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Turbine Engine Hot Section Technology, 1987Presentations were made concerning the development of design analysis tools for combustor liners, turbine vanes, and turbine blades. Presentations were divided into six sections: instrumentation, combustion, turbine heat transfer, structural analysis, fatigue and fracture, surface protective coatings, constitutive behavior of materials, stress-strain response and life prediction methods.
Document ID
19890007927
Acquisition Source
Legacy CDMS
Document Type
Other - Collected Works
Date Acquired
September 5, 2013
Publication Date
October 1, 1987
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CP-2493
E-3745
NAS 1.55:2493
Report Number: NASA-CP-2493
Report Number: E-3745
Report Number: NAS 1.55:2493
Accession Number
89N17298
Funding Number(s)
PROJECT: RTOP 533-04-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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