ファイルインデックス名　: File Index Name        : 1320        .A  
翼型整理番号　　　　　　: Airfoil Serial No.     : N06-0042-1
翼型名　　　　　　　　　: Airfoil Name           : N.A.C.A. 19
翼型ファイル番号　　　　: Airfoil File No.       : 1320
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

 0.99987, 0.00132
 0.98629, 0.00414
 0.97293, 0.00685
 0.95977, 0.00948
 0.94680, 0.01202
 0.93404, 0.01448
 0.92146, 0.01685
 0.90907, 0.01915
 0.89686, 0.02137
 0.88483, 0.02351
 0.87297, 0.02558
 0.86129, 0.02758
 0.84978, 0.02952
 0.83843, 0.03140
 0.82725, 0.03321
 0.81622, 0.03497
 0.80535, 0.03667
 0.79463, 0.03833
 0.78407, 0.03994
 0.77365, 0.04151
 0.76337, 0.04302
 0.75324, 0.04449
 0.74324, 0.04592
 0.73339, 0.04730
 0.72367, 0.04864
 0.71408, 0.04994
 0.70462, 0.05120
 0.69529, 0.05241
 0.68608, 0.05360
 0.67700, 0.05475
 0.66802, 0.05587
 0.65919, 0.05694
 0.65045, 0.05798
 0.64184, 0.05900
 0.63333, 0.05997
 0.62495, 0.06091
 0.61667, 0.06183
 0.60849, 0.06271
 0.60042, 0.06356
 0.59245, 0.06437
 0.58458, 0.06515
 0.57683, 0.06591
 0.56915, 0.06664
 0.56158, 0.06735
 0.55412, 0.06802
 0.54673, 0.06867
 0.53944, 0.06930
 0.53224, 0.06990
 0.52513, 0.07048
 0.51810, 0.07104
 0.51117, 0.07158
 0.50432, 0.07208
 0.49755, 0.07258
 0.49086, 0.07307
 0.48425, 0.07353
 0.47772, 0.07397
 0.47128, 0.07439
 0.46490, 0.07479
 0.45860, 0.07518
 0.45238, 0.07555
 0.44623, 0.07589
 0.44015, 0.07622
 0.43414, 0.07653
 0.42820, 0.07682
 0.42233, 0.07709
 0.41654, 0.07735
 0.41081, 0.07759
 0.40514, 0.07781
 0.39954, 0.07801
 0.39400, 0.07821
 0.38853, 0.07839
 0.38311, 0.07854
 0.37777, 0.07868
 0.37247, 0.07881
 0.36724, 0.07891
 0.36207, 0.07901
 0.35695, 0.07909
 0.35190, 0.07914
 0.34689, 0.07919
 0.34195, 0.07922
 0.33706, 0.07923
 0.33222, 0.07923
 0.32743, 0.07921
 0.32271, 0.07918
 0.31802, 0.07913
 0.31340, 0.07907
 0.30881, 0.07899
 0.30428, 0.07890
 0.29980, 0.07879
 0.29537, 0.07868
 0.29099, 0.07854
 0.28665, 0.07838
 0.28235, 0.07823
 0.27811, 0.07804
 0.27391, 0.07785
 0.26975, 0.07763
 0.26563, 0.07741
 0.26157, 0.07718
 0.25754, 0.07692
 0.25356, 0.07665
 0.24962, 0.07637
 0.24571, 0.07607
 0.24185, 0.07575
 0.23803, 0.07542
 0.23425, 0.07507
 0.23050, 0.07470
 0.22680, 0.07433
 0.22314, 0.07394
 0.21951, 0.07355
 0.21592, 0.07313
 0.21236, 0.07271
 0.20885, 0.07227
 0.20536, 0.07183
 0.20191, 0.07136
 0.19850, 0.07089
 0.19512, 0.07040
 0.19178, 0.06990
 0.18846, 0.06940
 0.18518, 0.06888
 0.18193, 0.06835
 0.17872, 0.06781
 0.17553, 0.06726
 0.17239, 0.06670
 0.16926, 0.06614
 0.16617, 0.06555
 0.16311, 0.06498
 0.16008, 0.06438
 0.15708, 0.06378
 0.15410, 0.06317
 0.15115, 0.06255
 0.14824, 0.06192
 0.14535, 0.06129
 0.14249, 0.06067
 0.13966, 0.06002
 0.13684, 0.05936
 0.13407, 0.05871
 0.13131, 0.05805
 0.12858, 0.05737
 0.12588, 0.05670
 0.12320, 0.05601
 0.12055, 0.05531
 0.11792, 0.05460
 0.11531, 0.05390
 0.11273, 0.05318
 0.11018, 0.05245
 0.10764, 0.05171
 0.10514, 0.05097
 0.10265, 0.05022
 0.10019, 0.04946
 0.09776, 0.04868
 0.09533, 0.04789
 0.09294, 0.04710
 0.09056, 0.04630
 0.08822, 0.04549
 0.08589, 0.04468
 0.08358, 0.04386
 0.08129, 0.04304
 0.07903, 0.04221
 0.07678, 0.04137
 0.07455, 0.04053
 0.07235, 0.03969
 0.07015, 0.03883
 0.06799, 0.03798
 0.06584, 0.03712
 0.06371, 0.03626
 0.06160, 0.03539
 0.05951, 0.03452
 0.05743, 0.03364
 0.05537, 0.03276
 0.05333, 0.03187
 0.05131, 0.03098
 0.04931, 0.03009
 0.04733, 0.02920
 0.04536, 0.02830
 0.04340, 0.02739
 0.04147, 0.02649
 0.03955, 0.02557
 0.03765, 0.02465
 0.03577, 0.02374
 0.03389, 0.02280
 0.03205, 0.02188
 0.03021, 0.02094
 0.02838, 0.01999
 0.02658, 0.01905
 0.02479, 0.01808
 0.02301, 0.01712
 0.02125, 0.01615
 0.01951, 0.01517
 0.01778, 0.01417
 0.01607, 0.01318
 0.01437, 0.01215
 0.01268, 0.01112
 0.01102, 0.01006
 0.00937, 0.00898
 0.00774, 0.00787
 0.00613, 0.00671
 0.00453, 0.00550
 0.00295, 0.00417
 0.00141, 0.00267
 0.00042, 0.00138
 0.00000, 0.00000
 0.00000, 0.00000
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