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dc.contributor.authorAmorim, José Carlos C.-
dc.contributor.authorAzevedo, João Luiz F.-
dc.identifier.citationAmerican Society of Mechanical Engineers, Fluids Engineering Division (Publication) FED, v. 237, p. 659-663.-
dc.description.abstractThis paper presents a viscous three-dimensional simulations coupling Euler and boundary layer codes for calculating flows over arbitrary surfaces. The governing equations are written in a general non orthogonal coordinate system. The Levy-Lees transformation generalized to three-dimensional flows is utilized. The inviscid properties are obtained from the Euler equations using the Beam and Warming implicit approximate factorization scheme. The resulting equations are discretized and approximated by a two-point fmitedifference numerical scheme. The code developed is validated and applied to the simulation of the flowfield over aerospace vehicle configurations. The results present good correlation with the available data.en
dc.subjectAerospace vehicles-
dc.subjectApproximation theory-
dc.subjectBoundary layers-
dc.subjectComputer simulation-
dc.subjectEquations of motion-
dc.subjectFinite difference method-
dc.subjectMathematical transformations-
dc.subjectThree dimensional-
dc.subjectEuler equation-
dc.subjectFactorization method-
dc.subjectLevy-Lees transformation-
dc.subjectNon orthogonal coordinate system-
dc.subjectViscous flow-
dc.titleNumerical simulation of viscous three-dimensional flow over aerospace vehicles using Euler/boundary-layer zonal approachen
dc.contributor.institutionUniversidade Estadual Paulista (UNESP)-
dc.description.affiliationUNESP-FEG, 12500-000 Guaratinguetá, S.P.-
dc.description.affiliationCTA-IAE, 12228-904 Sao Jose dos Campos, S. P.-
dc.description.affiliationUnespUNESP-FEG, 12500-000 Guaratinguetá, S.P.-
dc.rights.accessRightsAcesso restrito-
dc.relation.ispartofAmerican Society of Mechanical Engineers, Fluids Engineering Division (Publication) FED-
Appears in Collections:Artigos, TCCs, Teses e Dissertações da Unesp

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