ファイルインデックス名　: File Index Name        : 1025        .A00
翼型整理番号　　　　　　: Airfoil Serial No.     : N01-0025-0
翼型名　　　　　　　　　: Airfoil Name           : N.A.C.A. 2409
翼型ファイル番号　　　　: Airfoil File No.       : 1025
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. : 0.1
算出プログラム番号　　　: Computed Program No.   : ウハク-40B


座標　　　　　　　　　　: Plot Ordinates         :

 X             Y

 1.00006, 0.00094
 0.98686, 0.00320
 0.97385, 0.00539
 0.96103, 0.00750
 0.94839, 0.00955
 0.93593, 0.01153
 0.92365, 0.01345
 0.91155, 0.01530
 0.89961, 0.01710
 0.88784, 0.01884
 0.87623, 0.02053
 0.86479, 0.02216
 0.85350, 0.02375
 0.84237, 0.02528
 0.83140, 0.02677
 0.82057, 0.02821
 0.80989, 0.02960
 0.79936, 0.03096
 0.78897, 0.03227
 0.77871, 0.03354
 0.76860, 0.03478
 0.75862, 0.03597
 0.74878, 0.03713
 0.73906, 0.03825
 0.72947, 0.03934
 0.72001, 0.04039
 0.71068, 0.04142
 0.70146, 0.04241
 0.69237, 0.04336
 0.68339, 0.04429
 0.67453, 0.04519
 0.66578, 0.04606
 0.65714, 0.04691
 0.64862, 0.04772
 0.64020, 0.04851
 0.63189, 0.04928
 0.62368, 0.05001
 0.61557, 0.05073
 0.60757, 0.05142
 0.59967, 0.05209
 0.59186, 0.05273
 0.58415, 0.05335
 0.57654, 0.05395
 0.56902, 0.05453
 0.56159, 0.05509
 0.55425, 0.05563
 0.54700, 0.05614
 0.53984, 0.05664
 0.53276, 0.05712
 0.52577, 0.05758
 0.51886, 0.05803
 0.51203, 0.05845
 0.50529, 0.05886
 0.49862, 0.05925
 0.49204, 0.05963
 0.48553, 0.05999
 0.47909, 0.06033
 0.47273, 0.06065
 0.46645, 0.06097
 0.46023, 0.06126
 0.45409, 0.06154
 0.44802, 0.06181
 0.44202, 0.06207
 0.43608, 0.06231
 0.43022, 0.06253
 0.42442, 0.06275
 0.41868, 0.06295
 0.41301, 0.06313
 0.40740, 0.06331
 0.40186, 0.06347
 0.39635, 0.06362
 0.39090, 0.06375
 0.38550, 0.06387
 0.38016, 0.06398
 0.37489, 0.06407
 0.36966, 0.06414
 0.36450, 0.06420
 0.35939, 0.06425
 0.35434, 0.06428
 0.34934, 0.06430
 0.34439, 0.06431
 0.33950, 0.06430
 0.33466, 0.06428
 0.32987, 0.06425
 0.32513, 0.06421
 0.32044, 0.06415
 0.31580, 0.06409
 0.31121, 0.06401
 0.30667, 0.06393
 0.30218, 0.06383
 0.29773, 0.06372
 0.29333, 0.06360
 0.28897, 0.06347
 0.28466, 0.06334
 0.28039, 0.06319
 0.27617, 0.06303
 0.27198, 0.06286
 0.26785, 0.06269
 0.26375, 0.06250
 0.25970, 0.06231
 0.25568, 0.06211
 0.25171, 0.06190
 0.24778, 0.06168
 0.24388, 0.06146
 0.24003, 0.06123
 0.23621, 0.06098
 0.23243, 0.06074
 0.22869, 0.06048
 0.22499, 0.06022
 0.22132, 0.05995
 0.21769, 0.05967
 0.21409, 0.05938
 0.21053, 0.05909
 0.20700, 0.05880
 0.20351, 0.05849
 0.20005, 0.05818
 0.19663, 0.05786
 0.19324, 0.05754
 0.18988, 0.05721
 0.18655, 0.05688
 0.18326, 0.05653
 0.17999, 0.05619
 0.17676, 0.05583
 0.17356, 0.05547
 0.17039, 0.05511
 0.16725, 0.05474
 0.16413, 0.05436
 0.16105, 0.05398
 0.15800, 0.05360
 0.15497, 0.05321
 0.15198, 0.05281
 0.14901, 0.05241
 0.14607, 0.05200
 0.14315, 0.05159
 0.14027, 0.05117
 0.13741, 0.05075
 0.13457, 0.05032
 0.13177, 0.04988
 0.12899, 0.04945
 0.12623, 0.04900
 0.12350, 0.04856
 0.12079, 0.04810
 0.11811, 0.04764
 0.11545, 0.04718
 0.11282, 0.04671
 0.11021, 0.04624
 0.10763, 0.04576
 0.10506, 0.04528
 0.10252, 0.04479
 0.10001, 0.04430
 0.09751, 0.04380
 0.09504, 0.04330
 0.09259, 0.04279
 0.09017, 0.04227
 0.08776, 0.04175
 0.08538, 0.04123
 0.08301, 0.04070
 0.08067, 0.04016
 0.07835, 0.03962
 0.07605, 0.03907
 0.07377, 0.03852
 0.07151, 0.03796
 0.06927, 0.03739
 0.06705, 0.03682
 0.06485, 0.03624
 0.06267, 0.03565
 0.06050, 0.03506
 0.05836, 0.03446
 0.05624, 0.03385
 0.05413, 0.03323
 0.05205, 0.03260
 0.04998, 0.03197
 0.04793, 0.03133
 0.04590, 0.03067
 0.04388, 0.03001
 0.04189, 0.02934
 0.03991, 0.02865
 0.03795, 0.02795
 0.03601, 0.02724
 0.03409, 0.02652
 0.03218, 0.02578
 0.03029, 0.02503
 0.02842, 0.02426
 0.02656, 0.02347
 0.02473, 0.02266
 0.02291, 0.02183
 0.02111, 0.02097
 0.01932, 0.02008
 0.01756, 0.01916
 0.01581, 0.01821
 0.01408, 0.01722
 0.01237, 0.01617
 0.01069, 0.01507
 0.00902, 0.01390
 0.00737, 0.01263
 0.00576, 0.01124
 0.00417, 0.00969
 0.00263, 0.00786
 0.00115, 0.00552
 0.00025, 0.00317
 0.00000, 0.00000
 0.00000, 0.00000
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 0.00221,-0.00519
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 0.00598,-0.00868
 0.00784,-0.00990
 0.00968,-0.01094
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 0.01338,-0.01270
 0.01523,-0.01346
 0.01710,-0.01416
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 0.02085,-0.01542
 0.02274,-0.01599
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 0.02848,-0.01751
 0.03041,-0.01797
 0.03236,-0.01841
 0.03432,-0.01883
 0.03629,-0.01923
 0.03828,-0.01961
 0.04028,-0.01998
 0.04230,-0.02033
 0.04432,-0.02067
 0.04637,-0.02100
 0.04842,-0.02131
 0.05050,-0.02161
 0.05258,-0.02191
 0.05469,-0.02219
 0.05680,-0.02246
 0.05894,-0.02272
 0.06109,-0.02297
 0.06325,-0.02322
 0.06543,-0.02345
 0.06763,-0.02368
 0.06985,-0.02390
 0.07208,-0.02412
 0.07433,-0.02432
 0.07660,-0.02452
 0.07888,-0.02471
 0.08119,-0.02489
 0.08351,-0.02507
 0.08585,-0.02524
 0.08821,-0.02541
 0.09059,-0.02557
 0.09298,-0.02572
 0.09540,-0.02587
 0.09784,-0.02601
 0.10029,-0.02615
 0.10277,-0.02628
 0.10526,-0.02641
 0.10778,-0.02653
 0.11032,-0.02664
 0.11288,-0.02675
 0.11546,-0.02686
 0.11806,-0.02696
 0.12069,-0.02705
 0.12333,-0.02714
 0.12600,-0.02723
 0.12869,-0.02731
 0.13141,-0.02739
 0.13415,-0.02746
 0.13691,-0.02753
 0.13969,-0.02759
 0.14250,-0.02765
 0.14534,-0.02771
 0.14820,-0.02776
 0.15108,-0.02780
 0.15399,-0.02784
 0.15693,-0.02788
 0.15989,-0.02792
 0.16288,-0.02794
 0.16590,-0.02797
 0.16894,-0.02799
 0.17201,-0.02801
 0.17511,-0.02802
 0.17824,-0.02803
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 0.26677,-0.02704
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 0.49122,-0.02056
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