On the Similarity Between Combustion in a Detonation Wave and in a Rocket Motor - USSR -

Abstract

Thermal gas dynamic anlysis of an average image of the combustion process in a rocket engine (RE) shows that the deflagration leg of Hugoniot's curve can be considered as a locus of points each of which uniquely corresponds to a definite degree of the reheating condition of coombustion tbe RE chamber.

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Document Details

Document Type
Technical Report
Publication Date
May 27, 1960
Accession Number
ADA362119

Entities

People

  • K. T I. Scohelkin
  • Ya K. Toshin
  • Yu. N. Denisov

Organizations

  • Joint Publications Research Service

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Autoignition
  • Band Structures
  • Burning Rate
  • Chambers
  • Chemical Reaction Properties
  • Chemical Reactions
  • Combustion
  • Combustion Chambers
  • Combustion Products
  • Coordinate Systems
  • Detonation Waves
  • Equations
  • Frequency
  • Ignition
  • Ignition Lag
  • Rocket Engines
  • Shock Waves

Fields of Study

  • Physics

Readers

  • Combustion Dynamics and Shock Wave Physics.
  • Combustion and Flow Dynamics.