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Anwendung eines Flamelet-Modells zur numerischen Simulation von Hybridraketentriebwerken

Dabanovic, Andrija (2018) Anwendung eines Flamelet-Modells zur numerischen Simulation von Hybridraketentriebwerken. Other, Technische Universität Braunschweig.

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Item URL in elib:https://elib.dlr.de/126191/
Document Type:Thesis (Other)
Title:Anwendung eines Flamelet-Modells zur numerischen Simulation von Hybridraketentriebwerken
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Dabanovic, AndrijaAndrija.Dabanovic (at) dlr.deUNSPECIFIED
Date:December 2018
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:106
Status:Published
Keywords:Verbrennungssimulation, Flamelet model, Hybridraketentriebwerke
Institution:Technische Universität Braunschweig
Department:Institut für Raumfahrtsysteme
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):Project ATEK
Location: Braunschweig
Institutes and Institutions:Institute for Aerodynamics and Flow Technology > Spacecraft, BS
Deposited By: Steinberg, Silke
Deposited On:07 Feb 2019 15:24
Last Modified:07 Feb 2019 15:24

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