Stall onset on aerofoils at low to moderately high Reynolds number flows

DOI10.1017/JFM.2013.440zbMath1294.76092OpenAlexW2149329658WikidataQ56212529 ScholiaQ56212529MaRDI QIDQ2878410

Wallace J. Morris II, Zvi Rusak

Publication date: 29 August 2014

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

Full work available at URL: https://doi.org/10.1017/jfm.2013.440

zbMATH Keywords

boundary layersboundary layer separationaerodynamics

Mathematics Subject Classification ID

Navier-Stokes equations for incompressible viscous fluids (76D05) Finite difference methods applied to problems in fluid mechanics (76M20) Boundary-layer theory, separation and reattachment, higher-order effects (76D10)

Related Items (3)

Variation of leading-edge suction during stall for unsteady aerofoil motions ⋮ Flow criticality governs leading-edge-vortex initiation on finite wings in unsteady flow ⋮ On the leading-edge suction and stagnation-point location in unsteady flows past thin aerofoils

Cites Work

• Unnamed Item
• The spontaneous generation of the singularity in a separating laminar boundary layer
• The controversial stability analysis
• Separation and instabilities in the viscious flow over airfoil leading edges
• Marginal Separation
• The cell Reynolds number myth
• Dynamic stall due to unsteady marginal separation
• On nose separation
• Incompressible Laminar Boundary Layers on a Parabola at Angle of Attack: A Study of the Separation Point

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