Thermally Induced Bending and Wrinkling in Large Aspect Ratio Sandwich Panels
Abstract
The paper presents the solution of the problem of bending of a large aspect ratio simply supported sandwich panel with cross-ply facings subject to an elevated temperature or heat flux on one of the surfaces. The geometrically and physically linear problem for the central section is solved exactly in the cases where long edges are either unrestrained against or completely prevented from axial displacements. Wrinkling of the facings is also investigated, accounting for both thermal stresses as well as the effect of temperature on the properties of the facings and core. It is shown that thermally induced wrinkling may become the dominant mode of failure in a panel that does not wrinkle at the room temperature.
Recommended Citation
V. Birman, "Thermally Induced Bending and Wrinkling in Large Aspect Ratio Sandwich Panels," Composites Part A: Applied Science and Manufacturing, Elsevier, Jan 2005.
The definitive version is available at https://doi.org/10.1016/j.compositesa.2004.11.013
Department(s)
Mechanical and Aerospace Engineering
Sponsor(s)
United States. Office of Naval Research
Keywords and Phrases
Sandwich Structure
International Standard Serial Number (ISSN)
1359-835X
Document Type
Article - Journal
Document Version
Citation
File Type
text
Language(s)
English
Rights
© 2005 Elsevier, All rights reserved.
Publication Date
01 Jan 2005