Supersonic turbulent flow simulation using a scalable parallel modal discontinuous Galerkin numerical method.


Journal

Scientific reports
ISSN: 2045-2322
Titre abrégé: Sci Rep
Pays: England
ID NLM: 101563288

Informations de publication

Date de publication:
08 Oct 2019
Historique:
received: 25 03 2019
accepted: 10 09 2019
entrez: 10 10 2019
pubmed: 9 10 2019
medline: 9 10 2019
Statut: epublish

Résumé

The scalability and efficiency of numerical methods on parallel computer architectures is of prime importance as we march towards exascale computing. Classical methods like finite difference schemes and finite volume methods have inherent roadblocks in their mathematical construction to achieve good scalability. These methods are popularly used to solve the Navier-Stokes equations for fluid flow simulations. The discontinuous Galerkin family of methods for solving continuum partial differential equations has shown promise in realizing parallel efficiency and scalability when approaching petascale computations. In this paper an explicit modal discontinuous Galerkin (DG) method utilizing Implicit Large Eddy Simulation (ILES) is proposed for unsteady turbulent flow simulations involving the three-dimensional Navier-Stokes equations. A study of the method was performed for the Taylor-Green vortex case at a Reynolds number ranging from 100 to 1600. The polynomial order P = 2 (third order accurate) was found to closely match the Direct Navier-Stokes (DNS) results for all Reynolds numbers tested outside of Re = 1600, which had a normalized RMS error of 3.43 × 10

Identifiants

pubmed: 31594959
doi: 10.1038/s41598-019-50546-w
pii: 10.1038/s41598-019-50546-w
pmc: PMC6783428
doi:

Types de publication

Journal Article

Langues

eng

Sous-ensembles de citation

IM

Pagination

14442

Subventions

Organisme : Science Applications International Corporation (SAIC)
ID : GS04T09DBC0017
Organisme : Science Applications International Corporation (SAIC)
ID : GS04T09DBC0017
Organisme : Science Applications International Corporation (SAIC)
ID : GS04T09DBC0017
Organisme : Science Applications International Corporation (SAIC)
ID : GS04T09DBC0017
Organisme : National Science Foundation (NSF)
ID : ACI-1548562
Organisme : National Science Foundation (NSF)
ID : ACI-1548562
Organisme : National Science Foundation (NSF)
ID : ACI-1548562
Organisme : National Science Foundation (NSF)
ID : ACI-1548562
Organisme : NSF | National Science Board (NSB)
ID : ACI-1548562

Commentaires et corrections

Type : ErratumIn

Auteurs

Tomas Houba (T)

SurfPlasma Inc, Gainesville, FL, 32601, USA.

Arnob Dasgupta (A)

Applied Physics Research Group, Department of Mechanical and Aerospace Engineering, University of Florida, Gainesville, FL, 32601, USA.

Shivasubramanian Gopalakrishnan (S)

Department of Mechanical Engineering, Indian Institute of Technology Bombay, Mumbai, 400076, India.

Ryan Gosse (R)

Vanilla Peak Ct, Vail, AZ, 85641, USA.

Subrata Roy (S)

SurfPlasma Inc, Gainesville, FL, 32601, USA. roy@ufl.edu.
Applied Physics Research Group, Department of Mechanical and Aerospace Engineering, University of Florida, Gainesville, FL, 32601, USA. roy@ufl.edu.

Classifications MeSH