Konrath, Robert and Klein, Christian and Schröder, Andreas and Kompenhans, Jürgen (2006) Combined application of pressure sensitive paint and particle image velocimetry to the flow above a delta wing. Experiments in Fluids, Vol. 44 (3), pp. 357-366. Springer Verlag Berlin/Heidelberg. DOI: 10.1007/s00348-007-0445-5. ISSN 0723-4864 (print), 1432-1114 (online).
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The pressure sensitive paint (PSP) and particle image velocimetry (PIV) techniques are applied to the flow around a delta wing. These investigations are a contribution to the International Vortex Flow Experiment 2 (VFE-2). The delta wing is equipped with rounded as well as with sharp leading edges. To demonstrate the advantages of a combined application of PSP and PIV for flow investigation the results of a specific case are discussed, where an inner and outer primary vortex above the delta wing with rounded leading edges develop.
|Title:||Combined application of pressure sensitive paint and particle image velocimetry to the flow above a delta wing|
|Date:||15 December 2006|
|Journal or Publication Title:||Experiments in Fluids|
|In ISI Web of Science:||Yes|
|Page Range:||pp. 357-366|
|Publisher:||Springer Verlag Berlin/Heidelberg|
|Series Name:||Experimental Methods and their Applications to Fluid Flow|
|ISSN:||0723-4864 (print), 1432-1114 (online)|
|Keywords:||PSP, PIV, Delta-wing, VFE-2|
|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:||24 Apr 2008|
|Last Modified:||15 Jan 2010 00:00|
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