An investigation of shock/turbulent boundary layer bleed interactions
Author:
Affiliation:
1. Cincinnati, University, OH
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1992-3085
Reference36 articles.
1. Survey of validation data base for shockwave boundary-layer interactions in supersonic inlets
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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. Snowplow Surface Discharge in Magnetic Field for High Speed Boundary Layer Control;44th AIAA Aerospace Sciences Meeting and Exhibit;2006-01-09
4. Boundary conditions for CFD simulations of supersonic boundary-layer flow through discrete holes;38th Aerospace Sciences Meeting and Exhibit;2000-01-10
5. Structure of shock-wave/boundary-layer interactions with bleed through rows of circular holes;35th Aerospace Sciences Meeting and Exhibit;1997-01-06
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