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Life prediction and constitutive models for engine hot section anisotropic materials programThe purpose is to develop life prediction models for coated anisotropic materials used in gas temperature airfoils. Two single crystal alloys and two coatings are now being tested. These include PWA 1480; Alloy 185; overlay coating, PWA 286; and aluminide coating, PWA 273. Constitutive models are also being developed for these materials to predict the plastic and creep strain histories of the materials in the lab tests and for actual design conditions. This nonlinear material behavior is particularily important for high temperature gas turbine applications and is basic to any life prediction system.
Document ID
19880001793
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Swanson, G. A.
(Pratt and Whitney Aircraft East Hartford, CT, United States)
Date Acquired
September 5, 2013
Publication Date
October 1, 1985
Publication Information
Publication: NASA. Lewis Research Center, Turbine Engine Hot Section Technology, 1985
Subject Category
Structural Mechanics
Accession Number
88N11175
Funding Number(s)
CONTRACT_GRANT: NAS3-23939
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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