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Laminar wing design and verification via Temperature-Sensitive Paints

Costantini, Marco (2019) Laminar wing design and verification via Temperature-Sensitive Paints. Seminar of Fluid Mechanics, 21. Jan. 2019, Göttingen, Germany.

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Abstract

The focus of this presentation is on the laminar wing design and its verification by means of Temperature-Sensitive Paints (TSP). After an introduction to the development of the world air traffic and to the drag components of transport aircraft, the TSP technique for transition detection and the Cryogenic Ludwieg-Tube Göttingen are discussed. The results of the investigation of surface imperfection effects on laminar flow are also presented.

Item URL in elib:https://elib.dlr.de/129815/
Document Type:Conference or Workshop Item (Speech)
Title:Laminar wing design and verification via Temperature-Sensitive Paints
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Costantini, Marcomarco.costantini (at) dlr.dehttps://orcid.org/0000-0003-0642-0199
Date:21 January 2019
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:Laminar Wing, Temperature-Sensitive Paint, Wind Tunnels
Event Title:Seminar of Fluid Mechanics
Event Location:Göttingen, Germany
Event Type:Other
Event Dates:21. Jan. 2019
Organizer:Prof. Frank Jacobitz
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: Micknaus, Ilka
Deposited On:06 Nov 2019 15:58
Last Modified:06 Nov 2019 15:58

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