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Numerische Simulation der Strömung und Verbrennung in einem Green Propellant Raketentriebwerk

Bachmann, Ansgar (2021) Numerische Simulation der Strömung und Verbrennung in einem Green Propellant Raketentriebwerk. Bachelor's, TU Kaiserlsautern.

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Item URL in elib:https://elib.dlr.de/141818/
Document Type:Thesis (Bachelor's)
Title:Numerische Simulation der Strömung und Verbrennung in einem Green Propellant Raketentriebwerk
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Bachmann, AnsgarInstitut für Raumfahrtantriebe, DLR Lampoldshausen, Langer Grund, D - 74239 HardthausenUNSPECIFIED
Date:2021
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:130
Status:Published
Keywords:CFD-Simulation, Finite-Rate (FR), Eddy-Dissipation-Concept (EDC), Inverse Methode
Institution:TU Kaiserlsautern
Department:Lehrstuhl für Strömungsmechanik und Strömungsmaschinen
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 Future Fuels - Advanced Rocket Propellants
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Spacecraft and Orbital Propulsion
Deposited By: Hanke, Michaela
Deposited On:16 Apr 2021 07:44
Last Modified:16 Apr 2021 07:44

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