Stanewsky, E. and Rosemann, H. (2000) Aspects of Shock Control and Adaptive Wing Technology. Vieweg u. Sohn (to be published in 2001). CEAS/DragNet European Drag Reduction Conference 2000, Potsdam, 19-21 June 2000.
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The development of the boundary layer and shock boundary layer interaction es-sentially determine the performance boundaries of transonic transport aircraft. Employing shock and boundary layer control has therefore a large potential for improving flight perform-ance in terms of cruise drag and with regard to the drag-rise and buffet boundaries. Various means of shock and boundary layer control are described and aerodynamic performance im-provements due to control discussed. Shock conditions and critical stages in the development of the boundary layer on a wing are, however, strongly dependent on freestream conditions which change considerably during a typical aircraft flight mission. In order to optimize per-formance at all points of the flight envelope, the effective wing geometry and other means of control must therefore adjust to these changing conditions. Adaptive wing aspects are, conse-quently, being addressed.
|Document Type:||Conference or Workshop Item (Speech)|
|Title:||Aspects of Shock Control and Adaptive Wing Technology|
|Publisher:||Vieweg u. Sohn (to be published in 2001)|
|Keywords:||Transonic flow / flow control / adaptive wing / shock waves / boundary layers / drag reduction / wing aerodynamics|
|Event Title:||CEAS/DragNet European Drag Reduction Conference 2000, Potsdam, 19-21 June 2000|
|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):||UNSPECIFIED|
|Location:||Köln-Porz , Braunschweig , Göttingen|
|Institutes and Institutions:||Institute of Aerodynamics and Flow Technology > Institut für Strömungsmechanik|
|Deposited By:||elib DLR-Beauftragter|
|Deposited On:||16 Sep 2005|
|Last Modified:||14 Jan 2010 21:00|
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