Compact Direct Flux Reconstruction for the Navier-Stokes Equations on Dynamic Meshes

dc.contributor.authorWang, Lia
dc.contributor.authorYu, Meilin
dc.date.accessioned2018-01-23T15:20:06Z
dc.date.available2018-01-23T15:20:06Z
dc.date.issued2017
dc.description.abstractIn this study, the high-order discontinuous compact direct flux reconstruction (CDFR) method is used to solve the two-dimensional (2D) Navier-Stokes equations on quadrilateral unstructured dynamic meshes. Within a standard element, the CDFR method employs com-pact finite difference (FD) techniques to directly construct the nodal spatial derivatives on Gauss-Legendre solution points. In the procedure of constructing an arbitrary CDFR method, the spatial derivatives are approximated with local fluxes on solution points and common fluxes on element interfaces (flux points) in FD forms. No polynomial reconstruction needs to be employed explicitly. It is observed that the CDFR method is identical with the direct flux re-construction (DFR) method and the nodal flux reconstruction-discontinuous Galerkin (FR-DG) method if Gauss-Legendre points are selected as solution points. For simulations with dynamic meshes, the geometric conservation law (GCL) has been incorporated into the Navier-Stokes equations. The performance of CDFR methods has been verified with various test cases, in-cluding the Euler vortex propagation on deformable meshes, and the Couette flow. Laminar flows of Ma = 0.2 over a static circular cylinder (Re = 100, 185) and an oscillating circular cylinder (Re = 185) have been studied to demonstrate the capability of the solver developed in this study.en_US
dc.format.extent16 pagesen_US
dc.genreconference papers and proceedingsen_US
dc.identifierdoi:10.13016/M2QZ22J8F
dc.identifier.citationLai Wang and Meilin Yu. "Compact Direct Flux Reconstruction for the Navier-Stokes Equations on Dynamic Meshes", 23rd AIAA Computational Fluid Dynamics Conference, AIAA AVIATION Forum, (AIAA 2017-3098) https://doi.org/10.2514/6.2017-3098en_US
dc.identifier.urihttp://hdl.handle.net/11603/7702
dc.language.isoen_USen_US
dc.publisherAIAA Aviation Forumen_US
dc.relation.isAvailableAtThe University of Maryland, Baltimore County (UMBC)
dc.relation.ispartofUMBC Mechanical Engineering Department Collection
dc.relation.ispartofUMBC Faculty Collection
dc.relation.ispartofUMBC Student Collection
dc.relation.ispartofseries23rd AIAA Computational Fluid Dynamics Conference;AIAA 2017-3098
dc.rightsThis item may be protected under Title 17 of the U.S. Copyright Law. It is made available by UMBC for non-commercial research and education. For permission to publish or reproduce, please contact the author.
dc.subjectdynamic meshesen_US
dc.subjectNavier-Stokes equationsen_US
dc.subjectcompact direct flux reconstructionen_US
dc.subjectCDFRen_US
dc.subjectquadrilateral unstructured dynamic meshesen_US
dc.subjectfinite difference techniquesen_US
dc.titleCompact Direct Flux Reconstruction for the Navier-Stokes Equations on Dynamic Meshesen_US
dc.typeTexten_US

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