TY - GEN
T1 - Critical Parametric Studies of Combustion Instability in Solid Rocket Motors
AU - Lou, Yongchun
AU - Ji, Xiaoting
AU - Liu, Peijin
AU - Yin, Shengjie
AU - Cao, Qin Liu
N1 - Publisher Copyright:
© 2023 IEEE.
PY - 2023
Y1 - 2023
N2 - Vortex shedding, combustion response and damping can cause combustion instability under some conditions. In this paper, several mechanisms that cause combustion instability, including the geometry of the solid rocket motors (SRMs), the combustion response of the propellant, particle damping, and nozzle damping, are investigated. Specifically, the influence of the slot of the grains on the chamber acoustic mode, the content of aluminum on the combustion response and particle distribution, and the nozzle throat diameter on the nozzle damping are parametrically analyzed, respectively. Moreover, the critical parametric test in the SRM with a large length-To-diameter ratio is carried out. The results prove that the evaluation method promoted in this study can be used in the prediction of combustion instability in the SRMs.
AB - Vortex shedding, combustion response and damping can cause combustion instability under some conditions. In this paper, several mechanisms that cause combustion instability, including the geometry of the solid rocket motors (SRMs), the combustion response of the propellant, particle damping, and nozzle damping, are investigated. Specifically, the influence of the slot of the grains on the chamber acoustic mode, the content of aluminum on the combustion response and particle distribution, and the nozzle throat diameter on the nozzle damping are parametrically analyzed, respectively. Moreover, the critical parametric test in the SRM with a large length-To-diameter ratio is carried out. The results prove that the evaluation method promoted in this study can be used in the prediction of combustion instability in the SRMs.
KW - combustion instability
KW - combustion response
KW - evaluation method
KW - solid rocket motor
UR - http://www.scopus.com/inward/record.url?scp=85186745970&partnerID=8YFLogxK
U2 - 10.1109/ICMAE59650.2023.10424509
DO - 10.1109/ICMAE59650.2023.10424509
M3 - 会议稿件
AN - SCOPUS:85186745970
T3 - 2023 14th International Conference on Mechanical and Aerospace Engineering, ICMAE 2023
SP - 272
EP - 277
BT - 2023 14th International Conference on Mechanical and Aerospace Engineering, ICMAE 2023
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 14th International Conference on Mechanical and Aerospace Engineering, ICMAE 2023
Y2 - 18 July 2023 through 21 July 2023
ER -