ファイルインデックス名　: File Index Name        : 1077-2      .A00
翼型整理番号　　　　　　: Airfoil Serial No.     : N02-0005-2
翼型名　　　　　　　　　: Airfoil Name           : N.A.C.A. 23012
翼型ファイル番号　　　　: Airfoil File No.       : 1077
翼型情報　　　　　　　　: Airfoil Information    : Computed

算出前縁半径　　　　　　: Computed L.E.R.        : 1.59 %
算出前縁傾斜　　　　　　: Computed Slope of L.E. : ?
算出プログラム番号　　　: Computed Program No.   : W.S. Design A


座標　　　　　　　　　　: Plot Ordinates         :

 X             Y

 1.00003, 0.00126
 0.98678, 0.00340
 0.97373, 0.00548
 0.96087, 0.00750
 0.94819, 0.00947
 0.93571, 0.01138
 0.92341, 0.01325
 0.91128, 0.01506
 0.89932, 0.01682
 0.88754, 0.01854
 0.87593, 0.02022
 0.86448, 0.02185
 0.85319, 0.02344
 0.84205, 0.02500
 0.83108, 0.02651
 0.82026, 0.02799
 0.80959, 0.02943
 0.79906, 0.03083
 0.78869, 0.03221
 0.77844, 0.03355
 0.76835, 0.03485
 0.75838, 0.03613
 0.74855, 0.03738
 0.73886, 0.03859
 0.72930, 0.03978
 0.71986, 0.04094
 0.71055, 0.04207
 0.70136, 0.04318
 0.69229, 0.04426
 0.68334, 0.04531
 0.67449, 0.04634
 0.66578, 0.04734
 0.65717, 0.04832
 0.64868, 0.04928
 0.64028, 0.05022
 0.63201, 0.05113
 0.62383, 0.05202
 0.61576, 0.05288
 0.60779, 0.05373
 0.59992, 0.05455
 0.59214, 0.05536
 0.58448, 0.05614
 0.57689, 0.05691
 0.56940, 0.05765
 0.56202, 0.05838
 0.55471, 0.05909
 0.54749, 0.05978
 0.54036, 0.06045
 0.53332, 0.06110
 0.52636, 0.06174
 0.51949, 0.06235
 0.51270, 0.06295
 0.50599, 0.06354
 0.49936, 0.06411
 0.49281, 0.06466
 0.48633, 0.06519
 0.47994, 0.06571
 0.47361, 0.06622
 0.46735, 0.06671
 0.46118, 0.06718
 0.45507, 0.06764
 0.44903, 0.06808
 0.44306, 0.06851
 0.43716, 0.06893
 0.43132, 0.06933
 0.42556, 0.06972
 0.41985, 0.07009
 0.41422, 0.07045
 0.40864, 0.07080
 0.40313, 0.07114
 0.39767, 0.07146
 0.39228, 0.07177
 0.38695, 0.07207
 0.38168, 0.07235
 0.37646, 0.07262
 0.37130, 0.07288
 0.36620, 0.07313
 0.36115, 0.07337
 0.35615, 0.07360
 0.35121, 0.07381
 0.34633, 0.07401
 0.34149, 0.07421
 0.33670, 0.07439
 0.33197, 0.07456
 0.32728, 0.07472
 0.32265, 0.07487
 0.31806, 0.07501
 0.31352, 0.07514
 0.30903, 0.07526
 0.30458, 0.07537
 0.30019, 0.07547
 0.29583, 0.07556
 0.29152, 0.07564
 0.28726, 0.07571
 0.28304, 0.07577
 0.27886, 0.07582
 0.27472, 0.07586
 0.27063, 0.07590
 0.26658, 0.07592
 0.26257, 0.07594
 0.25860, 0.07595
 0.25465, 0.07595
 0.25076, 0.07594
 0.24691, 0.07592
 0.24309, 0.07590
 0.23930, 0.07586
 0.23556, 0.07582
 0.23186, 0.07577
 0.22818, 0.07571
 0.22455, 0.07564
 0.22095, 0.07557
 0.21738, 0.07549
 0.21385, 0.07540
 0.21035, 0.07530
 0.20688, 0.07520
 0.20345, 0.07509
 0.20005, 0.07497
 0.19666, 0.07484
 0.19330, 0.07470
 0.18996, 0.07456
 0.18664, 0.07440
 0.18334, 0.07424
 0.18007, 0.07407
 0.17682, 0.07388
 0.17358, 0.07368
 0.17037, 0.07348
 0.16719, 0.07326
 0.16402, 0.07303
 0.16087, 0.07278
 0.15775, 0.07252
 0.15465, 0.07225
 0.15157, 0.07197
 0.14852, 0.07167
 0.14549, 0.07136
 0.14247, 0.07104
 0.13948, 0.07070
 0.13651, 0.07034
 0.13357, 0.06997
 0.13064, 0.06959
 0.12774, 0.06919
 0.12486, 0.06878
 0.12200, 0.06835
 0.11916, 0.06790
 0.11635, 0.06744
 0.11355, 0.06697
 0.11078, 0.06647
 0.10803, 0.06596
 0.10531, 0.06544
 0.10260, 0.06490
 0.09993, 0.06434
 0.09726, 0.06377
 0.09463, 0.06318
 0.09201, 0.06257
 0.08942, 0.06195
 0.08685, 0.06131
 0.08431, 0.06065
 0.08178, 0.05997
 0.07928, 0.05928
 0.07680, 0.05857
 0.07435, 0.05785
 0.07192, 0.05710
 0.06950, 0.05634
 0.06712, 0.05556
 0.06475, 0.05476
 0.06241, 0.05395
 0.06010, 0.05311
 0.05780, 0.05226
 0.05553, 0.05139
 0.05328, 0.05050
 0.05105, 0.04959
 0.04885, 0.04866
 0.04668, 0.04771
 0.04454, 0.04674
 0.04241, 0.04575
 0.04030, 0.04473
 0.03823, 0.04370
 0.03617, 0.04265
 0.03414, 0.04156
 0.03215, 0.04046
 0.03017, 0.03933
 0.02822, 0.03818
 0.02630, 0.03699
 0.02441, 0.03578
 0.02254, 0.03453
 0.02070, 0.03326
 0.01890, 0.03194
 0.01712, 0.03059
 0.01538, 0.02920
 0.01367, 0.02776
 0.01200, 0.02627
 0.01037, 0.02472
 0.00877, 0.02310
 0.00723, 0.02140
 0.00573, 0.01961
 0.00430, 0.01770
 0.00294, 0.01563
 0.00167, 0.01333
 0.00052, 0.01068
-0.00038, 0.00738
-0.00065, 0.00416
 0.00000, 0.00000
 0.00000, 0.00000
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 0.01066,-0.01162
 0.01276,-0.01272
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 0.02473,-0.01720
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 0.03444,-0.01965
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 0.03832,-0.02047
 0.04026,-0.02086
 0.04219,-0.02123
 0.04415,-0.02159
 0.04610,-0.02194
 0.04807,-0.02228
 0.05003,-0.02261
 0.05200,-0.02293
 0.05399,-0.02325
 0.05598,-0.02356
 0.05798,-0.02386
 0.05999,-0.02416
 0.06201,-0.02446
 0.06404,-0.02475
 0.06609,-0.02504
 0.06814,-0.02532
 0.07020,-0.02560
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 0.07437,-0.02616
 0.07648,-0.02644
 0.07860,-0.02671
 0.08074,-0.02699
 0.08289,-0.02726
 0.08506,-0.02754
 0.08724,-0.02781
 0.08944,-0.02808
 0.09165,-0.02835
 0.09389,-0.02863
 0.09614,-0.02890
 0.09841,-0.02918
 0.10071,-0.02945
 0.10302,-0.02973
 0.10535,-0.03000
 0.10770,-0.03028
 0.11007,-0.03056
 0.11247,-0.03084
 0.11488,-0.03112
 0.11733,-0.03141
 0.11979,-0.03169
 0.12228,-0.03198
 0.12480,-0.03226
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 0.12990,-0.03284
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 0.13775,-0.03372
 0.14044,-0.03401
 0.14313,-0.03431
 0.14587,-0.03461
 0.14864,-0.03490
 0.15143,-0.03520
 0.15425,-0.03550
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 0.16001,-0.03610
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 0.16589,-0.03669
 0.16889,-0.03699
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