Time-resolved particle image velocimetry (TR-PIV) has become widespread in fluid
dynamics. Essentially a velocity field movie, the dynamic content provides temporal as well …

We investigate Reynolds number effects in strong shock-wave/turbulent boundary-layer
interactions (STBLI) by leveraging a new database of wall-resolved and long-integrated …

In shock wave/boundary layer interactions, two mechanisms have been recognized to drive
the low-frequency unsteadiness of the reflected shock: upstream boundary layer forcing and …

Experiments were performed to study the effects of an array of microramp sub-boundary-
layer vortex generators on a hypersonic shock/turbulent boundary-layer interaction. Two …

Flow unsteadiness in supersonic impinging jets due to the aeroacoustic feedback can lead
to practical problems like ground erosion in short takeoff and vertical landing aircraft, high …

Shock-wave/boundary-layer interactions (SWBLI) strongly influence the aerodynamic
behaviour of many aerospace, propulsion and transportation systems. They have therefore …

Experiments were performed to study two compression corner interactions at Mach 7.2 and
at a Reynolds number based on a momentum thickness of 3500. Turning angles were …

A new nanoscale thermal anemometry probe (NSTAP) was designed and fabricated to
measure mass flux in supersonic flows. This sensor was evaluated in the Trisonic Wind …

Upon its development and initial characterization, the supersonic variant of the nanoscale
thermal anemometry probe (S-NSTAP) was deployed in a supersonic wind tunnel facility …

In this paper, the dynamic regulating process of a variable-geometry power turbine is
investigated through wind-tunnel experiments. Particle image velocimetry is used to obtain …