Design optimization of the aerodynamic passive flow control on NACA 4415 airfoil using vortex generators
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 …
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 …
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 …
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 …
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
Active flow control is a rapidly developing topic because the associated industrial
applications are of immense importance, particularly for aeronautics. Among all the flow …
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 …
design for flow control consisting of an annular electrode in quiescent and flat plate …
Wind tunnel testing airfoils at low Reynolds numbers
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 …
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
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 …
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 …
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
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 …
demonstrated since the early days of aviation, with the initial technolology being based on …