Lift and drag performances of an axisymmetric airfoil controlled by plasma actuator

By N. Benard, J. Jolibois, Eric Moreau. 2009

159 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics

View Paper: https://www.semanticscholar.org/paper/2f3f16e0fdc11fc67211eb194143d1289fd73269

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. Igor V. Adamovich
2. Mohammad Samimy
3. J. Little
4. M. Nishihara
5. Marios Kotsonis

In Computational Mechanics

1. Igor V. Adamovich
2. Mohammad Samimy
3. M. Nishihara
4. J. Little

Citations in the corpus

• High-lift airfoil trailing edge separation control using a single dielectric barrier discharge plasma actuator (2010, background): “Like synthetics jets, AC driven DBD plasma actuators are often most effective for separation control and lift enhancement when excitation is created with reduced frequency (F?) on the order of unity (Huang et al. 2006; Greenblatt et al. 2008a; Patel et al. 2008; Benard et al. 2009b).”