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debut(); ?>In the framework of this project, numerical simulations of the noise generation of a jet impinging on a flat plate are analysed, discussed and validated against measurements in an anechoic wind tunnel. The research topics contain : 1. Computation of the noise based on steady and unsteady CFD flow computations done by Robert Bosch GmbH using the commercial code CFX. Noise is computed with the high order Discontinuous Galerkin (DG) code of IAG, University Stuttgart, solving the Linearized Euler Equations (LEE) with source terms, and with the high order continuous Finite Element code of IRMA, Université Louis Pasteur, Strasbourg, solving the linear second order wave equation with suitable source terms. 2. Large Eddy Simulation (LES) of the flow problem by Prof. Schneider using a multi-resolution wavelet algorithm, comparison with the results obtained with CFX. 3. Critical comparison of the numerical results with noise measurements obtained in the anechoic wind tunnel of Robert Bosch GmbH. Participants: Project leaders: Prof. Dr. Claus-Dieter Munz, University of Stuttgart Prof. Dr. Kai Schneider, Université de Provence, Marseille M. Fischer (Robert Bosch GmbH) Project members: Dipl.-Ing. Marco Zucchini (Robert Bosch GmbH) Dipl.-Ing. Michael Dumbser (IAG, University of Stuttgart) Dipl.-Math. Sébastien Jund (IRMA, ULP, Strasbourg) Sponsor: Robert Bosch GmbH IAG, University of Stuttgart IRMA, ULP, Strasbourg} if ($t=="LOMOTU") { ?>
Participants: P. Comte (IMFS, Strasbourg) B. Noack (Berlin) Sponsor:} if ($t=="SHONO") { ?>
Participants: R. Friedrich (München) D. Juvé (Lyon) J. Sesterhenn (München) Sponsor:} if ($t=="FLUAC") { ?>
Participants: E. Frénod (Vannes) C.-D. Munz (Stuttgart) E. Sonnendrücker (Strasbourg) Sponsor:} if ($t=="SUBMOD") { ?>
Participants: C. Cambon( Lyon) M. Oberlack (Darmstadt) Sponsor:} if ($t=="MEACCO") { ?>
Two- and three-dimensional compressible direct numerical simulations (DNS) of the plane mixing layer considered by Colonius, Lele and Moin (J. Fluid Mech. 330) for two-dimensional flow evolution are performed for investigating the influence of base flow parameters and three-dimensionality on the resulting flow structures and noise generation. Especially, a simulation at very low Mach number is planned to gain data with the same code for a quasi-incompressible case, enabling a reliable comparison of the flow fields with respect to compressibility effects on the acoustic field, cf. the work of Seo & Moon, AIAA-2003-3270. As for noise control, sensitivity studies and control in open and closed-loop fashion are investigated using the adjoint set of equations. Participants: Airiau () M. Kloker (Stuttgart) U. Rist (Stuttgart) Sponsor:} if ($t=="NOPRE") { ?>
Participants: P. Comte (Strasbourg) W. Schröder (Aachen) M. Meinke (Aachen) Sponsor:} if ($t=="JETMIX") { ?>
Participants: M. Jacob (Lyon) F. Thiele (Berlin) Sponsor:} if ($t=="FVPART") { ?>
Participants: N. Adams (München) G.-H. Cottet Sponsor:} if ($t=="TUFLOW") { ?>
Participants: H. Bockhorn (Karlsruhe) M. Farge (Paris) K.Schneider (Marseille) Sponsor:} if ($t=="HYWAMO") { ?>
The objective of the present underlying French-German research project is the development of urgently required techniques in order to apply large-eddy simulation (LES) and its derivatives to high Reynolds number turbulent flows of practical interest. Two main development strategies are considered: * appropriate wall models in order to bridge the near-wall region and therefore allow high-Re simulations * non-zonal hybrid LES-RANS methods which split up the simulation (ideally not the domain) into a RANS part and an LES part The basic concept of the hybrid approach is to combine the advantages of both methods yielding an optimal solution at least for a special class of flows. A real non-zonal hybrid technique is preferred since it avoids the predefinition of RANS and LES regions leading to an approach where the suitable simulation technique is chosen more or less automatically. Although the idea of combined LES-RANS methods is not new, a variety of open questions has to be answered. This includes in particular the demand for appropriate coupling techniques between LES and RANS, adaptive control mechanisms, and proper SGS/RANS models. Since approximate wall boundary conditions partially rely on RANS modeling and the classical wall function is a limiting case of a RANS model in the near-wall region, both topics of the present proposal, i.e., wall modeling and LES-RANS coupling, are strongly interconnected. In order to investigate the open questions mentioned above, in the first step it is definitely inevitable to consider some geometrically simple test cases including pressure-induced flow separation and subsequent reattachment, e.g. test configuration T2, the flow over periodic hills. The final objectives of the entire project are, of course, flow configurations of practical interest including high-Re cases. Within the CEMRACS Research Center it is planned to work together on specific hybrid approaches (e.g. DES, SAS or something similar). The details will be fixed later in close agreement with all participants. The objectives are to exchange ideas and experiences made with hybrid approaches and to learn from each other. The project is open for external participants. In case of interest in participation, please send an e-mail to breuer@lstm.uni-erlangen. Project leaders: Michael Breuer (LSTM Erlangen) Christian Tenaud (LIMSI Orsay) Michel Visonneau (EC Nantes) Ganbo Deng (EC Nantes) Project members: Benoit Jaffrezic (LSTM Erlangen) Oussama Chikhaoui (EC Nantes) Sponsor:} if ($t=="BRENNUS") { ?>
Le couplage des équations de Maxwell - calcul du champ électromagnétique - en 2d cartésien, 2d axisymétrique et 3d, résolues par une méthode d'éléments finis d'arêtes avec les équations de Vlasov résolues par une méthode PIC - calcul des distributions en espace et vitesse des particules chargées. La prise en compte de la relation de continuité champs-courants-charges via une technique éprouvée et robuste (type Marder). La visualisation des champs et des particules avec des sorties adaptéss (utilisation de Open DX). Project leaders: Patrick Lacoste (CEA) E. Sonnendrücker (IRMA, ULP, Strasbourg). Project members: Regine Barthelme (IRMA, ULP, Strasbourg) Pierre Navaro (IRMA, ULP, Strasbourg) Sponsor: CEA} if ($t=="LERACO") { ?>
Participants: J. Fröhlich (Karlsruhe) T. H. Le (Onera, Châtillon) I. Mary (Onera, Châtillon) W. Rodi (Karlsruhe) Sponsor:} if ($t=="SWIFLO") { ?>
Participants: M. Buffat (Lyon) S. Jakirlic (Darmstadt) L. LePenven (Lyon) C. Tropea (Darmstadt) Sponsor:} if ($t=="WALAMO") { ?>
Participants: C. Brun (Orléans) M. Manhart (München) Sponsor:} if ($t=="SPECOM") { ?>
The purpose of the present project is the development, analysis, and application of a flexible pseudo-spectral method allowing LES with high accuracy and efficiency for complex practical turbulent flow problems. The project work will include the joint implementation of a corresponding pseudo-spectral code involving adequate dynamic subgrid models and advanced numerical techniques for the discretization and solution of the governing model equations. Special emphasis will be given to validation and verification aspects as well as a quality assurance with respect to numerical accuracy and efficiency. This will include investigations of basic question regarding the interaction of LES subgrid scale models with spectral discretizations. For comparisons results from other projects within the Research Group as well as results of direct numerical simulations for basic cases of complex flows inside generic geometries will be considered. Participants: P. Bontoux (Marseille) R. Pasquetti (Nice) M. Schäfer (Darmstadt) Project closed for external co-workers. Sponsor:} if ($t=="NOGEN") { ?>
Participants: W. Schröder (Aerodynamics Institute, Aachen) P. Comte (IMFS, Strasbourg) Grünewald (EADS) Sponsor: Aerodynamics Institute, Aachen University of Technology IMFS, Strasbourg EADS} if ($t=="NORED") { ?>
Participants: W. Schröder (Aachen) Sponsor: Aerodynamics Institute, Aachen University of Technology Lufthansa} if ($t=="PULPLA") { ?>
Participants: Project leaders: C.-D. Munz (IAG, Stuttgart), E. Sonnendrücker (IRMA, ULP, Strasbourg). Sponsor:} if ($t=="HOMAX") { ?>
Participants: Project leaders: C.-D. Munz (IAG, Stuttgart) E. Sonnendrücker (IRMA, ULP, Strasbourg). Sponsor: CEA} if ($t=="HOWAVE") { ?>
Participants: M. Dumbser (IAG, Stuttgart), C.-D. Munz (IAG, Stuttgart) Sponsor:} if ($t=="DENPIC") { ?>
Participants: B. Afeyan (Pleasanton, USA), J.-L. Stark (CEA Saclay), E. Sonnendrücker (Strasbourg) Sponsor: CEA} if ($t=="TWOSCA") { ?>
The aim of this project will be to develop a numerical method which is able to deal with two different space scales. The source term will be defined on the smaller scale and be localized in the simulation domain and the acoustic or electromagnetic waves will be propagating on the larger scale. The numerical method will be based on an idea of Rappaz and Wagner using two different finite element spaces for the two-scales. We shall adapt this idea to the Maxwell and acoustics equations using Raviart-Thomas-Nedelec finite elements. Participants: S. Jund (IRMA, ULP, Strasbourg), S. Salmon (IRMA, ULP, Strasbourg), E. Sonnendrücker (IRMA, ULP, Strasbourg) Sponsor : IRMA} ?>