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Untersuchung der Injektor-Akustik mittels Netzwerk und FEM Modellierung einer experimentellen Raketenbrennkammer mit kryogener LOx/H2 Verbrennung - Investigation of the acoustics in the injector through network and FEA modelling of an experimental rocket combustor with cryogenic LOx/H2 propellants

Gradetzke, Malte (2016) Untersuchung der Injektor-Akustik mittels Netzwerk und FEM Modellierung einer experimentellen Raketenbrennkammer mit kryogener LOx/H2 Verbrennung - Investigation of the acoustics in the injector through network and FEA modelling of an experimental rocket combustor with cryogenic LOx/H2 propellants. Bachelor's. DLR-Interner Bericht. DLR-IB-RA-LA-2016-343.

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Item URL in elib:https://elib.dlr.de/109571/
Document Type:Monograph (DLR-Interner Bericht, Bachelor's)
Title:Untersuchung der Injektor-Akustik mittels Netzwerk und FEM Modellierung einer experimentellen Raketenbrennkammer mit kryogener LOx/H2 Verbrennung - Investigation of the acoustics in the injector through network and FEA modelling of an experimental rocket combustor with cryogenic LOx/H2 propellants
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Gradetzke, MalteDLR Institut für Raumfahrtantriebe, RaketenantriebeUNSPECIFIED
Date:2016
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:Raketenbrennkammer, FEM, kryogen, Injektor
Institution:Universität Stuttgart
Department:Institut für Raumfahrtsysteme
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:14 Dec 2016 07:53
Last Modified:14 Dec 2016 07:53

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