AIR-FLOW AND THRUST CHARACTERISTICS OF SEVERAL CYLINDRICAL COOLING-AIR EJECTORS WITH A PRIMARY TO SECONDARY TEMPERATURE RATIO OF 1.0

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Document Details

Document Type
Technical Report
Publication Date
Mar 06, 1953
Accession Number
AD0002826

Entities

People

  • D. P. Hollister
  • W. K. Greathouse

Organizations

  • National Advisory Committee for Aeronautics

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air Ejectors
  • Air Flow
  • Air Supplies
  • Boundary Layer
  • Convergent Divergent Nozzles
  • Dew Point
  • Diameters
  • Engines
  • Flow
  • Labyrinth Seals
  • Mach Number
  • Mass Flow
  • Plastic Explosives
  • Secondary Flow
  • Security
  • Static Pressure
  • Turbojet Engines