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Title: Turbine engine hot section technology 1986

Conference ·
OSTI ID:5669695

The Turbine engine hot section technology (HOST) Project of the NASA Lewis Research Center sponsored a workshop to discuss current research pertinent to turbine engine durability problems. Presentations were made concerning the hot-section environment and the behavior of combustion liners, turbine blades, and turbine vanes. The presentations were divided into six sessions: Instrumentation, Combustion, Turbine Heat Transfer, Structural Analysis, Fatigue and Fracture, and Surface Protection. Topics discussed included modeling of thermal and fluid-flow phenomena, structural analysis, fatigue and fracture, surface protective coatings, constitutive behavior of materials, stress-strain response, and life-prediction methods. Researchers from industry, academia, and government presented results of their work sponsored by the HOST project.

Research Organization:
National Aeronautics and Space Administration, Cleveland, OH (USA). Lewis Research Center
OSTI ID:
5669695
Report Number(s):
N-89-12876; NASA-CP-2444; E-3205; NAS-1.55:2444; CONF-8610163-
Resource Relation:
Conference: 5. annual workshop on turbine engine hot section technology, Cleveland, OH (United States), 21-22 Oct 1986
Country of Publication:
United States
Language:
English