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Receptivity of Stationary Crossflow Vortices to Distributed Surface Roughness - Experimental

Lemarechal, Jonathan (2017) Receptivity of Stationary Crossflow Vortices to Distributed Surface Roughness - Experimental. Airbus PhD Day, 05. Sep. 2017, Bristol, England.

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Abstract

The skin friction is the major contributor to the overall drag of aircraft. For swept wing aircraft transition occurs very early due te the statienary cressflew instabil ity. Therefore, experimental werk investigating the receptivity ef a wing's surface tewards stationary crossflow is investigated. The pester gives an update of the werk within the Patenschaft.

Item URL in elib:https://elib.dlr.de/118610/
Document Type:Conference or Workshop Item (Poster)
Title:Receptivity of Stationary Crossflow Vortices to Distributed Surface Roughness - Experimental
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Lemarechal, JonathanJonathan.Lemarechal (at) dlr.deUNSPECIFIED
Date:2017
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:TSP, Crossflow, Distributed Roughnes, Receptivity
Event Title:Airbus PhD Day
Event Location:Bristol, England
Event Type:Workshop
Event Dates:05. Sep. 2017
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:fixed-wing aircraft
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Simulation and Validation
Location: Göttingen
Institutes and Institutions:Institute for Aerodynamics and Flow Technology > Experimental Methods, GO
Deposited By: Bachmann, Barbara
Deposited On:31 Jan 2018 11:40
Last Modified:23 Jul 2018 07:58

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