A Computational Study on the Effect of Asymmetric Laminar-Turbulent Transition Conditions on a Tangent-Ogive-Cylinder Flight Vehicle at the High Angles of Attack
38th, AIAA fluid dynamics conference ; 2008 ; Seattle, WA
2008-01-01
9 pages
Includes bibliographical references and index
Aufsatz (Konferenz)
Englisch
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