In this study an efficient numerical code for shockwave boundary layer interaction (SWBLI) is
developed and non-thermal surface plasma actuation is evaluated for effective shockwave …

In this study we report Acetone Planar Laser Scattering (PLS) visualization of the boundary
layer structure inside Mach 2.6 indraft wind tunnel at Princeton University. The aim is to …

The shock wave/turbulent boundary layer interaction (SWBLI) exists widely in the internal
and external supersonic flow field. The interaction of shock waves with turbulent boundary …

The effect of magnetohydrodynamic (MHD) plasma actuators on the control of hypersonic
shock wave/turbulent boundary layer interactions is investigated here using Reynolds …

Abstract Three Plasma Synthetic Jet Actuators (PSJA) under the high-frequency actuation
are used to control the Shock Wave Boundary Layer Interaction (SWBLI), a high-speed …

Effective control of hypersonic transition is essential. In order to avoid affecting the structural
profile of the aircraft, as well as reducing power consumption and electromagnetic …

Shock Wave-Boundary Layer Interactions (SWBLIs) commonly occur in high-speed flows
from the transonic to the hypersonic regime. They can be found in a variety of applications …

The present work demonstrates feasibility of Mach 5 bow shock control by low-temperature,
nanosecond pulse, surface dielectric barrier discharge operated both single-pulse and at a …

The efficiency and mechanism of an active control device “SparkJet” and its application in
shock-induced separation control are studied using large-eddy simulation in this paper. The …

There are fewer reports on the impinging shock/boundary layer interaction in the high Mach
number and high-temperature flow than that in the supersonic flow. High-temperature flow …