Unsteady separation from the leading edge of a thin airfoil

DOI10.1063/1.868856zbMath1025.76516OpenAlexW2041077880MaRDI QIDQ4425524

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Publication date: 3 December 2003

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

Full work available at URL: https://doi.org/10.1063/1.868856

Mathematics Subject Classification ID

Boundary-layer theory, separation and reattachment, higher-order effects (76D10)

Related Items (4)

On unsteady boundary-layer separation in supersonic flow. Part 1. Upstream moving separation point ⋮ Boundary-element method for the prediction of performance of flapping foils with leading-edge separation ⋮ On quasi-steady boundary-layer separation in supersonic flow. Part 2. Downstream moving separation point ⋮ Discontinuous solutions of the boundary-layer equations

Cites Work

• The spontaneous generation of the singularity in a separating laminar boundary layer
• The initial flow past an impulsively started sphere at high Reynolds numbers
• On the use of lagrangian variables in descriptions of unsteady boundary-layer separation
• Marginal Separation
• The stability of solutions of the classical unsteady boundary-layer equation
• Dynamic stall due to unsteady marginal separation
• Vortex-induced boundary-layer separation. Part 1. The unsteady limit problem Re [rightward arrow [infty infinity]]
• Incompressible Laminar Boundary Layers on a Parabola at Angle of Attack: A Study of the Separation Point
• Higher approximations in boundary-layer theory Part 3. Parabola in uniform stream

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