Abstract

Governing equations for the statics and dynamics of reinforced composite shells are developed based on Vlasov's semi-membrane shell theory. These equations have closed-form solutions illustrated for buckling and free vibration problems. The buckling solution converges to the known result for unstiffened isotropic shells. © 1992 by ASME.

Department(s)

Mechanical and Aerospace Engineering

International Standard Serial Number (ISSN)

1528-9036; 0021-8936

Document Type

Article - Journal

Document Version

Citation

File Type

text

Language(s)

English

Rights

© 2023 American Society of Mechanical Engineers, All rights reserved.

Publication Date

01 Jan 1992

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