Computational study into the flow field developed around a cascade of NACA 0012 airfoils

DOI10.1016/S0045-7825(98)00104-2zbMath0951.76049MaRDI QIDQ1808127

Yanyan Li

Publication date: 13 December 2000

Published in: Computer Methods in Applied Mechanics and Engineering (Search for Journal in Brave)

zbMATH Keywords

liftboundary layerseparation pointcontrol volume approachdrag\(k\)-epsilon modeltwo-dimensional incompressible Navier-Stokes equationsangles of attackpressure contourscascade of NACA 0012 airfoils

Mathematics Subject Classification ID

Finite volume methods applied to problems in fluid mechanics (76M12) (k)-(varepsilon) modeling in turbulence (76F60) General aerodynamics and subsonic flows (76G25) Turbulent boundary layers (76F40)

Related Items (1)

Numerical simulation of the flow field around a cascade of NACA 0012 airfoils -- effects of solidity and stagger

Cites Work

• Numerical study of the turbulent flow past an airfoil with trailing edge separation

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