HEAL DSpace

Continuous adjoint approach to the Spalart-Allmaras turbulence model for incompressible flows

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dc.contributor.author Zymaris, AS en
dc.contributor.author Papadimitriou, DI en
dc.contributor.author Giannakoglou, KC en
dc.contributor.author Othmer, C en
dc.date.accessioned 2014-03-01T01:30:01Z
dc.date.available 2014-03-01T01:30:01Z
dc.date.issued 2009 en
dc.identifier.issn 0045-7930 en
dc.identifier.uri https://dspace.lib.ntua.gr/xmlui/handle/123456789/19458
dc.subject Adjoint Method en
dc.subject Boundary Condition en
dc.subject Differential Equation en
dc.subject Incompressible Flow en
dc.subject Integral Functional en
dc.subject Loss Function en
dc.subject Reference Value en
dc.subject Reynolds Number en
dc.subject Turbulence Model en
dc.subject spalart allmaras en
dc.subject.classification Computer Science, Interdisciplinary Applications en
dc.subject.classification Mechanics en
dc.subject.other DISCRETE ADJOINT en
dc.subject.other UNSTRUCTURED GRIDS en
dc.subject.other DESIGN en
dc.subject.other OPTIMIZATION en
dc.subject.other FORMULATION en
dc.title Continuous adjoint approach to the Spalart-Allmaras turbulence model for incompressible flows en
heal.type journalArticle en
heal.identifier.primary 10.1016/j.compfluid.2008.12.006 en
heal.identifier.secondary http://dx.doi.org/10.1016/j.compfluid.2008.12.006 en
heal.language English en
heal.publicationDate 2009 en
heal.abstract A continuous adjoint formulation for the computation of the sensitivities of integral functions used in steady-flow, incompressible aerodynamics is presented. Unlike earlier continuous adjoint methods, this paper computes the adjoint to both the mean-flow and turbulence equations by overcoming the frequently made assumption that the variation in turbulent viscosity can be neglected. The development is based on the Spalart-Allmaras turbulence model, using the adjoint to the corresponding differential equation and boundary conditions. The proposed formulation is general and can be used with any other integral function. Here, the continuous adjoint method yielding the sensitivities of the total pressure loss functional for duct flows with respect to the normal displacements of the solid wall nodes is presented. Using three duct flow problems, it is demonstrated that the adjoint to the turbulence equations should be taken into account to compute the sensitivity derivatives of this functional with high accuracy. The so-computed derivatives almost coincide with "reference" sensitivities resulting from the computationally expensive direct differentiation. This is not, however, the case of the sensitivities computed without solving the turbulence adjoint equation, which deviates from the reference values. The role of all newly appearing terms in the adjoint equations, their boundary conditions and the gradient expression is investigated, significant and insignificant terms are identified and a study on the Reynolds number effect is included. (C) 2008 Elsevier Ltd. All rights reserved. en
heal.publisher PERGAMON-ELSEVIER SCIENCE LTD en
heal.journalName COMPUTERS & FLUIDS en
dc.identifier.doi 10.1016/j.compfluid.2008.12.006 en
dc.identifier.isi ISI:000267201100004 en
dc.identifier.volume 38 en
dc.identifier.issue 8 en
dc.identifier.spage 1528 en
dc.identifier.epage 1538 en


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