Computations of Droplet/Flow Interactions In Sprays.

Abstract

The behavior of liquid fuel drops is studied by numerical simulations. The Navier-Stokes equations are solved by a finite difference/front tracking technique that allows resolution of inertial and viscous forces as well as the inclusion of surface tension at the deformable boundary between the fuel and the air. Two- and three-dimensional simulations are used to determine how the lift and the drag depend on the shear rate of the fluid. The deformation of the drops play a major role and while a nearly spherical drop experiences lift in the same direction as a solid particle, relatively modest deformation can lead to a lift force in the opposite direction. To examine more complex problems, a new three-dimensional code has been written that allows local grid refinement and the use of cylindrical coordinates. This code has been used to examine the development of three-dimensional disturbances during the primary breakup of jets. At finite amplitude the three-dimensional disturbance can dominate the two-dimensional one and lead to "fiber" breakup

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Document Details

Document Type
Technical Report
Publication Date
Aug 29, 1997
Accession Number
ADA353983

Entities

People

  • Gretar Tryggvason

Organizations

  • University of Michigan

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Amplitude
  • Applied Mechanics
  • Boundaries
  • Computational Fluid Dynamics
  • Engineering
  • Equations
  • Flow
  • Fluid Dynamics
  • Geometry
  • Mass Transfer
  • Multiphase Flow
  • Navier Stokes Equations
  • Simulations
  • Students
  • Surface Tension
  • Three Dimensional
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Aerosol Science/Aerosol Physics
  • Computational Fluid Dynamics (CFD)
  • Mechanical Engineering/Mechanics of Materials.