Hypersonic Shock Wave Turbulent Boundary Layers: Direct Numerical Simulation, Large Eddy Simulation and Experiment

Author:   Doyle Knight ,  Nadia Kianvashrad
Publisher:   Institute of Physics Publishing
ISBN:  

9780750350006


Pages:   630
Publication Date:   29 June 2023
Format:   Hardback
Availability:   In Print   Availability explained
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Hypersonic Shock Wave Turbulent Boundary Layers: Direct Numerical Simulation, Large Eddy Simulation and Experiment


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Author:   Doyle Knight ,  Nadia Kianvashrad
Publisher:   Institute of Physics Publishing
Imprint:   Institute of Physics Publishing
Dimensions:   Width: 17.80cm , Height: 4.40cm , Length: 25.40cm
ISBN:  

9780750350006


ISBN 10:   0750350008
Pages:   630
Publication Date:   29 June 2023
Audience:   Professional and scholarly ,  Professional & Vocational
Format:   Hardback
Publisher's Status:   Active
Availability:   In Print   Availability explained
This item will be ordered in for you from one of our suppliers. Upon receipt, we will promptly dispatch it out to you. For in store availability, please contact us.

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Doyle Knight is Distinguished Professor of Aerospace Engineering at Rutgers, The State University of New Jersey. He is the author of more than one hundred journal papers, over two hundred conference papers, and two books. His research in gas dynamics includes supersonic and hypersonic shock wave boundary layer interaction, turbulence model development, high-speed inlet unstart and effects of unsteady energy deposition in high-speed flows. His research activity in design optimization focuses on the application of computational fluid dynamics to the automated optimal design of high-speed air vehicles. Nadia Kianvashrad is Postdoctoral Associate in the Department of Mechanical and Aerospace Engineering at Rutgers, The State University of New Jersey. She is the author of six journal papers and 20 conference papers. Her research interests include computational gas dynamics. Her research in computational gas dynamics includes laminar and turbulent shock wave boundary layer interaction in hypersonic flows, and energy deposition for flow and flight control in supersonic and hypersonic flows.

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