ファイルインデックス名　: File Index Name        : 0210        .A  
翼型整理番号　　　　　　: Airfoil Serial No.     : N07-0012-1
翼型名　　　　　　　　　: Airfoil Name           : N 12
翼型ファイル番号　　　　: Airfoil File No.       : 0210
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, 0.00274
 0.97362, 0.00510
 0.96072, 0.00712
 0.94801, 0.00886
 0.93549, 0.01036
 0.92315, 0.01167
 0.91099, 0.01283
 0.89900, 0.01390
 0.88719, 0.01514
 0.87554, 0.01636
 0.86406, 0.01756
 0.85274, 0.01874
 0.84158, 0.01990
 0.83058, 0.02105
 0.81973, 0.02217
 0.80903, 0.02327
 0.79848, 0.02436
 0.78808, 0.02542
 0.77781, 0.02647
 0.76769, 0.02749
 0.75770, 0.02849
 0.74785, 0.02946
 0.73814, 0.03041
 0.72855, 0.03134
 0.71909, 0.03223
 0.70976, 0.03311
 0.70055, 0.03395
 0.69146, 0.03474
 0.68249, 0.03550
 0.67363, 0.03624
 0.66490, 0.03695
 0.65627, 0.03764
 0.64776, 0.03830
 0.63935, 0.03895
 0.63106, 0.03957
 0.62287, 0.04017
 0.61478, 0.04076
 0.60680, 0.04133
 0.59891, 0.04188
 0.59112, 0.04242
 0.58344, 0.04295
 0.57584, 0.04346
 0.56834, 0.04396
 0.56094, 0.04444
 0.55362, 0.04490
 0.54639, 0.04535
 0.53925, 0.04579
 0.53220, 0.04621
 0.52523, 0.04661
 0.51835, 0.04701
 0.51155, 0.04738
 0.50483, 0.04775
 0.49819, 0.04809
 0.49163, 0.04843
 0.48514, 0.04875
 0.47874, 0.04906
 0.47240, 0.04936
 0.46614, 0.04964
 0.45996, 0.04991
 0.45384, 0.05017
 0.44780, 0.05041
 0.44182, 0.05065
 0.43591, 0.05087
 0.43007, 0.05108
 0.42430, 0.05127
 0.41859, 0.05146
 0.41295, 0.05164
 0.40737, 0.05180
 0.40185, 0.05195
 0.39639, 0.05208
 0.39099, 0.05220
 0.38566, 0.05230
 0.38038, 0.05240
 0.37516, 0.05249
 0.37000, 0.05256
 0.36489, 0.05263
 0.35984, 0.05269
 0.35484, 0.05274
 0.34990, 0.05278
 0.34501, 0.05282
 0.34017, 0.05284
 0.33538, 0.05286
 0.33065, 0.05288
 0.32596, 0.05288
 0.32133, 0.05288
 0.31674, 0.05288
 0.31220, 0.05286
 0.30771, 0.05285
 0.30326, 0.05282
 0.29887, 0.05280
 0.29451, 0.05279
 0.29020, 0.05278
 0.28594, 0.05277
 0.28172, 0.05275
 0.27754, 0.05272
 0.27340, 0.05269
 0.26931, 0.05265
 0.26526, 0.05260
 0.26125, 0.05256
 0.25728, 0.05250
 0.25334, 0.05244
 0.24945, 0.05237
 0.24560, 0.05230
 0.24178, 0.05222
 0.23800, 0.05213
 0.23426, 0.05204
 0.23056, 0.05194
 0.22689, 0.05184
 0.22326, 0.05172
 0.21966, 0.05160
 0.21610, 0.05148
 0.21257, 0.05135
 0.20907, 0.05121
 0.20561, 0.05106
 0.20218, 0.05090
 0.19879, 0.05074
 0.19542, 0.05058
 0.19209, 0.05041
 0.18879, 0.05023
 0.18552, 0.05005
 0.18228, 0.04985
 0.17908, 0.04965
 0.17590, 0.04943
 0.17275, 0.04921
 0.16963, 0.04897
 0.16654, 0.04873
 0.16348, 0.04848
 0.16044, 0.04821
 0.15743, 0.04794
 0.15445, 0.04765
 0.15150, 0.04736
 0.14858, 0.04702
 0.14568, 0.04663
 0.14280, 0.04623
 0.13996, 0.04583
 0.13713, 0.04541
 0.13434, 0.04499
 0.13157, 0.04456
 0.12882, 0.04412
 0.12610, 0.04368
 0.12340, 0.04324
 0.12072, 0.04279
 0.11807, 0.04234
 0.11544, 0.04189
 0.11283, 0.04144
 0.11025, 0.04099
 0.10769, 0.04054
 0.10515, 0.04010
 0.10264, 0.03966
 0.10014, 0.03922
 0.09767, 0.03886
 0.09521, 0.03849
 0.09278, 0.03813
 0.09037, 0.03776
 0.08798, 0.03739
 0.08561, 0.03701
 0.08326, 0.03663
 0.08093, 0.03624
 0.07862, 0.03585
 0.07633, 0.03544
 0.07405, 0.03501
 0.07180, 0.03455
 0.06956, 0.03407
 0.06735, 0.03358
 0.06515, 0.03308
 0.06297, 0.03257
 0.06081, 0.03205
 0.05866, 0.03151
 0.05653, 0.03097
 0.05442, 0.03041
 0.05233, 0.02985
 0.05026, 0.02927
 0.04820, 0.02870
 0.04615, 0.02811
 0.04413, 0.02751
 0.04212, 0.02691
 0.04012, 0.02629
 0.03815, 0.02566
 0.03618, 0.02502
 0.03424, 0.02437
 0.03231, 0.02370
 0.03039, 0.02302
 0.02849, 0.02233
 0.02660, 0.02162
 0.02473, 0.02090
 0.02287, 0.02017
 0.02103, 0.01943
 0.01920, 0.01865
 0.01739, 0.01785
 0.01559, 0.01700
 0.01380, 0.01610
 0.01203, 0.01514
 0.01027, 0.01410
 0.00853, 0.01297
 0.00680, 0.01170
 0.00508, 0.01024
 0.00337, 0.00846
 0.00168, 0.00609
 0.00056, 0.00359
 0.00000, 0.00000
 0.00000, 0.00000
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 0.00168,-0.00652
 0.00337,-0.00887
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 0.00680,-0.01192
 0.00853,-0.01307
 0.01027,-0.01407
 0.01203,-0.01497
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 0.01559,-0.01657
 0.01739,-0.01729
 0.01920,-0.01798
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 0.02287,-0.01928
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 0.02849,-0.02122
 0.03039,-0.02186
 0.03231,-0.02250
 0.03424,-0.02314
 0.03618,-0.02377
 0.03815,-0.02440
 0.04012,-0.02502
 0.04212,-0.02564
 0.04413,-0.02625
 0.04615,-0.02686
 0.04820,-0.02747
 0.05026,-0.02808
 0.05233,-0.02873
 0.05442,-0.02937
 0.05653,-0.03000
 0.05866,-0.03062
 0.06081,-0.03124
 0.06297,-0.03184
 0.06515,-0.03242
 0.06735,-0.03299
 0.06956,-0.03354
 0.07180,-0.03408
 0.07405,-0.03459
 0.07633,-0.03505
 0.07862,-0.03547
 0.08093,-0.03588
 0.08326,-0.03626
 0.08561,-0.03663
 0.08798,-0.03699
 0.09037,-0.03734
 0.09278,-0.03767
 0.09521,-0.03800
 0.09767,-0.03831
 0.10014,-0.03862
 0.10264,-0.03895
 0.10515,-0.03927
 0.10769,-0.03958
 0.11025,-0.03989
 0.11283,-0.04020
 0.11544,-0.04050
 0.11807,-0.04080
 0.12072,-0.04110
 0.12340,-0.04139
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 0.13157,-0.04224
 0.13434,-0.04252
 0.13713,-0.04280
 0.13996,-0.04307
 0.14280,-0.04334
 0.14568,-0.04361
 0.14858,-0.04387
 0.15150,-0.04414
 0.15445,-0.04441
 0.15743,-0.04468
 0.16044,-0.04495
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 0.16654,-0.04548
 0.16963,-0.04574
 0.17275,-0.04599
 0.17590,-0.04625
 0.17908,-0.04650
 0.18228,-0.04674
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 0.26526,-0.05111
 0.26931,-0.05123
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 0.49163,-0.04733
 0.49819,-0.04707
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 1.00000, 0.00000