An experimental study of vortex generators in boundary layer ingesting diffusers with a centerline offset
Author:
Affiliation:
1. Southern California, Univ., Los Angeles, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1999-2110
Reference20 articles.
1. Aerospace RecommendedPractice (ARP) 1420, "Gas TurbineEngine Inlet Flow Distortion Guidelines,"SocietyofAutomotiveEngineers,1978.
2. Anabtawi, Amer; Blackwelder, Ron; Lissaman, Peter; and Liebeck, Robert, "An Experimental Investigationof BoundaryLayer Ingestionin a diffusing S-Ductwith andWithout PassiveFlow Control," AIAA PaperNo. 99-0739,1999.
3. Bansod,P.andBradshawP. "TheFlow in S-shaped Ducts,"AerodynamicQuarterZy,June1971.
4. The turbulence structure of equilibrium boundary layers
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