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An overview of aerospace gas turbine technology of relevance to the development of the automotive gas turbine engineThe NASA-Lewis Research Center (LeRC) has conducted, and has sponsored with industry and universities, extensive research into many of the technology areas related to gas turbine propulsion systems. This aerospace-related technology has been developed at both the component and systems level, and may have significant potential for application to the automotive gas turbine engine. This paper summarizes this technology and lists the associated references. The technology areas are system steady-state and transient performance prediction techniques, compressor and turbine design and performance prediction programs and effects of geometry, combustor technology and advanced concepts, and ceramic coatings and materials technology.
Document ID
19780049455
Document Type
Conference Paper
Authors
Evans, D. G. (NASA Lewis Research Center Cleveland, OH, United States)
Miller, T. J. (NASA Lewis Research Center Cleveland, Ohio, United States)
Date Acquired
August 9, 2013
Publication Date
February 1, 1978
Subject Category
MECHANICAL ENGINEERING
Report/Patent Number
SAE PAPER 780075
Meeting Information
Congress and Exposition(Detroit, MI)
Distribution Limits
Public
Copyright
Other