Time-domain characterization of the acoustic damping of a perforated liner with bias flow

Combustioninstabilities are caused by the interaction of unsteady heat releases and acoustic waves. To mitigate combustioninstabilities, perforated liners, typically subjected to a low Mach number bias flow (a cooling flow through perforated holes), are fitted along the bounding walls of a combustor...

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Bibliographic Details
Main Authors: Zhong, Zhiyuan, Zhao, Dan
Other Authors: School of Mechanical and Aerospace Engineering
Format: Journal Article
Language:English
Published: 2014
Subjects:
Online Access:https://hdl.handle.net/10356/101573
http://hdl.handle.net/10220/18696

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