Experimental and Numerical Investigation of Coherent Structures in Turbulent Wake Flows.

Abstract

Recent x wire measurements in a plane turbulent wake are presented. Sinuous disturbances at several amplitudes and frequencies were introduced to the wake by oscillating a small trailing edge flap. The Strouhal numbers of the perturbations were specially chosen so that the downstream location of the neutral point (where the spatial amplification rate obtained from linear stability theory vanishes) was well within the range of measurements. The stream wise variation of the half width of the wake and the centerline velocity deficit was dependent on the amplitude level and showed dramatic deviations at large forcing levels from the well-known square root behavior of the unforced case. The measured coherent Reynolds stressed were observed to change sign in the neighborhood of the location of the neutral point as predicted by linear viscous theory. The numerical simulations of free shear layers and progress towards the wake simulations are also discussed.

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Document Details

Document Type
Technical Report
Publication Date
Apr 07, 1987
Accession Number
ADA179720

Entities

People

  • F. H. Champagne
  • H. Fasel

Organizations

  • University of Arizona

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air Force
  • Air Force Facilities
  • Amplification
  • Amplitude
  • Measurement
  • Navier Stokes Equations
  • Numbers
  • Personal Information Managers
  • Perturbations
  • Scientific Research
  • Simulations
  • Square Roots
  • Strouhal Number
  • Three Dimensional
  • Trailing Edges
  • Turbulent Mixing
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Calculus or Mathematical Analysis
  • Fluid Mechanics and Fluid Dynamics.