Design optimization of the aerodynamic passive flow control on NACA 4415 airfoil using vortex generators

OM Fouatih, M Medale, O Imine, B Imine - European Journal of Mechanics …, 2016 - Elsevier
The present paper provides an experimental optimization of a NACA 4415 airfoil equipped
with vortex generators (VGs) to control its flow separation. To build this optimal configuration …

Airflow control by non-thermal plasma actuators

E Moreau - Journal of physics D: applied physics, 2007 - iopscience.iop.org
Active flow control is a topic in full expansion due to associated industrial applications of
huge importance, particularly for aeronautics. Among all flow control methods, such as the …

[PDF][PDF] Plasma actuators for aeronautics applications-State of art review

G Touchard - … Journal of Plasma Environmental Science and …, 2008 - ijpest.securesite.jp
The goal of this paper is to make a detailed review of the designs and associated setups of
the different aerodynamic plasma actuators developed these last twenty years. First, some …

Experimental study of a DBD surface discharge for the active control of subsonic airflow

B Dong, JM Bauchire, JM Pouvesle… - Journal of Physics D …, 2008 - iopscience.iop.org
The use of plasmas, created by electric discharges, as aerodynamic actuators has been an
exciting research topic for more than ten years. However, investigation of these electric …

Electric wind produced by surface plasma actuators: a new dielectric barrier discharge based on a three-electrode geometry

E Moreau, R Sosa, G Artana - Journal of Physics D: Applied …, 2008 - iopscience.iop.org
Active flow control is a rapidly developing topic because the associated industrial
applications are of immense importance, particularly for aeronautics. Among all the flow …

Flow control with plasma synthetic jet actuators

A Santhanakrishnan, JD Jacob - Journal of Physics D: Applied …, 2007 - iopscience.iop.org
This paper presents an experimental investigation of the characteristics of a plasma actuator
design for flow control consisting of an annular electrode in quiescent and flat plate …

Wind tunnel testing airfoils at low Reynolds numbers

M Selig, R Deters, G Wiliamson - 49th AIAA Aerospace Sciences …, 2011 - arc.aiaa.org
This paper describes the wind tunnel testing methodology that has been applied to testing
over 200 airfoils at low Reynolds numbers (40,000 to 500,000). The experiments were …

Stall control at high angle of attack with plasma sheet actuators

R Sosa, G Artana, E Moreau, G Touchard - Experiments in fluids, 2007 - Springer
We analyzed the modifications of the airflow around an NACA 0015 airfoil when the flow
was perturbed with electrohydrodynamic forces. The actuation was produced with a plasma …

Study of the flow induced by a sliding discharge

R Sosa, É Arnaud, E Mémin… - IEEE Transactions on …, 2009 - ieeexplore.ieee.org
In this work, we report on electrical and fluid-dynamics studies concerning the flow induced
by a sliding discharge (SD). This kind of discharge was created with a three electrode …

A review of thrust-vectoring in support of a V/STOL non-moving mechanical propulsion system

JC Páscoa, A Dumas, M Trancossi, P Stewart… - … European Journal of …, 2013 - Springer
The advantages associated to Vertical Short-Take-Off and Landing (V/STOL) have been
demonstrated since the early days of aviation, with the initial technolology being based on …