Separated Flow Studies.

Abstract

This report reviews the progress over the last decade on separated flows conducted at these laboratories. Experimental investigations conducted in the hypersonic wind tunnels is discussed. Advancements are summarized in the theoretical area which cover the development of interacting boundary layers to the numerical computation of the complete Navier-Stokes equations.

Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1975
Accession Number
ADA014245

Entities

People

  • W. L. Hankey

Organizations

  • Air Force Research Laboratory

Tags

DTIC Thesaurus Topics

  • Boundaries
  • Boundary Layer
  • Buildings And Structures
  • Computations
  • Equations
  • Hypersonic Wind Tunnels
  • Layers
  • Mathematics
  • Navier Stokes Equations
  • Research Facilities
  • Test Facilities
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Computational Fluid Dynamics (CFD)
  • Fluid Dynamics.
  • Technical Research and Report Writing.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow