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Evolution of engine cycles for STOVL propulsion conceptsShort Take-off, Vertical Landing (STOVL) demonstrator concepts using a common ATF engine core are discussed. These concepts include a separate fan and core flow engine cycle, mixed flow STOVL cycles, separate flow cycles convertible to mixed flow, and reaction control system engine air bleed. STOVL propulsion controls are discussed.
Document ID
19900055712
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bucknell, R. L. (Pratt and Whitney Aircraft West Palm Beach, FL, United States)
Frazier, R. H. (United Technologies Corp. Pratt and Whitney Group, West Palm Beach, FL, United States)
Giulianetti, D. J. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 14, 2013
Publication Date
July 1, 1990
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
AIAA PAPER 90-2272
Report Number: AIAA PAPER 90-2272
Accession Number
90A42767
Distribution Limits
Public
Copyright
Other

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