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Numerical Model for Nozzle Flow Application under LOX/Methane Hot Flow Conditions

Schneider, Dirk and Génin, Chloé and Stark, Ralf and Oschwald, Michael and Karl, Sebastian and Hannemann, Volker (2017) Numerical Model for Nozzle Flow Application under LOX/Methane Hot Flow Conditions. Journal of Propulsion and Power. American Institute of Aeronautics and Astronautics (AIAA). DOI: 10.2514/1.B36611 ISSN 0748-4658

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Item URL in elib:https://elib.dlr.de/117058/
Document Type:Article
Title:Numerical Model for Nozzle Flow Application under LOX/Methane Hot Flow Conditions
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Schneider, DirkDirk.Schneider (at) dlr.dehttps://orcid.org/0000-0002-4785-4244
Génin, Chloéchloe.genin (at) dlr.dehttps://orcid.org/0000-0002-5752-0643
Stark, RalfRalf.Stark (at) dlr.dehttps://orcid.org/0000-0003-1923-1901
Oschwald, MichaelMichael.Oschwald (at) dlr.dehttps://orcid.org/0000-0002-9579-9825
Karl, SebastianSebastian.Karl (at) dlr.deUNSPECIFIED
Hannemann, VolkerVolker.Hannemann (at) dlr.deUNSPECIFIED
Date:2017
Journal or Publication Title:Journal of Propulsion and Power
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:Yes
DOI :10.2514/1.B36611
Publisher:American Institute of Aeronautics and Astronautics (AIAA)
ISSN:0748-4658
Status:Published
Keywords:rocket nozzle, nozzle flow
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: Göttingen , Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Rocket Propulsion
Institute for Aerodynamics and Flow Technology > Spacecraft, GO
Deposited By: Hanke, Michaela
Deposited On:11 Dec 2017 16:27
Last Modified:08 Mar 2018 18:45

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