Role of Actuation Frequency in Controlled Flow Reattachment over a Stalled Airfoil

By M. Amitay, Ari Glezer. 2002

286 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics

View Paper: https://www.semanticscholar.org/paper/2947b49335719281305f828ebad398fc2d8245d2

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. J. Dandois
2. Eric Garnier
3. Igor V. Adamovich
4. Mohammad Samimy
5. J. Little
6. M. Nishihara
7. Pierre Sagaut
8. Sergio Pirozzoli

In Computational Mechanics

1. S. Gordeyev
2. Eric Garnier
3. J. Dandois
4. Igor V. Adamovich
5. E. Jumper
6. Mohammad Samimy
7. Pierre Sagaut
8. M. Nishihara

Citations in the corpus

• Fluid dynamics and aero-optics of turrets (2010, background): “separation line was shown to be effective in delaying flow separation over bluff bodies [41,42] and a variety of compact and powerful active-flow-control devices are now available.”
• High-lift airfoil trailing edge separation control using a single dielectric barrier discharge plasma actuator (2010, background): “[ 10) has been classified as a different regime and is characterized by enhanced energy dissipation associated with spatial scales in the boundary layer (Amitay and Glezer 2002).”
• Numerical simulation of active separation control by a synthetic jet (2007, background): “The first is to study the ‘virtual aeroshaping effect’ discussed by Amitay & Glezer (2002) and Glezer et al. (2005).”