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 …

This manuscript reviews published works related to plasma assistance in supersonic
combustion; focusing on mixing enhancement, ignition and flameholding. A special attention …

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 …

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 …

An array of 16 surface arc plasma actuators (SAPAs) is employed to control the shock wave
boundary layer interaction (SWBLI) at a 26 compression ramp in a Mach 2.0 flow. A new …

The problem considered in this work is shock wave (SW) positioning control in shock-
dominated flows. Experiments are conducted to investigate the triggering effect of patterned …

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 …

The current study investigates the control effect of the pulsed arc discharge plasma on the
impinging shock wave and boundary layer interaction (SWBLI) generated by a 14 wedge in …

An experimental study on controlling hypersonic boundary layer transition using a surface
arc plasma actuation array was conducted. First, base boundary transition characteristics …

This study evaluated the effects of the adding of flow momentum using artificial external
source on the controlling of oblique shock wave of a supersonic flow in a three dimensional …