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 …

Instability evolution in a transitional hypersonic boundary layer and its effects on
aerodynamic heating are investigated over a 260 mm long flared cone. Experiments are …

A hypersonic shock wave/turbulent boundary layer interaction (STBLI) is investigated using
direct numerical simulation (DNS). The geometry is an 8∘ compression ramp, and the flow …

In the present work, a non-intrusive diagnostic technique known as molecular tagging
velocimetry was used to collect quantitative freestream velocity measurements in the Mach 7 …

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 …

The characterization of a hypersonic impulse facility is performed using a variety of methods
including Pitot probe scans, particle image velocimetry, and schlieren imaging to verify …

Jets-in-supersonic-crossflow have many influential areas of technical applications, amongst
them the field of separation control when implemented as air-jet vortex generators (AJVGs) …

The flow organisation of air-jet vortex generators (AJVGs) of elliptical cross sections and
their control effectiveness on a 24∘-compression-ramp-induced shock-wave/boundary-layer …

In practical aerodynamic problems, curved shock/boundary layer interaction (CSBLI) is more
frequently encountered than the canonical shock/boundary layer interaction (SBLI). Owing to …

A direct numerical simulation of hypersonic Shock wave and Turbulent Boundary Layer
Interaction (STBLI) at Mach 6.0 on a sharp 7° half-angle circular cone/flare configuration at …