Frontiers in Aerospace Science

Frontiers in Aerospace Science

Volume: 2

High Order Large Eddy Simulation for Shock-Boundary Layer Interaction Control by a Micro-ramp Vortex Generator

Indexed in: EBSCO.

This volume presents an implicitly implemented large eddy simulation (ILES) by using the fifth order bandwidth-optimized WENO scheme. The chosen method is applied to make comprehensive studies on ...
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Interaction Between Ramp Shock Wave and Ringlike Vortices

Pp. 221-236 (16)

Chaoqun Liu, Qin Li, Yonghua Yan, Yong Yang, Guang Yang and Xiangrui Dong


In this chapter, interaction of shock and vortex rings which were generated by MVG is described and analyzed in details. The change of vorticity, vortex, shock strength and location is described in details. The physics of shock and vortex interaction and its influence on the flow structure is also discussed.


Flow separation, Shock, Shock and vortex interaction, Vortex ring, Vorticity.


Center for Numerical Simulation and Modeling, Department of Mathematics, University of Texas at Arlington, Arlington, Texas 76019, TX, USA.