ファイルインデックス名　: File Index Name        : 0784        .A  
翼型整理番号　　　　　　: Airfoil Serial No.     : R01-0012-1
翼型名　　　　　　　　　: Airfoil Name           : R.A.F. 12
翼型ファイル番号　　　　: Airfoil File No.       : 0784
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, 0.00528
 0.97362, 0.00975
 0.96072, 0.01351
 0.94801, 0.01666
 0.93549, 0.01929
 0.92315, 0.02149
 0.91099, 0.02334
 0.89900, 0.02496
 0.88719, 0.02678
 0.87554, 0.02850
 0.86406, 0.03013
 0.85274, 0.03166
 0.84158, 0.03310
 0.83058, 0.03446
 0.81973, 0.03574
 0.80903, 0.03694
 0.79848, 0.03806
 0.78808, 0.03912
 0.77781, 0.04012
 0.76769, 0.04104
 0.75770, 0.04190
 0.74785, 0.04270
 0.73814, 0.04343
 0.72855, 0.04410
 0.71909, 0.04471
 0.70976, 0.04527
 0.70055, 0.04577
 0.69146, 0.04612
 0.68249, 0.04640
 0.67363, 0.04665
 0.66490, 0.04687
 0.65627, 0.04705
 0.64776, 0.04722
 0.63935, 0.04736
 0.63106, 0.04750
 0.62287, 0.04762
 0.61478, 0.04775
 0.60680, 0.04788
 0.59891, 0.04804
 0.59112, 0.04836
 0.58344, 0.04869
 0.57584, 0.04903
 0.56834, 0.04937
 0.56094, 0.04972
 0.55362, 0.05007
 0.54639, 0.05042
 0.53925, 0.05077
 0.53220, 0.05112
 0.52523, 0.05147
 0.51835, 0.05181
 0.51155, 0.05214
 0.50483, 0.05247
 0.49819, 0.05277
 0.49163, 0.05303
 0.48514, 0.05327
 0.47874, 0.05351
 0.47240, 0.05374
 0.46614, 0.05396
 0.45996, 0.05417
 0.45384, 0.05437
 0.44780, 0.05456
 0.44182, 0.05475
 0.43591, 0.05493
 0.43007, 0.05510
 0.42430, 0.05526
 0.41859, 0.05542
 0.41295, 0.05557
 0.40737, 0.05572
 0.40185, 0.05585
 0.39639, 0.05599
 0.39099, 0.05611
 0.38566, 0.05623
 0.38038, 0.05634
 0.37516, 0.05644
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 0.35984, 0.05673
 0.35484, 0.05682
 0.34990, 0.05690
 0.34501, 0.05697
 0.34017, 0.05704
 0.33538, 0.05711
 0.33065, 0.05718
 0.32596, 0.05723
 0.32133, 0.05729
 0.31674, 0.05734
 0.31220, 0.05739
 0.30771, 0.05743
 0.30326, 0.05747
 0.29887, 0.05752
 0.29451, 0.05758
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 0.28594, 0.05769
 0.28172, 0.05773
 0.27754, 0.05778
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 0.26931, 0.05786
 0.26526, 0.05789
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 0.24945, 0.05798
 0.24560, 0.05799
 0.24178, 0.05799
 0.23800, 0.05799
 0.23426, 0.05798
 0.23056, 0.05797
 0.22689, 0.05795
 0.22326, 0.05792
 0.21966, 0.05789
 0.21610, 0.05786
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 0.19879, 0.05757
 0.19542, 0.05749
 0.19209, 0.05740
 0.18879, 0.05730
 0.18552, 0.05720
 0.18228, 0.05709
 0.17908, 0.05697
 0.17590, 0.05685
 0.17275, 0.05672
 0.16963, 0.05658
 0.16654, 0.05643
 0.16348, 0.05628
 0.16044, 0.05612
 0.15743, 0.05595
 0.15445, 0.05578
 0.15150, 0.05560
 0.14858, 0.05541
 0.14568, 0.05523
 0.14280, 0.05503
 0.13996, 0.05483
 0.13713, 0.05462
 0.13434, 0.05440
 0.13157, 0.05417
 0.12882, 0.05393
 0.12610, 0.05368
 0.12340, 0.05342
 0.12072, 0.05315
 0.11807, 0.05286
 0.11544, 0.05257
 0.11283, 0.05226
 0.11025, 0.05194
 0.10769, 0.05161
 0.10515, 0.05126
 0.10264, 0.05090
 0.10014, 0.05052
 0.09767, 0.05011
 0.09521, 0.04969
 0.09278, 0.04925
 0.09037, 0.04880
 0.08798, 0.04833
 0.08561, 0.04786
 0.08326, 0.04737
 0.08093, 0.04686
 0.07862, 0.04635
 0.07633, 0.04582
 0.07405, 0.04527
 0.07180, 0.04472
 0.06956, 0.04415
 0.06735, 0.04357
 0.06515, 0.04298
 0.06297, 0.04237
 0.06081, 0.04174
 0.05866, 0.04110
 0.05653, 0.04045
 0.05442, 0.03978
 0.05233, 0.03909
 0.05026, 0.03839
 0.04820, 0.03765
 0.04615, 0.03688
 0.04413, 0.03611
 0.04212, 0.03531
 0.04012, 0.03449
 0.03815, 0.03366
 0.03618, 0.03280
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 0.03231, 0.03104
 0.03039, 0.03012
 0.02849, 0.02919
 0.02660, 0.02823
 0.02473, 0.02726
 0.02287, 0.02630
 0.02103, 0.02532
 0.01920, 0.02429
 0.01739, 0.02322
 0.01559, 0.02210
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 0.00853, 0.01681
 0.00680, 0.01515
 0.00508, 0.01324
 0.00337, 0.01093
 0.00168, 0.00786
 0.00056, 0.00462
 0.00000, 0.00000
 0.00000, 0.00000
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 0.03618,-0.00759
 0.03815,-0.00779
 0.04012,-0.00799
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 0.05653,-0.00935
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 0.06081,-0.00962
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 0.08093,-0.01093
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 0.10769,-0.01250
 0.11025,-0.01258
 0.11283,-0.01266
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 0.14568,-0.01325
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 1.00000, 0.00000