Governed by: Ministry of Industry and Information Technology of the People's Republic of China
Sponsored by: Northwestern Polytechnical University  Chinese Society Aeronautics and Astronautics
Address: Aviation Building,Youyi Campus, Northwestern Polytechnical University
Critical Experimental Research on Liquid Rocket Engine Combustion Instabilities
DOI:
Author:
Affiliation:

Zhang Minqing1,Zhang Mengzheng2,Mao Genwang1(1.School of Astronautics,Northwestern Polytechnical University,Xi'an 710072,China)(2.The Xi'an Aerospace Propulsion Institute,Xi'an 710100,China)

Clc Number:

V434+.13

Fund Project:

  • Article
  • |
  • Figures
  • |
  • Metrics
  • |
  • Reference
  • |
  • Related
  • |
  • Cited by
  • |
  • Materials
  • |
  • Comments
    Abstract:

    In this paper,the combustion wave is produced by a pulse gun in the liquid rocket engine combustion chamber;the pulsating pressure and mechanism vibration of the chamber are recorded by the experimental data record and analysis system;and the damping ratio of pulsating pressure is obtained.The damping ratio is compared with parameter of congener engine.The experimental result indicates that the combustion process of the engine chamber is stable for pulsate disturbing.

    Reference
    Related
    Cited by
Get Citation

Zhang Minqing, Zhang Mengzheng, Mao Genwang. Critical Experimental Research on Liquid Rocket Engine Combustion Instabilities[J]. Advances in Aeronautical Science and Engineering,2011,2(2):

Copy
Share
Article Metrics
  • Abstract:
  • PDF:
  • HTML:
  • Cited by:
History
  • Received:
  • Revised:
  • Adopted:
  • Online: January 13,2012
  • Published: