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NASA NTRS ยท 19870001747

Turbine Engine Hot Section Technology, 1984

Abstract

Presentations were made concerning the hot section environment and behavior of combustion liners, turbine blades, and waves. The presentations were divided into six sessions: instrumentation, combustion, turbine heat transfer, structural analysis, fatigue and fracture, and surface properties. The principal objective of each session was to disseminate research results to date, along with future plans. Topics discussed included modeling of thermal and fluid flow phenomena, structural analysis, fatigue and fracture, surface protective coatings, constitutive behavior, stress-strain response, and life prediction methods.

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BibTeXRIS

1984-10-01. Turbine Engine Hot Section Technology, 1984. https://ntrs.nasa.gov/citations/19870001747

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