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A Robust hp-Adaptation Method for Discontinuous Galerkin Discretizations Applied to Aerodynamic Flows.

dc.contributor.authorCeze, Marco Antonio de Barrosen_US
dc.date.accessioned2013-06-12T14:15:01Z
dc.date.availableNO_RESTRICTIONen_US
dc.date.available2013-06-12T14:15:01Z
dc.date.issued2013en_US
dc.date.submitted2013en_US
dc.identifier.urihttps://hdl.handle.net/2027.42/97795
dc.description.abstractQuantitatively accurate results from realistic Computational Fluid Dynamics (CFD) simulations are often accompanied by high computational expense. Higher-order methods are good candidates for providing accurate solutions at reduced cost. However, these methods are still not robust for industrial applications. This thesis presents a solution advancement method that improves robustness of discontinuous Galerkin (DG) discretizations in the iteration to steady-state. The method includes physical realizability constraints in the solution path and provides the solver with the ability of circumventing non-physical regions of the solution space that can occur during the solution transient. Affordable accurate solutions for challenging problems are obtained via output-based $hp$-adaptation. The adaptation method proposed in this thesis directly targets output error by locally choosing between subdividing an element or raising the approximation order. The decision is made by finding the refinement option that maximizes a merit function that involves output sensitivity and computational cost. Results in two and three dimensions show savings of up to an order of magnitude in terms of number of degrees of freedom and at least a factor of two in terms of computational time when compared to uniform refinement.en_US
dc.language.isoen_USen_US
dc.subjectComputational Fluid Dynamics CFDen_US
dc.subjectMesh Adaptationen_US
dc.subjectAdjoint Methoden_US
dc.subjectOutput Error Estimationen_US
dc.subjectDrag Prediction Workshopen_US
dc.subjectDiscontinuous Galerkinen_US
dc.titleA Robust hp-Adaptation Method for Discontinuous Galerkin Discretizations Applied to Aerodynamic Flows.en_US
dc.typeThesisen_US
dc.description.thesisdegreenamePhDen_US
dc.description.thesisdegreedisciplineAerospace Engineeringen_US
dc.description.thesisdegreegrantorUniversity of Michigan, Horace H. Rackham School of Graduate Studiesen_US
dc.contributor.committeememberFidkowski, Krzysztof J.en_US
dc.contributor.committeememberJohnsen, Ericen_US
dc.contributor.committeememberVan Leer, Bramen_US
dc.contributor.committeememberZingg, Daviden_US
dc.subject.hlbsecondlevelAerospace Engineeringen_US
dc.subject.hlbtoplevelEngineeringen_US
dc.description.bitstreamurlhttp://deepblue.lib.umich.edu/bitstream/2027.42/97795/1/mceze_1.pdf
dc.owningcollnameDissertations and Theses (Ph.D. and Master's)


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