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Direct Numerical Simulation of Supersonic Turbulent Boundary Layer Flow 被引量:8

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出处 《Chinese Physics Letters》 SCIE CAS CSCD 2005年第7期1709-1712,共4页 中国物理快报(英文版)
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参考文献12

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同被引文献54

  • 1LI XinLiang1,FU DeXun2,MA YanWen2 & LIANG Xian1 1 Key Laboratory of High Temperature Gas Dynamics,Institute of Mechanics,Chinese Academy of Sciences,Beijing 100190,China,2 The State Key Laboratory of Nonlinear Mechanics,Institute of Mechanics,Chinese Academy of Sciences,Beijing 100190,China.Direct numerical simulation of shock/turbulent boundary layer interaction in a supersonic compression ramp[J].Science China(Physics,Mechanics & Astronomy),2010,53(9):1651-1658. 被引量:26
  • 2黄章峰,周恒,罗纪生.超音速平板边界层湍流的直接数值模拟及分析[J].中国科学(G辑),2006,36(1):46-58. 被引量:7
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  • 5Settles G S, Vas I E, Bogdonoff S M. Details of a shock-separated turbulent boundary layer at a compression corner [ J ]. AIAA Journal,1976,14(12) :1709 - 1715.
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  • 10Wilcox D C. Reassessment of the scale determining equation for advanced turbulence models [ J ]. AIAA Journal, 1988,26 ( 11 ) : 1299 - 1310.

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