Controlling the crossflow in the yawed-wing boundary layer using a near-wall body force

DOI10.1134/S0015462820010097zbMath1476.76034OpenAlexW3011455137MaRDI QIDQ2238160

S. V. Manuilovich

Publication date: 29 October 2021

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

Full work available at URL: https://doi.org/10.1134/s0015462820010097

zbMATH Keywords

finite difference schemeflow controlboundary layer stabilityFourier series expansionplasma actuator

Mathematics Subject Classification ID

Finite difference methods applied to problems in fluid mechanics (76M20) Parallel shear flows in hydrodynamic stability (76E05) Ionized gas flow in electromagnetic fields; plasmic flow (76X05)

Related Items (1)

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

Cites Work

• 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
• Longitudinally periodic viscous flows generated by a near-wall volume force
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