Publisher
American Institute of Aeronautics and Astronautics
Cited by
4 articles.
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1. Flow Expansion Based Model for 3-D Multi Bleed Hole Rows;51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2013-01-05
2. Investigation of Segmented Bleed Model in Supersonic Turbulent Boundary Layer;49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2011-01-04
3. Effect of Reynolds number on supersonic flow bleed;48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition;2010-01-04
4. Flowfield measurements inside a boundary-layer bleed slot;AIAA Journal;1996-10