Turbulence in Electrostatic Ion Acoustic Shocks.

Abstract

Three types of collisionless electrostatic ion acoustic shocks are investigated using the University of California, Los Angeles, double plasma (DP) device: (a) laminar shocks; (b) small amplitude turbulent shocks in which the turbulence is confined to be upstream of the shock potential jump; (c) large amplitude turbulent shocks in which the wave turbulence occurs throughout the shock transition. The wave turbulence is generated by ions which are reflected from the shock potential; linear theory spatial growth increments agree with experimental values. The experimental relationship between the shock Mach number and the shock potential is shown to be inconsistent with theoretical shock models which assume that the electrons are isothermal. Theoretical calculations which assume a trapped electron equation of a state and a turbulently flattened velocity distribution function for the reflected ions yields a Mach number vs potential relationship in agreement with experiment. (Author)

Document Details

Document Type
Technical Report
Publication Date
May 01, 1973
Accession Number
AD0762472

Entities

People

  • Alfred Y. Wong
  • Ferdinand V. Coroniti
  • Oscoe B. White
  • Robert W. Means

Organizations

  • University of California, Los Angeles

Tags

DTIC Thesaurus Topics

  • Agreements
  • Amplitude
  • California
  • Distribution Functions
  • Electrons
  • Equations
  • Mach Number
  • Motion
  • Physical Properties
  • Transitions
  • Turbulence
  • Universities

Fields of Study

  • Physics

Readers

  • Atmospheric Science / Meteorology, specifically Wind Wave Turbulence.
  • Fluid Dynamics.
  • Plasma Physics / Magnetohydrodynamics

Technology Areas

  • Microelectronics