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Response of a Reacting LOx jet to a Transverse Acoustic Oscilllation

Hardi, Justin and Gomez Martinez, H. C. and Oschwald, Michael and Dally, B. (2012) Response of a Reacting LOx jet to a Transverse Acoustic Oscilllation. In: Proceedings. Space Propulsion 2012, 2012-05-07 - 2012-05-10, Bordeaux, France.

Full text not available from this repository.

Abstract

Testing has been conducted in the BKH rocket combustor at the European Research and Technology Test Facility P8 for cryogenic rocket engines at DLR Lampoldshausen.

Item URL in elib:https://elib.dlr.de/77474/
Document Type:Conference or Workshop Item (Speech, Paper)
Title:Response of a Reacting LOx jet to a Transverse Acoustic Oscilllation
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Hardi, JustinUNSPECIFIEDhttps://orcid.org/0000-0003-3258-5261UNSPECIFIED
Gomez Martinez, H. C.Institut für RaumfahrtantriebeUNSPECIFIEDUNSPECIFIED
Oschwald, MichaelUNSPECIFIEDhttps://orcid.org/0000-0002-9579-9825UNSPECIFIED
Dally, B.University of Adelaide, AustraliaUNSPECIFIEDUNSPECIFIED
Date:2012
Journal or Publication Title:Proceedings
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:combustion instabilities, rocket engine, cryogenic, LOx
Event Title:Space Propulsion 2012
Event Location:Bordeaux, France
Event Type:international Conference
Event Start Date:7 May 2012
Event End Date:10 May 2012
Organizer:3AF, ESA, CNES
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Transportation
DLR - Research area:Raumfahrt
DLR - Program:R RP - Space Transportation
DLR - Research theme (Project):R - Antriebsystemtechnik - Schubkammertechnologie (old)
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Rocket Propulsion
Deposited By: Hanke, Michaela
Deposited On:24 Sep 2012 18:00
Last Modified:24 Apr 2024 19:43

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