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Three-dimensional inelastic analysis methods for hot section componentsThe objective of this program is to produce a series of new computer codes that permit more accurate and efficient three-dimensional inelastic structural analysis of combustor liners, turbine blades, and turbine vanes. Each code embodies a progression of mathematical models for increasingly comprehensive representation of the geometrical features, loading conditions, and forms of nonlinear material response that distinguish these three groups of hot section components.
Document ID
19890007945
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Todd, E. S. (Pratt and Whitney Aircraft East Hartford, CT, United States)
Date Acquired
September 5, 2013
Publication Date
October 1, 1987
Publication Information
Publication: NASA, Lewis Research Center, Turbine Engine Hot Section Technology, 1987
Subject Category
Structural Mechanics
Accession Number
89N17316
Funding Number(s)
CONTRACT_GRANT: NAS3-23697
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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