COMBUSTION PERFORMANCE OF TWO EXPERIMENTAL TURBOJET ANNULAR COMBUSTORS AT CONDITIONS SIMULATING HIGH-ALTITUDE SUPERSONIC FLIGHT

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Document Details

Document Type
Technical Report
Publication Date
Mar 26, 1954
Accession Number
AD0028728

Entities

People

  • Carl T. Norgren
  • Eugene V. Zettle
  • Herman Mark

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air Flow
  • Air Temperature
  • Aircrafts
  • Combustion
  • Combustors
  • Efficiency
  • Engines
  • Flight Speeds
  • Fuel Consumption
  • High Altitude
  • Jet Aircraft
  • Mach Number
  • Static Pressure
  • Supersonic Aircraft
  • Supersonic Flight
  • Turbines
  • Turbojet Engines

Technology Areas

  • Hypersonics