Serpentine Inlet Performance Enhancement Using Vortex Generator Based Flow Control
Author:
Publisher
Elsevier BV
Subject
Mechanical Engineering,Aerospace Engineering
Reference15 articles.
1. Gridley M C, Walker S H. Inlet and nozzle technology for 21st century fighter aircraft[R]. ASME Paper 96-GT-244, 1996.
2. Flow separation within the engine inlet of an uninhabited combat air vehicle (UCAV) [J];Michael;Journal of Fluids Engineering,2004
3. Reichert BA, Wendt B J. Improving diffusing S duct performance by secondary flow control[R]. AIAA Paper 94–0365, 1994.
4. Subsonic diffuser designed integrally with vortex generators[J];Brown;Journal of Aircraft,1968
5. Anabtawi A J, Blackwelder R F, Lissaman P, et al. An experimental study of vortex generators in boundary layer ingesting diffusers with a centerline offset[R]. AIAA Paper 99–2110, 1999.
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