Buckling and post-buckling of composite plates and shells subjected to elevated temperature

Journal Article · Tue Jun 01 00:00:00 EDT 1993 · Journal of Applied Mechanics (Transactions of the ASME, Series E); (United States)

DOI:https://doi.org/10.1115/1.2900823· OSTI ID:5936633

Birman, V; Bert, C W ^[1]

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1. Missouri-Rolla Univ., Saint Louis (United States) Oklahoma Univ., Norman (United States)

Effects of temperature on buckling and post-buckling behavior of reinforced and unstiffened composite plates or cylindrical shells are considered. First, equilibrium equations are formulated for a shell subjected to the simultaneous action of a thermal field and an axial loading. These equations are used to predict a general form of the algebraic equations describing the post-buckling response of a shell. Conditions for the snap-through of a shell subjected to thermomechanical loading are formulated. As an example, the theory is applied to prediction of post-buckling response of flat large-aspect-ratio panels reinforced in the direction of their short edges. 19 refs.

• OSTI ID: 5936633
• Journal Information: Journal of Applied Mechanics (Transactions of the ASME, Series E); (United States), Journal Name: Journal of Applied Mechanics (Transactions of the ASME, Series E); (United States) Vol. 60:2; ISSN 0021-8936; ISSN JAMCAV
• Country of Publication: United States
• Language: English

Related Subjects

36 MATERIALS SCIENCE
360603* -- Materials-- Properties
ASPECT RATIO
BUCKLING
COMPOSITE MATERIALS
HEAT TREATMENTS
MATERIALS
REINFORCED MATERIALS
STRESSES
TEMPERATURE DEPENDENCE
THERMAL STRESSES