ファイルインデックス名　: File Index Name        : 1084        .A00
翼型整理番号　　　　　　: Airfoil Serial No.     : N02-0012-0
翼型名　　　　　　　　　: Airfoil Name           : N.A.C.A. 43009
翼型ファイル番号　　　　: Airfoil File No.       : 1084
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. : 0.61
算出プログラム番号　　　: Computed Program No.   : ウハク-40D


座標　　　　　　　　　　: Plot Ordinates         :

 X             Y

 1.00004, 0.00094
 0.98681, 0.00292
 0.97378, 0.00484
 0.96094, 0.00671
 0.94829, 0.00854
 0.93582, 0.01032
 0.92353, 0.01205
 0.91142, 0.01375
 0.89948, 0.01540
 0.88772, 0.01702
 0.87612, 0.01859
 0.86468, 0.02014
 0.85341, 0.02164
 0.84229, 0.02311
 0.83133, 0.02455
 0.82052, 0.02596
 0.80987, 0.02734
 0.79935, 0.02868
 0.78899, 0.03000
 0.77876, 0.03128
 0.76867, 0.03254
 0.75872, 0.03378
 0.74891, 0.03498
 0.73922, 0.03616
 0.72967, 0.03732
 0.72024, 0.03845
 0.71094, 0.03956
 0.70176, 0.04064
 0.69270, 0.04170
 0.68375, 0.04274
 0.67493, 0.04375
 0.66622, 0.04475
 0.65762, 0.04572
 0.64913, 0.04667
 0.64075, 0.04760
 0.63248, 0.04852
 0.62431, 0.04941
 0.61625, 0.05028
 0.60829, 0.05114
 0.60042, 0.05197
 0.59266, 0.05279
 0.58499, 0.05359
 0.57742, 0.05438
 0.56994, 0.05514
 0.56255, 0.05589
 0.55525, 0.05662
 0.54804, 0.05734
 0.54092, 0.05804
 0.53388, 0.05872
 0.52693, 0.05939
 0.52006, 0.06005
 0.51328, 0.06068
 0.50657, 0.06131
 0.49995, 0.06192
 0.49340, 0.06251
 0.48693, 0.06309
 0.48053, 0.06366
 0.47421, 0.06421
 0.46796, 0.06475
 0.46179, 0.06528
 0.45568, 0.06579
 0.44965, 0.06629
 0.44368, 0.06678
 0.43778, 0.06725
 0.43195, 0.06771
 0.42619, 0.06816
 0.42049, 0.06860
 0.41485, 0.06903
 0.40928, 0.06944
 0.40377, 0.06985
 0.39832, 0.07024
 0.39293, 0.07062
 0.38759, 0.07099
 0.38232, 0.07135
 0.37711, 0.07170
 0.37195, 0.07204
 0.36685, 0.07236
 0.36180, 0.07268
 0.35681, 0.07299
 0.35187, 0.07329
 0.34698, 0.07357
 0.34214, 0.07385
 0.33736, 0.07412
 0.33263, 0.07438
 0.32794, 0.07463
 0.32331, 0.07487
 0.31872, 0.07510
 0.31419, 0.07532
 0.30970, 0.07554
 0.30525, 0.07574
 0.30085, 0.07594
 0.29650, 0.07612
 0.29219, 0.07630
 0.28792, 0.07647
 0.28370, 0.07664
 0.27952, 0.07679
 0.27539, 0.07694
 0.27129, 0.07708
 0.26724, 0.07721
 0.26322, 0.07733
 0.25925, 0.07745
 0.25531, 0.07755
 0.25142, 0.07766
 0.24756, 0.07775
 0.24374, 0.07783
 0.23996, 0.07791
 0.23621, 0.07799
 0.23250, 0.07805
 0.22883, 0.07811
 0.22519, 0.07816
 0.22159, 0.07820
 0.21802, 0.07824
 0.21449, 0.07827
 0.21099, 0.07829
 0.20752, 0.07831
 0.20409, 0.07832
 0.20067, 0.07832
 0.19728, 0.07832
 0.19390, 0.07831
 0.19054, 0.07829
 0.18720, 0.07826
 0.18387, 0.07822
 0.18056, 0.07816
 0.17727, 0.07809
 0.17400, 0.07801
 0.17074, 0.07791
 0.16751, 0.07780
 0.16429, 0.07767
 0.16109, 0.07752
 0.15791, 0.07736
 0.15475, 0.07718
 0.15161, 0.07697
 0.14849, 0.07675
 0.14538, 0.07651
 0.14230, 0.07624
 0.13924, 0.07596
 0.13620, 0.07565
 0.13318, 0.07532
 0.13017, 0.07497
 0.12719, 0.07460
 0.12424, 0.07420
 0.12130, 0.07378
 0.11838, 0.07334
 0.11549, 0.07287
 0.11261, 0.07238
 0.10976, 0.07186
 0.10693, 0.07132
 0.10413, 0.07076
 0.10135, 0.07017
 0.09859, 0.06956
 0.09585, 0.06892
 0.09314, 0.06825
 0.09045, 0.06756
 0.08778, 0.06685
 0.08514, 0.06611
 0.08252, 0.06535
 0.07993, 0.06456
 0.07736, 0.06374
 0.07482, 0.06291
 0.07230, 0.06204
 0.06981, 0.06115
 0.06735, 0.06024
 0.06491, 0.05930
 0.06249, 0.05834
 0.06010, 0.05735
 0.05774, 0.05634
 0.05541, 0.05531
 0.05310, 0.05425
 0.05082, 0.05316
 0.04857, 0.05205
 0.04635, 0.05092
 0.04415, 0.04976
 0.04198, 0.04858
 0.03984, 0.04738
 0.03773, 0.04615
 0.03565, 0.04489
 0.03360, 0.04361
 0.03158, 0.04231
 0.02959, 0.04098
 0.02763, 0.03963
 0.02571, 0.03824
 0.02381, 0.03684
 0.02195, 0.03540
 0.02012, 0.03394
 0.01833, 0.03245
 0.01657, 0.03092
 0.01486, 0.02937
 0.01318, 0.02778
 0.01154, 0.02615
 0.00994, 0.02448
 0.00839, 0.02277
 0.00690, 0.02101
 0.00545, 0.01919
 0.00408, 0.01730
 0.00277, 0.01532
 0.00156, 0.01324
 0.00046, 0.01101
-0.00047, 0.00854
-0.00109, 0.00563
-0.00106, 0.00302
 0.00000, 0.00000
 0.00000, 0.00000
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 0.01429,-0.00538
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 0.03685,-0.00417
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 0.04080,-0.00380
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 0.04473,-0.00343
 0.04670,-0.00324
 0.04867,-0.00306
 0.05063,-0.00288
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 0.05458,-0.00254
 0.05655,-0.00238
 0.05853,-0.00223
 0.06051,-0.00208
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 0.06650,-0.00167
 0.06851,-0.00155
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 0.07869,-0.00106
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 0.08704,-0.00083
 0.08916,-0.00080
 0.09129,-0.00077
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 0.10220,-0.00080
 0.10443,-0.00084
 0.10668,-0.00088
 0.10896,-0.00094
 0.11125,-0.00100
 0.11357,-0.00108
 0.11591,-0.00116
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 0.12306,-0.00149
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 0.14067,-0.00259
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