ファイルインデックス名　: File Index Name        : 1225-2      .A  
翼型整理番号　　　　　　: Airfoil Serial No.     : N06-0007-2
翼型名　　　　　　　　　: Airfoil Name           : N.A.C.A. 5-H-10
翼型ファイル番号　　　　: Airfoil File No.       : 1225
翼型情報　　　　　　　　: Airfoil Information    : 

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, 0.00000
 0.98671, 0.00061
 0.97362, 0.00128
 0.96072, 0.00202
 0.94801, 0.00283
 0.93549, 0.00371
 0.92315, 0.00467
 0.91099, 0.00569
 0.89900, 0.00680
 0.88719, 0.00803
 0.87554, 0.00933
 0.86406, 0.01071
 0.85274, 0.01216
 0.84158, 0.01368
 0.83058, 0.01525
 0.81973, 0.01687
 0.80903, 0.01854
 0.79848, 0.02026
 0.78808, 0.02211
 0.77781, 0.02399
 0.76769, 0.02588
 0.75770, 0.02778
 0.74785, 0.02968
 0.73814, 0.03157
 0.72855, 0.03345
 0.71909, 0.03530
 0.70976, 0.03711
 0.70055, 0.03889
 0.69146, 0.04050
 0.68249, 0.04204
 0.67363, 0.04354
 0.66490, 0.04500
 0.65627, 0.04642
 0.64776, 0.04779
 0.63935, 0.04912
 0.63106, 0.05040
 0.62287, 0.05165
 0.61478, 0.05286
 0.60680, 0.05403
 0.59891, 0.05516
 0.59112, 0.05626
 0.58344, 0.05733
 0.57584, 0.05836
 0.56834, 0.05935
 0.56094, 0.06030
 0.55362, 0.06121
 0.54639, 0.06209
 0.53925, 0.06293
 0.53220, 0.06373
 0.52523, 0.06449
 0.51835, 0.06521
 0.51155, 0.06590
 0.50483, 0.06655
 0.49819, 0.06715
 0.49163, 0.06770
 0.48514, 0.06820
 0.47874, 0.06867
 0.47240, 0.06911
 0.46614, 0.06952
 0.45996, 0.06989
 0.45384, 0.07023
 0.44780, 0.07053
 0.44182, 0.07081
 0.43591, 0.07106
 0.43007, 0.07128
 0.42430, 0.07147
 0.41859, 0.07164
 0.41295, 0.07178
 0.40737, 0.07189
 0.40185, 0.07198
 0.39639, 0.07202
 0.39099, 0.07204
 0.38566, 0.07203
 0.38038, 0.07200
 0.37516, 0.07195
 0.37000, 0.07188
 0.36489, 0.07179
 0.35984, 0.07168
 0.35484, 0.07156
 0.34990, 0.07141
 0.34501, 0.07126
 0.34017, 0.07108
 0.33538, 0.07089
 0.33065, 0.07069
 0.32596, 0.07047
 0.32133, 0.07024
 0.31674, 0.07000
 0.31220, 0.06975
 0.30771, 0.06948
 0.30326, 0.06921
 0.29887, 0.06892
 0.29451, 0.06861
 0.29020, 0.06829
 0.28594, 0.06797
 0.28172, 0.06764
 0.27754, 0.06731
 0.27340, 0.06697
 0.26931, 0.06663
 0.26526, 0.06630
 0.26125, 0.06596
 0.25728, 0.06562
 0.25334, 0.06529
 0.24945, 0.06496
 0.24560, 0.06469
 0.24178, 0.06442
 0.23800, 0.06415
 0.23426, 0.06389
 0.23056, 0.06362
 0.22689, 0.06334
 0.22326, 0.06306
 0.21966, 0.06278
 0.21610, 0.06249
 0.21257, 0.06218
 0.20907, 0.06187
 0.20561, 0.06155
 0.20218, 0.06122
 0.19879, 0.06085
 0.19542, 0.06041
 0.19209, 0.05997
 0.18879, 0.05951
 0.18552, 0.05903
 0.18228, 0.05855
 0.17908, 0.05806
 0.17590, 0.05755
 0.17275, 0.05704
 0.16963, 0.05652
 0.16654, 0.05600
 0.16348, 0.05546
 0.16044, 0.05493
 0.15743, 0.05438
 0.15445, 0.05383
 0.15150, 0.05328
 0.14858, 0.05274
 0.14568, 0.05219
 0.14280, 0.05164
 0.13996, 0.05110
 0.13713, 0.05055
 0.13434, 0.05000
 0.13157, 0.04945
 0.12882, 0.04891
 0.12610, 0.04836
 0.12340, 0.04781
 0.12072, 0.04727
 0.11807, 0.04673
 0.11544, 0.04619
 0.11283, 0.04565
 0.11025, 0.04512
 0.10769, 0.04459
 0.10515, 0.04406
 0.10264, 0.04355
 0.10014, 0.04303
 0.09767, 0.04256
 0.09521, 0.04210
 0.09278, 0.04164
 0.09037, 0.04118
 0.08798, 0.04071
 0.08561, 0.04024
 0.08326, 0.03976
 0.08093, 0.03928
 0.07862, 0.03879
 0.07633, 0.03830
 0.07405, 0.03777
 0.07180, 0.03723
 0.06956, 0.03667
 0.06735, 0.03610
 0.06515, 0.03551
 0.06297, 0.03492
 0.06081, 0.03431
 0.05866, 0.03369
 0.05653, 0.03306
 0.05442, 0.03241
 0.05233, 0.03176
 0.05026, 0.03109
 0.04820, 0.03038
 0.04615, 0.02965
 0.04413, 0.02891
 0.04212, 0.02816
 0.04012, 0.02739
 0.03815, 0.02662
 0.03618, 0.02583
 0.03424, 0.02503
 0.03231, 0.02422
 0.03039, 0.02340
 0.02849, 0.02257
 0.02660, 0.02172
 0.02473, 0.02088
 0.02287, 0.02008
 0.02103, 0.01926
 0.01920, 0.01842
 0.01739, 0.01756
 0.01559, 0.01666
 0.01380, 0.01572
 0.01203, 0.01473
 0.01027, 0.01367
 0.00853, 0.01253
 0.00680, 0.01127
 0.00508, 0.00983
 0.00337, 0.00810
 0.00168, 0.00581
 0.00056, 0.00341
 0.00000, 0.00000
 0.00000, 0.00000
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 0.00680,-0.00727
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 0.01559,-0.01012
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 0.02849,-0.01257
 0.03039,-0.01286
 0.03231,-0.01314
 0.03424,-0.01340
 0.03618,-0.01364
 0.03815,-0.01388
 0.04012,-0.01410
 0.04212,-0.01431
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 0.04615,-0.01469
 0.04820,-0.01486
 0.05026,-0.01501
 0.05233,-0.01511
 0.05442,-0.01519
 0.05653,-0.01527
 0.05866,-0.01535
 0.06081,-0.01543
 0.06297,-0.01551
 0.06515,-0.01559
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 0.06956,-0.01576
 0.07180,-0.01585
 0.07405,-0.01595
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 0.07862,-0.01626
 0.08093,-0.01644
 0.08326,-0.01662
 0.08561,-0.01681
 0.08798,-0.01700
 0.09037,-0.01720
 0.09278,-0.01740
 0.09521,-0.01760
 0.09767,-0.01781
 0.10014,-0.01801
 0.10264,-0.01819
 0.10515,-0.01836
 0.10769,-0.01854
 0.11025,-0.01871
 0.11283,-0.01888
 0.11544,-0.01905
 0.11807,-0.01922
 0.12072,-0.01938
 0.12340,-0.01955
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 0.12882,-0.01987
 0.13157,-0.02003
 0.13434,-0.02018
 0.13713,-0.02033
 0.13996,-0.02049
 0.14280,-0.02064
 0.14568,-0.02078
 0.14858,-0.02093
 0.15150,-0.02107
 0.15445,-0.02122
 0.15743,-0.02136
 0.16044,-0.02150
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 0.16654,-0.02177
 0.16963,-0.02190
 0.17275,-0.02203
 0.17590,-0.02216
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 0.26526,-0.02431
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 1.00000, 0.00000