Linear compensator control of a pointsource induced perturbation in a Falkner–Skan–Cooke boundary layer

DOI10.1063/1.1584434zbMath1186.76232OpenAlexW1968985878MaRDI QIDQ3554007

Markus Högberg, Mattias Chevalier, Dan S. Henningson

Publication date: 22 April 2010

Published in: Physics of Fluids (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1063/1.1584434

zbMATH Keywords

boundary layersflow controlaerodynamics

Mathematics Subject Classification ID

Fluid mechanics (76-XX)

Cites Work

• Experimental study of the K-regime of breakdown in straight and swept wing boundary layers
• Optimal and robust control and estimation of linear paths to transition
• Skin-friction Drag ReductionViaRobust Reduced-order Linear Feedback Control
• The Fringe Region Technique and the Fourier Method Used in the Direct Numerical Simulation of Spatially Evolving Viscous Flows
• Linear optimal control applied to instabilities in spatially developing boundary layers
• Linear feedback control and estimation of transition in plane channel flow