ZHAO Lu-shun, SHAN Peng, JIE Ke, YANG Zhan-yu, WANG Hong-ming. Numerical study of the cold flowfield of Mach number 2.5 supersonic combustor with supersonic/subsonic streamwise vortices mixing[J]. ACTA AERODYNAMICA SINICA, 2009, 27(2): 160-166.
Citation: ZHAO Lu-shun, SHAN Peng, JIE Ke, YANG Zhan-yu, WANG Hong-ming. Numerical study of the cold flowfield of Mach number 2.5 supersonic combustor with supersonic/subsonic streamwise vortices mixing[J]. ACTA AERODYNAMICA SINICA, 2009, 27(2): 160-166.
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Numerical study of the cold flowfield of Mach number 2.5 supersonic combustor with supersonic/subsonic streamwise vortices mixing

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