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NASA NTRS · 20060008934

Simulated Data for High Temperature Composite Design

Abstract

The paper describes an effective formal method that can be used to simulate design properties for composites that is inclusive of all the effects that influence those properties. This effective simulation method is integrated computer codes that include composite micromechanics, composite macromechanics, laminate theory, structural analysis, and multi-factor interaction model. Demonstration of the method includes sample examples for static, thermal, and fracture reliability for a unidirectional metal matrix composite as well as rupture strength and fatigue strength for a high temperature super alloy. Typical results obtained for a unidirectional composite show that the thermal properties are more sensitive to internal local damage, the longitudinal properties degrade slowly with temperature, the transverse and shear properties degrade rapidly with temperature as do rupture strength and fatigue strength for super alloys.

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BibTeXRIS

Chamis, Christos C., Abumeri, Galib H.. 2006-02-01. Simulated Data for High Temperature Composite Design. https://ntrs.nasa.gov/citations/20060008934

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