A hypersonic inlet/isolator acts as the “compressor” for scramjet engines through a series of
shocks, which induces complex internal flows. This paper comprehensively reviews the …

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 …

A multi-channel gliding arc (MCGA) plasma was used to enhance ignition and combustion of
ethylene fuel in a cavity-based scramjet combustor with an inflow speed of Ma= 2.92 …

This paper numerically investigates the energy expenditure of the coflow wall jet for
separation control by analyzing the widely studied NASA hump with two-dimensional …

Particle image velocimetry measurement on shock wave/boundary layer interaction in a
Mach 2.0 supersonic wind tunnel is performed to quantitatively reveal the plasma flow …

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 …

A streamwise array of pulsed spark discharge operating at a high frequency of 10 kHz is
used to control the shock wave/boundary layer interaction (SWBLI) induced by a 24 …

An array of 26 plasma synthetic jet actuators (PSJA) is flush-mounted on a NACA-0015
airfoil model to control the leading-edge flow separation at moderate Reynolds number …

Plasma synthetic jet actuator (PSJA), which produces pulsed jets, is used to control the
shock wave boundary layer interaction at a compression ramp at Ma= 2.0. The flow topology …

Ignition characteristics of the long electrode distance high-energy spark igniter (LHSI) in a
cavity-stabilized scramjet combustor at low flight Mach has been numerically and …