Laminar Boundary-Layer Response to Step Input by an Array of Plasma Actuators
Author:
Affiliation:
1. York University, Toronto, Ontario M3J 1P3, Canada
2. University of Toronto, Toronto, Ontario M3H 5T6, Canada
Funder
Natural Sciences and Engineering Research Council of Canada
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J061792
Reference43 articles.
1. Transient growth: A factor in bypass transition
2. BOUNDARY-LAYER RECEPTIVITY TO FREESTREAM DISTURBANCES
3. From Streaks to Spots and on to Turbulence: Exploring the Dynamics of Boundary Layer Transition
4. Feedback control of slowly-varying transient growth by an array of plasma actuators
5. Active control of streamwise vortices and streaks in boundary layers
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1. Streamwise Extent and Ramp Rate Effects on Laminar Boundary Layer Response to Plasma Actuator Vortex Generators;Journal of Fluids Engineering;2023-03-08
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