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Composite sandwich thermostructural behavior - Computational simulationComputational methods have been developed for simulating the thermomechanical behavior of composite sandwiches, in which the analyses with several levels of progressive sophistication were used in conjunction with composite hygrothermomechanical theory. The sophistication levels include: (1) three-dimensional detailed finite element modeling of the honeycomb, the adhesive, and the composite faces; (2) three-dimensional finite element modeling assuming a homogeneous core; (3) laminate theory simulation; and (4) simple equations for predicting the equivalent properties of the honeycomb core. These levels have been packaged into a procedure embedded in a computer code streamlined for the simulation of the composite sandwich hygrothermal and structural behavior. It is shown that in order to properly simulate the thermomechanical response of the composite sandwich, all the honeycomb thermal and mechanical properties must be used.
Document ID
19860054104
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Chamis, C. C.
(NASA Lewis Research Center Cleveland, OH, United States)
Aiello, R. A.
(NASA Lewis Research Center Cleveland, OH, United States)
Murthy, P. L. N.
(Cleveland State University OH, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1986
Subject Category
Structural Mechanics
Report/Patent Number
AIAA PAPER 86-0948
Accession Number
86A38842
Distribution Limits
Public
Copyright
Other

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