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Investigation of failure modes in fiber-reinforced ceramic-matrix composites. Master's thesis

Technical Report ·
OSTI ID:6291927
This experimental study was conducted to investigate the damage progression in fiber-reinforced ceramic-matrix composites under tensile loading. As part of this study, the effect of the residual stresses at the fiber-matrix interface on damage progression was evaluated. Composite samples were fabricated from silicon carbide fibers and borosilicate glass matrices. Each glass had a different coefficient of thermal expansion than the fiber and through the variation of this mismatch, the residual stresses at the fiber-matrix interface were varied resulting in different bonding conditions at the fiber-matrix interface. The mechanical properties of the composites were measured using a servo-hydraulic mechanical testing machine. During these tests, transverse strain reversal was observed that is believed to be caused by axial matrix cracks and fiber-matrix debonding. Tensile tests were conducted on the composites using a constant-load straining device in which damage progression was observed using an optical microscope.
Research Organization:
Air Force Inst. of Tech., Wright-Patterson AFB, OH (USA). School of Engineering
OSTI ID:
6291927
Report Number(s):
AD-A-202705/0/XAB; AFIT/GAE/AA-88D-28
Country of Publication:
United States
Language:
English