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Detached Eddy Simulation of Supersonic Shear Layer Wake Flows

Lüdeke, Heinrich and Togiti, Vamshi (2006) Detached Eddy Simulation of Supersonic Shear Layer Wake Flows. In: Int. Conference on Boundary and Interior Layers. Int. Conference on Boundary and Interior Layers, 2006-07-24 - 2006-07-28, Göttingen, Germany.



One challenge of numerical investigations of unsteady super- and hypersonic flow fields is the study of the turbulent wake at complex vehicle configurations. A recent promising approach is the technique of detached-eddy simulation (DES) proposed by Spalart et.al. Detached-eddy simulation is a hybrid approach for the modelling of turbulent flow fields at complex geometries. The intention of the current work is an investigation of the shear flow in the wake of a blunt cylinder at M=2.4 at high Reynolds numbers. This is used as a basic configuration for re-entry vehicles with a blunt base. Additionally simulations of the SARA capsule, a facility conceived to be a recovery orbital platform to perform orbital flights, are carried out to give a practical demonstratin of DES modelling for hypersonic flight To ensure turbulent wake flow the trajectory point at M=5.1, Re= 20 10^6 was chosen. The influence of unsteady loads, generated by the turbulent wake flow was investigated for this vehicle.

Item URL in elib:https://elib.dlr.de/46936/
Document Type:Conference or Workshop Item (Speech, Paper)
Title:Detached Eddy Simulation of Supersonic Shear Layer Wake Flows
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Date:June 2006
Journal or Publication Title:Int. Conference on Boundary and Interior Layers
Refereed publication:No
Open Access:Yes
Gold Open Access:No
In ISI Web of Science:No
University of Göttingen, UNSPECIFIED
Keywords:re-entry, unsteady, wake, turbulent, detached eddy simulation
Event Title:Int. Conference on Boundary and Interior Layers
Event Location:Göttingen, Germany
Event Type:international Conference
Event Dates:2006-07-24 - 2006-07-28
Organizer:University of Göttingen
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
Institute of Aerodynamics and Flow Technology > CASE
Deposited By: Lüdeke, Dr.-Ing. Heinrich
Deposited On:19 Jan 2007
Last Modified:31 Jul 2019 19:18

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