ファイルインデックス名　: File Index Name        : 0959        .A  
翼型整理番号　　　　　　: Airfoil Serial No.     : 900-0031-1
翼型名　　　　　　　　　: Airfoil Name           : 航研 B10
翼型ファイル番号　　　　: Airfoil File No.       : 0959
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, 0.00189
 0.97362, 0.00391
 0.96072, 0.00603
 0.94801, 0.00823
 0.93549, 0.01050
 0.92315, 0.01282
 0.91099, 0.01518
 0.89900, 0.01756
 0.88719, 0.01990
 0.87554, 0.02224
 0.86406, 0.02456
 0.85274, 0.02686
 0.84158, 0.02913
 0.83058, 0.03137
 0.81973, 0.03356
 0.80903, 0.03571
 0.79848, 0.03780
 0.78808, 0.03979
 0.77781, 0.04172
 0.76769, 0.04359
 0.75770, 0.04540
 0.74785, 0.04716
 0.73814, 0.04885
 0.72855, 0.05049
 0.71909, 0.05206
 0.70976, 0.05358
 0.70055, 0.05503
 0.69146, 0.05639
 0.68249, 0.05769
 0.67363, 0.05893
 0.66490, 0.06011
 0.65627, 0.06123
 0.64776, 0.06230
 0.63935, 0.06332
 0.63106, 0.06428
 0.62287, 0.06520
 0.61478, 0.06606
 0.60680, 0.06688
 0.59891, 0.06765
 0.59112, 0.06837
 0.58344, 0.06904
 0.57584, 0.06967
 0.56834, 0.07025
 0.56094, 0.07080
 0.55362, 0.07131
 0.54639, 0.07178
 0.53925, 0.07221
 0.53220, 0.07261
 0.52523, 0.07297
 0.51835, 0.07330
 0.51155, 0.07360
 0.50483, 0.07387
 0.49819, 0.07411
 0.49163, 0.07431
 0.48514, 0.07449
 0.47874, 0.07463
 0.47240, 0.07476
 0.46614, 0.07485
 0.45996, 0.07493
 0.45384, 0.07498
 0.44780, 0.07501
 0.44182, 0.07502
 0.43591, 0.07501
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 0.38038, 0.07407
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 0.34017, 0.07248
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 0.33065, 0.07199
 0.32596, 0.07173
 0.32133, 0.07146
 0.31674, 0.07118
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 0.30771, 0.07061
 0.30326, 0.07031
 0.29887, 0.07001
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 0.28594, 0.06908
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 0.27754, 0.06842
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 0.24945, 0.06596
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 0.24178, 0.06521
 0.23800, 0.06483
 0.23426, 0.06444
 0.23056, 0.06406
 0.22689, 0.06366
 0.22326, 0.06326
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 0.21610, 0.06246
 0.21257, 0.06205
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 0.20561, 0.06121
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 0.19879, 0.06037
 0.19542, 0.05994
 0.19209, 0.05951
 0.18879, 0.05907
 0.18552, 0.05863
 0.18228, 0.05819
 0.17908, 0.05774
 0.17590, 0.05729
 0.17275, 0.05684
 0.16963, 0.05638
 0.16654, 0.05592
 0.16348, 0.05546
 0.16044, 0.05499
 0.15743, 0.05452
 0.15445, 0.05404
 0.15150, 0.05357
 0.14858, 0.05308
 0.14568, 0.05260
 0.14280, 0.05211
 0.13996, 0.05162
 0.13713, 0.05112
 0.13434, 0.05062
 0.13157, 0.05011
 0.12882, 0.04960
 0.12610, 0.04909
 0.12340, 0.04858
 0.12072, 0.04806
 0.11807, 0.04753
 0.11544, 0.04700
 0.11283, 0.04647
 0.11025, 0.04594
 0.10769, 0.04540
 0.10515, 0.04485
 0.10264, 0.04431
 0.10014, 0.04375
 0.09767, 0.04319
 0.09521, 0.04263
 0.09278, 0.04206
 0.09037, 0.04149
 0.08798, 0.04091
 0.08561, 0.04033
 0.08326, 0.03974
 0.08093, 0.03915
 0.07862, 0.03856
 0.07633, 0.03795
 0.07405, 0.03735
 0.07180, 0.03673
 0.06956, 0.03611
 0.06735, 0.03549
 0.06515, 0.03486
 0.06297, 0.03423
 0.06081, 0.03359
 0.05866, 0.03294
 0.05653, 0.03228
 0.05442, 0.03161
 0.05233, 0.03094
 0.05026, 0.03027
 0.04820, 0.02957
 0.04615, 0.02887
 0.04413, 0.02816
 0.04212, 0.02744
 0.04012, 0.02671
 0.03815, 0.02597
 0.03618, 0.02521
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 0.02473, 0.02038
 0.02287, 0.01950
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 0.01739, 0.01674
 0.01559, 0.01575
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 0.01027, 0.01251
 0.00853, 0.01130
 0.00680, 0.00999
 0.00508, 0.00854
 0.00337, 0.00685
 0.00168, 0.00475
 0.00056, 0.00269
 0.00000, 0.00000
 0.00000, 0.00000
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 1.00000, 0.00000