Klein, Christian and Engler, Rolf and Sachs, Werner and Henne, Ulrich (2005) Application of Pressure Sensitive Paint (PSP) for Determination of the Pressure Field and Calculation of Forces and Moments of Models in a Wind Tunnel. Experiments in Fluids, Volume 39 (Heft 2), pp. 475-483. Springer-Verlag Berlin Heidelberg. ISSN 0723-4864.
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The Visualization and measurements of aerodynamic effects on a three-dimensional aircraft model were conducted using an optical pressure measurement system, based on the Pressure Sensitive Paint (PSP) technique. The PSP technology provides a good understanding of the flow around the wind tunnel model. The PSP technique can be used to carry out absolute pressure measurements on a surface of the model and to determine additional aerodynamic data using scientific grade cameras and image processing techniques. Surface pressures from top, bottom, left and right viewing directions were obtained using the DLR-PSP system on the entire surface which can be observed by eight CCD-cameras. Finally, the measured pressures can be integrated to calculate forces and moments of the complete model or parts thereof.
|Title:||Application of Pressure Sensitive Paint (PSP) for Determination of the Pressure Field and Calculation of Forces and Moments of Models in a Wind Tunnel|
|Journal or Publication Title:||Experiments in Fluids|
|In ISI Web of Science:||Yes|
|Page Range:||pp. 475-483|
|Publisher:||Springer-Verlag Berlin Heidelberg|
|Keywords:||Pressure Sensitive Paint (PSP), 3D aircraft model, image processing techniques, forces and moments|
|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 04:56|
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