超声速及高超声速飞行器在飞行过程中存在复杂的激波/边界层干扰问题,
有效的流动控制技术已成为研究热点, 鼓包是一项具有发展前景的被动控制技术 …

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 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 …

Boundary layer separation is a common phenomenon in supersonic/hypersonic vehicles,
and can adversely affect the lift coefficient. Currently, active flow control based on microjets …

Shock wave/boundary layer interaction (SBLWI) is a common coupling phenomenon that
occurs in hypersonic vehicles, and it adversely affects the flow fields inside and outside the …

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 …

To control the supersonic compressor cascade flow at low Reynolds numbers, this paper
describes the use of nanosecond dielectric barrier discharge (NS-DBD) plasma actuation for …

The control effects of a high-frequency pulsed discharge on a hypersonic separated flow
induced by a 42 compression ramp are studied with high-speed schlieren imaging. A …

ABSTRACT A plasma synthetic jet (PSJ) actuator (PSJA) with a Laval-shaped exit is
investigated using a numerical method alongside a PSJA with a straight-shaped exit for …

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 …