STUDY OF PLASMAS IN HYPERSONIC FLOW,

Abstract

A Mach 6 low-density nozzle has been designed and constructed for studies of the decay of a nitrogen plasma after excitation by a radio-fre quency discharge. Aerodynamic measurements have been made of the Mach number and density distri bution for both cold and hot flow conditions. A method of measuring the heavy particle temper ature in a plasma is described using the rota tional structure of the N sub 2 second positive band system. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1963
Accession Number
AD0417468

Entities

People

  • David Robinson
  • James C. Williams

Organizations

  • University of Southern California

Tags

DTIC Thesaurus Topics

  • Excitation
  • Flow
  • Hypersonic Flow
  • Low Density
  • Mach Number
  • Measurement
  • Nitrogen
  • Particles
  • Physical Properties

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Pulsed Power and Plasma Physics.
  • Snow Cover Descriptors for Reptiles and Their Illustrations.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow