Review of flow-control devices for wind-turbine performance enhancement
It is projected that, in the following years, the wind-energy industry will maintain its rapid
growth over the last few decades. Such growth in the industry has been accompanied by the …
growth over the last few decades. Such growth in the industry has been accompanied by the …
Current state and future trends in boundary layer control on lifting surfaces
J Svorcan, JM Wang, KP Griffin - Advances in Mechanical …, 2022 - journals.sagepub.com
Successful flow control may bring numerous benefits, such as flow stabilization, flow
reattachment, separation delay, drag reduction, lift increase, aerodynamic performance …
reattachment, separation delay, drag reduction, lift increase, aerodynamic performance …
[HTML][HTML] Enhancement of a cycloidal self-pitch vertical axis wind turbine performance through DBD plasma actuators at low tip speed ratio
A Benmoussa, JC Páscoa - International Journal of Thermofluids, 2023 - Elsevier
Harvesting a maximum power from wind turbines especially at low tip speed ratio still
remains a challenge. Vertical axis wind turbines (VAWTs) suffer periodically from stall which …
remains a challenge. Vertical axis wind turbines (VAWTs) suffer periodically from stall which …
Effect of dielectric barrier discharge plasma actuator on the dynamic moment behavior of pitching airfoil at low Reynolds number
The purpose of this paper is to investigate the feasibility of using dielectric barrier discharge
plasma actuation for the pitch stability control of a National Advisory Committee for …
plasma actuation for the pitch stability control of a National Advisory Committee for …
An experimental study on different plasma actuator layouts for aircraft icing mitigation
An experimental study was conducted to examine the effects of dielectric-barrier-discharge
plasma (DBD) actuator layout on the plasma-induced thermal characteristics and evaluate …
plasma (DBD) actuator layout on the plasma-induced thermal characteristics and evaluate …
Influence of actuation parameters of multi-DBD plasma actuators on the static and dynamic behaviour of an airfoil in unsteady flow
The purpose of this paper is to perform a numerical study regarding the implementation of
dielectric barrier discharge plasma micro-actuators for load alleviation on a NACA 23012 …
dielectric barrier discharge plasma micro-actuators for load alleviation on a NACA 23012 …
Quasi-stationary modeling of the DBD plasma flow control around airfoil
K Adamiak - Physics of Fluids, 2020 - pubs.aip.org
This paper presents the results of numerical simulation of a dielectric barrier discharge
(DBD) plasma actuator and shows its effectiveness to control air flow around the NACA …
(DBD) plasma actuator and shows its effectiveness to control air flow around the NACA …
Study on inner characteristics of plasma synthetic jet actuator and geometric effects
W Zhang, X Geng, Z Shi, S Jin - Aerospace Science and Technology, 2020 - Elsevier
In order to further study the inner characteristics of the plasma synthetic jet actuator (PSJA)
which consists of a cavity, two electrodes and a lid with orifice, a two-dimensional numerical …
which consists of a cavity, two electrodes and a lid with orifice, a two-dimensional numerical …
Flow control on a high-lift wing with microsecond pulsed surface dielectric barrier discharge actuator
B Wei, Y Wu, H Liang, Z Su, Y Li - Aerospace Science and Technology, 2020 - Elsevier
In this study, microsecond pulsed surface dielectric barrier discharge (mSDBD) is utilized to
improve the aerodynamic characteristics of a high-lift wing. First, the characteristics of the …
improve the aerodynamic characteristics of a high-lift wing. First, the characteristics of the …
Flow control around NACA0015 airfoil using a dielectric barrier discharge plasma actuator over a wide range of the Reynolds number
In this study, an experimental investigation of separation control using a dielectric barrier
discharge plasma actuator was performed on an NACA0015 airfoil over a wide range of …
discharge plasma actuator was performed on an NACA0015 airfoil over a wide range of …