A three-point Focused Laser Differential Interferometer (FLDI) instrument was implemented
to investigate the freestream disturbance environment in a Mach-6 shock tunnel. The FLDI …

Focused laser differential interferometry (FLDI), first introduced in the 1970s, has developed
into a powerful tool for the analysis of turbulent dynamics and fluctuations in fluid flows …

View Video Presentation: https://doi. org/10.2514/6.2023-1234. vid An experimental
investigation on Shockwave/Boundary Layer Interaction (SBLI) induced by an unswept fin is …

Global surface temperature distributions were investigated on the Initial Concept 3. X vehicle
model in the UTSA Mach 7 Wind Tunnel for two different angles of attack, 0° and 5° at a …

High-speed global surface temperature distributions and heat flux measurements on the
Initial Concept 3. X vehicle (IC3X) model were investigated at the UTSA Mach 7 wind tunnel …

A new approach for measuring boundary-layer disturbances with focused laser differential
interferometry (FLDI) for planar models is presented. By integrating a glass window into a flat …

This research work studies the effects of surface roughness on shock-wave/boundary-layer
interactions (SWBLIs). SWBLI are prevalent in supersonic and hypersonic flows and occur …

View Video Presentation: https://doi. org/10.2514/6.2023-3449. vid A new approach for
measuring boundary layer disturbances with focused laser differential interferometry at …

Experimental investigation of swept impinging oblique shock boundary-layer interaction
(SBLI) over a flat plate at Mach 1.85 is presented. A SBLI control technique based on a two …

View Video Presentation: https://doi. org/10.2514/6.2023-3700. vid Fin-induced Shock
Boundary Layer Interactions (SBLIs) are investigated on a hollow cylinder at Mach 5 across …