Trenker, M. and Sobieczky, H. (2002) Using the Gasdynamic Knowledge Base for Aerodynamic Design and Optimization in the Transonic Regime. In: Inverse Problems in Engineering Mechanics 1, 3. Elsevier Science, Oxford. ISBN 0-08-043951-9.
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Refined concepts for high speed flow control in aerospace and turbomachinery applications suggest a retrospective look onto theoretical results of pre-CFD time for special airfoils, wings, bodies and internal flows because such results exhibit theoretically idealized behavior for some aspects in practical applications. Novel control mechanisms bring us closer to a mechanical realization of such special case studies. These provide known shape and (inviscid) flow properties in the transonic flow regime near Mach number unity, where numerical verification has always been a challenge to CFD and, for future generation SST concepts, an application to swept wings in supersonic flow.
|Document Type:||Contribution to a Collection|
|Title:||Using the Gasdynamic Knowledge Base for Aerodynamic Design and Optimization in the Transonic Regime|
|Journal or Publication Title:||Inverse Problems in Engineering Mechanics|
|In ISI Web of Science:||No|
|Publisher:||Elsevier Science, Oxford|
|Keywords:||Airfoils, Transonics, Inverse Design, Shock Waves, SST|
|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 - Flight Physics|
|Location:||Köln-Porz , Braunschweig , Göttingen|
|Institutes and Institutions:||Institute of Aerodynamics and Flow Technology|
|Deposited By:||elib DLR-Beauftragter|
|Deposited On:||31 Jan 2006|
|Last Modified:||14 Jan 2010 19:19|
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