| N.A.C.A. 13-H-12 | page.AF1305_A 内容更新日 (Content Update):2015.05.05. レイアウト更新日 (Layout Update):2024.10.08. |
![]() |
ファイルインデックス名 (File Index Name) :1305 .A : 翼型整理番号 (Airfoil Serial No.) :N06-0027-1 翼型ファイル番号 (Airfoil File No.) :1305 翼型情報 (Airfoil Information) :Original |
Xu (%) |
Yu (%) |
Xl (%) |
Yl (%) |
0
- 0.025
0.213
0.642
1.820
4.268
6.772
9.299
14.410
19.553
24.708
29.867
35.045
40.282
45.455
50.555
55.588
60.574
65.523
70.440
75.335
80.220
85.114
90.034
94.993
100.000
|
0
1.183
1.511
2.057
3.110
4.674
5.883
6.882
8.426
9.535
10.296
10.757
10.929
10.794
10.284
9.501
8.521
7.395
6.172
4.889
3.596
2.350
1.220
0.306
- 0.257
0
|
0
0.975
1.287
1.858
3.180
5.732
8.228
10.701
15.590
20.447
25.292
30.133
34.955
39.718
44.545
49.445
54.412
59.426
64.477
69.560
74.665
79.780
84.886
89.966
95.007
100.000
|
0
- 0.527
- 0.589
- 0.663
- 0.726
- 0.762
- 0.747
- 0.732
- 0.738
- 0.773
- 0.840
- 0.927
- 1.027
- 1.154
- 1.276
- 1.403
- 1.523
- 1.629
- 1.706
- 1.753
- 1.752
- 1.684
- 1.534
- 1.264
- 0.833
0
|
前縁半径 : L.E.R. : 1.040 % 前縁傾斜 : Slope of L.E. : 0.556 |
|||
引用文献 : Reference (for input) : 76 同一文献 : References (same data) : |
|||
| [Comments] |
|
|