Airfoils with separation and the resulting wakes

DOI10.1017/S0022112086002318zbMath0591.76054OpenAlexW2008257545MaRDI QIDQ3720085

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Publication date: 1986

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

Full work available at URL: https://doi.org/10.1017/s0022112086002318

zbMATH Keywords

conformal mappingnumerical solutionangle of attackairfoil thicknessalgebraic eddy viscosityboundary-layer procedureinviscid-flow methodlarge flow separationrole of transition on the lift coefficientviscous/inviscid interaction method

Mathematics Subject Classification ID

Boundary-layer theory, separation and reattachment, higher-order effects (76D10) Wakes and jets (76D25) Basic methods in fluid mechanics (76M99)

Related Items (2)

Free streamline--boundary layer analysis for separated flow over an airfoil ⋮ SUPERPOSITION TECHNIQUE FOR POTENTIAL FLOW AROUND AN AEROFOIL AND CONTROL OF THE CIRCULATION

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