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Flow separation study in stiff ovalized rocket nozzles, Part I: experimental approach

Génin, C. and Jack, Sebastian (2015) Flow separation study in stiff ovalized rocket nozzles, Part I: experimental approach. 51st AIAA Joint Propulsion Conference, 27. - 29. Jul. 2015, Orlando, FL, USA.

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Item URL in elib:https://elib.dlr.de/99608/
Document Type:Conference or Workshop Item (Speech)
Title:Flow separation study in stiff ovalized rocket nozzles, Part I: experimental approach
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Génin, C.Chloe.Genin (at) dlr.deUNSPECIFIED
Jack, SebastianSebastian.Jack (at) dlr.dehttps://orcid.org/0000-0002-1554-6503
Date:2015
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:rocket nozzle, flow separation
Event Title:51st AIAA Joint Propulsion Conference
Event Location:Orlando, FL, USA
Event Type:international Conference
Event Dates:27. - 29. Jul. 2015
Organizer:AIAA
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: Braunschweig , Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Rocket Propulsion
Institute of Aerodynamics and Flow Technology > Spacecraft
Deposited By: Hanke, Michaela
Deposited On:20 Nov 2015 09:12
Last Modified:01 Dec 2018 19:51

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