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Numerical High Lift Research II/III

In: High Performance Computing in Science and Engineering’ 04

Author

Listed:
  • S. Melber-Wilkending

    (DLR Braunschweig, Institute of Aerodynamics and Flow Technology)

  • A. Stürmer

    (DLR Braunschweig, Institute of Aerodynamics and Flow Technology)

  • E. Stumpf

    (DLR Braunschweig, Institute of Aerodynamics and Flow Technology)

  • J. Wild

    (DLR Braunschweig, Institute of Aerodynamics and Flow Technology)

  • R. Rudnik

    (DLR Braunschweig, Institute of Aerodynamics and Flow Technology)

Abstract

The project NHLRes ([1], [2]) is concerned with the simulation of aircraft aerodynamics and thus belongs to the research field of computational fluid dynamics (CFD) for aerospace applications. NHLRes comprises the numerical simulation of the viscous flow around transport aircraft high lift configurations based on the solution of the Reynolds-averaged Navier-Stokes equations. The project NHLRes consists of five parts representing the analysis of complex 3D-flow features, wake vortex simulation, optimization for three-dimensional high lift flow, aerodynamic interactions between the propeller and high lift wings and finally the usage of large eddy simulation (LES) of the flow around high lift configurations.

Suggested Citation

  • S. Melber-Wilkending & A. Stürmer & E. Stumpf & J. Wild & R. Rudnik, 2005. "Numerical High Lift Research II/III," Springer Books, in: Egon Krause & Willi Jäger & Michael Resch (ed.), High Performance Computing in Science and Engineering’ 04, pages 237-259, Springer.
    • Handle: RePEc:spr:sprchp:978-3-540-26589-4_24
    DOI: 10.1007/3-540-26589-9_24
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