28th Congress of the International Council of the Aeronautical Sciences, 23 - 28 September 2012, Brisbane, Australia
Paper ICAS2012-11.4ST

EXTENSIONS OF MENTER’S SST TRANSITION MODEL TO SIMULATE HYPERSONIC AND CROSS-FLOW TRANSITION

X. Zhang, Z. Gao, B. Zhong*
NWPU, Xi'an, China; *COMAC, China

Keywords: hypersonic; boundary layer; transition model; compressibility correlation

An improvement based on Menter’s transition model has been made to expand its application in this paper. a double wedge flat plate and a swept wing are numerically tested to validate the modified model which gets reasonable numerical results compared with the experiment data.

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