Air Entrainment in a Jet Flame Stabilizer in Supersonic Flow.

Abstract

An analytical technique, based upon a turbulent boundary layer separation model, has been suggested for determining the amount of air entrained into a fuel jet injected transversely into a supersonic air stream. The amount of air entrained into the fuel jet was found to vary directly with the jet induced blockage. However, the jet induced blockage and hence the amount of air entrained does have a limiting value. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Nov 24, 1976
Accession Number
ADA035309

Entities

People

  • R. A. Cookson

Organizations

  • Cranfield University

Tags

DTIC Thesaurus Topics

  • Air Entrainment
  • Boundary Layer
  • Combustion
  • Combustors
  • Entrainment
  • Flame Propagation
  • Flames
  • Flow
  • Flow Rate
  • Hydrocarbon Fuels
  • Ignition
  • Mass Flow
  • Pressure Distribution
  • Shock
  • Stagnation Temperature
  • Static Pressure
  • Turbulent Boundary Layer

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.

Technology Areas

  • Hypersonics