ファイルインデックス名　: File Index Name        : 1020        .A00
翼型整理番号　　　　　　: Airfoil Serial No.     : N01-0020-0
翼型名　　　　　　　　　: Airfoil Name           : N.A.C.A. 1408
翼型ファイル番号　　　　: Airfoil File No.       : 1020
翼型情報　　　　　　　　: Airfoil Information    : Computed

算出前縁半径　　　　　　: Computed L.E.R.        : 0.71 %
算出前縁傾斜　　　　　　: Computed Slope of L.E. : 0.05
算出プログラム番号　　　: Computed Program No.   : ウハク-40B


座標　　　　　　　　　　: Plot Ordinates         :

 X             Y

 1.00003, 0.00084
 0.98678, 0.00251
 0.97372, 0.00413
 0.96086, 0.00569
 0.94818, 0.00721
 0.93569, 0.00868
 0.92337, 0.01010
 0.91124, 0.01148
 0.89927, 0.01281
 0.88748, 0.01411
 0.87585, 0.01537
 0.86438, 0.01659
 0.85308, 0.01777
 0.84193, 0.01892
 0.83094, 0.02003
 0.82010, 0.02112
 0.80941, 0.02217
 0.79887, 0.02318
 0.78847, 0.02417
 0.77821, 0.02513
 0.76809, 0.02607
 0.75811, 0.02697
 0.74826, 0.02785
 0.73855, 0.02871
 0.72896, 0.02953
 0.71950, 0.03034
 0.71017, 0.03112
 0.70095, 0.03188
 0.69186, 0.03261
 0.68289, 0.03333
 0.67403, 0.03402
 0.66529, 0.03469
 0.65666, 0.03534
 0.64814, 0.03598
 0.63973, 0.03659
 0.63143, 0.03718
 0.62323, 0.03776
 0.61513, 0.03832
 0.60714, 0.03886
 0.59925, 0.03938
 0.59145, 0.03989
 0.58376, 0.04038
 0.57615, 0.04085
 0.56864, 0.04131
 0.56123, 0.04175
 0.55390, 0.04218
 0.54666, 0.04260
 0.53951, 0.04299
 0.53245, 0.04338
 0.52547, 0.04375
 0.51858, 0.04411
 0.51177, 0.04445
 0.50503, 0.04478
 0.49838, 0.04510
 0.49181, 0.04541
 0.48531, 0.04570
 0.47889, 0.04598
 0.47255, 0.04625
 0.46628, 0.04651
 0.46008, 0.04676
 0.45395, 0.04699
 0.44790, 0.04722
 0.44191, 0.04743
 0.43599, 0.04763
 0.43014, 0.04783
 0.42435, 0.04801
 0.41863, 0.04818
 0.41298, 0.04834
 0.40738, 0.04850
 0.40185, 0.04864
 0.39637, 0.04877
 0.39095, 0.04890
 0.38559, 0.04901
 0.38028, 0.04911
 0.37504, 0.04920
 0.36985, 0.04928
 0.36472, 0.04935
 0.35964, 0.04941
 0.35462, 0.04946
 0.34965, 0.04950
 0.34473, 0.04953
 0.33987, 0.04955
 0.33506, 0.04957
 0.33030, 0.04957
 0.32559, 0.04957
 0.32093, 0.04956
 0.31632, 0.04953
 0.31176, 0.04950
 0.30725, 0.04947
 0.30278, 0.04942
 0.29836, 0.04937
 0.29398, 0.04931
 0.28965, 0.04924
 0.28537, 0.04916
 0.28113, 0.04908
 0.27693, 0.04899
 0.27277, 0.04890
 0.26866, 0.04879
 0.26459, 0.04868
 0.26056, 0.04856
 0.25657, 0.04844
 0.25262, 0.04831
 0.24871, 0.04818
 0.24483, 0.04803
 0.24100, 0.04788
 0.23721, 0.04773
 0.23345, 0.04757
 0.22973, 0.04740
 0.22604, 0.04723
 0.22239, 0.04705
 0.21878, 0.04687
 0.21520, 0.04668
 0.21166, 0.04649
 0.20815, 0.04629
 0.20468, 0.04609
 0.20124, 0.04588
 0.19783, 0.04566
 0.19445, 0.04544
 0.19111, 0.04522
 0.18780, 0.04499
 0.18451, 0.04475
 0.18127, 0.04451
 0.17805, 0.04427
 0.17486, 0.04402
 0.17170, 0.04376
 0.16857, 0.04351
 0.16547, 0.04324
 0.16240, 0.04297
 0.15935, 0.04270
 0.15634, 0.04243
 0.15335, 0.04214
 0.15039, 0.04186
 0.14746, 0.04157
 0.14455, 0.04127
 0.14168, 0.04098
 0.13882, 0.04067
 0.13599, 0.04036
 0.13319, 0.04005
 0.13042, 0.03974
 0.12767, 0.03941
 0.12494, 0.03909
 0.12224, 0.03876
 0.11956, 0.03843
 0.11690, 0.03809
 0.11427, 0.03774
 0.11167, 0.03740
 0.10908, 0.03705
 0.10652, 0.03669
 0.10398, 0.03633
 0.10147, 0.03596
 0.09897, 0.03559
 0.09650, 0.03522
 0.09405, 0.03484
 0.09162, 0.03445
 0.08921, 0.03406
 0.08682, 0.03367
 0.08445, 0.03327
 0.08211, 0.03287
 0.07978, 0.03246
 0.07747, 0.03204
 0.07519, 0.03162
 0.07292, 0.03120
 0.07067, 0.03076
 0.06844, 0.03033
 0.06623, 0.02988
 0.06404, 0.02943
 0.06187, 0.02898
 0.05972, 0.02851
 0.05758, 0.02804
 0.05546, 0.02756
 0.05336, 0.02708
 0.05128, 0.02658
 0.04922, 0.02608
 0.04717, 0.02557
 0.04514, 0.02505
 0.04313, 0.02452
 0.04113, 0.02398
 0.03916, 0.02343
 0.03719, 0.02287
 0.03525, 0.02229
 0.03332, 0.02171
 0.03141, 0.02110
 0.02951, 0.02049
 0.02763, 0.01985
 0.02577, 0.01920
 0.02392, 0.01852
 0.02209, 0.01783
 0.02027, 0.01711
 0.01847, 0.01636
 0.01669, 0.01558
 0.01492, 0.01476
 0.01317, 0.01389
 0.01143, 0.01298
 0.00971, 0.01200
 0.00801, 0.01094
 0.00633, 0.00977
 0.00467, 0.00845
 0.00304, 0.00688
 0.00144, 0.00486
 0.00042, 0.00281
 0.00000, 0.00000
 0.00000, 0.00000
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 0.00192,-0.00469
 0.00371,-0.00655
 0.00548,-0.00794
 0.00726,-0.00909
 0.00904,-0.01009
 0.01083,-0.01098
 0.01263,-0.01179
 0.01444,-0.01254
 0.01626,-0.01323
 0.01809,-0.01388
 0.01994,-0.01448
 0.02179,-0.01506
 0.02366,-0.01561
 0.02554,-0.01613
 0.02744,-0.01663
 0.02935,-0.01710
 0.03127,-0.01756
 0.03320,-0.01800
 0.03515,-0.01843
 0.03712,-0.01884
 0.03910,-0.01924
 0.04109,-0.01962
 0.04310,-0.01999
 0.04513,-0.02035
 0.04717,-0.02070
 0.04922,-0.02104
 0.05129,-0.02137
 0.05338,-0.02169
 0.05548,-0.02201
 0.05761,-0.02231
 0.05974,-0.02260
 0.06190,-0.02289
 0.06407,-0.02317
 0.06626,-0.02345
 0.06846,-0.02371
 0.07069,-0.02397
 0.07293,-0.02423
 0.07519,-0.02448
 0.07747,-0.02472
 0.07976,-0.02495
 0.08208,-0.02518
 0.08441,-0.02541
 0.08677,-0.02563
 0.08914,-0.02584
 0.09153,-0.02605
 0.09395,-0.02625
 0.09638,-0.02645
 0.09884,-0.02664
 0.10131,-0.02683
 0.10381,-0.02702
 0.10632,-0.02719
 0.10886,-0.02737
 0.11142,-0.02754
 0.11400,-0.02770
 0.11661,-0.02787
 0.11923,-0.02802
 0.12188,-0.02818
 0.12456,-0.02832
 0.12725,-0.02847
 0.12997,-0.02861
 0.13271,-0.02874
 0.13548,-0.02887
 0.13827,-0.02900
 0.14109,-0.02912
 0.14393,-0.02924
 0.14680,-0.02936
 0.14969,-0.02947
 0.15261,-0.02958
 0.15556,-0.02968
 0.15853,-0.02978
 0.16153,-0.02988
 0.16455,-0.02997
 0.16761,-0.03006
 0.17069,-0.03014
 0.17380,-0.03022
 0.17694,-0.03030
 0.18011,-0.03037
 0.18330,-0.03044
 0.18653,-0.03050
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 0.22412,-0.03096
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 0.24636,-0.03101
 0.25020,-0.03101
 0.25407,-0.03100
 0.25798,-0.03099
 0.26194,-0.03097
 0.26593,-0.03095
 0.26996,-0.03093
 0.27404,-0.03090
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 0.28231,-0.03083
 0.28651,-0.03079
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 0.29504,-0.03070
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 0.30817,-0.03053
 0.31264,-0.03047
 0.31716,-0.03040
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 0.33571,-0.03009
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 0.36004,-0.02961
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 0.42425,-0.02804
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 0.65589,-0.01899
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