Direct Numerical Simulation of Hypersonic Boundary Layer Transition over a Blunt Cone

Xinliang Li; Dexun Fu; Yanwen Ma

doi:10.2514/1.37305

journal article Nov 01, 2008

Direct Numerical Simulation of Hypersonic Boundary Layer Transition over a Blunt Cone

Xinliang Li Dexun Fu Yanwen Ma

AIAA Journal Vol. 46 No. 11 pp. 2899-2913 · American Institute of Aeronautics and Astronautics (AIAA)

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Details

Published: Nov 01, 2008
Vol/Issue: 46(11)
Pages: 2899-2913

Authors

X

Xinliang Li

Institute of Mechanics, Chinese Academy of Sciences, 100080 Beijing, People’s Republic of China

D

Dexun Fu

Institute of Mechanics, Chinese Academy of Sciences, 100080 Beijing, People’s Republic of China

Y

Yanwen Ma

Institute of Mechanics, Chinese Academy of Sciences, 100080 Beijing, People’s Republic of China

Cite This Article

Xinliang Li, Dexun Fu, Yanwen Ma (2008). Direct Numerical Simulation of Hypersonic Boundary Layer Transition over a Blunt Cone. AIAA Journal, 46(11), 2899-2913. https://doi.org/10.2514/1.37305

Direct Numerical Simulation of Hypersonic Boundary Layer Transition over a Blunt Cone

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