ファイルインデックス名　: File Index Name        : 0161        .A  
翼型整理番号　　　　　　: Airfoil Serial No.     : Z00-0001-1
翼型名　　　　　　　　　: Airfoil Name           : Zurich 11
翼型ファイル番号　　　　: Airfoil File No.       : 0161
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, 0.00441
 0.97362, 0.00858
 0.96072, 0.01251
 0.94801, 0.01621
 0.93549, 0.01971
 0.92315, 0.02300
 0.91099, 0.02611
 0.89900, 0.02904
 0.88719, 0.03180
 0.87554, 0.03440
 0.86406, 0.03685
 0.85274, 0.03915
 0.84158, 0.04133
 0.83058, 0.04338
 0.81973, 0.04531
 0.80903, 0.04713
 0.79848, 0.04885
 0.78808, 0.05049
 0.77781, 0.05205
 0.76769, 0.05352
 0.75770, 0.05490
 0.74785, 0.05621
 0.73814, 0.05743
 0.72855, 0.05859
 0.71909, 0.05967
 0.70976, 0.06069
 0.70055, 0.06164
 0.69146, 0.06255
 0.68249, 0.06339
 0.67363, 0.06418
 0.66490, 0.06492
 0.65627, 0.06561
 0.64776, 0.06625
 0.63935, 0.06685
 0.63106, 0.06741
 0.62287, 0.06792
 0.61478, 0.06840
 0.60680, 0.06885
 0.59891, 0.06926
 0.59112, 0.06964
 0.58344, 0.06999
 0.57584, 0.07031
 0.56834, 0.07061
 0.56094, 0.07088
 0.55362, 0.07112
 0.54639, 0.07134
 0.53925, 0.07154
 0.53220, 0.07172
 0.52523, 0.07187
 0.51835, 0.07201
 0.51155, 0.07213
 0.50483, 0.07223
 0.49819, 0.07233
 0.49163, 0.07243
 0.48514, 0.07252
 0.47874, 0.07259
 0.47240, 0.07265
 0.46614, 0.07269
 0.45996, 0.07272
 0.45384, 0.07274
 0.44780, 0.07275
 0.44182, 0.07274
 0.43591, 0.07272
 0.43007, 0.07268
 0.42430, 0.07264
 0.41859, 0.07258
 0.41295, 0.07251
 0.40737, 0.07243
 0.40185, 0.07233
 0.39639, 0.07222
 0.39099, 0.07210
 0.38566, 0.07197
 0.38038, 0.07182
 0.37516, 0.07167
 0.37000, 0.07150
 0.36489, 0.07133
 0.35984, 0.07114
 0.35484, 0.07095
 0.34990, 0.07074
 0.34501, 0.07053
 0.34017, 0.07031
 0.33538, 0.07007
 0.33065, 0.06983
 0.32596, 0.06958
 0.32133, 0.06933
 0.31674, 0.06906
 0.31220, 0.06879
 0.30771, 0.06851
 0.30326, 0.06822
 0.29887, 0.06792
 0.29451, 0.06761
 0.29020, 0.06728
 0.28594, 0.06696
 0.28172, 0.06662
 0.27754, 0.06628
 0.27340, 0.06593
 0.26931, 0.06558
 0.26526, 0.06522
 0.26125, 0.06485
 0.25728, 0.06448
 0.25334, 0.06410
 0.24945, 0.06372
 0.24560, 0.06334
 0.24178, 0.06295
 0.23800, 0.06255
 0.23426, 0.06215
 0.23056, 0.06175
 0.22689, 0.06134
 0.22326, 0.06093
 0.21966, 0.06051
 0.21610, 0.06009
 0.21257, 0.05967
 0.20907, 0.05924
 0.20561, 0.05881
 0.20218, 0.05838
 0.19879, 0.05795
 0.19542, 0.05753
 0.19209, 0.05711
 0.18879, 0.05668
 0.18552, 0.05625
 0.18228, 0.05582
 0.17908, 0.05539
 0.17590, 0.05495
 0.17275, 0.05451
 0.16963, 0.05407
 0.16654, 0.05363
 0.16348, 0.05318
 0.16044, 0.05273
 0.15743, 0.05227
 0.15445, 0.05182
 0.15150, 0.05136
 0.14858, 0.05089
 0.14568, 0.05043
 0.14280, 0.04995
 0.13996, 0.04948
 0.13713, 0.04900
 0.13434, 0.04853
 0.13157, 0.04804
 0.12882, 0.04755
 0.12610, 0.04706
 0.12340, 0.04657
 0.12072, 0.04607
 0.11807, 0.04557
 0.11544, 0.04506
 0.11283, 0.04455
 0.11025, 0.04403
 0.10769, 0.04352
 0.10515, 0.04299
 0.10264, 0.04246
 0.10014, 0.04193
 0.09767, 0.04138
 0.09521, 0.04082
 0.09278, 0.04026
 0.09037, 0.03969
 0.08798, 0.03912
 0.08561, 0.03854
 0.08326, 0.03796
 0.08093, 0.03738
 0.07862, 0.03679
 0.07633, 0.03619
 0.07405, 0.03559
 0.07180, 0.03498
 0.06956, 0.03437
 0.06735, 0.03376
 0.06515, 0.03313
 0.06297, 0.03250
 0.06081, 0.03187
 0.05866, 0.03122
 0.05653, 0.03057
 0.05442, 0.02992
 0.05233, 0.02925
 0.05026, 0.02859
 0.04820, 0.02790
 0.04615, 0.02720
 0.04413, 0.02650
 0.04212, 0.02579
 0.04012, 0.02507
 0.03815, 0.02434
 0.03618, 0.02360
 0.03424, 0.02285
 0.03231, 0.02208
 0.03039, 0.02130
 0.02849, 0.02051
 0.02660, 0.01970
 0.02473, 0.01888
 0.02287, 0.01804
 0.02103, 0.01717
 0.01920, 0.01629
 0.01739, 0.01538
 0.01559, 0.01443
 0.01380, 0.01345
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 0.01027, 0.01136
 0.00853, 0.01023
 0.00680, 0.00900
 0.00508, 0.00766
 0.00337, 0.00611
 0.00168, 0.00420
 0.00056, 0.00236
 0.00000, 0.00000
 0.00000, 0.00000
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 0.00168,-0.00382
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 0.03039,-0.01225
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 0.03618,-0.01292
 0.03815,-0.01313
 0.04012,-0.01333
 0.04212,-0.01352
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 0.04615,-0.01388
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 0.05442,-0.01458
 0.05653,-0.01475
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 0.06081,-0.01509
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 0.08093,-0.01643
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 0.09037,-0.01694
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 0.10264,-0.01750
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 0.11025,-0.01777
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 0.11544,-0.01793
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 0.13996,-0.01851
 0.14280,-0.01856
 0.14568,-0.01860
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 0.15150,-0.01869
 0.15445,-0.01873
 0.15743,-0.01876
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 0.26526,-0.01862
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 1.00000, 0.00000