Computational Studies of Evaporating Sprays in a Shear Layer

Abstract

The objective of the research project was to numerically predict the characteristics of evaporating sprays in a turbulent shear layer. The calculations were performed such that the essential physical processes in spray evaporation in gas turbine combustors are adequately realized . The calculations modeled parallel experiments (ARO Contract number DAAG29-84-K-0165)carried out in a vertically down-flowing wind tunnel where a splitter plate separates two air streams having different velocities. The two air streams meet at the end of the splitter plate and give rise to a confined shear layer. A flat prefilming airblast atomizer is located at the trip of the splitter plate. A liquid spray formed at the atomizer tip evaporates in the turbulent shear layer and is convected downstream. An Eulerian description of the turbulent gas phase flow and a Lagrangian formulation of the droplet size class motion and heat and mass transfer were considered. Single phase two dimensional turbulent flow calculations in a duct were considered. Spray evaporation, turbulent shear layers, computational methods.

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Document Details

Document Type
Technical Report
Publication Date
Oct 21, 1988
Accession Number
ADA201932

Entities

People

  • Bakhtier Farouk

Organizations

  • Drexel University

Tags

Communities of Interest

  • Energy and Power Technologies
  • Weapons Technologies

DTIC Thesaurus Topics

  • Boundary Layer
  • Computational Fluid Dynamics
  • Computational Science
  • Differential Equations
  • Distribution Functions
  • Equations
  • Equations Of Motion
  • Flow Fields
  • Fluid Dynamics
  • Fluid Mechanics
  • Gas Turbines
  • Heat Transfer
  • Mass Transfer
  • Turbines
  • Turbulence
  • Turbulent Flow
  • Turbulent Mixing

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.
  • Fluid Mechanics and Fluid Dynamics.
  • Internal Combustion Engine (ICE) Technology.