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High-performance-vehicle technologyPropulsion needs of high performance military aircraft are discussed. Inlet performance, nozzle performance and cooling, and afterburner performance are covered. It is concluded that nonaxisymmetric nozzles provide cleaner external lines and enhanced maneuverability, but the internal flows are more complex. Swirl afterburners show promise for enhanced performance in the high altitude, low Mach number region.
Document ID
19800001980
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Povinelli, L. A. (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
80N10219
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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