Wake classification of heaving airfoils using the spectral/hp element method

DOI10.1016/j.cam.2011.11.004zbMath1396.76066OpenAlexW2054623123MaRDI QIDQ432814

W. Medjroubi, B. Stoevesandt, Joachim Peinke

Publication date: 4 July 2012

Published in: Journal of Computational and Applied Mathematics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.cam.2011.11.004

zbMATH Keywords

oscillating airfoilsmoving frame of reference techniquemultiple-vortices-per-half-cycle modethrust generation

Mathematics Subject Classification ID

Navier-Stokes equations for incompressible viscous fluids (76D05) Spectral methods applied to problems in fluid mechanics (76M22) Finite element methods applied to problems in fluid mechanics (76M10) Wakes and jets (76D25)

Related Items (2)

Large eddy simulation of a heaving wing on the cusp of transition to turbulence ⋮ Comparative analysis of the characteristics of the vortex wake behind a flapping wing performing oscillations of different types

Cites Work

• High-order numerical simulations of the flow around a heaving airfoil
• High-order splitting methods for the incompressible Navier-Stokes equations
• A high-order immersed interface method for simulating unsteady incompressible flows on irregular domains
• Frequency selection and asymptotic states in laminar wakes
• A moving frame of reference algorithm for fluid/structure interaction of rotating and translating bodies
• Wake transition in the flow around two circular cylinders in staggered arrangements
• Spectral/hp Element Methods for Computational Fluid Dynamics

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