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Aerodynamic Analysis of Flows with Low Mach- and Reynolds-Number under Consideration and Forecast of Transition on the Example of a Glider

Melber-Wilkending, S. and Schrauf, G. and Rakowitz, M. (2004) Aerodynamic Analysis of Flows with Low Mach- and Reynolds-Number under Consideration and Forecast of Transition on the Example of a Glider. 14th AG STAB/DGLR Symposium, Bremen (de), 16.-18.11.2004.

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Abstract

For the simulation of low Reynolds- and Mach number flows, a boundary layer code in combination with a database method are coupled with an unstructured RANS code. The technique is validated in 2D using a glider airfoil and in 3D for a glider, showing good agreement with experiments and a well-validated 2D design code.

Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=2005,
Title:Aerodynamic Analysis of Flows with Low Mach- and Reynolds-Number under Consideration and Forecast of Transition on the Example of a Glider
Authors:
AuthorsInstitution or Email of Authors
Melber-Wilkending, S.UNSPECIFIED
Schrauf, G.Airbus GmbH Deutschland
Rakowitz, M.UNSPECIFIED
Date:2004
Status:Published
Keywords:Transition, Glider, CFD
Event Title:14th AG STAB/DGLR Symposium, Bremen (de), 16.-18.11.2004
Organizer:DGLR
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:Aircraft Research
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Flight Physics
Location: Köln-Porz , Braunschweig , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology
Deposited By: Claudia Grant
Deposited On:31 Jan 2006
Last Modified:14 Jan 2010 19:42

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