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Large-eddy simulation using a discontinuous Galerkin spectral element method

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

In this paper we discuss the development of a robust, high-order discontinuous Galerkin (DG) spectral element method for large-eddy simulation (LES) of compressible flows. The method secures geometrical flexibility through a fully unstructured grid (triangles in 2D and tetrahedral elements in 3D), allows for arbitrary order of accuracy and has excellent stability properties. An element based filtering technique is used in conjunction with the dynamic procedure to model the effect of sub-grid scales. We aim to use the LES methodology for large-scale simulation in geometrically complex dump combustors. As a first step towards these simulations, we perform validation simulations of compressible, turbulent flow in a plane channel with isothermal walls.

Original languageEnglish (US)
Title of host publicationCollection of Technical Papers - 45th AIAA Aerospace Sciences Meeting
Pages4838-4849
Number of pages12
StatePublished - 2007
Externally publishedYes
Event45th AIAA Aerospace Sciences Meeting 2007 - Reno, NV, United States
Duration: Jan 8 2007Jan 11 2007

Publication series

NameCollection of Technical Papers - 45th AIAA Aerospace Sciences Meeting
Volume7

Other

Other45th AIAA Aerospace Sciences Meeting 2007
Country/TerritoryUnited States
CityReno, NV
Period1/8/071/11/07

ASJC Scopus subject areas

  • Space and Planetary Science
  • Aerospace Engineering

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