VORTEX LOOPS IN THE TRAILS BEHIND HYPERVELOCITY PELLETS

Abstract

The periodic shedding of vortices behind bluff bodies in subsonic flow at low Reynolds numbers is a well-known phenomenon. Self-luminous photographs of the hypervelocity trail behind spherical pellets in xenon at a free stream Mach number of about 25 are compared with those of dye-traced incompressible wakes. As a result it is postulated that, as in the subsonic case, vortex loop generation in the body base region is the controlling mechanism for transition to and development of the turbulent hypersonic wake. (Author)

Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1962
Accession Number
AD0274535

Entities

People

  • Aaron Z. Goldberg
  • J.a. Fay

Tags

DTIC Thesaurus Topics

  • Demographic Cohorts
  • Flow
  • Fluid Dynamics
  • Fluid Flow
  • Free Stream
  • Mach Number
  • Photographs
  • Photography
  • Reynolds Number
  • Subsonic Flow
  • Transitions

Fields of Study

  • Physics

Readers

  • Fluid Mechanics and Fluid Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers
  • Hypersonics - Hypersonic Flight