Computational simulation of high-temperature metal matrix composites cyclic behaviorA procedure was developed and is described that can be used to computationally simulate the cyclic behavior of high-temperature metal matrix composites (HTMMC) and its degradation effects on the structural response. This procedure consists of HTMMC mechanics coupled with a multifactor-interaction constituent material relationship and with an incremental iterative nonlinear analysis. The procedure is implemented in a computer code that can be used to computationally simulate the thermomechanical behavior of HTMMC starting from the fabrication process and proceeding through thermomechanical cycling, accounting for the interface/interphase region. Results show that combined thermal/mechanical cycling, the interphase, and in situ matrix properties have significant effects on the structural integrity of HTMMC.
Document ID
19910034057
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Chamis, Christos C. (NASA Lewis Research Center Cleveland, OH, United States)
Murthy, Pappu L. N. (NASA Lewis Research Center Cleveland, OH, United States)
Hopkins, Dale A. (NASA Lewis Research Center Cleveland, OH, United States)