ファイルインデックス名　: File Index Name        : 1250        .A00
翼型整理番号　　　　　　: Airfoil Serial No.     : N01-0085-0
翼型名　　　　　　　　　: Airfoil Name           : N.A.C.A. 2306
翼型ファイル番号　　　　: Airfoil File No.       : 1250
翼型情報　　　　　　　　: Airfoil Information    : Computed

算出前縁半径　　　　　　: Computed L.E.R.        : 0.4 %
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

 1.00004, 0.00063
 0.98680, 0.00230
 0.97376, 0.00393
 0.96090, 0.00550
 0.94823, 0.00702
 0.93575, 0.00849
 0.92344, 0.00992
 0.91131, 0.01130
 0.89936, 0.01265
 0.88757, 0.01395
 0.87595, 0.01521
 0.86449, 0.01643
 0.85320, 0.01762
 0.84206, 0.01877
 0.83107, 0.01989
 0.82024, 0.02097
 0.80955, 0.02203
 0.79902, 0.02305
 0.78862, 0.02404
 0.77837, 0.02500
 0.76826, 0.02593
 0.75828, 0.02684
 0.74844, 0.02772
 0.73872, 0.02857
 0.72914, 0.02940
 0.71968, 0.03020
 0.71035, 0.03098
 0.70114, 0.03173
 0.69205, 0.03247
 0.68308, 0.03318
 0.67423, 0.03387
 0.66549, 0.03454
 0.65686, 0.03519
 0.64835, 0.03582
 0.63994, 0.03643
 0.63164, 0.03702
 0.62344, 0.03759
 0.61535, 0.03815
 0.60736, 0.03869
 0.59947, 0.03921
 0.59168, 0.03971
 0.58398, 0.04020
 0.57638, 0.04067
 0.56887, 0.04113
 0.56145, 0.04157
 0.55413, 0.04200
 0.54689, 0.04241
 0.53975, 0.04281
 0.53268, 0.04319
 0.52571, 0.04356
 0.51881, 0.04392
 0.51200, 0.04427
 0.50527, 0.04460
 0.49862, 0.04492
 0.49205, 0.04523
 0.48555, 0.04552
 0.47913, 0.04581
 0.47279, 0.04608
 0.46652, 0.04634
 0.46032, 0.04660
 0.45419, 0.04684
 0.44813, 0.04707
 0.44215, 0.04729
 0.43623, 0.04750
 0.43038, 0.04770
 0.42459, 0.04789
 0.41887, 0.04807
 0.41321, 0.04824
 0.40762, 0.04840
 0.40209, 0.04856
 0.39662, 0.04870
 0.39121, 0.04884
 0.38586, 0.04897
 0.38057, 0.04909
 0.37534, 0.04920
 0.37016, 0.04930
 0.36505, 0.04940
 0.35998, 0.04949
 0.35497, 0.04957
 0.35002, 0.04964
 0.34512, 0.04971
 0.34027, 0.04977
 0.33547, 0.04982
 0.33072, 0.04987
 0.32603, 0.04991
 0.32138, 0.04994
 0.31678, 0.04997
 0.31223, 0.04999
 0.30773, 0.05000
 0.30327, 0.05001
 0.29885, 0.05001
 0.29444, 0.05000
 0.29007, 0.04998
 0.28575, 0.04994
 0.28147, 0.04990
 0.27724, 0.04984
 0.27305, 0.04977
 0.26890, 0.04969
 0.26480, 0.04959
 0.26073, 0.04949
 0.25671, 0.04938
 0.25273, 0.04926
 0.24878, 0.04912
 0.24488, 0.04898
 0.24102, 0.04883
 0.23719, 0.04867
 0.23340, 0.04850
 0.22965, 0.04832
 0.22594, 0.04813
 0.22226, 0.04794
 0.21862, 0.04773
 0.21501, 0.04752
 0.21144, 0.04730
 0.20790, 0.04707
 0.20440, 0.04684
 0.20093, 0.04660
 0.19750, 0.04635
 0.19410, 0.04609
 0.19073, 0.04583
 0.18739, 0.04556
 0.18409, 0.04528
 0.18082, 0.04500
 0.17757, 0.04471
 0.17436, 0.04441
 0.17118, 0.04411
 0.16803, 0.04381
 0.16491, 0.04349
 0.16182, 0.04317
 0.15876, 0.04285
 0.15572, 0.04252
 0.15271, 0.04218
 0.14974, 0.04184
 0.14679, 0.04150
 0.14386, 0.04115
 0.14097, 0.04079
 0.13810, 0.04043
 0.13526, 0.04006
 0.13244, 0.03969
 0.12965, 0.03932
 0.12688, 0.03894
 0.12414, 0.03855
 0.12143, 0.03816
 0.11874, 0.03777
 0.11607, 0.03737
 0.11343, 0.03697
 0.11081, 0.03656
 0.10822, 0.03615
 0.10564, 0.03573
 0.10310, 0.03531
 0.10057, 0.03489
 0.09807, 0.03446
 0.09559, 0.03402
 0.09313, 0.03359
 0.09069, 0.03314
 0.08828, 0.03270
 0.08589, 0.03225
 0.08351, 0.03179
 0.08116, 0.03133
 0.07883, 0.03087
 0.07652, 0.03040
 0.07423, 0.02992
 0.07197, 0.02945
 0.06972, 0.02896
 0.06749, 0.02847
 0.06528, 0.02798
 0.06309, 0.02748
 0.06092, 0.02698
 0.05877, 0.02647
 0.05663, 0.02596
 0.05452, 0.02544
 0.05243, 0.02491
 0.05035, 0.02438
 0.04829, 0.02384
 0.04625, 0.02330
 0.04423, 0.02275
 0.04222, 0.02219
 0.04024, 0.02162
 0.03827, 0.02105
 0.03632, 0.02046
 0.03439, 0.01987
 0.03247, 0.01927
 0.03057, 0.01865
 0.02869, 0.01803
 0.02683, 0.01739
 0.02498, 0.01674
 0.02315, 0.01607
 0.02134, 0.01539
 0.01955, 0.01469
 0.01777, 0.01397
 0.01601, 0.01322
 0.01427, 0.01245
 0.01255, 0.01164
 0.01085, 0.01080
 0.00917, 0.00990
 0.00751, 0.00895
 0.00588, 0.00792
 0.00428, 0.00677
 0.00271, 0.00545
 0.00121, 0.00378
 0.00028, 0.00214
 0.00000, 0.00000
 0.00000, 0.00000
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 0.00215,-0.00333
 0.00403,-0.00455
 0.00588,-0.00543
 0.00771,-0.00613
 0.00954,-0.00671
 0.01138,-0.00721
 0.01321,-0.00765
 0.01506,-0.00805
 0.01691,-0.00840
 0.01877,-0.00872
 0.02064,-0.00901
 0.02252,-0.00928
 0.02441,-0.00952
 0.02631,-0.00975
 0.02822,-0.00996
 0.03015,-0.01016
 0.03209,-0.01034
 0.03404,-0.01050
 0.03600,-0.01066
 0.03798,-0.01080
 0.03997,-0.01094
 0.04198,-0.01106
 0.04400,-0.01118
 0.04603,-0.01129
 0.04808,-0.01139
 0.05014,-0.01148
 0.05222,-0.01156
 0.05431,-0.01164
 0.05642,-0.01172
 0.05855,-0.01178
 0.06069,-0.01184
 0.06285,-0.01190
 0.06502,-0.01195
 0.06721,-0.01200
 0.06942,-0.01204
 0.07164,-0.01207
 0.07388,-0.01211
 0.07614,-0.01213
 0.07842,-0.01216
 0.08071,-0.01218
 0.08303,-0.01220
 0.08536,-0.01221
 0.08771,-0.01222
 0.09008,-0.01222
 0.09246,-0.01223
 0.09487,-0.01223
 0.09730,-0.01222
 0.09975,-0.01222
 0.10221,-0.01221
 0.10470,-0.01220
 0.10721,-0.01219
 0.10974,-0.01217
 0.11229,-0.01215
 0.11486,-0.01213
 0.11745,-0.01211
 0.12007,-0.01208
 0.12271,-0.01205
 0.12537,-0.01202
 0.12805,-0.01199
 0.13075,-0.01196
 0.13348,-0.01193
 0.13624,-0.01189
 0.13901,-0.01185
 0.14181,-0.01181
 0.14464,-0.01177
 0.14749,-0.01173
 0.15037,-0.01169
 0.15327,-0.01164
 0.15619,-0.01160
 0.15915,-0.01155
 0.16213,-0.01151
 0.16513,-0.01146
 0.16817,-0.01141
 0.17123,-0.01136
 0.17432,-0.01131
 0.17743,-0.01126
 0.18058,-0.01121
 0.18375,-0.01116
 0.18696,-0.01111
 0.19019,-0.01105
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 0.21369,-0.01070
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 0.22425,-0.01055
 0.22784,-0.01051
 0.23146,-0.01046
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 0.24631,-0.01030
 0.25012,-0.01026
 0.25396,-0.01022
 0.25784,-0.01019
 0.26176,-0.01016
 0.26572,-0.01013
 0.26972,-0.01011
 0.27376,-0.01008
 0.27784,-0.01006
 0.28196,-0.01004
 0.28613,-0.01003
 0.29033,-0.01002
 0.29459,-0.01001
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 0.30769,-0.01000
 0.31217,-0.01000
 0.31670,-0.00999
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 0.41268,-0.00928
 0.41831,-0.00922
 0.42401,-0.00915
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 0.43560,-0.00900
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 0.47834,-0.00842
 0.48474,-0.00832
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 0.65568,-0.00555
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