An Approach of Preventing Combustion Vibrations of Rocket Engine with Lateral Baffle,

Abstract

In the process of developing the variable thrust rocket engine, combustion vibrations are encountered in the low end of the operating conditions. We used a lateral baffle to satisfactorily solve the problem. This paper mainly introduces the experimental results and qualitative analysis. The approach is novel. It can be used as a reference. (Keywords: rocket engines)

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Document Details

Document Type
Technical Report
Publication Date
Mar 25, 1987
Accession Number
ADA179222

Entities

People

  • Di. Lianshun
  • Xing Fuyuan

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Amplitude
  • Chambers
  • Combustion
  • Combustion Chambers
  • Control Systems
  • Efficiency
  • Engines
  • Feedback
  • Flow
  • Flow Rate
  • Foreign Technology
  • High Temperature
  • Pressure Transducers
  • Propellants
  • Rocket Engines
  • Rockets
  • Thrust Chambers

Fields of Study

  • Engineering

Readers

  • Combustion science or combustion engineering.
  • Control Systems Engineering.
  • Military Engineering.