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Hierarchical Simulation of Hot Composite StructuresComputational procedures are described to simulate the thermal and mechanical behavior of high temperature metal matrix composites (HT-MMC) in the following three broad areas: (1) Behavior of HT-MMC's from micromechanics to laminate via Metal Matrix Composite Analyzer (METCAN), (2) tailoring of HT-MMC behavior for optimum specific performance via Metal Matrix Laminate Tailoring (MMLT), and (3) HT-MMC structural response for hot structural components via High Temperature Composite Analyzer (HITCAN). Representative results from each area are presented to illustrate the effectiveness of computational simulation procedures. The sample case results show that METCAN can be used to simulate material behavior such as strength, stress-strain response, and cyclic life in HTMMC's; MMLT can be used to tailor the fabrication process for optimum performance such as that for in-service load carrying capacity of HT-MMC's; and HITCAN can be used to evaluate static fracture and fatigue life of hot pressurized metal matrix composite rings.
Document ID
19940006307
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Chamis, C. C.
(NASA Lewis Research Center Cleveland, OH, United States)
Murthy, P. L. N.
(NASA Lewis Research Center Cleveland, OH, United States)
Singhal, S. N.
(Sverdrup Technology, Inc. Brook Park, OH., United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1993
Subject Category
Structural Mechanics
Report/Patent Number
E-7908
NASA-TM-106200
NAS 1.15:106200
Report Number: E-7908
Report Number: NASA-TM-106200
Report Number: NAS 1.15:106200
Meeting Information
Meeting: Biennial Conference on Reliability, Stress Analysis and Failure Prevention
Location: Albuquerque, NM
Country: United States
Start Date: September 19, 1993
End Date: September 22, 1993
Sponsors: ASME
Accession Number
94N10762
Funding Number(s)
PROJECT: RTOP 510-01-50
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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