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Application of the DLR TAU-Code to the RCM-1 Test Case: Penn State Preburner Combustor

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.

Full text not available from this repository.

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.

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:
AuthorsInstitution or Email of Authors
Karl, SebastianUNSPECIFIED
Hannemann, KlausUNSPECIFIED
Date:2006
Journal or Publication Title:Proceedings of the 3rd International workshop on Rocket Combustion Modeling Snecma 2006
Refereed publication: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 Dates:2006-03-13 - 2006-03-15
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: Dagmar Brennecke-Hosseinzadeh
Deposited On:21 Aug 2007
Last Modified:27 Apr 2009 12:56

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