NASA NTRS · 20030112240
Micromechanics-Based Computational Simulation of Ceramic Matrix Composites
Abstract
Advanced high-temperature Ceramic Matrix Composites (CMC) hold an enormous potential for use in aerospace propulsion system components and certain land-based applications. However, being relatively new materials, a reliable design properties database of sufficient fidelity does not yet exist. To characterize these materials solely by testing is cost and time prohibitive. Computational simulation then becomes very useful to limit the experimental effort and reduce the design cycle time, Authors have been involved for over a decade in developing micromechanics- based computational simulation techniques (computer codes) to simulate all aspects of CMC behavior including quantification of scatter that these materials exhibit. A brief summary/capability of these computer codes with typical examples along with their use in design/analysis of certain structural components is the subject matter of this presentation.
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Murthy, Pappu L. N., Mutal, Subodh K., Duff, Dennis L.. 2003-01-01. Micromechanics-Based Computational Simulation of Ceramic Matrix Composites. https://ntrs.nasa.gov/citations/20030112240
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