ファイルインデックス名　: File Index Name        : 0873        .A  
翼型整理番号　　　　　　: Airfoil Serial No.     : U01-0017-1
翼型名　　　　　　　　　: Airfoil Name           : U.S.A. 17
翼型ファイル番号　　　　: Airfoil File No.       : 0873
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, 0.00315
 0.97362, 0.00610
 0.96072, 0.00884
 0.94801, 0.01139
 0.93549, 0.01376
 0.92315, 0.01595
 0.91099, 0.01798
 0.89900, 0.01985
 0.88719, 0.02149
 0.87554, 0.02299
 0.86406, 0.02436
 0.85274, 0.02562
 0.84158, 0.02678
 0.83058, 0.02785
 0.81973, 0.02886
 0.80903, 0.02982
 0.79848, 0.03076
 0.78808, 0.03183
 0.77781, 0.03288
 0.76769, 0.03389
 0.75770, 0.03487
 0.74785, 0.03582
 0.73814, 0.03674
 0.72855, 0.03762
 0.71909, 0.03847
 0.70976, 0.03928
 0.70055, 0.04005
 0.69146, 0.04074
 0.68249, 0.04139
 0.67363, 0.04200
 0.66490, 0.04259
 0.65627, 0.04315
 0.64776, 0.04369
 0.63935, 0.04421
 0.63106, 0.04471
 0.62287, 0.04520
 0.61478, 0.04566
 0.60680, 0.04612
 0.59891, 0.04657
 0.59112, 0.04706
 0.58344, 0.04753
 0.57584, 0.04800
 0.56834, 0.04846
 0.56094, 0.04890
 0.55362, 0.04934
 0.54639, 0.04976
 0.53925, 0.05018
 0.53220, 0.05058
 0.52523, 0.05096
 0.51835, 0.05134
 0.51155, 0.05170
 0.50483, 0.05205
 0.49819, 0.05238
 0.49163, 0.05269
 0.48514, 0.05298
 0.47874, 0.05325
 0.47240, 0.05352
 0.46614, 0.05377
 0.45996, 0.05402
 0.45384, 0.05425
 0.44780, 0.05447
 0.44182, 0.05469
 0.43591, 0.05489
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 0.41859, 0.05546
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 0.38038, 0.05656
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 0.34017, 0.05748
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 0.33065, 0.05764
 0.32596, 0.05771
 0.32133, 0.05778
 0.31674, 0.05784
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 0.23800, 0.05768
 0.23426, 0.05761
 0.23056, 0.05754
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 0.22326, 0.05738
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 0.21610, 0.05720
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 0.19879, 0.05666
 0.19542, 0.05654
 0.19209, 0.05642
 0.18879, 0.05630
 0.18552, 0.05616
 0.18228, 0.05603
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 0.17590, 0.05573
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 0.16963, 0.05541
 0.16654, 0.05524
 0.16348, 0.05507
 0.16044, 0.05489
 0.15743, 0.05470
 0.15445, 0.05451
 0.15150, 0.05431
 0.14858, 0.05410
 0.14568, 0.05388
 0.14280, 0.05366
 0.13996, 0.05343
 0.13713, 0.05319
 0.13434, 0.05295
 0.13157, 0.05269
 0.12882, 0.05243
 0.12610, 0.05217
 0.12340, 0.05189
 0.12072, 0.05161
 0.11807, 0.05131
 0.11544, 0.05101
 0.11283, 0.05070
 0.11025, 0.05039
 0.10769, 0.05006
 0.10515, 0.04972
 0.10264, 0.04938
 0.10014, 0.04902
 0.09767, 0.04867
 0.09521, 0.04831
 0.09278, 0.04794
 0.09037, 0.04755
 0.08798, 0.04715
 0.08561, 0.04673
 0.08326, 0.04630
 0.08093, 0.04585
 0.07862, 0.04538
 0.07633, 0.04489
 0.07405, 0.04437
 0.07180, 0.04381
 0.06956, 0.04323
 0.06735, 0.04263
 0.06515, 0.04201
 0.06297, 0.04137
 0.06081, 0.04071
 0.05866, 0.04002
 0.05653, 0.03932
 0.05442, 0.03860
 0.05233, 0.03786
 0.05026, 0.03710
 0.04820, 0.03634
 0.04615, 0.03557
 0.04413, 0.03479
 0.04212, 0.03398
 0.04012, 0.03314
 0.03815, 0.03229
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 0.02473, 0.02532
 0.02287, 0.02408
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 0.01739, 0.02008
 0.01559, 0.01864
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 0.00680, 0.01047
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 0.00337, 0.00647
 0.00168, 0.00410
 0.00056, 0.00208
 0.00000, 0.00000
 0.00000, 0.00000
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 1.00000, 0.00000