Research Article
Dec 1971

Dynamic Stability of Circular Cylindrical Sandwich Panels

Publication: Journal of the Engineering Mechanics Division
Volume 97, Issue 6

Abstract

A theoretical study of the dynamic stability of simply supported sandwich plates and circular cylindrical sandwich panels with dissimilar face-sheets and orthotropic cores is presented. The uniformly distributed periodic edge loads consist of steady components and oscillating components which are impulsive or vary according to an arbitrary piecewise constant law. It was observed that stable regions exist when the steady component of the applied load exceeds the static buckling load. For the particular combination of parameters associated with these regions the oscillating component of the load has a stabilizing effect on the structure. It was further observed that the mathematical structure of the equations governing the dynamic stability of simply supported sandwich plates and circular cylindrical sandwich panels is the same as that for the corresponding simply supported, homogeneous plates and panels, and a complete analogy exists between them.

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Published In

Journal of the Engineering Mechanics Division
Volume 97Issue 6December 1971
Pages: 1643 - 1661

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Published in print: Dec 1971
Published online: Feb 3, 2021

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Conor D. Johnson
Aerospace Engr., Air Force Flight Dynamics Lab., Wright-Patterson AFB, Ohio; formerly Grad. Student, Dept. of Engrg. Mechanics, Clemson Univ., Clemson, S.C.
Nelson R. Bauld Jr.
Prof., Dept. of Engrg. Mechanics, Clemson Univ., Clemson, S.C.

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