Effect of Upstream Flow Deformation Using Plasma Actuators on Crossflow Transition Induced by Unsteady Vortical Free-Stream Disturbances
Author:
Affiliation:
1. University of Stuttgart
2. Royal Institute of Technology (KTH)
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2017-3114
Reference36 articles.
1. STABILITY AND TRANSITION OF THREE-DIMENSIONAL BOUNDARY LAYERS
2. Mechanisms and passive control of crossflow-vortex-induced transition in a three-dimensional boundary layer
3. Transition mechanisms induced by travelling crossflow vortices in a three-dimensional boundary layer
4. Receptivity mechanisms in three-dimensional boundary-layer flows
5. Receptivity of a swept-wing boundary layer to micron-sized discrete roughness elements
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