A review of fundamental research in combustion stabilization for hypersonic airbreathing
propulsion is presented. Combustion in high-speed airbreathing propulsion systems …

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 main focus of the review is on dynamics and kinetics of near-surface discharge
plasmas, such as surface dielectric barrier discharges sustained by AC and repetitively …

The streamwise pulsed arc discharge array (S-PADA), in which five actuators are connected
in series with adjustable frequency, is employed to control the shock wave/boundary layer …

A summary is presented of research progress in the design and technology of hypersonic air
intakes and variable-geometry turbine based combined cycle (TBCC) intakes. Development …

This paper studies the response characteristics of shock wave and boundary layer
interaction (SWBLI) controlled by high-frequency pulsed arc discharge (PAD) in a Mach 2.5 …

The actuations generated by the plasma synthetic jet actuator (PSJA) may become weak
under multiple pulses when the discharge frequency increases. In order to further study the …

The plasma synthetic jet actuator (PSJA) has been proven to have potential for shock wave
control in the supersonic/hypersonic flow. To evaluate the possibility for the PSJA applied in …

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 …

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 …