Symmetric Interior Penalty DG Methods for the Compressible Navier-Stokes Equations II: Goal--Oriented A Posteriori Error Estimation
By Ralf Hartmann, Paul Houston. 2005
98 citations recorded by the source corpus.
View Paper: https://www.semanticscholar.org/paper/73dc0538ff610f280178718129104fa5e6eb3dd5
How researchers see this paper
The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.
- Krzysztof J. Fidkowski
- Tobias Leicht
- David L. Darmofal
- Ralf Hartmann
- Paul Houston
- Wolfgang Bangerth
- Guido Kanschat
- Bernardo Cockburn
Citations in the corpus
- deal.II—A general-purpose object-oriented finite element library (2007, background): “[Hartmann and Houston 2006a], Figure 6 shows a subsonic viscous compressible flow with separation (taken from [Hartmann and Houston 2006b]).”
- Adaptive discontinuous Galerkin methods with shock‐capturing for the compressible Navier–Stokes equations (2006, methodology): “Reference [6], but does not require the solution of an auxiliary (dual) problem.”
- Symmetric Interior Penalty DG Methods for the CompressibleNavier-Stokes Equations I: Method Formulation (2005, methodology): “Finite element methods, discontinuous Galerkin methods, compressible Navier– Stokes equations”
- Anisotropic mesh refinement for discontinuous Galerkin methods in two‐dimensional aerodynamic flow simulations (2008, methodology): “[6], the error in the target quantity can be represented as follows: J (u) − J (uh) = −N(uh, z − zh) (10)”
- Review of Output-Based Error Estimation and Mesh Adaptation in Computational Fluid Dynamics (2011, background): “Later, they extended their approach to viscous flows [149] and demonstrated applications to a variety of laminar, aerodynamic flows including shock waves (Hartmann [150]).”