Hysteresis in flow past a NACA 0012 airfoil

DOI10.1016/S0045-7825(01)00382-6zbMath1031.76028MaRDI QIDQ1600767

Sanjay Mittal, Priyank Saxena

Publication date: 16 June 2002

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

zbMATH Keywords

hysteresisNACA 0012 airfoilseparation pointangle of attackstabilized finite element formulationBaldwin-Lomax modelturbulence closureincompressible Reynolds averaged Navier-Stokes equations

Mathematics Subject Classification ID

Navier-Stokes equations for incompressible viscous fluids (76D05) Shear flows and turbulence (76F10) Finite element methods applied to problems in fluid mechanics (76M10)

Related Items

Genuinely characteristic-based scheme for the incompressible turbulent flows ⋮ Selective frequency damping method for steady RANS solutions of turbulent separated flows around an airfoil at stall ⋮ Bifurcation scenario for a two-dimensional static airfoil exhibiting trailing edge stall

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