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Fiber Composite Sandwich Thermostructural Behavior: Computational SimulationSeveral computational levels of progressive sophistication/simplification are described to computationally simulate composite sandwich hygral, thermal, and structural behavior. The computational levels of sophistication include: (1) three-dimensional detailed finite element modeling of the honeycomb, the adhesive and the composite faces; (2) three-dimensional finite element modeling of the honeycomb assumed to be an equivalent continuous, homogeneous medium, the adhesive and the composite faces; (3) laminate theory simulation where the honeycomb (metal or composite) is assumed to consist of plies with equivalent properties; and (4) derivations of approximate, simplified equations for thermal and mechanical properties by simulating the honeycomb as an equivalent homogeneous medium. The approximate equations are combined with composite hygrothermomechanical and laminate theories to provide a simple and effective computational procedure for simulating the thermomechanical/thermostructural behavior of fiber composite sandwich structures.
Document ID
19860022191
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 Univ. Ohio, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1986
Subject Category
Composite Materials
Report/Patent Number
NAS 1.15:88787
NASA-TM-88787
E-3112
Report Number: NAS 1.15:88787
Report Number: NASA-TM-88787
Report Number: E-3112
Meeting Information
Meeting: Structures, Structural Dynamics and Materials Conference (SDM),
Location: San Antonio, TX
Country: United States
Start Date: May 19, 1986
End Date: May 21, 1986
Sponsors: AHS, ASCE, ASME, AIAA
Accession Number
86N31663
Funding Number(s)
PROJECT: RTOP 505-63-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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