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Investigation of Shock-Shock Investigations in Hypersonic Reentry Flows

Brück, S. (1997) Investigation of Shock-Shock Investigations in Hypersonic Reentry Flows. In: 20th International Symposium on Shock Waves, Vol. I, pp. 215-220. World Scientific. 20th International Symposium on Shock Waves,.

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Abstract

Numerical simulations of shock-shock interactions in front of a circular cylinder have been performed. The numerical results of a validation test case are compared with experimental data. The modelling of a perfect gas and a mixture of chemically reacting perfect gases have been applied to reentry flow conditions. Differences of the results of the two models are demonstrated in view to the calculated shock configurations and the peak loads on the surface

Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=1999,
Title:Investigation of Shock-Shock Investigations in Hypersonic Reentry Flows
Authors:
AuthorsInstitution or Email of Authors
Brück, S.UNSPECIFIED
Date:1997
Journal or Publication Title:20th International Symposium on Shock Waves
Volume:Vol. I
Page Range:pp. 215-220
Editors:
EditorsEmail
Sturtevant, B.UNSPECIFIED
Shepherd, J.E.UNSPECIFIED
Hornung, H.G.UNSPECIFIED
Publisher:World Scientific
Status:Published
Keywords:Shock-shock interactions, viscous nonequilibrium flows, TVD method, cylinder flow
Event Title:20th International Symposium on Shock Waves,
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):UNSPECIFIED
Location: Köln-Porz , Braunschweig , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Institut für Strömungsmechanik
Deposited By: elib DLR-Beauftragter
Deposited On:16 Sep 2005
Last Modified:14 Jan 2010 20:40

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