Development and characterization of plasma actuators for high-speed jet control

M Samimy, I Adamovich, B Webb, J Kastner… - Experiments in …, 2004 - Springer
Active control of high Reynolds number and high-speed jets has been hampered due to the
lack of suitable actuators. Some of the attributes that would make an actuator suitable for …

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 …

[图书][B] Fundamentals and applications of modern flow control

RD Joslin, DN Miller - 2009 - arc.aiaa.org
Flow control technologies have been used in the past century to control fluid flows. This text
presents the current state of the art in emerging modern flow control technologies and …

Flow control using plasma actuators and linear/annular plasma synthetic jet actuators

A Santhanakrishnan, J Jacob, Y Suzen - 3rd AIAA Flow Control …, 2006 - arc.aiaa.org
This paper investigates the use of dielectric barrier discharge plasma actuators in low Re
flow control applications. Three different actuator geometries have been tested: a …

Experimental estimation of sparkjet efficiency

S Haack, T Taylor, B Cybyk, C Foster… - … AIAA Plasmadynamics and …, 2011 - arc.aiaa.org
EVERAL classes of micro-actuators are currently under investigation for flow control with the
goal of influencing the boundary layer to improve the flow environment on the surface and …

Adjustable frequency fluidic oscillator with supermode frequency

MN Tomac, E Sundström - AIAA Journal, 2019 - arc.aiaa.org
This Paper introduces a feedback-type fluidic oscillator design with adjustable frequency at
a constant flow rate. Details of the internal and external flowfields were revealed by …

Total drag and lift measurements in a Mach 5 flow affected by a plasma discharge and a magnetic field

J Menart, J Shang, C Atzbach, S Magoteaux… - 43rd AIAA Aerospace …, 2005 - arc.aiaa.org
T this time it is known that a plasma discharge applied to a high speed flow will alter the
characteristics of that flow1-12. The reason for this alteration is the direct heating of the gas …

Analytical model: Characteristics of nanosecond pulsed plasma synthetic jet actuator in multiple-pulsed mode

Z Li, Z Shi, H Du - Advances in Applied Mathematics and Mechanics, 2017 - cambridge.org
Multi-field coupling simulation method based on the physical principles is used to simulate
the discharge characteristics of nanosecond pulsed plasma synthetic jet actuator …

Effect of dielectric barrier discharge plasma actuators on non-equilibrium hypersonic flows

A Bhatia, S Roy, R Gosse - Journal of Applied Physics, 2014 - pubs.aip.org
A numerical study employing discontinuous Galerkin method demonstrating net surface heat
reduction for a cylindrical body in Mach 17 hypersonic flow is presented. This application …

Wind tunnel testing of multi-tip corona actuators on a symmetric airfoil

M Belan, F Messanelli - Journal of Electrostatics, 2017 - Elsevier
A set of 15 different corona actuators with triangular tips on their anodes is studied by
installing them on the leading edge of a NACA 0015 airfoil. Each actuator is identified by its …