Engler, Rolf and Fey, Uwe and Henne, Ulrich and Klein, Christian and Sachs, Werner (2005) Pressure Sensitive Paints and Temperature Sensitive Paints in Quantitative Wind Tunnel Studies. Journal of Visualization, Vol. 8 (3), pp. 277-284. Journal of Visualization. ISSN 1343-8875 8 (3) 193-284.
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The pressure sensitive paint (PSP) intensity and lifetime system is an optical measurement technique to investigate absolute pressure fields on model surfaces for basic research in laboratories, industrial wind tunnels or high speed rotating turbo machines. Detailed qualitative and quantitative information and understanding of flow phenomena can be obtained in speed ranges from U∞ = 20 m/s up to Ma = 5.0. A number of projects of industrial interest has been investigated in different wind tunnels covering low speed, transonic, trisonic and cryogenic facilities. The influence of the main error sources for the components of the PSP system have been checked. Comparison of experimental pressure fields obtained by means of PSP and the results of numerical calculations have been carried out. Different wind tunnel models ranging from basic configurations such as a cropped delta wing to a complex half model of a large propeller-driven transport aircraft with all flaps, rudders and shrouds, and rotating or oscillating models as well as Reynolds number effects on models have been investigated.
|Title:||Pressure Sensitive Paints and Temperature Sensitive Paints in Quantitative Wind Tunnel Studies|
|Journal or Publication Title:||Journal of Visualization|
|In ISI Web of Science:||Yes|
|Page Range:||pp. 277-284|
|Publisher:||Journal of Visualization|
|ISSN:||1343-8875 8 (3) 193-284|
|Keywords:||Pressure sensitive paint, PSP, Temperature sensitive paint, TSP, Optical sensors|
|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:||30 Jan 2006|
|Last Modified:||27 Apr 2009 04:59|
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