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Micromechanical models for textile compositesNumerical and analytical micromechanical models are presented to predict the thermoelastic behavior of a textile composite. In the numerical model, the unit-cell is discretized with finite elements, and periodic boundary conditions are imposed between opposite faces of the unit-cell. For a thin textile composite, stress gradients effects through the thickness are demonstrated. The consequent difference in the stiffness and strength behavior of thick and thin composites are discussed. The numerical model is implemented to predict 3-D thermo-elastic constants for a thick textile composite, and the plate thermo-mechanical properties for a thin textile composite. The numerical model is extended to compute the thermal residual microstresses due to processing to predict the composite failure envelopes. An analytical model - Selective Averaging Method (SAM) - is proposed, which is based on a judicious combination of stiffness and compliance averaging to estimate the 3-D elastic constants. Both the models are tested and verified for several examples by comparing the stiffness properties with elasticity solutions and available results.
Document ID
19960010553
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Sankar, Bhavani V.
(Florida Univ. Gainesville, FL, United States)
Marrey, Ramesh V.
(Florida Univ. Gainesville, FL, United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1995
Publication Information
Publication: NASA, Langley Research Center Mechanics of Textile Composites Conference
Subject Category
Composite Materials
Accession Number
96N17719
Funding Number(s)
CONTRACT_GRANT: NAG1-1226
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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