ファイルインデックス名　: File Index Name        : 1170        .A  
翼型整理番号　　　　　　: Airfoil Serial No.     : N04-0075-1
翼型名　　　　　　　　　: Airfoil Name           : N.A.C.A. 65-210
翼型ファイル番号　　　　: Airfoil File No.       : 1170
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
 0.98658, 0.00156
 0.97335, 0.00319
 0.96031, 0.00487
 0.94746, 0.00658
 0.93479, 0.00833
 0.92230, 0.01009
 0.90999, 0.01186
 0.89785, 0.01362
 0.88590, 0.01536
 0.87410, 0.01709
 0.86248, 0.01879
 0.85102, 0.02047
 0.83972, 0.02213
 0.82858, 0.02376
 0.81760, 0.02536
 0.80676, 0.02692
 0.79608, 0.02845
 0.78556, 0.02994
 0.77517, 0.03140
 0.76493, 0.03281
 0.75482, 0.03420
 0.74486, 0.03554
 0.73504, 0.03685
 0.72534, 0.03812
 0.71578, 0.03935
 0.70635, 0.04055
 0.69704, 0.04170
 0.68786, 0.04281
 0.67879, 0.04390
 0.66985, 0.04494
 0.66103, 0.04593
 0.65232, 0.04690
 0.64373, 0.04784
 0.63525, 0.04874
 0.62688, 0.04960
 0.61862, 0.05042
 0.61047, 0.05122
 0.60242, 0.05198
 0.59447, 0.05269
 0.58663, 0.05339
 0.57889, 0.05404
 0.57124, 0.05466
 0.56369, 0.05526
 0.55624, 0.05581
 0.54888, 0.05634
 0.54160, 0.05683
 0.53443, 0.05730
 0.52734, 0.05773
 0.52034, 0.05813
 0.51342, 0.05850
 0.50659, 0.05885
 0.49985, 0.05916
 0.49319, 0.05943
 0.48661, 0.05968
 0.48010, 0.05989
 0.47368, 0.06007
 0.46733, 0.06024
 0.46106, 0.06038
 0.45487, 0.06050
 0.44874, 0.06059
 0.44269, 0.06068
 0.43671, 0.06073
 0.43079, 0.06077
 0.42495, 0.06079
 0.41918, 0.06078
 0.41347, 0.06077
 0.40784, 0.06074
 0.40226, 0.06069
 0.39674, 0.06064
 0.39129, 0.06056
 0.38590, 0.06048
 0.38058, 0.06038
 0.37531, 0.06027
 0.37010, 0.06014
 0.36495, 0.06001
 0.35985, 0.05987
 0.35481, 0.05972
 0.34983, 0.05955
 0.34490, 0.05939
 0.34002, 0.05921
 0.33520, 0.05902
 0.33043, 0.05883
 0.32571, 0.05862
 0.32104, 0.05842
 0.31643, 0.05820
 0.31186, 0.05798
 0.30734, 0.05775
 0.30287, 0.05751
 0.29844, 0.05727
 0.29407, 0.05702
 0.28973, 0.05677
 0.28544, 0.05651
 0.28120, 0.05624
 0.27701, 0.05597
 0.27285, 0.05570
 0.26873, 0.05541
 0.26467, 0.05513
 0.26064, 0.05484
 0.25666, 0.05454
 0.25271, 0.05424
 0.24880, 0.05393
 0.24493, 0.05363
 0.24111, 0.05332
 0.23732, 0.05300
 0.23356, 0.05268
 0.22985, 0.05235
 0.22618, 0.05202
 0.22254, 0.05169
 0.21894, 0.05136
 0.21536, 0.05102
 0.21183, 0.05067
 0.20833, 0.05033
 0.20486, 0.04997
 0.20143, 0.04962
 0.19803, 0.04927
 0.19467, 0.04891
 0.19133, 0.04855
 0.18803, 0.04818
 0.18476, 0.04782
 0.18152, 0.04746
 0.17832, 0.04709
 0.17515, 0.04671
 0.17200, 0.04633
 0.16888, 0.04595
 0.16579, 0.04557
 0.16274, 0.04518
 0.15971, 0.04480
 0.15670, 0.04441
 0.15372, 0.04401
 0.15078, 0.04362
 0.14786, 0.04323
 0.14497, 0.04282
 0.14211, 0.04242
 0.13926, 0.04202
 0.13646, 0.04161
 0.13366, 0.04121
 0.13091, 0.04080
 0.12817, 0.04038
 0.12545, 0.03997
 0.12277, 0.03955
 0.12011, 0.03912
 0.11746, 0.03870
 0.11485, 0.03828
 0.11225, 0.03785
 0.10968, 0.03742
 0.10714, 0.03699
 0.10461, 0.03655
 0.10211, 0.03611
 0.09964, 0.03567
 0.09717, 0.03523
 0.09474, 0.03479
 0.09232, 0.03434
 0.08993, 0.03388
 0.08756, 0.03343
 0.08520, 0.03297
 0.08287, 0.03252
 0.08056, 0.03205
 0.07827, 0.03159
 0.07600, 0.03112
 0.07375, 0.03065
 0.07151, 0.03017
 0.06930, 0.02970
 0.06710, 0.02921
 0.06493, 0.02873
 0.06277, 0.02824
 0.06063, 0.02775
 0.05852, 0.02725
 0.05641, 0.02676
 0.05432, 0.02625
 0.05225, 0.02573
 0.05021, 0.02522
 0.04818, 0.02471
 0.04616, 0.02418
 0.04416, 0.02364
 0.04218, 0.02311
 0.04022, 0.02256
 0.03827, 0.02201
 0.03634, 0.02145
 0.03442, 0.02088
 0.03253, 0.02031
 0.03065, 0.01973
 0.02878, 0.01913
 0.02693, 0.01853
 0.02509, 0.01792
 0.02327, 0.01730
 0.02147, 0.01668
 0.01968, 0.01604
 0.01791, 0.01538
 0.01615, 0.01469
 0.01441, 0.01397
 0.01269, 0.01320
 0.01099, 0.01238
 0.00930, 0.01150
 0.00764, 0.01054
 0.00600, 0.00946
 0.00439, 0.00823
 0.00280, 0.00674
 0.00128, 0.00479
 0.00033, 0.00279
 0.00000, 0.00000
 0.00000, 0.00000
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 0.03166,-0.01508
 0.03361,-0.01548
 0.03558,-0.01586
 0.03755,-0.01624
 0.03955,-0.01661
 0.04155,-0.01698
 0.04358,-0.01734
 0.04562,-0.01769
 0.04767,-0.01804
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 0.05393,-0.01905
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 0.06252,-0.02035
 0.06471,-0.02066
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 0.07364,-0.02189
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 0.08054,-0.02278
 0.08287,-0.02308
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 0.08760,-0.02365
 0.09000,-0.02394
 0.09241,-0.02423
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 0.09978,-0.02507
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 0.10989,-0.02615
 0.11247,-0.02642
 0.11508,-0.02668
 0.11771,-0.02694
 0.12036,-0.02720
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 0.14242,-0.02921
 0.14528,-0.02945
 0.14818,-0.02969
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 0.15404,-0.03016
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 0.16304,-0.03087
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 0.17859,-0.03200
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 0.31542,-0.03827
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 0.49477,-0.03731
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 1.00000, 0.00000