The Flow of Marking Particles for a Two Dimensional Source/Sink and a Two Dimensional Potential Vortex

Abstract

The flow of marker particles in a two dimensional source/sink and a two dimensional potential vortex are theoretically calculated. The flow is considered to be defined by a complex potential and is limited to steady, inviscid, incompressible, irrotational flow. The particles are assumed to be spherical and not to interact with each other. The gas and dust stream-lines are determined for two cases; one, the particles follow the gas stream-lines, analogous to no dust in the gas, and secondly, when the particles are free to move independently.

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1981
Accession Number
ADA379866

Entities

People

  • George L. Seibert

Organizations

  • Wright Laboratory

Tags

DTIC Thesaurus Topics

  • Aerodynamics
  • Aeronautical Laboratories
  • Air Force
  • Air Force Facilities
  • Airframes
  • Case Studies
  • Equations
  • Equations Of Motion
  • Flow
  • Fluid Flow
  • Gas Flow
  • Numerical Integration
  • Particle Size
  • Particles
  • Reynolds Number
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Aerosol Science/Aerosol Physics
  • Neural Network Machine Learning.
  • Plasma Physics / Magnetohydrodynamics