Injection, Atomization, Ignition and Combustion of Liquid Fuels in High-Speed Air Streams.

Abstract

Experimental and numerical studies of liquid and slurry jet penetration, break-up and atomization were performed. The measurements were done mainly at Mach 3.0 with P sub 0 = 4 atm. and T sub 0 = 300 k. Brief summaries of recent progress on various tasks are given.

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1984
Accession Number
ADA154056

Entities

People

  • J. A. Schetz

Organizations

  • Virginia Tech

Tags

Communities of Interest

  • Air Platforms
  • Materials and Manufacturing Processes
  • Weapons Technologies

DTIC Thesaurus Topics

  • Abstracts
  • Atomization
  • Combustion
  • Combustors
  • Engineering
  • Flow
  • Heat Transfer
  • Ignition
  • Ignition Lag
  • Liquid Jets
  • Mass Flow
  • Mass Transfer
  • Measurement
  • Phase
  • Phase Separation
  • Shape
  • Supersonic Combustion Ramjet Engines

Fields of Study

  • Chemistry
  • Physics

Readers

  • Combustion and Flow Dynamics.
  • Combustion science or combustion engineering.