ファイルインデックス名　: File Index Name        : 0004-2      .A  
翼型整理番号　　　　　　: Airfoil Serial No.     : R01-0028-2
翼型名　　　　　　　　　: Airfoil Name           : R.A.F. 28
翼型ファイル番号　　　　: Airfoil File No.       : 0004
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-C01G2


座標　　　　　　　　　　: Plot Ordinates         :

 X             Y

 1.00000, 0.00000
 0.98671, 0.00256
 0.97362, 0.00493
 0.96072, 0.00715
 0.94801, 0.00922
 0.93549, 0.01116
 0.92315, 0.01301
 0.91099, 0.01476
 0.89900, 0.01645
 0.88719, 0.01815
 0.87554, 0.01982
 0.86406, 0.02146
 0.85274, 0.02305
 0.84158, 0.02461
 0.83058, 0.02613
 0.81973, 0.02762
 0.80903, 0.02908
 0.79848, 0.03051
 0.78808, 0.03191
 0.77781, 0.03329
 0.76769, 0.03463
 0.75770, 0.03594
 0.74785, 0.03722
 0.73814, 0.03847
 0.72855, 0.03968
 0.71909, 0.04086
 0.70976, 0.04201
 0.70055, 0.04313
 0.69146, 0.04421
 0.68249, 0.04525
 0.67363, 0.04626
 0.66490, 0.04724
 0.65627, 0.04819
 0.64776, 0.04911
 0.63935, 0.05001
 0.63106, 0.05088
 0.62287, 0.05172
 0.61478, 0.05254
 0.60680, 0.05334
 0.59891, 0.05411
 0.59112, 0.05487
 0.58344, 0.05560
 0.57584, 0.05631
 0.56834, 0.05700
 0.56094, 0.05766
 0.55362, 0.05830
 0.54639, 0.05892
 0.53925, 0.05952
 0.53220, 0.06009
 0.52523, 0.06064
 0.51835, 0.06117
 0.51155, 0.06168
 0.50483, 0.06216
 0.49819, 0.06262
 0.49163, 0.06305
 0.48514, 0.06346
 0.47874, 0.06385
 0.47240, 0.06421
 0.46614, 0.06456
 0.45996, 0.06489
 0.45384, 0.06519
 0.44780, 0.06548
 0.44182, 0.06575
 0.43591, 0.06601
 0.43007, 0.06624
 0.42430, 0.06646
 0.41859, 0.06666
 0.41295, 0.06684
 0.40737, 0.06700
 0.40185, 0.06715
 0.39639, 0.06729
 0.39099, 0.06740
 0.38566, 0.06750
 0.38038, 0.06759
 0.37516, 0.06766
 0.37000, 0.06772
 0.36489, 0.06776
 0.35984, 0.06778
 0.35484, 0.06780
 0.34990, 0.06780
 0.34501, 0.06779
 0.34017, 0.06776
 0.33538, 0.06772
 0.33065, 0.06767
 0.32596, 0.06760
 0.32133, 0.06753
 0.31674, 0.06744
 0.31220, 0.06734
 0.30771, 0.06722
 0.30326, 0.06710
 0.29887, 0.06696
 0.29451, 0.06680
 0.29020, 0.06663
 0.28594, 0.06644
 0.28172, 0.06625
 0.27754, 0.06605
 0.27340, 0.06583
 0.26931, 0.06561
 0.26526, 0.06538
 0.26125, 0.06514
 0.25728, 0.06489
 0.25334, 0.06463
 0.24945, 0.06436
 0.24560, 0.06409
 0.24178, 0.06381
 0.23800, 0.06352
 0.23426, 0.06322
 0.23056, 0.06291
 0.22689, 0.06260
 0.22326, 0.06228
 0.21966, 0.06196
 0.21610, 0.06162
 0.21257, 0.06129
 0.20907, 0.06094
 0.20561, 0.06059
 0.20218, 0.06023
 0.19879, 0.05987
 0.19542, 0.05950
 0.19209, 0.05913
 0.18879, 0.05876
 0.18552, 0.05837
 0.18228, 0.05798
 0.17908, 0.05759
 0.17590, 0.05719
 0.17275, 0.05679
 0.16963, 0.05638
 0.16654, 0.05597
 0.16348, 0.05555
 0.16044, 0.05513
 0.15743, 0.05470
 0.15445, 0.05426
 0.15150, 0.05383
 0.14858, 0.05338
 0.14568, 0.05293
 0.14280, 0.05247
 0.13996, 0.05201
 0.13713, 0.05154
 0.13434, 0.05107
 0.13157, 0.05060
 0.12882, 0.05012
 0.12610, 0.04964
 0.12340, 0.04915
 0.12072, 0.04866
 0.11807, 0.04817
 0.11544, 0.04768
 0.11283, 0.04718
 0.11025, 0.04667
 0.10769, 0.04617
 0.10515, 0.04566
 0.10264, 0.04515
 0.10014, 0.04463
 0.09767, 0.04413
 0.09521, 0.04362
 0.09278, 0.04311
 0.09037, 0.04260
 0.08798, 0.04208
 0.08561, 0.04155
 0.08326, 0.04101
 0.08093, 0.04046
 0.07862, 0.03990
 0.07633, 0.03934
 0.07405, 0.03875
 0.07180, 0.03814
 0.06956, 0.03751
 0.06735, 0.03688
 0.06515, 0.03623
 0.06297, 0.03558
 0.06081, 0.03491
 0.05866, 0.03422
 0.05653, 0.03353
 0.05442, 0.03283
 0.05233, 0.03212
 0.05026, 0.03139
 0.04820, 0.03065
 0.04615, 0.02990
 0.04413, 0.02914
 0.04212, 0.02836
 0.04012, 0.02758
 0.03815, 0.02678
 0.03618, 0.02597
 0.03424, 0.02515
 0.03231, 0.02432
 0.03039, 0.02348
 0.02849, 0.02262
 0.02660, 0.02175
 0.02473, 0.02088
 0.02287, 0.02000
 0.02103, 0.01911
 0.01920, 0.01820
 0.01739, 0.01726
 0.01559, 0.01629
 0.01380, 0.01527
 0.01203, 0.01421
 0.01027, 0.01309
 0.00853, 0.01189
 0.00680, 0.01058
 0.00508, 0.00911
 0.00337, 0.00740
 0.00168, 0.00520
 0.00056, 0.00299
 0.00000, 0.00000
 0.00000, 0.00000
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 0.00168,-0.00518
 0.00337,-0.00712
 0.00508,-0.00854
 0.00680,-0.00969
 0.00853,-0.01067
 0.01027,-0.01153
 0.01203,-0.01231
 0.01380,-0.01301
 0.01559,-0.01367
 0.01739,-0.01428
 0.01920,-0.01486
 0.02103,-0.01541
 0.02287,-0.01593
 0.02473,-0.01643
 0.02660,-0.01694
 0.02849,-0.01743
 0.03039,-0.01792
 0.03231,-0.01839
 0.03424,-0.01884
 0.03618,-0.01928
 0.03815,-0.01971
 0.04012,-0.02013
 0.04212,-0.02054
 0.04413,-0.02093
 0.04615,-0.02131
 0.04820,-0.02169
 0.05026,-0.02204
 0.05233,-0.02237
 0.05442,-0.02270
 0.05653,-0.02301
 0.05866,-0.02331
 0.06081,-0.02361
 0.06297,-0.02389
 0.06515,-0.02417
 0.06735,-0.02444
 0.06956,-0.02470
 0.07180,-0.02495
 0.07405,-0.02520
 0.07633,-0.02544
 0.07862,-0.02567
 0.08093,-0.02589
 0.08326,-0.02611
 0.08561,-0.02633
 0.08798,-0.02654
 0.09037,-0.02674
 0.09278,-0.02694
 0.09521,-0.02713
 0.09767,-0.02732
 0.10014,-0.02751
 0.10264,-0.02770
 0.10515,-0.02789
 0.10769,-0.02807
 0.11025,-0.02825
 0.11283,-0.02843
 0.11544,-0.02861
 0.11807,-0.02878
 0.12072,-0.02895
 0.12340,-0.02911
 0.12610,-0.02927
 0.12882,-0.02943
 0.13157,-0.02959
 0.13434,-0.02974
 0.13713,-0.02988
 0.13996,-0.03003
 0.14280,-0.03017
 0.14568,-0.03030
 0.14858,-0.03044
 0.15150,-0.03057
 0.15445,-0.03069
 0.15743,-0.03081
 0.16044,-0.03093
 0.16348,-0.03104
 0.16654,-0.03115
 0.16963,-0.03125
 0.17275,-0.03135
 0.17590,-0.03145
 0.17908,-0.03154
 0.18228,-0.03162
 0.18552,-0.03171
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 0.24945,-0.03201
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 0.26526,-0.03183
 0.26931,-0.03177
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 0.31220,-0.03096
 0.31674,-0.03086
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 0.33538,-0.03043
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 0.42430,-0.02779
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 0.49163,-0.02532
 0.49819,-0.02507
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 0.64776,-0.01867
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 0.68249,-0.01690
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 1.00000, 0.00000