ファイルインデックス名　: File Index Name        : 1176        .A  
翼型整理番号　　　　　　: Airfoil Serial No.     : N04-0081-1
翼型名　　　　　　　　　: Airfoil Name           : N.A.C.A. 65-410
翼型ファイル番号　　　　: Airfoil File No.       : 1176
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-A01C


座標　　　　　　　　　　: Plot Ordinates         :

 X             Y

 1.00000, 0.00000
 0.98626, 0.00263
 0.97274, 0.00518
 0.95942, 0.00767
 0.94630, 0.01010
 0.93337, 0.01248
 0.92064, 0.01480
 0.90810, 0.01706
 0.89573, 0.01930
 0.88355, 0.02148
 0.87153, 0.02363
 0.85970, 0.02572
 0.84803, 0.02777
 0.83653, 0.02976
 0.82521, 0.03169
 0.81404, 0.03358
 0.80302, 0.03541
 0.79217, 0.03720
 0.78148, 0.03893
 0.77092, 0.04061
 0.76053, 0.04224
 0.75027, 0.04382
 0.74016, 0.04534
 0.73020, 0.04682
 0.72037, 0.04825
 0.71067, 0.04962
 0.70112, 0.05095
 0.69169, 0.05223
 0.68239, 0.05346
 0.67322, 0.05464
 0.66417, 0.05578
 0.65526, 0.05687
 0.64645, 0.05792
 0.63777, 0.05892
 0.62919, 0.05988
 0.62075, 0.06080
 0.61241, 0.06168
 0.60418, 0.06251
 0.59606, 0.06331
 0.58804, 0.06407
 0.58013, 0.06479
 0.57234, 0.06546
 0.56463, 0.06609
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 0.52047, 0.06914
 0.51344, 0.06953
 0.50650, 0.06988
 0.49965, 0.07019
 0.49288, 0.07047
 0.48620, 0.07071
 0.47960, 0.07092
 0.47308, 0.07109
 0.46666, 0.07125
 0.46030, 0.07137
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 0.44170, 0.07160
 0.43565, 0.07163
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 0.31442, 0.06803
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 0.23894, 0.06197
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 0.23140, 0.06118
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 0.22402, 0.06038
 0.22039, 0.05997
 0.21679, 0.05957
 0.21323, 0.05915
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 0.19933, 0.05746
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 0.17630, 0.05437
 0.17313, 0.05393
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 0.16384, 0.05255
 0.16080, 0.05209
 0.15778, 0.05163
 0.15480, 0.05115
 0.15184, 0.05068
 0.14891, 0.05022
 0.14602, 0.04973
 0.14315, 0.04926
 0.14031, 0.04878
 0.13749, 0.04830
 0.13469, 0.04780
 0.13194, 0.04732
 0.12919, 0.04683
 0.12648, 0.04634
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 0.11588, 0.04434
 0.11329, 0.04383
 0.11072, 0.04332
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 0.09582, 0.04023
 0.09341, 0.03970
 0.09103, 0.03917
 0.08866, 0.03864
 0.08632, 0.03810
 0.08400, 0.03756
 0.08170, 0.03702
 0.07942, 0.03647
 0.07717, 0.03593
 0.07493, 0.03538
 0.07271, 0.03483
 0.07052, 0.03427
 0.06833, 0.03371
 0.06618, 0.03314
 0.06404, 0.03258
 0.06192, 0.03200
 0.05982, 0.03143
 0.05774, 0.03085
 0.05568, 0.03027
 0.05363, 0.02968
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 0.04368, 0.02666
 0.04173, 0.02603
 0.03982, 0.02542
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 0.03417, 0.02348
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 0.00219, 0.00694
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