Control of normal shock wave/turbulent boundary layer interactions using streamwise grooves
Author:
Affiliation:
1. Cambridge, Univ., United Kingdom
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2002-978
Reference5 articles.
1. A Review of Flow Control Research at Dera
2. Smith, A. N., Babinsky, H., Fulker, J. L., Ashill, P. A. "Control of Normal Shock Wave / Turbulent Boundary-Layer Interaction Using Streamwise Slots", AIAA 2001-0739.
3. An Experimental Investigation of Passive Shock/Boundary-Layer Control on an Aerofoil
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