Using the Gasdynamic Knowledge Base for Aerodynamic Design and Optimization in the Transonic Regime
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.
Full text not available from this repository.
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|
|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 - 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|
Repository Staff Only: item control page