We perform direct numerical simulation of supersonic turbulent channel flow over cubical
roughness elements, spanning bulk Mach numbers, both in the transitional and fully rough …

Particle image velocimetry experiments were performed to study the effects of surface
roughness on a hypersonic (M ≈ 7.3 M≈ 7.3), flat-plate turbulent boundary layer. Diamond …

View Video Presentation: https://doi. org/10.2514/6.2022-1313. vid In this work, a
configuration of linear array-focused laser differential interferometry (LA-FLDI) is used to …

An experimental study concerning an underexpanded, screeching, Mach 1.5 jet operating at
a stagnation-to-ambient pressure ratio of 4.4 is presented. Experimental data were acquired …

This work expands on previous efforts that observed high-intensity resonance in the
dynamic shock motion generated by shock wave/boundary layer interactions with Mach 1.8 …

This study investigates the effects of near wall disturbances in the form of roughness on a
compressible turbulent boundary layer. The studies were carried out using numerical …

View Video Presentation: https://doi. org/10.2514/6.2022-3925. vid An experimental test
campaign is being conducted to better understand the effects that surface roughness has on …

View Video Presentation: https://doi. org/10.2514/6.2023-2490. vid We investigate the
unsteadiness of a 2D and 3D shock-wave/boundary layer interaction (SBLI) and the effect …

Two-component particle image velocimetry was employed to measure the influence of
surface roughness on a Mach 2 boundary layer. Three surface conditions were examined: a …

This work expands on previous efforts that have observed spectral peaks in the dynamic
shock motion generated by shock wave/boundary layer interactions with Mach 1.8 edge …