NONLINEAR TRANSMISSION CHARACTERISTICS OF THE PLASMA SHEATH

Abstract

A model is constructed of a nonlinear, one dimensional inhomogeneous multicomponent plasma slab which has the characteristics of the plasma sheath surrounding a typical hypersonic re-entry vehicle at 200,000 ft while traveling at about 18,000 ft/second. A plane wave incident upon the slab at arbitrary angle can induce changes in electron temperature without affecting the neutral gas temperature. The variations of electron temperature produce changes in collision frequency and the rate coefficients describing the various electron production and loss mechanisms. Such changes cause alterations in the effective dielectric constant of the medium. On the basis of a model of a plane-layered medium composed of a stack of linear homogeneous sheets, the reflection and transmission coefficients of the nonlinear slab may be computed by a step-by-step numerical integration of Maxwell's equations expressed in the form of difference equations.

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Document Details

Document Type
Technical Report
Publication Date
May 01, 1963
Accession Number
AD0407089

Entities

People

  • Robert J. Papa

Organizations

  • Air Force Cambridge Research Laboratories

Tags

Communities of Interest

  • Advanced Electronics
  • Energy and Power Technologies
  • Materials and Manufacturing Processes

DTIC Thesaurus Topics

  • Air Force
  • Boltzmann Equation
  • Chemical Reactions
  • Difference Equations
  • Dissociation
  • Electric Fields
  • Electromagnetic Fields
  • Electromagnetic Radiation
  • Electron Density
  • Electron Energy
  • Energy
  • Energy Transfer
  • Heat Transfer
  • Ionization
  • Temperature Gradients
  • Thermal Conductivity
  • Wave Propagation

Fields of Study

  • Physics

Readers

  • Plasma Physics / Magnetohydrodynamics

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers
  • Hypersonics - Hypersonic Flight
  • Microelectronics