Direct numerical simulation of supersonic flows passing a backward step
(2014)
Presentation / Conference
Yao, Y., Fang, J., Zheltovodov, A. A., & Lu, L. (2014, September). Direct numerical simulation of supersonic flows passing a backward step. Presented at UK Turbulence Consortium Workshop, Imperial College, London
The Mach 2.9 supersonic turbulent flow over an expansion-compression corner with a sharp deflection angle of 25° at three Reynolds numbers Re_δ=20000, Re_δ=40000 and Re_δ=80000 were studied by using a recently developed direct numerical simulation (... Read More about Direct numerical simulation of supersonic flows passing a backward step.