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Flow Modulation and Fluid—Structure Interaction at Airplane Wings

Research Results of the Collaborative Research Center SFB 401 at RWTH Aachen, University of Technology, Aachen, Germany

  • Josef Ballmann

Table of contents

  1. Front Matter
    Pages I-X
  2. Introduction

    1. Josef Ballmann
      Pages 1-3
  3. Model Flow, Wakes and Vortices in High Lift Configuration

    1. Front Matter
      Pages 5-5
    2. Erol Özger, Ingmar Schell, Dieter Jacob
      Pages 7-38
    3. Ingmar Schell, Erol Özger, Dieter Jacob
      Pages 39-56
    4. E. Fares, W. Schröder
      Pages 57-84
    5. A. Meijering, W. Limberg, W. Schröder
      Pages 85-103
  4. Numerical Tools and Approaches for Flow Simulation with Local Adaptivity

    1. Front Matter
      Pages 123-123
    2. F. Bramkamp, M. Hesse, J. Ballmann, B. Gottschlich-Müller, Ph. Lamby, S. Müller et al.
      Pages 125-204
    3. Christian H. Bischof, H. Martin Bicker, Bruno Lang, Arno Rasch
      Pages 205-224
  5. Computational and Experimental Aeroelasticity

    1. Front Matter
      Pages 225-225
    2. Ralf Massjung, Jörg Hurka, Wolfgang Dahmen, Josef Ballmann
      Pages 227-247
    3. G. Britten, C. Braun, M. Hesse, J. Ballmann
      Pages 275-299
    4. N. Siepenkötter, W. Kasberg, W. Alles
      Pages 301-322
    5. X. Bertrán, H. Olivier, S. Turek
      Pages 323-350
    6. C. Hillenherms, W. Schröder, W. Limberg
      Pages 351-376
    7. M. Kämpchen, H. Korsch, A. Dafnis, H.-G. Reimerdes
      Pages 377-396
  6. Back Matter
    Pages 397-398

About these proceedings

Introduction

This volume presents results of the interdisciplinary research work from the collaborative research center SFB 401: "Flow Modulation and Fluid-Structure Interaction at Airplane Wings" at RWTH Aachen, Germany The research reported here comprises work from the first five years of its funding by the Deutsche Forschungsgemeinschaft, DFG. The center is concerned with fundamental problems of very high capacity aircraft with large elastic wings capable of transonic transport. In all of the 14 projects to date, the following laboratories have cooperated: Aircraft Design and Aeronautics, Aerodynamics, Lightweight Structures, Flight Dynamics, Geometry and Practical Mathematics, Numerical Mathematics, Scientific Computing and Mechanics. The work is still in progress and presently approved to continue until the end of 2005.

Keywords

Adaptive Multiscale Schemes for Aerodynamics Automated Differentiation Computational and Experimental Aeroelasticity Dynamics Experimental High Speed Aeropdynamics at High Reynolds Numbe High-Lift Configurations aerodynamics aircraft design mathem

Editors and affiliations

  • Josef Ballmann
    • 1
  1. 1.Lehr- und Forschungsgebiet MechanikRWTH AachenAachenGermany

Bibliographic information

  • DOI https://doi.org/10.1007/978-3-540-44866-2
  • Copyright Information Springer-Verlag Berlin Heidelberg 2003
  • Publisher Name Springer, Berlin, Heidelberg
  • eBook Packages Springer Book Archive
  • Print ISBN 978-3-642-53613-7
  • Online ISBN 978-3-540-44866-2
  • Series Print ISSN 1612-2909
  • Series Online ISSN 1860-0824
  • Buy this book on publisher's site
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