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RANS Modelling of a LOX/CH4 Single Injector Rocket Combustion Chamber

McNutt, Benjamin Alexander (2022) RANS Modelling of a LOX/CH4 Single Injector Rocket Combustion Chamber. Master's, University of Sydney.

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Item URL in elib:https://elib.dlr.de/192044/
Document Type:Thesis (Master's)
Title:RANS Modelling of a LOX/CH4 Single Injector Rocket Combustion Chamber
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
McNutt, Benjamin AlexanderDLR, LampoldshausenUNSPECIFIEDUNSPECIFIED
Date:14 July 2022
Refereed publication:Yes
Open Access:Yes
Number of Pages:158
Status:Published
Keywords:Methan, Verbrennung, Combustion, CFD, BKN
Institution:University of Sydney
Department:School of Aerospace, Mechanical and Mechatronic Engineering
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 - Project Amadeus
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Rocket Propulsion Technology
Deposited By: Böhringer, Isabell
Deposited On:12 Dec 2022 09:57
Last Modified:12 Dec 2022 09:57

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