This paper presents the numerical simulation (DLR TAU-code) and the analysis of viscous high-lift flow around a complex wing/body configuration (DLR ALVAST) in landing configuration. The investigations aim for a better understanding of the aerodynamics at the wing root and the lift breakdown for such a configuration.
Aerodynamics of the Wing/Fuselage Junction at an Transport Aircraft in High-Lift Configuration
2010
8 Seiten
Conference paper
English
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