Scholarlink

Abstract— <p>This paper describes a study of strength and stability of oval composite cylindrical shells under axial compression. The geometrically nonlinear problem for the shell is solved using the finite element method. The geometric dimensions of the shell are close to those of fuselages of modern passenger aircrafts. The other phenomena described in this paper are the effect of the cross-sectional out-of-roundness of the shell, the nonlinearity of the initial stress-strain state, and the stacking of monolayers by thickness on the critical loads and weight efficiency of composite and metal shells.</p>

错误：搜索内容不能为空，请输入英文关键词
错误：关键词超出字数限制，请精简
高级检索

Okstability of a Noncircular Composite Shell under Axial Compression and Nonlinear Deformation

  • 期刊论文

  • 发表日期：

    2025年2月1日

查看全文
  • L. P. Zheleznov

摘要

Abstract—

This paper describes a study of strength and stability of oval composite cylindrical shells under axial compression. The geometrically nonlinear problem for the shell is solved using the finite element method. The geometric dimensions of the shell are close to those of fuselages of modern passenger aircrafts. The other phenomena described in this paper are the effect of the cross-sectional out-of-roundness of the shell, the nonlinearity of the initial stress-strain state, and the stacking of monolayers by thickness on the critical loads and weight efficiency of composite and metal shells.