Computational Analysis of Shock Wave Turbulent Boundary Layer Interaction (AIAA 2014-0951)
52nd, Aerospace sciences meeting; held at the AIAA SciTech Forum 2014 ; 2014 ; National Harbor, MD
2014-01-01
33 pages
Includes bibliographical references and author index
Conference paper
English
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
LES for Separated Supersonic Turbulent Boundary Layer and Shock Interaction (AIAA 2014-0437)
British Library Conference Proceedings | 2014
|AIAA 2006-0951 A Convective-Diffusive Reaction Zone Structure Model for Turbulent Detonations
British Library Conference Proceedings | 2006
|British Library Conference Proceedings | 2014
|British Library Conference Proceedings | 2014
|Study of 2-D Shock-Wave / Turbulent Boundary Layer Interaction (AIAA 2017-4123)
British Library Conference Proceedings | 2017
|