ファイルインデックス名　: File Index Name        : 1026        .A00
翼型整理番号　　　　　　: Airfoil Serial No.     : N01-0026-0
翼型名　　　　　　　　　: Airfoil Name           : N.A.C.A. 2410
翼型ファイル番号　　　　: Airfoil File No.       : 1026
翼型情報　　　　　　　　: Airfoil Information    : Computed

算出前縁半径　　　　　　: Computed L.E.R.        : 1.1 %
算出前縁傾斜　　　　　　: Computed Slope of L.E. : 0.1
算出プログラム番号　　　: Computed Program No.   : ウハク-40B


座標　　　　　　　　　　: Plot Ordinates         :

 X             Y

 1.00007, 0.00105
 0.98688, 0.00346
 0.97388, 0.00580
 0.96107, 0.00806
 0.94844, 0.01024
 0.93598, 0.01236
 0.92371, 0.01441
 0.91161, 0.01639
 0.89967, 0.01832
 0.88791, 0.02018
 0.87631, 0.02198
 0.86487, 0.02373
 0.85359, 0.02543
 0.84246, 0.02707
 0.83149, 0.02866
 0.82066, 0.03021
 0.80999, 0.03170
 0.79945, 0.03316
 0.78906, 0.03456
 0.77881, 0.03593
 0.76870, 0.03725
 0.75872, 0.03854
 0.74888, 0.03978
 0.73916, 0.04099
 0.72958, 0.04216
 0.72012, 0.04329
 0.71078, 0.04439
 0.70156, 0.04545
 0.69247, 0.04649
 0.68349, 0.04749
 0.67463, 0.04845
 0.66588, 0.04939
 0.65724, 0.05030
 0.64871, 0.05118
 0.64029, 0.05203
 0.63198, 0.05286
 0.62377, 0.05366
 0.61566, 0.05443
 0.60766, 0.05517
 0.59975, 0.05590
 0.59194, 0.05659
 0.58423, 0.05727
 0.57662, 0.05792
 0.56909, 0.05854
 0.56166, 0.05915
 0.55432, 0.05973
 0.54707, 0.06029
 0.53990, 0.06083
 0.53282, 0.06136
 0.52583, 0.06186
 0.51892, 0.06234
 0.51209, 0.06280
 0.50534, 0.06325
 0.49867, 0.06367
 0.49208, 0.06408
 0.48557, 0.06447
 0.47913, 0.06485
 0.47277, 0.06520
 0.46648, 0.06554
 0.46026, 0.06587
 0.45412, 0.06618
 0.44804, 0.06647
 0.44204, 0.06675
 0.43610, 0.06701
 0.43023, 0.06726
 0.42443, 0.06750
 0.41869, 0.06772
 0.41302, 0.06793
 0.40741, 0.06812
 0.40186, 0.06830
 0.39635, 0.06847
 0.39089, 0.06862
 0.38548, 0.06875
 0.38014, 0.06887
 0.37485, 0.06897
 0.36963, 0.06906
 0.36446, 0.06913
 0.35934, 0.06919
 0.35428, 0.06923
 0.34928, 0.06926
 0.34433, 0.06927
 0.33943, 0.06927
 0.33458, 0.06926
 0.32978, 0.06923
 0.32504, 0.06920
 0.32035, 0.06915
 0.31570, 0.06908
 0.31110, 0.06901
 0.30656, 0.06892
 0.30206, 0.06883
 0.29760, 0.06872
 0.29319, 0.06860
 0.28883, 0.06847
 0.28451, 0.06833
 0.28024, 0.06818
 0.27601, 0.06802
 0.27183, 0.06785
 0.26768, 0.06767
 0.26358, 0.06748
 0.25952, 0.06728
 0.25551, 0.06707
 0.25153, 0.06686
 0.24759, 0.06663
 0.24369, 0.06640
 0.23983, 0.06615
 0.23601, 0.06590
 0.23223, 0.06564
 0.22848, 0.06538
 0.22477, 0.06510
 0.22110, 0.06482
 0.21747, 0.06453
 0.21387, 0.06423
 0.21030, 0.06392
 0.20677, 0.06361
 0.20328, 0.06329
 0.19982, 0.06297
 0.19639, 0.06263
 0.19299, 0.06229
 0.18963, 0.06195
 0.18630, 0.06159
 0.18300, 0.06123
 0.17974, 0.06087
 0.17650, 0.06049
 0.17330, 0.06011
 0.17013, 0.05973
 0.16698, 0.05934
 0.16387, 0.05894
 0.16078, 0.05854
 0.15773, 0.05813
 0.15470, 0.05771
 0.15170, 0.05729
 0.14873, 0.05686
 0.14579, 0.05643
 0.14287, 0.05599
 0.13999, 0.05555
 0.13712, 0.05510
 0.13429, 0.05465
 0.13148, 0.05419
 0.12870, 0.05372
 0.12594, 0.05325
 0.12321, 0.05277
 0.12050, 0.05229
 0.11782, 0.05180
 0.11516, 0.05131
 0.11253, 0.05081
 0.10992, 0.05030
 0.10733, 0.04979
 0.10477, 0.04928
 0.10223, 0.04875
 0.09972, 0.04823
 0.09722, 0.04769
 0.09475, 0.04716
 0.09230, 0.04661
 0.08987, 0.04606
 0.08747, 0.04550
 0.08509, 0.04494
 0.08272, 0.04437
 0.08038, 0.04380
 0.07806, 0.04321
 0.07576, 0.04263
 0.07348, 0.04203
 0.07123, 0.04143
 0.06899, 0.04082
 0.06677, 0.04020
 0.06457, 0.03958
 0.06239, 0.03895
 0.06023, 0.03831
 0.05809, 0.03766
 0.05597, 0.03700
 0.05387, 0.03634
 0.05178, 0.03566
 0.04972, 0.03498
 0.04767, 0.03428
 0.04564, 0.03358
 0.04363, 0.03286
 0.04164, 0.03213
 0.03967, 0.03139
 0.03771, 0.03064
 0.03577, 0.02987
 0.03385, 0.02908
 0.03195, 0.02828
 0.03007, 0.02747
 0.02820, 0.02663
 0.02635, 0.02577
 0.02452, 0.02489
 0.02271, 0.02398
 0.02091, 0.02305
 0.01913, 0.02209
 0.01738, 0.02109
 0.01564, 0.02005
 0.01392, 0.01896
 0.01222, 0.01782
 0.01054, 0.01661
 0.00888, 0.01533
 0.00725, 0.01394
 0.00564, 0.01242
 0.00407, 0.01071
 0.00254, 0.00870
 0.00109, 0.00612
 0.00021, 0.00352
 0.00000, 0.00000
 0.00000, 0.00000
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 0.07917,-0.02822
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 0.08850,-0.02908
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 0.10306,-0.03017
 0.10556,-0.03033
 0.10807,-0.03049
 0.11061,-0.03064
 0.11317,-0.03078
 0.11575,-0.03092
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 0.14279,-0.03201
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