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New Results in Numerical and Experimental Fluid Mechanics V

Contributions to the 14th STAB/DGLR Symposium Bremen, Germany 2004

  • Conference proceedings
  • © 2006

Overview

Editors:
  1. Hans-Josef Rath

    1. ZARM - University of Bremen Am Fallturm/Hochschulring, Bremen

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  2. Carsten Holze

    1. ZARM - University of Bremen Am Fallturm/Hochschulring, Bremen

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  3. Hans-Joachim Heinemann

    1. Aerospace Science and Technology, AST, DLR, Götingen

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  4. Rolf Henke

    1. Airbus Deutschland GmbH, Bremen

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  5. Heinz Hönlinger

    1. DLR - AE, Göttingen

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  • All about new results in Aerospace in Germany

Part of the book series: Notes on Numerical Fluid Mechanics and Multidisciplinary Design (NNFM, volume 92)

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Table of contents (64 papers)

  1. Front Matter

    Pages I-XIV
    Download chapter PDF

  2. High Aspect-Ratio Wings

    1. High Reynolds-Number Windtunnel Testing for the Design of Airbus High-Lift Wings

      • Daniel Reckzeh, Heinz Hansen
      Pages 1-8

    2. Aerodynamic Analysis of Flows with Low Mach- and Reynolds-Number under Consideration and Forecast of Transition on the Example of a Glider

      • S. Melber-Wilkending, G. Schrauf, M. Rakowitz
      Pages 9-16

    3. Analysis of PIV Flow Measurements behind the ALVAST-Model in High-Lift Configuration

      • H. Vollmers, W. Puffert-Meissner, A. Schröder
      Pages 17-24

    4. Effect of Differential Flap Settings on the Wake Vortex Evolution of Large Transport Aircraft

      • C. Bellastrada, C. Breitsamter
      Pages 25-32

    5. Investigations on the Influence of Fins on the Extended Nearfield of a Wing inHigh-Lift Configuration

      • Sebastian Kauertz, Giinther Neuwerth, Robert Schüll
      Pages 33-40

    6. Application of the PSP Technique in Low Speed Wind Tunnels

      • U. Henne
      Pages 41-49

    7. Investigation of tailplane stall for a generic transport aircraft configuration

      • Arne Grote, Rolf Radespiel
      Pages 50-58

    8. Numerical analysis of transport aircraft using different wing tip devices

      • TH. Streit, A. Ronzheimer, A. BüScher
      Pages 59-68

    9. Aerodynamic Optimisation of a Flying Wing Transport Aircraft

      • H. Strüber, M. Hepperle
      Pages 69-76

  3. Low Aspect-Ratio Wings

    1. Delta Wing Steady Pressure Investigations for Sharp and Rounded Leading Edges

      • Andrej Furman, Christian Breitsamter
      Pages 77-84

    2. Computation of Delta Wing Flap Oscillations with a Reynolds-Averaged Navier-Stokes Solver

      • Alexander Allen, Michail Iatrou, Alexander Pechloff, Boris Laschka
      Pages 85-93

    3. Experimental study on the Flowfield of a Delta-Canard-Configuration with Deflected Leading Edge

      • A. Schmid, C. Breitsamter
      Pages 94-102

    4. Numerical simulation of maneuvering combat aircraft

      • Andreas Schütte, Gunnar Einarsson, Britta Schöning, Axel Raichle, Thomas Alrutz, Wulf Mönnich et al.
      Pages 103-111

    5. Experimental investigation on periodic rolling of a delta wing flow at transonic Mach numbers

      • B. Gölling, O. Erne
      Pages 112-119

    6. Numerical Design of a Low-Noise High-Lift System for a Supersonic Aircraft

      • U. Herrmann
      Pages 120-127
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Keywords

About this book

This volume contains the contributions to the 14. Symposium of the STAB (German Aerospace Aerodynamics Association). In this association all those German scientists and engineers from universities, research establishments and industry are involved, who are doing research and project work in numerical and experimental fluid mechanics and aerodynamics, mainly for aerospace but for other applications, too. Many of the contributions are presenting results from national and European Community sponsored projects. The volume gives a broad overview over the ongoing work in this field in Germany, with the topics being high-aspect ratio wings, low aspect-ratio wings, bluff bodies, laminar flow control and transition, active flow control, hypersonic flows, aeroelasticity, aeroacoustics, mathematical fundamentals/ numerical simulation, physical fundamentals, and facilities.

Editors and Affiliations

  • ZARM - University of Bremen Am Fallturm/Hochschulring, Bremen

    Hans-Josef Rath, Carsten Holze

  • Aerospace Science and Technology, AST, DLR, Götingen

    Hans-Joachim Heinemann

  • Airbus Deutschland GmbH, Bremen

    Rolf Henke

  • DLR - AE, Göttingen

    Heinz Hönlinger

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