Schröder, A. and Arnott, A. and Agocs, J. and Sammler, B. and Schneider, G. and Kompenhans, J. (2004) PIV for high lift applications. European Windtunnel Association Initial Joint Workshop, Toulouse, October 18-20, 2004.
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Within the framework of the EUROLIFT and EUROPIV-2 programme, experiments using particle image velocimetry (PIV) were performed in the low-speed wind tunnel of Airbus Bremen, Germany. The goal was to investigate the flow over slat/wing/flap models in a high-lift configuration. For this, a system for acquiring PIV data from multiple cameras simultaneously was devised and installed underneath the wind tunnel. The PIV experiments were performed at different span positions of the models, for different angles of incidence. In total more than 5000 PIV images were obtained, the images capturing the flow fields from the slat wake, slat/wing-gap, flow mixing over the main wing, wing/flap-gap and wing wake. The analysis of the results reveals that PIV is feasible in industrial-type wind tunnel tests, with high-quality data revealing the unsteady nature of the flow around high-lift configurations, the mixing that occurs across wakes, plus intermittent flow separation over the flap.
|Document Type:||Conference or Workshop Item (Paper)|
|Title:||PIV for high lift applications|
|Page Range:||pp. 1-29|
|Keywords:||particle image velocimetry (PIV) , high-lift configuration, multiple cameras, unsteady flow|
|Event Title:||European Windtunnel Association Initial Joint Workshop, Toulouse, October 18-20, 2004|
|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:||Köln-Porz , Braunschweig , Göttingen|
|Institutes and Institutions:||Institute of Aerodynamics and Flow Technology|
|Deposited By:||Ilka Micknaus|
|Deposited On:||31 Jan 2006|
|Last Modified:||14 Jan 2010 19:36|
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