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

By Mohammad Samimy, Igor V. Adamovich, B. Webb, J. Kastner, J. Hileman, S. Keshav, P. Palm. 2004

278 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics

View Paper: https://www.semanticscholar.org/paper/ebca825b60ad9e811e80ed4af89da6d318baa29a

How researchers see this paper

The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.

In Aerospace Engineering

1. Marios Kotsonis
2. Igor V. Adamovich
3. Thomas C. Corke
4. Martiqua L. Post
5. Mohammad Samimy
6. Mehul P. Patel
7. Thomas McLaughlin
8. Eric Moreau

In Computational Mechanics

1. Igor V. Adamovich
2. Thomas C. Corke
3. Martiqua L. Post
4. Mehul P. Patel
5. Marios Kotsonis
6. Mohammad Samimy
7. Thomas McLaughlin
8. Y. Utkin

Citations in the corpus

• Active control of a Mach 0.9 jet for noise mitigation using plasma actuators (2007, methodology): “We have used various nozzle extensions attached to the nozzle exit to house the electrodes, as well as various type and size electrodes [44].”
• Scaling Effects of an Aerodynamic Plasma Actuator (2007, background): “Anumber of different plasma actuators have been considered for controlling fluid flow phenomena, including dielectric barrier discharge (DBD) [1,2], dc glow discharge [3], radio-frequency glow discharge [4], and filamentary arc discharge [5].”
• Active control of high-speed and high-Reynolds-number jets using plasma actuators (2005, background): “We have recently developed a class of plasma actuators, called localized arc filament plasma actuators (LAFPA) that can provide excitation signals of high amplitude and high bandwidth for high-speed and high-Reynolds-number flow control (Samimy et al. 2004; Utkin et al. 2007).”
• Diagnostics for characterisation of plasma actuators (2015, background): “Several variations of plasma actuators exist such as nonthermal alternating current dielectric barrier discharge (AC-DBD) [4], direct current corona (DC-corona) [5], nanosecond pulsed dielectric barrier discharge (ns-DBD) [6], and arc filament actuators [7].”
• Development and use of localized arc filament plasma actuators for high-speed flow control (2007, background): “in a nozzle extension without the groove [31], plasma filament”
• Experimental Study for Momentum Transfer in a Dielectric Barrier Discharge Plasma Actuator (2008, background): “In the first category, there are many studies that investigate the applicability of the DBD plasma actuator to flow control for flat plates [3,6,7], bluff bodies [8,9], airfoils [10–16], jets [17], mixing layers [18], 3-D vehicles [19–21], and so on.”