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Flow separation in rocket nozzles under high altitude condition

Stark, Ralf and Génin, Chloé (2016) Flow separation in rocket nozzles under high altitude condition. Shock Waves. Springer. DOI: 10.1007/s00193-016-0631-6 ISSN 0938-1287

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Item URL in elib:https://elib.dlr.de/107804/
Document Type:Article
Title:Flow separation in rocket nozzles under high altitude condition
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Stark, RalfRalf.Stark (at) dlr.deUNSPECIFIED
Génin, ChloéChloe.Genin (at) dlr.deUNSPECIFIED
Date:2016
Journal or Publication Title:Shock Waves
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:Yes
DOI :10.1007/s00193-016-0631-6
Publisher:Springer
ISSN:0938-1287
Status:Published
Keywords:rocket nozzle, flow Separation, high altitude
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:16 Nov 2016 07:51
Last Modified:10 Jan 2019 15:50

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