FEASIBILITY OF A DIFFUSER CENTERBODY INJECTOR FOR THE 16-FOOT SUPERSONIC TUNNEL OF THE PROPULSION WIND TUNNEL FACILITY

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1962
Accession Number
AD0274219

Entities

People

  • E. H. Sloan Jr.
  • M. W. Davis

Organizations

  • Arnold Engineering Development Complex

Tags

Communities of Interest

  • Air Platforms
  • Materials and Manufacturing Processes

DTIC Thesaurus Topics

  • Air Force
  • Boundary Layer
  • Compressors
  • Diffusers
  • Flow Fields
  • Geometry
  • Injectors
  • Mach Number
  • Mass Flow
  • Model Tests
  • Pressure Measurement
  • Stagnation Pressure
  • Stagnation Temperature
  • Static Pressure
  • Supersonic Diffusers
  • Two Dimensional
  • Wind Tunnels

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow