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Fiber Composite Sandwich Thermostructural Behavior - Computational SimulationFour 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.
Document ID
19890023875
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Chamis, Christos C.
(NASA Lewis Research Center Cleveland, OH, United States)
Aiello, Robert A.
(NASA Lewis Research Center Cleveland, OH, United States)
Murthy, Pappu L. N.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1988
Publication Information
Publication: Journal of Composites Technology and Research
Volume: 10
ISSN: 0885-6804
Subject Category
Structural Mechanics
Accession Number
89A11246
Distribution Limits
Public
Copyright
Other

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