ファイルインデックス名　: File Index Name        : 9018        .A00
翼型整理番号　　　　　　: Airfoil Serial No.     : B09-0002-0
翼型名　　　　　　　　　: Airfoil Name           : Bw 3-0616
翼型ファイル番号　　　　: Airfoil File No.       : 9018
翼型情報　　　　　　　　: Airfoil Information    : Computed

算出前縁半径　　　　　　: Computed L.E.R.        : 2.00 %
算出前縁傾斜　　　　　　: Computed Slope of L.E. : ?
算出プログラム番号　　　: Computed Program No.   : Bw 3/3A


座標　　　　　　　　　　: Plot Ordinates         :

 X             Y

 1.00000, 0.00000
 0.98688, 0.00303
 0.97397, 0.00610
 0.96127, 0.00917
 0.94876, 0.01225
 0.93645, 0.01532
 0.92432, 0.01838
 0.91237, 0.02141
 0.90059, 0.02442
 0.88899, 0.02741
 0.87754, 0.03037
 0.86627, 0.03329
 0.85515, 0.03618
 0.84418, 0.03903
 0.83337, 0.04184
 0.82271, 0.04461
 0.81219, 0.04734
 0.80181, 0.05003
 0.79158, 0.05268
 0.78146, 0.05528
 0.77150, 0.05784
 0.76165, 0.06035
 0.75194, 0.06282
 0.74236, 0.06524
 0.73289, 0.06761
 0.72355, 0.06994
 0.71432, 0.07222
 0.70521, 0.07445
 0.69621, 0.07664
 0.68733, 0.07878
 0.67854, 0.08087
 0.66988, 0.08292
 0.66130, 0.08492
 0.65285, 0.08687
 0.64448, 0.08877
 0.63622, 0.09063
 0.62806, 0.09244
 0.61999, 0.09421
 0.61202, 0.09593
 0.60413, 0.09761
 0.59634, 0.09924
 0.58864, 0.10082
 0.58102, 0.10236
 0.57350, 0.10386
 0.56606, 0.10531
 0.55870, 0.10672
 0.55142, 0.10809
 0.54423, 0.10942
 0.53711, 0.11070
 0.53007, 0.11194
 0.52312, 0.11314
 0.51624, 0.11429
 0.50943, 0.11541
 0.50269, 0.11649
 0.49603, 0.11752
 0.48943, 0.11852
 0.48292, 0.11948
 0.47646, 0.12040
 0.47007, 0.12128
 0.46376, 0.12212
 0.45751, 0.12293
 0.45133, 0.12370
 0.44520, 0.12443
 0.43914, 0.12513
 0.43314, 0.12579
 0.42721, 0.12641
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 0.41551, 0.12756
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 0.38729, 0.12983
 0.38181, 0.13019
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 0.35002, 0.13165
 0.34489, 0.13179
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 0.33477, 0.13197
 0.32979, 0.13202
 0.32484, 0.13203
 0.31994, 0.13202
 0.31507, 0.13197
 0.31024, 0.13189
 0.30544, 0.13179
 0.30066, 0.13165
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 0.27304, 0.13015
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 0.25579, 0.12865
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 0.23527, 0.12631
 0.23130, 0.12579
 0.22736, 0.12525
 0.22348, 0.12469
 0.21963, 0.12412
 0.21582, 0.12352
 0.21204, 0.12292
 0.20831, 0.12229
 0.20462, 0.12165
 0.20095, 0.12100
 0.19733, 0.12033
 0.19375, 0.11964
 0.19020, 0.11895
 0.18668, 0.11823
 0.18321, 0.11750
 0.17977, 0.11676
 0.17636, 0.11601
 0.17298, 0.11524
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 0.16634, 0.11367
 0.16306, 0.11287
 0.15982, 0.11205
 0.15661, 0.11122
 0.15343, 0.11038
 0.15028, 0.10952
 0.14716, 0.10866
 0.14407, 0.10778
 0.14102, 0.10689
 0.13799, 0.10599
 0.13500, 0.10508
 0.13202, 0.10416
 0.12909, 0.10322
 0.12617, 0.10228
 0.12329, 0.10132
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 0.11761, 0.09938
 0.11481, 0.09839
 0.11204, 0.09739
 0.10929, 0.09637
 0.10657, 0.09535
 0.10388, 0.09432
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 0.09857, 0.09222
 0.09596, 0.09116
 0.09337, 0.09008
 0.09081, 0.08899
 0.08827, 0.08789
 0.08576, 0.08679
 0.08326, 0.08566
 0.08079, 0.08453
 0.07835, 0.08339
 0.07594, 0.08223
 0.07355, 0.08106
 0.07118, 0.07988
 0.06883, 0.07869
 0.06651, 0.07749
 0.06421, 0.07627
 0.06193, 0.07504
 0.05968, 0.07380
 0.05745, 0.07254
 0.05525, 0.07127
 0.05306, 0.06999
 0.05090, 0.06869
 0.04876, 0.06737
 0.04664, 0.06604
 0.04455, 0.06469
 0.04248, 0.06333
 0.04043, 0.06195
 0.03842, 0.06055
 0.03641, 0.05913
 0.03443, 0.05769
 0.03248, 0.05623
 0.03055, 0.05475
 0.02863, 0.05324
 0.02676, 0.05172
 0.02489, 0.05016
 0.02306, 0.04858
 0.02125, 0.04697
 0.01947, 0.04532
 0.01771, 0.04364
 0.01598, 0.04191
 0.01429, 0.04015
 0.01262, 0.03834
 0.01098, 0.03649
 0.00938, 0.03457
 0.00782, 0.03260
 0.00630, 0.03055
 0.00482, 0.02841
 0.00341, 0.02618
 0.00205, 0.02382
 0.00077, 0.02132
-0.00041, 0.01862
-0.00145, 0.01565
-0.00228, 0.01226
-0.00267, 0.00811
-0.00224, 0.00426
 0.00000, 0.00000
 0.00000, 0.00000
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 0.04542,-0.01902
 0.04747,-0.01932
 0.04954,-0.01962
 0.05161,-0.01989
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 0.05578,-0.02040
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 0.06210,-0.02108
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 0.06636,-0.02148
 0.06851,-0.02166
 0.07068,-0.02184
 0.07286,-0.02200
 0.07504,-0.02216
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 0.08617,-0.02283
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 0.09303,-0.02314
 0.09534,-0.02324
 0.09767,-0.02332
 0.10002,-0.02340
 0.10239,-0.02347
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 0.10716,-0.02360
 0.10958,-0.02366
 0.11201,-0.02371
 0.11447,-0.02375
 0.11693,-0.02379
 0.11942,-0.02382
 0.12193,-0.02385
 0.12445,-0.02387
 0.12700,-0.02389
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 1.00000, 0.00000