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Three dimensional large scale aerodynamic shape optimization based on shape calculus

Schmidt, Stephan and Gauger, Nicolas and Ilic, Caslav and Schulz, Volker (2011) Three dimensional large scale aerodynamic shape optimization based on shape calculus. 41st AIAA Fluid Dynamics Conference and Exhibit, June 27-30, 2011, Honolulu, USA.

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Abstract

Large scale three dimensional aerodynamic shape optimization based on the compressible Euler equations is considered. Shape calculus is used to derive an exact surface formulation of the gradients, enabling the computation of shape gradient information for each surface mesh node without having to calculate further mesh sensitivities. Special attention is paid to the applicability to large scale three dimensional problems like the optimization of an Onera M6 wing or a complete blended wing-body aircraft. The actual optimization is conducted in a one-shot fashion where the tangential Laplace-operator is used as a Hessian approximation, thereby also preserving the regularity of the shape.

Item URL in elib:https://elib.dlr.de/75982/
Document Type:Conference or Workshop Item (Paper)
Title:Three dimensional large scale aerodynamic shape optimization based on shape calculus
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Schmidt, StephanUniversity of TrierUNSPECIFIED
Gauger, NicolasRWTH Aachen UniversityUNSPECIFIED
Ilic, CaslavGerman Aerospace Center (DLR)UNSPECIFIED
Schulz, VolkerUniversity of TrierUNSPECIFIED
Date:June 2011
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:shape derivative, large scale, aerodynamic optimization, adjoint, Euler flow
Event Title:41st AIAA Fluid Dynamics Conference and Exhibit
Event Location:Honolulu, USA
Event Type:international Conference
Event Dates:June 27-30, 2011
Organizer:AIAA
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 - Flight Physics (old)
Location: Braunschweig
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Transport Aircraft
Deposited By: Ilic, Caslav
Deposited On:14 Jun 2012 09:53
Last Modified:31 Jul 2019 19:36

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