ファイルインデックス名　: File Index Name        : 1251        .A00
翼型整理番号　　　　　　: Airfoil Serial No.     : N01-0086-0
翼型名　　　　　　　　　: Airfoil Name           : N.A.C.A. 2309
翼型ファイル番号　　　　: Airfoil File No.       : 1251
翼型情報　　　　　　　　: Airfoil Information    : Computed

算出前縁半径　　　　　　: Computed L.E.R.        : 0.89 %
算出前縁傾斜　　　　　　: Computed Slope of L.E. : 0.133
算出プログラム番号　　　: Computed Program No.   : ウハク-40B


座標　　　　　　　　　　: Plot Ordinates         :

 X             Y

 1.00005, 0.00094
 0.98684, 0.00308
 0.97382, 0.00515
 0.96099, 0.00715
 0.94834, 0.00910
 0.93588, 0.01098
 0.92359, 0.01281
 0.91148, 0.01458
 0.89954, 0.01629
 0.88776, 0.01796
 0.87616, 0.01958
 0.86471, 0.02114
 0.85342, 0.02267
 0.84229, 0.02414
 0.83132, 0.02558
 0.82049, 0.02697
 0.80982, 0.02833
 0.79929, 0.02964
 0.78890, 0.03092
 0.77865, 0.03216
 0.76854, 0.03336
 0.75857, 0.03453
 0.74873, 0.03567
 0.73902, 0.03677
 0.72944, 0.03784
 0.71998, 0.03888
 0.71065, 0.03989
 0.70144, 0.04088
 0.69235, 0.04183
 0.68338, 0.04276
 0.67453, 0.04365
 0.66579, 0.04453
 0.65716, 0.04537
 0.64864, 0.04620
 0.64023, 0.04699
 0.63193, 0.04777
 0.62373, 0.04852
 0.61564, 0.04925
 0.60764, 0.04995
 0.59975, 0.05064
 0.59195, 0.05130
 0.58425, 0.05194
 0.57665, 0.05256
 0.56913, 0.05316
 0.56171, 0.05375
 0.55438, 0.05431
 0.54714, 0.05486
 0.53999, 0.05538
 0.53292, 0.05589
 0.52594, 0.05638
 0.51904, 0.05686
 0.51223, 0.05732
 0.50549, 0.05776
 0.49883, 0.05818
 0.49226, 0.05859
 0.48575, 0.05899
 0.47933, 0.05937
 0.47298, 0.05973
 0.46670, 0.06008
 0.46050, 0.06042
 0.45436, 0.06074
 0.44830, 0.06105
 0.44231, 0.06134
 0.43638, 0.06162
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 0.35008, 0.06451
 0.34517, 0.06460
 0.34032, 0.06469
 0.33551, 0.06476
 0.33076, 0.06482
 0.32606, 0.06487
 0.32141, 0.06492
 0.31680, 0.06495
 0.31225, 0.06498
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 0.21810, 0.06232
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 0.20380, 0.06125
 0.20031, 0.06096
 0.19686, 0.06066
 0.19344, 0.06035
 0.19005, 0.06004
 0.18669, 0.05971
 0.18337, 0.05938
 0.18008, 0.05904
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 0.17040, 0.05797
 0.16723, 0.05760
 0.16410, 0.05722
 0.16099, 0.05683
 0.15791, 0.05644
 0.15486, 0.05604
 0.15185, 0.05563
 0.14885, 0.05521
 0.14589, 0.05479
 0.14296, 0.05437
 0.14005, 0.05393
 0.13717, 0.05349
 0.13432, 0.05304
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 0.12317, 0.05119
 0.12044, 0.05071
 0.11774, 0.05022
 0.11507, 0.04973
 0.11242, 0.04924
 0.10980, 0.04873
 0.10720, 0.04822
 0.10462, 0.04771
 0.10207, 0.04719
 0.09954, 0.04666
 0.09703, 0.04612
 0.09455, 0.04558
 0.09209, 0.04504
 0.08965, 0.04449
 0.08723, 0.04393
 0.08484, 0.04336
 0.08247, 0.04279
 0.08011, 0.04222
 0.07778, 0.04163
 0.07548, 0.04104
 0.07319, 0.04044
 0.07092, 0.03984
 0.06868, 0.03923
 0.06645, 0.03861
 0.06424, 0.03799
 0.06206, 0.03735
 0.05989, 0.03671
 0.05775, 0.03606
 0.05562, 0.03541
 0.05351, 0.03474
 0.05143, 0.03407
 0.04936, 0.03339
 0.04731, 0.03269
 0.04528, 0.03199
 0.04327, 0.03128
 0.04127, 0.03056
 0.03930, 0.02982
 0.03734, 0.02907
 0.03541, 0.02831
 0.03349, 0.02754
 0.03159, 0.02675
 0.02970, 0.02594
 0.02784, 0.02512
 0.02600, 0.02428
 0.02417, 0.02342
 0.02236, 0.02253
 0.02057, 0.02162
 0.01880, 0.02068
 0.01705, 0.01971
 0.01532, 0.01871
 0.01361, 0.01766
 0.01193, 0.01656
 0.01026, 0.01541
 0.00862, 0.01418
 0.00701, 0.01287
 0.00542, 0.01143
 0.00388, 0.00982
 0.00238, 0.00795
 0.00097, 0.00556
 0.00015, 0.00318
 0.00000, 0.00000
 0.00000, 0.00000
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