ファイルインデックス名　: File Index Name        : 0872        .A  
翼型整理番号　　　　　　: Airfoil Serial No.     : U01-0016-1
翼型名　　　　　　　　　: Airfoil Name           : U.S.A. 16
翼型ファイル番号　　　　: Airfoil File No.       : 0872
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, 0.00424
 0.97362, 0.00798
 0.96072, 0.01126
 0.94801, 0.01413
 0.93549, 0.01664
 0.92315, 0.01883
 0.91099, 0.02075
 0.89900, 0.02244
 0.88719, 0.02405
 0.87554, 0.02550
 0.86406, 0.02681
 0.85274, 0.02799
 0.84158, 0.02908
 0.83058, 0.03006
 0.81973, 0.03097
 0.80903, 0.03182
 0.79848, 0.03263
 0.78808, 0.03352
 0.77781, 0.03437
 0.76769, 0.03518
 0.75770, 0.03596
 0.74785, 0.03671
 0.73814, 0.03743
 0.72855, 0.03812
 0.71909, 0.03879
 0.70976, 0.03944
 0.70055, 0.04006
 0.69146, 0.04068
 0.68249, 0.04128
 0.67363, 0.04186
 0.66490, 0.04243
 0.65627, 0.04299
 0.64776, 0.04353
 0.63935, 0.04406
 0.63106, 0.04458
 0.62287, 0.04509
 0.61478, 0.04559
 0.60680, 0.04608
 0.59891, 0.04657
 0.59112, 0.04709
 0.58344, 0.04760
 0.57584, 0.04810
 0.56834, 0.04860
 0.56094, 0.04909
 0.55362, 0.04956
 0.54639, 0.05003
 0.53925, 0.05049
 0.53220, 0.05094
 0.52523, 0.05137
 0.51835, 0.05180
 0.51155, 0.05221
 0.50483, 0.05262
 0.49819, 0.05300
 0.49163, 0.05336
 0.48514, 0.05371
 0.47874, 0.05405
 0.47240, 0.05438
 0.46614, 0.05469
 0.45996, 0.05499
 0.45384, 0.05528
 0.44780, 0.05556
 0.44182, 0.05582
 0.43591, 0.05607
 0.43007, 0.05631
 0.42430, 0.05654
 0.41859, 0.05676
 0.41295, 0.05697
 0.40737, 0.05716
 0.40185, 0.05734
 0.39639, 0.05750
 0.39099, 0.05764
 0.38566, 0.05777
 0.38038, 0.05789
 0.37516, 0.05800
 0.37000, 0.05810
 0.36489, 0.05819
 0.35984, 0.05827
 0.35484, 0.05834
 0.34990, 0.05840
 0.34501, 0.05846
 0.34017, 0.05851
 0.33538, 0.05854
 0.33065, 0.05857
 0.32596, 0.05860
 0.32133, 0.05861
 0.31674, 0.05862
 0.31220, 0.05863
 0.30771, 0.05862
 0.30326, 0.05861
 0.29887, 0.05860
 0.29451, 0.05858
 0.29020, 0.05856
 0.28594, 0.05854
 0.28172, 0.05851
 0.27754, 0.05847
 0.27340, 0.05843
 0.26931, 0.05839
 0.26526, 0.05834
 0.26125, 0.05828
 0.25728, 0.05822
 0.25334, 0.05816
 0.24945, 0.05809
 0.24560, 0.05801
 0.24178, 0.05793
 0.23800, 0.05785
 0.23426, 0.05776
 0.23056, 0.05767
 0.22689, 0.05757
 0.22326, 0.05747
 0.21966, 0.05737
 0.21610, 0.05726
 0.21257, 0.05714
 0.20907, 0.05703
 0.20561, 0.05691
 0.20218, 0.05678
 0.19879, 0.05666
 0.19542, 0.05653
 0.19209, 0.05640
 0.18879, 0.05627
 0.18552, 0.05613
 0.18228, 0.05599
 0.17908, 0.05584
 0.17590, 0.05569
 0.17275, 0.05553
 0.16963, 0.05537
 0.16654, 0.05521
 0.16348, 0.05504
 0.16044, 0.05486
 0.15743, 0.05468
 0.15445, 0.05449
 0.15150, 0.05430
 0.14858, 0.05411
 0.14568, 0.05392
 0.14280, 0.05372
 0.13996, 0.05351
 0.13713, 0.05330
 0.13434, 0.05309
 0.13157, 0.05286
 0.12882, 0.05263
 0.12610, 0.05239
 0.12340, 0.05215
 0.12072, 0.05189
 0.11807, 0.05163
 0.11544, 0.05136
 0.11283, 0.05107
 0.11025, 0.05078
 0.10769, 0.05048
 0.10515, 0.05017
 0.10264, 0.04985
 0.10014, 0.04952
 0.09767, 0.04917
 0.09521, 0.04880
 0.09278, 0.04842
 0.09037, 0.04804
 0.08798, 0.04764
 0.08561, 0.04723
 0.08326, 0.04681
 0.08093, 0.04638
 0.07862, 0.04593
 0.07633, 0.04547
 0.07405, 0.04500
 0.07180, 0.04450
 0.06956, 0.04399
 0.06735, 0.04348
 0.06515, 0.04294
 0.06297, 0.04240
 0.06081, 0.04184
 0.05866, 0.04127
 0.05653, 0.04069
 0.05442, 0.04010
 0.05233, 0.03949
 0.05026, 0.03888
 0.04820, 0.03831
 0.04615, 0.03773
 0.04413, 0.03715
 0.04212, 0.03654
 0.04012, 0.03592
 0.03815, 0.03528
 0.03618, 0.03460
 0.03424, 0.03390
 0.03231, 0.03317
 0.03039, 0.03239
 0.02849, 0.03157
 0.02660, 0.03069
 0.02473, 0.02975
 0.02287, 0.02865
 0.02103, 0.02750
 0.01920, 0.02627
 0.01739, 0.02498
 0.01559, 0.02360
 0.01380, 0.02213
 0.01203, 0.02057
 0.01027, 0.01890
 0.00853, 0.01709
 0.00680, 0.01511
 0.00508, 0.01290
 0.00337, 0.01033
 0.00168, 0.00711
 0.00056, 0.00399
 0.00000, 0.00000
 0.00000, 0.00000
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 0.00168,-0.00105
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 0.00508,-0.00224
 0.00680,-0.00276
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 0.01027,-0.00367
 0.01203,-0.00409
 0.01380,-0.00449
 0.01559,-0.00486
 0.01739,-0.00520
 0.01920,-0.00553
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 0.02473,-0.00636
 0.02660,-0.00655
 0.02849,-0.00671
 0.03039,-0.00685
 0.03231,-0.00697
 0.03424,-0.00707
 0.03618,-0.00716
 0.03815,-0.00725
 0.04012,-0.00732
 0.04212,-0.00739
 0.04413,-0.00745
 0.04615,-0.00750
 0.04820,-0.00756
 0.05026,-0.00761
 0.05233,-0.00769
 0.05442,-0.00777
 0.05653,-0.00784
 0.05866,-0.00791
 0.06081,-0.00798
 0.06297,-0.00804
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 0.07405,-0.00829
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 0.07862,-0.00833
 0.08093,-0.00834
 0.08326,-0.00835
 0.08561,-0.00836
 0.08798,-0.00836
 0.09037,-0.00835
 0.09278,-0.00834
 0.09521,-0.00833
 0.09767,-0.00832
 0.10014,-0.00830
 0.10264,-0.00829
 0.10515,-0.00829
 0.10769,-0.00828
 0.11025,-0.00826
 0.11283,-0.00825
 0.11544,-0.00823
 0.11807,-0.00820
 0.12072,-0.00818
 0.12340,-0.00815
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 0.13434,-0.00798
 0.13713,-0.00792
 0.13996,-0.00786
 0.14280,-0.00779
 0.14568,-0.00772
 0.14858,-0.00764
 0.15150,-0.00754
 0.15445,-0.00742
 0.15743,-0.00729
 0.16044,-0.00715
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 0.16654,-0.00686
 0.16963,-0.00671
 0.17275,-0.00656
 0.17590,-0.00640
 0.17908,-0.00623
 0.18228,-0.00606
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 0.26526,-0.00186
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 0.30771,-0.00044
 0.31220,-0.00036
 0.31674,-0.00028
 0.32133,-0.00021
 0.32596,-0.00014
 0.33065,-0.00009
 0.33538,-0.00004
 0.34017, 0.00001
 0.34501, 0.00005
 0.34990, 0.00008
 0.35484, 0.00010
 0.35984, 0.00012
 0.36489, 0.00013
 0.37000, 0.00013
 0.37516, 0.00012
 0.38038, 0.00011
 0.38566, 0.00009
 0.39099, 0.00006
 0.39639, 0.00003
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 0.41859,-0.00014
 0.42430,-0.00020
 0.43007,-0.00027
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 0.48514,-0.00143
 0.49163,-0.00163
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 1.00000, 0.00000