Density disturbances in the freestream of the University of Southern Queensland's Mach 6
wind tunnel (ρ _ ∞ ≈ 34\, gm^-3 ρ∞≈ 34 gm-3) have been measured using a focused …

This work discusses the design, measurement, and simulation of an oscillating shock-
wave/boundary-layer interaction on a flat plate at Mach 5.8 and R e∞= 7× 10 6 m− 1. The …

Fast-response coaxial surface junction thermocouples have been used to measure time-
resolved stagnation temperature of the Mach 6 flow produced by the University of Southern …

Hypersonic aerothermoelastic data are needed to investigate fundamental physics and
support the validation of numerical models. To this end, a novel experimental model …

This work investigates first-of-kind experiments to measure fluid-structure interactions (FSI)
on a clamped-free-clamped-free compliant panel at Mach 5.8 in a Ludwieg tube. The panel …

The University of Southern Queensland Hypersonic Testing Facility (TUSQ) is used for
experimentation involving supersonic and hypersonic aerodynamics. TUSQ has four …