Hydrocarbon-Fueled Scramjet Research at Hypersonic Mach Numbers

Abstract

Planar laser-induced fluorescence (PLIF) of OH and wall-pressure measurements have been used to investigate the combustion in a cavity flame-holder scramjet combuster.

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Document Details

Document Type
Technical Report
Publication Date
Mar 31, 2005
Accession Number
ADA439189

Entities

People

  • Frank Houwing

Organizations

  • Australian National University

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies
  • Weapons Technologies

DTIC Thesaurus Topics

  • Boundary Layer
  • Chemical Reactions
  • Chemistry
  • Combustion
  • Combustion Products
  • Computational Fluid Dynamics
  • Energy Transfer
  • Flow Visualization
  • Fluid Dynamics
  • Ignition Lag
  • Laser Beams
  • Laser Induced Fluorescence
  • Lasers
  • Pressure Measurement
  • Supersonic Combustion Ramjet Engines
  • Three Dimensional
  • Turbulent Mixing

Fields of Study

  • Physics

Technology Areas

  • Directed Energy
  • Hypersonics
  • Hypersonics - Hypersonic Flow