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

Schneider, Dirk and Génin, Chloé (2016) Numerical Investigation of Flow Transition Behavior in Cold Flow Dual-Bell Rocket Nozzles. Journal of Propulsion and Power. American Institute of Aeronautics and Astronautics (AIAA). doi: 10.2514/1.B36010. ISSN 0748-4658.

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Item URL in elib:https://elib.dlr.de/107795/
Document Type:Article
Title:Numerical Investigation of Flow Transition Behavior in Cold Flow Dual-Bell Rocket Nozzles
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Schneider, DirkUNSPECIFIEDhttps://orcid.org/0000-0002-4785-4244UNSPECIFIED
Génin, ChloéUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Date:2016
Journal or Publication Title:Journal of Propulsion and Power
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:Yes
DOI:10.2514/1.B36010
Publisher:American Institute of Aeronautics and Astronautics (AIAA)
ISSN:0748-4658
Status:Published
Keywords:nozzle flow, dual-bell nozzle, numerical nozzle flow Simulation, flow separation
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Transportation
DLR - Research area:Raumfahrt
DLR - Program:R RP - Space Transportation
DLR - Research theme (Project):R - ProTAU + Prop2020 Hochleistungstriebwerke (old)
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Rocket Propulsion
Deposited By: Hanke, Michaela
Deposited On:16 Nov 2016 07:50
Last Modified:28 Nov 2023 09:21

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