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Aspects of 3D RANS Simulations for Transport Aircraft High-Lift Configurations

Rudnik, R. and Melber, S. and Ronzheimer, A. and Brodersen, O. (2000) Aspects of 3D RANS Simulations for Transport Aircraft High-Lift Configurations. 18th AIAA Applied Aerodynamics Conference, Denver (usa), 14.-17.08.2000.

Full text not available from this repository.

Abstract

Computations of lift and drag polars for a transport aircraft wing/fuselage high lift configurations using the block-structured and hybrid MEGAFLOW code system (FLOWer/Tau) are carried out and compared to windtunnel experiments.

Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=2001, monograph_id=AIAA-2000-4326,
Title:Aspects of 3D RANS Simulations for Transport Aircraft High-Lift Configurations
Authors:
AuthorsInstitution or Email of Authors
Rudnik, R.UNSPECIFIED
Melber, S.UNSPECIFIED
Ronzheimer, A.UNSPECIFIED
Brodersen, O.UNSPECIFIED
Date:2000
Status:Published
Event Title:18th AIAA Applied Aerodynamics Conference, Denver (usa), 14.-17.08.2000
Organizer:AIAA
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:other
DLR - Research area:Aeronautics
DLR - Program:L ST - Starrflüglertechnologien
DLR - Research theme (Project):L - Concepts & Integration
Location: Köln-Porz , Braunschweig , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Institut für Entwurfsaerodynamik
Deposited By: Claudia Grant
Deposited On:16 Sep 2005
Last Modified:14 Jan 2010 20:16

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