A Turbulent Model Study for the Multicomponent Nonsimilar Turbulent Boundary Layer Program

Abstract

An investigation of the accuracy of the Air Force Weapons Laboratory Nonsimilar Turbulent Boundary Layer Computer Code through comparisons of predictions with experimental data is presented. Five complete data sets are selected from a literature survey of flat plate supersonic flow, hypersonic flow with and without accerleration, supersonic flow with highly nonsimilar wall temperature wall blowing. Comparisons are presented which include velocity, total temperature, and Mach number profiles at several axial stations.

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Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1971
Accession Number
AD0734752

Entities

People

  • Howard L. Morse
  • Larry W. Anderson

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Boundary Layer
  • Computational Fluid Dynamics
  • Computers
  • Experimental Data
  • Fluid Dynamics
  • Hypersonic Flow
  • Incompressible Flow
  • Inviscid Flow
  • Jet Propulsion
  • Literature Surveys
  • Mach Number
  • Measurement
  • Plastic Explosives
  • Pressure Distribution
  • Pressure Gradients
  • Test And Evaluation
  • Test Facilities

Fields of Study

  • Physics

Readers

  • Business Analytics
  • Fluid Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers
  • Hypersonics - Hypersonic Flow