ファイルインデックス名　: File Index Name        : 1168        .A  
翼型整理番号　　　　　　: Airfoil Serial No.     : N04-0073-1
翼型名　　　　　　　　　: Airfoil Name           : N.A.C.A. 65-206
翼型ファイル番号　　　　: Airfoil File No.       : 1168
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
 0.98660, 0.00136
 0.97339, 0.00272
 0.96038, 0.00405
 0.94756, 0.00537
 0.93493, 0.00667
 0.92248, 0.00796
 0.91021, 0.00923
 0.89812, 0.01048
 0.88620, 0.01171
 0.87445, 0.01292
 0.86287, 0.01410
 0.85146, 0.01526
 0.84020, 0.01639
 0.82911, 0.01748
 0.81817, 0.01856
 0.80738, 0.01961
 0.79674, 0.02063
 0.78626, 0.02161
 0.77591, 0.02258
 0.76571, 0.02351
 0.75564, 0.02441
 0.74572, 0.02528
 0.73594, 0.02614
 0.72628, 0.02695
 0.71675, 0.02774
 0.70736, 0.02851
 0.69809, 0.02924
 0.68894, 0.02995
 0.67991, 0.03063
 0.67099, 0.03130
 0.66221, 0.03192
 0.65353, 0.03254
 0.64497, 0.03312
 0.63651, 0.03367
 0.62818, 0.03421
 0.61995, 0.03473
 0.61181, 0.03521
 0.60380, 0.03568
 0.59587, 0.03613
 0.58804, 0.03656
 0.58033, 0.03696
 0.57270, 0.03733
 0.56517, 0.03769
 0.55774, 0.03803
 0.55039, 0.03834
 0.54314, 0.03864
 0.53597, 0.03891
 0.52890, 0.03917
 0.52191, 0.03941
 0.51501, 0.03962
 0.50820, 0.03982
 0.50146, 0.03999
 0.49481, 0.04015
 0.48824, 0.04028
 0.48174, 0.04041
 0.47533, 0.04051
 0.46898, 0.04060
 0.46272, 0.04067
 0.45653, 0.04074
 0.45041, 0.04077
 0.44436, 0.04082
 0.43838, 0.04083
 0.43247, 0.04084
 0.42663, 0.04084
 0.42086, 0.04082
 0.41515, 0.04080
 0.40952, 0.04077
 0.40394, 0.04072
 0.39842, 0.04068
 0.39297, 0.04061
 0.38758, 0.04055
 0.38225, 0.04047
 0.37698, 0.04039
 0.37177, 0.04029
 0.36662, 0.04020
 0.36151, 0.04009
 0.35647, 0.03998
 0.35148, 0.03986
 0.34655, 0.03975
 0.34167, 0.03962
 0.33685, 0.03948
 0.33207, 0.03935
 0.32735, 0.03920
 0.32267, 0.03906
 0.31805, 0.03890
 0.31348, 0.03875
 0.30895, 0.03859
 0.30448, 0.03842
 0.30004, 0.03826
 0.29566, 0.03809
 0.29132, 0.03790
 0.28702, 0.03773
 0.28278, 0.03755
 0.27857, 0.03736
 0.27441, 0.03717
 0.27029, 0.03698
 0.26621, 0.03678
 0.26218, 0.03658
 0.25819, 0.03638
 0.25423, 0.03617
 0.25031, 0.03597
 0.24644, 0.03575
 0.24261, 0.03554
 0.23881, 0.03532
 0.23505, 0.03509
 0.23132, 0.03487
 0.22764, 0.03465
 0.22399, 0.03442
 0.22038, 0.03419
 0.21680, 0.03396
 0.21326, 0.03373
 0.20975, 0.03349
 0.20627, 0.03325
 0.20283, 0.03301
 0.19942, 0.03277
 0.19605, 0.03252
 0.19270, 0.03228
 0.18939, 0.03203
 0.18611, 0.03179
 0.18287, 0.03153
 0.17965, 0.03128
 0.17647, 0.03102
 0.17331, 0.03077
 0.17018, 0.03051
 0.16708, 0.03025
 0.16401, 0.03000
 0.16098, 0.02973
 0.15796, 0.02947
 0.15497, 0.02919
 0.15201, 0.02893
 0.14909, 0.02866
 0.14619, 0.02839
 0.14331, 0.02812
 0.14046, 0.02784
 0.13764, 0.02757
 0.13483, 0.02730
 0.13207, 0.02701
 0.12932, 0.02673
 0.12659, 0.02645
 0.12390, 0.02618
 0.12122, 0.02589
 0.11856, 0.02561
 0.11594, 0.02532
 0.11333, 0.02503
 0.11075, 0.02474
 0.10819, 0.02444
 0.10566, 0.02415
 0.10314, 0.02386
 0.10066, 0.02356
 0.09818, 0.02326
 0.09574, 0.02295
 0.09330, 0.02265
 0.09090, 0.02234
 0.08851, 0.02203
 0.08615, 0.02173
 0.08381, 0.02142
 0.08148, 0.02111
 0.07918, 0.02080
 0.07690, 0.02047
 0.07463, 0.02016
 0.07238, 0.01983
 0.07016, 0.01951
 0.06794, 0.01919
 0.06576, 0.01886
 0.06359, 0.01854
 0.06144, 0.01821
 0.05930, 0.01788
 0.05718, 0.01754
 0.05508, 0.01720
 0.05300, 0.01686
 0.05094, 0.01651
 0.04890, 0.01617
 0.04687, 0.01582
 0.04485, 0.01546
 0.04286, 0.01510
 0.04088, 0.01474
 0.03891, 0.01437
 0.03697, 0.01400
 0.03503, 0.01363
 0.03312, 0.01324
 0.03123, 0.01286
 0.02934, 0.01246
 0.02747, 0.01207
 0.02562, 0.01166
 0.02378, 0.01125
 0.02196, 0.01085
 0.02015, 0.01043
 0.01836, 0.00998
 0.01659, 0.00953
 0.01483, 0.00905
 0.01308, 0.00856
 0.01136, 0.00801
 0.00964, 0.00742
 0.00796, 0.00679
 0.00629, 0.00608
 0.00464, 0.00526
 0.00301, 0.00429
 0.00143, 0.00302
 0.00041, 0.00174
 0.00000, 0.00000
 0.00000, 0.00000
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 0.01075,-0.00566
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 0.01796,-0.00682
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 0.03108,-0.00825
 0.03302,-0.00844
 0.03497,-0.00862
 0.03692,-0.00879
 0.03891,-0.00898
 0.04089,-0.00914
 0.04290,-0.00931
 0.04493,-0.00949
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 0.04903,-0.00981
 0.05110,-0.00997
 0.05318,-0.01012
 0.05529,-0.01028
 0.05741,-0.01043
 0.05955,-0.01058
 0.06171,-0.01073
 0.06389,-0.01088
 0.06608,-0.01103
 0.06829,-0.01117
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 0.07276,-0.01146
 0.07503,-0.01161
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 0.08194,-0.01202
 0.08428,-0.01216
 0.08665,-0.01229
 0.08903,-0.01244
 0.09143,-0.01256
 0.09385,-0.01270
 0.09629,-0.01283
 0.09876,-0.01296
 0.10124,-0.01309
 0.10375,-0.01321
 0.10627,-0.01334
 0.10882,-0.01347
 0.11139,-0.01359
 0.11398,-0.01372
 0.11661,-0.01384
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 0.12730,-0.01430
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 0.13837,-0.01476
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 0.14406,-0.01499
 0.14695,-0.01510
 0.14986,-0.01520
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 0.15575,-0.01542
 0.15874,-0.01553
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 0.17097,-0.01595
 0.17410,-0.01605
 0.17726,-0.01616
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 0.32293,-0.01903
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 0.34178,-0.01917
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 0.36651,-0.01928
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 0.49316,-0.01813
 0.49970,-0.01798
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 0.64041,-0.01261
 0.64879,-0.01221
 0.65726,-0.01179
 0.66586,-0.01137
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 0.68337,-0.01047
 0.69230,-0.01001
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 0.93540, 0.00106
 0.94791, 0.00120
 0.96062, 0.00120
 0.97353, 0.00101
 0.98666, 0.00062
 1.00000, 0.00000