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NASA NTRS · 19890023875

Fiber Composite Sandwich Thermostructural Behavior - Computational Simulation

Abstract

Four computational simulation methods with different levels of sophistication were used to simulate thermal behavior and structural changes of composite sandwich panels with a honeycomb core subjected to a variety of environmental effects. The models on thich these methods are based include three-dimensional finite-element modeling, three-dimensional finite-element modeling assuming a homogeneous core, laminate theory, and simple equations for predicting the equivalent properties of the honeycomb core. A procedure was developed and embedded in a composite mechanics computer code, which made it possile to conduct parametric studies to determine 'optimum' composite sandwich configurations for specific applications. The procedure was applied for the evaluation of composite sandwich behavior at the global, local, laminate, ply, and micromechanics levels when the composite sandwich is subjected to hygral, thermal, and mechanical loading environments.

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BibTeXRIS

Chamis, Christos C., Aiello, Robert A., Murthy, Pappu L. N.. 1988-01-01. Fiber Composite Sandwich Thermostructural Behavior - Computational Simulation. https://ntrs.nasa.gov/citations/19890023875

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