Research on the Difference between the Linear and Nonlinear Analysis of a Wing Structure

Author:

Liang Ke,Sun Qin

Publisher

Springer Netherlands

Reference10 articles.

1. An Y. (2007).Research of design optimization and stability analysis of composite shell structure. Xi'an, Northwestern Polytechnical University: 1–86 [in Chinese].

2. Barski M. (2006). Optimal design of shells against buckling subjected to combined loadings. Structural and Multidisciplinary Optimization, (31): 146–154.

3. Chen G. (2004). The foundation of aeroelastic design. Beijing: Beihang University Press, 1–200 [in Chinese].

4. Crisfield M.A. (1997). Nonlinear finite element analysis of solids and structures. Advanced topics, Vol. 2. UK, Wiley: 1–150.

5. Ling D. and Xu X. (2004). Nonlinear FEM and program. Hangzhou, Press of ZJU: 1–5 [in Chinese].

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