Properties of Dynamical Systems Describing the Evolution of Coherent Structures in a Transitional Boundary Layer

  • D. Rempfer
Conference paper
Part of the Fluid Mechanics and Its Applications book series (FMIA, volume 24)

Abstract

To gain a better understanding of the evolution of a flat-plate boundary layer during the process of transition, we have constructed low-dimensional models for the dynamics of this flow that describe the behaviour in time of so-called ‘coherent structures’. These coherent structures were calculated at 23 streamwise positions within thin cross-stream slices of the boundary layer, evenly spaced between x = 407 mm and x = 470 mm distance from the leading edge of the flat plate. The Reynolds numbers based on displacement thickness at these positions were Re δ1 = 854 and Re δ1= 918, respectively. Each of the slices was about 1.2 mm thick in the streamwise direction and extended 24.5 mm in the span wise direction. The height of these slices corresponds to about three boundary layer thicknesses at the first position considered, and about two boundary layer thicknesses at the last.

Keywords

Boundary Layer Direct Numerical Simulation Coherent Structure Proper Orthogonal Decomposition Boundary Layer Thickness 
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 Science+Business Media Dordrecht 1995

Authors and Affiliations

  • D. Rempfer
    • 1
  1. 1.Institut für Aerodynamik und GasdynamikUniversity of StuttgartStuttgartGermany

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