Interaction between the acoustic pressure fluctuations and the unsteady flow field through circular holes

Gas turbine combustion systems are prone to thermo-acoustic instabilities, and this is particularly the case for new low emission lean burn type systems. The presence of such instabilities is basically a function of the unsteady heat release within the system (i.e., both magnitude and phase) and the...

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Bibliographic Details

Main Authors:	Jochen Rupp, Jon Carrotte, Adrian Spencer
Format:	Default Article
Published:	2010
Subjects:	Aerospace engineering not elsewhere classified Mechanical engineering not elsewhere classified Other engineering not elsewhere classified untagged Aerospace Engineering Mechanical Engineering Engineering not elsewhere classified
Online Access:	https://hdl.handle.net/2134/6111
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