ファイルインデックス名　: File Index Name        : 0785        .A  
翼型整理番号　　　　　　: Airfoil Serial No.     : R01-0013-1
翼型名　　　　　　　　　: Airfoil Name           : R.A.F. 13
翼型ファイル番号　　　　: Airfoil File No.       : 0785
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-C01G3


座標　　　　　　　　　　: Plot Ordinates         :

 X             Y

 1.00000, 0.00000
 0.98671, 0.00396
 0.97362, 0.00737
 0.96072, 0.01028
 0.94801, 0.01277
 0.93549, 0.01489
 0.92315, 0.01672
 0.91099, 0.01831
 0.89900, 0.01973
 0.88719, 0.02129
 0.87554, 0.02278
 0.86406, 0.02420
 0.85274, 0.02556
 0.84158, 0.02686
 0.83058, 0.02811
 0.81973, 0.02931
 0.80903, 0.03045
 0.79848, 0.03156
 0.78808, 0.03268
 0.77781, 0.03375
 0.76769, 0.03477
 0.75770, 0.03576
 0.74785, 0.03670
 0.73814, 0.03760
 0.72855, 0.03845
 0.71909, 0.03927
 0.70976, 0.04003
 0.70055, 0.04076
 0.69146, 0.04123
 0.68249, 0.04165
 0.67363, 0.04205
 0.66490, 0.04243
 0.65627, 0.04281
 0.64776, 0.04320
 0.63935, 0.04360
 0.63106, 0.04402
 0.62287, 0.04447
 0.61478, 0.04496
 0.60680, 0.04550
 0.59891, 0.04615
 0.59112, 0.04726
 0.58344, 0.04841
 0.57584, 0.04961
 0.56834, 0.05083
 0.56094, 0.05207
 0.55362, 0.05332
 0.54639, 0.05458
 0.53925, 0.05583
 0.53220, 0.05706
 0.52523, 0.05828
 0.51835, 0.05946
 0.51155, 0.06061
 0.50483, 0.06172
 0.49819, 0.06269
 0.49163, 0.06336
 0.48514, 0.06398
 0.47874, 0.06455
 0.47240, 0.06508
 0.46614, 0.06556
 0.45996, 0.06600
 0.45384, 0.06641
 0.44780, 0.06678
 0.44182, 0.06712
 0.43591, 0.06743
 0.43007, 0.06771
 0.42430, 0.06796
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 0.40737, 0.06858
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 0.38566, 0.06937
 0.38038, 0.06955
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 0.35984, 0.07014
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 0.34990, 0.07034
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 0.34017, 0.07049
 0.33538, 0.07055
 0.33065, 0.07059
 0.32596, 0.07061
 0.32133, 0.07062
 0.31674, 0.07062
 0.31220, 0.07061
 0.30771, 0.07058
 0.30326, 0.07054
 0.29887, 0.07048
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 0.28594, 0.07014
 0.28172, 0.07000
 0.27754, 0.06986
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 0.25334, 0.06876
 0.24945, 0.06855
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 0.23800, 0.06787
 0.23426, 0.06763
 0.23056, 0.06738
 0.22689, 0.06712
 0.22326, 0.06686
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 0.21257, 0.06605
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 0.19879, 0.06490
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 0.19209, 0.06431
 0.18879, 0.06401
 0.18552, 0.06371
 0.18228, 0.06340
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 0.17275, 0.06247
 0.16963, 0.06215
 0.16654, 0.06183
 0.16348, 0.06150
 0.16044, 0.06117
 0.15743, 0.06084
 0.15445, 0.06051
 0.15150, 0.06017
 0.14858, 0.05985
 0.14568, 0.05954
 0.14280, 0.05923
 0.13996, 0.05891
 0.13713, 0.05859
 0.13434, 0.05827
 0.13157, 0.05794
 0.12882, 0.05760
 0.12610, 0.05726
 0.12340, 0.05692
 0.12072, 0.05656
 0.11807, 0.05620
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 0.11283, 0.05546
 0.11025, 0.05507
 0.10769, 0.05468
 0.10515, 0.05427
 0.10264, 0.05385
 0.10014, 0.05342
 0.09767, 0.05298
 0.09521, 0.05252
 0.09278, 0.05205
 0.09037, 0.05157
 0.08798, 0.05107
 0.08561, 0.05056
 0.08326, 0.05003
 0.08093, 0.04949
 0.07862, 0.04893
 0.07633, 0.04835
 0.07405, 0.04773
 0.07180, 0.04708
 0.06956, 0.04640
 0.06735, 0.04571
 0.06515, 0.04500
 0.06297, 0.04427
 0.06081, 0.04353
 0.05866, 0.04277
 0.05653, 0.04200
 0.05442, 0.04121
 0.05233, 0.04041
 0.05026, 0.03960
 0.04820, 0.03882
 0.04615, 0.03803
 0.04413, 0.03724
 0.04212, 0.03643
 0.04012, 0.03560
 0.03815, 0.03477
 0.03618, 0.03391
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 0.02849, 0.03031
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 0.02473, 0.02835
 0.02287, 0.02732
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 0.01559, 0.02278
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 0.00680, 0.01530
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 0.00337, 0.01088
 0.00168, 0.00773
 0.00056, 0.00450
 0.00000, 0.00000
 0.00000, 0.00000
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 1.00000, 0.00000