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Reliability analysis of laminated CMC components through shell subelement techniquesAn 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.
Document ID
19920051698
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Starlinger, A.
(NASA Lewis Research Center Cleveland, OH, United States)
Duffy, S. F.
(Cleveland State University OH, United States)
Gyekenyesi, J. P.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1992
Subject Category
Structural Mechanics
Report/Patent Number
AIAA PAPER 92-2348
Meeting Information
Meeting: AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
Location: Dallas, TX
Country: United States
Start Date: April 13, 1992
End Date: April 15, 1992
Accession Number
92A34322
Distribution Limits
Public
Copyright
Other

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