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Assaad, W. (author), Pasaribu, H.R. (author), Zijsling, DJ (author), van Dalen, K.N. (author), Metrikine, A. (author)Shell has developed a novel monodiameter well concept for oil and gas wells as opposed to the traditional telescopic well design. A Mono diameter well contains multiple casing sections with the same internal diameter. This is achieved by expansion of the casing sections concerned using an expansion cone. Since the well is drilled in stages and...conference paper 2017
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Fernandes, O. (author), Blom, D.S. (author), Frey, S. (author), Van Zuijlen, A.H. (author), Bijl, H. (author), Ertl, T. (author)We present an integrated insitu visualization approach for partitioned multiphysics simulation of fluidstructure interaction. The simulation itself is treated as a black box and only the information at the fluidstructure interface is considered, and communicated between the fluid and solid solvers with a separate coupling tool. The...conference paper 2015
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Blom, D.S. (author), Van Zuylen, A.H. (author), Bijl, H. (author)Strongly coupled partitioned fluidstructure interaction problems require multiple coupling iterations per time step. The fluid domain and the structure domain are solved multiple times in each time step such that the kinematic and dynamic interface conditions on the fluidstructure interface are satisfied. QuasiNewton methods have been...conference paper 2014
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Scholcz, T.P. (author), Van Zuijlen, A.H. (author), Bijl, H. (author)The focus of this paper is on acceleration of strong partitioned coupling algorithms for fluidstructure interaction. Strong partitioned coupling requires the solution of a coupled problem at each time step during the simulation. Hereto, an interface residual is defined such that the kinematic and dynamic interface conditions on the fluid...conference paper 2012
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Coarse level NewtonKrylov acceleration of subiterations in partitioned fluidstructure interactionVan Zuijlen, A.H. (author), Bijl, H. (author)Computational fluidstructure interaction is commonly performed using a partitioned approach. For strongly coupled problems subiterations are required, increasing computational time as flow and structure have to be resolved multiple times every time step. Reductions in computing times can be achieved by e.g. improving the convergence of the sub...conference paper 2011
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Sterenborg, J.J.H.M. (author), Van Zuijlen, A.H. (author), Bijl, H. (author)In order to validate fluidstructure interaction solvers, a one degree of freedom (1 DOF) aeroelastic experiment is performed. A rigid wing with an harmonically actuated flap, is suspended by springs to allow a free heaving motion. Displacements and time dependent aerodynamic forces are measured for reduced flap frequencies ranging from k = 0.1...conference paper 2011
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Kreeft, J.J. (author), Weghs, M. (author), Van Zuijlen, A.H. (author), Bijl, H. (author)Two reduced order models are presented for the simulation of physically strong coupled fluidstructure interaction problem, based on computationally partitioned flow and structure solvers. The reduced order models used are a class of quasiNewton coupling methods to obtain a stable solution and to reduce the number of subiterations. The second...conference paper 2011
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Scholcz, T.P. (author), Van Zuijlen, A.H. (author), Bijl, H. (author)High fidelity analysis of fluidstructure interaction systems is often too timeconsuming when a large number of model evaluations are required. The choice for a solution procedure depends often on the efficiency of the method and the possibility of reusing existing field solvers. Aggressive SpaceMapping, a technique originally developed for...conference paper 2011
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Witteveen, J.A.S. (author), Bijl, H. (author)A robust and efficient uncertainty quantification method is presented for resolving the effect of uncertainty on the behavior of multiphysics systems. The extrema diminishing method in probability space maintains a bounded error due to the interpolation of deterministic samples at constant phase in a transonic airfoil flutter problem.conference paper 2009
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Michler, A.K. (author), Dwight, R.P. (author), Heinrich, R. (author)The accurate prediction of the aerodynamic coefficients under cruise conditions is of major importance for assessing the aircraft’s fuel consumption. To this end, fluid dynamics, structural mechanics and flight mechanics have to be considered: on the one hand, the structure elastically deforms under the influence of the flow and a state of...conference paper 2009
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Witteveen, J.A.S. (author), Bijl, H. (author)An explicit mesh motion algorithm based on inverse distance weighting interpolation is presented. The explicit formulation leads to a fast mesh motion algorithm and an easy implementation. In addition, the proposed pointbypoint method is robust and flexible in case of large deformations, hanging nodes, and parallelization. Mesh quality results...conference paper 2009
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 Witteveen, J.A.S. (author), Bijl, H. (author) conference paper 2008
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Wendland, H. (author)This paper gives a survey on kernelbased scattered data interpolation methods in the context of static aeroelastic computations. We describe the general procedure, address problems and solutions for largescale data sets, for flat data sets, and for rotational information. Finally, we demonstrate the versatility of the method by showing two...conference paper 2006
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Murea, C.M. (author), Vazquez, C. (author)We study the fluidstructure coupled problem between an incompressible fluid and an elastic curved arch. The fluid flow is modeled by 2D steady Stokes equations with normal velocity boundary condition on the curved interface and the arch verifies a particular 1D case of the thin shell theory of Koiter. We present an optimal control formulation...conference paper 2006
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Förster, C. (author), Wall, W.A. (author), Ramm, E. (author)The artificial added mass effect inherent in sequentially staggered coupling schemes is investigated by means of a fluidstructure interaction problem. A discrete representation of a simplified added mass operator in terms of the participating coefficient matrices is given and instability conditions are evaluated for different temporal...conference paper 2006
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De Boer, A. (author), Van der Schoot, M.S. (author), Bijl, H. (author)A new pointbypoint mesh movement algorithm is developed for the deformation of unstructured grids. The method is based on using radial basis function, RBFs, to interpolate the displacements of the boundary nodes to the whole flow mesh. A small system of equations has to be solved, only involving the nodes on the boundary of the flow domain....conference paper 2006
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Loeven, A. (author), Witteveen, J.A.S. (author), Bijl, H. (author)In this paper a Two Step approach with Chaos Collocation for efficient uncertainty quantification in computational fluidstructure interactions is followed. In Step I, a Sensitivity Analysis is used to efficiently narrow the problem down from multiple uncertain parameters to one parameter which has the largest influence on the solution. In Step...conference paper 2006
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Van der Zee, K.G. (author), Van Brummelen, E.H. (author), De Borst, R. (author)Numerical simulations of fluidstructure interaction typically require vast computational resources. Finiteelement techniques employing goaloriented hpadaptation strategies could offer a substantial improvement in the efficiency of such simulations. These strategies rely on dualbased aposteriori error estimates for quantities of interest....conference paper 2006
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Gerstenberger, A. (author), Wall, W.A. (author)This paper illustrates aspects of an ongoing effort to develop a fixed grid fluidstructure interaction scheme that can be applied to the interaction of most general structures with incompressible flow. After presenting a list of requirements for future fixed grid methods, an eXtended Finite Element Method (XFEM) based fixed grid method is...conference paper 2006
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Hron, J. (author), Turek, S. (author)We investigate a monolithic algorithm to solve the problem of time dependent interaction between an incompressible viscous fluid and an elastic solid. The continuous formulation of the problem and its discretization is done in a monolithic way, treating the problem as one continuum. The Q2/P1 finite elements are used for the discretization and...conference paper 2006
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