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  • Conference proceedings
  • © 2004

New Results in Numerical and Experimental Fluid Mechanics IV

Contributions to the 13th STAB/DGLR Symposium Munich, Germany 2002

  • Broad overview about ongoing work and results in Aerospace in Germany
  • Collected results of project work in numerical and experimental aerodynamics and fluidmechanics for aerospace and other applications
  • Includes supplementary material: sn.pub/extras

Part of the book series: Notes on Numerical Fluid Mechanics and Multidisciplinary Design (NNFM, volume 87)

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Table of contents (59 papers)

  1. Front Matter

    Pages I-XIII
  2. Wake vortex and Configurations

    1. Large Transport Aircraft Wake Vortex Affected by Vortex Devices

      • C. Bellastrada, C. Breitsamter
      Pages 1-9
    2. Environmental Friendly Transport Aircraft

      • Martin Hepperle
      Pages 26-33
  3. Numerical Simulation

    1. DLR τ-Code for High Enthalpy Flows

      • Bodo Reimann, Ian Johnston, Volker Hannemann
      Pages 99-106
  4. Low Aspect-Ratio Wings

    1. High Incidence Buffet Flow over Fighter Type Aircraft

      • Arne Schmid, Christian Breitsamter
      Pages 107-115
    2. Flap efficiency of a delta wing with an external store using an Euler code for small disturbances

      • Alexander Allen, Caroline Weishäupl, Boris Laschka
      Pages 116-123
  5. Laminar Flow Control and Transition

About this book

This volume contains 59 papers presented at the 13th Symposium of 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 also in other applications. Many of the contributions give results from federal and European-Union sponsored projects. The volume gives a broad overview of the ongoing work in this field in Germany. Covered are flow problems of high and low aspect-ratio wings and bluff bodies, laminar flow control and transition, hypersonic flows, transition and fluid mechanical modelling, LES and DNS, numerical simulation, aeroelasticity, measuring techniques and propulsion flows.

Editors and Affiliations

  • Lehrstuhl für Fluidmechanik, Technische Universität München, Garching, Germany

    Christian Breitsamter, Boris Laschka

  • Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR), Göttingen, Germany

    Hans-Joachim Heinemann

  • Deutsche Airbus GmbH, Bremen, Germany

    Reinhard Hilbig

Bibliographic Information

  • Book Title: New Results in Numerical and Experimental Fluid Mechanics IV

  • Book Subtitle: Contributions to the 13th STAB/DGLR Symposium Munich, Germany 2002

  • Editors: Christian Breitsamter, Boris Laschka, Hans-Joachim Heinemann, Reinhard Hilbig

  • Series Title: Notes on Numerical Fluid Mechanics and Multidisciplinary Design

  • DOI: https://doi.org/10.1007/978-3-540-39604-8

  • Publisher: Springer Berlin, Heidelberg

  • eBook Packages: Springer Book Archive

  • Copyright Information: Springer-Verlag Berlin Heidelberg 2004

  • Hardcover ISBN: 978-3-540-20258-5Published: 28 January 2004

  • Softcover ISBN: 978-3-642-53546-8Published: 05 August 2012

  • eBook ISBN: 978-3-540-39604-8Published: 13 August 2012

  • Series ISSN: 1612-2909

  • Series E-ISSN: 1860-0824

  • Edition Number: 1

  • Number of Pages: XIII, 484

  • Number of Illustrations: 696 b/w illustrations, 53 illustrations in colour

  • Topics: Engineering Fluid Dynamics, Automotive Engineering, Fluid- and Aerodynamics, Computational Intelligence

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