Reinforcement Mechanisms in Metal-Matrix Composites.
Abstract
A finite-element program was modified and used to analyze the macro- and micro-mechanical behavior of several unidirectional boron-aluminum (6061-T6) composites subject to plane-strain transverse-normal tension in the elastic and plastic ranges of the matrix. Mechanical properties were found to depend on: the reinforcement concentration, the packing arrangement of the circular reinforcements, the direction of the applied transverse-normal stress relative to the packing symmetry, the extent of reinforcement-matrix interface debonding, and the thermal history of the composite. Specially prepared tungsten-aluminum (6061-T6 and -0), unidirectional, square-array composites were tested in transverse-normal tension to verify theoretical predictions.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jul 01, 1974
- Accession Number
- ADA032407
Entities
People
- F. W. Crossman
- Janet Grant
- R. F. Karlak
Organizations
- Lockheed Martin Missiles and Space