Experimental Investigation of the Interaction between Strong Shock Waves and Water Droplets.

Abstract

The results of an experimental study on water droplet shock wave interactions are presented. The experimental facility employed on this investigation was the NASA Ames Research Center Electric Arc Shock Tube. Tests were conducted at free stream pressures ranging from 0.13 atm to 0.50 atm and shock velocities varying from 8.4 to 15.5 kfps on spherical droplets having diameters ranging from 53 micrometers to 180 micrometers. Spark shadowgraph pictures over time duration, after passage of the shock, of 4 microsec were obtained with a multiframing image converter camera. The results demonstrate the effects of shock waves on droplet break-up and drag. Correlations were obtained employing dimensionless times and displacements.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1975
Accession Number
ADA035093

Entities

People

  • N. A. Jaffe

Tags

Communities of Interest

  • Energy and Power Technologies
  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Altitude
  • Cameras
  • Electric Arcs
  • Electric Discharges
  • Energy
  • Energy Transfer
  • Free Stream
  • Heat Transfer
  • Image Converters
  • Light Sources
  • Mass Transfer
  • Materials
  • Photographs
  • Photography
  • Shock Waves
  • Signal Generators
  • X Rays

Fields of Study

  • Physics

Readers

  • Aerosol Science/Aerosol Physics
  • Fluid Dynamics.