NONLINEAR ASPECTS OF COMBUSTION INSTABILITY IN LIQUID PROPELLANT ROCKET MOTORS

Abstract

Contents: Injection orientation Sector motor (Variable-angle) Sector motor (Variable-length) Pulsed limits tests Effect of the approximation to the velocity distribution in instability calculations Determination of characteristics velocity with cooled exhaust nozzle Basic pulse studies Nonlinear transverse combustion instability Some effects of injection droplet variation and vaporization rate perturbations on combustion instability Significance of the Quasi-Steady-State Assumption in droplet vaporization theory

Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1962
Accession Number
AD0287987

Entities

People

  • David T. Harrje
  • W.c. Strahle
  • William A. Sirignano

Organizations

  • Princeton University

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Combustion
  • Exhaust Nozzles
  • Instability
  • Liquid Propellants
  • Nozzles
  • Orientation (Direction)
  • Perturbations
  • Propellants
  • Rocket Engines
  • Rockets
  • Steady State
  • Transverse
  • Vaporization

Fields of Study

  • Physics

Readers

  • Combustion science or combustion engineering.
  • Fluid Dynamics.
  • Rocket Propulsion.