Abstract
The problem of thermoacoustic instabilities in the combustor of modern air-breathing engines has become a topic of concern, which occurs as a result of unstable coupling between the heat release fluctuations and acoustic perturbations. A three-dimensional thermoacoustic model including the distributed non-uniform heat source and non-uniform flow is developed based on the domain decomposition spectral method. The importance of distributed heat source on combustion instabilities of longitudinal modes is analyzed with the help of a simplified geometrical configuration of combustor. The results show that the longitudinal distribution of heat source has a crucial effect on instabilities. In addition, the effect of circumferentially non-uniform heat source and non-uniform flow on longitudinal instabilities is also investigated. It can be found that the influence of circumferential non-uniformity can become significant on the lowest frequency instabilities, in particular, the oscillation frequency and growth rate are all evidently affected by temperature non-uniformity and time delay non-uniformity.
| Original language | English |
|---|---|
| Pages (from-to) | 3098-3111 |
| Number of pages | 14 |
| Journal | Journal of Sound and Vibration |
| Volume | 332 |
| Issue number | 12 |
| DOIs | |
| State | Published - 10 Jun 2013 |
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