CHEMICAL NON-EQUILIBRIUM SHOCK FLOW,

Abstract

The problem of calculating the flow behind a normal shock front is discussed. The additional complication of finite reaction rate chemistry has been included. A numerical method and several results of flow across a shock wave with an eleven-species, thirteen reaction model of air are presented. Results of the method are discussed and compared with those of Hall, Escheroeder, and Marrone (inviscid hypersonic air flows with coupled non-equilibrium processes. IAS 30th annual meeting, Jan 1962). (Author)

Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1963
Accession Number
AD0421018

Entities

People

  • V. A. Langelo

Organizations

  • General Electric

Tags

DTIC Thesaurus Topics

  • Air Flow
  • Chemical Reaction Properties
  • Chemistry
  • Flow
  • Shock
  • Shock Waves
  • Waves

Readers

  • Clinical Trial Research.
  • Combustion Dynamics and Shock Wave Physics.
  • Fluid Dynamics.

Technology Areas

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