In a wide range of aerospace applications like supersonic inlets, transonic airfoils, rocket
engine nozzles and hypersonic vehicles, shock wave boundary layer interactions are a …

View Video Presentation: https://doi. org/10.2514/6.2021-1314. vid A promising flow control
strategy to mitigate shock-induced flow separation is the application of air-jet vortex …

An experimental analysis was carried out to study the control effectiveness and turbulence
behavior of an array of steady air-jet vortex generators on a shock-induced boundary-layer …

Shock-induced separation is a common phenomenon in aero-space transportation
applications which can result in strong detrimental effects. A promising method of passive …

Shock-wave/boundary-layer interactions and associated flow separation are frequently
occurring phenomena in many high-speed flow applications. Injection of spanwise-inclined …

Control of shock wave and boundary layer interaction continues to attract a lot of attention. In
recent decades several methods of interaction control have been investigated in particular …

Flow separation has always been a major concern in all sort of aerodynamic applications,
from aircraft wings, to turbomachinery, wind turbines, and more others. It consists in an …

Shock-wave/turbulent boundary layer interaction are complex flow-fields, commonly
encountered in many air and space transportation applications. A common flow control …

Air jet vortex generators were originally investigated by RA Wallis. Results showed that their
effectiveness in delaying shock induced boundary layer separation was not as good as …

View Video Presentation: https://doi. org/10.2514/6.2022-0700. vid The unsteady features of
a 24 deg compression-ramp interaction controlled with air-jet vortex generators (AJVGs) …