ファイルインデックス名　: File Index Name        : 1005        .A00
翼型整理番号　　　　　　: Airfoil Serial No.     : N01-0005-0
翼型名　　　　　　　　　: Airfoil Name           : N.A.C.A. 0010
翼型ファイル番号　　　　: Airfoil File No.       : 1005
翼型情報　　　　　　　　: Airfoil Information    : Computed

算出前縁半径　　　　　　: Computed L.E.R.        : 1.102 %
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, 0.00105
 0.98671, 0.00259
 0.97362, 0.00408
 0.96072, 0.00553
 0.94801, 0.00694
 0.93549, 0.00830
 0.92315, 0.00963
 0.91099, 0.01092
 0.89900, 0.01217
 0.88719, 0.01338
 0.87554, 0.01457
 0.86406, 0.01572
 0.85274, 0.01684
 0.84158, 0.01792
 0.83058, 0.01898
 0.81973, 0.02002
 0.80903, 0.02102
 0.79848, 0.02200
 0.78808, 0.02295
 0.77781, 0.02388
 0.76769, 0.02478
 0.75770, 0.02566
 0.74785, 0.02652
 0.73814, 0.02736
 0.72855, 0.02817
 0.71909, 0.02896
 0.70976, 0.02974
 0.70055, 0.03049
 0.69146, 0.03122
 0.68249, 0.03193
 0.67363, 0.03263
 0.66490, 0.03331
 0.65627, 0.03396
 0.64776, 0.03461
 0.63935, 0.03523
 0.63106, 0.03584
 0.62287, 0.03643
 0.61478, 0.03700
 0.60680, 0.03756
 0.59891, 0.03810
 0.59112, 0.03863
 0.58344, 0.03914
 0.57584, 0.03964
 0.56834, 0.04012
 0.56094, 0.04059
 0.55362, 0.04105
 0.54639, 0.04149
 0.53925, 0.04192
 0.53220, 0.04233
 0.52523, 0.04273
 0.51835, 0.04312
 0.51155, 0.04350
 0.50483, 0.04386
 0.49819, 0.04421
 0.49163, 0.04455
 0.48514, 0.04488
 0.47874, 0.04519
 0.47240, 0.04550
 0.46614, 0.04579
 0.45996, 0.04607
 0.45384, 0.04634
 0.44780, 0.04660
 0.44182, 0.04685
 0.43591, 0.04709
 0.43007, 0.04731
 0.42430, 0.04753
 0.41859, 0.04774
 0.41295, 0.04794
 0.40737, 0.04812
 0.40185, 0.04830
 0.39639, 0.04847
 0.39099, 0.04863
 0.38566, 0.04878
 0.38038, 0.04892
 0.37516, 0.04905
 0.37000, 0.04917
 0.36489, 0.04928
 0.35984, 0.04939
 0.35484, 0.04949
 0.34990, 0.04957
 0.34501, 0.04965
 0.34017, 0.04972
 0.33538, 0.04979
 0.33065, 0.04984
 0.32596, 0.04989
 0.32133, 0.04993
 0.31674, 0.04996
 0.31220, 0.04999
 0.30771, 0.05000
 0.30326, 0.05001
 0.29887, 0.05001
 0.29451, 0.05001
 0.29020, 0.05000
 0.28594, 0.04998
 0.28172, 0.04995
 0.27754, 0.04992
 0.27340, 0.04988
 0.26931, 0.04983
 0.26526, 0.04978
 0.26125, 0.04972
 0.25728, 0.04965
 0.25334, 0.04958
 0.24945, 0.04950
 0.24560, 0.04941
 0.24178, 0.04932
 0.23800, 0.04922
 0.23426, 0.04912
 0.23056, 0.04901
 0.22689, 0.04889
 0.22326, 0.04877
 0.21966, 0.04864
 0.21610, 0.04851
 0.21257, 0.04837
 0.20907, 0.04822
 0.20561, 0.04807
 0.20218, 0.04792
 0.19879, 0.04775
 0.19542, 0.04759
 0.19209, 0.04741
 0.18879, 0.04723
 0.18552, 0.04705
 0.18228, 0.04686
 0.17908, 0.04666
 0.17590, 0.04646
 0.17275, 0.04626
 0.16963, 0.04605
 0.16654, 0.04583
 0.16348, 0.04561
 0.16044, 0.04538
 0.15743, 0.04515
 0.15445, 0.04491
 0.15150, 0.04467
 0.14858, 0.04442
 0.14568, 0.04417
 0.14280, 0.04391
 0.13996, 0.04365
 0.13713, 0.04338
 0.13434, 0.04310
 0.13157, 0.04282
 0.12882, 0.04254
 0.12610, 0.04225
 0.12340, 0.04195
 0.12072, 0.04165
 0.11807, 0.04134
 0.11544, 0.04103
 0.11283, 0.04071
 0.11025, 0.04039
 0.10769, 0.04006
 0.10515, 0.03973
 0.10264, 0.03939
 0.10014, 0.03904
 0.09767, 0.03869
 0.09521, 0.03833
 0.09278, 0.03797
 0.09037, 0.03760
 0.08798, 0.03722
 0.08561, 0.03684
 0.08326, 0.03645
 0.08093, 0.03605
 0.07862, 0.03565
 0.07633, 0.03524
 0.07405, 0.03482
 0.07180, 0.03440
 0.06956, 0.03397
 0.06735, 0.03353
 0.06515, 0.03308
 0.06297, 0.03262
 0.06081, 0.03216
 0.05866, 0.03168
 0.05653, 0.03120
 0.05442, 0.03071
 0.05233, 0.03020
 0.05026, 0.02969
 0.04820, 0.02916
 0.04615, 0.02862
 0.04413, 0.02807
 0.04212, 0.02751
 0.04012, 0.02693
 0.03815, 0.02634
 0.03618, 0.02574
 0.03424, 0.02511
 0.03231, 0.02447
 0.03039, 0.02381
 0.02849, 0.02312
 0.02660, 0.02241
 0.02473, 0.02168
 0.02287, 0.02092
 0.02103, 0.02013
 0.01920, 0.01930
 0.01739, 0.01843
 0.01559, 0.01751
 0.01380, 0.01654
 0.01203, 0.01550
 0.01027, 0.01438
 0.00853, 0.01316
 0.00680, 0.01180
 0.00508, 0.01025
 0.00337, 0.00841
 0.00168, 0.00598
 0.00056, 0.00348
 0.00000, 0.00000
 0.00000, 0.00000
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 0.00168,-0.00598
 0.00337,-0.00841
 0.00508,-0.01025
 0.00680,-0.01180
 0.00853,-0.01316
 0.01027,-0.01438
 0.01203,-0.01550
 0.01380,-0.01654
 0.01559,-0.01751
 0.01739,-0.01843
 0.01920,-0.01930
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 0.02287,-0.02092
 0.02473,-0.02168
 0.02660,-0.02241
 0.02849,-0.02312
 0.03039,-0.02381
 0.03231,-0.02447
 0.03424,-0.02511
 0.03618,-0.02574
 0.03815,-0.02634
 0.04012,-0.02693
 0.04212,-0.02751
 0.04413,-0.02807
 0.04615,-0.02862
 0.04820,-0.02916
 0.05026,-0.02969
 0.05233,-0.03020
 0.05442,-0.03071
 0.05653,-0.03120
 0.05866,-0.03168
 0.06081,-0.03216
 0.06297,-0.03262
 0.06515,-0.03308
 0.06735,-0.03353
 0.06956,-0.03397
 0.07180,-0.03440
 0.07405,-0.03482
 0.07633,-0.03524
 0.07862,-0.03565
 0.08093,-0.03605
 0.08326,-0.03645
 0.08561,-0.03684
 0.08798,-0.03722
 0.09037,-0.03760
 0.09278,-0.03797
 0.09521,-0.03833
 0.09767,-0.03869
 0.10014,-0.03904
 0.10264,-0.03939
 0.10515,-0.03973
 0.10769,-0.04006
 0.11025,-0.04039
 0.11283,-0.04071
 0.11544,-0.04103
 0.11807,-0.04134
 0.12072,-0.04165
 0.12340,-0.04195
 0.12610,-0.04225
 0.12882,-0.04254
 0.13157,-0.04282
 0.13434,-0.04310
 0.13713,-0.04338
 0.13996,-0.04365
 0.14280,-0.04391
 0.14568,-0.04417
 0.14858,-0.04442
 0.15150,-0.04467
 0.15445,-0.04491
 0.15743,-0.04515
 0.16044,-0.04538
 0.16348,-0.04561
 0.16654,-0.04583
 0.16963,-0.04605
 0.17275,-0.04626
 0.17590,-0.04646
 0.17908,-0.04666
 0.18228,-0.04686
 0.18552,-0.04705
 0.18879,-0.04723
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 0.19542,-0.04759
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 0.23800,-0.04922
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 0.24560,-0.04941
 0.24945,-0.04950
 0.25334,-0.04958
 0.25728,-0.04965
 0.26125,-0.04972
 0.26526,-0.04978
 0.26931,-0.04983
 0.27340,-0.04988
 0.27754,-0.04992
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 0.30771,-0.05000
 0.31220,-0.04999
 0.31674,-0.04996
 0.32133,-0.04993
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 0.42430,-0.04753
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 0.43591,-0.04709
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 0.49163,-0.04455
 0.49819,-0.04421
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 0.55362,-0.04105
 0.56094,-0.04059
 0.56834,-0.04012
 0.57584,-0.03964
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 0.63935,-0.03523
 0.64776,-0.03461
 0.65627,-0.03396
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 0.67363,-0.03263
 0.68249,-0.03193
 0.69146,-0.03122
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