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 this experimental study, panel flutter induced by an impinging oblique shockwave is
investigated at a freestream Mach number of 2, using the combination of planar particle …

An experiment has been performed in order to provide support for wave-packet jet-noise
modeling efforts. Recent work has shown that the nonlinear effects responsible for the two …

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 …

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 …

This paper aims to study the internal aerodynamics of a Miller cycle gasoline engine. This
cycle uses an over-expanded stroke to recover more work, for the same amount of fuel, than …

In the past decade, advances in electronics technology have made larger imaging sensors
available to the experimental fluid mechanics community. These advancements have …

A comprehensive characterization of the thermal response of nanoscale hot-wire probes is
performed in both subsonic and supersonic flows. A constant current anemometer was …

This work presents a simple analytical model for the streamwise and radial variations of
turbulent kinetic energy dissipation in an incompressible round turbulent jet. The key …

The present paper presents the application of a technique to estimate velocity spectra on the
complex supersonic flowfield of a shock-wave/turbulent boundary-layer interaction. A …