CRITERION OF THE INSTABILITY OF AN ARBITRARY SYSTEM OF DEFLAGRATION IN THE COMBUSTION CHAMBER OF A ROCKET ENGINE WITH SUCCESSIVE AUTOIGNITION OF THE FUEL (KRITERII NEUSTOICHIVOSTI PROIZVOLNOGO REZHIMA DEFLAGRATSII V KAMERE SGORANIYA RAKETNOGO DVIGATELYA S POSLEDOVATELNYM SAMOVOSPLAMENENIEM TOPLIVA)

Abstract

A criterion is developed for the evaluation of combustion stability in a liquid rocket engine.

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Document Details

Document Type
Technical Report
Publication Date
Nov 29, 1967
Accession Number
AD0675234

Entities

People

  • S. K. Aslanov

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Chambers
  • Chemical Reactions
  • Combustion
  • Combustion Chambers
  • Combustion Products
  • Combustion Stability
  • Combustors
  • Deflagration
  • Endothermic Reactions
  • Engines
  • Fuels
  • Ignition
  • Instability
  • Mach Number
  • Rocket Engines
  • Rockets
  • Translations

Fields of Study

  • Physics

Readers

  • Combustion science or combustion engineering.
  • Information Retrieval