DISTORTION OF A SHOCK WAVE TRAVERSED BY A VORTEX,

Abstract

A theoretical treatment of the sound field produced upon the interaction of a vortex and a normal shock wave was presented some time ago in UTIA Report No. 61 (H.S. Ribner, 1959). The techniques of this analysis are used to derive expressions for the shape of the distorted shock front. It is found that outside of the section cut off by the cylindrical acoustic wave emanating from the vortex center, the shock remains essentially straight. The portion within this section has curvature, resulting in a finite displacement of the two straight segments. These theoretical predictions are in qualitative agreement with the features noted by experimental investigators of the same phenomenon. As no other presently published theory yields the shock wave shape, this work demonstrates the generality of the approach used. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1967
Accession Number
AD0646759

Entities

People

  • L. T. Filotas

Organizations

  • University of Toronto

Tags

DTIC Thesaurus Topics

  • Acoustic Waves
  • Agreements
  • Curvature
  • Displacement
  • Distortion
  • Geometry
  • Shape
  • Shock
  • Shock Waves
  • Waves

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Combustion Dynamics and Shock Wave Physics.
  • Theoretical Analysis.