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Transition Prediction and Impact on a Three-Dimensional High-Lift-Wing Configuration
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2008 (English)In: Journal of Aircraft, ISSN 0021-8669, E-ISSN 1533-3868, Vol. 45, no 5, 1751-1766 p.Article in journal (Refereed) Published
Abstract [en]

The evolution of the 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-up project EUROLIFT II, a major step was the integration of transition-prediction tools within Reynolds-averaged Navier-Stokes solvers 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
2008. Vol. 45, no 5, 1751-1766 p.
Keyword [en]
boundary-layers, swept, stability
National Category
Aerospace Engineering
Identifiers
URN: urn:nbn:se:kth:diva-17893DOI: 10.2514/1.36238ISI: 000260074500029Scopus ID: 2-s2.0-54549092552OAI: oai:DiVA.org:kth-17893DiVA: diva2:335938
Note

QC 20100525

Available from: 2010-08-05 Created: 2010-08-05 Last updated: 2017-12-12Bibliographically approved

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Hanifi, Ardeshir

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