COMBUSTION INSTABILITY IN LIQUID PROPELLANT ROCKET ENGINES.

Abstract

The investigation is concerned with the development of a theoretical model for combustion instability, in the longitudinal mode, occurring in liquid propellant rocket engines that are employed in current practice. Experimental results are used both to help generate realistic physical models for combustion-wave phenomena in heterogeneously reacting systems, and for subsequent verification of theoretical results. (Author)

Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1966
Accession Number
AD0645634

Entities

People

  • Sanford S. Hammer
  • Vito D. Agosta

Organizations

  • New York University Tandon School of Engineering

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Combustion
  • Energetic Materials
  • Engines
  • Instability
  • Liquid Propellant Rocket Engines
  • Liquid Propellants
  • Liquid Rocket Propellants
  • Propellants
  • Rocket Engines
  • Rocket Propellants
  • Rockets
  • Wave Phenomena

Fields of Study

  • Physics

Readers

  • Atmospheric Science / Meteorology, specifically Wind Wave Turbulence.
  • Combustion science or combustion engineering.
  • Systems Analysis and Design