NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Simulated Data for High Temperature Composite DesignThe 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.
Document ID
20060008934
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Chamis, Christos C.
(NASA Glenn Research Center Cleveland, OH, United States)
Abumeri, Galib H.
(QSS Group, Inc. Cleveland, OH, United States)
Date Acquired
September 7, 2013
Publication Date
February 1, 2006
Subject Category
Composite Materials
Report/Patent Number
E-15445
NASA/TM-2006-214111
Report Number: E-15445
Report Number: NASA/TM-2006-214111
Funding Number(s)
WBS: WBS 754.02.07.03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available