A COMPARISON OF TRANSITION REYNOLDS NUMBERS FROM 12-IN. AND 40-IN. SUPERSONIC TUNNELS

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1963
Accession Number
AD0299290

Entities

People

  • C. J. Schueler

Organizations

  • Arnold Engineering Development Complex

Tags

Communities of Interest

  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Air Force
  • Boundary Layer
  • Boundary Layer Transition
  • Dynamics
  • Fluid Dynamics
  • Fluid Mechanics
  • Free Stream
  • Gas Dynamics
  • Instrumentation
  • Layers
  • Mach Number
  • Measurement
  • Pressure Measurement
  • Reynolds Number
  • Transitions
  • Turbulent Boundary Layer
  • Wind Tunnels

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers
  • Hypersonics - Hypersonic Flow