Schulze, Sebastian (2019) Modellierung der Heißgasströmung in einer Raketenbrennkammer hinsichtlich des Wandwärmestromverlaufs. Master's, Ruhr-Uni Bochum.
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Item URL in elib: | https://elib.dlr.de/132950/ | ||||||||
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Document Type: | Thesis (Master's) | ||||||||
Title: | Modellierung der Heißgasströmung in einer Raketenbrennkammer hinsichtlich des Wandwärmestromverlaufs | ||||||||
Authors: |
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Date: | 2019 | ||||||||
Refereed publication: | No | ||||||||
Open Access: | No | ||||||||
Status: | Published | ||||||||
Keywords: | Raketenbrennkammer, Heißgas | ||||||||
Institution: | Ruhr-Uni Bochum | ||||||||
Department: | Thermische Turbomaschinen | ||||||||
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 - Antriebsystemtechnik - Schubkammertechnologie (old) | ||||||||
Location: | Lampoldshausen | ||||||||
Institutes and Institutions: | Institute of Space Propulsion > Rocket Propulsion | ||||||||
Deposited By: | Hanke, Michaela | ||||||||
Deposited On: | 18 Dec 2019 16:06 | ||||||||
Last Modified: | 18 Dec 2019 16:06 |
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