A Hybridized Discontinuous Galerkin Solver for High-Speed Compressible Flow

Author:

May GeorgORCID,Devesse KoenORCID,Rangarajan Ajay,Magin Thierry

Abstract

We present a high-order consistent compressible flow solver, based on a hybridized discontinuous Galerkin (HDG) discretization, for applications covering subsonic to hypersonic flow. In the context of high-order discretization, this broad range of applications presents unique difficulty, especially at the high-Mach number end. For instance, if a high-order discretization is to efficiently resolve shock and shear layers, it is imperative to use adaptive methods. Furthermore, high-Enthalpy flow requires non-trivial physical modeling. The aim of the present paper is to present the key enabling technologies. We discuss efficient discretization methods, including anisotropic metric-based adaptation, as well as the implementation of flexible modeling using object-oriented programming and algorithmic differentiation. We present initial verification and validation test cases focusing on external aerodynamics.

Funder

Deutsche Forschungsgemeinschaft

European Research Council

United States Air Force Office of Scientific Research

Publisher

MDPI AG

Subject

Aerospace Engineering

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