ROCKET EXHAUST INTO A HYPERVELOCITY STREAM. FAR FIELD ANALYSIS

Abstract

Far field of a rocket jet exhausting into a surrounding medium moving at hypervelocity is analyzed using the compressible turbulent NavierStokes equations simplified by the boundary layer approximations. (Author)

Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1962
Accession Number
AD0272813

Entities

People

  • Hideo Yoshihara

Organizations

  • General Dynamics

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Boundaries
  • Boundary Layer
  • Equations
  • Far Field
  • Layers
  • Rocket Exhaust

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.
  • Fluid Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers