Dynamic Stability of Composite-Material Circular Cylindrical Shells with Orthogonal Stiffeners
Abstract
The governing equations are formulated for general (axisymmetric or unsymmetric) vibrations of thin circular cylindrical shells of composite material and reinforced with axial (stringer) and/or circumferential (ring) stiffeners. The loading is direct axial compression fluctuating about a mean value. Attention is paid to the dynamic stability of such shells. The shells are modeled by use of three different shell theories (Donnell, Morley, and Sanders) and the stiffeners are modeled as being either discrete or smeared.
Recommended Citation
C. W. Bert et al., "Dynamic Stability of Composite-Material Circular Cylindrical Shells with Orthogonal Stiffeners," Proceedings of Engineering Mechanics, American Society of Civil Engineers (ASCE), Jan 1992.
Meeting Name
Proceedings of Engineering Mechanics (1992, College Station, TX, USA)
Department(s)
Mechanical and Aerospace Engineering
Document Type
Article - Conference proceedings
Document Version
Citation
File Type
text
Language(s)
English
Rights
© 1992 American Society of Civil Engineers (ASCE), All rights reserved.
Publication Date
01 Jan 1992
