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Shock induced fluid structure interaction on a flexible wall in supersonic turbulent flow

Willems, Sebastian and Gülhan, Ali and Esser, Burkard (2011) Shock induced fluid structure interaction on a flexible wall in supersonic turbulent flow. 4th European Conference for Aerospace Sciences (EUCASS), 4.-8. Juli 2011, St. Petersburg, Russland.

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Abstract

A detailed knowledge of the flow structure interaction in supersonic flows is important for the design of future space transportation systems. Therefore this work was devoted to the investigation of the shock wave boundary layer interaction on an elastic panel. During the wind tunnel experiments the panel deflection was measured with fast non-intrusive displacement sensors. On the flow side pressure, high-speed Schlieren photography and oil-film technique were used. The flow manipulation due to the panel deflection becomes manifest in a deformation of the impinging shock and the separation zone. The panel deflection consists of a constant and a dynamic component. The experimental results are discussed and compared to numerical results.

Item URL in elib:https://elib.dlr.de/73954/
Document Type:Conference or Workshop Item (Paper)
Title:Shock induced fluid structure interaction on a flexible wall in supersonic turbulent flow
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Willems, Sebastiansebastian.willems (at) dlr.deUNSPECIFIED
Gülhan, AliAli.Guelhan (at) dlr.deUNSPECIFIED
Esser, BurkardBurkard.Esser (at) dlr.deUNSPECIFIED
Date:July 2011
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Accepted
Keywords:fluid structure interaction, shock wave boundary layer interaction
Event Title:4th European Conference for Aerospace Sciences (EUCASS)
Event Location:St. Petersburg, Russland
Event Type:international Conference
Event Dates:4.-8. Juli 2011
Organizer:European Conference for Aerospace Sciences
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:other
DLR - Research area:Raumfahrt
DLR - Program:R - no assignment
DLR - Research theme (Project):R - no assignment
Location: Köln-Porz
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Supersonic and Hypersonic Technology
Deposited By: Willems, Sebastian
Deposited On:13 Jan 2012 07:55
Last Modified:31 Jul 2019 19:34

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