ファイルインデックス名　: File Index Name        : 1210        .A00
翼型整理番号　　　　　　: Airfoil Serial No.     : N02-0023-0
翼型名　　　　　　　　　: Airfoil Name           : N.A.C.A. 33012
翼型ファイル番号　　　　: Airfoil File No.       : 1210
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. : 0.458
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
 0.98681, 0.00355
 0.97378, 0.00577
 0.96094, 0.00794
 0.94829, 0.01005
 0.93582, 0.01210
 0.92353, 0.01409
 0.91142, 0.01604
 0.89948, 0.01794
 0.88772, 0.01979
 0.87612, 0.02159
 0.86468, 0.02335
 0.85341, 0.02507
 0.84229, 0.02675
 0.83133, 0.02838
 0.82052, 0.02998
 0.80987, 0.03154
 0.79935, 0.03306
 0.78899, 0.03455
 0.77876, 0.03600
 0.76867, 0.03742
 0.75872, 0.03881
 0.74891, 0.04016
 0.73922, 0.04149
 0.72967, 0.04278
 0.72024, 0.04404
 0.71094, 0.04528
 0.70176, 0.04649
 0.69270, 0.04767
 0.68376, 0.04882
 0.67493, 0.04994
 0.66622, 0.05105
 0.65762, 0.05212
 0.64913, 0.05317
 0.64075, 0.05420
 0.63248, 0.05520
 0.62431, 0.05618
 0.61625, 0.05714
 0.60829, 0.05807
 0.60042, 0.05898
 0.59266, 0.05988
 0.58499, 0.06074
 0.57742, 0.06159
 0.56994, 0.06242
 0.56255, 0.06323
 0.55525, 0.06402
 0.54804, 0.06479
 0.54092, 0.06554
 0.53388, 0.06627
 0.52693, 0.06698
 0.52006, 0.06767
 0.51328, 0.06835
 0.50657, 0.06901
 0.49995, 0.06965
 0.49340, 0.07027
 0.48693, 0.07088
 0.48053, 0.07147
 0.47421, 0.07204
 0.46796, 0.07260
 0.46179, 0.07314
 0.45568, 0.07367
 0.44965, 0.07418
 0.44368, 0.07468
 0.43778, 0.07516
 0.43195, 0.07562
 0.42619, 0.07608
 0.42049, 0.07651
 0.41485, 0.07694
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 0.39832, 0.07813
 0.39293, 0.07849
 0.38760, 0.07885
 0.38232, 0.07919
 0.37711, 0.07952
 0.37195, 0.07984
 0.36685, 0.08015
 0.36180, 0.08044
 0.35681, 0.08072
 0.35187, 0.08099
 0.34698, 0.08125
 0.34215, 0.08149
 0.33736, 0.08173
 0.33263, 0.08195
 0.32795, 0.08216
 0.32331, 0.08236
 0.31873, 0.08255
 0.31419, 0.08273
 0.30970, 0.08290
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 0.29650, 0.08335
 0.29219, 0.08348
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 0.28370, 0.08370
 0.27952, 0.08380
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 0.26724, 0.08404
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 0.25531, 0.08419
 0.25142, 0.08423
 0.24756, 0.08425
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 0.23996, 0.08428
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 0.23250, 0.08427
 0.22883, 0.08425
 0.22519, 0.08422
 0.22159, 0.08419
 0.21802, 0.08415
 0.21449, 0.08410
 0.21099, 0.08404
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 0.20068, 0.08381
 0.19728, 0.08372
 0.19390, 0.08362
 0.19054, 0.08352
 0.18720, 0.08340
 0.18387, 0.08326
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 0.17727, 0.08296
 0.17400, 0.08279
 0.17075, 0.08261
 0.16751, 0.08241
 0.16429, 0.08220
 0.16109, 0.08197
 0.15791, 0.08172
 0.15475, 0.08146
 0.15161, 0.08118
 0.14849, 0.08088
 0.14538, 0.08057
 0.14230, 0.08024
 0.13924, 0.07988
 0.13620, 0.07951
 0.13318, 0.07912
 0.13017, 0.07871
 0.12719, 0.07828
 0.12423, 0.07783
 0.12130, 0.07736
 0.11838, 0.07687
 0.11548, 0.07636
 0.11261, 0.07583
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 0.10693, 0.07470
 0.10412, 0.07410
 0.10134, 0.07348
 0.09857, 0.07284
 0.09584, 0.07218
 0.09312, 0.07150
 0.09043, 0.07080
 0.08776, 0.07007
 0.08511, 0.06932
 0.08249, 0.06855
 0.07989, 0.06776
 0.07732, 0.06694
 0.07477, 0.06610
 0.07225, 0.06524
 0.06975, 0.06436
 0.06728, 0.06345
 0.06483, 0.06253
 0.06241, 0.06158
 0.06001, 0.06060
 0.05764, 0.05961
 0.05530, 0.05859
 0.05298, 0.05755
 0.05069, 0.05648
 0.04843, 0.05540
 0.04619, 0.05428
 0.04398, 0.05315
 0.04180, 0.05199
 0.03965, 0.05081
 0.03753, 0.04960
 0.03544, 0.04837
 0.03337, 0.04711
 0.03134, 0.04582
 0.02934, 0.04451
 0.02737, 0.04317
 0.02543, 0.04180
 0.02352, 0.04041
 0.02165, 0.03898
 0.01981, 0.03752
 0.01801, 0.03602
 0.01624, 0.03449
 0.01452, 0.03292
 0.01283, 0.03131
 0.01119, 0.02965
 0.00959, 0.02794
 0.00804, 0.02617
 0.00655, 0.02434
 0.00511, 0.02243
 0.00374, 0.02042
 0.00245, 0.01830
 0.00125, 0.01603
 0.00019, 0.01355
-0.00070, 0.01074
-0.00126, 0.00730
-0.00117, 0.00405
 0.00000, 0.00000
 0.00000, 0.00000
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 0.08920,-0.01973
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 0.11126,-0.02178
 0.11357,-0.02201
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