Abstract Using Lagrangian Coherent Structures, the influences of synthetic jet parameters,
namely, velocity and frequency, on lift at post-stall attack angle are studied in detail, from …

ABSTRACT A new flow control strategy based on leading-edge vortex (LEV) manipulation is
proposed to improve the aerodynamic performance of a plunging airfoil. It has been found …

The mass transport and lift enhancement in flows over the NACA0015 airfoil with a synthetic
jet (SJ) are studied numerically using Lagrangian coherent structures (LCSs). Trajectories of …

We obtain an optimal actuation waveform for fast synchronization of periodic airfoil wakes
through the phase reduction approach. Using the phase reduction approach for periodic …

The aim of the present work is to control the dynamic stall of a pitching NACA0012 airfoil and
improve its aerodynamic performance by using a synthetic jet in a low Reynolds number …

Flow control of a low-aspect-ratio flat-plate heaving wing at an average angle of attack of
increases from 1000 to 5000 due to its self-limiting mechanism. A mid-chord vertical blowing …

Aiming at aerodynamic drag reduction for transportation systems, a new active surface is
proposed that combines a bionic nonsmooth surface with a jet. Simulations were performed …

In this manuscript, the vortex generated by the main frequency excitation of the shedding
vortex at various attack angles is investigated by employing the synthetic jet control …

Nowadays, synthetic jets have various applications such as cooling enhancement and
active flow control. In the present paper, the capability of two turbulence modelling …

Abstract The Synthetic Jet (SJ) control on the propulsion behavior of a foil in plunge-pitch
motion is examined in this work by numerical simulations. An elliptic foil with ratio of 8 …