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RANS Solution for a Complex High-Lift Configuration of a Transport Aircraft with Engine Including Improved Resolution of the Nearfield

Melber-Wilkending, S. and Wilhelm, R. and Geyr, H. von (2004) RANS Solution for a Complex High-Lift Configuration of a Transport Aircraft with Engine Including Improved Resolution of the Nearfield. 22nd AIAA Applied Aerodynamics Conference, Rhode Island (usa), 16.-19.08.2004.

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Abstract

Numerical results of the solution of the Reynolds-averaged Navier-Stokes equations (RANS)for a complex high-lift configuration of a transport aircraft are shown. Two different configurations with an open and a closed thrust-gate are considered. The following topics are discussed: the grid generation process, the flow solution method and comparison of numerical and experimental data obtained during wind-tunnel tests.

Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=2005,
Title:RANS Solution for a Complex High-Lift Configuration of a Transport Aircraft with Engine Including Improved Resolution of the Nearfield
Authors:
AuthorsInstitution or Email of Authors
Melber-Wilkending, S.UNSPECIFIED
Wilhelm, R.UNSPECIFIED
Geyr, H. vonUNSPECIFIED
Date:2004
Status:Published
Keywords:RANS, Complex High-Lift, Transport Aircraft with Engine, Improved Resolution of the Nearfield, Wake-Vortex
Event Title:22nd AIAA Applied Aerodynamics Conference, Rhode Island (usa), 16.-19.08.2004
Organizer:AIAA
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 19:44

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