Investigation of Unsteady Loads due to Turbulent Supersonic Wake Flow.
In: Proceedings of the RTO AVT-123 Syposium: Flow Induced Unsteady Loads and the Impact on Military Applications.
RTO AVT-123 Syposium: Flow Induced Unsteady Loads and the Impact on Military Applications, 2005-04-25 - 2005-04-28, Budapest.
The modelling of unsteady side loads induced by the interaction of flow separation in the wake of
hypersonic re-entry vehicles play an important role for the design of such systems. The simulation of
these phenomena is one of the main challenges during decent. To investigate the turbulent wake flow,
basic studies of generic configurations and the applicability of advanced turbulence modelling are
necessary. For this reason validations of Detached Eddy Simulation for an axisymmetric supersonic
cylinder configuration at M=2.4 are carried out to earn experience for unsteady simulations of re-entry vehicles. For this case different variations of hybrid RANS-LES methods like DES are tested by using the hybrid structured/ unstructured DLR-τ-code on hexahedral and tetrahedral grids. As a practical test case a cylindrical re-entry capsule at a hypersonic Mach number of M=5.1 under free-flight conditions was investigated.
|Document Type:||Conference or Workshop Item (Speech, Paper)|
|Title:||Investigation of Unsteady Loads due to Turbulent Supersonic Wake Flow|
|Authors||Institution or Email of Authors|
|Date:||25 April 2005|
|Journal or Publication Title:||Proceedings of the RTO AVT-123 Syposium: Flow Induced Unsteady Loads and the Impact on Military Applications|
|In ISI Web of Science:||No|
|RTO AVT-123, ||UNSPECIFIED|
|Keywords:||Detached Eddy Simulation, Unsteady base flow, compressible flow, Re-entry|
|Event Title:||RTO AVT-123 Syposium: Flow Induced Unsteady Loads and the Impact on Military Applications|
|Event Type:||international Conference|
|Event Dates:||2005-04-25 - 2005-04-28|
|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)|
|Institutes and Institutions:||Institute of Aerodynamics and Flow Technology > Spacecraft|
Dr.-Ing. Heinrich Lüdeke
|Deposited On:||19 Jan 2007|
|Last Modified:||12 Dec 2013 20:23|
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