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Turbomachinery technologyA technology assessment of turbomachinery is presented. The design of the fan, compressor, and turbine components for future advanced aircraft engines is discussed. Basic flow characteristics in compressors and turbines and the heat transfer phenomena in cooled turbines are also discussed.
Document ID
19800001973
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hauser, C. H. (NASA Lewis Research Center Cleveland, OH, United States)
Haas, J. E. (U.S. Army Res. and Technol. Labs. Cleveland, Ohio, United States)
Reid, L. (NASA Lewis Research Center Cleveland, OH, United States)
Stepka, F. S. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 10, 2013
Publication Date
January 1, 1979
Publication Information
Publication: Aeropropulsion 1979
Subject Category
Aircraft Propulsion And Power
Accession Number
80N10212
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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