NASA NTRS · 19890007927
Turbine Engine Hot Section Technology, 1987
Abstract
Presentations 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.
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1987-10-01. Turbine Engine Hot Section Technology, 1987. https://ntrs.nasa.gov/citations/19890007927
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