ファイルインデックス名　: File Index Name        : 1327        .A  
翼型整理番号　　　　　　: Airfoil Serial No.     : N06-0049-1
翼型名　　　　　　　　　: Airfoil Name           : N.A.C.A. 27
翼型ファイル番号　　　　: Airfoil File No.       : 1327
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.   : VB6B05-A01C


座標　　　　　　　　　　: Plot Ordinates         :

 X             Y

 1.00000, 0.00000
 0.98670, 0.00006
 0.97359, 0.00019
 0.96066, 0.00038
 0.94791, 0.00065
 0.93535, 0.00098
 0.92295, 0.00138
 0.91072, 0.00184
 0.89866, 0.00236
 0.88675, 0.00299
 0.87500, 0.00368
 0.86341, 0.00442
 0.85198, 0.00521
 0.84070, 0.00604
 0.82957, 0.00691
 0.81859, 0.00780
 0.80776, 0.00872
 0.79707, 0.00965
 0.78654, 0.01057
 0.77613, 0.01150
 0.76587, 0.01245
 0.75574, 0.01340
 0.74575, 0.01435
 0.73590, 0.01531
 0.72617, 0.01627
 0.71657, 0.01723
 0.70711, 0.01818
 0.69776, 0.01913
 0.68853, 0.02006
 0.67943, 0.02098
 0.67043, 0.02189
 0.66157, 0.02280
 0.65281, 0.02369
 0.64417, 0.02458
 0.63563, 0.02546
 0.62722, 0.02632
 0.61890, 0.02717
 0.61069, 0.02801
 0.60259, 0.02884
 0.59458, 0.02965
 0.58667, 0.03045
 0.57888, 0.03122
 0.57117, 0.03199
 0.56356, 0.03274
 0.55605, 0.03347
 0.54863, 0.03420
 0.54129, 0.03490
 0.53405, 0.03559
 0.52690, 0.03626
 0.51984, 0.03691
 0.51287, 0.03755
 0.50598, 0.03817
 0.49917, 0.03877
 0.49244, 0.03934
 0.48580, 0.03990
 0.47923, 0.04045
 0.47276, 0.04097
 0.46634, 0.04148
 0.46001, 0.04197
 0.45376, 0.04244
 0.44758, 0.04289
 0.44147, 0.04333
 0.43543, 0.04375
 0.42946, 0.04416
 0.42356, 0.04456
 0.41774, 0.04493
 0.41198, 0.04529
 0.40629, 0.04563
 0.40066, 0.04596
 0.39509, 0.04626
 0.38959, 0.04655
 0.38415, 0.04682
 0.37879, 0.04706
 0.37347, 0.04731
 0.36822, 0.04753
 0.36303, 0.04774
 0.35789, 0.04794
 0.35281, 0.04813
 0.34779, 0.04830
 0.34282, 0.04846
 0.33791, 0.04861
 0.33305, 0.04875
 0.32824, 0.04887
 0.32350, 0.04898
 0.31879, 0.04909
 0.31415, 0.04919
 0.30955, 0.04926
 0.30500, 0.04933
 0.30050, 0.04940
 0.29604, 0.04945
 0.29164, 0.04950
 0.28728, 0.04954
 0.28296, 0.04956
 0.27870, 0.04959
 0.27448, 0.04959
 0.27030, 0.04958
 0.26616, 0.04958
 0.26208, 0.04955
 0.25803, 0.04951
 0.25403, 0.04946
 0.25007, 0.04940
 0.24614, 0.04932
 0.24226, 0.04924
 0.23843, 0.04913
 0.23462, 0.04903
 0.23086, 0.04891
 0.22714, 0.04878
 0.22346, 0.04865
 0.21981, 0.04850
 0.21620, 0.04833
 0.21263, 0.04818
 0.20909, 0.04799
 0.20559, 0.04782
 0.20212, 0.04762
 0.19868, 0.04742
 0.19529, 0.04721
 0.19193, 0.04699
 0.18859, 0.04677
 0.18529, 0.04654
 0.18203, 0.04630
 0.17880, 0.04605
 0.17559, 0.04579
 0.17243, 0.04553
 0.16929, 0.04526
 0.16618, 0.04498
 0.16310, 0.04470
 0.16005, 0.04442
 0.15704, 0.04412
 0.15404, 0.04383
 0.15108, 0.04351
 0.14814, 0.04320
 0.14524, 0.04288
 0.14236, 0.04256
 0.13951, 0.04223
 0.13668, 0.04190
 0.13389, 0.04156
 0.13111, 0.04120
 0.12837, 0.04086
 0.12566, 0.04050
 0.12296, 0.04015
 0.12029, 0.03978
 0.11765, 0.03940
 0.11502, 0.03903
 0.11243, 0.03865
 0.10985, 0.03826
 0.10730, 0.03787
 0.10478, 0.03747
 0.10228, 0.03707
 0.09980, 0.03666
 0.09734, 0.03626
 0.09491, 0.03585
 0.09250, 0.03543
 0.09010, 0.03501
 0.08773, 0.03459
 0.08538, 0.03415
 0.08306, 0.03371
 0.08075, 0.03326
 0.07847, 0.03281
 0.07621, 0.03235
 0.07396, 0.03188
 0.07175, 0.03139
 0.06954, 0.03090
 0.06736, 0.03041
 0.06519, 0.02990
 0.06306, 0.02939
 0.06093, 0.02887
 0.05883, 0.02835
 0.05675, 0.02781
 0.05468, 0.02726
 0.05263, 0.02672
 0.05060, 0.02616
 0.04859, 0.02561
 0.04660, 0.02504
 0.04462, 0.02448
 0.04266, 0.02390
 0.04073, 0.02332
 0.03880, 0.02272
 0.03689, 0.02212
 0.03501, 0.02151
 0.03313, 0.02089
 0.03128, 0.02026
 0.02944, 0.01963
 0.02762, 0.01897
 0.02582, 0.01831
 0.02402, 0.01763
 0.02226, 0.01694
 0.02050, 0.01623
 0.01877, 0.01550
 0.01705, 0.01476
 0.01535, 0.01398
 0.01367, 0.01318
 0.01200, 0.01234
 0.01036, 0.01146
 0.00873, 0.01053
 0.00714, 0.00954
 0.00556, 0.00846
 0.00402, 0.00725
 0.00252, 0.00585
 0.00108, 0.00408
 0.00022, 0.00232
 0.00000, 0.00000
 0.00000, 0.00000
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 0.03592,-0.01147
 0.03788,-0.01165
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 0.04187,-0.01198
 0.04389,-0.01213
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 0.05210,-0.01259
 0.05418,-0.01267
 0.05628,-0.01274
 0.05840,-0.01281
 0.06054,-0.01286
 0.06270,-0.01291
 0.06486,-0.01296
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 0.08754,-0.01319
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 0.09960,-0.01320
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 0.10708,-0.01320
 0.10962,-0.01320
 0.11218,-0.01319
 0.11476,-0.01319
 0.11736,-0.01318
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 0.13903,-0.01303
 0.14186,-0.01300
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 0.14757,-0.01294
 0.15046,-0.01289
 0.15337,-0.01284
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 0.16229,-0.01267
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 0.17456,-0.01240
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 1.00000, 0.00000