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Flow Separation in Rocket Nozzles under High Altitude Condition

Stark, Ralf and Génin, C. (2015) Flow Separation in Rocket Nozzles under High Altitude Condition. 30th International Symposium on Shock Waves (ISSW30), 19. - 24. Jul. 2015, Tel Aviv, Israel.

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Item URL in elib:https://elib.dlr.de/99689/
Document Type:Conference or Workshop Item (Speech)
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, C.Chloe.Genin (at) dlr.deUNSPECIFIED
Date:2015
Refereed publication:No
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:nozzle flow, separated flows, altitude simulation
Event Title:30th International Symposium on Shock Waves (ISSW30)
Event Location:Tel Aviv, Israel
Event Type:international Conference
Event Dates:19. - 24. Jul. 2015
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 - ProTAU + Prop2020 Hochleistungstriebwerke
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Rocket Propulsion
Deposited By: Hanke, Michaela
Deposited On:20 Nov 2015 11:05
Last Modified:31 Jul 2019 19:56

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