DIFFRACTION AND PROPAGATION OF A PLANE SHOCK WAVE AT A FREE SURFACE.

Abstract

The propagation of shock waves in stratified media finds important application in the oceans and upper atmosphere. Such shocks or blast waves may be formed by supersonically traveling vehicles or as a direct consequence of strong explosions. This work is divided into two parts. The first part examines the motion of an initially uniform shock front traveling parallel to the y-axis. At time t=0, the shock crosses the free interface (y=0) separating a homogeneous fluid in the upper half-plane (x>0, y>0) from a different homogeneous fluid in the lower half-plane (x>0, y<0). The subsequent motion of the shock front is determined as it propagates through two fluids. The interaction obtained depends on the initial speed of the shock relative to the sound speeds or more generally on the acoustic impedances in each of the two media. The second part deals with the motion of the shock itself which may be approximated by Whitham's method, using a coordinate system consisting of a network formed by successive shock wave positions on one hand, and the orthogonal trajectory to the shock on the other. The diffracted shock is found to be surprisingly uniform, except in the vicinity of the free surface and the undisturbed shock, where it undergoes large changes in curvature. The work provides the possibility of extension to shock propagation in general stratified media. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1969
Accession Number
AD0690919

Entities

People

  • Michael Hsiang-ten Chen
  • Richard L Collins

Organizations

  • University of California, Los Angeles

Tags

DTIC Thesaurus Topics

  • Acoustic Impedance
  • Atmospheres
  • Blast
  • Blast Waves
  • Coordinate Systems
  • Curvature
  • Diffraction
  • Explosions
  • Geometry
  • Impedance
  • Shock
  • Shock Waves
  • Trajectories
  • Waves

Fields of Study

  • Physics

Readers

  • Atmospheric Science / Meteorology, specifically Wind Wave Turbulence.
  • Combustion Dynamics and Shock Wave Physics.
  • Electromagnetic Wave Scattering and Antenna Radiation Engineering

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers
  • Hypersonics - Hypersonic Flow