STAGNATION TEMPERATURE PROBES FOR USE AT HIGH SUPERSONIC SPEEDS AND ELEVATED TEMPERATURES

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Document Details

Document Type
Technical Report
Publication Date
Oct 12, 1954
Accession Number
AD0058826

Entities

People

  • E. M. Winkler

Organizations

  • Naval Ordnance Laboratory

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Air Force
  • Boundary Layer
  • Fluid Dynamics
  • Heat Transfer
  • Jet Propulsion
  • Mach Number
  • Mechanical Properties
  • Munitions
  • Navy
  • Physics Laboratories
  • Reynolds Number
  • Stagnation Temperature
  • Test Facilities
  • Thermal Conductivity
  • Turbulent Boundary Layer
  • Wind Tunnels

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow