EFFECT OF FUEL INJECTORS AND LINER DESIGN ON PERFORMANCE OF AN ANNULAR TURBOJET COMBUSTOR WITH VAPOR FUEL

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Document Details

Document Type
Technical Report
Publication Date
Apr 06, 1953
Accession Number
AD0005538

Entities

People

  • Carl T. Norgren
  • J. H. Childs

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air Flow
  • Altitude
  • Combustion
  • Combustors
  • Diameters
  • Engine Components
  • Engines
  • Experimental Data
  • Flow Rate
  • Fuel Air Ratio
  • Fuel Injection
  • Fuel Injectors
  • Gas Turbines
  • Mach Number
  • Mass Flow
  • Production Models
  • Turbojet Engines