ファイルインデックス名　: File Index Name        : 0960        .A  
翼型整理番号　　　　　　: Airfoil Serial No.     : 900-0032-1
翼型名　　　　　　　　　: Airfoil Name           : 航研 B12
翼型ファイル番号　　　　: Airfoil File No.       : 0960
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-C01G4


座標　　　　　　　　　　: Plot Ordinates         :

 X             Y

 1.00000, 0.00000
 0.98671, 0.00227
 0.97362, 0.00469
 0.96072, 0.00724
 0.94801, 0.00988
 0.93549, 0.01261
 0.92315, 0.01539
 0.91099, 0.01822
 0.89900, 0.02107
 0.88719, 0.02388
 0.87554, 0.02669
 0.86406, 0.02947
 0.85274, 0.03223
 0.84158, 0.03496
 0.83058, 0.03764
 0.81973, 0.04027
 0.80903, 0.04285
 0.79848, 0.04536
 0.78808, 0.04774
 0.77781, 0.05006
 0.76769, 0.05231
 0.75770, 0.05448
 0.74785, 0.05659
 0.73814, 0.05863
 0.72855, 0.06059
 0.71909, 0.06248
 0.70976, 0.06430
 0.70055, 0.06605
 0.69146, 0.06768
 0.68249, 0.06923
 0.67363, 0.07072
 0.66490, 0.07213
 0.65627, 0.07348
 0.64776, 0.07476
 0.63935, 0.07598
 0.63106, 0.07714
 0.62287, 0.07824
 0.61478, 0.07928
 0.60680, 0.08026
 0.59891, 0.08118
 0.59112, 0.08204
 0.58344, 0.08284
 0.57584, 0.08360
 0.56834, 0.08430
 0.56094, 0.08496
 0.55362, 0.08557
 0.54639, 0.08613
 0.53925, 0.08665
 0.53220, 0.08713
 0.52523, 0.08757
 0.51835, 0.08796
 0.51155, 0.08832
 0.50483, 0.08865
 0.49819, 0.08893
 0.49163, 0.08917
 0.48514, 0.08938
 0.47874, 0.08956
 0.47240, 0.08971
 0.46614, 0.08982
 0.45996, 0.08991
 0.45384, 0.08998
 0.44780, 0.09001
 0.44182, 0.09003
 0.43591, 0.09002
 0.43007, 0.08998
 0.42430, 0.08993
 0.41859, 0.08985
 0.41295, 0.08976
 0.40737, 0.08965
 0.40185, 0.08952
 0.39639, 0.08938
 0.39099, 0.08923
 0.38566, 0.08907
 0.38038, 0.08889
 0.37516, 0.08869
 0.37000, 0.08849
 0.36489, 0.08827
 0.35984, 0.08803
 0.35484, 0.08779
 0.34990, 0.08753
 0.34501, 0.08726
 0.34017, 0.08698
 0.33538, 0.08669
 0.33065, 0.08638
 0.32596, 0.08607
 0.32133, 0.08575
 0.31674, 0.08542
 0.31220, 0.08508
 0.30771, 0.08473
 0.30326, 0.08438
 0.29887, 0.08402
 0.29451, 0.08365
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 0.28594, 0.08289
 0.28172, 0.08250
 0.27754, 0.08210
 0.27340, 0.08170
 0.26931, 0.08129
 0.26526, 0.08087
 0.26125, 0.08045
 0.25728, 0.08002
 0.25334, 0.07959
 0.24945, 0.07915
 0.24560, 0.07870
 0.24178, 0.07825
 0.23800, 0.07779
 0.23426, 0.07733
 0.23056, 0.07687
 0.22689, 0.07640
 0.22326, 0.07592
 0.21966, 0.07544
 0.21610, 0.07495
 0.21257, 0.07446
 0.20907, 0.07396
 0.20561, 0.07346
 0.20218, 0.07296
 0.19879, 0.07245
 0.19542, 0.07193
 0.19209, 0.07141
 0.18879, 0.07089
 0.18552, 0.07037
 0.18228, 0.06983
 0.17908, 0.06930
 0.17590, 0.06876
 0.17275, 0.06822
 0.16963, 0.06767
 0.16654, 0.06711
 0.16348, 0.06656
 0.16044, 0.06600
 0.15743, 0.06543
 0.15445, 0.06486
 0.15150, 0.06429
 0.14858, 0.06371
 0.14568, 0.06312
 0.14280, 0.06253
 0.13996, 0.06194
 0.13713, 0.06134
 0.13434, 0.06074
 0.13157, 0.06014
 0.12882, 0.05953
 0.12610, 0.05891
 0.12340, 0.05829
 0.12072, 0.05767
 0.11807, 0.05704
 0.11544, 0.05640
 0.11283, 0.05576
 0.11025, 0.05512
 0.10769, 0.05447
 0.10515, 0.05382
 0.10264, 0.05316
 0.10014, 0.05250
 0.09767, 0.05183
 0.09521, 0.05115
 0.09278, 0.05047
 0.09037, 0.04978
 0.08798, 0.04909
 0.08561, 0.04839
 0.08326, 0.04769
 0.08093, 0.04698
 0.07862, 0.04627
 0.07633, 0.04554
 0.07405, 0.04481
 0.07180, 0.04408
 0.06956, 0.04334
 0.06735, 0.04259
 0.06515, 0.04184
 0.06297, 0.04108
 0.06081, 0.04031
 0.05866, 0.03953
 0.05653, 0.03874
 0.05442, 0.03794
 0.05233, 0.03714
 0.05026, 0.03632
 0.04820, 0.03549
 0.04615, 0.03465
 0.04413, 0.03380
 0.04212, 0.03293
 0.04012, 0.03205
 0.03815, 0.03116
 0.03618, 0.03026
 0.03424, 0.02934
 0.03231, 0.02840
 0.03039, 0.02744
 0.02849, 0.02647
 0.02660, 0.02547
 0.02473, 0.02445
 0.02287, 0.02340
 0.02103, 0.02233
 0.01920, 0.02123
 0.01739, 0.02009
 0.01559, 0.01890
 0.01380, 0.01767
 0.01203, 0.01638
 0.01027, 0.01502
 0.00853, 0.01357
 0.00680, 0.01199
 0.00508, 0.01025
 0.00337, 0.00823
 0.00168, 0.00570
 0.00056, 0.00323
 0.00000, 0.00000
 0.00000, 0.00000
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 0.00168,-0.00500
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 0.03039,-0.01609
 0.03231,-0.01640
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 0.03618,-0.01697
 0.03815,-0.01724
 0.04012,-0.01750
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 0.04615,-0.01821
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 0.05442,-0.01903
 0.05653,-0.01922
 0.05866,-0.01941
 0.06081,-0.01958
 0.06297,-0.01976
 0.06515,-0.01992
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 0.07862,-0.02086
 0.08093,-0.02100
 0.08326,-0.02115
 0.08561,-0.02129
 0.08798,-0.02143
 0.09037,-0.02157
 0.09278,-0.02170
 0.09521,-0.02184
 0.09767,-0.02197
 0.10014,-0.02210
 0.10264,-0.02223
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 0.10769,-0.02248
 0.11025,-0.02260
 0.11283,-0.02273
 0.11544,-0.02285
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 0.13996,-0.02392
 0.14280,-0.02403
 0.14568,-0.02415
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 0.15150,-0.02438
 0.15445,-0.02450
 0.15743,-0.02462
 0.16044,-0.02473
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 0.16654,-0.02497
 0.16963,-0.02509
 0.17275,-0.02520
 0.17590,-0.02532
 0.17908,-0.02543
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 1.00000, 0.00000