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  • Conference proceedings
  • © 2010

Summary of Flow Modulation and Fluid-Structure Interaction Findings

Results of the Collaborative Research Center SFB 401 at the RWTH Aachen University, Aachen, Germany, 1997-2008

  • Summary of Flow Modulation and Fluid-Structure Interaction Findings
  • Results of the Collaborative Research Center SFB 401 at the RWTH Aachen University, Aachen, Germany, 1997-2008
  • Written by experts in the field

Part of the book series: Notes on Numerical Fluid Mechanics and Multidisciplinary Design (NNFM, volume 109)

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Table of contents (15 papers)

  1. Front Matter

  2. Vortex Sheets of Aircraft in Takeoff and Landing

    • Robert Schöll, Rolf Henke, Günther Neuwerth
    Pages 1-23
  3. An Adaptive Implicit Finite Volume Scheme for Compressible Turbulent Flows about Elastic Configurations

    • Gero Schieffer, Saurya Ray, Frank Dieter Bramkamp, Marek Behr, Josef Ballmann
    Pages 25-51
  4. Timestep Control for Weakly Instationary Flows

    • Christina Steiner, Sebastian Noelle
    Pages 53-75
  5. Adaptive Multiscale Methods for Flow Problems: Recent Developments

    • Wolfgang Dahmen, Nune Hovhannisyan, Siegfried Müller
    Pages 77-103
  6. Interaction of Wing-Tip Vortices and Jets in the Extended Wake

    • Frank T. Zurheide, Guido Huppertz, Ehab Fares, Matthias Meinke, Wolfgang Schröder
    Pages 105-135
  7. Experimental and Numerical Investigation of Unsteady Transonic Airfoil Flow

    • Atef Alshabu, Viktor Hermes, Igor Klioutchnikov, Herbert Olivier
    Pages 137-151
  8. Enabling Technologies for Robust High-Performance Simulations in Computational Fluid Dynamics

    • Christian H. Bischof, H. Martin Bücker, Arno Rasch
    Pages 153-180
  9. Influencing Aircraft Wing Vortices

    • R. Hörnschemeyer, G. Neuwerth, R. Henke
    Pages 181-204
  10. Development of a Modular Method for Computational Aero-structural Analysis of Aircraft

    • Lars Reimer, Carsten Braun, Georg Wellmer, Marek Behr, Josef Ballmann
    Pages 205-238
  11. Parallel and Adaptive Methods for Fluid-Structure-Interactions

    • Josef Ballmann, Marek Behr, Kolja Brix, Wolfgang Dahmen, Christoph Hohn, Ralf Massjung et al.
    Pages 265-294
  12. Iterative Solvers for Discretized Stationary Euler Equations

    • Bernhard Pollul, Arnold Reusken
    Pages 295-323
  13. Structural Idealization of Flexible Generic Wings in Computational Aeroelasticity

    • J. A. Kengmogne Tchakam, H. -G. Reimerdes
    Pages 363-387
  14. Aero-structural Dynamics Experiments at High Reynolds Numbers

    • Josef Ballmann, Athanasios Dafnis, Arndt Baars, Alexander Boucke, Karl-Heinz Brakhage, Carsten Braun et al.
    Pages 389-424
  15. Back Matter

About this book

The Collaborative Research Center SFB 401: Flow Modulation and Fluid-Structure Interaction at Airplane Wings investigates numerically and experimentally fundamental problems of very high capacity aircraft having large elastic wings. This issue summarizes the findings of the 12-year research program at RWTH Aachen University which was funded by the Deutsche Forschungsgemeinschaft (DFG) from 1997 through 2008. The research program covered the following three main topics of large transport aircraft: (i) Model flow, wakes, and vortices of airplanes in high-lift-configuration, (ii) Numerical tools for large scale adaptive flow simulation based on multiscale analysis and a parametric mapping concept for grid generation, and (iii) Validated computational design tools based on direct aeroelastic simulation with reduced structural models.

Editors and Affiliations

  • RWTH Aachen University, Aachen, Germany

    Wolfgang Schröder

Bibliographic Information

Buy it now

Buying options

eBook USD 169.00
Price excludes VAT (USA)
  • Available as PDF
  • Read on any device
  • Instant download
  • Own it forever
Softcover Book USD 219.99
Price excludes VAT (USA)
  • Compact, lightweight edition
  • Dispatched in 3 to 5 business days
  • Free shipping worldwide - see info
Hardcover Book USD 219.99
Price excludes VAT (USA)
  • Durable hardcover edition
  • Dispatched in 3 to 5 business days
  • Free shipping worldwide - see info

Tax calculation will be finalised at checkout

Other ways to access