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Study of LOX/H2 spray flame response to acoustic excitation in a rectangular rocket combustor

Hardi, Justin and Oschwald, Michael and Dally, B.B. (2013) Study of LOX/H2 spray flame response to acoustic excitation in a rectangular rocket combustor. 49th AIAA/ASME/SAE/ASEE Joint PropulsionConference, 14.-17. Jul. 2013, San Jose, USA.

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Item URL in elib:https://elib.dlr.de/87532/
Document Type:Conference or Workshop Item (Speech)
Title:Study of LOX/H2 spray flame response to acoustic excitation in a rectangular rocket combustor
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Hardi, JustinJustin.Hardi (at) dlr.dehttps://orcid.org/0000-0003-3258-5261
Oschwald, MichaelMichael.Oschwald (at) dlr.dehttps://orcid.org/0000-0002-9579-9825
Dally, B.B.University of Adelaide, South AustraliaUNSPECIFIED
Date:July 2013
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:rocket propulsion
Event Title:49th AIAA/ASME/SAE/ASEE Joint PropulsionConference
Event Location:San Jose, USA
Event Type:international Conference
Event Dates:14.-17. Jul. 2013
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Transport
DLR - Research area:Raumfahrt
DLR - Program:R RP - Raumtransport
DLR - Research theme (Project):R - Antriebsystemtechnik - Schubkammertechnologie
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Rocket Propulsion
Deposited By: Hanke, Michaela
Deposited On:13 Jan 2014 15:41
Last Modified:01 Dec 2018 19:50

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