Experimental transition delay using glow-discharge plasma actuators
By Sven Grundmann, Cameron Tropea. 2007
177 citations recorded by the source corpus.
Subfields: Aerospace Engineering, Computational Mechanics
View Paper: https://www.semanticscholar.org/paper/231d676605dcc2a54fd93bfa2203fcec28ccad26
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
In Computational Mechanics
Citations in the corpus
- Active cancellation of artificially introduced Tollmien–Schlichting waves using plasma actuators (2008, background): “In comparison to the previously published damping of perturbations in a boundary layer by steadily operated actuators in Grundmann and Tropea (2007) this procedure consumes only 12% of the energy since the actuator is operated at lower voltages and with duty cycles lower than DCpl = 100%.”
- Electrical and mechanical characteristics of surface AC dielectric barrier discharge plasma actuators applied to airflow control (2014, background): “…McLaughlin et al. 2006; Benard and Moreau 2011; Kelley et al. 2012; Jukes and Choi 2009), developing shear layers (Sosa et al. 2009a; Benard et al. 2008; Thomas et al. 2008) or boundary layer laminar-to-turbulent transitions (Joussot et al. 2010; Grundmann and Tropea 2007; Hanson et al. 2010).”