SOME OBSERVATIONS OF SHOCK-INDUCED TURBULENT SEPARATION ON SUPERSONIC DIFFUSERS

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Document Details

Document Type
Technical Report
Publication Date
May 04, 1954
Accession Number
AD0029847

Entities

People

  • Theodore J. Nussdorfer

Organizations

  • National Aeronautics and Space Administration

Tags

DTIC Thesaurus Topics

  • Boundaries
  • Boundary Layer
  • Diffusers
  • Flow
  • Free Stream
  • Layers
  • Mach Number
  • Pressure Measurement
  • Reynolds Number
  • Specific Heat
  • Static Pressure
  • Supersonic Diffusers
  • Supersonic Inlets
  • Three Dimensional
  • Turbojet Engines
  • Turbulent Boundary Layer
  • Two Dimensional

Technology Areas

  • Hypersonics