Nonlinear Structural Response of Laminated Composite Plates Subjected to Blast Loading

We are concerned with the theoretical analysis of the laminated composite plates exposed to normal blast shock waves as well as presenting correlation between the theoretical analysis and the experimental results of the strain time histories. The laminated composite plate is clamped at all edges.

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Bibliographic Details
Published in:AIAA journal 1999-12, Vol.37 (12), p.1639-1647
Main Authors: Turkmen, Halit S, Mecitoglu, Zahit
Format: Article
Language:English
Subjects:
Aerodynamics
Approximation theory
Composite materials
Dynamic response
Exact sciences and technology
Finite element method
Fundamental areas of phenomenology (including applications)
Laminated composites
Mechanics
Physics
Plates (structural components)
Problem solving
Runge Kutta methods
Shock waves
Solid mechanics
Structural and continuum mechanics
Theory
Vibration, mechanical wave, dynamic stability (aeroelasticity, vibration control...)
Vibrations and mechanical waves
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Description
Summary:We are concerned with the theoretical analysis of the laminated composite plates exposed to normal blast shock waves as well as presenting correlation between the theoretical analysis and the experimental results of the strain time histories. The laminated composite plate is clamped at all edges.
ISSN:0001-1452
1533-385X
DOI:10.2514/2.646