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Advances in Simulation of Wing and Nacelle Stall

Results of the Closing Symposium of the DFG Research Unit FOR 1066, December 1-2, 2014, Braunschweig, Germany

  • Conference proceedings
  • © 2016

Overview

Editors:
  1. Rolf Radespiel

    1. Institute of Fluid Mechanics, Technische Universität Braunschweig, Braunschweig, Germany

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  2. Reinhard Niehuis

    1. Institute of Jet Propulsion, Universität der Bundeswehr München, Neubiberg, Germany

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  3. Norbert Kroll

    1. Institute of Aerodynamics and Flow Technology, German Aerospace Center (DLR), Braunschweig, Germany

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  4. Kathrin Behrends

    1. Institute of Fluid Mechanics, Technische Universität Braunschweig, Braunschweig, Germany

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  • Reports on advanced findings in the field of flight simulation
  • Provides readers with a good balance of theories, models and experimental work
  • Offers a comprehensive report on the state-of-the-art in the field

Part of the book series: Notes on Numerical Fluid Mechanics and Multidisciplinary Design (NNFM, volume 131)

Included in the following conference series:

Conference proceedings info: FOR 1066 2014.

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Table of contents (24 papers)

  1. Front Matter

    Pages I-IX
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  2. Modelling

    1. Front Matter

      Pages 1-1
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    2. The Delay of RANS-to-LES Transition in Hybrid RANS-LES Approaches and Some Recently Proposed Remedies

      • Mikhail Strelets, Mikhail Shur, Andrey Travin, Philippe R. Spalart
      Pages 3-21

    3. Computations of Separated Flows with a Hybrid RANS/LES Approach

      • Daniela G. Francois, Rolf Radespiel, Silvia Reuß, Axel Probst
      Pages 23-39

    4. Hybrid RANS/LES Study of the Development of an Airfoil-Generated Vortex

      • Silvia Reuß, Axel Probst, Tobias Knopp, Katharina P. Wawrzinek
      Pages 41-54

    5. Interaction of Three-Dimensional Disturbances with the Flow Around a Two-Element High-Lift Airfoil

      • Simon Klein, Peter Scholz, Rolf Radespiel
      Pages 55-73

    6. The Discontinuous Galerkin Method as an Enabling Technology for DNS and LES of Industrial Aeronautical Applications

      • Koen Hillewaert, Corentin Carton de Wiart
      Pages 75-96

    7. Body Force Modelling of Internal Geometry for Jet Noise Prediction

      • James C. Tyacke, Iftekhar Z. Naqavi, Paul G. Tucker
      Pages 97-109

    8. Numerical Studies of Turbulent Flow Influence on a Two-Element Airfoil

      • Katharina P. Wawrzinek, Thorsten Lutz, Ewald Krämer
      Pages 111-135

    9. CFD for Prediction of Flow Separation from Aircraft Tail Surfaces

      • Andrea Masi, Jeremy Benton, Paul G. Tucker
      Pages 137-150

    10. Zonal RANS-LES Computation for Near-Stall-Airfoil Flow

      • Benedikt Roidl, Koen J. Geurts, Wolfgang Schröder
      Pages 151-164

  4. Inlet and Engine Flows

    1. Front Matter

      Pages 249-249
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    2. Integration- and Intake-Induced Flow Distortions and Their Impact on Aerodynamic Fan Performance

      • Rainer Schnell, Dirk Schönweitz, Marius Theune, Johakim Corroyer
      Pages 251-269

    3. Flow Investigations in a Stalling Nacelle Inlet Under Disturbed Inflow

      • Simon Übelacker, Rainer Hain, Christian J. Kähler
      Pages 271-283
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  1. Advances in Simulation of Wing and Nacelle Stall

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About this book

The book reports on advanced solutions to the problem of simulating wing and nacelle stall, as presented and discussed by internationally recognized researchers at the Closing Symposium of the DFG Research Unit FOR 1066. Reliable simulations of flow separation on airfoils, wings and powered engine nacelles at high Reynolds numbers represent great challenges in defining suitable mathematical models, computing numerically accurate solutions and providing comprehensive experimental data for the validation of numerical simulations. Additional problems arise from the need to consider airframe-engine interactions and inhomogeneous onset flow conditions, as real aircraft operate in atmospheric environments with often-large distortions. The findings of fundamental and applied research into these and other related issues are reported in detail in this book, which targets all readers, academics and professionals alike, interested in the development of advanced computational fluid dynamics modeling for the simulation of complex aircraft flows with flow separation.

Editors and Affiliations

  • Institute of Fluid Mechanics, Technische Universität Braunschweig, Braunschweig, Germany

    Rolf Radespiel, Kathrin Behrends

  • Institute of Jet Propulsion, Universität der Bundeswehr München, Neubiberg, Germany

    Reinhard Niehuis

  • Institute of Aerodynamics and Flow Technology, German Aerospace Center (DLR), Braunschweig, Germany

    Norbert Kroll

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