ファイルインデックス名　: File Index Name        : 1018        .A  
翼型整理番号　　　　　　: Airfoil Serial No.     : N01-0018-1
翼型名　　　　　　　　　: Airfoil Name           : N.A.C.A. 0010-34 a=0.8(modified),Cli=0.2
翼型ファイル番号　　　　: Airfoil File No.       : 1018
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.   : VB6B05-A01B1


座標　　　　　　　　　　: Plot Ordinates         :

 X             Y

 0.99990, 0.00102
 0.98635, 0.00380
 0.97300, 0.00651
 0.95985, 0.00914
 0.94690, 0.01170
 0.93414, 0.01417
 0.92157, 0.01657
 0.90919, 0.01888
 0.89699, 0.02113
 0.88497, 0.02329
 0.87312, 0.02538
 0.86145, 0.02739
 0.84995, 0.02933
 0.83861, 0.03119
 0.82744, 0.03298
 0.81642, 0.03469
 0.80557, 0.03633
 0.79487, 0.03786
 0.78433, 0.03932
 0.77393, 0.04070
 0.76369, 0.04202
 0.75358, 0.04328
 0.74361, 0.04447
 0.73379, 0.04560
 0.72410, 0.04669
 0.71454, 0.04772
 0.70512, 0.04870
 0.69582, 0.04963
 0.68665, 0.05052
 0.67759, 0.05138
 0.66866, 0.05219
 0.65986, 0.05294
 0.65116, 0.05367
 0.64258, 0.05436
 0.63411, 0.05501
 0.62576, 0.05563
 0.61751, 0.05621
 0.60937, 0.05676
 0.60134, 0.05728
 0.59340, 0.05778
 0.58557, 0.05824
 0.57785, 0.05868
 0.57021, 0.05909
 0.56267, 0.05946
 0.55524, 0.05983
 0.54789, 0.06017
 0.54063, 0.06047
 0.53346, 0.06076
 0.52638, 0.06103
 0.51939, 0.06127
 0.51249, 0.06149
 0.50567, 0.06170
 0.49893, 0.06189
 0.49228, 0.06206
 0.48570, 0.06222
 0.47920, 0.06235
 0.47279, 0.06247
 0.46644, 0.06258
 0.46017, 0.06268
 0.45398, 0.06275
 0.44786, 0.06281
 0.44181, 0.06286
 0.43583, 0.06289
 0.42992, 0.06291
 0.42408, 0.06291
 0.41831, 0.06291
 0.41260, 0.06288
 0.40696, 0.06285
 0.40139, 0.06281
 0.39587, 0.06276
 0.39042, 0.06269
 0.38502, 0.06262
 0.37970, 0.06253
 0.37443, 0.06244
 0.36922, 0.06234
 0.36407, 0.06223
 0.35897, 0.06210
 0.35394, 0.06197
 0.34895, 0.06182
 0.34402, 0.06167
 0.33915, 0.06152
 0.33432, 0.06135
 0.32955, 0.06117
 0.32484, 0.06099
 0.32017, 0.06080
 0.31556, 0.06060
 0.31099, 0.06038
 0.30647, 0.06016
 0.30200, 0.05995
 0.29757, 0.05972
 0.29320, 0.05947
 0.28887, 0.05922
 0.28458, 0.05897
 0.28035, 0.05871
 0.27615, 0.05844
 0.27200, 0.05817
 0.26788, 0.05788
 0.26382, 0.05760
 0.25980, 0.05731
 0.25582, 0.05701
 0.25188, 0.05670
 0.24797, 0.05640
 0.24411, 0.05608
 0.24029, 0.05576
 0.23650, 0.05544
 0.23275, 0.05510
 0.22904, 0.05477
 0.22537, 0.05443
 0.22174, 0.05408
 0.21814, 0.05374
 0.21457, 0.05338
 0.21105, 0.05302
 0.20755, 0.05266
 0.20409, 0.05229
 0.20066, 0.05192
 0.19727, 0.05155
 0.19391, 0.05117
 0.19058, 0.05078
 0.18729, 0.05040
 0.18403, 0.05000
 0.18079, 0.04961
 0.17759, 0.04920
 0.17443, 0.04880
 0.17129, 0.04840
 0.16818, 0.04798
 0.16510, 0.04757
 0.16205, 0.04715
 0.15903, 0.04673
 0.15603, 0.04630
 0.15306, 0.04587
 0.15012, 0.04544
 0.14721, 0.04499
 0.14434, 0.04454
 0.14148, 0.04409
 0.13864, 0.04364
 0.13585, 0.04318
 0.13306, 0.04272
 0.13031, 0.04225
 0.12759, 0.04178
 0.12488, 0.04132
 0.12221, 0.04084
 0.11955, 0.04037
 0.11692, 0.03988
 0.11432, 0.03940
 0.11173, 0.03892
 0.10917, 0.03843
 0.10663, 0.03794
 0.10412, 0.03745
 0.10163, 0.03695
 0.09917, 0.03645
 0.09671, 0.03596
 0.09429, 0.03547
 0.09188, 0.03497
 0.08950, 0.03446
 0.08713, 0.03395
 0.08479, 0.03345
 0.08247, 0.03293
 0.08017, 0.03241
 0.07789, 0.03190
 0.07563, 0.03138
 0.07339, 0.03084
 0.07116, 0.03031
 0.06896, 0.02977
 0.06678, 0.02922
 0.06462, 0.02867
 0.06247, 0.02812
 0.06034, 0.02756
 0.05824, 0.02700
 0.05614, 0.02643
 0.05407, 0.02585
 0.05201, 0.02527
 0.04998, 0.02468
 0.04796, 0.02409
 0.04596, 0.02350
 0.04397, 0.02290
 0.04201, 0.02229
 0.04005, 0.02168
 0.03811, 0.02105
 0.03620, 0.02043
 0.03429, 0.01979
 0.03242, 0.01914
 0.03055, 0.01848
 0.02869, 0.01782
 0.02686, 0.01715
 0.02503, 0.01645
 0.02323, 0.01575
 0.02144, 0.01502
 0.01967, 0.01428
 0.01791, 0.01352
 0.01618, 0.01274
 0.01445, 0.01195
 0.01274, 0.01111
 0.01105, 0.01026
 0.00938, 0.00936
 0.00773, 0.00842
 0.00609, 0.00740
 0.00448, 0.00630
 0.00289, 0.00503
 0.00135, 0.00346
 0.00038, 0.00194
 0.00000, 0.00000
 0.00000, 0.00000
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 0.01647,-0.00924
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 0.03361,-0.01366
 0.03558,-0.01409
 0.03756,-0.01451
 0.03957,-0.01492
 0.04158,-0.01533
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 0.04772,-0.01651
 0.04981,-0.01690
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 0.05614,-0.01803
 0.05828,-0.01840
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 0.06263,-0.01913
 0.06483,-0.01949
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 0.08304,-0.02216
 0.08540,-0.02248
 0.08778,-0.02279
 0.09018,-0.02310
 0.09260,-0.02340
 0.09504,-0.02370
 0.09750,-0.02401
 0.09999,-0.02430
 0.10248,-0.02460
 0.10501,-0.02490
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 0.11012,-0.02549
 0.11271,-0.02578
 0.11531,-0.02608
 0.11795,-0.02636
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 0.14271,-0.02885
 0.14557,-0.02911
 0.14848,-0.02937
 0.15140,-0.02962
 0.15435,-0.02987
 0.15732,-0.03011
 0.16032,-0.03036
 0.16335,-0.03059
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 0.17261,-0.03127
 0.17575,-0.03150
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 1.00000, 0.00000