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Ceramics for the advanced automotive gas turbine engine - A look at a single shaft designA single-shaft regenerative design with a single-stage radial turbine is analyzed in terms of achievable fuel economy for the cases of both limited and unlimited turbine tip speed and regenerator inlet temperature. The 100-hp engine for a 3500-lb automobile is designed to use gasoline. Fuel economy data and operating parameters are presented for different values of turbine inlet temperatures, and turbine stress estimates and ceramic design stress estimates are discussed.
Document ID
19790028837
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Nosek, S. M. (NASA Lewis Research Center Cleveland, Ohio, United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1978
Subject Category
Mechanical Engineering
Meeting Information
Meeting: Ceramics for high performance applications - II;Fifth Army Materials Technology Conference
Location: Newport, RI
Start Date: March 21, 1977
End Date: March 25, 1977
Sponsors: ERDA, Army, ARPA
Accession Number
79A12850
Distribution Limits
Public
Copyright
Other

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