Separation and instabilities in the viscious flow over airfoil leading edges

DOI10.1016/S0045-7930(98)00014-0zbMath0978.76062MaRDI QIDQ1975507

Rajesh Bhaskaran, Alric P. Rothmayer

Publication date: 31 January 2002

Published in: Computers and Fluids (Search for Journal in Brave)

zbMATH Keywords

Navier-Stokes equationsskin frictionboundary layersmall perturbationsoscillating airfoilsunsteady separationRayleigh instabilityeddiespitching airfoilsstationary airfoilstwo-dimensional unsteady leading-edge flow

Mathematics Subject Classification ID

Navier-Stokes equations for incompressible viscous fluids (76D05) Finite difference methods applied to problems in fluid mechanics (76M20)

Related Items (4)

Numerical prediction of unsteady vortex shedding for large leading-edge roughness. ⋮ Laminar boundary layer flow of saturated vapor and its condensate over a horizontal tube ⋮ Mathematical modelling of the active flow control by periodic excitation ⋮ Stall onset on aerofoils at low to moderately high Reynolds number flows

Uses Software

• EDDIE

Cites Work

• The spontaneous generation of the singularity in a separating laminar boundary layer
• The stability of solutions of the classical unsteady boundary-layer equation
• On the stability and the numerical solution of the unsteady interactive boundary-layer equation
• Numerical solution of the Navier-Stokes equations for symmetric laminar incompressible flow past a parabola

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