EFFECT OF IGNITOR DESIGN AND IGNITOR SPARKGAP ENVIRONMENT ON IGNITION IN A TURBOJET COMBUSTOR

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1954
Accession Number
AD0028727

Entities

People

  • David M. Straight
  • Hampton H. Foster

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Air Flow
  • Air Gaps
  • Air Pressure
  • Combustion
  • Combustors
  • Energy Levels
  • Flow Rate
  • Fuel Nozzles
  • Fuel Sprays
  • Gas Turbine Nozzles
  • Ignition
  • Ignition Systems
  • Repetition Rate
  • Spark Gaps
  • Turbojet Engines
  • Vapor Pressure
  • Voltage