Active cancellation of artificially introduced Tollmien–Schlichting waves using plasma actuators
By Sven Grundmann, Cameron Tropea. 2008
176 citations recorded by the source corpus.
Subfields: Aerospace Engineering, Computational Mechanics
View Paper: https://www.semanticscholar.org/paper/883b8a52d1534067c811689710a60242de0d5b36
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
- Marios Kotsonis
- N. Benard
- Eric Moreau
- Fulvio Scarano
- S. Ghaemi
- L. Veldhuis
- B. W. van Oudheusden
- Bernhard Wieneke
In Computational Mechanics
- S. Ghaemi
- Fulvio Scarano
- N. Benard
- Eric Moreau
- L. Veldhuis
- Marios Kotsonis
- B. W. van Oudheusden
- Bernhard Wieneke
Citations in the corpus
- Measurement of the body force field of plasma actuators (2011, methodology): “Plasma actuators have been used in several studies aiming at separation control [1], turbulent drag reduction [2], boundary layer control [3–5], noise reduction [6] and laminar-turbulent transition delay [7].”
- Diagnostics for characterisation of plasma actuators (2015, background): “Their utilisation has been proposed, among others, for airfoil separation control [41–45], turbine blade separation control [46], laminar-turbulent transition delay [47], lift enhancement [48, 49], bluff body flow control [50, 51], shock wave control [52] and combustion augmentation [38].”
- Electrical and mechanical characteristics of surface AC dielectric barrier discharge plasma actuators applied to airflow control (2014, methodology): “In most of these papers, the actuator is used in context of open-loop control, but plasma discharges find a new route in the construction of closed-loop strategies by using DBD (Lombardi et al. 2012; Benard et al. 2010, 2011; Rethmel et al. 2011; Grundmann and Tropea 2008; Kriegseis et al. 2011a).”