This article describes the spatial development of a laminar separation bubble (LSB), its
transition, and eventual breakdown under the influence of adverse pressure gradients …

A well-resolved large eddy simulation is employed to study the transition of spatially
developing boundary layer when excited by distributed blade-riblets that are arranged in …

The spatial manifestation of a boundary layer subjected to an adverse pressure gradient for
varying freestream turbulence (FST) is discussed here through experiments and a wall …

This experimental investigation studies the impact of streaks on two-dimensional laminar
separation bubbles forming over an aerofoil. Streaks are introduced into the boundary layer …

The evolution of a separated boundary layer on the rough surface in the vicinity of a leading
edge of a model airfoil is documented at varying angles of attack. Particle image velocimetry …

Two separate experiments were conducted on a three-bladed NACA0012 rotor operating at
a blade tip Reynolds number ranging from 44–110× 10 3 using phase-locked infrared …

This study investigates a mechanism for controlling separated flows around an airfoil using a
synthetic jet (SJ). A large-eddy simulation (LES) was performed for a leading-edge …

This study delves into the aerodynamic behaviour of a highly flexible NACA 0012 aerofoil,
drawing inspiration from avian feathers to handle a gust. We first examined unsteady flow on …

Laminar separation bubbles (LSB's) over the suction surface of a wing at low Reynolds
number (O (10 4)− O (10 6) based on the airfoil chord length) can significantly affect the …

The boundary-layer stability on a section of a rotating wind turbine blade with an FFA-W3
series aerofoil at a chord Reynolds number of of the free stream velocity directed towards …