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An assessment of the fast multipole method applied to a vortex sheet roll-up problem

dc.contributor.authorRicciardi, Tulio R.
dc.contributor.authorWolf, William R.
dc.contributor.authorBimbato, Alex M. [UNESP]
dc.contributor.institutionUniversidade Estadual de Campinas (UNICAMP)
dc.contributor.institutionUniversidade Estadual Paulista (UNESP)
dc.date.accessioned2022-04-28T19:27:23Z
dc.date.available2022-04-28T19:27:23Z
dc.date.issued2016-01-01
dc.description.abstractAerodynamic wakes of large aircraft and their induced velocity may cause serious hazards to smaller aircraft, affecting the take-off and landing operations in airports. A simplified but representative model of the problem is the evolution of a vortex sheet in the Trefftz plane. In this work, we employ the discrete vortex method (DVM) accelerated by the fast multipole method (FMM) to simulate this problem. Due to the cost associated with vortex clustering, the reduction in time from O(N2) to O(N) by the FMM is achieved when N is sufficiently large and a hierarchical multi-level multipole expansion is used. In the current paper, we show a study of the accuracy of the FMM compared to the Biot-Savart law when applied to the Trefftz plane simulation, which is shown to be a very sensitive non-linear problem where accuracy is a critical factor to avoid spurious instabilities. The analysis discusses the effects of time marching method, time step, level of refinement of the FMM, number of particles in the discretization and the balance between near and far-field computational costs. The DVM-FMM algorithm is also employed to solve the temporal evolution in a shear-layer with periodic boundary conditions.en
dc.description.affiliationDepartment of Energy Universidade Estadual de Campinas
dc.description.affiliationDepartment of Energy Universidade Estadual Paulista ‘Júlio de Mesquita Filho’
dc.description.affiliationUnespDepartment of Energy Universidade Estadual Paulista ‘Júlio de Mesquita Filho’
dc.identifierhttp://dx.doi.org/10.2514/6.2016-4173
dc.identifier.citation34th AIAA Applied Aerodynamics Conference.
dc.identifier.doi10.2514/6.2016-4173
dc.identifier.scopus2-s2.0-85067319523
dc.identifier.urihttp://hdl.handle.net/11449/221308
dc.language.isoeng
dc.relation.ispartof34th AIAA Applied Aerodynamics Conference
dc.sourceScopus
dc.titleAn assessment of the fast multipole method applied to a vortex sheet roll-up problemen
dc.typeTrabalho apresentado em evento

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