Multiple time scale analysis of pressure oscillations in solid rocket motors

被引:2
|
作者
Ahmed, Waqas [1 ]
Maqsood, Adnan [1 ]
Riaz, Rizwan [1 ]
机构
[1] Natl Univ Sci & Technol NUST, Res Ctr Modeling & Simulat, H-12 Campus, Islamabad 44000, Pakistan
关键词
COMBUSTION-CHAMBERS; MODEL;
D O I
10.1016/j.rinp.2018.01.033
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
In this study, acoustic pressure oscillations for single and coupled longitudinal acoustic modes in Solid Rocket Motor (SRM) are investigated using Multiple Time Scales (MTS) method. Two independent time scales are introduced. The oscillations occur on fast time scale whereas the amplitude and phase changes on slow time scale. Hopf bifurcation is employed to investigate the properties of the solution. The supercritical bifurcation phenomenon is observed for linearly unstable system. The amplitude of the oscillations result from equal energy gain and loss rates of longitudinal acoustic modes. The effect of linear instability and frequency of longitudinal modes on amplitude and phase of oscillations are determined for both single and coupled modes. For both cases, the maximum amplitude of oscillations decreases with the frequency of acoustic mode and linear instability of SRM. The comparison of analytical MTS results and numerical simulations demonstrate an excellent agreement. (C) 2018 The Authors. Published by Elsevier B.V.
引用
收藏
页码:1068 / 1075
页数:8
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