ファイルインデックス名　: File Index Name        : 9021        .A00
翼型整理番号　　　　　　: Airfoil Serial No.     : B09-0005-0
翼型名　　　　　　　　　: Airfoil Name           : Bw 3-0816
翼型ファイル番号　　　　: Airfoil File No.       : 9021
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
 0.98690, 0.00316
 0.97401, 0.00637
 0.96133, 0.00958
 0.94884, 0.01280
 0.93655, 0.01600
 0.92444, 0.01919
 0.91251, 0.02237
 0.90075, 0.02551
 0.88917, 0.02863
 0.87774, 0.03172
 0.86648, 0.03477
 0.85538, 0.03778
 0.84443, 0.04075
 0.83364, 0.04369
 0.82298, 0.04658
 0.81248, 0.04942
 0.80211, 0.05223
 0.79189, 0.05498
 0.78179, 0.05769
 0.77183, 0.06035
 0.76199, 0.06296
 0.75228, 0.06553
 0.74271, 0.06804
 0.73324, 0.07050
 0.72390, 0.07292
 0.71468, 0.07528
 0.70556, 0.07759
 0.69656, 0.07986
 0.68767, 0.08207
 0.67888, 0.08423
 0.67021, 0.08634
 0.66163, 0.08841
 0.65316, 0.09042
 0.64479, 0.09238
 0.63652, 0.09429
 0.62834, 0.09615
 0.62026, 0.09796
 0.61227, 0.09972
 0.60437, 0.10144
 0.59655, 0.10311
 0.58884, 0.10472
 0.58120, 0.10629
 0.57364, 0.10781
 0.56618, 0.10928
 0.55879, 0.11071
 0.55149, 0.11209
 0.54426, 0.11342
 0.53711, 0.11471
 0.53004, 0.11595
 0.52304, 0.11714
 0.51612, 0.11829
 0.50927, 0.11940
 0.50249, 0.12046
 0.49578, 0.12148
 0.48913, 0.12245
 0.48257, 0.12338
 0.47605, 0.12426
 0.46961, 0.12511
 0.46323, 0.12591
 0.45691, 0.12666
 0.45065, 0.12738
 0.44445, 0.12805
 0.43830, 0.12868
 0.43221, 0.12927
 0.42618, 0.12982
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 0.39074, 0.13215
 0.38509, 0.13237
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 0.33222, 0.13274
 0.32727, 0.13262
 0.32236, 0.13247
 0.31751, 0.13230
 0.31271, 0.13210
 0.30797, 0.13188
 0.30327, 0.13163
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 0.27177, 0.12933
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 0.23452, 0.12504
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 0.22669, 0.12390
 0.22285, 0.12331
 0.21903, 0.12271
 0.21526, 0.12209
 0.21152, 0.12146
 0.20783, 0.12081
 0.20416, 0.12015
 0.20053, 0.11948
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 0.19338, 0.11809
 0.18987, 0.11738
 0.18638, 0.11665
 0.18293, 0.11591
 0.17952, 0.11516
 0.17613, 0.11440
 0.17278, 0.11363
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 0.16619, 0.11205
 0.16294, 0.11124
 0.15971, 0.11042
 0.15653, 0.10959
 0.15337, 0.10874
 0.15024, 0.10789
 0.14714, 0.10702
 0.14407, 0.10615
 0.14104, 0.10527
 0.13803, 0.10437
 0.13505, 0.10346
 0.13210, 0.10255
 0.12918, 0.10162
 0.12628, 0.10068
 0.12342, 0.09974
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 0.11777, 0.09781
 0.11499, 0.09683
 0.11223, 0.09584
 0.10950, 0.09484
 0.10679, 0.09383
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 0.10146, 0.09178
 0.09883, 0.09075
 0.09623, 0.08970
 0.09365, 0.08864
 0.09111, 0.08757
 0.08858, 0.08648
 0.08608, 0.08539
 0.08359, 0.08429
 0.08114, 0.08318
 0.07871, 0.08205
 0.07630, 0.08092
 0.07392, 0.07977
 0.07156, 0.07861
 0.06922, 0.07744
 0.06691, 0.07626
 0.06462, 0.07507
 0.06235, 0.07386
 0.06011, 0.07264
 0.05788, 0.07141
 0.05568, 0.07016
 0.05351, 0.06890
 0.05135, 0.06763
 0.04922, 0.06634
 0.04710, 0.06504
 0.04501, 0.06371
 0.04295, 0.06238
 0.04091, 0.06103
 0.03889, 0.05966
 0.03689, 0.05827
 0.03491, 0.05686
 0.03296, 0.05543
 0.03103, 0.05398
 0.02912, 0.05250
 0.02724, 0.05101
 0.02538, 0.04948
 0.02355, 0.04794
 0.02174, 0.04636
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 0.01819, 0.04309
 0.01646, 0.04141
 0.01476, 0.03968
 0.01308, 0.03791
 0.01144, 0.03609
 0.00983, 0.03421
 0.00826, 0.03228
 0.00673, 0.03027
 0.00524, 0.02817
 0.00381, 0.02598
 0.00243, 0.02366
 0.00113, 0.02120
-0.00007, 0.01854
-0.00115, 0.01561
-0.00202, 0.01226
-0.00248, 0.00816
-0.00213, 0.00431
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 0.00000, 0.00000
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 0.04493,-0.01997
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 0.05951,-0.02201
 0.06163,-0.02224
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 0.06805,-0.02289
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 0.07240,-0.02327
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 0.08575,-0.02421
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 0.09496,-0.02468
 0.09730,-0.02478
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 0.10683,-0.02512
 0.10926,-0.02518
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 0.11417,-0.02530
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 0.12167,-0.02543
 0.12420,-0.02546
 0.12677,-0.02548
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 1.00000, 0.00000