PARAMETRIC STUDY OF ROCKET INSTABILITY.

Abstract

The research program was concerned with (1) the problem of high frequency longitudinal pressure oscillations in premixed gaseous propellant combustors and (2) the steady-state and stability operating characteristics of bi-phase propellant rocket combustors operating at sub-critical conditions. Both analytical and experimental work were performed in order to study the aforementioned problems. (Author)

Document Details

Document Type
Technical Report
Publication Date
Feb 15, 1968
Accession Number
AD0829888

Entities

People

  • D. W. Netzer
  • J .r. Osborn

Organizations

  • Purdue University

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Combustors
  • Frequency
  • Frequency Bands
  • Instability
  • Oscillation
  • Propellants
  • Radio Frequency
  • Steady State

Fields of Study

  • Physics

Readers

  • Atmospheric Science / Meteorology, specifically Wind Wave Turbulence.
  • Internal Combustion Engine (ICE) Technology.
  • Rocket Propulsion.