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Transition Prediction and Impact on 3D High-Lift Wing Configuration
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2007 (English)In: A collection of technical papers: 25th AIAA Applied Aerodynamics Conference : Miami, Florida, 25-28 June 2007, American Institute of Aeronautics and Astronautics, 2007, 1593-1613 p.Conference paper, Published paper (Refereed)
Abstract [en]

The evolution of maximum lift coefficient of a transport aircraft as a function of Reynolds number can be linked to modifications of the laminar-turbulent transition process. In the framework of European project EUROLIFT (I), a task was dedicated to the physical understanding and the numerical modeling of the transition process in high-lift configurations. Then, in the follow-on project EUROLIFT II, a major step is the integration of transition prediction tools within Reynolds-averaged Navier-Stokes (RANS) solvers in order to estimate the impact of transition on performance. This paper presents an overview of the different activities dealing with transition in the EUROLIFT II project.

Place, publisher, year, edition, pages
American Institute of Aeronautics and Astronautics, 2007. 1593-1613 p.
Series
AIAA paper, 2007-4302
Keyword [en]
Numerische Verfahren, transition prediction, RANS solvers, high-lift, 3d, realistic aircraft
National Category
Aerospace Engineering
Identifiers
URN: urn:nbn:se:kth:diva-93991ISBN: 978-156347898-7 (print)OAI: oai:DiVA.org:kth-93991DiVA: diva2:524819
Conference
25th AIAA Applied Aerodynamics Conference, 2007; Miami, FL; 25 June 2007 through 28 June 2007
Note

QC 20120919

Available from: 2012-05-04 Created: 2012-05-03 Last updated: 2012-09-19Bibliographically approved

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Hanifi, Ardeshir

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