NASA NTRS · 19920051698
Reliability analysis of laminated CMC components through shell subelement techniques
Abstract
An updated version of the integrated design program C/CARES (composite ceramic analysis and reliability evaluation of structures) was developed for the reliability evaluation of CMC laminated shell components. The algorithm is now split in two modules: a finite-element data interface program and a reliability evaluation algorithm. More flexibility is achieved, allowing for easy implementation with various finite-element programs. The new interface program from the finite-element code MARC also includes the option of using hybrid laminates and allows for variations in temperature fields throughout the component.
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Starlinger, A., Duffy, S. F., Gyekenyesi, J. P.. 1992-01-01. Reliability analysis of laminated CMC components through shell subelement techniques. https://ntrs.nasa.gov/citations/19920051698
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