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NASA NTRS · 19970003424

Discontinuously Stiffened Composite Panel under Compressive Loading

Abstract

The design of composite structures requires an evaluation of their safety and durability under service loads and possible overload conditions. This paper presents a computational tool that has been developed to examine the response of stiffened composite panels via the simulation of damage initiation, growth, accumulation, progression, and propagation to structural fracture or collapse. The structural durability of a composite panel with a discontinuous stiffener is investigated under compressive loading induced by the gradual displacement of an end support. Results indicate damage initiation and progression to have significant effects on structural behavior under loading. Utilization of an integrated computer code for structural durability assessment is demonstrated.

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BibTeXRIS

Minnetyan, Levon, Rivers, James M., Chamis, Christos C., Murthy, Pappu L. N.. 1995-01-01. Discontinuously Stiffened Composite Panel under Compressive Loading. https://ntrs.nasa.gov/citations/19970003424

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