Theoretical Temperature Distribution in the Precursor Region Ahead of Projectiles Traveling at Hypersonic Velocities.

Abstract

An attempt is made to obtain order-of-magnitude estimates of the radiant intensity profiles for the precursor region of a gas, ahead of a hypervelocity shock wave. An approximate expression for the temperature distribution in the precursor is derived for the case where gamma is very large. The parameter, gamma, appears in the nondimensionalization of the flow equations. The importance of radiative heat transfer relative to convective heat transfer is characterized by the size of gamma. The approximation for the temperature is then used to predict the radiant intensity profile in the precursor for a specific example. The values of the parameters used for the calculation were chosen from a prior experiment in which the profile was measured. (Author)

Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1970
Accession Number
AD0718641

Entities

People

  • Wallace Henry Clay

Organizations

  • Ballistic Research Laboratory

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Equations
  • Heat Transfer
  • Hypersonic Velocity
  • Intensity
  • Precursors
  • Projectiles
  • Radiant Intensity
  • Shock
  • Shock Waves
  • Waves

Fields of Study

  • Physics

Readers

  • Fluid Dynamics.
  • Solar Physics

Technology Areas

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