AN ANOMALOUS EFFECT OF MAGNETIC FIELD ON STAGNATION-POINT HEAT-TRANSFER IN A SUPERSONIC PLASMA.

Abstract

An investigation of the effect of a dipole-like magnetic field on heat transfer to a forward stagnation point in a Mach 3 Argon plasma has led to a surprising result. Rather than indicating a change in heat transfer coefficient, the measurements point to a change in the flow field of such a nature that the effective recovery temperature of the gas at the stagnation point is reduced. This effect is much larger than that which present continuum theory predicts, is dependent on conditions upstream of the test section and is also a function of magnetic field direction. (Author)

Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1964
Accession Number
AD0609214

Entities

People

  • S. A. Gordon

Tags

DTIC Thesaurus Topics

  • Coefficients
  • Flow
  • Flow Fields
  • Heat Transfer
  • Heat Transfer Coefficients
  • Magnetic Fields
  • Measurement
  • Recovery
  • Stagnation Point

Fields of Study

  • Physics

Readers

  • Fluid Dynamics.
  • Mathematics or Statistics
  • Plasma Physics / Magnetohydrodynamics

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flight
  • Hypersonics - Hypersonic Flow