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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

  • Conference proceedings
  • © 2003

Overview

Editors:
  1. Josef Ballmann

    1. Lehr- und Forschungsgebiet Mechanik, RWTH Aachen, Aachen, Germany

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  • Large Wing Aerodynamics and Aeroelasticity
  • Includes supplementary material: sn.pub/extras

Part of the book series: Notes on Numerical Fluid Mechanics and Multidisciplinary Design (NNFM, volume 84)

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Table of contents (16 papers)

  1. Front Matter

    Pages I-X
    Download chapter PDF

  2. Introduction

    1. Introduction

      • Josef Ballmann
      Pages 1-3

  3. Model Flow, Wakes and Vortices in High Lift Configuration

    1. Front Matter

      Pages 5-5
      Download chapter PDF

    2. Experimental Analysis and Modulation of Vortices

      • Erol Özger, Ingmar Schell, Dieter Jacob
      Pages 7-38

    3. Simulation of Vortex Sheets at Take-Off and Landing

      • Ingmar Schell, Erol Özger, Dieter Jacob
      Pages 39-56

    4. Analysis of Wakes and Wake-Jet Interaction

      • E. Fares, W. Schröder
      Pages 57-84

    5. Aerodynamic Design of Transonic Adaptive Airfoils with Natural Transition

      • A. Meijering, W. Limberg, W. Schröder
      Pages 85-103

    6. Experiments in a Transonic Shock Tube at Subsonic Mach and High Reynolds Numbers

      • Th. Reichel, M. Zechner, H. Olivier
      Pages 105-122

  4. Numerical Tools and Approaches for Flow Simulation with Local Adaptivity

    1. Front Matter

      Pages 123-123
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    2. H-Adaptive Multiscale Schemes for the Compressible Navier-Stokes Equations — Polyhedral Discretization, Data Compression and Mesh Generation

      • F. Bramkamp, M. Hesse, J. Ballmann, B. Gottschlich-Müller, Ph. Lamby, S. Müller et al.
      Pages 125-204

    3. Automated Gradient Calculation

      • Christian H. Bischof, H. Martin Bücker, Bruno Lang, Arno Rasch
      Pages 205-224

  5. Computational and Experimental Aeroelasticity

    1. Front Matter

      Pages 225-225
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    2. On Well-Posedness and Modelling for Nonlinear Aeroelasticity

      • Ralf Massjung, Jörg Hurka, Wolfgang Dahmen, Josef Ballmann
      Pages 227-247

    3. Concepts for Reduced Structural Models of Airplane Wings in Aeroelasticity

      • W. Jung, H.-G. Reimerdes
      Pages 249-273

    4. Computational Aeroelasticity with Reduced Structural Models

      • G. Britten, C. Braun, M. Hesse, J. Ballmann
      Pages 275-299

    5. Approximated Nonlinear Stability Analysis of the Dynamics of Flexible Aircraft

      • N. Siepenkötter, W. Kasberg, W. Alles
      Pages 301-322

    6. Analysis of Unsteady Airfoils at Low Speeds

      • X. Bertrán, H. Olivier, S. Turek
      Pages 323-350

    7. Experiments on Transonic Aerodynamics about Elastically Suspended Airfoils

      • C. Hillenherms, W. Schröder, W. Limberg
      Pages 351-376

    8. Design, Qualification and Experimental Investigation on Flexible Wind Tunnel Wing Models

      • M. Kämpchen, H. Korsch, A. Dafnis, H.-G. Reimerdes
      Pages 377-396

    9. Correction to: Automated Gradient Calculation

      • Josef Ballmann
      Pages C1-C1
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Keywords

About this book

The research work of the collaborative research center SFB401 Flow Modulation and Fluid-Structure Interaction at Airplane Wings at the Rheinisch-Westfälische Technische Hochschule (RWTH) Aachen, which is reported in this book, was pos­ sible due to the financial support of the Deutsche Forschungsgemeinschaft (DFG). The proposal has been approved after evaluation by the referees of DFG selected from other universities and industry, which is gratefully acknowledged. The work is still in progress and now approved to continue until the end of year 2005. More than 50 scientists from universities of the United States, Russia, France, Italy, Japan, Great Britain, Sweden, Netherlands, Switzerland, Austria and research orga­ nizations NASA, ONERA, NLR, DLR could be invited and have visited the research center, gave seminars on their research on related topics and some of them stayed longer for joined work. Besides its scientific value, also the importance of the pro gram for scientific educa­ tion becomes evident by looking at the numbers of completed theses, which are up to now about 15 doctoral theses, 40 diploma theses and 70 study theses. The authors of this book acknowledge the valuable support coming from all these persons and institutions. They are especially grateful to the referees having reviewed this work, A. Cohen (Universite Pierre et Marie Curie), J. Cooper (Manchester School of Engineering), W. Devenport (Virginia Tech.), M. Drela (MIT), F. Gern (Avionics Specialties Inc.), A. Griewank (TU Dresden), H. Hönlinger (DLR), P.

Editors and Affiliations

  • Lehr- und Forschungsgebiet Mechanik, RWTH Aachen, Aachen, Germany

    Josef Ballmann

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