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Development and validation of a SUPG finite element scheme for the compressible Navier–Stokes equations using a modified inviscid flux discretization
Authors:Benjamin S. Kirk  Graham F. Carey
Affiliation:1. NASA Lyndon B. Johnson Space Center, Houston, TX 77058, U.S.A.;2. The University of Texas at Austin, Austin, TX 78712, U.S.A.
Abstract:This paper considers the streamline‐upwind Petrov–Galerkin (SUPG) method applied to the unsteady compressible Navier–Stokes equations in conservation‐variable form. The spatial discretization, including a modified approach for interpolating the inviscid flux terms in the SUPG finite element formulation, and the second‐order accurate time discretization are presented. The numerical method is discussed in detail. The performance of the algorithm is then investigated by considering inviscid flow past a circular cylinder. Validation of the finite element formulation via comparisons with experimental data for high‐Mach number perfect gas laminar flows is presented, with a specific focus on comparisons with experimentally measured skin friction and convective heat transfer on a 15° compression ramp. Copyright © 2007 John Wiley & Sons, Ltd.
Keywords:SUPG  finite element  compressible flows  shock capturing  inviscid flux discretization  validation
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