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

  • Alexander Allen
  • Michail Iatrou
  • Alexander Pechloff
  • Boris Laschka
Part of the Notes on Numerical Fluid Mechanics and Multidisciplinary Design (NNFM) book series (NNFM, volume 92)

Summary

A selection of steady and unsteady validation results for the Reynolds-averaged Navier-Stokes solver FLM-NS with respect to an experimental delta wing test case is presented and compared to other numerical results. Having put the numerical method’s validity into evidence, the unsteady flow induced by an oscillating flap is investigated for a Fighter Type Delta Wing.

Keywords

Turbulence Model Pressure Coefficient Wing Surface Span Station Freestream Mach Number 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

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Copyright information

© Springer-Verlag Berlin Heidelberg 2006

Authors and Affiliations

  • Alexander Allen
    • 1
  • Michail Iatrou
    • 1
  • Alexander Pechloff
    • 1
  • Boris Laschka
    • 1
  1. 1.Technische Universität München, Lehrstuhl für Fluidmechanik, Abteilung Aerodynamik

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