Excitation of controllable perturbations in the three-dimensional boundary layer using plasma actuators

DOI10.1134/S0015462817020107zbMath1368.76078OpenAlexW2606327560MaRDI QIDQ2397904

S. L. Chernyshev, A. P. Kuryachij, A. F. Kiselev

Publication date: 11 August 2017

Published in: Fluid Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1134/s0015462817020107

zbMATH Keywords

boundary layerswept wingcrossflow instabilitydielectric barrier discharge

Mathematics Subject Classification ID

Flow control and optimization for compressible fluids and gas dynamics (76N25) Ionized gas flow in electromagnetic fields; plasmic flow (76X05) Boundary-layer theory for compressible fluids and gas dynamics (76N20)

Related Items (1)

Distinctive features of the distributions of the body force produced by a plasma actuator

Cites Work

• Nonlinear stability and transition in 3-D boundary layers
• Numerical modeling of the laminar-turbulent transition control using a dielectric barrier discharge
• On the formation of streamwise vortices by plasma vortex generators

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