ファイルインデックス名　: File Index Name        : 1188        .A  
翼型整理番号　　　　　　: Airfoil Serial No.     : N04-0093-1
翼型名　　　　　　　　　: Airfoil Name           : N.A.C.A. 66-009
翼型ファイル番号　　　　: Airfoil File No.       : 1188
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, 0.00071
 0.97362, 0.00162
 0.96072, 0.00271
 0.94801, 0.00394
 0.93549, 0.00529
 0.92315, 0.00672
 0.91099, 0.00821
 0.89900, 0.00974
 0.88719, 0.01124
 0.87554, 0.01275
 0.86406, 0.01425
 0.85274, 0.01575
 0.84158, 0.01722
 0.83058, 0.01866
 0.81973, 0.02008
 0.80903, 0.02147
 0.79848, 0.02282
 0.78808, 0.02414
 0.77781, 0.02542
 0.76769, 0.02666
 0.75770, 0.02786
 0.74785, 0.02902
 0.73814, 0.03015
 0.72855, 0.03123
 0.71909, 0.03227
 0.70976, 0.03327
 0.70055, 0.03422
 0.69146, 0.03513
 0.68249, 0.03600
 0.67363, 0.03682
 0.66490, 0.03759
 0.65627, 0.03832
 0.64776, 0.03899
 0.63935, 0.03962
 0.63106, 0.04020
 0.62287, 0.04074
 0.61478, 0.04123
 0.60680, 0.04168
 0.59891, 0.04209
 0.59112, 0.04244
 0.58344, 0.04276
 0.57584, 0.04304
 0.56834, 0.04329
 0.56094, 0.04352
 0.55362, 0.04372
 0.54639, 0.04390
 0.53925, 0.04408
 0.53220, 0.04423
 0.52523, 0.04437
 0.51835, 0.04449
 0.51155, 0.04460
 0.50483, 0.04469
 0.49819, 0.04477
 0.49163, 0.04484
 0.48514, 0.04489
 0.47874, 0.04494
 0.47240, 0.04497
 0.46614, 0.04499
 0.45996, 0.04500
 0.45384, 0.04500
 0.44780, 0.04499
 0.44182, 0.04497
 0.43591, 0.04494
 0.43007, 0.04490
 0.42430, 0.04486
 0.41859, 0.04480
 0.41295, 0.04474
 0.40737, 0.04467
 0.40185, 0.04460
 0.39639, 0.04451
 0.39099, 0.04442
 0.38566, 0.04433
 0.38038, 0.04422
 0.37516, 0.04411
 0.37000, 0.04400
 0.36489, 0.04387
 0.35984, 0.04375
 0.35484, 0.04361
 0.34990, 0.04348
 0.34501, 0.04334
 0.34017, 0.04319
 0.33538, 0.04304
 0.33065, 0.04288
 0.32596, 0.04272
 0.32133, 0.04256
 0.31674, 0.04239
 0.31220, 0.04222
 0.30771, 0.04204
 0.30326, 0.04187
 0.29887, 0.04168
 0.29451, 0.04150
 0.29020, 0.04131
 0.28594, 0.04111
 0.28172, 0.04092
 0.27754, 0.04072
 0.27340, 0.04051
 0.26931, 0.04031
 0.26526, 0.04010
 0.26125, 0.03989
 0.25728, 0.03968
 0.25334, 0.03946
 0.24945, 0.03924
 0.24560, 0.03902
 0.24178, 0.03879
 0.23800, 0.03857
 0.23426, 0.03834
 0.23056, 0.03810
 0.22689, 0.03787
 0.22326, 0.03763
 0.21966, 0.03740
 0.21610, 0.03716
 0.21257, 0.03691
 0.20907, 0.03667
 0.20561, 0.03642
 0.20218, 0.03617
 0.19879, 0.03592
 0.19542, 0.03567
 0.19209, 0.03541
 0.18879, 0.03515
 0.18552, 0.03489
 0.18228, 0.03463
 0.17908, 0.03437
 0.17590, 0.03411
 0.17275, 0.03384
 0.16963, 0.03357
 0.16654, 0.03330
 0.16348, 0.03303
 0.16044, 0.03276
 0.15743, 0.03248
 0.15445, 0.03220
 0.15150, 0.03192
 0.14858, 0.03164
 0.14568, 0.03136
 0.14280, 0.03107
 0.13996, 0.03079
 0.13713, 0.03050
 0.13434, 0.03021
 0.13157, 0.02992
 0.12882, 0.02962
 0.12610, 0.02933
 0.12340, 0.02903
 0.12072, 0.02873
 0.11807, 0.02843
 0.11544, 0.02813
 0.11283, 0.02783
 0.11025, 0.02752
 0.10769, 0.02721
 0.10515, 0.02690
 0.10264, 0.02659
 0.10014, 0.02628
 0.09767, 0.02596
 0.09521, 0.02564
 0.09278, 0.02532
 0.09037, 0.02500
 0.08798, 0.02468
 0.08561, 0.02435
 0.08326, 0.02402
 0.08093, 0.02369
 0.07862, 0.02336
 0.07633, 0.02303
 0.07405, 0.02269
 0.07180, 0.02235
 0.06956, 0.02201
 0.06735, 0.02167
 0.06515, 0.02133
 0.06297, 0.02098
 0.06081, 0.02064
 0.05866, 0.02028
 0.05653, 0.01993
 0.05442, 0.01957
 0.05233, 0.01921
 0.05026, 0.01885
 0.04820, 0.01848
 0.04615, 0.01810
 0.04413, 0.01772
 0.04212, 0.01734
 0.04012, 0.01695
 0.03815, 0.01655
 0.03618, 0.01615
 0.03424, 0.01575
 0.03231, 0.01534
 0.03039, 0.01492
 0.02849, 0.01449
 0.02660, 0.01406
 0.02473, 0.01362
 0.02287, 0.01319
 0.02103, 0.01275
 0.01920, 0.01229
 0.01739, 0.01180
 0.01559, 0.01129
 0.01380, 0.01073
 0.01203, 0.01013
 0.01027, 0.00946
 0.00853, 0.00872
 0.00680, 0.00789
 0.00508, 0.00692
 0.00337, 0.00574
 0.00168, 0.00414
 0.00056, 0.00245
 0.00000, 0.00000
 0.00000, 0.00000
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 0.03618,-0.01615
 0.03815,-0.01655
 0.04012,-0.01695
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 0.05442,-0.01957
 0.05653,-0.01993
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 0.08093,-0.02369
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 0.09037,-0.02500
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 0.10014,-0.02628
 0.10264,-0.02659
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 0.10769,-0.02721
 0.11025,-0.02752
 0.11283,-0.02783
 0.11544,-0.02813
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 0.12072,-0.02873
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 0.14280,-0.03107
 0.14568,-0.03136
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 0.15445,-0.03220
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 1.00000, 0.00000