NASA NTRS · 19900055712
Evolution of engine cycles for STOVL propulsion concepts
Abstract
Short 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.
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Bucknell, R. L., Frazier, R. H., Giulianetti, D. J.. 1990-07-01. Evolution of engine cycles for STOVL propulsion concepts. https://ntrs.nasa.gov/citations/19900055712
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