ファイルインデックス名　: File Index Name        : 1109        .A  
翼型整理番号　　　　　　: Airfoil Serial No.     : N04-0014-1
翼型名　　　　　　　　　: Airfoil Name           : N.A.C.A. 63-209
翼型ファイル番号　　　　: Airfoil File No.       : 1109
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-A01B1


座標　　　　　　　　　　: Plot Ordinates         :

 X             Y

 1.00000, 0.00000
 0.98660, 0.00133
 0.97339, 0.00267
 0.96038, 0.00403
 0.94756, 0.00539
 0.93492, 0.00676
 0.92246, 0.00814
 0.91019, 0.00952
 0.89808, 0.01092
 0.88615, 0.01232
 0.87438, 0.01372
 0.86278, 0.01511
 0.85135, 0.01650
 0.84007, 0.01786
 0.82896, 0.01920
 0.81800, 0.02054
 0.80719, 0.02184
 0.79653, 0.02313
 0.78602, 0.02439
 0.77565, 0.02562
 0.76542, 0.02684
 0.75533, 0.02802
 0.74539, 0.02919
 0.73558, 0.03032
 0.72590, 0.03143
 0.71635, 0.03251
 0.70693, 0.03357
 0.69763, 0.03459
 0.68846, 0.03560
 0.67940, 0.03657
 0.67046, 0.03751
 0.66166, 0.03842
 0.65295, 0.03931
 0.64437, 0.04016
 0.63589, 0.04099
 0.62753, 0.04179
 0.61928, 0.04257
 0.61112, 0.04332
 0.60308, 0.04404
 0.59513, 0.04473
 0.58729, 0.04540
 0.57955, 0.04604
 0.57190, 0.04667
 0.56435, 0.04727
 0.55690, 0.04783
 0.54954, 0.04839
 0.54226, 0.04891
 0.53508, 0.04941
 0.52799, 0.04988
 0.52098, 0.05033
 0.51407, 0.05076
 0.50723, 0.05118
 0.50048, 0.05156
 0.49381, 0.05193
 0.48722, 0.05227
 0.48070, 0.05260
 0.47427, 0.05290
 0.46791, 0.05319
 0.46163, 0.05345
 0.45543, 0.05370
 0.44929, 0.05393
 0.44323, 0.05414
 0.43723, 0.05433
 0.43131, 0.05451
 0.42546, 0.05466
 0.41967, 0.05481
 0.41395, 0.05493
 0.40830, 0.05504
 0.40272, 0.05513
 0.39719, 0.05522
 0.39172, 0.05528
 0.38632, 0.05533
 0.38099, 0.05537
 0.37570, 0.05539
 0.37048, 0.05539
 0.36533, 0.05539
 0.36022, 0.05538
 0.35517, 0.05535
 0.35017, 0.05531
 0.34524, 0.05525
 0.34035, 0.05518
 0.33552, 0.05510
 0.33074, 0.05502
 0.32602, 0.05491
 0.32133, 0.05481
 0.31671, 0.05469
 0.31214, 0.05455
 0.30761, 0.05442
 0.30313, 0.05428
 0.29869, 0.05411
 0.29432, 0.05395
 0.28997, 0.05378
 0.28568, 0.05359
 0.28143, 0.05341
 0.27723, 0.05321
 0.27307, 0.05301
 0.26894, 0.05280
 0.26487, 0.05259
 0.26084, 0.05237
 0.25685, 0.05215
 0.25290, 0.05191
 0.24898, 0.05167
 0.24511, 0.05144
 0.24128, 0.05118
 0.23748, 0.05093
 0.23372, 0.05068
 0.23001, 0.05041
 0.22633, 0.05014
 0.22268, 0.04986
 0.21907, 0.04959
 0.21550, 0.04931
 0.21196, 0.04902
 0.20846, 0.04873
 0.20498, 0.04843
 0.20155, 0.04814
 0.19814, 0.04783
 0.19478, 0.04753
 0.19143, 0.04722
 0.18813, 0.04690
 0.18486, 0.04658
 0.18162, 0.04626
 0.17840, 0.04594
 0.17523, 0.04561
 0.17208, 0.04527
 0.16896, 0.04494
 0.16587, 0.04460
 0.16280, 0.04426
 0.15977, 0.04391
 0.15676, 0.04356
 0.15378, 0.04321
 0.15083, 0.04286
 0.14791, 0.04249
 0.14502, 0.04214
 0.14216, 0.04176
 0.13931, 0.04140
 0.13650, 0.04102
 0.13370, 0.04065
 0.13094, 0.04027
 0.12820, 0.03989
 0.12549, 0.03951
 0.12280, 0.03913
 0.12013, 0.03874
 0.11748, 0.03835
 0.11487, 0.03794
 0.11227, 0.03754
 0.10969, 0.03715
 0.10715, 0.03674
 0.10462, 0.03634
 0.10212, 0.03592
 0.09964, 0.03551
 0.09718, 0.03509
 0.09474, 0.03467
 0.09232, 0.03424
 0.08993, 0.03382
 0.08755, 0.03339
 0.08520, 0.03295
 0.08287, 0.03251
 0.08055, 0.03208
 0.07826, 0.03163
 0.07599, 0.03118
 0.07374, 0.03073
 0.07150, 0.03027
 0.06928, 0.02980
 0.06708, 0.02934
 0.06491, 0.02886
 0.06275, 0.02839
 0.06061, 0.02791
 0.05850, 0.02742
 0.05639, 0.02693
 0.05430, 0.02642
 0.05223, 0.02591
 0.05019, 0.02541
 0.04816, 0.02489
 0.04614, 0.02437
 0.04414, 0.02383
 0.04216, 0.02329
 0.04020, 0.02274
 0.03825, 0.02218
 0.03633, 0.02162
 0.03440, 0.02105
 0.03251, 0.02047
 0.03063, 0.01987
 0.02876, 0.01926
 0.02692, 0.01864
 0.02508, 0.01800
 0.02327, 0.01736
 0.02146, 0.01670
 0.01968, 0.01603
 0.01791, 0.01533
 0.01616, 0.01461
 0.01442, 0.01384
 0.01270, 0.01304
 0.01100, 0.01219
 0.00932, 0.01127
 0.00766, 0.01028
 0.00602, 0.00921
 0.00440, 0.00800
 0.00282, 0.00656
 0.00128, 0.00468
 0.00033, 0.00275
 0.00000, 0.00000
 0.00000, 0.00000
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 0.03363,-0.01563
 0.03559,-0.01602
 0.03756,-0.01641
 0.03957,-0.01679
 0.04157,-0.01717
 0.04360,-0.01753
 0.04564,-0.01789
 0.04769,-0.01823
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 0.05186,-0.01892
 0.05395,-0.01924
 0.05607,-0.01956
 0.05821,-0.01989
 0.06036,-0.02020
 0.06254,-0.02051
 0.06473,-0.02081
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 0.08055,-0.02283
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 0.08523,-0.02338
 0.08760,-0.02364
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 0.09977,-0.02492
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 0.10479,-0.02542
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 0.10988,-0.02589
 0.11246,-0.02614
 0.11506,-0.02637
 0.11768,-0.02660
 0.12033,-0.02683
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 0.14237,-0.02857
 0.14523,-0.02877
 0.14813,-0.02898
 0.15104,-0.02917
 0.15398,-0.02937
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 0.17534,-0.03069
 0.17851,-0.03087
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 0.34794,-0.03472
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 0.49415,-0.02986
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 0.98665, 0.00066
 1.00000, 0.00000