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Fatigue life prediction of an intermetallic matrix composite at elevated temperaturesA strain-based fatigue life prediction method is proposed for an intermetallic matrix composite (IMC) under tensile cyclic loadings at elevated temperatures. Styled after the Universal Slopes method, the model utilizes the composite's tensile properties to estimate fatigue life. Factors such as fiber volume ratio, number of plys and temperature dependence are implicitly incorporated into the model through these properties. The model constants are determined by using unidirectional fatigue data at temperatures of 425 and 815 C. Fatigue lives from two independent sources are used to verify the model at temperatures of 650 and 760 C. Cross-ply lives at 760 C are also predicted. It is demonstrated that the correlation between experimental and predicted lives is within a factor of two.
Document ID
19910016128
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bartolotta, Paul A.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1991
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TM-104494
E-6352
NAS 1.15:104494
Report Number: NASA-TM-104494
Report Number: E-6352
Report Number: NAS 1.15:104494
Meeting Information
Meeting: 1991 Winter Annual Meeting of ASME
Location: Atlanta, GA
Country: United States
Start Date: December 1, 1991
End Date: December 6, 1991
Accession Number
91N25442
Funding Number(s)
PROJECT: RTOP 510-01-50
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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