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Numerical Investigation of Flow Transition Behavior in Cold Flow Dual Bell Rocket Nozzles

Schneider, Dirk and Génin, C. (2015) Numerical Investigation of Flow Transition Behavior in Cold Flow Dual Bell Rocket Nozzles. 51st AIAA Joint Propulsion Conference, 27. - 29. Jul. 2015, Orlando, FL, USA.

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Item URL in elib:https://elib.dlr.de/99609/
Document Type:Conference or Workshop Item (Speech)
Title:Numerical Investigation of Flow Transition Behavior in Cold Flow Dual Bell Rocket Nozzles
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Schneider, DirkDirk.Schneider (at) dlr.dehttps://orcid.org/0000-0002-4785-4244
Génin, C.Chloe.Genin (at) dlr.deUNSPECIFIED
Date:2015
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:dual bell nozzle, flow separation, altitude adaptive nozzles, nozzle flow
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: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Rocket Propulsion
Deposited By: Hanke, Michaela
Deposited On:20 Nov 2015 09:13
Last Modified:31 Jul 2019 19:56

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