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Experimental investigation of the effect on boundary-layer transition of forward-facing steps, pressure gradient, and a non-adiabatic surface

Costantini, Marco (2015) Experimental investigation of the effect on boundary-layer transition of forward-facing steps, pressure gradient, and a non-adiabatic surface. Seminar des Instituts für Strömungsmechanik und Aerodynamik, Universität der Bundeswehr München, 12. Nov. 2015, München, Deutschland.

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Item URL in elib:https://elib.dlr.de/99725/
Document Type:Conference or Workshop Item (Speech)
Title:Experimental investigation of the effect on boundary-layer transition of forward-facing steps, pressure gradient, and a non-adiabatic surface
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Costantini, MarcoMarco.Costantini (at) dlr.deUNSPECIFIED
Date:2015
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:Boundary-layer transition; forward-facing steps; non-adiabatic surface; Temperature-Sensitive Paint
Event Title:Seminar des Instituts für Strömungsmechanik und Aerodynamik, Universität der Bundeswehr München
Event Location:München, Deutschland
Event Type:Other
Event Dates:12. Nov. 2015
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:11 Dec 2015 15:26
Last Modified:10 May 2016 23:35

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