Abstract

Thermal deflections of symmetrically laminated plates that are continuous over many line supports are determined using the Rayleigh-Ritz method. The constitutive equations and the thermal loads are expressed in terms of four non-dimensional lamination parameters. Layups that minimize thermal deflections are determined for several types of composite plates subjected to temperature increases that vary linearly through the thickness.

Department(s)

Mechanical and Aerospace Engineering

International Standard Book Number (ISBN)

978-079181172-6

Document Type

Article - Conference proceedings

Document Version

Citation

File Type

text

Language(s)

English

Rights

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

Publication Date

01 Jan 1993

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