ファイルインデックス名　: File Index Name        : 1323        .A  
翼型整理番号　　　　　　: Airfoil Serial No.     : N06-0045-1
翼型名　　　　　　　　　: Airfoil Name           : N.A.C.A. 23
翼型ファイル番号　　　　: Airfoil File No.       : 1323
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
 0.98670, 0.00007
 0.97358, 0.00028
 0.96063, 0.00063
 0.94785, 0.00109
 0.93525, 0.00165
 0.92281, 0.00233
 0.91054, 0.00308
 0.89843, 0.00391
 0.88649, 0.00480
 0.87470, 0.00576
 0.86307, 0.00677
 0.85160, 0.00782
 0.84028, 0.00892
 0.82911, 0.01005
 0.81810, 0.01121
 0.80722, 0.01239
 0.79650, 0.01359
 0.78593, 0.01477
 0.77548, 0.01598
 0.76518, 0.01719
 0.75502, 0.01840
 0.74499, 0.01963
 0.73510, 0.02084
 0.72533, 0.02207
 0.71569, 0.02329
 0.70619, 0.02450
 0.69680, 0.02571
 0.68754, 0.02690
 0.67839, 0.02809
 0.66936, 0.02926
 0.66046, 0.03042
 0.65167, 0.03157
 0.64299, 0.03270
 0.63442, 0.03382
 0.62597, 0.03492
 0.61762, 0.03601
 0.60937, 0.03708
 0.60124, 0.03814
 0.59320, 0.03917
 0.58526, 0.04018
 0.57744, 0.04116
 0.56970, 0.04213
 0.56206, 0.04308
 0.55452, 0.04400
 0.54707, 0.04491
 0.53971, 0.04580
 0.53245, 0.04666
 0.52527, 0.04751
 0.51818, 0.04833
 0.51118, 0.04914
 0.50427, 0.04992
 0.49744, 0.05068
 0.49069, 0.05141
 0.48403, 0.05212
 0.47744, 0.05281
 0.47094, 0.05348
 0.46451, 0.05413
 0.45816, 0.05476
 0.45189, 0.05536
 0.44568, 0.05595
 0.43956, 0.05651
 0.43350, 0.05705
 0.42751, 0.05758
 0.42160, 0.05809
 0.41576, 0.05857
 0.40998, 0.05903
 0.40428, 0.05947
 0.39864, 0.05989
 0.39306, 0.06029
 0.38754, 0.06066
 0.38209, 0.06101
 0.37671, 0.06135
 0.37139, 0.06166
 0.36612, 0.06196
 0.36092, 0.06224
 0.35578, 0.06251
 0.35069, 0.06275
 0.34566, 0.06298
 0.34068, 0.06320
 0.33577, 0.06339
 0.33090, 0.06358
 0.32609, 0.06373
 0.32133, 0.06389
 0.31662, 0.06402
 0.31198, 0.06415
 0.30737, 0.06426
 0.30282, 0.06435
 0.29832, 0.06442
 0.29385, 0.06450
 0.28946, 0.06455
 0.28509, 0.06459
 0.28078, 0.06462
 0.27652, 0.06463
 0.27230, 0.06463
 0.26812, 0.06462
 0.26398, 0.06459
 0.25990, 0.06455
 0.25585, 0.06450
 0.25185, 0.06443
 0.24790, 0.06435
 0.24397, 0.06426
 0.24010, 0.06415
 0.23626, 0.06403
 0.23246, 0.06390
 0.22870, 0.06375
 0.22499, 0.06360
 0.22131, 0.06342
 0.21767, 0.06325
 0.21406, 0.06306
 0.21049, 0.06286
 0.20696, 0.06265
 0.20347, 0.06243
 0.20000, 0.06220
 0.19658, 0.06196
 0.19318, 0.06171
 0.18983, 0.06145
 0.18650, 0.06118
 0.18321, 0.06090
 0.17995, 0.06062
 0.17672, 0.06032
 0.17353, 0.06001
 0.17037, 0.05970
 0.16724, 0.05938
 0.16414, 0.05905
 0.16107, 0.05871
 0.15803, 0.05837
 0.15502, 0.05801
 0.15203, 0.05766
 0.14908, 0.05729
 0.14615, 0.05691
 0.14326, 0.05652
 0.14039, 0.05613
 0.13755, 0.05573
 0.13473, 0.05532
 0.13195, 0.05491
 0.12918, 0.05449
 0.12646, 0.05406
 0.12375, 0.05362
 0.12107, 0.05318
 0.11841, 0.05273
 0.11578, 0.05228
 0.11316, 0.05182
 0.11058, 0.05134
 0.10802, 0.05086
 0.10548, 0.05038
 0.10297, 0.04990
 0.10049, 0.04940
 0.09802, 0.04890
 0.09558, 0.04839
 0.09316, 0.04789
 0.09076, 0.04737
 0.08838, 0.04684
 0.08603, 0.04630
 0.08370, 0.04576
 0.08139, 0.04520
 0.07910, 0.04465
 0.07683, 0.04407
 0.07459, 0.04349
 0.07237, 0.04289
 0.07017, 0.04227
 0.06798, 0.04165
 0.06582, 0.04102
 0.06367, 0.04038
 0.06156, 0.03972
 0.05945, 0.03906
 0.05737, 0.03840
 0.05531, 0.03772
 0.05326, 0.03703
 0.05123, 0.03633
 0.04922, 0.03563
 0.04723, 0.03495
 0.04526, 0.03426
 0.04331, 0.03355
 0.04136, 0.03283
 0.03945, 0.03210
 0.03755, 0.03136
 0.03566, 0.03060
 0.03380, 0.02983
 0.03195, 0.02904
 0.03012, 0.02824
 0.02831, 0.02741
 0.02652, 0.02655
 0.02475, 0.02566
 0.02299, 0.02473
 0.02126, 0.02376
 0.01955, 0.02276
 0.01786, 0.02173
 0.01619, 0.02067
 0.01454, 0.01956
 0.01291, 0.01840
 0.01129, 0.01718
 0.00971, 0.01591
 0.00814, 0.01457
 0.00661, 0.01314
 0.00511, 0.01158
 0.00364, 0.00986
 0.00222, 0.00789
 0.00089, 0.00543
 0.00012, 0.00304
 0.00000, 0.00000
 0.00000, 0.00000
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 0.01579,-0.01367
 0.01768,-0.01436
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 0.03113,-0.01809
 0.03309,-0.01851
 0.03507,-0.01892
 0.03705,-0.01930
 0.03905,-0.01968
 0.04107,-0.02003
 0.04309,-0.02036
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 0.04719,-0.02099
 0.04926,-0.02130
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 0.05345,-0.02187
 0.05556,-0.02215
 0.05769,-0.02241
 0.05983,-0.02266
 0.06200,-0.02290
 0.06418,-0.02313
 0.06638,-0.02335
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 0.07305,-0.02394
 0.07532,-0.02412
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 0.08220,-0.02457
 0.08453,-0.02471
 0.08688,-0.02483
 0.08925,-0.02495
 0.09163,-0.02506
 0.09404,-0.02517
 0.09646,-0.02527
 0.09891,-0.02536
 0.10138,-0.02545
 0.10387,-0.02555
 0.10638,-0.02565
 0.10890,-0.02574
 0.11146,-0.02582
 0.11403,-0.02591
 0.11662,-0.02599
 0.11924,-0.02606
 0.12188,-0.02613
 0.12454,-0.02620
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 0.14100,-0.02651
 0.14383,-0.02654
 0.14667,-0.02657
 0.14956,-0.02659
 0.15246,-0.02660
 0.15538,-0.02661
 0.15833,-0.02661
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 0.17041,-0.02657
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 0.17662,-0.02653
 0.17976,-0.02650
 0.18294,-0.02647
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 0.26895,-0.02532
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 0.31573,-0.02422
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 0.33883,-0.02363
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 0.49445,-0.01936
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 1.00000, 0.00000