THE EFFECT OF SOUND WAVES AND FLEXIBLE BOUNDARIES OF TURBULENCE.

Abstract

Research was conducted on separation of boundary layers on airfoils at high angles of attack, and skin friction drag in laminar and turbulent boundary layers on airfoils at low angles of attack. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1965
Accession Number
AD0616713

Entities

People

  • Donald Herbert Fisher

Organizations

  • University of Oklahoma

Tags

DTIC Thesaurus Topics

  • Acoustic Propagation
  • Boundaries
  • Boundary Layer
  • Drag
  • Friction
  • High Angles
  • Layers
  • Low Angles
  • Skin Friction
  • Sound Waves
  • Turbulent Boundary Layer

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Fluid Mechanics and Fluid Dynamics.