Pagan, Adam S. (2013) Numerische Simulation einer Modell-Raketenbrennkammer mit Einzelinjektor und Untersuchung des Einflusses einer Variation des Turbulenzgrades sowie der turbulenten Schmidt-und Prandtl-Zahl. Other, Universität Stuttgart.
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Item URL in elib: | https://elib.dlr.de/81809/ | ||||||
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Document Type: | Thesis (Other) | ||||||
Additional Information: | Studienarbeit | ||||||
Title: | Numerische Simulation einer Modell-Raketenbrennkammer mit Einzelinjektor und Untersuchung des Einflusses einer Variation des Turbulenzgrades sowie der turbulenten Schmidt-und Prandtl-Zahl | ||||||
Authors: |
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Date: | March 2013 | ||||||
Refereed publication: | No | ||||||
Open Access: | No | ||||||
Gold Open Access: | No | ||||||
In SCOPUS: | No | ||||||
In ISI Web of Science: | No | ||||||
Number of Pages: | 86 | ||||||
Status: | Published | ||||||
Keywords: | Numerische Simulation, Modellraketenbrennkammer, Prandtl-Zahl | ||||||
Institution: | Universität Stuttgart | ||||||
Department: | Institut für Verbrennungstechnik der Luft- und Raumfahrt | ||||||
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 - Propulsion 2020 / CFD und Simulation (old) | ||||||
Location: | Stuttgart | ||||||
Institutes and Institutions: | Institute of Combustion Technology > Computer Simulation | ||||||
Deposited By: | Bonfert, Anneliese | ||||||
Deposited On: | 12 Apr 2013 15:38 | ||||||
Last Modified: | 12 Apr 2013 15:42 |
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