Optimization of the Aerodynamic Plasma Actuator as an Electrohydrodynamic (EHD) Electrical Device

By J. Roth, Xin Dai. 2006

250 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Electrical and Electronic Engineering

View Paper: https://www.semanticscholar.org/paper/ed9d67ef21b1198d09633a2a1f357147b9e26d5a

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. N. Benard
4. J. Little
5. Mohammad Samimy
6. Eric Moreau
7. M. Nishihara
8. J. Pouvesle

In Electrical and Electronic Engineering

1. Marios Kotsonis
2. N. Benard
3. Igor V. Adamovich
4. Eric Moreau
5. J. Little
6. Mohammad Samimy
7. M. Nishihara
8. J. Pouvesle

Citations in the corpus

• Experimental study of a DBD surface discharge for the active control of subsonic airflow (2008, background): “This structure is similar to the one used by Roth et al [6].”
• High-lift airfoil trailing edge separation control using a single dielectric barrier discharge plasma actuator (2010, background): “Roth and Dai (2006) refer to this region as being characterized by dielectric heating.”
• Modeling of dielectric barrier discharge plasma actuators driven by repetitive nanosecond pulses (2007, background): “Asymmetric dielectric barrier discharge (DBD) plasma actuators are known to be effective in aerodynamic control [1-16].”
• Electrical and mechanical characteristics of surface AC dielectric barrier discharge plasma actuators applied to airflow control (2014, background): “In 2006, Roth and Dai provided an exhaustive parametric study for the optimization of plasma actuators (Roth and Dai 2006).”