ファイルインデックス名　: File Index Name        : 1136        .A  
翼型整理番号　　　　　　: Airfoil Serial No.     : N04-0041-1
翼型名　　　　　　　　　: Airfoil Name           : N.A.C.A. 64-110
翼型ファイル番号　　　　: Airfoil File No.       : 1136
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-A01B1


座標　　　　　　　　　　: Plot Ordinates         :

 X             Y

 1.00000, 0.00000
 0.98667, 0.00094
 0.97354, 0.00197
 0.96059, 0.00309
 0.94783, 0.00427
 0.93526, 0.00552
 0.92286, 0.00680
 0.91065, 0.00812
 0.89860, 0.00946
 0.88674, 0.01080
 0.87503, 0.01216
 0.86349, 0.01352
 0.85211, 0.01488
 0.84090, 0.01623
 0.82984, 0.01757
 0.81894, 0.01890
 0.80818, 0.02022
 0.79758, 0.02152
 0.78712, 0.02280
 0.77680, 0.02406
 0.76663, 0.02530
 0.75659, 0.02652
 0.74669, 0.02771
 0.73693, 0.02887
 0.72729, 0.03001
 0.71778, 0.03111
 0.70841, 0.03220
 0.69915, 0.03325
 0.69002, 0.03427
 0.68101, 0.03528
 0.67211, 0.03625
 0.66334, 0.03721
 0.65467, 0.03812
 0.64612, 0.03903
 0.63767, 0.03989
 0.62935, 0.04073
 0.62112, 0.04155
 0.61300, 0.04234
 0.60499, 0.04310
 0.59707, 0.04384
 0.58925, 0.04455
 0.58154, 0.04524
 0.57391, 0.04590
 0.56638, 0.04653
 0.55896, 0.04715
 0.55161, 0.04774
 0.54436, 0.04830
 0.53720, 0.04885
 0.53013, 0.04936
 0.52313, 0.04986
 0.51623, 0.05033
 0.50942, 0.05079
 0.50268, 0.05121
 0.49602, 0.05162
 0.48944, 0.05200
 0.48294, 0.05237
 0.47653, 0.05270
 0.47017, 0.05302
 0.46390, 0.05332
 0.45771, 0.05359
 0.45158, 0.05384
 0.44553, 0.05408
 0.43954, 0.05430
 0.43362, 0.05450
 0.42777, 0.05467
 0.42200, 0.05482
 0.41628, 0.05496
 0.41064, 0.05507
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 0.38867, 0.05530
 0.38334, 0.05531
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 0.36768, 0.05522
 0.36257, 0.05515
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 0.34759, 0.05492
 0.34271, 0.05482
 0.33787, 0.05471
 0.33309, 0.05460
 0.32836, 0.05448
 0.32368, 0.05434
 0.31905, 0.05420
 0.31447, 0.05405
 0.30994, 0.05389
 0.30545, 0.05372
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 0.29227, 0.05319
 0.28797, 0.05299
 0.28372, 0.05279
 0.27951, 0.05258
 0.27534, 0.05237
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 0.25513, 0.05122
 0.25120, 0.05097
 0.24732, 0.05072
 0.24348, 0.05047
 0.23967, 0.05020
 0.23590, 0.04994
 0.23217, 0.04966
 0.22848, 0.04940
 0.22483, 0.04912
 0.22121, 0.04883
 0.21762, 0.04854
 0.21407, 0.04825
 0.21055, 0.04797
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 0.20362, 0.04736
 0.20020, 0.04706
 0.19683, 0.04676
 0.19347, 0.04645
 0.19015, 0.04614
 0.18686, 0.04582
 0.18361, 0.04550
 0.18038, 0.04518
 0.17720, 0.04485
 0.17403, 0.04453
 0.17089, 0.04420
 0.16779, 0.04387
 0.16471, 0.04353
 0.16166, 0.04320
 0.15864, 0.04285
 0.15564, 0.04250
 0.15268, 0.04216
 0.14974, 0.04182
 0.14684, 0.04146
 0.14395, 0.04110
 0.14109, 0.04075
 0.13826, 0.04039
 0.13545, 0.04002
 0.13267, 0.03966
 0.12992, 0.03929
 0.12718, 0.03893
 0.12448, 0.03855
 0.12180, 0.03817
 0.11913, 0.03780
 0.11650, 0.03742
 0.11388, 0.03703
 0.11129, 0.03664
 0.10873, 0.03625
 0.10618, 0.03586
 0.10366, 0.03547
 0.10117, 0.03507
 0.09868, 0.03467
 0.09623, 0.03426
 0.09379, 0.03386
 0.09137, 0.03345
 0.08898, 0.03304
 0.08661, 0.03262
 0.08426, 0.03220
 0.08192, 0.03178
 0.07961, 0.03135
 0.07732, 0.03093
 0.07505, 0.03049
 0.07279, 0.03006
 0.07056, 0.02961
 0.06833, 0.02917
 0.06614, 0.02871
 0.06396, 0.02826
 0.06180, 0.02780
 0.05966, 0.02734
 0.05753, 0.02687
 0.05542, 0.02639
 0.05333, 0.02591
 0.05126, 0.02544
 0.04921, 0.02494
 0.04717, 0.02444
 0.04514, 0.02394
 0.04315, 0.02342
 0.04116, 0.02290
 0.03918, 0.02237
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 0.03529, 0.02128
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 0.00639, 0.00974
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 0.00308, 0.00701
 0.00147, 0.00504
 0.00044, 0.00296
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