Karl, Sebastian and Hannemann, Klaus (2006) Application of the DLR TAU-Code to the RCM-1 Test Case: Penn State Preburner Combustor. In: Proceedings of the 3rd International workshop on Rocket Combustion Modeling Snecma 2006. 3rd International Workshop on Rocket Combustion Modeling, 2006-03-13 - 2006-03-15, Paris.
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Abstract
Numerical simulations of the stationary flow in the Penn State Preburner Combustor were performed using the DLR TAU Code including a detailed finite rate combustion model. Different turbulence models were applied and the obtained wall heat flux data were compared to experimental results.
Item URL in elib: | https://elib.dlr.de/43912/ | ||||||||||||
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Document Type: | Conference or Workshop Item (Paper) | ||||||||||||
Title: | Application of the DLR TAU-Code to the RCM-1 Test Case: Penn State Preburner Combustor | ||||||||||||
Authors: |
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Date: | 2006 | ||||||||||||
Journal or Publication Title: | Proceedings of the 3rd International workshop on Rocket Combustion Modeling Snecma 2006 | ||||||||||||
Refereed publication: | No | ||||||||||||
Open Access: | No | ||||||||||||
Gold Open Access: | No | ||||||||||||
In SCOPUS: | No | ||||||||||||
In ISI Web of Science: | No | ||||||||||||
Status: | Published | ||||||||||||
Keywords: | Combustion, TAU, chemistry | ||||||||||||
Event Title: | 3rd International Workshop on Rocket Combustion Modeling | ||||||||||||
Event Location: | Paris | ||||||||||||
Event Type: | international Conference | ||||||||||||
Event Start Date: | 13 March 2006 | ||||||||||||
Event End Date: | 15 March 2006 | ||||||||||||
Organizer: | SNECMA | ||||||||||||
HGF - Research field: | Aeronautics, Space and Transport (old) | ||||||||||||
HGF - Program: | Space (old) | ||||||||||||
HGF - Program Themes: | W RP - Raumtransport | ||||||||||||
DLR - Research area: | Space | ||||||||||||
DLR - Program: | W RP - Raumtransport | ||||||||||||
DLR - Research theme (Project): | W - Grundlagen Raumtransport - numerische Verfahren (old) | ||||||||||||
Location: | Braunschweig , Göttingen | ||||||||||||
Institutes and Institutions: | Institute of Aerodynamics and Flow Technology > Spacecraft | ||||||||||||
Deposited By: | Brennecke-Hosseinzadeh, Dagmar | ||||||||||||
Deposited On: | 21 Aug 2007 | ||||||||||||
Last Modified: | 24 Apr 2024 19:05 |
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