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Time Accurate Simulation of Turbulent Nozzle Flow by the DLR TAU-Code

Lüdeke, H. and Filimon, A. (2004) Time Accurate Simulation of Turbulent Nozzle Flow by the DLR TAU-Code. (In Press)

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Fundamental requirements for future launcher technologies are a cost-efficient access to space as well as the improvement of safety and reliability. In the presented contribution an unsteady turbulent flow simulation of the Ariane-5 launcher during ascent will be carried out by detached eddy simulation (DES). In a first step the nature of separation shocks in turbulent over-expanded axisymmetric nozzles is simulated. Different implementations of detached eddy simulation models are investigated for a compressible wake flow as a validation case. Finally steady and unsteady Ariane-5 simulations are carried out at Mach 0.8 wind tunnel conditions including jet flow and the wake of the boosters.

Item URL in elib:https://elib.dlr.de/12983/
Document Type:Article
Additional Information: LIDO-Berichtsjahr=2005,
Title:Time Accurate Simulation of Turbulent Nozzle Flow by the DLR TAU-Code
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In ISI Web of Science:Yes
Series Name:Notes on Numerical Fluid Mechanics and Multidisciplinary Design
Status:In Press
Keywords:Detached Eddy Simulation, Unsteady nozzle flow, Buffeting coupling, Turbulence
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 - Anlagen und Messtechnik (old)
Location: Köln-Porz , Braunschweig , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology
Deposited By: Grant, Claudia
Deposited On:10 Jan 2006
Last Modified:22 Jan 2018 16:49

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