Numerical Investigation of Supersonic Transition for a Circular Cone at Mach 3.5
38th, AIAA fluid dynamics conference ; 2008 ; Seattle, WA
2008-01-01
24 pages
Includes bibliographical references and index
Conference paper
English
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Numerical Investigation of Transition for a Cone at Mach 3.5: Oblique Breakdown
British Library Conference Proceedings | 2009
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