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A hybridized discontinuous galerkin solver for high-speed compressible flow

Publication ,  Journal Article
May, G; Devesse, K; Rangarajan, A; Magin, T
Published in: Aerospace
November 1, 2021

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.

Duke Scholars

Published In

Aerospace

DOI

EISSN

2226-4310

Publication Date

November 1, 2021

Volume

8

Issue

11

Related Subject Headings

  • 4001 Aerospace engineering
 

Citation

APA
Chicago
ICMJE
MLA
NLM
May, G., Devesse, K., Rangarajan, A., & Magin, T. (2021). A hybridized discontinuous galerkin solver for high-speed compressible flow. Aerospace, 8(11). https://doi.org/10.3390/aerospace8110322
May, G., K. Devesse, A. Rangarajan, and T. Magin. “A hybridized discontinuous galerkin solver for high-speed compressible flow.” Aerospace 8, no. 11 (November 1, 2021). https://doi.org/10.3390/aerospace8110322.
May G, Devesse K, Rangarajan A, Magin T. A hybridized discontinuous galerkin solver for high-speed compressible flow. Aerospace. 2021 Nov 1;8(11).
May, G., et al. “A hybridized discontinuous galerkin solver for high-speed compressible flow.” Aerospace, vol. 8, no. 11, Nov. 2021. Scopus, doi:10.3390/aerospace8110322.
May G, Devesse K, Rangarajan A, Magin T. A hybridized discontinuous galerkin solver for high-speed compressible flow. Aerospace. 2021 Nov 1;8(11).

Published In

Aerospace

DOI

EISSN

2226-4310

Publication Date

November 1, 2021

Volume

8

Issue

11

Related Subject Headings

  • 4001 Aerospace engineering