ファイルインデックス名　: File Index Name        : 1039        .A00
翼型整理番号　　　　　　: Airfoil Serial No.     : N01-0039-0
翼型名　　　　　　　　　: Airfoil Name           : N.A.C.A. 4409
翼型ファイル番号　　　　: Airfoil File No.       : 1039
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. : 0.2
算出プログラム番号　　　: Computed Program No.   : ウハク-40B


座標　　　　　　　　　　: Plot Ordinates         :

 X             Y

 1.00012, 0.00094
 0.98701, 0.00406
 0.97409, 0.00709
 0.96134, 0.01001
 0.94877, 0.01283
 0.93637, 0.01556
 0.92415, 0.01820
 0.91210, 0.02075
 0.90021, 0.02322
 0.88848, 0.02560
 0.87692, 0.02791
 0.86551, 0.03014
 0.85426, 0.03230
 0.84316, 0.03439
 0.83221, 0.03641
 0.82140, 0.03836
 0.81074, 0.04025
 0.80023, 0.04208
 0.78985, 0.04385
 0.77961, 0.04556
 0.76951, 0.04721
 0.75953, 0.04881
 0.74969, 0.05035
 0.73998, 0.05185
 0.73040, 0.05329
 0.72093, 0.05469
 0.71159, 0.05604
 0.70237, 0.05734
 0.69327, 0.05860
 0.68429, 0.05982
 0.67542, 0.06099
 0.66666, 0.06213
 0.65801, 0.06322
 0.64947, 0.06428
 0.64104, 0.06530
 0.63271, 0.06628
 0.62449, 0.06723
 0.61637, 0.06814
 0.60835, 0.06902
 0.60042, 0.06986
 0.59260, 0.07068
 0.58487, 0.07146
 0.57724, 0.07221
 0.56969, 0.07294
 0.56224, 0.07363
 0.55488, 0.07430
 0.54761, 0.07494
 0.54042, 0.07555
 0.53332, 0.07614
 0.52630, 0.07670
 0.51937, 0.07724
 0.51252, 0.07775
 0.50575, 0.07824
 0.49906, 0.07871
 0.49244, 0.07915
 0.48591, 0.07958
 0.47945, 0.07998
 0.47306, 0.08036
 0.46675, 0.08072
 0.46051, 0.08106
 0.45434, 0.08138
 0.44824, 0.08168
 0.44221, 0.08197
 0.43625, 0.08223
 0.43036, 0.08248
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 0.38534, 0.08385
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 0.34378, 0.08391
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 0.32909, 0.08363
 0.32430, 0.08350
 0.31956, 0.08335
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 0.30564, 0.08283
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 0.19449, 0.07264
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 0.18768, 0.07164
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 0.18101, 0.07060
 0.17772, 0.07008
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 0.16805, 0.06846
 0.16489, 0.06790
 0.16176, 0.06734
 0.15865, 0.06678
 0.15558, 0.06621
 0.15254, 0.06563
 0.14953, 0.06505
 0.14655, 0.06446
 0.14359, 0.06386
 0.14066, 0.06326
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 0.13205, 0.06143
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 0.11822, 0.05827
 0.11554, 0.05763
 0.11288, 0.05697
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 0.10504, 0.05499
 0.10248, 0.05432
 0.09994, 0.05364
 0.09742, 0.05296
 0.09493, 0.05227
 0.09246, 0.05158
 0.09002, 0.05088
 0.08759, 0.05018
 0.08519, 0.04947
 0.08282, 0.04876
 0.08046, 0.04804
 0.07813, 0.04732
 0.07582, 0.04659
 0.07353, 0.04586
 0.07126, 0.04512
 0.06901, 0.04437
 0.06679, 0.04362
 0.06458, 0.04286
 0.06240, 0.04210
 0.06023, 0.04133
 0.05809, 0.04055
 0.05597, 0.03977
 0.05386, 0.03898
 0.05178, 0.03818
 0.04972, 0.03738
 0.04768, 0.03656
 0.04565, 0.03574
 0.04365, 0.03491
 0.04167, 0.03407
 0.03970, 0.03321
 0.03776, 0.03235
 0.03583, 0.03148
 0.03393, 0.03059
 0.03204, 0.02970
 0.03017, 0.02879
 0.02832, 0.02786
 0.02650, 0.02692
 0.02469, 0.02595
 0.02290, 0.02497
 0.02113, 0.02397
 0.01939, 0.02295
 0.01766, 0.02189
 0.01596, 0.02081
 0.01427, 0.01969
 0.01262, 0.01853
 0.01098, 0.01733
 0.00938, 0.01607
 0.00780, 0.01473
 0.00625, 0.01331
 0.00475, 0.01177
 0.00329, 0.01006
 0.00190, 0.00809
 0.00063, 0.00561
-0.00005, 0.00318
 0.00000, 0.00000
 0.00000, 0.00000
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 0.11804,-0.01689
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