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
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 (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|
|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|
Repository Staff Only: item control page