elib
DLR-Header
DLR-Logo -> http://www.dlr.de
DLR Portal Home | Imprint | Privacy Policy | Contact | Deutsch
Fontsize: [-] Text [+]

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.

Item URL in elib:https://elib.dlr.de/43912/
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 AuthorsAuthor's ORCID iDORCID Put Code
Karl, SebastianUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Hannemann, KlausUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
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

Repository Staff Only: item control page

Browse
Search
Help & Contact
Information
electronic library is running on EPrints 3.3.12
Website and database design: Copyright © German Aerospace Center (DLR). All rights reserved.