Dynamic stall due to unsteady marginal separation

DOI10.1017/S0022112087001629zbMath0636.76054OpenAlexW2105029068MaRDI QIDQ3776866

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Publication date: 1987

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

Full work available at URL: https://doi.org/10.1017/s0022112087001629

zbMATH Keywords

Euler equationsboundary layerdynamic stallaerofoil's leading edgeunsteady viscous- inviscid interacting marginal separation

Mathematics Subject Classification ID

General aerodynamics and subsonic flows (76G25)

Related Items (12)

A simple interaction law for viscous-inviscid interaction ⋮ Vortex-induced boundary-layer separation. Part 1. The unsteady limit problem Re [rightward arrow [infty infinity]] ⋮ An airfoil theory of bifurcating laminar separation from thin obstacles ⋮ Unsteady three-dimensional marginal separation, including breakdown ⋮ On recent developments in marginal separation theory ⋮ Entrainment and boundary-layer separation: a modeling history ⋮ On turbulent separation ⋮ Unsteady separation from the leading edge of a thin airfoil ⋮ On a similarity solution in the theory of unsteady marginal separation ⋮ The triple-deck stage of marginal separation ⋮ Marginal separation in three-dimensional flows ⋮ Stall onset on aerofoils at low to moderately high Reynolds number flows

Cites Work

• Triple-deck solutions for subsonic flow past humps, steps, concave or convex corners and wedged trailing edges
• Marginal Separation
• Laminar flow over unsteady humps: the formation of waves
• On the non-parallel flow stability of the Blasius boundary layer
• Is the singularity at separation removable?

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