In this chapter, an introduction of shock-boundary layer interaction (SBLI)
is given. A paper review about the driven mechanism of pressure fluctuation caused by
shock induced flow separation on a ramp corner is presented and a research history on
micro vortex generator (MVG) is briefly reviewed. In particular, a series of new
findings made by the LES team at the Center of Numerical Simulation and Modeling
led by Dr. Chaoqun Liu under the support of US Air Force Office of Scientific
Research (AFOSR) is briefly reported. These new findings are milestone work which
have made a breakthrough in understanding the physics of SBLI, shock-vortex ring
interaction, control of shock induced flow separation and noise generation.
Keywords: Flow separation control, Large eddy simulation, Micro vortex
generator, Shock boundary layer interaction, Shock vortex interaction.