Flow Separation Control by Plasma Actuator with Nanosecond Pulsed-Periodic Discharge

By D. Roupassov, A. Nikipelov, M. Nudnova, A. Starikovskii. 2009

483 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Electrical and Electronic Engineering, Radiology, Nuclear Medicine and Imaging

View Paper: https://www.semanticscholar.org/paper/e28af8bebe3a20b6f5ded4d817f0d864158f6bb2

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 Electrical and Electronic Engineering

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

In Radiology, Nuclear Medicine and Imaging

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

Citations in the corpus

• High-lift airfoil trailing edge separation control using a single dielectric barrier discharge plasma actuator (2010, background): “These waveforms seem to accomplish control based on thermal effects alone similar to arc filament-based plasma actuators (Samimy et al. 2007) and have demonstrated leading edge airfoil separation control authority up to Mach 0.85 ( Roupassov et al. 2009 ).”