ファイルインデックス名　: File Index Name        : 1110        .A  
翼型整理番号　　　　　　: Airfoil Serial No.     : N04-0015-1
翼型名　　　　　　　　　: Airfoil Name           : N.A.C.A. 63-210
翼型ファイル番号　　　　: Airfoil File No.       : 1110
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, 0.00136
 0.97339, 0.00274
 0.96037, 0.00415
 0.94754, 0.00559
 0.93490, 0.00704
 0.92243, 0.00851
 0.91015, 0.00999
 0.89803, 0.01149
 0.88609, 0.01299
 0.87432, 0.01449
 0.86271, 0.01599
 0.85126, 0.01748
 0.83998, 0.01896
 0.82886, 0.02041
 0.81789, 0.02184
 0.80707, 0.02327
 0.79640, 0.02465
 0.78588, 0.02602
 0.77550, 0.02738
 0.76527, 0.02870
 0.75517, 0.03000
 0.74521, 0.03127
 0.73540, 0.03251
 0.72570, 0.03372
 0.71614, 0.03491
 0.70672, 0.03607
 0.69741, 0.03719
 0.68823, 0.03830
 0.67917, 0.03936
 0.67022, 0.04040
 0.66141, 0.04140
 0.65269, 0.04238
 0.64410, 0.04332
 0.63562, 0.04424
 0.62725, 0.04512
 0.61899, 0.04598
 0.61083, 0.04682
 0.60278, 0.04761
 0.59483, 0.04839
 0.58697, 0.04913
 0.57923, 0.04984
 0.57158, 0.05053
 0.56402, 0.05119
 0.55657, 0.05182
 0.54920, 0.05242
 0.54192, 0.05301
 0.53473, 0.05357
 0.52763, 0.05410
 0.52062, 0.05461
 0.51370, 0.05509
 0.50686, 0.05554
 0.50010, 0.05599
 0.49343, 0.05640
 0.48684, 0.05678
 0.48032, 0.05715
 0.47389, 0.05749
 0.46752, 0.05781
 0.46124, 0.05811
 0.45503, 0.05839
 0.44889, 0.05865
 0.44283, 0.05889
 0.43683, 0.05911
 0.43090, 0.05931
 0.42505, 0.05949
 0.41927, 0.05965
 0.41354, 0.05980
 0.40789, 0.05994
 0.40230, 0.06005
 0.39677, 0.06014
 0.39131, 0.06021
 0.38590, 0.06028
 0.38057, 0.06033
 0.37529, 0.06036
 0.37006, 0.06038
 0.36490, 0.06038
 0.35980, 0.06036
 0.35475, 0.06034
 0.34975, 0.06030
 0.34481, 0.06025
 0.33993, 0.06018
 0.33510, 0.06010
 0.33032, 0.06001
 0.32559, 0.05990
 0.32091, 0.05979
 0.31629, 0.05966
 0.31172, 0.05953
 0.30719, 0.05938
 0.30271, 0.05923
 0.29828, 0.05906
 0.29390, 0.05889
 0.28956, 0.05870
 0.28526, 0.05851
 0.28102, 0.05831
 0.27682, 0.05810
 0.27265, 0.05788
 0.26853, 0.05766
 0.26446, 0.05742
 0.26043, 0.05718
 0.25644, 0.05694
 0.25250, 0.05669
 0.24858, 0.05643
 0.24471, 0.05617
 0.24088, 0.05591
 0.23709, 0.05563
 0.23333, 0.05535
 0.22961, 0.05507
 0.22594, 0.05477
 0.22229, 0.05448
 0.21869, 0.05418
 0.21511, 0.05387
 0.21158, 0.05356
 0.20808, 0.05325
 0.20460, 0.05293
 0.20117, 0.05260
 0.19777, 0.05228
 0.19441, 0.05194
 0.19106, 0.05161
 0.18776, 0.05126
 0.18449, 0.05092
 0.18125, 0.05057
 0.17804, 0.05022
 0.17487, 0.04986
 0.17172, 0.04950
 0.16860, 0.04913
 0.16551, 0.04876
 0.16246, 0.04839
 0.15943, 0.04802
 0.15642, 0.04763
 0.15344, 0.04725
 0.15049, 0.04686
 0.14758, 0.04648
 0.14469, 0.04608
 0.14182, 0.04568
 0.13898, 0.04528
 0.13617, 0.04488
 0.13338, 0.04447
 0.13062, 0.04406
 0.12789, 0.04365
 0.12517, 0.04323
 0.12249, 0.04281
 0.11982, 0.04239
 0.11718, 0.04195
 0.11457, 0.04152
 0.11197, 0.04109
 0.10940, 0.04065
 0.10686, 0.04021
 0.10433, 0.03976
 0.10183, 0.03932
 0.09936, 0.03887
 0.09690, 0.03841
 0.09447, 0.03796
 0.09205, 0.03749
 0.08966, 0.03702
 0.08728, 0.03656
 0.08493, 0.03608
 0.08261, 0.03560
 0.08030, 0.03512
 0.07801, 0.03463
 0.07574, 0.03414
 0.07349, 0.03365
 0.07125, 0.03314
 0.06905, 0.03264
 0.06685, 0.03213
 0.06468, 0.03161
 0.06253, 0.03109
 0.06039, 0.03057
 0.05827, 0.03004
 0.05617, 0.02950
 0.05409, 0.02895
 0.05202, 0.02840
 0.04998, 0.02784
 0.04796, 0.02728
 0.04595, 0.02670
 0.04395, 0.02612
 0.04198, 0.02553
 0.04002, 0.02493
 0.03807, 0.02433
 0.03615, 0.02371
 0.03423, 0.02308
 0.03235, 0.02245
 0.03047, 0.02180
 0.02861, 0.02113
 0.02676, 0.02045
 0.02493, 0.01976
 0.02312, 0.01904
 0.02133, 0.01830
 0.01955, 0.01754
 0.01779, 0.01675
 0.01604, 0.01596
 0.01431, 0.01514
 0.01259, 0.01429
 0.01089, 0.01346
 0.00920, 0.01264
 0.00755, 0.01167
 0.00592, 0.01041
 0.00434, 0.00881
 0.00279, 0.00685
 0.00131, 0.00442
 0.00037, 0.00224
 0.00000, 0.00000
 0.00000, 0.00000
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 0.03184,-0.01715
 0.03380,-0.01762
 0.03577,-0.01808
 0.03774,-0.01852
 0.03975,-0.01895
 0.04176,-0.01938
 0.04379,-0.01980
 0.04583,-0.02020
 0.04789,-0.02060
 0.04997,-0.02099
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 0.05417,-0.02175
 0.05629,-0.02213
 0.05843,-0.02250
 0.06059,-0.02286
 0.06277,-0.02321
 0.06496,-0.02356
 0.06717,-0.02391
 0.06940,-0.02425
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 0.07390,-0.02491
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 0.08080,-0.02589
 0.08314,-0.02620
 0.08550,-0.02650
 0.08787,-0.02682
 0.09027,-0.02711
 0.09268,-0.02742
 0.09512,-0.02772
 0.09757,-0.02801
 0.10006,-0.02830
 0.10255,-0.02859
 0.10508,-0.02887
 0.10761,-0.02915
 0.11017,-0.02943
 0.11276,-0.02970
 0.11536,-0.02996
 0.11799,-0.03023
 0.12064,-0.03050
 0.12332,-0.03076
 0.12602,-0.03102
 0.12874,-0.03127
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 0.13985,-0.03226
 0.14270,-0.03250
 0.14556,-0.03274
 0.14846,-0.03298
 0.15138,-0.03322
 0.15432,-0.03344
 0.15729,-0.03367
 0.16029,-0.03390
 0.16332,-0.03412
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 0.17256,-0.03476
 0.17570,-0.03498
 0.17887,-0.03518
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 0.34353,-0.03976
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 0.36318,-0.03954
 0.36822,-0.03945
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 0.42748,-0.03771
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 0.48807,-0.03467
 0.49452,-0.03427
 0.50105,-0.03386
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 0.64962,-0.02205
 0.65807,-0.02127
 0.66663,-0.02048
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 0.68408,-0.01886
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 0.96063, 0.00109
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 0.98666, 0.00063
 1.00000, 0.00000