ファイルインデックス名　: File Index Name        : 1085        .A00
翼型整理番号　　　　　　: Airfoil Serial No.     : N02-0013-0
翼型名　　　　　　　　　: Airfoil Name           : N.A.C.A. 43012
翼型ファイル番号　　　　: Airfoil File No.       : 1085
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. : 0.61
算出プログラム番号　　　: Computed Program No.   : ウハク-40D


座標　　　　　　　　　　: Plot Ordinates         :

 X             Y

 1.00006, 0.00126
 0.98685, 0.00369
 0.97384, 0.00606
 0.96102, 0.00837
 0.94838, 0.01062
 0.93593, 0.01280
 0.92366, 0.01494
 0.91157, 0.01702
 0.89965, 0.01905
 0.88789, 0.02103
 0.87631, 0.02296
 0.86489, 0.02485
 0.85363, 0.02669
 0.84253, 0.02849
 0.83158, 0.03024
 0.82079, 0.03196
 0.81014, 0.03364
 0.79965, 0.03527
 0.78929, 0.03688
 0.77908, 0.03844
 0.76900, 0.03997
 0.75906, 0.04147
 0.74926, 0.04293
 0.73959, 0.04436
 0.73004, 0.04576
 0.72062, 0.04713
 0.71133, 0.04847
 0.70216, 0.04978
 0.69311, 0.05106
 0.68418, 0.05231
 0.67536, 0.05353
 0.66666, 0.05473
 0.65807, 0.05590
 0.64959, 0.05704
 0.64122, 0.05816
 0.63296, 0.05926
 0.62480, 0.06033
 0.61674, 0.06137
 0.60878, 0.06239
 0.60093, 0.06339
 0.59317, 0.06437
 0.58551, 0.06532
 0.57794, 0.06626
 0.57047, 0.06717
 0.56309, 0.06806
 0.55579, 0.06893
 0.54859, 0.06977
 0.54147, 0.07060
 0.53444, 0.07141
 0.52750, 0.07220
 0.52063, 0.07297
 0.51385, 0.07372
 0.50715, 0.07445
 0.50053, 0.07517
 0.49399, 0.07586
 0.48752, 0.07654
 0.48113, 0.07720
 0.47481, 0.07785
 0.46857, 0.07847
 0.46240, 0.07908
 0.45629, 0.07968
 0.45026, 0.08025
 0.44430, 0.08082
 0.43841, 0.08136
 0.43258, 0.08189
 0.42682, 0.08241
 0.42112, 0.08291
 0.41549, 0.08340
 0.40991, 0.08387
 0.40441, 0.08432
 0.39896, 0.08477
 0.39357, 0.08519
 0.38824, 0.08561
 0.38297, 0.08601
 0.37776, 0.08640
 0.37260, 0.08677
 0.36750, 0.08714
 0.36245, 0.08748
 0.35746, 0.08782
 0.35252, 0.08814
 0.34764, 0.08846
 0.34280, 0.08875
 0.33802, 0.08904
 0.33329, 0.08932
 0.32860, 0.08958
 0.32397, 0.08983
 0.31939, 0.09007
 0.31485, 0.09030
 0.31036, 0.09052
 0.30591, 0.09073
 0.30151, 0.09093
 0.29716, 0.09111
 0.29285, 0.09129
 0.28859, 0.09145
 0.28436, 0.09161
 0.28018, 0.09175
 0.27605, 0.09189
 0.27195, 0.09201
 0.26789, 0.09213
 0.26388, 0.09223
 0.25990, 0.09233
 0.25597, 0.09241
 0.25207, 0.09249
 0.24821, 0.09256
 0.24439, 0.09262
 0.24061, 0.09267
 0.23686, 0.09271
 0.23315, 0.09274
 0.22948, 0.09276
 0.22584, 0.09277
 0.22223, 0.09278
 0.21866, 0.09278
 0.21513, 0.09277
 0.21163, 0.09275
 0.20816, 0.09272
 0.20472, 0.09268
 0.20130, 0.09264
 0.19790, 0.09258
 0.19451, 0.09252
 0.19112, 0.09245
 0.18776, 0.09236
 0.18440, 0.09226
 0.18106, 0.09215
 0.17773, 0.09203
 0.17442, 0.09188
 0.17112, 0.09172
 0.16783, 0.09155
 0.16456, 0.09135
 0.16131, 0.09114
 0.15807, 0.09090
 0.15485, 0.09065
 0.15165, 0.09037
 0.14846, 0.09008
 0.14529, 0.08976
 0.14213, 0.08942
 0.13900, 0.08905
 0.13588, 0.08866
 0.13279, 0.08825
 0.12971, 0.08781
 0.12665, 0.08735
 0.12361, 0.08686
 0.12060, 0.08635
 0.11760, 0.08581
 0.11463, 0.08524
 0.11167, 0.08465
 0.10874, 0.08404
 0.10583, 0.08339
 0.10294, 0.08272
 0.10008, 0.08202
 0.09724, 0.08129
 0.09442, 0.08054
 0.09163, 0.07976
 0.08886, 0.07895
 0.08612, 0.07812
 0.08340, 0.07725
 0.08070, 0.07636
 0.07804, 0.07545
 0.07540, 0.07450
 0.07278, 0.07353
 0.07020, 0.07253
 0.06764, 0.07150
 0.06511, 0.07045
 0.06261, 0.06936
 0.06013, 0.06825
 0.05769, 0.06712
 0.05527, 0.06595
 0.05289, 0.06476
 0.05053, 0.06355
 0.04821, 0.06230
 0.04591, 0.06103
 0.04365, 0.05973
 0.04142, 0.05840
 0.03922, 0.05705
 0.03706, 0.05567
 0.03493, 0.05426
 0.03283, 0.05283
 0.03076, 0.05136
 0.02873, 0.04987
 0.02674, 0.04835
 0.02478, 0.04680
 0.02286, 0.04522
 0.02098, 0.04361
 0.01914, 0.04197
 0.01734, 0.04029
 0.01557, 0.03858
 0.01386, 0.03683
 0.01218, 0.03504
 0.01056, 0.03322
 0.00898, 0.03134
 0.00746, 0.02942
 0.00599, 0.02744
 0.00459, 0.02540
 0.00326, 0.02329
 0.00201, 0.02108
 0.00085, 0.01877
-0.00019, 0.01632
-0.00108, 0.01367
-0.00174, 0.01072
-0.00201, 0.00717
-0.00160, 0.00391
 0.00000, 0.00000
 0.00000, 0.00000
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 0.00849,-0.00667
 0.01123,-0.00764
 0.01378,-0.00832
 0.01620,-0.00883
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 0.02080,-0.00952
 0.02302,-0.00976
 0.02519,-0.00995
 0.02732,-0.01010
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 0.03763,-0.01049
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 0.04363,-0.01057
 0.04561,-0.01059
 0.04758,-0.01060
 0.04955,-0.01061
 0.05151,-0.01062
 0.05347,-0.01063
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 0.05738,-0.01066
 0.05934,-0.01068
 0.06129,-0.01069
 0.06324,-0.01072
 0.06520,-0.01074
 0.06715,-0.01077
 0.06912,-0.01081
 0.07108,-0.01084
 0.07305,-0.01089
 0.07502,-0.01094
 0.07701,-0.01099
 0.07900,-0.01105
 0.08099,-0.01112
 0.08300,-0.01120
 0.08501,-0.01128
 0.08704,-0.01136
 0.08907,-0.01146
 0.09112,-0.01156
 0.09318,-0.01166
 0.09526,-0.01178
 0.09735,-0.01190
 0.09945,-0.01203
 0.10157,-0.01216
 0.10371,-0.01231
 0.10586,-0.01246
 0.10803,-0.01262
 0.11023,-0.01279
 0.11244,-0.01296
 0.11467,-0.01315
 0.11693,-0.01334
 0.11921,-0.01354
 0.12151,-0.01374
 0.12384,-0.01396
 0.12620,-0.01418
 0.12858,-0.01441
 0.13098,-0.01465
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 0.13838,-0.01541
 0.14091,-0.01568
 0.14347,-0.01596
 0.14607,-0.01624
 0.14870,-0.01653
 0.15136,-0.01683
 0.15406,-0.01714
 0.15680,-0.01745
 0.15957,-0.01777
 0.16239,-0.01809
 0.16524,-0.01842
 0.16814,-0.01875
 0.17108,-0.01909
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