Shock Wave Laminar Boundary Layer Interaction Over a Double Wedge in a High Mach Number Flow
52nd, Aerospace sciences meeting; held at the AIAA SciTech Forum 2014 ; 2014 ; National Harbor, MD
01.01.2014
11 pages
Includes bibliographical references and author index
Aufsatz (Konferenz)
Englisch
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Shock-Wave/Boundary-Layer Interactions in High-Mach-Number Flows
British Library Online Contents | 1996
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