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The 3D inelastic analysis methods for hot section componentsAdvanced 3-D inelastic structural/stress analysis methods and solution strategies for more accurate and yet more cost-effective analysis of combustors, turbine blades, and vanes are being developed. The approach is to develop four different theories, one linear and three higher order with increasing complexities including embedded singularities. Progress in each area is reported.
Document ID
19870001773
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Roberts, M. L. (General Electric Co. Fairfield, CT, United States)
Mcknight, R. L. (General Electric Co. Fairfield, CT, United States)
Dame, L. T. (General Electric Co. Fairfield, CT, United States)
Chen, P. C. (General Electric Co. Fairfield, CT, United States)
Date Acquired
August 13, 2013
Publication Date
October 1, 1984
Publication Information
Publication: NASA. Lewis Research Center Turbine Engine Hot Section Technology, 1984
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
87N11206
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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