The impact of a forward-facing step (FFS) on the development of stationary crossflow
instability is investigated on a swept wing model in a low-turbulence wind tunnel at chord …

An experimental study has been carried out to determine the influence of a forward facing-
step (FFS) on the laminar–turbulent transition of a swept wing boundary layer. Wind tunnel …

Experiments have been conducted on a swept wing model in a low-turbulence wind tunnel
at chord Reynolds number of to investigate the unsteady interaction of a forward-facing step …

A combined experimental and numerical approach to the analysis of the secondary stability
of realistic swept-wing boundary layers is presented. Global linear stability theory is applied …

Recent experiments and numerical simulations demonstrated that discrete roughness
elements can be used to control cross-flow instability over a swept wing. Here, the …

A new experimental facility named Swept Transition Experimental Platform (STEP) has been
designed and built for detailed studies of crossflow instability and its interaction with surface …

The present study is to experimentally investigate flow interactions downstream of a bluff-
body incorporated with an annular plasma actuator, potentially for flame stabilization …

This work investigates the response of a transitional boundary layer to spanwise-invariant
dielectric barrier discharge plasma actuator (PA) forcing on a 45 swept wing at a chord …

This paper investigates the potential use of dielectric-barrier-discharge (DBD) plasma
actuators to control the crossflow instability of the boundary layer on a 45° swept NLF-0415 …

Wind tunnel experiments on the receptivity of three-dimensional boundary layers were
performed in a range of freestream turbulence intensities, Tu, from 0.01%—the lowest level …