posted on 2022-03-08, 09:46authored byThomas A McCaughtry, Rob WatsonRob Watson, Marco Geron
A novel implementation of the flux reconstruction (FR) approach featuring a hyperbolic reformulation of the governing equations in space-time is presented for viscous linear and non-linear flow problems in both one and two spatial dimensions. The procedure generates high-order accurate schemes — in both space and time — that can analyse diffusion-type equations by recasting second-order equations as first-order systems. Conventional high-order accurate analysis of parabolic equations is severely restricted by limits on time step, which can be avoided by reformulation into a system of hyperbolic equations, with the caveat that only steady solutions may be considered. However, the computation of the resulting system within the space-time FR framework permits the high-order accuracy analysis of unsteady flows with rapid convergence to the steady state, in the pseudo-time sense, within a procedure that can be implemented in a straightforward manner for diffusion-type problems. Eigendecomposition is used to demonstrate that the new systems are hyperbolic in nature for both the 1D and 2D Advection-Diffusion Equations. The development and successful implementation of first-order space-time FR schemes for the 1D and 2D Diffusion Equations is illustrated. It is also verified that the target order-of-accuracy (OOA) is achieved for schemes involving both one and two spatial dimensions. An application of the space-time flux reconstruction approach to the Euler Equations is presented and discussed, with a view to future implementation to the Unsteady Navier-Stokes Equations with similar hyperbolic reformulation of viscous terms.
History
School
Aeronautical, Automotive, Chemical and Materials Engineering
Department
Aeronautical and Automotive Engineering
Published in
AIAA AVIATION 2021 FORUM
Source
AIAA AVIATION 2021 FORUM
Publisher
American Institute of Aeronautics and Astronautics, Inc.
This is the accepted version of a paper presented at the AIAA AVIATION 2021 FORUM. The definitive published version is available at https://doi.org/10.2514/6.2021-2736