Numerical Investigations on Tollmien–Schlichting Wave Attenuation Using Plasma-Actuator Vortex Generators
Author:
Affiliation:
1. University of Stuttgart, 70550 Stuttgart, Germany
Funder
Deutsche Forschungsgemeinschaft
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J056779
Reference17 articles.
1. Experimental transition delay using glow-discharge plasma actuators
2. Numerical Study of the Control of Tollmien–Schlichting Waves Using Plasma Actuators
3. Feedback control of slowly-varying transient growth by an array of plasma actuators
4. Numerical investigation of plasma-actuator force-term estimations from flow experiments
5. Control of stationary cross-flow modes in a Mach 3.5 boundary layer using patterned passive and active roughness
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