Shock-wave/boundary-layer interactions (SWBLIs) are complex flowfields commonly
encountered in many high-speed aerospace applications. A strong shock wave imposes a …

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

Within the inlet of high-speed air-breathing air-vehicles, it is often desirable to employ some
form of flow control to increase inlet performance and flexibility. 1, 2 Traditionally, this has …

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 …

View Video Presentation: https://doi. org/10.2514/6.2023-2138. vid Motivated by the
beneficial effects of air-jet vortex-generators (AJVG) in controlling shock-induced flow …

An experimental analysis was carried out to assess the flow organisation and control
effectiveness of an array of air-jet vortex generators (AJVGs) on an axisymmetric 33 flare …

View Video Presentation: https://doi. org/10.2514/6.2023-4238. vid Beneficial effects of air-
jet vortex generators (AJVGs) in controlling shock-induced flow separation motivated us to …

Experiments were carried out to assess the influence of spanwise spacing between adjacent
orifices of an air-jet vortex-generator (AJVG) array on their separation-control effectiveness …

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) …

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