Matrix cracking in ceramic matrix composites with fine grained fibers at high temperatures will be governed by fiber creep, as relaxation of the fibers eliminates crack tip shielding. Using a time dependent bridging law which describes the effect of creeping fibers bridging a crack in an elastic matrix, crack growth initiation and history have been modeled. For a stationary crack, crack tip stress intensity factors as a function of time are presented to predict incubation times before subcritical crack growth. Two crack growth studies are reviewed: a constant velocity approximation for small-scale bridging, and a complete velocity history analysis which can be used to predict crack length as a function of time. The predictions are summarized and discussed in terms of identifying various regimes of crack growth initiation, subcritical growth, and catastrophic matrix cracking.
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ASME 1997 International Gas Turbine and Aeroengine Congress and Exhibition
June 2–5, 1997
Orlando, Florida, USA
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-7871-2
PROCEEDINGS PAPER
Time Dependent Crack Initiation and Growth in Ceramic Matrix Composites
Matthew R. Begley,
Matthew R. Begley
Harvard University, Cambridge, MA
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Brian N. Cox,
Brian N. Cox
Rockwell International, Thousand Oaks, CA
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Robert M. McMeeking
Robert M. McMeeking
University of California, Santa Barbara, Santa Barbara, CA
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Matthew R. Begley
Harvard University, Cambridge, MA
Brian N. Cox
Rockwell International, Thousand Oaks, CA
Robert M. McMeeking
University of California, Santa Barbara, Santa Barbara, CA
Paper No:
97-GT-275, V004T14A051; 11 pages
Published Online:
December 24, 2014
Citation
Begley, MR, Cox, BN, & McMeeking, RM. "Time Dependent Crack Initiation and Growth in Ceramic Matrix Composites." Proceedings of the ASME 1997 International Gas Turbine and Aeroengine Congress and Exhibition. Volume 4: Manufacturing Materials and Metallurgy; Ceramics; Structures and Dynamics; Controls, Diagnostics and Instrumentation; Education; IGTI Scholar Award. Orlando, Florida, USA. June 2–5, 1997. V004T14A051. ASME. https://doi.org/10.1115/97-GT-275
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