A HIGH TEMPERATURE STREAM TUBE FOR A SUPERSONIC WIND TUNNEL

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Document Details

Document Type
Technical Report
Publication Date
May 01, 1958
Accession Number
AD0200634

Entities

People

  • Eugene S. Rubin
  • Richard H. Adams

Organizations

  • Massachusetts Institute of Technology

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerodynamic Heating
  • Boundary Layer
  • Fluid Dynamics
  • Heat Transfer
  • Heat Transmission
  • High Temperature
  • Hypersonic Wind Tunnels
  • Mach Number
  • Mass Flow
  • Measurement
  • Pressure Measurement
  • Stagnation Pressure
  • Stagnation Temperature
  • Supersonic Wind Tunnels
  • Test Facilities
  • Turbulent Mixing
  • Wind Tunnels

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow