Atomization and Combustion of a Gelled, Metallized Slurry Fuel

Abstract

Two commercially available atomizers were tested for their ability to atomize a gelled boron slurry fuel. Particle size distributions were measured in non-reacting flow using a Malvern 2600 HSD Laser Diffraction Particle Sizer. A sub-scale ramjet combustor was designed and fabricated which utilized a sudden expansion inlet dump together with inlet air swirl for flame stabilization. An airblast atomizer produced sufficiently small particles for good combustion, but at the cost of a high pressure drop across the atomizer, making it impractical for use in a slurry fueled ramjet. Sustained steady combustion of the slurry fuel was not achieved using the airblast atomizer. A whistle type ultrasonic atomizer also produced sufficiently small particles and at a much lower pressure drop across the atomizer. Sustained stable combustion was achieved using the ultrasonic atomizer which yielded a combustion efficiency of 76% at 96 psia and an equivalence ratio of 0.78.

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1992
Accession Number
ADA261778

Entities

People

  • Bruce C. Urbon

Organizations

  • Naval Postgraduate School

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Masses
  • Combustion
  • Combustors
  • Diffraction
  • Efficiency
  • Energy
  • Flow
  • Flow Rate
  • Fuel Additives
  • High Pressure
  • Hydrocarbon Fuels
  • Ignition
  • Ignition Systems
  • Mass Flow
  • Measurement
  • Particle Size
  • Slurry Fuels

Readers

  • Aerosol Science/Aerosol Physics
  • Internal Combustion Engine (ICE) Technology.
  • Rocket Propulsion.

Technology Areas

  • Directed Energy