ファイルインデックス名　: File Index Name        : 1253        .A  
翼型整理番号　　　　　　: Airfoil Serial No.     : N01-0088-1
翼型名　　　　　　　　　: Airfoil Name           : N.A.C.A. 0012F/0
翼型ファイル番号　　　　: Airfoil File No.       : 1253
翼型情報　　　　　　　　: Airfoil Information    : Original

算出前縁半径　　　　　　: Computed L.E.R.        : ?
算出前縁傾斜　　　　　　: Computed Slope of L.E. : ?
算出プログラム番号　　　: Computed Program No.   : X68eB03-C01G2


座標　　　　　　　　　　: Plot Ordinates         :

 X             Y

 1.00000, 0.00500
 0.98671, 0.00500
 0.97362, 0.00500
 0.96072, 0.00500
 0.94801, 0.00500
 0.93549, 0.00500
 0.92315, 0.00500
 0.91099, 0.00500
 0.89900, 0.00500
 0.88719, 0.00500
 0.87554, 0.00500
 0.86406, 0.00500
 0.85274, 0.00500
 0.84158, 0.00500
 0.83058, 0.00500
 0.81973, 0.00500
 0.80903, 0.00500
 0.79848, 0.00497
 0.78808, 0.00476
 0.77781, 0.00456
 0.76769, 0.00439
 0.75770, 0.00427
 0.74785, 0.00419
 0.73814, 0.00418
 0.72855, 0.00424
 0.71909, 0.00439
 0.70976, 0.00463
 0.70055, 0.00498
 0.69146, 0.00574
 0.68249, 0.00664
 0.67363, 0.00763
 0.66490, 0.00871
 0.65627, 0.00987
 0.64776, 0.01111
 0.63935, 0.01243
 0.63106, 0.01380
 0.62287, 0.01523
 0.61478, 0.01672
 0.60680, 0.01825
 0.59891, 0.01983
 0.59112, 0.02154
 0.58344, 0.02326
 0.57584, 0.02501
 0.56834, 0.02677
 0.56094, 0.02854
 0.55362, 0.03030
 0.54639, 0.03205
 0.53925, 0.03378
 0.53220, 0.03550
 0.52523, 0.03718
 0.51835, 0.03883
 0.51155, 0.04043
 0.50483, 0.04200
 0.49819, 0.04345
 0.49163, 0.04468
 0.48514, 0.04585
 0.47874, 0.04697
 0.47240, 0.04805
 0.46614, 0.04907
 0.45996, 0.05004
 0.45384, 0.05096
 0.44780, 0.05184
 0.44182, 0.05267
 0.43591, 0.05345
 0.43007, 0.05419
 0.42430, 0.05488
 0.41859, 0.05553
 0.41295, 0.05614
 0.40737, 0.05671
 0.40185, 0.05723
 0.39639, 0.05766
 0.39099, 0.05802
 0.38566, 0.05835
 0.38038, 0.05864
 0.37516, 0.05889
 0.37000, 0.05912
 0.36489, 0.05932
 0.35984, 0.05949
 0.35484, 0.05963
 0.34990, 0.05976
 0.34501, 0.05986
 0.34017, 0.05994
 0.33538, 0.06000
 0.33065, 0.06004
 0.32596, 0.06007
 0.32133, 0.06008
 0.31674, 0.06008
 0.31220, 0.06007
 0.30771, 0.06005
 0.30326, 0.06003
 0.29887, 0.06000
 0.29451, 0.06000
 0.29020, 0.05999
 0.28594, 0.05997
 0.28172, 0.05994
 0.27754, 0.05990
 0.27340, 0.05985
 0.26931, 0.05979
 0.26526, 0.05973
 0.26125, 0.05965
 0.25728, 0.05957
 0.25334, 0.05948
 0.24945, 0.05939
 0.24560, 0.05929
 0.24178, 0.05918
 0.23800, 0.05906
 0.23426, 0.05894
 0.23056, 0.05881
 0.22689, 0.05867
 0.22326, 0.05853
 0.21966, 0.05838
 0.21610, 0.05822
 0.21257, 0.05806
 0.20907, 0.05789
 0.20561, 0.05771
 0.20218, 0.05752
 0.19879, 0.05733
 0.19542, 0.05713
 0.19209, 0.05693
 0.18879, 0.05671
 0.18552, 0.05649
 0.18228, 0.05627
 0.17908, 0.05604
 0.17590, 0.05580
 0.17275, 0.05555
 0.16963, 0.05530
 0.16654, 0.05504
 0.16348, 0.05478
 0.16044, 0.05451
 0.15743, 0.05423
 0.15445, 0.05394
 0.15150, 0.05365
 0.14858, 0.05335
 0.14568, 0.05304
 0.14280, 0.05273
 0.13996, 0.05241
 0.13713, 0.05208
 0.13434, 0.05175
 0.13157, 0.05141
 0.12882, 0.05106
 0.12610, 0.05071
 0.12340, 0.05035
 0.12072, 0.04998
 0.11807, 0.04961
 0.11544, 0.04923
 0.11283, 0.04884
 0.11025, 0.04845
 0.10769, 0.04805
 0.10515, 0.04765
 0.10264, 0.04724
 0.10014, 0.04682
 0.09767, 0.04640
 0.09521, 0.04598
 0.09278, 0.04554
 0.09037, 0.04510
 0.08798, 0.04465
 0.08561, 0.04420
 0.08326, 0.04373
 0.08093, 0.04326
 0.07862, 0.04278
 0.07633, 0.04229
 0.07405, 0.04179
 0.07180, 0.04128
 0.06956, 0.04075
 0.06735, 0.04022
 0.06515, 0.03968
 0.06297, 0.03913
 0.06081, 0.03857
 0.05866, 0.03799
 0.05653, 0.03741
 0.05442, 0.03681
 0.05233, 0.03620
 0.05026, 0.03558
 0.04820, 0.03495
 0.04615, 0.03430
 0.04413, 0.03364
 0.04212, 0.03296
 0.04012, 0.03227
 0.03815, 0.03156
 0.03618, 0.03083
 0.03424, 0.03008
 0.03231, 0.02931
 0.03039, 0.02852
 0.02849, 0.02770
 0.02660, 0.02685
 0.02473, 0.02597
 0.02287, 0.02506
 0.02103, 0.02411
 0.01920, 0.02311
 0.01739, 0.02207
 0.01559, 0.02097
 0.01380, 0.01980
 0.01203, 0.01856
 0.01027, 0.01722
 0.00853, 0.01576
 0.00680, 0.01414
 0.00508, 0.01228
 0.00337, 0.01006
 0.00168, 0.00716
 0.00056, 0.00416
 0.00000, 0.00000
 0.00000, 0.00000
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 0.00168,-0.00716
 0.00337,-0.01006
 0.00508,-0.01228
 0.00680,-0.01414
 0.00853,-0.01576
 0.01027,-0.01722
 0.01203,-0.01856
 0.01380,-0.01980
 0.01559,-0.02097
 0.01739,-0.02207
 0.01920,-0.02311
 0.02103,-0.02411
 0.02287,-0.02506
 0.02473,-0.02597
 0.02660,-0.02685
 0.02849,-0.02770
 0.03039,-0.02852
 0.03231,-0.02931
 0.03424,-0.03008
 0.03618,-0.03083
 0.03815,-0.03156
 0.04012,-0.03227
 0.04212,-0.03296
 0.04413,-0.03364
 0.04615,-0.03430
 0.04820,-0.03495
 0.05026,-0.03558
 0.05233,-0.03620
 0.05442,-0.03681
 0.05653,-0.03741
 0.05866,-0.03799
 0.06081,-0.03857
 0.06297,-0.03913
 0.06515,-0.03968
 0.06735,-0.04022
 0.06956,-0.04075
 0.07180,-0.04128
 0.07405,-0.04179
 0.07633,-0.04229
 0.07862,-0.04278
 0.08093,-0.04326
 0.08326,-0.04373
 0.08561,-0.04420
 0.08798,-0.04465
 0.09037,-0.04510
 0.09278,-0.04554
 0.09521,-0.04598
 0.09767,-0.04640
 0.10014,-0.04682
 0.10264,-0.04724
 0.10515,-0.04765
 0.10769,-0.04805
 0.11025,-0.04845
 0.11283,-0.04884
 0.11544,-0.04923
 0.11807,-0.04961
 0.12072,-0.04998
 0.12340,-0.05035
 0.12610,-0.05071
 0.12882,-0.05106
 0.13157,-0.05141
 0.13434,-0.05175
 0.13713,-0.05208
 0.13996,-0.05241
 0.14280,-0.05273
 0.14568,-0.05304
 0.14858,-0.05335
 0.15150,-0.05365
 0.15445,-0.05394
 0.15743,-0.05423
 0.16044,-0.05451
 0.16348,-0.05478
 0.16654,-0.05504
 0.16963,-0.05530
 0.17275,-0.05555
 0.17590,-0.05580
 0.17908,-0.05604
 0.18228,-0.05627
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 0.23800,-0.05906
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 0.24945,-0.05939
 0.25334,-0.05948
 0.25728,-0.05957
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 0.26526,-0.05973
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 0.30326,-0.06003
 0.30771,-0.06005
 0.31220,-0.06007
 0.31674,-0.06008
 0.32133,-0.06008
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 0.33538,-0.06000
 0.34017,-0.05994
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