CONSTANT AREA MIXING OF NON-ISOENERGETIC COAXIAL COMPRESSIBLE STREAMS

Abstract

As part of a general investigation of two-stream supersonic diffusers, a theory was developed for the bounded turbulent mixing between coaxial high velocity streams of different composition and temperature. The usual assumption of negligible axial pressure gradient is invalid in this case because the outer stream is bounded by a cylindrical duct. A highly simplified flow model is used which retains the essential features of the actual mixing process; the resulting system of equations is amenable to manual calculation. The theory is correlated with data obtained from an annular nozzle wind tunnel having a central supersonic core of rocket exhaust gases. Correlation is also made with Mikhail's low velocity data for which his more elaborate theory is available for comparison. The simplified theory predicts with reasonable accuracy the experimental axial static pressure and velocity distributions.

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1962
Accession Number
AD0270156

Entities

People

  • C. E. Peters
  • S. Wehofer

Organizations

  • Arnold Engineering Development Complex

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Diffusers
  • Exhaust Gases
  • Flow
  • Gas Turbine Nozzles
  • Gases
  • Government Procurement
  • Instrumentation
  • Mach Number
  • Nozzles
  • Pressure Distribution
  • Pressure Gradients
  • Rocket Exhaust
  • Rocket Nozzles
  • Static Pressure
  • Test Facilities
  • Turbulent Mixing
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.
  • Fluid Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow