Numerical investigation of thermoacoustic combustion instability of high-pressure combustion in rocket engines

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dc.contributor.author	Coclite, Alessandro
dc.contributor.author	Camporeale, Sergio M.
dc.contributor.author	Pascazio, Giuseppe
dc.contributor.author	Laera, Davide	en_US
dc.contributor.other	International Society for Air Breathing Engines
dc.date.accessioned	2015-10-22T15:51:41Z
dc.date.available	2015-10-22T15:51:41Z
dc.date.created	2015	en_US
dc.date.issued	2015-10-22
dc.identifier	20206	en_US
dc.identifier.uri	http://hdl.handle.net/2374.UC/745782
dc.description	This paper is part of the conference proceedings from the 22nd International Symposium on Air Breathing Engines.	en_US
dc.relation.ispartof	ISABE 2015 (Awatef Hamed, Faculty Work and Research, College of Engineering and Applied Science)	en_US
dc.rights	Attribution-NonCommercial-NoDerivs 3.0 United States	en_US
dc.rights.uri	http://creativecommons.org/licenses/by-nc-nd/3.0/us/	en_US
dc.subject	Engineering sciences: Combustion	en_US
dc.subject.lcsh	Airplanes -- Motors	en_US
dc.subject.lcsh	Airplanes -- Jet propulsion	en_US
dc.subject.lcsh	Aircraft gas-turbines	en_US
dc.title	Numerical investigation of thermoacoustic combustion instability of high-pressure combustion in rocket engines	en_US