Analysis of the Flow Interactions between Large Water Droplets and Air in Droplet Acceleration Nozzles

Abstract

The conditions under which large drops, on the order of 150 micron in diameter, are formed from high-velocity liquid jets and their subsequent behavior in high-velocity airstreams are discussed. The quasi-one-dimensional equations for fully coupled two-phase turbulent flow of a noncondensable gas with evaporating droplets in a convergent-divergent nozzle are formulated. Droplet performance predictions for the Dust Erosion Tunnel (DET) are reviewed in the light of existing two-phase flow test data. Criteria for the aerodynamic design of a droplet acceleration nozzle that would inhibit droplet breakup are developed and used for studying the performance of a droplet acceleration nozzle in the AEDC High Enthalpy Arc Tunnel (HEAT) test facility (H-1) and the DET facility. The conclusion is that although acceleration of large drops without breakup is feasible, many problems will have to be solved to obtain high droplet velocities with large droplets.

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Document Details

Document Type
Technical Report
Publication Date
May 01, 1980
Accession Number
ADA085114

Entities

People

  • P. A. Kessel

Organizations

  • Arnold Engineering Development Complex

Tags

Communities of Interest

  • Materials and Manufacturing Processes
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aerodynamic Forces
  • Air Force
  • Boundary Layer
  • Coefficients
  • Computational Fluid Dynamics
  • Crystal Structure
  • Energy
  • Energy Transfer
  • Engineering
  • Equations
  • Equations Of State
  • Heat Energy
  • Heat Transfer
  • Latent Heat
  • Phase Transformations
  • Pressure Measurement
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Aerosol Science/Aerosol Physics
  • Combustion and Flow Dynamics.
  • Fluid Dynamics.