ファイルインデックス名　: File Index Name        : 1076        .A00
翼型整理番号　　　　　　: Airfoil Serial No.     : N02-0004-0
翼型名　　　　　　　　　: Airfoil Name           : N.A.C.A. 23009
翼型ファイル番号　　　　: Airfoil File No.       : 1076
翼型情報　　　　　　　　: Airfoil Information    : Computed

算出前縁半径　　　　　　: Computed L.E.R.        : 0.89 %
算出前縁傾斜　　　　　　: Computed Slope of L.E. : 0.305
算出プログラム番号　　　: Computed Program No.   : ウハク-40D


座標　　　　　　　　　　: Plot Ordinates         :

 X             Y

 1.00002, 0.00094
 0.98676, 0.00262
 0.97370, 0.00426
 0.96083, 0.00585
 0.94815, 0.00739
 0.93566, 0.00890
 0.92334, 0.01036
 0.91121, 0.01179
 0.89924, 0.01318
 0.88745, 0.01453
 0.87583, 0.01586
 0.86437, 0.01714
 0.85308, 0.01840
 0.84194, 0.01963
 0.83096, 0.02082
 0.82013, 0.02199
 0.80945, 0.02313
 0.79892, 0.02424
 0.78853, 0.02533
 0.77829, 0.02639
 0.76818, 0.02743
 0.75821, 0.02844
 0.74838, 0.02943
 0.73868, 0.03040
 0.72911, 0.03134
 0.71967, 0.03226
 0.71035, 0.03317
 0.70115, 0.03405
 0.69208, 0.03491
 0.68312, 0.03575
 0.67428, 0.03657
 0.66556, 0.03737
 0.65695, 0.03815
 0.64845, 0.03892
 0.64005, 0.03966
 0.63177, 0.04039
 0.62359, 0.04110
 0.61552, 0.04180
 0.60754, 0.04248
 0.59967, 0.04314
 0.59189, 0.04379
 0.58421, 0.04442
 0.57663, 0.04503
 0.56914, 0.04564
 0.56174, 0.04622
 0.55444, 0.04679
 0.54722, 0.04735
 0.54009, 0.04789
 0.53304, 0.04842
 0.52608, 0.04894
 0.51921, 0.04944
 0.51241, 0.04993
 0.50570, 0.05040
 0.49907, 0.05086
 0.49251, 0.05131
 0.48604, 0.05175
 0.47963, 0.05218
 0.47331, 0.05259
 0.46705, 0.05299
 0.46087, 0.05338
 0.45476, 0.05376
 0.44872, 0.05412
 0.44275, 0.05448
 0.43685, 0.05482
 0.43101, 0.05516
 0.42524, 0.05548
 0.41954, 0.05579
 0.41390, 0.05610
 0.40832, 0.05639
 0.40281, 0.05667
 0.39735, 0.05694
 0.39196, 0.05720
 0.38663, 0.05746
 0.38135, 0.05770
 0.37613, 0.05793
 0.37097, 0.05816
 0.36587, 0.05837
 0.36082, 0.05858
 0.35582, 0.05877
 0.35088, 0.05896
 0.34599, 0.05914
 0.34116, 0.05931
 0.33637, 0.05948
 0.33164, 0.05963
 0.32695, 0.05978
 0.32232, 0.05991
 0.31773, 0.06004
 0.31319, 0.06017
 0.30870, 0.06028
 0.30426, 0.06039
 0.29986, 0.06049
 0.29551, 0.06058
 0.29120, 0.06066
 0.28693, 0.06074
 0.28271, 0.06081
 0.27853, 0.06087
 0.27440, 0.06093
 0.27030, 0.06097
 0.26625, 0.06101
 0.26224, 0.06105
 0.25826, 0.06108
 0.25433, 0.06110
 0.25043, 0.06111
 0.24658, 0.06112
 0.24276, 0.06112
 0.23898, 0.06112
 0.23524, 0.06111
 0.23153, 0.06109
 0.22786, 0.06107
 0.22423, 0.06104
 0.22062, 0.06100
 0.21706, 0.06096
 0.21353, 0.06091
 0.21003, 0.06086
 0.20657, 0.06080
 0.20314, 0.06073
 0.19973, 0.06066
 0.19635, 0.06058
 0.19300, 0.06050
 0.18967, 0.06041
 0.18636, 0.06031
 0.18308, 0.06020
 0.17982, 0.06009
 0.17659, 0.05996
 0.17337, 0.05983
 0.17019, 0.05968
 0.16702, 0.05953
 0.16388, 0.05936
 0.16077, 0.05919
 0.15767, 0.05900
 0.15460, 0.05880
 0.15156, 0.05859
 0.14853, 0.05836
 0.14553, 0.05813
 0.14255, 0.05788
 0.13960, 0.05762
 0.13667, 0.05735
 0.13376, 0.05706
 0.13087, 0.05676
 0.12801, 0.05645
 0.12516, 0.05612
 0.12235, 0.05578
 0.11955, 0.05543
 0.11678, 0.05506
 0.11402, 0.05468
 0.11129, 0.05429
 0.10859, 0.05388
 0.10590, 0.05345
 0.10324, 0.05301
 0.10060, 0.05256
 0.09798, 0.05209
 0.09539, 0.05161
 0.09281, 0.05111
 0.09026, 0.05060
 0.08773, 0.05007
 0.08522, 0.04953
 0.08274, 0.04898
 0.08028, 0.04841
 0.07783, 0.04782
 0.07541, 0.04722
 0.07302, 0.04660
 0.07064, 0.04597
 0.06829, 0.04532
 0.06595, 0.04466
 0.06364, 0.04398
 0.06136, 0.04328
 0.05909, 0.04257
 0.05685, 0.04184
 0.05463, 0.04110
 0.05243, 0.04034
 0.05025, 0.03956
 0.04809, 0.03877
 0.04596, 0.03796
 0.04385, 0.03713
 0.04176, 0.03629
 0.03970, 0.03542
 0.03766, 0.03454
 0.03564, 0.03363
 0.03364, 0.03271
 0.03167, 0.03177
 0.02972, 0.03080
 0.02780, 0.02981
 0.02590, 0.02880
 0.02403, 0.02777
 0.02218, 0.02670
 0.02036, 0.02561
 0.01856, 0.02449
 0.01679, 0.02334
 0.01506, 0.02215
 0.01335, 0.02092
 0.01167, 0.01964
 0.01003, 0.01831
 0.00843, 0.01692
 0.00687, 0.01545
 0.00536, 0.01390
 0.00390, 0.01222
 0.00252, 0.01037
 0.00124, 0.00827
 0.00014, 0.00566
-0.00035, 0.00317
 0.00000, 0.00000
 0.00000, 0.00000
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 0.03295,-0.01288
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 0.04070,-0.01367
 0.04265,-0.01384
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 0.04658,-0.01417
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 0.05455,-0.01478
 0.05657,-0.01493
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 0.06477,-0.01549
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 0.07964,-0.01649
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 0.08402,-0.01678
 0.08624,-0.01693
 0.08848,-0.01709
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 0.09995,-0.01788
 0.10230,-0.01805
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 0.10706,-0.01840
 0.10948,-0.01857
 0.11192,-0.01875
 0.11437,-0.01894
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 0.12189,-0.01950
 0.12445,-0.01970
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 0.14031,-0.02094
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 0.14862,-0.02159
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