Journal of Materials and Engineering Structures
Volume 1, Numéro 2, Pages 73-88
2014-09-01
Authors : Boun-jad Mohamed . Zebbiche Toufik . Allali Abderrazak .
The presented work is to develop a numerical computation program to determine the distribution of the shear stress in closed tubes with asymmetric single thin wall section with a constant thickness and applications to airfoils, and therefore determining the position and value of the maximum stress. In the literature, there are exact analytical solutions only for some sections of simple geometries such as circular section. Hence our interest is focused on the search of approximate numerical solutions for more complex sections used in aeronautics. In the second stage the position of the shear center is determined so that the section does not undergo torsion. The analytic function of the airfoil boundary is obtained by using the cubic spline interpolation since it is given in the form of tabulated points.
Thin Wall; Shear center; Shear stress; Airfoil section
Le Luu Xuan
.
To Lam Giang
.
Nguyen Nghia Trong
.
Khatir Samir
.
Tiachacht Samir
.
Le Cuong Thanh
.
pages 21-30.
Bui-tien Thanh
.
Tien Nguyen-duy
.
Pham Phe Van
.
pages 571-578.
Boumaaza Messaouda
.
Bezazi Abderrezak
.
Bouchelaghem Hafida
.
Benzannache Naziha
.
Amziane Sofiane
.
Scarpa Fabrizio
.
pages 84-92.
محمد بلهادف
.
مصطفى بوزازوة
.
ص 199-226.
Zebbiche Toufik
.
Boun-jad Mohamed
.
Allali Abderrazak
.
pages 89-98.