Active separation control: an overview of Reynolds and Mach numbers effects

By Avi Seifert, D. Greenblatt, I. Wygnanski. 2004

146 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics

View Paper: https://www.semanticscholar.org/paper/996c4e58aeb1e5083a12fdbbada7cf3340c82a01

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. K. Takashima
6. Marios Kotsonis

In Computational Mechanics

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

Citations in the corpus

• Separation control with nanosecond-pulse-driven dielectric barrier discharge plasma actuators (2012, background): “It has been suggested that one–four vortices should exist over the controlled region, but the optimal F is dependent on boundary-layer state and forcing amplitude [39].”