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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.

Abstract

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.

Item URL in elib:https://elib.dlr.de/12673/
Document Type:Contribution to a Collection
Additional Information: LIDO-Berichtsjahr=2003,
Title:Using the Gasdynamic Knowledge Base for Aerodynamic Design and Optimization in the Transonic Regime
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Trenker, M.UNSPECIFIEDUNSPECIFIED
Sobieczky, H.UNSPECIFIEDUNSPECIFIED
Date:2002
Journal or Publication Title:Inverse Problems in Engineering Mechanics
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Volume:3
Editors:
EditorsEmail
Tanaka, M.UNSPECIFIED
Dulikravich, G.S.UNSPECIFIED
Publisher:Elsevier Science, Oxford
Series Name:1
ISBN:0-08-043951-9
Status:Published
Keywords:Airfoils, Transonics, Inverse Design, Shock Waves, SST
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:Aircraft Research (old)
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Flight Physics (old)
Location: Köln-Porz , Braunschweig , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology
Deposited By: DLR-Beauftragter, elib
Deposited On:31 Jan 2006
Last Modified:14 Jan 2010 19:19

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