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Computational methods for aero-structural analysis and optimisation of aircrafts based on reduced-order structural models

  • In this part of the MEGADESIGN project, aeroelastic effects are introduced into the aerodynamic analysis of aircrafts by coupling DLR’s flow solvers TAU and FLOWer to a Timoshenko-beam solver. The emerging aeroelastic solvers and a method for the automatic identification of Timoshenko-beam models for wing-box structures were integrated into a simulation environment enabling the combined optimisation of aerodynamic wing shape and structure.

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Metadaten
Author:Lars Reimer, Georg Wellmer, Carsten BraunORCiD, Josef Ballmann
ISBN:978-3-642-04092-4
Parent Title (English):MEGADESIGN and MegaOpt - German initiatives for aerodynamic simulation and optimization in aircraft design. Results of the closing symposium of the MEGADESIGN and MegaOpt projects, Braunschweig, Germany, 23 - 24 May, 2007 / Norbert Kroll ... (Eds.) Notes on numerical fluid mechanics and multidisciplinary design. Vol. 107
Publisher:Springer
Place of publication:Berlin
Document Type:Part of a Book
Language:English
Year of Completion:2009
Date of the Publication (Server):2013/06/21
First Page:135
Last Page:150
Link:http://link.springer.com/chapter/10.1007/978-3-642-04093-1_10
Zugriffsart:bezahl
Institutes:FH Aachen / Fachbereich Luft- und Raumfahrttechnik
collections:Verlag / Springer