Comparison of high-order numerical methodologies for the simulation of the supersonic Taylor–Green vortex flow

Author:

Chapelier Jean-Baptiste1ORCID,Lusher David J.2ORCID,Van Noordt William3,Wenzel Christoph4ORCID,Gibis Tobias4ORCID,Mossier Pascal4,Beck Andrea4ORCID,Lodato Guido5ORCID,Brehm Christoph6ORCID,Ruggeri Matteo7ORCID,Scalo Carlo7ORCID,Sandham Neil2ORCID

Affiliation:

1. ONERA—Department of Aerodynamics, Aeroelasticity and Acoustics 1 , 92322 Châtillon, France

2. Aerodynamics and Flight Mechanics Group, University of Southampton 2 , Southampton SO17 1BJ, United Kingdom

3. Department of Engineering Science, University of Oxford 3 , Wellington Square, Oxford OX1 2JD, United Kingdom

4. Institute of Aerodynamics and Gas Dynamics, University of Stuttgart 4 , 70569 Stuttgart, Germany

5. INSA Rouen Normandie—CORIA-CNRS 5 —76800 Saint-Etienne-du-Rouvray, France

6. Aerospace Engineering, Alfred Gessow Rotorcraft Center, University of Maryland at College Park, College Park 6 , Maryland 20742, USA

7. School of Mechanical Engineering, Purdue University, West Lafayette 7 , Indiana 47906, USA

Abstract

This work presents a comparison of several high-order numerical methodologies for simulating shock/turbulence interactions based on the supersonic Taylor–Green vortex flow, considering a Reynolds number of 1600 and a Mach number of 1.25. The numerical schemes considered include high-order Finite Difference, Targeted Essentially Non-Oscillatory, Discontinuous Galerkin, and Spectral Difference schemes. The shock capturing methods include high-order filtering, localized artificial diffusivity, non-oscillatory numerical fluxes, and local low-order switching. The ability of the various high-order numerical methodologies to both capture shocks and represent accurately the development of turbulent vortices is assessed.

Publisher

AIP Publishing

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