AN EXPERIMENTAL INVESTIGATION OF THE EFFECTS OF SEVERAL TYPES OF SURFACE ROUGHNESS ON TURBULENT BOUNDARY LAYER CHARACTERISTICS AT SUPERSONIC SPEEDS

Abstract

A theory is described which can be used to predict accurately the skin friction drag of surfaces with uniform grain-type roughness. The roughness does not necessarily have to extend to the leading edge of the surface for an accurate calculation to be made. Uniform surface roughness composed of spherical beads does not affect the boundary layer in a manner significantly different from grain-type roughness, provided that the grains and the spheres are bonded to the surface in a similar manner. Consequently, the theory accurately predicts the effects of spherical roughness elements on skin friction under these conditions. The effect of a given type of roughness on turbulent boundary layer characteristics is strongly dependent upon the density of distribution of the roughness elements. The effect of maximum density V-grooves on turbulent boundary layer characteristics is dependent upon the sweepback angle. The effect of increasing sweepback is to reduce the skin friction drag.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Feb 06, 1953
Accession Number
AD0657134

Entities

People

  • Felix W. Fenter
  • W. C. Lyons Jr.

Organizations

  • University of Texas at Austin

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Boundary Layer
  • Coefficients
  • Data Reduction
  • Free Stream
  • Grain Size
  • Leading Edges
  • Mach Number
  • Measurement
  • Physics Laboratories
  • Pressure Measurement
  • Shear Stresses
  • Skin Friction
  • Static Pressure
  • Supersonic Wind Tunnels
  • Surface Roughness
  • Turbulent Boundary Layer
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Fluid Dynamics.
  • Fluid Mechanics and Fluid Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers