ファイルインデックス名　: File Index Name        : 1195        .A  
翼型整理番号　　　　　　: Airfoil Serial No.     : N04-0100-1
翼型名　　　　　　　　　: Airfoil Name           : N.A.C.A. 66-209
翼型ファイル番号　　　　: Airfoil File No.       : 1195
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
 0.98656, 0.00173
 0.97332, 0.00353
 0.96026, 0.00541
 0.94739, 0.00732
 0.93471, 0.00927
 0.92220, 0.01124
 0.90988, 0.01323
 0.89772, 0.01519
 0.88575, 0.01712
 0.87394, 0.01904
 0.86230, 0.02092
 0.85082, 0.02276
 0.83951, 0.02456
 0.82836, 0.02631
 0.81737, 0.02802
 0.80653, 0.02967
 0.79585, 0.03127
 0.78532, 0.03282
 0.77492, 0.03433
 0.76468, 0.03577
 0.75457, 0.03717
 0.74461, 0.03851
 0.73479, 0.03980
 0.72510, 0.04103
 0.71554, 0.04221
 0.70611, 0.04335
 0.69681, 0.04442
 0.68763, 0.04543
 0.67858, 0.04640
 0.66965, 0.04731
 0.66084, 0.04816
 0.65215, 0.04897
 0.64358, 0.04970
 0.63511, 0.05039
 0.62676, 0.05102
 0.61852, 0.05161
 0.61039, 0.05215
 0.60237, 0.05263
 0.59444, 0.05306
 0.58662, 0.05344
 0.57891, 0.05377
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 0.56376, 0.05434
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 0.54901, 0.05479
 0.54176, 0.05500
 0.53460, 0.05518
 0.52754, 0.05534
 0.52056, 0.05547
 0.51367, 0.05559
 0.50686, 0.05569
 0.50013, 0.05578
 0.49349, 0.05585
 0.48692, 0.05590
 0.48043, 0.05594
 0.47403, 0.05597
 0.46769, 0.05598
 0.46143, 0.05598
 0.45525, 0.05596
 0.44913, 0.05594
 0.44309, 0.05590
 0.43712, 0.05585
 0.43121, 0.05579
 0.42538, 0.05572
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 0.38104, 0.05482
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 0.32153, 0.05258
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 0.31235, 0.05213
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 0.28170, 0.05041
 0.27750, 0.05015
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 0.26516, 0.04934
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 0.24542, 0.04792
 0.24159, 0.04763
 0.23780, 0.04733
 0.23404, 0.04703
 0.23033, 0.04673
 0.22665, 0.04642
 0.22301, 0.04611
 0.21940, 0.04581
 0.21583, 0.04549
 0.21230, 0.04518
 0.20879, 0.04485
 0.20532, 0.04454
 0.20189, 0.04421
 0.19848, 0.04389
 0.19512, 0.04356
 0.19178, 0.04323
 0.18848, 0.04290
 0.18521, 0.04257
 0.18196, 0.04223
 0.17875, 0.04189
 0.17558, 0.04156
 0.17243, 0.04121
 0.16931, 0.04087
 0.16622, 0.04052
 0.16316, 0.04017
 0.16013, 0.03982
 0.15712, 0.03947
 0.15414, 0.03911
 0.15119, 0.03875
 0.14827, 0.03839
 0.14538, 0.03803
 0.14251, 0.03767
 0.13966, 0.03730
 0.13685, 0.03693
 0.13405, 0.03655
 0.13129, 0.03618
 0.12855, 0.03581
 0.12584, 0.03543
 0.12315, 0.03505
 0.12048, 0.03468
 0.11783, 0.03430
 0.11522, 0.03391
 0.11262, 0.03352
 0.11004, 0.03313
 0.10749, 0.03274
 0.10497, 0.03235
 0.10246, 0.03195
 0.09998, 0.03156
 0.09752, 0.03116
 0.09508, 0.03075
 0.09265, 0.03035
 0.09026, 0.02995
 0.08788, 0.02954
 0.08553, 0.02913
 0.08319, 0.02871
 0.08088, 0.02829
 0.07858, 0.02788
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 0.07405, 0.02705
 0.07181, 0.02662
 0.06959, 0.02619
 0.06739, 0.02576
 0.06522, 0.02534
 0.06305, 0.02491
 0.06091, 0.02447
 0.05879, 0.02403
 0.05667, 0.02359
 0.05458, 0.02314
 0.05251, 0.02269
 0.05046, 0.02224
 0.04843, 0.02178
 0.04641, 0.02132
 0.04439, 0.02085
 0.04241, 0.02038
 0.04045, 0.01989
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 0.03656, 0.01892
 0.03463, 0.01843
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 0.00286, 0.00608
 0.00131, 0.00435
 0.00034, 0.00256
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