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Flow Separation in Rocket Nozzles under High Altitude Condition

Stark, Ralf and Génin, Chloé (2017) Flow Separation in Rocket Nozzles under High Altitude Condition. Shock Waves, 27 (1), pp. 63-68. Springer. DOI: 10.1007/s00193-016-0631- ISSN 0938-1287

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Item URL in elib:https://elib.dlr.de/117105/
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.dehttps://orcid.org/0000-0003-1923-1901
Génin, ChloéChloe.Genin (at) dlr.dehttps://orcid.org/0000-0002-5752-0643
Date:2017
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
Volume:27
DOI :10.1007/s00193-016-0631-
Page Range:pp. 63-68
Publisher:Springer
ISSN:0938-1287
Status:Published
Keywords:rocket nozzle, high altitude conditions
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:13 Dec 2017 08:04
Last Modified:10 Jan 2019 15:50

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