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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: |
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| 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 | ||||
| HGF - Program: | Aeronautics | ||||
| HGF - Program Themes: | L AR - 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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