Control of a Shock-Wave/Boundary-Layer Interaction and Subsequent Subsonic Diffuser Using a Combination of Vortex Generators and Bleed
50th, Aerospace sciences meeting; including the new horizons forum and aerospace exposition 2012 ; 2012 ; Nashville, TN
Aerospace sciences meeting; including the new horizons forum and aerospace exposition 2012 ; 3989-4007
2012-01-01
19 pages
Includes bibliographical references and index
Conference paper
English
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