205
 0.75427, 0.02355
 0.74420, 0.02506
 0.73426, 0.02657
 0.72445, 0.02808
 0.71478, 0.02958
 0.70523, 0.03108
 0.69580, 0.03256
 0.68650, 0.03401
 0.67732, 0.03545
 0.66825, 0.03688
 0.65932, 0.03828
 0.65048, 0.03967
 0.64177, 0.04105
 0.63317, 0.04240
 0.62468, 0.04374
 0.61630, 0.04506
 0.60802, 0.04635
 0.59986, 0.04762
 0.59178, 0.04887
 0.58382, 0.05008
 0.57596, 0.05127
 0.56819, 0.05244
 0.56053, 0.05359
 0.55296, 0.05471
 0.54548, 0.05581
 0.53810, 0.05688
 0.53080, 0.05792
 0.52360, 0.05895
 0.51649, 0.05994
 0.50947, 0.06092
 0.50253, 0.06186
 0.49568, 0.06278
 0.48891, 0.06366
 0.48222, 0.06451
 0.47561, 0.06535
 0.46909, 0.06615
 0.46264, 0.06693
 0.45627, 0.06769
 0.44998, 0.06842
 0.44376, 0.06913
 0.43762, 0.06981
 0.43155, 0.07046
 0.42554, 0.07110
 0.41961, 0.07171
 0.41376, 0.07230
 0.40797, 0.07286
 0.40225, 0.07340
 0.39659, 0.07391
 0.39100, 0.07438
 0.38548, 0.07484
 0.38001, 0.07527
 0.37462, 0.07568
 0.36929, 0.07607
 0.36401, 0.07644
 0.35880, 0.07678
 0.35365, 0.07711
 0.34855, 0.07742
 0.34351, 0.07771
 0.33853, 0.07796
 0.33361, 0.07821
 0.32873, 0.07843
 0.32391, 0.07864
 0.31916, 0.07882
 0.31444, 0.07899
 0.30979, 0.07914
 0.30518, 0.07927
 0.30062, 0.07938
 0.29612, 0.07948
 0.29166, 0.07955
 0.28726, 0.07960
 0.28290, 0.07964
 0.27858, 0.07967
 0.27432, 0.07967
 0.27010, 0.07966
 0.26593, 0.07964
 0.26179, 0.07960
 0.25771, 0.07954
 0.25367, 0.07948
 0.24967, 0.07939
 0.24572, 0.07929
 0.24179, 0.07918
 0.23792, 0.07905
 0.23409, 0.07892
 0.23029, 0.07877
 0.22654, 0.07861
 0.22282, 0.07843
 0.21915, 0.07824
 0.21551, 0.07803
 0.21191, 0.07782
 0.20835, 0.07759
 0.20482, 0.07735
 0.20133, 0.07710
 0.19787, 0.07684
 0.19445, 0.07656
 0.19106, 0.07628
 0.18771, 0.07599
 0.18439, 0.07567
 0.18110, 0.07536
 0.17785, 0.07503
 0.17463, 0.07469
 0.17144, 0.07434
 0.16829, 0.07398
 0.16517, 0.07361
 0.16207, 0.07323
 0.15901, 0.07283
 0.15598, 0.07243
 0.15298, 0.07202
 0.15000, 0.07160
 0.14705, 0.07116
 0.14414, 0.07071
 0.14126, 0.07025
 0.13840, 0.06979
 0.13557, 0.06930
 0.13277, 0.06881
 0.13000, 0.06832
 0.12724, 0.06782
 0.12453, 0.06730
 0.12183, 0.06677
 0.11916, 0.06624
 0.11652, 0.06571
 0.11390, 0.06515
 0.11130, 0.06459
 0.10873, 0.06403
 0.10619, 0.06345
 0.10366, 0.06287
 0.10117, 0.06229
 0.09870, 0.06168
 0.09624, 0.06108
 0.09382, 0.06048
 0.09141, 0.05986
 0.08903, 0.05923
 0.08667, 0.05859
 0.08433, 0.05795
 0.08202, 0.05729
 0.07972, 0.05663
 0.07745, 0.05595
 0.07520, 0.05526
 0.07297, 0.05456
 0.07077, 0.05384
 0.06858, 0.05312
 0.06641, 0.05238
 0.06427, 0.05163
 0.06214, 0.05086
 0.06005, 0.05009
 0.05796, 0.04930
 0.05590, 0.04850
 0.05386, 0.04770
 0.05183, 0.04686
 0.04982, 0.04603
 0.04783, 0.04516
 0.04587, 0.04430
 0.04393, 0.04341
 0.04200, 0.04251
 0.04009, 0.04158
 0.03820, 0.04065
 0.03633, 0.03970
 0.03447, 0.03873
 0.03265, 0.03775
 0.03082, 0.03675
 0.02903, 0.03572
 0.02725, 0.03467
 0.02549, 0.03361
 0.02375, 0.03252
 0.02202, 0.03140
 0.02032, 0.03026
 0.01863, 0.02909
 0.01697, 0.02788
 0.01532, 0.02661
 0.01370, 0.02532
 0.01210, 0.02395
 0.01052, 0.02252
 0.00897, 0.02100
 0.00744, 0.01938
 0.00596, 0.01765
 0.00450, 0.01574
 0.00310, 0.01358
 0.00176, 0.01104
 0.00054, 0.00779
-0.00009, 0.00448
 0.00000, 0.00000
 0.00000, 0.00000
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 0.00272,-0.00716
 0.00482,-0.00994
 0.00683,-0.01202
 0.00880,-0.01374
 0.01075,-0.01521
 0.01268,-0.01652
 0.01461,-0.01770
 0.01654,-0.01877
 0.01848,-0.01979
 0.02041,-0.02072
 0.02235,-0.02159
 0.02430,-0.02241
 0.02625,-0.02320
 0.02822,-0.02394
 0.03019,-0.02465
 0.03218,-0.02533
 0.03418,-0.02597
 0.03619,-0.02659
 0.03820,-0.02719
 0.04023,-0.02776
 0.04228,-0.02832
 0.04433,-0.02884
 0.04640,-0.02936
 0.04848,-0.02985
 0.05057,-0.03032
 0.05269,-0.03079
 0.05482,-0.03124
 0.05695,-0.03168
 0.05910,-0.03209
 0.06127,-0.03249
 0.06346,-0.03289
 0.06566,-0.03327
 0.06787,-0.03363
 0.07011,-0.03398
 0.07236,-0.03432
 0.07461,-0.03464
 0.07690,-0.03495
 0.07919,-0.03525
 0.08151,-0.03553
 0.08384,-0.03580
 0.08619,-0.03607
 0.08856,-0.03632
 0.09094,-0.03656
 0.09335,-0.03680
 0.09577,-0.03702
 0.09821,-0.03724
 0.10067,-0.03746
 0.10316,-0.03767
 0.10566,-0.03787
 0.10819,-0.03807
 0.11073,-0.03826
 0.11330,-0.03844
 0.11588,-0.03862
 0.11849,-0.03879
 0.12112,-0.03896
 0.12377,-0.03911
 0.12644,-0.03926
 0.12915,-0.03941
 0.13187,-0.03955
 0.13461,-0.03968
 0.13737,-0.03981
 0.14016,-0.03993
 0.14297,-0.04004
 0.14582,-0.04015
 0.14867,-0.04025
 0.15156,-0.04035
 0.15448,-0.04044
 0.15741,-0.04053
 0.16037,-0.04060
 0.16336,-0.04067
 0.16638,-0.04073
 0.16943,-0.04079
 0.17250,-0.04085
 0.17559,-0.04090
 0.17872,-0.04094
 0.18188,-0.04098
 0.18506,-0.04101
 0.18826,-0.04104
 0.19151,-0.04107
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 0.22564,-0.04102
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 0.25537,-0.04059
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 0.26713,-0.04033
 0.27113,-0.04023
 0.27516,-0.04013
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 0.28336,-0.03990
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 0.31339,-0.03897
 0.31786,-0.03883
 0.32238,-0.03867
 0.32695,-0.03851
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 0.34092,-0.03801
 0.34569,-0.03783
 0.35050,-0.03764
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 0.36027,-0.03726
 0.36524,-0.03706
 0.37027,-0.03686
 0.37534,-0.03665
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 0.39091,-0.03600
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 0.42363,-0.03454
 0.42930,-0.03428
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 0.44670,-0.03345
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 0.49615,-0.03100
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 0.65103,-0.02241
 0.65946,-0.02190
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 0.68545,-0.02031
 0.69434,-0.01975
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 1.00000, 0.00000