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Application of the DLR TAU-Code to the RCM-4 Test Case: Microcombustor Ignition

Karl, Sebastian and Hannemann, Klaus (2006) Application of the DLR TAU-Code to the RCM-4 Test Case: Microcombustor Ignition. 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

The DLR-Tau code was used to perform transient numerical simulations of the ignition process of an H2/O2 flame A detailed finite rate combustion model was applied. The influence of turbulence was neglected in the present investigation. Numerical results of the temporal evolution of the combustor pressure and flame size are compared to experiments.

Document Type:Conference or Workshop Item (Paper)
Title:Application of the DLR TAU-Code to the RCM-4 Test Case: Microcombustor Ignition
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, ignition, TAU
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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