NUMERICAL SIMULATION OF HYPERSONIC AIR INTAKE FLOW IN SCRAMJET PROPULSION USING A MESH-ADAPTIVE APPROACH
18th, AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference ; 2012 ; Tours, France
2012-01-01
22 pages
Includes bibliographical references and index
Conference paper
English
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Simulation of hypersonic scramjet exhaust
NTRS | 1975
|Simulation of hypersonic scramjet exhaust
TIBKAT | 1975
|