Grid Effects on LES Thermo-Acoustic Limit-Cycle of a Full Annular Aeronautical Engine

DOI10.1007/978-94-007-0231-8_22zbMath1303.76075OpenAlexW195203140MaRDI QIDQ2940921

Gabriel Staffelbach, Thierry Poinsot, Pierre Wolf, Laurent Yves Marcel Gicquel

Publication date: 21 January 2015

Published in: Quality and Reliability of Large-Eddy Simulations II (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/978-94-007-0231-8_22

zbMATH Keywords

reliabilitycomplex geometrylarge-eddy simulationturbulent reacting flows

Mathematics Subject Classification ID

Direct numerical and large eddy simulation of turbulence (76F65) Hydro- and aero-acoustics (76Q05) Reaction effects in flows (76V05)

Cites Work

• Boundary conditions for direct simulations of compressible viscous flows
• Development of high-order Taylor-Galerkin schemes for LES
• The basic equations for the large eddy simulation of turbulent flows in complex geometry
• A thickened flame model for large eddy simulations of turbulent premixed combustion
• Database analysis of errors in large-eddy simulation
• LARGE-EDDY SIMULATION OF TURBULENT COMBUSTION
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