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New Results in Numerical and Experimental Fluid Mechanics VI

Contributions to the 15th STAB/DGLR Symposium Darmstadt, Germany 2006

  • Conference proceedings
  • © 2008

Overview

Editors:
  1. Cameron Tropea

    1. TU Darmstadt, Darmstadt, Germany

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  2. Suad Jakirlic

    1. TU Darmstadt, Darmstadt, Germany

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  3. Hans-Joachim Heinemann

    1. DLR, Göttingen, Germany

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  4. Rolf Henke

    1. RWTH Aachen, Aachen, Germany

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  5. Heinz Hönlinger

    1. DLR - AE, Göttingen, Germany

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  • Contributions to the 15.
  • Symposium of the STAB (German Aero-space Aerodynamics Association)

Part of the book series: Notes on Numerical Fluid Mechanics and Multidisciplinary Design (NNFM, volume 96)

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Table of contents (57 papers)

  1. Front Matter

    Pages I-XIV
    Download chapter PDF

  2. Airplane Acrodynamics

    1. An Airbrake Design Methodology for Steep Approaches

      • B. Anil Mertol
      Pages 1-8

    2. High-Reynolds-Number Design of a Wing Section Including Control of Boundary Layer Properties

      • K. Richter, S. Koch, H. Rosemann
      Pages 9-16

    3. Numerical Analysis of Wing Vortices

      • Frank Zurheide, Wolfgang Schröder
      Pages 17-25

    4. Studies on Tailplane Stall for a Generic Transport Aircraft Wind Tunnel Model

      • Arne Grote, Rolf Radespiel
      Pages 26-35

    5. URANS and DES Simulation of Flow Around a Rectangular Cylinder

      • Claudio Mannini, Ante Soda, Ralph Voß, Günter Schewe
      Pages 36-43

    6. Active Manipulation of a Rectangular Wing Vortex Wake with Oscillating Ailerons and Winglet-Integrated Rudders

      • Ralf Hörnschemeyer, Christoph Rixen, Sebastian Kauertz, Günther Neuwerth, Rolf Henke
      Pages 44-51

    7. A New Actuator Disk Model for the TAU Code and Application to a Sailplaine with a Folding Engine

      • Axel Raichle, Stefan Melber-Wilkending, Jan Himisch
      Pages 52-61

    8. Design of a Retrofit Winglet for a Transport Aircraft with Assessment of Cruise and Ultimate Structural Loads

      • Th. Streit, J. Himisch, R. Heinrich, B. Nagel, K.H. Horstmann, C. Liersch
      Pages 62-70

  3. Flow Control

    1. Numerical Simulation of a Wing with a Gapless High-Lift System Using Circulation Control

      • K.-C. Pfingsten, R. Radespiel
      Pages 71-79

    2. Shock Control Bumps on Flexible and Trimmed Transport Aircraft in Transonic Flow

      • Benedikt König, Martin Pätzold, Thorsten Lutz, Ewald Krämer
      Pages 80-87

    3. A Flat Plate Experiment for Investigations of Vortex Generator Jets at High Reynolds Number

      • Jens Ortmanns, Christian J. Kähler, Rolf Radespiel
      Pages 88-95

  4. Experimental Simulation and Test Techniques

    1. Measurement of Unsteady Surface Forces by Means of Piezoelectrical Copolymer Coatings

      • J. Domhardt, J. Leuckert, I. Peltzer, W. Nitsche
      Pages 96-103

    2. Studies of Reynolds Number Effects on Wing Tip Vortex Positions by Means of Laser Light Sheet (LLS) and Background Oriented Schlieren (BOS) Technique Under Cryogenic Conditions

      • D. Pallek, F. Klinge
      Pages 104-112

    3. Project ForMEx — A New CFD Approach for Transposition of Wind Tunnel Data Towards Flight Conditions

      • Stefan Melber-Wilkending, Georg Wichmann
      Pages 113-120

    4. Pressure and Heat Flux Measurements on the Surface of a Low-Aspect-Ratio Circular Cylinder Mounted on a Ground Plate

      • T. Rödiger, H. Knauss, U. Gaisbauer, E. Krämer
      Pages 121-128

    5. An Investigation into Internal and External Force Balance Configurations for Short Duration Wind Tunnels

      • Matthew Robinson, Jan Martinez Schramm, Klaus Hannemann
      Pages 129-136
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Keywords

About this book

This volume contains the contributions to the 15. Symposium of the STAB (German Aero-space 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

  • TU Darmstadt, Darmstadt, Germany

    Cameron Tropea, Suad Jakirlic

  • DLR, Göttingen, Germany

    Hans-Joachim Heinemann

  • RWTH Aachen, Aachen, Germany

    Rolf Henke

  • DLR - AE, Göttingen, Germany

    Heinz Hönlinger

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