This work is focused on the experimental characterization of shock-dominated flow
structures, parameters, and dynamics under control by a filamentary plasma array. Testing …

The shock-wave/boundary-layer interactions (SWBLIs) at compression ramps (ramp angle
α= 20–30 deg) are studied at M a= 2.0 and under two Reynolds numbers (Re 1= 18,600 and …

The experiment is conducted to investigate the effect of expansion on the shock wave
boundary layer interaction near a compression ramp. The small-angle expansion with an …

In the present work, wall modeled large-eddy simulation (WMLES) in the Fluent software is
used to investigate the flow physics of a three-dimensional shock–turbulent boundary layer …

Characterization of the M= 4.5 flow over a flat-plate model with a 30 deg compression ramp
was performed with low-enthalpy (T 0= 300 K) and high-enthalpy (T 0= 800–1250 K) flow …

By employing a nanoparticle-based planar laser scattering technique, with inflow Mach
number of 2.95, boundary layers formed over two concave walls with respective curvature …

This study considers the effect of an electric discharge on the flow structure near a 19.4°
compression ramp in Mach-2 supersonic flow. The experiments were conducted in the …

The coherent structures arising during flat-plate boundary layer transition at Mach number
3.4 are investigated using a custom-built hyper-rate imaging system. The evolution 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 …

The objective of this work is to perform a feasibility study on the steering effect of a weakly
ionized transient plasma on the corner separation zone of a compression surface with a …