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Application of PSP and TSP for determination of the pressure and temperature field of aircraft models in wind tunnels

Henne, Ulrich (2008) Application of PSP and TSP for determination of the pressure and temperature field of aircraft models in wind tunnels. DLR visit JAXA, 2008-09-04, Tokio (Japan).

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Item URL in elib:https://elib.dlr.de/55344/
Document Type:Conference or Workshop Item (Speech)
Title:Application of PSP and TSP for determination of the pressure and temperature field of aircraft models in wind tunnels
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Henne, UlrichUNSPECIFIEDUNSPECIFIED
Date:2008
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:PSP, pressure sensitive paint, in-flight test
Event Title:DLR visit JAXA
Event Location:Tokio (Japan)
Event Type:Other
Event Dates:2008-09-04
Organizer:JAXA
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:Aircraft Research (old)
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Flight Physics (old)
Location: Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Experimental Methods
Deposited By: Micknaus, Ilka
Deposited On:13 Oct 2008
Last Modified:27 Apr 2009 15:14

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