New Results in Numerical and Experimental Fluid Mechanics III

1. Front Matter

   Pages I-XII

   PDF

2. High Aspect-Ratio Wings

   1. Front Matter

      Pages 1-1

      PDF

   2. Design Work for the A3XX High-Lift-Wing

      • D. Reckzeh

      Pages 3-10

   3. Recent Improvements in the Measurement of Aerodynamic Damping Derivatives

      • A.-R. Hübner, T. Löser

      Pages 11-18

   4. Calculation of Horizontal Stabilizer Efficiency with a Navier-Stokes Code

      • C. Nebel, D. Hummel

      Pages 19-26

   5. 3D RANS Simulations for High-Lift Analysis of Transport Aircraft Configurations

      • S. Melber

      Pages 27-34

   6. Numerical Investigation of the Reynolds-Number-Effect on the Setting Sensitivity of a 2D High-Lift Multi-Element Airfoil

      • J. Wild

      Pages 35-41

   7. Separation Control on a High-Lift Configuration by Periodic Exitation

      • F. Tinapp, W. Nitsche

      Pages 42-49

   8. Numerical Investigation of the Effect of the High-Lift Configuration of a Transport Aircraft on its Vortex Wake

      • E. Stumpf

      Pages 50-57

   9. The Relationship Between Near- and-Far-Field of Vortex Wakes from Aircraft with High Aspect Ratio Wings

      • R. Stuff

      Pages 58-65

   10. Influence of Different Flap Settings on the Hazard Posed to Following Aircraft

       • I. Schell, E. Özger, D. Jacob

       Pages 66-73

   11. Numerical Simulation of Wake-Vortex Encounters Using the Chimera-Technique

       • R. Heinrich

       Pages 74-81

   12. Aspects of Low Speed Wind Tunnel Testing on an A400M Model with Propeller Simulation

       • M. Huhnd, S. Schmid-Göller

       Pages 82-91

   13. Coupling of DLR Navier-Stokes Solver FLOWer with an eN-Database Method for Laminar-Turbulent Transition Prediction on Airfoils

       • A. Krumbein

       Pages 92-99

3. Low Aspect-Ratio Wings

   1. Front Matter

      Pages 101-101

      PDF

   2. Unsteady Measurements with the Continuously Rotating DLR-PSP-Model at the Transonic Wind Tunnel Göttingen (DNW-TWG)

      • M. Bruse, K.-W. Bock, S. Tusche, M. Jacobs

      Pages 103-110

4. Hypersonic Flows

   1. Front Matter

      Pages 111-111

      PDF

   2. Turbulence Modeling for Reentry-Vehicles

      • C. Weber, R. Behr, C. Weiland

      Pages 113-120

   3. Computation of the Two-Dimensional Flow in SERN Nozzles

      • Thomas Link, Wolfgang W. Koschel

      Pages 121-128

   4. Experimental Investigation of a Hypersonic Inlet for the TSTO-Configuration ELAC

      • R. Neubacher, A. Henckels, T. Gawehn

      Pages 129-136

This volume contains the papers of the 12. Symposium of the STAB (German Aerospace Aerodynamics Association). In this association, german scientists and engineers from universities, research-establishments and industry are involved, who are doing research and project work in numerical and experimental fluidmechanics and aerodynamics for aerospace and other applications. Many of the contributions give results from the "Luftfahrt- forschungsprogram der Bundesregierung (German Aeronautical Research Program)". Some of the papers report on work sponsored by the Deutsche Forschungsgemeinschaft, DFG, who were also present at the symposium. This volume gives a broad overview of the ongoing work in this field in Germany.

• Aerodynamics
• Analytical Methods
• Experimental Fluid Mechanics
• Numerical Methods
• Windtunnels
• fluid mechanics
• simulation
• turbulence
• turbulent flow
• fluid- and aerodynamics

• Institut für Aerodynamik und Gasdynamik, Universität Stuttgart, Stuttgart, Germany

  Siegfried Wagner, Ulrich Rist

• DLR, Göttingen, Germany

  Hans-Joachim Heinemann

• Technology Programmes “Flight Physics”, DaimlerChrysler Aerospace Airbus, Bremen, Germany

  Reinhard Hilbig

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