Stability and receptivity of the swept-wing boundary-layer flow controlled by a periodic sequence of plasma actuators

DOI10.1134/S0015462821050086zbMath1478.76029OpenAlexW3203218695MaRDI QIDQ2052745

S. V. Manuilovich

Publication date: 26 November 2021

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

Full work available at URL: https://doi.org/10.1134/s0015462821050086

zbMATH Keywords

Navier-Stokes equationslinear approximationbody forcestability controllarge Reynolds numberboundary layer crossflow

Mathematics Subject Classification ID

Navier-Stokes equations for incompressible viscous fluids (76D05) Boundary-layer theory, separation and reattachment, higher-order effects (76D10) Parallel shear flows in hydrodynamic stability (76E05) Ionized gas flow in electromagnetic fields; plasmic flow (76X05) Flow control and optimization for incompressible viscous fluids (76D55)

Cites Work

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• Role of the pressure gradient in flows controlled by a near-wall body force
• Control of cross flow in the three-dimensional boundary layer using space-periodic body force action
• Bulk forces removing the crossflow in a laminar boundary layer
• Controlling the crossflow in the yawed-wing boundary layer using a near-wall body force
• Experimental control of swept-wing transition through base-flow modification by plasma actuators

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