Nonlinear combustion instability analysis method of solid rocket motor

被引：0
|
作者：
Liu, Pei-Jin [1 ]
Wei, Shao-Juan [1 ]
Yang, Shang-Rong [1 ]
机构：
[1] Science and Technology on Combustion, Internal Flow and Thermal-Structure Laboratory, Northwestern Polytechnical University, Xi'an 710072, China
来源：
Guti Huojian Jishu/Journal of Solid Rocket Technology | 2013年 / 36卷 / 03期
关键词：
Calculation programs - Calculation results - Combustion characteristics - Combustion instabilities - Experimental datum - Nonlinear instability - Prediction methods - Solid rocket motors;
D O I：
10.7673/j.issn.1006-2793.2013.03.004
中图分类号：
学科分类号：
摘要：
A nonlinear instability prediction method based on energy balance theory was derived to predict nonlinear combustion characteristics of solid rocket motor: limit cycle and DC shift. A cylindrical solid rocket motor was selected to construct the physical and mathematical model. Blomshield's stability testing was chosen to validate the model and calculation program. The calculation results agree well with the experimental data in a certain degree. The sensitivity of important parameters such as chamber radius and burning rate was analyzed to study their effects on the instability of the motor.
引用
下载
收藏
页码：302 / 309
相关论文
共 50 条
  • [1] Mache effect and combustion instability in solid rocket motor
    Assovskiy, IG
    Rashkovskiy, SA
    JOURNAL OF PROPULSION AND POWER, 1999, 15 (06) : 856 - 860
  • [2] Combustion instability at end of burning in a solid rocket motor
    School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China
    不详
    Hangkong Dongli Xuebao, 2013, 10 (2376-2383):
  • [3] Impacts of Flight Acceleration on Combustion Instability of Solid Rocket Motor
    Zhang X.-Y.
    Gao B.
    Gan X.-S.
    Ma L.
    Zhou Y.-Q.
    Yuhang Xuebao/Journal of Astronautics, 2019, 40 (08): : 972 - 976
  • [4] Combustion Instability and LES Analysis in Hybrid Rocket Motor
    Bohoon, Kim
    Changjin, Lee
    Na, Yang
    PROCEEDINGS OF 2010 ASIA-PACIFIC INTERNATIONAL SYMPOSIUM ON AEROSPACE TECHNOLOGY, VOL 1 AND 2, 2010, : 367 - +
  • [5] Numerical study of triggered thermoacoustic instability driven by linear and nonlinear combustion response in a solid rocket motor
    Xu, Guanyu
    Wang, Bing
    Jin, Bingning
    Wang, Zhuopu
    Liu, Peijin
    PHYSICS OF FLUIDS, 2024, 36 (03)
  • [6] Coning instability analysis of spinning solid rocket motor
    Gao, Ye
    Yang, Dan
    Xiong, Yong-Liang
    Yuhang Xuebao/Journal of Astronautics, 2008, 29 (01): : 270 - 275
  • [7] APPLICATION OF COMBUSTION INSTABILITY TECHNOLOGY TO SOLID-PROPELLANT ROCKET MOTOR PROBLEMS
    BROWNING, SC
    THACHER, JH
    KRASHIN, M
    JOURNAL OF SPACECRAFT AND ROCKETS, 1972, 9 (05) : 293 - &
  • [8] A study on combustion instability of solid rocket motor with cylinder-slot grain
    Lee, Dohyung
    Kim, Hongjip
    JOURNAL OF THE ACOUSTICAL SOCIETY OF KOREA, 2020, 39 (04): : 371 - 377
  • [9] Inert Particles for Axial-Combustion-Instability Suppression in a Solid Rocket Motor
    Greatrix, David R.
    JOURNAL OF PROPULSION AND POWER, 2008, 24 (06) : 1347 - 1354
  • [10] Combustion instability in a small liquid rocket motor
    Osherov, A
    Natan, B
    AERONAUTICAL JOURNAL, 1999, 103 (1023): : 245 - 252
12345