ファイルインデックス名　: File Index Name        : 1001        .A00
翼型整理番号　　　　　　: Airfoil Serial No.     : N01-0001-0
翼型名　　　　　　　　　: Airfoil Name           : N.A.C.A. 0006
翼型ファイル番号　　　　: Airfoil File No.       : 1001
翼型情報　　　　　　　　: Airfoil Information    : Computed

算出前縁半径　　　　　　: Computed L.E.R.        : 0.397 %
算出前縁傾斜　　　　　　: Computed Slope of L.E. : 0
算出プログラム番号　　　: Computed Program No.   : ウハク-40


座標　　　　　　　　　　: Plot Ordinates         :

 X             Y

 1.00000, 0.00063
 0.98671, 0.00155
 0.97362, 0.00245
 0.96072, 0.00332
 0.94801, 0.00416
 0.93549, 0.00498
 0.92315, 0.00578
 0.91099, 0.00655
 0.89900, 0.00730
 0.88719, 0.00803
 0.87554, 0.00874
 0.86406, 0.00943
 0.85274, 0.01010
 0.84158, 0.01075
 0.83058, 0.01139
 0.81973, 0.01201
 0.80903, 0.01261
 0.79848, 0.01320
 0.78808, 0.01377
 0.77781, 0.01433
 0.76769, 0.01487
 0.75770, 0.01540
 0.74785, 0.01591
 0.73814, 0.01641
 0.72855, 0.01690
 0.71909, 0.01738
 0.70976, 0.01784
 0.70055, 0.01829
 0.69146, 0.01873
 0.68249, 0.01916
 0.67363, 0.01958
 0.66490, 0.01998
 0.65627, 0.02038
 0.64776, 0.02076
 0.63935, 0.02114
 0.63106, 0.02150
 0.62287, 0.02186
 0.61478, 0.02220
 0.60680, 0.02254
 0.59891, 0.02286
 0.59112, 0.02318
 0.58344, 0.02349
 0.57584, 0.02378
 0.56834, 0.02407
 0.56094, 0.02436
 0.55362, 0.02463
 0.54639, 0.02489
 0.53925, 0.02515
 0.53220, 0.02540
 0.52523, 0.02564
 0.51835, 0.02587
 0.51155, 0.02610
 0.50483, 0.02632
 0.49819, 0.02653
 0.49163, 0.02673
 0.48514, 0.02693
 0.47874, 0.02712
 0.47240, 0.02730
 0.46614, 0.02747
 0.45996, 0.02764
 0.45384, 0.02780
 0.44780, 0.02796
 0.44182, 0.02811
 0.43591, 0.02825
 0.43007, 0.02839
 0.42430, 0.02852
 0.41859, 0.02864
 0.41295, 0.02876
 0.40737, 0.02887
 0.40185, 0.02898
 0.39639, 0.02908
 0.39099, 0.02918
 0.38566, 0.02927
 0.38038, 0.02935
 0.37516, 0.02943
 0.37000, 0.02950
 0.36489, 0.02957
 0.35984, 0.02963
 0.35484, 0.02969
 0.34990, 0.02974
 0.34501, 0.02979
 0.34017, 0.02983
 0.33538, 0.02987
 0.33065, 0.02991
 0.32596, 0.02993
 0.32133, 0.02996
 0.31674, 0.02998
 0.31220, 0.02999
 0.30771, 0.03000
 0.30326, 0.03001
 0.29887, 0.03001
 0.29451, 0.03001
 0.29020, 0.03000
 0.28594, 0.02999
 0.28172, 0.02997
 0.27754, 0.02995
 0.27340, 0.02993
 0.26931, 0.02990
 0.26526, 0.02987
 0.26125, 0.02983
 0.25728, 0.02979
 0.25334, 0.02975
 0.24945, 0.02970
 0.24560, 0.02965
 0.24178, 0.02959
 0.23800, 0.02953
 0.23426, 0.02947
 0.23056, 0.02941
 0.22689, 0.02934
 0.22326, 0.02926
 0.21966, 0.02919
 0.21610, 0.02911
 0.21257, 0.02902
 0.20907, 0.02893
 0.20561, 0.02884
 0.20218, 0.02875
 0.19879, 0.02865
 0.19542, 0.02855
 0.19209, 0.02845
 0.18879, 0.02834
 0.18552, 0.02823
 0.18228, 0.02812
 0.17908, 0.02800
 0.17590, 0.02788
 0.17275, 0.02776
 0.16963, 0.02763
 0.16654, 0.02750
 0.16348, 0.02737
 0.16044, 0.02723
 0.15743, 0.02709
 0.15445, 0.02695
 0.15150, 0.02680
 0.14858, 0.02665
 0.14568, 0.02650
 0.14280, 0.02635
 0.13996, 0.02619
 0.13713, 0.02603
 0.13434, 0.02586
 0.13157, 0.02569
 0.12882, 0.02552
 0.12610, 0.02535
 0.12340, 0.02517
 0.12072, 0.02499
 0.11807, 0.02481
 0.11544, 0.02462
 0.11283, 0.02443
 0.11025, 0.02424
 0.10769, 0.02404
 0.10515, 0.02384
 0.10264, 0.02363
 0.10014, 0.02343
 0.09767, 0.02321
 0.09521, 0.02300
 0.09278, 0.02278
 0.09037, 0.02256
 0.08798, 0.02233
 0.08561, 0.02210
 0.08326, 0.02187
 0.08093, 0.02163
 0.07862, 0.02139
 0.07633, 0.02114
 0.07405, 0.02089
 0.07180, 0.02064
 0.06956, 0.02038
 0.06735, 0.02012
 0.06515, 0.01985
 0.06297, 0.01957
 0.06081, 0.01929
 0.05866, 0.01901
 0.05653, 0.01872
 0.05442, 0.01842
 0.05233, 0.01812
 0.05026, 0.01781
 0.04820, 0.01750
 0.04615, 0.01717
 0.04413, 0.01684
 0.04212, 0.01651
 0.04012, 0.01616
 0.03815, 0.01581
 0.03618, 0.01544
 0.03424, 0.01507
 0.03231, 0.01468
 0.03039, 0.01428
 0.02849, 0.01387
 0.02660, 0.01345
 0.02473, 0.01301
 0.02287, 0.01255
 0.02103, 0.01208
 0.01920, 0.01158
 0.01739, 0.01106
 0.01559, 0.01051
 0.01380, 0.00992
 0.01203, 0.00930
 0.01027, 0.00863
 0.00853, 0.00790
 0.00680, 0.00708
 0.00508, 0.00615
 0.00337, 0.00504
 0.00168, 0.00359
 0.00056, 0.00209
 0.00000, 0.00000
 0.00000, 0.00000
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 0.00168,-0.00359
 0.00337,-0.00504
 0.00508,-0.00615
 0.00680,-0.00708
 0.00853,-0.00790
 0.01027,-0.00863
 0.01203,-0.00930
 0.01380,-0.00992
 0.01559,-0.01051
 0.01739,-0.01106
 0.01920,-0.01158
 0.02103,-0.01208
 0.02287,-0.01255
 0.02473,-0.01301
 0.02660,-0.01345
 0.02849,-0.01387
 0.03039,-0.01428
 0.03231,-0.01468
 0.03424,-0.01507
 0.03618,-0.01544
 0.03815,-0.01581
 0.04012,-0.01616
 0.04212,-0.01651
 0.04413,-0.01684
 0.04615,-0.01717
 0.04820,-0.01750
 0.05026,-0.01781
 0.05233,-0.01812
 0.05442,-0.01842
 0.05653,-0.01872
 0.05866,-0.01901
 0.06081,-0.01929
 0.06297,-0.01957
 0.06515,-0.01985
 0.06735,-0.02012
 0.06956,-0.02038
 0.07180,-0.02064
 0.07405,-0.02089
 0.07633,-0.02114
 0.07862,-0.02139
 0.08093,-0.02163
 0.08326,-0.02187
 0.08561,-0.02210
 0.08798,-0.02233
 0.09037,-0.02256
 0.09278,-0.02278
 0.09521,-0.02300
 0.09767,-0.02321
 0.10014,-0.02343
 0.10264,-0.02363
 0.10515,-0.02384
 0.10769,-0.02404
 0.11025,-0.02424
 0.11283,-0.02443
 0.11544,-0.02462
 0.11807,-0.02481
 0.12072,-0.02499
 0.12340,-0.02517
 0.12610,-0.02535
 0.12882,-0.02552
 0.13157,-0.02569
 0.13434,-0.02586
 0.13713,-0.02603
 0.13996,-0.02619
 0.14280,-0.02635
 0.14568,-0.02650
 0.14858,-0.02665
 0.15150,-0.02680
 0.15445,-0.02695
 0.15743,-0.02709
 0.16044,-0.02723
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 0.16654,-0.02750
 0.16963,-0.02763
 0.17275,-0.02776
 0.17590,-0.02788
 0.17908,-0.02800
 0.18228,-0.02812
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 0.18879,-0.02834
 0.19209,-0.02845
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 0.24560,-0.02965
 0.24945,-0.02970
 0.25334,-0.02975
 0.25728,-0.02979
 0.26125,-0.02983
 0.26526,-0.02987
 0.26931,-0.02990
 0.27340,-0.02993
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 0.31220,-0.02999
 0.31674,-0.02998
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 0.33538,-0.02987
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 0.35984,-0.02963
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 0.49163,-0.02673
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 0.63935,-0.02114
 0.64776,-0.02076
 0.65627,-0.02038
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