DLR-Logo -> http://www.dlr.de
DLR Portal Home | Imprint | Contact | Deutsch
Fontsize: [-] Text [+]

Response of a Reacting LOx jet to a Transverse Acoustic Oscilllation

Hardi, J. and Gomez Martinez, H. C. and Oschwald, M. and Dally, B. (2012) Response of a Reacting LOx jet to a Transverse Acoustic Oscilllation. In: Proceedings. Space Propulsion 2012, 7. - 10. Mai 2012, Bordeaux, France.

Full text not available from this repository.


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.

Document Type:Conference or Workshop Item (Speech, Paper)
Title:Response of a Reacting LOx jet to a Transverse Acoustic Oscilllation
AuthorsInstitution or Email of Authors
Hardi, J.Justin.Hardi@dlr.de
Gomez Martinez, H. C.Institut für Raumfahrtantriebe
Oschwald, M.Michael.Oschwald@dlr.de
Dally, B.University of Adelaide, Australia
Journal or Publication Title:Proceedings
Refereed publication:Yes
In ISI Web of Science:No
Keywords:combustion instabilities, rocket engine, cryogenic, LOx
Event Title:Space Propulsion 2012
Event Location:Bordeaux, France
Event Type:international Conference
Event Dates:7. - 10. Mai 2012
Organizer:3AF, ESA, CNES
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 > Raketenantriebe
Deposited By: Michaela Hanke
Deposited On:24 Sep 2012 18:00
Last Modified:04 Nov 2012 09:11

Repository Staff Only: item control page

Help & Contact
electronic library is running on EPrints 3.3.12
Copyright © 2008-2012 German Aerospace Center (DLR). All rights reserved.