The Effect of Injection on Nonequilibrium Hypersonic Flow in the Vicinity of the Stagnation Point of a Body with Arbitrary Catalytic Activity of the Surface Including the Effects of Low Reynolds Numbers,

Abstract

The purpose of the paper is to examine the influence of injection on the characteristics of a viscous shock layer that forms between a blunt body and the shock wave during hypersonic flow past the body under conditions of a nonequilibrium dissociation reaction in the gaseous phase and a nonequilibrium recombination reaction on the surface.

Document Details

Document Type
Technical Report
Publication Date
Aug 10, 1973
Accession Number
AD0766042

Entities

People

  • L. A. Ladnova

Organizations

  • National Air and Space Intelligence Center

Tags

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Blunt Bodies
  • Bodies
  • Dissociation
  • Flow
  • Fluid Dynamics
  • Fluid Flow
  • Hypersonic Flow
  • Recombination Reactions
  • Reynolds Number
  • Shock
  • Shock Waves
  • Stagnation Point
  • Waves

Fields of Study

  • Physics

Readers

  • Fluid Dynamics.
  • Organic Chemistry

Technology Areas

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