The pervasiveness of unmanned air vehicles (UAVs), from insect to airplane scales,
combined with active flow control maturity, has set the scene for vehicles that differ markedly …

The quest for increased performance in the aeronautical and aerospace industries has
provided the driving force and motivation for the research, investigation, and development of …

We conduct large-eddy simulations of separated airfoil flows with control by a dielectric-
barrier-discharge plasma actuator over a wide range of Reynolds numbers. The Reynolds …

The paper compares the influence of different waveforms as input for a dielectric barrier
discharge plasma actuator investigated in context of plasma-assisted flow control. The …

Large-eddy simulations have been conducted to investigate the mechanisms of separated-
flow control using a dielectric barrier discharge plasma actuator at a low Reynolds number …

Control of flow separation from the deflected flap of a high-lift airfoil up to Reynolds numbers
of 240,000 (15 m/s) is explored using a single dielectric barrier discharge (DBD) plasma …

Flow control over a NACA 0012 airfoil is carried out using a dielectric barrier discharge
(DBD) plasma actuator at the Reynolds number of 20 000. Here, the plasma actuator is …

In the present work, we studied numerical and experimentally analysis lift and drag
performances of NACA 0015 airfoil at different attack angle at low Reynolds numbers (Re) …

The effectiveness of closed-loop flow control using a deep Q network (DQN), such as deep
reinforcement learning algorithm, was experimentally researched for a NACA0015 airfoil …

This paper reports experimental results on using steady and unsteady plasma aerodynamic
actuation to control the corner separation, which forms over the suction surface and end wall …