The aim of present study is to delay stall and increase the aerodynamic performance of
NASA GAW-(2) supercritical airfoil by using a synthetic jet actuator. In this research, the …

In this research, the aerodynamic performance of a wing with NASA SC (2)-0714 airfoil and
a high-lift configuration, including the main element and the slotted flap at the trailing edge …

The purpose of this research is to use the artificial jet actuator to control the boundary layer
with the approach of improving the aerodynamic performance of NASA GAW-2 supercritical …

Plasma actuator is one of the newest ways in vortex generation and flow control techniques
that can enhance heat transfer rate by inducing external momentum to the boundary layer of …

Plasma actuator is one of the newest devices in flow control techniques which can delay
sepration by inducing external momentum to the boundary layer of the flow. The purpose of …

Interest in plasma actuator as an active flow control has grown rapidly in the last years.
Plasma actuator consists of a pair of electrodes that are separated by a dielectric material …

In the present study, the effects of plasma actuator on the flow and thermal fields of the film
cooling through a single row of inclined fan-shaped hole over a flat plate model have been …

In this study, the effect of blowing angle on coefficients of aerodynamic of NACA0012 airfoil
at Re= 4× 106 has been investigated. In the present research, the effect of three …

This research aims to improve the aerodynamics performance of a NACA 23012 airfoil
equipped with a High lift device by changing one of its most important geometric parameters …

The aim of this research is to improve the aerodynamic performance of a NACA-23012 airfoil
equipped with a High lift device by changing its geometric parameters. In this research …