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Effect of forward-facing steps on boundary layer transition at a subsonic Mach number

Costantini, Marco and Risius, Steffen and Klein, Christian and Kühn, Winfried (2014) Effect of forward-facing steps on boundary layer transition at a subsonic Mach number. 19. DGLR-Fachsymposium der STAB, 04. - 05. Nov. 2014, München, Deutschland.

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Official URL: http://www.stab2014.tum.de/


Item URL in elib:https://elib.dlr.de/89793/
Document Type:Conference or Workshop Item (Speech)
Title:Effect of forward-facing steps on boundary layer transition at a subsonic Mach number
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Costantini, MarcoMarco.Costantini (at) dlr.deUNSPECIFIED
Risius, Steffensteffen.risius (at) dlr.deUNSPECIFIED
Klein, Christianchristian.klein (at) dlr.deUNSPECIFIED
Kühn, WinfriedAirbus Operations SASUNSPECIFIED
Date:2014
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Page Range:pp. 68-69
Series Name:Jahresbericht 2014
Status:Published
Keywords:Boundary layer transition, forward-facing steps, Temperature-Sensitive Paint
Event Title:19. DGLR-Fachsymposium der STAB
Event Location:München, Deutschland
Event Type:national Conference
Event Dates:04. - 05. Nov. 2014
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 of Aerodynamics and Flow Technology > Experimental Methods
Deposited By: Micknaus, Ilka
Deposited On:24 Nov 2014 11:48
Last Modified:24 Nov 2014 11:48

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