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Numerical Design of a Low-Noise High-Lift System for a Supersonic Aircraft

Herrmann, U. (2004) Numerical Design of a Low-Noise High-Lift System for a Supersonic Aircraft. 14th DGLR/STAB Symposium, Bremen (de), 16.-18.11.2004.

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Abstract

Supersonic commercial transport aircraft (SCT) are known for their favourable short travel times and their low-speed noise. Any attempt towards new SCT`s therefore needs to aim at technologies for low noise take-off and landing. The EC-Project EPISTLE focuses on aerodynamic high-lift system designs contributing significant low-speed noise reductions. The high-lift system design and validation work at DLR relying on separated flow topology will be reported.

Document Type:Conference or Workshop Item (Speech)
Additional Information: LIDO-Berichtsjahr=2005,
Title:Numerical Design of a Low-Noise High-Lift System for a Supersonic Aircraft
Authors:
AuthorsInstitution or Email of Authors
Herrmann, U.UNSPECIFIED
Date:2004
Status:Published
Keywords:Low drag, high-lift design, noise reduction
Event Title:14th DGLR/STAB 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 - Concepts & Integration
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 19:48

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