Failure Modes in Brittle Matrix Composites (BMC).
Abstract
The objective of this program was to derive theoretical models to predict micromechanical fracture events in BMC. Incorporate the micromechanical models into composite laminate theory. Provide experimental confirmation and characterization approaches. Delineate interface interphase effects on BMC response. This is a bibliography of the publications generated by this program.
Document Details
- Document Type
- Technical Report
- Publication Date
- Apr 01, 1998
- Accession Number
- ADA342734
Entities
People
- G. P. Tandon
- Nicholas J. Pagano
- R. Y. Kim
Organizations
- Air Force Research Laboratory