ファイルインデックス名　: File Index Name        : 1284        .A00
翼型整理番号　　　　　　: Airfoil Serial No.     : N02-0029-0
翼型名　　　　　　　　　: Airfoil Name           : N.A.C.A. 42012
翼型ファイル番号　　　　: Airfoil File No.       : 1284
翼型情報　　　　　　　　: Airfoil Information    : Computed

算出前縁半径　　　　　　: Computed L.E.R.        : 1.59 %
算出前縁傾斜　　　　　　: Computed Slope of L.E. : 0.785
算出プログラム番号　　　: Computed Program No.   : ウハク-40D


座標　　　　　　　　　　: Plot Ordinates         :

 X             Y

 1.00004, 0.00126
 0.98682, 0.00356
 0.97379, 0.00581
 0.96095, 0.00799
 0.94830, 0.01011
 0.93583, 0.01218
 0.92355, 0.01419
 0.91144, 0.01616
 0.89950, 0.01807
 0.88774, 0.01994
 0.87614, 0.02176
 0.86471, 0.02353
 0.85344, 0.02526
 0.84232, 0.02695
 0.83136, 0.02860
 0.82056, 0.03021
 0.80990, 0.03179
 0.79939, 0.03332
 0.78902, 0.03482
 0.77880, 0.03629
 0.76871, 0.03772
 0.75876, 0.03912
 0.74895, 0.04049
 0.73927, 0.04183
 0.72971, 0.04313
 0.72029, 0.04441
 0.71098, 0.04566
 0.70180, 0.04688
 0.69275, 0.04807
 0.68381, 0.04923
 0.67498, 0.05037
 0.66627, 0.05148
 0.65767, 0.05257
 0.64919, 0.05363
 0.64081, 0.05467
 0.63254, 0.05568
 0.62437, 0.05667
 0.61631, 0.05764
 0.60835, 0.05858
 0.60048, 0.05951
 0.59272, 0.06041
 0.58505, 0.06129
 0.57748, 0.06215
 0.57000, 0.06298
 0.56261, 0.06380
 0.55531, 0.06460
 0.54811, 0.06538
 0.54099, 0.06614
 0.53395, 0.06688
 0.52700, 0.06760
 0.52013, 0.06830
 0.51335, 0.06898
 0.50664, 0.06965
 0.50002, 0.07030
 0.49347, 0.07093
 0.48700, 0.07155
 0.48060, 0.07215
 0.47428, 0.07273
 0.46803, 0.07330
 0.46186, 0.07385
 0.45575, 0.07438
 0.44972, 0.07490
 0.44376, 0.07540
 0.43786, 0.07589
 0.43203, 0.07637
 0.42626, 0.07683
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 0.39839, 0.07891
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 0.38767, 0.07965
 0.38240, 0.08000
 0.37718, 0.08034
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 0.36188, 0.08127
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 0.35194, 0.08184
 0.34706, 0.08210
 0.34222, 0.08235
 0.33744, 0.08259
 0.33271, 0.08282
 0.32802, 0.08304
 0.32339, 0.08325
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 0.31427, 0.08363
 0.30977, 0.08381
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 0.27960, 0.08474
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 0.24764, 0.08524
 0.24382, 0.08526
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 0.22891, 0.08526
 0.22527, 0.08524
 0.22167, 0.08521
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 0.21106, 0.08507
 0.20760, 0.08501
 0.20416, 0.08494
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 0.19739, 0.08477
 0.19405, 0.08468
 0.19074, 0.08458
 0.18747, 0.08447
 0.18422, 0.08436
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 0.17782, 0.08410
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 0.17153, 0.08382
 0.16843, 0.08366
 0.16536, 0.08350
 0.16231, 0.08333
 0.15930, 0.08316
 0.15631, 0.08298
 0.15335, 0.08279
 0.15041, 0.08259
 0.14750, 0.08239
 0.14462, 0.08218
 0.14176, 0.08196
 0.13893, 0.08173
 0.13612, 0.08150
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 0.12511, 0.08050
 0.12237, 0.08023
 0.11962, 0.07995
 0.11685, 0.07966
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 0.11130, 0.07903
 0.10851, 0.07869
 0.10572, 0.07833
 0.10293, 0.07795
 0.10014, 0.07754
 0.09734, 0.07711
 0.09455, 0.07665
 0.09176, 0.07616
 0.08897, 0.07564
 0.08619, 0.07509
 0.08341, 0.07450
 0.08064, 0.07388
 0.07789, 0.07323
 0.07514, 0.07254
 0.07241, 0.07180
 0.06969, 0.07103
 0.06699, 0.07022
 0.06431, 0.06936
 0.06164, 0.06847
 0.05900, 0.06753
 0.05638, 0.06654
 0.05379, 0.06551
 0.05122, 0.06444
 0.04867, 0.06332
 0.04616, 0.06215
 0.04368, 0.06094
 0.04123, 0.05968
 0.03882, 0.05838
 0.03644, 0.05703
 0.03410, 0.05563
 0.03180, 0.05418
 0.02954, 0.05269
 0.02733, 0.05115
 0.02516, 0.04956
 0.02304, 0.04793
 0.02096, 0.04624
 0.01894, 0.04451
 0.01696, 0.04273
 0.01505, 0.04090
 0.01319, 0.03902
 0.01138, 0.03709
 0.00965, 0.03510
 0.00797, 0.03306
 0.00637, 0.03095
 0.00484, 0.02879
 0.00340, 0.02655
 0.00205, 0.02423
 0.00080, 0.02182
-0.00033, 0.01930
-0.00132, 0.01665
-0.00212, 0.01381
-0.00264, 0.01068
-0.00267, 0.00700
-0.00200, 0.00373
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 0.08397,-0.01309
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 0.10920,-0.01789
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