6   Artículos

 
en línea
Jiangge Deng, Ting Li, Jinkui Wang and Chicheng Gao    
Thermoacoustic instabilities occur when heat release is coupled with pressure fluctuation, which may cause performance degradation of the combustor and serious structural damage. This study focued on an active control method using discharge plasma and sh... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Jiaqi Nan, Jingxuan Li and Lijun Yang    
Cylindrical ducts with axial mean temperature gradient and mean flows are typical elements in rocket engines, can combustors, and afterburners. Accurate analytical solutions for the acoustic waves of the longitudinal and transverse modes within these duc... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Yuze Sun, Dan Zhao and Xiaowei Zhu    
In the present work, 3D Unsteady Reynolds-Averaged Navier-Stokes (URANS) simulations are performed to investigate the generation and mitigation mechanism of combustion-sustained thermoacoustic instabilities in a modelled swirl combustor. The effects of (... ver más
Revista: Aerospace    Formato: Electrónico

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