Abstract
This paper examines the damage process of fiber reinforced glass matrix composites under tensile loading. The tensile damage initiation and growth in BN-coated HI-NICALON SiC fiber reinforced glass matrix cross-ply composites were experimentally clarified by replica observations. An improved shear-lag model with two major cracks, which penetrate both 0 and 90 degree plies, were used to predict the stress-strain behavior. This model reasonably well predicted the stress-strain curve until matrix cracks in 0 degree ply saturated.
Original language | English |
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Pages (from-to) | 221-224 |
Number of pages | 4 |
Journal | Key Engineering Materials |
Volume | 164-165 |
Publication status | Published - 1999 |
Keywords
- Ceramic Matrix Composites
- Energy Release Rate
- Interface Debonding
- Matrix Crack