Buchmann, N. A. und Cierpka, Christian und Knopp, Tobias und Schanz, Daniel und Schröder, Andreas und Hain, R. und Kähler, Christian (2014) Large Scale Adverse Pressure Gradient Turbulent Boundary Investigation by means of PIV and PTV. 17th Internatinal Symposium on Application Laser Techniques to Fluid Mechanics, 2014-07-07 - 2014-07-10, Lisbon, Portugal.
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Offizielle URL: http://ltces.dem.ist.utl.pt/lxlaser/lxlaser2014/finalworks2014/papers/03.7_5_210paper.pdf
Kurzfassung
subjected to a streamwise adverse pressure gradient Δp+ =ν/(ρu3 τ) dp/dx. However the statistically averaged behaviour of turbulent boundary layers subjected to adverse pressure gradients (i.e.Δp+ >0) is still an poorly understood. For zero-pressure gradient boundary layers the log-law u+ = 1/Ki log(y+) + Bi gives a proper description of the mean velocity at sufficiently large Reτ [7]. However, for adverse pressure gradient flows the log-law breaks down and a socalled half-power law or modified log-law with a functional depends on Δp+ may exist [4, 6]. Another open point is the spatial (and temporal) organisation of the coherent large and small-scale structures. While these aspects are far better understood for zero-pressure gradient boundary layers, there is little information for wall-bounded flows with streamwise adverse pressure gradients. In order to study the coherent flow structures, higher-order turbulent statistics and wall shear stress characteristics in a turbulent boundary layer subjected to adverse pressure gradients an experiment that builds on the recent progress in Particle Image Velocimetry (PIV) and Particle Tracking Velocimetry (PTV) is carried out. The experiment is designed such that the flow starts with a fully developed zeropressure gradient turbulent boundary layer and subsequently the flow experiences a streamwise adverse pressure gradient. The imposed pressure gradient is such that the streamwise flow development is slow with no history effects, but sufficiently large to cause changes from the universal log-law (e.g. Δp+ ≫0.015).
elib-URL des Eintrags: | https://elib.dlr.de/89903/ | ||||||||||||||||||||||||||||||||
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Dokumentart: | Konferenzbeitrag (Vortrag) | ||||||||||||||||||||||||||||||||
Zusätzliche Informationen: | Paper-Nr.: 03.7_5_210, Book of Abstracts | ||||||||||||||||||||||||||||||||
Titel: | Large Scale Adverse Pressure Gradient Turbulent Boundary Investigation by means of PIV and PTV | ||||||||||||||||||||||||||||||||
Autoren: |
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Datum: | 2014 | ||||||||||||||||||||||||||||||||
Referierte Publikation: | Ja | ||||||||||||||||||||||||||||||||
Open Access: | Nein | ||||||||||||||||||||||||||||||||
Gold Open Access: | Nein | ||||||||||||||||||||||||||||||||
In SCOPUS: | Nein | ||||||||||||||||||||||||||||||||
In ISI Web of Science: | Nein | ||||||||||||||||||||||||||||||||
Seitenbereich: | Seite 1 | ||||||||||||||||||||||||||||||||
Name der Reihe: | Conference Proceedings online | ||||||||||||||||||||||||||||||||
Status: | veröffentlicht | ||||||||||||||||||||||||||||||||
Stichwörter: | Turbulent Boundary Layer, Adverse Pressure Gradient, PIV, long-range micro PIV, Wall Shear Stress | ||||||||||||||||||||||||||||||||
Veranstaltungstitel: | 17th Internatinal Symposium on Application Laser Techniques to Fluid Mechanics | ||||||||||||||||||||||||||||||||
Veranstaltungsort: | Lisbon, Portugal | ||||||||||||||||||||||||||||||||
Veranstaltungsart: | internationale Konferenz | ||||||||||||||||||||||||||||||||
Veranstaltungsbeginn: | 7 Juli 2014 | ||||||||||||||||||||||||||||||||
Veranstaltungsende: | 10 Juli 2014 | ||||||||||||||||||||||||||||||||
HGF - Forschungsbereich: | Luftfahrt, Raumfahrt und Verkehr | ||||||||||||||||||||||||||||||||
HGF - Programm: | Luftfahrt | ||||||||||||||||||||||||||||||||
HGF - Programmthema: | Flugzeuge | ||||||||||||||||||||||||||||||||
DLR - Schwerpunkt: | Luftfahrt | ||||||||||||||||||||||||||||||||
DLR - Forschungsgebiet: | L AR - Aircraft Research | ||||||||||||||||||||||||||||||||
DLR - Teilgebiet (Projekt, Vorhaben): | L - Simulation und Validierung (alt) | ||||||||||||||||||||||||||||||||
Standort: | Göttingen | ||||||||||||||||||||||||||||||||
Institute & Einrichtungen: | Institut für Aerodynamik und Strömungstechnik > Experimentelle Verfahren Institut für Aerodynamik und Strömungstechnik > C²A²S²E - Center for Computer Applications in AeroSpace Science and Engineering | ||||||||||||||||||||||||||||||||
Hinterlegt von: | Micknaus, Ilka | ||||||||||||||||||||||||||||||||
Hinterlegt am: | 30 Jul 2014 17:01 | ||||||||||||||||||||||||||||||||
Letzte Änderung: | 24 Apr 2024 19:55 |
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