ファイルインデックス名　: File Index Name        : 1083        .A00
翼型整理番号　　　　　　: Airfoil Serial No.     : N02-0011-0
翼型名　　　　　　　　　: Airfoil Name           : N.A.C.A. 25012
翼型ファイル番号　　　　: Airfoil File No.       : 1083
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. : 0.215
算出プログラム番号　　　: Computed Program No.   : ウハク-40D


座標　　　　　　　　　　: Plot Ordinates         :

 X             Y

 1.00004, 0.00126
 0.98681, 0.00354
 0.97378, 0.00575
 0.96094, 0.00790
 0.94828, 0.01000
 0.93581, 0.01204
 0.92352, 0.01402
 0.91141, 0.01596
 0.89947, 0.01784
 0.88770, 0.01968
 0.87610, 0.02148
 0.86467, 0.02323
 0.85339, 0.02493
 0.84227, 0.02660
 0.83131, 0.02822
 0.82050, 0.02981
 0.80984, 0.03136
 0.79933, 0.03287
 0.78896, 0.03435
 0.77873, 0.03579
 0.76865, 0.03720
 0.75869, 0.03858
 0.74888, 0.03992
 0.73919, 0.04124
 0.72964, 0.04252
 0.72021, 0.04378
 0.71090, 0.04500
 0.70172, 0.04620
 0.69266, 0.04737
 0.68372, 0.04852
 0.67489, 0.04964
 0.66618, 0.05073
 0.65758, 0.05180
 0.64909, 0.05284
 0.64071, 0.05386
 0.63244, 0.05485
 0.62427, 0.05583
 0.61621, 0.05677
 0.60824, 0.05770
 0.60038, 0.05861
 0.59262, 0.05949
 0.58495, 0.06035
 0.57737, 0.06119
 0.56989, 0.06201
 0.56250, 0.06282
 0.55520, 0.06360
 0.54799, 0.06436
 0.54087, 0.06510
 0.53384, 0.06583
 0.52688, 0.06653
 0.52002, 0.06722
 0.51323, 0.06789
 0.50652, 0.06854
 0.49990, 0.06917
 0.49335, 0.06979
 0.48688, 0.07039
 0.48048, 0.07098
 0.47416, 0.07155
 0.46791, 0.07210
 0.46173, 0.07263
 0.45563, 0.07316
 0.44959, 0.07366
 0.44363, 0.07415
 0.43773, 0.07463
 0.43190, 0.07509
 0.42613, 0.07553
 0.42043, 0.07597
 0.41480, 0.07638
 0.40922, 0.07679
 0.40371, 0.07718
 0.39826, 0.07756
 0.39287, 0.07792
 0.38754, 0.07827
 0.38226, 0.07861
 0.37703, 0.07893
 0.37185, 0.07924
 0.36673, 0.07954
 0.36165, 0.07982
 0.35663, 0.08009
 0.35165, 0.08035
 0.34672, 0.08058
 0.34184, 0.08081
 0.33701, 0.08102
 0.33222, 0.08121
 0.32748, 0.08139
 0.32279, 0.08156
 0.31814, 0.08170
 0.31353, 0.08184
 0.30897, 0.08196
 0.30445, 0.08206
 0.29997, 0.08215
 0.29554, 0.08222
 0.29115, 0.08228
 0.28680, 0.08232
 0.28249, 0.08235
 0.27822, 0.08236
 0.27399, 0.08236
 0.26981, 0.08234
 0.26566, 0.08231
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 0.25747, 0.08219
 0.25344, 0.08212
 0.24944, 0.08202
 0.24548, 0.08192
 0.24156, 0.08180
 0.23767, 0.08166
 0.23382, 0.08151
 0.23000, 0.08135
 0.22622, 0.08117
 0.22248, 0.08097
 0.21877, 0.08077
 0.21509, 0.08055
 0.21145, 0.08031
 0.20784, 0.08007
 0.20427, 0.07981
 0.20072, 0.07953
 0.19721, 0.07924
 0.19374, 0.07894
 0.19029, 0.07863
 0.18687, 0.07830
 0.18349, 0.07796
 0.18014, 0.07761
 0.17682, 0.07725
 0.17353, 0.07687
 0.17027, 0.07648
 0.16704, 0.07608
 0.16384, 0.07566
 0.16066, 0.07524
 0.15752, 0.07480
 0.15441, 0.07435
 0.15132, 0.07389
 0.14827, 0.07341
 0.14524, 0.07293
 0.14224, 0.07243
 0.13927, 0.07193
 0.13632, 0.07141
 0.13340, 0.07088
 0.13051, 0.07034
 0.12765, 0.06978
 0.12481, 0.06922
 0.12199, 0.06865
 0.11921, 0.06806
 0.11645, 0.06746
 0.11371, 0.06686
 0.11100, 0.06624
 0.10832, 0.06561
 0.10566, 0.06497
 0.10303, 0.06432
 0.10042, 0.06366
 0.09783, 0.06299
 0.09527, 0.06231
 0.09274, 0.06162
 0.09022, 0.06091
 0.08774, 0.06020
 0.08527, 0.05947
 0.08283, 0.05874
 0.08041, 0.05799
 0.07802, 0.05724
 0.07564, 0.05647
 0.07329, 0.05569
 0.07097, 0.05490
 0.06866, 0.05410
 0.06638, 0.05328
 0.06412, 0.05246
 0.06189, 0.05162
 0.05967, 0.05077
 0.05748, 0.04991
 0.05531, 0.04904
 0.05316, 0.04815
 0.05104, 0.04725
 0.04893, 0.04634
 0.04685, 0.04541
 0.04479, 0.04447
 0.04275, 0.04351
 0.04073, 0.04254
 0.03874, 0.04155
 0.03676, 0.04054
 0.03481, 0.03952
 0.03288, 0.03847
 0.03097, 0.03741
 0.02909, 0.03632
 0.02723, 0.03522
 0.02539, 0.03408
 0.02357, 0.03292
 0.02178, 0.03174
 0.02001, 0.03052
 0.01827, 0.02927
 0.01655, 0.02797
 0.01486, 0.02664
 0.01319, 0.02526
 0.01156, 0.02382
 0.00996, 0.02232
 0.00839, 0.02073
 0.00686, 0.01906
 0.00537, 0.01726
 0.00394, 0.01530
 0.00257, 0.01312
 0.00129, 0.01059
 0.00019, 0.00738
-0.00031, 0.00420
 0.00000, 0.00000
 0.00000, 0.00000
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 0.00966,-0.01244
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 0.03938,-0.02306
 0.04139,-0.02347
 0.04341,-0.02387
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 0.04747,-0.02461
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 0.05364,-0.02562
 0.05572,-0.02594
 0.05781,-0.02624
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 0.06416,-0.02709
 0.06630,-0.02735
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 0.07063,-0.02786
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 0.07944,-0.02878
 0.08168,-0.02900
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 0.08850,-0.02961
 0.09081,-0.02981
 0.09313,-0.03000
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 0.10501,-0.03089
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 0.10989,-0.03122
 0.11235,-0.03138
 0.11484,-0.03153
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 0.14359,-0.03309
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