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

Klein, Christian (2008) Application of PSP and TSP for determination of the pressure and temperature field of aircraft models in wind tunnels. DTU Fluid Seminar, 2008-02-05, Kopenhagen (Dänemark).

Full text not available from this repository.

Official URL: http://www.fluid.dtu.dk/englisch/seminar

Abstract

Visualization and quantitave measurement of aerodynamic effects on several aircraft models have been conducted using an optical pressure measurement system, based on the pressure-sensitive paint (PSP) technique. The PSP technology not only provides a good understanding of the flow topology around a wind tunnel model, but can be used to carry out absolute pressure measurements on a surface of the model and to determine additional aerodynamic data such as loads on it as well. The identification of laminar-turbulent boundary layer transition on models in wind tunnels yields essential information for the design of modern wings. Among other techniques, transition detection can be done using the temperature-sensitive paint (TSP) technique.

Document Type:Conference or Workshop Item (Speech)
Additional Information:78 Folien
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 Authors
Klein, ChristianUNSPECIFIED
Date:2008
Refereed publication:No
In SCOPUS:No
In ISI Web of Science:No
Series Name:The DTU - Fluid Seminar
Status:Published
Keywords:pressure-sensitive paint (PSP), temperature-sensitive paint (TSP)
Event Title:DTU Fluid Seminar
Event Location:Kopenhagen (Dänemark)
Event Type:Other
Event Dates:2008-02-05
Organizer:DTU
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:Aircraft Research
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Flight Physics
Location: Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Experimental Methods
Deposited By: Ilka Micknaus
Deposited On:04 Mar 2008
Last Modified:27 Apr 2009 14:42

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