Control of a swept-wing boundary layer using ring-type plasma actuators

DOI10.1017/JFM.2018.195zbMath1446.76040OpenAlexW2795394560WikidataQ57856645 ScholiaQ57856645MaRDI QIDQ4563613

Matthias R. Kollert, Nima Shahriari, A. Hanifi

Publication date: 4 June 2018

Published in: Journal of Fluid Mechanics (Search for Journal in Brave)

Full work available at URL: https://semanticscholar.org/paper/e8b5a9ff78ae02bdade7c23adfc756a2f06e31db

zbMATH Keywords

boundary layer stabilitytransition to turbulenceboundary layer control

Mathematics Subject Classification ID

Boundary-layer theory, separation and reattachment, higher-order effects (76D10) Flow control and optimization for incompressible viscous fluids (76D55) Transition to turbulence (76F06) Mathematical modeling or simulation for problems pertaining to fluid mechanics (76-10)

Related Items (5)

Instabilities in three-dimensional boundary-layer flows with a highly non-ideal fluid ⋮ Control of crossflow-vortex-induced transition by unsteady control vortices ⋮ A realizable data-driven approach to delay bypass transition with control theory ⋮ On the role of actuation for the control of streaky structures in boundary layers ⋮ Transition in an infinite swept-wing boundary layer subject to surface roughness and free-stream turbulence

Uses Software

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• Nek5000
• GitHub
• gridgen

Cites Work

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• A spectral element method for fluid dynamics: Laminar flow in a channel expansion
• Passive control of transition in three-dimensional boundary layers, with emphasis on discrete roughness elements
• Secondary instability of cross-flow vortices in Falkner–Skan–Cooke boundary layers
• Transition mechanisms induced by travelling crossflow vortices in a three-dimensional boundary layer
• S<scp>TABILITY AND</scp> T<scp>RANSITION OF</scp> T<scp>HREE</scp>-D<scp>IMENSIONAL</scp> B<scp>OUNDARY</scp> L<scp>AYERS</scp>
• An explicit algebraic Reynolds stress model for incompressible and compressible turbulent flows
• Mechanisms and passive control of crossflow-vortex-induced transition in a three-dimensional boundary layer
• Secondary instability of crossflow vortices
• Secondary instability of crossflow vortices and swept-wing boundary-layer transition
• Control of stationary cross-flow modes in a Mach 3.5 boundary layer using patterned passive and active roughness
• Stabilization of a swept-wing boundary layer by distributed roughness elements
• Fast parallel direct solvers for coarse grid problems

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