EFFECTS OF A MAGNETIC FIELD ON THE HYPERVELOCITY FLOW ABOUT A BLUNT BODY,

Abstract

An experimental investigation was made of the effect of an applied magnetic field on the bow shock of a blunt body in hypervelocity air flow. Quantitative measurements of the stand-off distance were made in a three-inch electromagnetic shock tube with free-stream velocities up to 22,000 feet per second. The test body was a hemispherical cylinder containing a coaxial pulsed magnet coil in the nose which produced field strengths at the stagnation point of up to 40 kilogauss. The application of the magnetic field displaced the bow shock upstream and the stand-off distance increased by a factor of 7.5 for the condition, nondimensional parameter = 69. The experimental results were compared with theory and good agreement was obtained within the range of experimental conditions. (Author)

Document Details

Document Type
Technical Report
Publication Date
Aug 27, 1958
Accession Number
AD0606333

Entities

People

  • Richard W. Ziemer

Organizations

  • TRW Inc.

Tags

DTIC Thesaurus Topics

  • Air Flow
  • Blunt Bodies
  • Bodies
  • Bow Shock
  • Flow
  • Fluid Dynamics
  • Fluid Flow
  • Free Stream
  • Hypervelocity Flow
  • Magnet Coils
  • Magnetic Fields
  • Shock
  • Shock Tubes
  • Stagnation Point

Fields of Study

  • Physics

Readers

  • Explosive Engineering.
  • Fluid Dynamics.
  • Superconducting Magnet Technology

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow