Herrmann, U. (2004) High Performance High-Lift System Design for SCT in the EC-project EPISTLE. ECCOMAS 2004, Jyväskylä (fi), 24.-28.07.2004.
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The EC research project EPISTLE was able to design new low-drag high-lift systems using numerical tools. These high-lift systems were manufactured into a large scale wind tunnel model. The predicted drag reductions (20% compared to a datum system) were confirmed by wind tunnel tests at high Reynolds numbers in a pressurized wind tunnel. These drag reductions were confirmed to reduce the low-speed noise for such aircraft configurations considerable.
|Document Type:||Conference or Workshop Item (Paper)|
|Title:||High Performance High-Lift System Design for SCT in the EC-project EPISTLE|
|Keywords:||Viscous low-speed flow computations, High-Lift system design, Low-Speed drag reduction, Noise reduction, Large Scale Test, Validated numerical design method|
|Event Title:||ECCOMAS 2004, Jyväskylä (fi), 24.-28.07.2004|
|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 19:49|
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