NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Approximating the stress field within the unit cell of a fabric reinforced composite using replacement elementsThis report concerns the prediction of the elastic moduli and the internal stresses within the unit cell of a fabric reinforced composite. In the proposed analysis no restrictions or assumptions are necessary concerning yarn or tow cross-sectional shapes or paths through the unit cell but the unit cell itself must be a right hexagonal parallelepiped. All the unit cell dimensions are assumed to be small with respect to the thickness of the composite structure that it models. The finite element analysis of a unit cell is usually complicated by the mesh generation problems and the non-standard, adjacent-cell boundary conditions. This analysis avoids these problems through the use of preprogrammed boundary conditions and replacement materials (or elements). With replacement elements it is not necessary to match all the constitutional material interfaces with finite element boundaries. Simple brick-shaped elements can be used to model the unit cell structure. The analysis predicts the elastic constants and the average stresses within each constituent material of each brick element. The application and results of this analysis are demonstrated through several example problems which include a number of composite microstructures.
Document ID
19930014688
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Foye, R. L.
(Lockheed Engineering and Sciences Co. Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1993
Subject Category
Composite Materials
Report/Patent Number
NASA-CR-191422
NAS 1.26:191422
Report Number: NASA-CR-191422
Report Number: NAS 1.26:191422
Accession Number
93N23877
Funding Number(s)
PROJECT: RTOP 505-63-50-04
CONTRACT_GRANT: NAS1-19000
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available