Recent advances in shock wave boundary layer interaction research are reviewed in four
areas:(i) understanding low frequency unsteadiness,(ii) heat transfer prediction …

Flow control using DBD (dielectric-barrier-discharge) plasma actuators is a relatively new,
but rapidly expanding area of research. There are a number of review papers available on …

The shock wave/boundary-layer interaction is a common phenomenon, and it occurs in the
internal and external flow fields of the hypersonic vehicle. Then, the separation, the …

The pervasiveness of unmanned air vehicles (UAVs), from insect to airplane scales,
combined with active flow control maturity, has set the scene for vehicles that differ markedly …

In an air-breathing engine the flow deceleration from supersonic to subsonic conditions
takes places inside the isolator through a gradual compression consisting of a series of …

A pulsed-plasma jet actuator is used to control the unsteady motion of the separation shock
of a shock wave/boundary layer interaction formed by a compression ramp in a Mach 3 flow …

Localized arc filament plasma actuators (LAFPAs) are used for shock wave/boundary layer
interaction induced separation control in a Mach 2.3 flow. The boundary layer is fully …

The plasma synthetic jet actuator (PSJA), also named as sparkjet actuator, is a special type
of zero-net mass flux actuator, driven thermodynamically by pulsed arc/spark discharge …

Abstract A Quasi-DC (Q-DC) electrical discharge generates a highly transient filamentary
plasma in high-speed airflow. Major specific properties of this type of discharge are realized …

In this paper, the hypersonic shock-shock interaction control using plasma actuator array is
experimentally studied to explore a new surface thermal protection method of hypersonic …