ファイルインデックス名　: File Index Name        : 0965        .A  
翼型整理番号　　　　　　: Airfoil Serial No.     : R06-0001-1
翼型名　　　　　　　　　: Airfoil Name           : Republic R-4,40-413-.6
翼型ファイル番号　　　　: Airfoil File No.       : 0965
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

 0.99991, 0.00041
 0.98588, 0.00382
 0.97207, 0.00716
 0.95847, 0.01043
 0.94506, 0.01363
 0.93186, 0.01678
 0.91885, 0.01987
 0.90603, 0.02293
 0.89339, 0.02595
 0.88093, 0.02897
 0.86864, 0.03193
 0.85653, 0.03482
 0.84460, 0.03765
 0.83284, 0.04040
 0.82127, 0.04308
 0.80985, 0.04568
 0.79860, 0.04822
 0.78752, 0.05069
 0.77660, 0.05309
 0.76582, 0.05543
 0.75521, 0.05769
 0.74475, 0.05990
 0.73443, 0.06204
 0.72427, 0.06412
 0.71425, 0.06612
 0.70438, 0.06803
 0.69466, 0.06984
 0.68507, 0.07156
 0.67563, 0.07320
 0.66632, 0.07476
 0.65714, 0.07624
 0.64811, 0.07766
 0.63919, 0.07900
 0.63040, 0.08028
 0.62173, 0.08150
 0.61319, 0.08264
 0.60477, 0.08370
 0.59646, 0.08470
 0.58829, 0.08561
 0.58021, 0.08647
 0.57225, 0.08726
 0.56441, 0.08799
 0.55667, 0.08867
 0.54903, 0.08930
 0.54150, 0.08988
 0.53407, 0.09042
 0.52673, 0.09092
 0.51949, 0.09137
 0.51235, 0.09178
 0.50530, 0.09216
 0.49835, 0.09250
 0.49148, 0.09280
 0.48470, 0.09307
 0.47801, 0.09331
 0.47141, 0.09352
 0.46488, 0.09369
 0.45845, 0.09384
 0.45208, 0.09395
 0.44580, 0.09405
 0.43961, 0.09412
 0.43348, 0.09416
 0.42743, 0.09418
 0.42145, 0.09418
 0.41555, 0.09416
 0.40972, 0.09411
 0.40396, 0.09404
 0.39827, 0.09396
 0.39265, 0.09386
 0.38710, 0.09374
 0.38161, 0.09361
 0.37618, 0.09346
 0.37082, 0.09329
 0.36553, 0.09311
 0.36029, 0.09291
 0.35511, 0.09270
 0.35000, 0.09247
 0.34495, 0.09223
 0.33995, 0.09198
 0.33501, 0.09171
 0.33013, 0.09143
 0.32530, 0.09114
 0.32052, 0.09085
 0.31580, 0.09053
 0.31114, 0.09021
 0.30652, 0.08987
 0.30197, 0.08953
 0.29745, 0.08918
 0.29299, 0.08882
 0.28858, 0.08845
 0.28421, 0.08808
 0.27991, 0.08769
 0.27563, 0.08730
 0.27141, 0.08690
 0.26724, 0.08648
 0.26311, 0.08607
 0.25902, 0.08565
 0.25497, 0.08521
 0.25098, 0.08478
 0.24702, 0.08433
 0.24311, 0.08390
 0.23924, 0.08344
 0.23540, 0.08298
 0.23161, 0.08251
 0.22786, 0.08204
 0.22414, 0.08156
 0.22047, 0.08109
 0.21683, 0.08060
 0.21324, 0.08010
 0.20968, 0.07960
 0.20616, 0.07910
 0.20267, 0.07858
 0.19922, 0.07806
 0.19580, 0.07753
 0.19242, 0.07700
 0.18908, 0.07645
 0.18577, 0.07591
 0.18250, 0.07535
 0.17924, 0.07480
 0.17604, 0.07424
 0.17286, 0.07368
 0.16971, 0.07310
 0.16660, 0.07253
 0.16352, 0.07195
 0.16047, 0.07137
 0.15744, 0.07078
 0.15445, 0.07020
 0.15149, 0.06960
 0.14856, 0.06901
 0.14565, 0.06842
 0.14276, 0.06782
 0.13991, 0.06723
 0.13709, 0.06663
 0.13430, 0.06602
 0.13153, 0.06543
 0.12878, 0.06481
 0.12608, 0.06419
 0.12338, 0.06357
 0.12073, 0.06296
 0.11809, 0.06232
 0.11548, 0.06170
 0.11290, 0.06106
 0.11034, 0.06041
 0.10779, 0.05977
 0.10529, 0.05912
 0.10280, 0.05846
 0.10033, 0.05780
 0.09790, 0.05713
 0.09548, 0.05644
 0.09309, 0.05576
 0.09073, 0.05507
 0.08838, 0.05438
 0.08606, 0.05368
 0.08375, 0.05298
 0.08148, 0.05227
 0.07922, 0.05156
 0.07699, 0.05084
 0.07477, 0.05011
 0.07258, 0.04939
 0.07040, 0.04868
 0.06825, 0.04795
 0.06612, 0.04721
 0.06400, 0.04647
 0.06191, 0.04573
 0.05984, 0.04497
 0.05779, 0.04422
 0.05575, 0.04345
 0.05374, 0.04268
 0.05175, 0.04190
 0.04977, 0.04110
 0.04781, 0.04030
 0.04588, 0.03949
 0.04397, 0.03866
 0.04208, 0.03783
 0.04020, 0.03698
 0.03834, 0.03613
 0.03651, 0.03526
 0.03469, 0.03437
 0.03288, 0.03347
 0.03111, 0.03257
 0.02934, 0.03164
 0.02760, 0.03070
 0.02588, 0.02974
 0.02417, 0.02875
 0.02249, 0.02776
 0.02082, 0.02673
 0.01918, 0.02568
 0.01755, 0.02460
 0.01595, 0.02350
 0.01437, 0.02236
 0.01281, 0.02119
 0.01127, 0.01998
 0.00975, 0.01871
 0.00827, 0.01739
 0.00681, 0.01600
 0.00539, 0.01451
 0.00401, 0.01291
 0.00268, 0.01110
 0.00142, 0.00900
 0.00031, 0.00632
-0.00023, 0.00363
 0.00000, 0.00000
 0.00000, 0.00000
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 0.04267,-0.02089
 0.04473,-0.02130
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 0.05315,-0.02287
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 0.06620,-0.02492
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 0.09164,-0.02790
 0.09407,-0.02815
 0.09650,-0.02837
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 0.10395,-0.02905
 0.10647,-0.02927
 0.10902,-0.02949
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 0.11416,-0.02991
 0.11676,-0.03012
 0.11939,-0.03032
 0.12204,-0.03053
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 1.00000, 0.00000