EXPERIMENTAL INVESTIGATION ON BOUNDARY LAYER SUCTION BY SERIES OF SLITS AND HOLES

Abstract

The development of laminar and turbulent boundary layers with pressure gradient on various permeable test walls (filter paper, slits, holes, perforations) has been studied in the low-turbulence wind-tunnel of the Aerodynamische Versuchsanstalt. The behaviour of wall-stress, dissipation and the different boundary layer parameters is deduced from the measurements. (Author)

Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1960
Accession Number
AD0262623

Entities

People

  • W. Wuest

Organizations

  • AGARD

Tags

DTIC Thesaurus Topics

  • Boundaries
  • Boundary Layer
  • Dissipation
  • Filter Paper
  • Filters
  • Fluid Mechanics
  • Layers
  • Measurement
  • Paper
  • Perforation
  • Pressure Gradients
  • Turbulence
  • Turbulent Boundary Layer
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Ocean-Atmosphere Mesoscale Modeling, Data Assimilation, and Flux Boundary Layers
  • Structural Dynamics.