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High temperature stress-strain analysisThe objectives are threefold: to assist in developing predictive tools needed to improve design analyses and procedures for the efficient and accurate prediction of burner liner structural performance and response; to calibrate, validate, and evaluate these predictive tools by comparing the predicted results with the experimental data; and to evaluate existing as well as advanced temperature and strain measurement instrumentation, through both contact and noncontact efforts, in a simulated turbine engine combustor environment. As the predictive tool, tests, test methods, instrumentation, and data acquisition and reduction methods are developed and evaluated, a proven, integrated analysis/experiment method will be developed that will permit the accurate prediction of the cyclic life of a burner liner.
Document ID
19870001776
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Thompson, R. L. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 13, 2013
Publication Date
October 1, 1984
Publication Information
Publication: Turbine Engine Hot Section Technology, 1984
Subject Category
Structural Mechanics
Accession Number
87N11209
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19870001747Collected WorksTurbine Engine Hot Section Technology, 1984
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