ファイルインデックス名　: File Index Name        : 1255        .A00
翼型整理番号　　　　　　: Airfoil Serial No.     : N01-0090-0
翼型名　　　　　　　　　: Airfoil Name           : N.A.C.A. 2506
翼型ファイル番号　　　　: Airfoil File No.       : 1255
翼型情報　　　　　　　　: Airfoil Information    : Computed

算出前縁半径　　　　　　: Computed L.E.R.        : 0.4 %
算出前縁傾斜　　　　　　: Computed Slope of L.E. : 0.08
算出プログラム番号　　　: Computed Program No.   : ウハク-40C


座標　　　　　　　　　　: Plot Ordinates         :

 X             Y

 1.00005, 0.00063
 0.98683, 0.00260
 0.97381, 0.00450
 0.96097, 0.00633
 0.94831, 0.00810
 0.93584, 0.00980
 0.92354, 0.01144
 0.91142, 0.01302
 0.89947, 0.01455
 0.88768, 0.01602
 0.87606, 0.01744
 0.86461, 0.01881
 0.85331, 0.02013
 0.84217, 0.02140
 0.83118, 0.02263
 0.82034, 0.02382
 0.80965, 0.02496
 0.79911, 0.02606
 0.78871, 0.02712
 0.77845, 0.02814
 0.76833, 0.02912
 0.75834, 0.03007
 0.74848, 0.03099
 0.73876, 0.03187
 0.72917, 0.03271
 0.71970, 0.03353
 0.71035, 0.03431
 0.70113, 0.03507
 0.69203, 0.03579
 0.68305, 0.03649
 0.67418, 0.03716
 0.66542, 0.03780
 0.65678, 0.03842
 0.64825, 0.03901
 0.63983, 0.03958
 0.63151, 0.04012
 0.62330, 0.04064
 0.61519, 0.04114
 0.60718, 0.04162
 0.59927, 0.04208
 0.59146, 0.04251
 0.58375, 0.04293
 0.57613, 0.04332
 0.56861, 0.04370
 0.56117, 0.04406
 0.55383, 0.04440
 0.54658, 0.04472
 0.53941, 0.04503
 0.53233, 0.04532
 0.52534, 0.04559
 0.51843, 0.04585
 0.51160, 0.04609
 0.50485, 0.04631
 0.49818, 0.04653
 0.49159, 0.04672
 0.48508, 0.04691
 0.47864, 0.04708
 0.47228, 0.04724
 0.46599, 0.04738
 0.45978, 0.04751
 0.45364, 0.04763
 0.44756, 0.04774
 0.44156, 0.04784
 0.43562, 0.04792
 0.42976, 0.04800
 0.42395, 0.04806
 0.41822, 0.04811
 0.41255, 0.04815
 0.40694, 0.04818
 0.40139, 0.04821
 0.39591, 0.04822
 0.39049, 0.04822
 0.38512, 0.04822
 0.37982, 0.04820
 0.37457, 0.04818
 0.36938, 0.04814
 0.36425, 0.04810
 0.35917, 0.04805
 0.35415, 0.04800
 0.34918, 0.04793
 0.34427, 0.04786
 0.33941, 0.04778
 0.33460, 0.04769
 0.32984, 0.04760
 0.32513, 0.04750
 0.32047, 0.04739
 0.31586, 0.04728
 0.31130, 0.04716
 0.30679, 0.04703
 0.30232, 0.04690
 0.29790, 0.04676
 0.29353, 0.04661
 0.28920, 0.04646
 0.28491, 0.04630
 0.28067, 0.04614
 0.27647, 0.04597
 0.27232, 0.04580
 0.26821, 0.04562
 0.26414, 0.04544
 0.26011, 0.04525
 0.25612, 0.04505
 0.25217, 0.04486
 0.24826, 0.04465
 0.24439, 0.04445
 0.24056, 0.04423
 0.23677, 0.04402
 0.23301, 0.04380
 0.22929, 0.04357
 0.22561, 0.04334
 0.22196, 0.04311
 0.21835, 0.04287
 0.21477, 0.04263
 0.21123, 0.04238
 0.20773, 0.04213
 0.20425, 0.04188
 0.20081, 0.04162
 0.19741, 0.04136
 0.19403, 0.04110
 0.19069, 0.04083
 0.18738, 0.04056
 0.18410, 0.04028
 0.18086, 0.04000
 0.17764, 0.03972
 0.17445, 0.03944
 0.17130, 0.03915
 0.16817, 0.03886
 0.16507, 0.03856
 0.16200, 0.03827
 0.15896, 0.03797
 0.15595, 0.03766
 0.15297, 0.03735
 0.15001, 0.03704
 0.14708, 0.03673
 0.14418, 0.03641
 0.14130, 0.03610
 0.13845, 0.03577
 0.13563, 0.03545
 0.13283, 0.03512
 0.13005, 0.03479
 0.12731, 0.03446
 0.12458, 0.03412
 0.12188, 0.03378
 0.11921, 0.03344
 0.11656, 0.03309
 0.11393, 0.03274
 0.11132, 0.03239
 0.10874, 0.03204
 0.10618, 0.03168
 0.10365, 0.03132
 0.10114, 0.03095
 0.09864, 0.03059
 0.09618, 0.03022
 0.09373, 0.02984
 0.09130, 0.02947
 0.08890, 0.02909
 0.08651, 0.02870
 0.08415, 0.02832
 0.08180, 0.02793
 0.07948, 0.02753
 0.07718, 0.02714
 0.07490, 0.02674
 0.07263, 0.02633
 0.07039, 0.02592
 0.06816, 0.02551
 0.06596, 0.02509
 0.06377, 0.02467
 0.06160, 0.02425
 0.05945, 0.02382
 0.05732, 0.02338
 0.05521, 0.02294
 0.05311, 0.02249
 0.05104, 0.02204
 0.04898, 0.02158
 0.04694, 0.02112
 0.04491, 0.02065
 0.04290, 0.02017
 0.04091, 0.01969
 0.03894, 0.01920
 0.03698, 0.01870
 0.03504, 0.01819
 0.03312, 0.01767
 0.03121, 0.01714
 0.02932, 0.01660
 0.02744, 0.01605
 0.02559, 0.01548
 0.02374, 0.01490
 0.02192, 0.01430
 0.02011, 0.01369
 0.01832, 0.01305
 0.01654, 0.01239
 0.01478, 0.01170
 0.01303, 0.01098
 0.01131, 0.01022
 0.00960, 0.00942
 0.00791, 0.00855
 0.00624, 0.00760
 0.00459, 0.00654
 0.00297, 0.00530
 0.00139, 0.00371
 0.00039, 0.00212
 0.00000, 0.00000
 0.00000, 0.00000
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 0.00556,-0.00573
 0.00735,-0.00652
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 0.01640,-0.00925
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 0.03340,-0.01214
 0.03536,-0.01238
 0.03733,-0.01261
 0.03931,-0.01283
 0.04131,-0.01304
 0.04332,-0.01323
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 0.04740,-0.01361
 0.04946,-0.01378
 0.05153,-0.01395
 0.05363,-0.01411
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 0.06000,-0.01454
 0.06216,-0.01468
 0.06433,-0.01481
 0.06653,-0.01493
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 0.07547,-0.01536
 0.07776,-0.01546
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 0.08238,-0.01563
 0.08471,-0.01572
 0.08707,-0.01579
 0.08945,-0.01587
 0.09185,-0.01593
 0.09426,-0.01600
 0.09670,-0.01606
 0.09916,-0.01612
 0.10164,-0.01617
 0.10414,-0.01622
 0.10666,-0.01626
 0.10920,-0.01630
 0.11176,-0.01634
 0.11435,-0.01637
 0.11695,-0.01640
 0.11958,-0.01643
 0.12223,-0.01645
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 0.12761,-0.01649
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 0.15007,-0.01649
 0.15299,-0.01648
 0.15594,-0.01646
 0.15892,-0.01644
 0.16192,-0.01641
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 0.17109,-0.01632
 0.17420,-0.01628
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