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).
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Official URL: http://www.fluid.dtu.dk/englisch/seminar
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|
|In ISI Web of Science:||No|
|Series Name:||The DTU - Fluid Seminar|
|Keywords:||pressure-sensitive paint (PSP), temperature-sensitive paint (TSP)|
|Event Title:||DTU Fluid Seminar|
|Event Location:||Kopenhagen (Dänemark)|
|HGF - Research field:||Aeronautics, Space and Transport|
|HGF - Program:||Aeronautics|
|HGF - Program Themes:||L AR - Aircraft Research|
|DLR - Research area:||Aeronautics|
|DLR - Program:||L AR - Aircraft Research|
|DLR - Research theme (Project):||L - Flight Physics|
|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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