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TECHNICAL PAPERS

Large-Eddy Simulation of Supersonic Flat-Plate Boundary Layers Using the Monotonically Integrated Large-Eddy Simulation (MILES) Technique

[+] Author and Article Information
H. Yan, D. Knight

Department of Mechanical and Aerospace Engineering, Rutgers—The State University of New Jersey, Piscataway, NJ 08854-8058

A. A. Zheltovodov

Institute of Theoretical and Applied Mechanics, Russian Academy of Sciences, Siberian Branch, Novosibirsk 630090, Russiae-mail: zhelt@itam.nsc.ru

J. Fluids Eng 124(4), 868-875 (Dec 04, 2002) (8 pages) doi:10.1115/1.1516578 History: Received March 25, 2002; Revised May 29, 2002; Online December 04, 2002
Copyright © 2002 by ASME
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References

Figures

Grahic Jump Location
Van Driest velocity at M=2.88
Grahic Jump Location
Van Driest velocity at M=4
Grahic Jump Location
Mean streamwise velocity at M=2.88
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Mean streamwise velocity at M=4
Grahic Jump Location
Mean temperature at M=2.88
Grahic Jump Location
Streamwise Reynolds stress at M=2.88
Grahic Jump Location
Streamwise Reynolds stress at M=4
Grahic Jump Location
Reynolds shear stress at M=2.88
Grahic Jump Location
Reynolds shear stress at M=4
Grahic Jump Location
Turbulent Prandtl number

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