An overset-mesh approach for large-Eddy simulation of high-Reynolds number aerofoil flow

DOI10.1080/10618562.2018.1532505OpenAlexW2903749070WikidataQ128785738 ScholiaQ128785738MaRDI QIDQ5031504

Miguel R. Visbal, Donald P. Rizzetta

Publication date: 16 February 2022

Published in: International Journal of Computational Fluid Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1080/10618562.2018.1532505

zbMATH Keywords

large-eddy simulationhigh-order interpolationhigh-order numerical methodhigh-Reynolds number aerofoilnested-grid approach

Mathematics Subject Classification ID

Fluid mechanics (76-XX) Geophysics (86-XX)

Uses Software

• XFOIL
• FDL3DI

Cites Work

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• Compact finite difference schemes with spectral-like resolution
• Effects of the computational time step on numerical solutions of turbulent flow
• Resolution effects in compressible, turbulent boundary layer simulations
• High-order compact finite-difference methods on general overset grids
• VERY HIGH-ORDER SPATIALLY IMPLICIT SCHEMES FOR COMPUTATIONAL ACOUSTICS ON CURVILINEAR MESHES
• Viscous-inviscid analysis of transonic and low Reynolds number airfoils
• An Implicit Factored Scheme for the Compressible Navier-Stokes Equations
• Numerical simulation of delta-wing roll
• On the identification of a vortex
• Implicit Large Eddy Simulation
• Multi‐resolution implicit large eddy simulations using a high‐order overset‐grid approach