摘要
Combustion noise in propulsion systems, particularly in choked-nozzle combustion chambers, remains a critical challenge for propulsion system design. This study extends the semi-analytical approach of Duran et al. from subsonic to choked-nozzle conditions, developing a theoretical model to predict direct and indirect noise. A cylindrical model combustion chamber with a choked throat is investigated, incorporating entropy wave dissipation and acoustic wave attenuation. The model is validated against Domenico's experimental data, demonstrating errors within 4.6 % for indirect noise and 0.49 % for direct noise. This investigation systematically evaluates three critical factors governing combustion noise generation: Combustion chamber geometry effects, Flow field parameter variations and Unsteady heat release characteristics. The developed semi-analytical methodology provides fundamental insights into noise generation mechanisms and propagation dynamics in choked-nozzle systems.
| 源语言 | 英语 |
|---|---|
| 期刊论文编号 | 110635 |
| 期刊 | Aerospace Science and Technology |
| 卷 | 167 |
| DOI | |
| 出版状态 | 已出版 - 12月 2025 |
| 已对外发布 | 是 |
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