ファイルインデックス名　: File Index Name        : 1189        .A  
翼型整理番号　　　　　　: Airfoil Serial No.     : N04-0094-1
翼型名　　　　　　　　　: Airfoil Name           : N.A.C.A. 66-010
翼型ファイル番号　　　　: Airfoil File No.       : 1189
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, 0.00000
 0.98671, 0.00077
 0.97362, 0.00176
 0.96072, 0.00295
 0.94801, 0.00430
 0.93549, 0.00578
 0.92315, 0.00735
 0.91099, 0.00900
 0.89900, 0.01068
 0.88719, 0.01234
 0.87554, 0.01401
 0.86406, 0.01567
 0.85274, 0.01733
 0.84158, 0.01895
 0.83058, 0.02055
 0.81973, 0.02212
 0.80903, 0.02365
 0.79848, 0.02515
 0.78808, 0.02661
 0.77781, 0.02803
 0.76769, 0.02941
 0.75770, 0.03075
 0.74785, 0.03204
 0.73814, 0.03328
 0.72855, 0.03448
 0.71909, 0.03564
 0.70976, 0.03674
 0.70055, 0.03781
 0.69146, 0.03883
 0.68249, 0.03981
 0.67363, 0.04074
 0.66490, 0.04162
 0.65627, 0.04245
 0.64776, 0.04322
 0.63935, 0.04392
 0.63106, 0.04458
 0.62287, 0.04518
 0.61478, 0.04574
 0.60680, 0.04625
 0.59891, 0.04671
 0.59112, 0.04711
 0.58344, 0.04746
 0.57584, 0.04778
 0.56834, 0.04807
 0.56094, 0.04832
 0.55362, 0.04855
 0.54639, 0.04876
 0.53925, 0.04895
 0.53220, 0.04913
 0.52523, 0.04928
 0.51835, 0.04942
 0.51155, 0.04954
 0.50483, 0.04964
 0.49819, 0.04973
 0.49163, 0.04981
 0.48514, 0.04988
 0.47874, 0.04993
 0.47240, 0.04996
 0.46614, 0.04999
 0.45996, 0.05000
 0.45384, 0.05000
 0.44780, 0.05000
 0.44182, 0.04997
 0.43591, 0.04994
 0.43007, 0.04990
 0.42430, 0.04985
 0.41859, 0.04979
 0.41295, 0.04972
 0.40737, 0.04965
 0.40185, 0.04956
 0.39639, 0.04947
 0.39099, 0.04937
 0.38566, 0.04926
 0.38038, 0.04914
 0.37516, 0.04902
 0.37000, 0.04889
 0.36489, 0.04876
 0.35984, 0.04862
 0.35484, 0.04847
 0.34990, 0.04832
 0.34501, 0.04816
 0.34017, 0.04799
 0.33538, 0.04783
 0.33065, 0.04765
 0.32596, 0.04747
 0.32133, 0.04729
 0.31674, 0.04710
 0.31220, 0.04691
 0.30771, 0.04671
 0.30326, 0.04651
 0.29887, 0.04631
 0.29451, 0.04610
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 0.28594, 0.04567
 0.28172, 0.04546
 0.27754, 0.04523
 0.27340, 0.04501
 0.26931, 0.04478
 0.26526, 0.04455
 0.26125, 0.04432
 0.25728, 0.04408
 0.25334, 0.04384
 0.24945, 0.04360
 0.24560, 0.04335
 0.24178, 0.04310
 0.23800, 0.04285
 0.23426, 0.04259
 0.23056, 0.04234
 0.22689, 0.04208
 0.22326, 0.04181
 0.21966, 0.04155
 0.21610, 0.04128
 0.21257, 0.04101
 0.20907, 0.04074
 0.20561, 0.04047
 0.20218, 0.04019
 0.19879, 0.03991
 0.19542, 0.03963
 0.19209, 0.03934
 0.18879, 0.03906
 0.18552, 0.03877
 0.18228, 0.03848
 0.17908, 0.03819
 0.17590, 0.03789
 0.17275, 0.03759
 0.16963, 0.03729
 0.16654, 0.03699
 0.16348, 0.03669
 0.16044, 0.03639
 0.15743, 0.03608
 0.15445, 0.03577
 0.15150, 0.03546
 0.14858, 0.03515
 0.14568, 0.03483
 0.14280, 0.03452
 0.13996, 0.03420
 0.13713, 0.03388
 0.13434, 0.03356
 0.13157, 0.03323
 0.12882, 0.03291
 0.12610, 0.03258
 0.12340, 0.03225
 0.12072, 0.03192
 0.11807, 0.03158
 0.11544, 0.03125
 0.11283, 0.03091
 0.11025, 0.03057
 0.10769, 0.03023
 0.10515, 0.02988
 0.10264, 0.02954
 0.10014, 0.02919
 0.09767, 0.02884
 0.09521, 0.02848
 0.09278, 0.02813
 0.09037, 0.02777
 0.08798, 0.02741
 0.08561, 0.02705
 0.08326, 0.02668
 0.08093, 0.02632
 0.07862, 0.02595
 0.07633, 0.02558
 0.07405, 0.02520
 0.07180, 0.02483
 0.06956, 0.02445
 0.06735, 0.02407
 0.06515, 0.02369
 0.06297, 0.02330
 0.06081, 0.02292
 0.05866, 0.02252
 0.05653, 0.02213
 0.05442, 0.02173
 0.05233, 0.02133
 0.05026, 0.02092
 0.04820, 0.02051
 0.04615, 0.02009
 0.04413, 0.01967
 0.04212, 0.01924
 0.04012, 0.01880
 0.03815, 0.01836
 0.03618, 0.01792
 0.03424, 0.01747
 0.03231, 0.01701
 0.03039, 0.01654
 0.02849, 0.01606
 0.02660, 0.01558
 0.02473, 0.01509
 0.02287, 0.01462
 0.02103, 0.01413
 0.01920, 0.01361
 0.01739, 0.01308
 0.01559, 0.01251
 0.01380, 0.01189
 0.01203, 0.01123
 0.01027, 0.01049
 0.00853, 0.00967
 0.00680, 0.00874
 0.00508, 0.00765
 0.00337, 0.00631
 0.00168, 0.00453
 0.00056, 0.00266
 0.00000, 0.00000
 0.00000, 0.00000
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 0.03618,-0.01792
 0.03815,-0.01836
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 0.05442,-0.02173
 0.05653,-0.02213
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 0.08093,-0.02632
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 0.10014,-0.02919
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 0.10769,-0.03023
 0.11025,-0.03057
 0.11283,-0.03091
 0.11544,-0.03125
 0.11807,-0.03158
 0.12072,-0.03192
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 0.14568,-0.03483
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 1.00000, 0.00000