Divergence Instability of Reinforced Composite Circular Cylindrical Shells
Divergence instability of a simply supported orthotropic composite shell reinforced in both axial and circumferential directions is considered. The shell is subject to an axial static load and to the action of an external supersonic gas flow in the direction parallel to the shell axis. Two variants of the solution considered in the paper include discrete widely spaced stiffeners and closely spaced stiffeners; the latter case can be treated using a smeared stiffeners technique. © 1990.
V. Birman, "Divergence Instability of Reinforced Composite Circular Cylindrical Shells," International Journal of Solids and Structures, Elsevier, Jan 1990.
The definitive version is available at https://doi.org/10.1016/0020-7683(90)90030-Y
Mechanical and Aerospace Engineering
International Standard Serial Number (ISSN)
Article - Journal
© 1990 Elsevier, All rights reserved.
01 Jan 1990