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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. Hindawi Publishing Corporation. 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.

Item URL in elib:https://elib.dlr.de/78115/
Document Type:Article
Title:Non-uniform rational B-splines based aerodynamic shape design optimization with the DLR TAU code
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Martin, Mario Jaimemariojmartin (at) telefonica.netUNSPECIFIED
Andres, Estheresther.andres (at) insa.esUNSPECIFIED
Widhalm, Markusmarkus.widhalm (at) dlr.deUNSPECIFIED
Bitrian, Pablocfd03 (at) inta.esUNSPECIFIED
Lozano, Carloslozanorc (at) inta.esUNSPECIFIED
Date:10 October 2012
Journal or Publication Title:International Journal of Aerospace Engineering
Refereed publication:Yes
Open Access:Yes
Gold Open Access:Yes
In SCOPUS:Yes
In ISI Web of Science:Yes
Volume:226
DOI :10.1177/0954410011421704
Page Range:pp. 1225-1242
Editors:
EditorsEmailEditor's ORCID iD
Martinez-Val, RodrigoUNSPECIFIEDUNSPECIFIED
Publisher:Hindawi Publishing Corporation
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 (old)
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Simulation & Validation (old)
Location: Braunschweig
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > C²A²S²E - Center for Computer Applications in AeroSpace Science and Engineering
Deposited By: Widhalm, Markus
Deposited On:19 Nov 2012 14:08
Last Modified:14 Dec 2019 04:27

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