Exploding Wire Simulation of Jet-Engine Gas-Path Microdistresses.

Abstract

Exploding wires were used to simulate jet-engine gas-path microdistresses. The physical processes involved in the formation of boluses of charge in a flowstream were investigated and the amounts of bolus charge produced under various conditions were measured. Ion-probe response were concurrently recorded. The results of the investigation were used to construct a theory of bolus formation. Large negative boluses of charge were produced by the injection of hot metal particles into a flowstream. Smaller positive boluses were produced by heating a wire to a temperature near its melting point. Ion-probe responses were shown to be very misleading when used as a sole source of information as to the charge in a bolus. It is recommended that immediate attention be given to the detection of negative boluses of charge in a jet engine exhaust since negative boluses would most probably be produced by the more severe (very hot particles) microdistress which could lead to catastrophic engine failure. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1975
Accession Number
ADA039239

Entities

People

  • John E. Mitchell

Organizations

  • Air Force Institute of Technology

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Air Compressors
  • Air Force
  • Aircrafts
  • Charged Particles
  • Combustion
  • Combustion Products
  • Detection
  • Electrons
  • Exploding Wires
  • Jet Engine Exhaust
  • Jet Engines
  • Measurement
  • Melting Point
  • Particle Size
  • Thermionic Emission
  • Turbine Blades
  • Turbines

Readers

  • Aerospace Engineering
  • Snow Cover Descriptors for Reptiles and Their Illustrations.
  • Thermal Physics or Thermal Science.