ALTITUDE PERFORMANCE EVALUATION OF TWO AFTERBURNER FUEL MANIFOLD CONFIGURATIONS IN AN IROQUOIS SERIES 2 TURBOJET ENGINE

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1959
Accession Number
AD0221389

Entities

People

  • James Neeley
  • T. R. Ward

Organizations

  • Arnold Engineering Development Complex

Tags

Communities of Interest

  • Materials and Manufacturing Processes

DTIC Thesaurus Topics

  • Air Force
  • Calorific Value
  • Combustion
  • Combustion Chambers
  • Compressor Rotors
  • Exhaust Nozzles
  • Flow Rate
  • Fuel Air Ratio
  • Fuel Consumption
  • Gas Flow
  • High Pressure
  • High Pressure Compressors
  • Mach Number
  • Measurement
  • Research Facilities
  • Test Facilities
  • Turbojet Engines