ROUGH WALL TURBULENT BOUNDARY LAYERS.

Abstract

The paper describes a detailed experimental study of turbulent boundary layer development over rough walls in both zero and adverse pressure gradients. Skin friction was determined by pressure tapping the roughness elements and measuring their form drag. Two wall roughness geometries were chosen each giving a different law of behaviour. However, it has been found that results for both types of roughness correlate with a Reynolds number based on wall shear velocity and on the distance below the crests of the elements from which the logarithmic distribution of velocity is measured. One important implication of this is that a zero pressure gradient boundary layer with a cavity type rough wall conforms to Rotta's condition of precise self preserving flow. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1968
Accession Number
AD0685396

Entities

People

  • Anthony E. Perry
  • Peter N. Joubert
  • William H. Schofield

Organizations

  • University of Melbourne

Tags

DTIC Thesaurus Topics

  • Boundaries
  • Boundary Layer
  • Drag
  • Fluid Mechanics
  • Friction
  • Geometry
  • Layers
  • Pressure Distribution
  • Pressure Gradients
  • Reynolds Number
  • Roughness
  • Skin Friction
  • Turbulent Boundary Layer

Fields of Study

  • Physics

Readers

  • Fluid Mechanics and Fluid Dynamics.
  • Systems Analysis and Design