A Numerical Investigation of the Flow Field Developed Behind (A) An Oblique Shock Wave Propagating into a Dusty Gas (B) A Normal Shock Wave Propagating into a Dusty Gas Having Dust Particles of Various Size

Abstract

The dependence of the shock induced flow field on non-uniformities of the various physical properties of the dust (namely, the diameter, the material density and the heat capacity) were investigated numerically. The flow field which is developed when a dusty gas steady suspension passes through an oblique shock wave was investigated numerically. In addition, the dependence of the shock induced flow field on the various physical properties of the dust was investigated.

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Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1988
Accession Number
ADA204219

Entities

People

  • G. Ben-dor
  • O. Igra

Tags

Communities of Interest

  • Energy and Power Technologies
  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Boundary Layer
  • Computational Fluid Dynamics
  • Differential Equations
  • Energy Transfer
  • Flow
  • Flow Fields
  • Fluid Dynamics
  • Fluid Mechanics
  • Heat Capacity
  • Heat Transfer
  • Mach Number
  • Materials
  • Physical Properties
  • Shock Waves
  • Specific Heat
  • Thermal Conductivity

Fields of Study

  • Physics

Readers

  • Atmospheric Science / Meteorology, specifically Wind Wave Turbulence.
  • Combustion Dynamics and Shock Wave Physics.
  • Surface Engineering/Surface Coating Technology.