ROCKET TUNNEL GAS PROPERTIES,

Abstract

An analysis was made of the specific heat, wind tunnel expansion processes, and shock wave properties of gas mixtures in a solid propellant rocket driven supersonic wind tunnel.

Document Details

Document Type
Technical Report
Publication Date
Sep 12, 1957
Accession Number
AD0657160

Entities

People

  • F. K. Hill

Organizations

  • Johns Hopkins University Applied Physics Laboratory

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Buildings And Structures
  • Energetic Materials
  • Materials
  • Propellants
  • Shock
  • Shock Waves
  • Solid Propellants
  • Specific Heat
  • Supersonic Wind Tunnels
  • Waves
  • Wind Tunnels

Fields of Study

  • Engineering
  • Physics

Readers

  • Fluid Dynamics.
  • Rocket Propulsion.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flight
  • Hypersonics - Hypersonic Flow