Mechanism of Intermittent Atomization

Abstract

A theory is developed for the purpose of enhancing the efficiency of internal combustion engines, and to reduce the air pollution caused by inefficient combustion. The theoretical results show that the droplet formation from the leading edge of the liquid fuel jet is caused by th Taylor-Lamb instability during the decerelation phase of the intermittent spray. The mechanism of droplet formation from the rest of the liquid-gas interface is caused by the interfacial stress fluctuation. The decerelation of the liquid jet tends to reduce the droplet diameter at the same pressure. However, finer sprays can be produced with a more sudden reduction in the nozzle inlet pressure after its peak during the injection period. An increase in the compressibility of the liquid jet is shown the promote the generation of smaller droplets, although at a slower rate. The compressibility of the ambient gas, as well as the surface tension, tends to promote absolute instability. The precise physical meaning remains unclear. The absolute instability can be reduced to convective instability by reducing the surface tension and/or increasing the compressibility of the jet fluid. The convective instability is responsible for the formation of sprays.... Intermittent fuel sprays, Atomization

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1993
Accession Number
ADA266625

Entities

People

  • S. P. Lin

Organizations

  • Clarkson University

Tags

Communities of Interest

  • C4I
  • Energy and Power Technologies
  • Materials and Manufacturing Processes
  • Space

DTIC Thesaurus Topics

  • Combustion
  • Combustion Chambers
  • Computational Fluid Dynamics
  • Computational Science
  • Computer Programs
  • Efficiency
  • Fluid Flow
  • Fluid Mechanics
  • Froude Number
  • Fuel Sprays
  • Internal Combustion Engines
  • Leading Edges
  • Liquid Jets
  • Measurement
  • Mechanics
  • Surface Tension
  • Waveforms

Readers

  • Aerosol Science/Aerosol Physics
  • Combustion and Flow Dynamics.