Change search
ReferencesLink to record
Permanent link

Direct link
Transition Prediction and Impact on 3D High-Lift Wing Configuration
Show others and affiliations
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 (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.
, AIAA paper, 2007-4302
Keyword [en]
Numerische Verfahren, transition prediction, RANS solvers, high-lift, 3d, realistic aircraft
National Category
Aerospace Engineering
URN: urn:nbn:se:kth:diva-93991ISBN: 978-156347898-7OAI: diva2:524819
25th AIAA Applied Aerodynamics Conference, 2007; Miami, FL; 25 June 2007 through 28 June 2007

QC 20120919

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

Open Access in DiVA

No full text

Search in DiVA

By author/editor
Hanifi, Ardeshir
Aerospace Engineering

Search outside of DiVA

GoogleGoogle Scholar
The number of downloads is the sum of all downloads of full texts. It may include eg previous versions that are now no longer available

Total: 27 hits
ReferencesLink to record
Permanent link

Direct link