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Probabilistic Evaluation of Advanced Ceramic Matrix Composite StructuresThe objective of this report is to summarize the deterministic and probabilistic structural evaluation results of two structures made with advanced ceramic composites (CMC): internally pressurized tube and uniformly loaded flange. The deterministic structural evaluation includes stress, displacement, and buckling analyses. It is carried out using the finite element code MHOST, developed for the 3-D inelastic analysis of structures that are made with advanced materials. The probabilistic evaluation is performed using the integrated probabilistic assessment of composite structures computer code IPACS. The affects of uncertainties in primitive variables related to the material, fabrication process, and loadings on the material property and structural response behavior are quantified. The primitive variables considered are: thermo-mechanical properties of fiber and matrix, fiber and void volume ratios, use temperature, and pressure. The probabilistic structural analysis and probabilistic strength results are used by IPACS to perform reliability and risk evaluation of the two structures. The results will show that the sensitivity information obtained for the two composite structures from the computational simulation can be used to alter the design process to meet desired service requirements. In addition to detailed probabilistic analysis of the two structures, the following were performed specifically on the CMC tube: (1) predicted the failure load and the buckling load, (2) performed coupled non-deterministic multi-disciplinary structural analysis, and (3) demonstrated that probabilistic sensitivities can be used to select a reduced set of design variables for optimization.
Document ID
20030068318
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Abumeri, Galib H.
(QSS Group, Inc. Cleveland, OH, United States)
Chamis, Christos C.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
September 7, 2013
Publication Date
July 1, 2003
Subject Category
Composite Materials
Report/Patent Number
E-14075
NASA/TM-2003-212515
NAS 1.15:212515
Report Number: E-14075
Report Number: NASA/TM-2003-212515
Report Number: NAS 1.15:212515
Funding Number(s)
WBS: WBS-22-708-48-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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