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 investigation of primary and secondary crossflow instability developing in
the boundary layer of a is presented. Linear stability theory is applied for preliminary …

The effect of discrete roughness elements on the development and breakdown of stationary
crossflow instability on a swept wing is explored. Receptivity to various element heights and …

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 …

This work experimentally investigates plasma actuator (PA) forcing effects on the base flow
and developing crossflow (CF) instabilities in a swept wing boundary layer. Spanwise …

The presented work introduces a cancellation technique, based on the linear superposition
of stationary crossflow instabilities (CFIs) through the application of a streamwise series of …

The present work is dedicated to the investigation of the effect of an isolated roughness
element on a swept wing boundary layer. In particular, the flow modifications incurred by a …

The variable-sweep wing, as an important morphing wing technology, has received
widespread attention because it can change the sweep angle according to different flight …

At the beginning of the 20th century, the benefits of air transportation were only available to
a handful of travelers. Nowadays, it is an ordinary method of transportation, which 3.8 billion …