The problem considered in this work is shock wave (SW) positioning control in shock-
dominated flows. Experiments are conducted to investigate the triggering effect of patterned …

The supersonic wind tunnel facility SBR-50 at the University of Notre Dame was built in 2015
for experimental research related to shock wave (SW) interactions with obstacles and …

This review examines studies aimed at the organization of energy (non-mechanical) control
of high-speed flow/flight using spatially multi-component plasma structures and combined …

This study examines the mixing and flameholding characteristics of a plasma stabilized
planewall supersonic combustor. Fuel injection, ignition, and flameholding are provided by …

Laminar–turbulent transition control is one of the key problems in the design of hypersonic
vehicles. In particular, for air-breathing hypersonic vehicles, early onset turbulence in the …

Pressure-sensitive paint (PSP) was applied to the surface of a NACA0012 airfoil to
investigate pressure fluctuations associated with trailing edge (TE) noise under low-velocity …

Pressure‐sensitive paints (PSPs) have been demonstrated to be very important for
aerodynamics research. In order to improve the pressure sensitivity and adhesion ability of …

Several classical and non-classical reduced-order nucleation rate models are presented
and compared to experimental values for the homogeneous nucleation rate of CO 2 in …

A new design of plasma-assisted injector to ignite or stabilize combustion is presented. This
design is intended to produce discharges that penetrate the combustion chamber instead of …

View Video Presentation: https://doi. org/10.2514/6.2023-1864. vid This paper focuses on
the experimental study of shock wave positioning and control of the reflection pattern by a …