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Large eddy simulation of high re number partially separated flow
Defense and Security Systems and Technology, Sweden.ORCID iD: 0000-0002-3829-0918
2012 (English)Conference paper, Published paper (Refereed)
Abstract [en]

The predictive capability for Large Eddy Simulation (LES) for flows with unsteady separation at curved surfaces is investigated. LES with near wall modeling is applied and a range of subgrid models is evaluated for four different validation cases for which experimental flow measurement data is available. A novel model for the simulation of the effect of boundary layer tripping devices used in experiments is also proposed and evaluated. The validation focuses on the mean velocity distribution in the region of separation, as well as on the skin friction and the surface streamlines. The flow physics of separation for these four cases is illustrated and discussed in detail. 

Place, publisher, year, edition, pages
American Institute of Aeronautics and Astronautics Inc. , 2012.
Keywords [en]
Aerospace engineering; Boundary layers, Curved surfaces; Flow physics; Mean velocity distribution; Near wall models; Predictive capabilities; Separated flows; Subgrid model; Surface streamlines, Large eddy simulation
National Category
Mechanical Engineering
Identifiers
URN: urn:nbn:se:ri:diva-72610DOI: 10.2514/6.2012-100Scopus ID: 2-s2.0-84871874500OAI: oai:DiVA.org:ri-72610DiVA, id: diva2:1851588
Conference
50th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition
Available from: 2024-04-15 Created: 2024-04-15 Last updated: 2024-04-15Bibliographically approved

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Liefvendahl, Mattias

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