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Application of finite element substructuring to composite micromechanicsFinite element substructuring is used to predict unidirectional fiber composite hygral (moisture), thermal, and mechanical properties. COSMIC NASTRAN and MSC/NASTRAN are used to perform the finite element analysis. The results obtained from the finite element model are compared with those obtained from the simplified composite micromechanics equations. A unidirectional composite structure made of boron/HM-epoxy, S-glass/IMHS-epoxy and AS/IMHS-epoxy are studied. The finite element analysis is performed using three dimensional isoparametric brick elements and two distinct models. The first model consists of a single cell (one fiber surrounded by matrix) to form a square. The second model uses the single cell and substructuring to form a nine cell square array. To compare computer time and results with the nine cell superelement model, another nine cell model is constructed using conventional mesh generation techniques. An independent computer program consisting of the simplified micromechanics equation is developed to predict the hygral, thermal, and mechanical properties for this comparison. The results indicate that advanced techniques can be used advantageously for fiber composite micromechanics.
Document ID
19840023218
Acquisition Source
Legacy CDMS
Document Type
Thesis/Dissertation
Authors
Caruso, J. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
August 1, 1984
Subject Category
Composite Materials
Report/Patent Number
E-2203
NAS 1.15:83729
NASA-TM-83729
Report Number: E-2203
Report Number: NAS 1.15:83729
Report Number: NASA-TM-83729
Accession Number
84N31288
Funding Number(s)
PROJECT: RTOP 505-33-5B
CONTRACT_GRANT: NSG-350
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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