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Non-uniform rational B-splines based aerodynamic shape design optimization with the DLR TAU code

Martin, Mario Jaime and Andres, Esther and Widhalm, Markus and Bitrian, Pablo and Lozano, Carlos (2012) Non-uniform rational B-splines based aerodynamic shape design optimization with the DLR TAU code. International Journal of Aerospace Engineering, 226 (10), pp. 1225-1242. Sage Publications, Ltd.. DOI: 10.1177/0954410011421704.

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Abstract

With the improving capabilities of computational fluid dynamics (CFD) for the prediction of aerodynamic performance, CFD tools are now being increasingly used for aerodynamic design optimization in the aerospace industry. In this article, an automated optimization framework is presented to address inviscid aerodynamic design problems. Key aspects of this framework include the use of the continuous adjoint methodology to make the computational requirements independent of the number of design variables, and computer-aided design-based shape parameterization, which uses the flexibility of non-uniform rational B-splines to handle complex configurations.

Document Type:Article
Title:Non-uniform rational B-splines based aerodynamic shape design optimization with the DLR TAU code
Authors:
AuthorsInstitution or Email of Authors
Martin, Mario Jaimemariojmartin@telefonica.net
Andres, Estheresther.andres@insa.es
Widhalm, Markusmarkus.widhalm@dlr.de
Bitrian, Pablocfd03@inta.es
Lozano, Carloslozanorc@inta.es
Date:10 October 2012
Journal or Publication Title:International Journal of Aerospace Engineering
Refereed publication:Yes
In Open Access:Yes
In SCOPUS:Yes
In ISI Web of Science:No
Volume:226
DOI:10.1177/0954410011421704
Page Range:pp. 1225-1242
Editors:
EditorsEmail
Martinez-Val, RodrigoUNSPECIFIED
Publisher:Sage Publications, Ltd.
Status:Published
Keywords:shape design, gradient-based optimization, adjoint methods, CAD-based parameterization, NURBS
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Aircraft Research
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Simulation & Validation
Location: Braunschweig
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > C²A²S²E - Center for Computer Applications in AeroSpace Science and Engineering
Deposited By: Markus Widhalm
Deposited On:19 Nov 2012 14:08
Last Modified:12 Dec 2013 21:49

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