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Reliability analysis of a structural ceramic combustion chamberThe Weibull modulus, fracture toughness and thermal properties of a silicon nitride material used to make a gas turbine combustor were experimentally measured. The location and nature of failure origins resulting from bend tests were determined with fractographic analysis. The measured Weibull parameters were used along with thermal and stress analysis to determine failure probabilities of the combustor with the CARES design code. The effect of data censoring, FEM mesh refinement, and fracture criterion were considered in the analysis.
Document ID
19900018796
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Salem, Jonathan A.
(NASA Lewis Research Center Cleveland, OH, United States)
Manderscheid, Jane M.
(NASA Lewis Research Center Cleveland, OH, United States)
Freedman, Marc R.
(NASA Lewis Research Center Cleveland, OH, United States)
Gyekenyesi, John P.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1990
Subject Category
Structural Mechanics
Report/Patent Number
E-5699
NASA-TM-103264
NAS 1.15:103264
Report Number: E-5699
Report Number: NASA-TM-103264
Report Number: NAS 1.15:103264
Meeting Information
Meeting: International Gas Turbine and Aeroengine Congress and Exposition
Location: Orlando, FL
Country: United States
Start Date: June 3, 1991
End Date: June 6, 1991
Sponsors: ASME
Accession Number
90N28112
Funding Number(s)
PROJECT: RTOP 505-63-1M
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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