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Surrogate-Based Robust Aerodynamic Shape Optimization of Airfoils Considering Geometric Uncertainties

Maruyama, Daigo and Liu, Dishi and Görtz, Stefan (2015) Surrogate-Based Robust Aerodynamic Shape Optimization of Airfoils Considering Geometric Uncertainties. 17. STAB Workshop, 10.-11. Nov. 2015, Göttingen, Deutschland.

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Item URL in elib:https://elib.dlr.de/100743/
Document Type:Conference or Workshop Item (Speech)
Title:Surrogate-Based Robust Aerodynamic Shape Optimization of Airfoils Considering Geometric Uncertainties
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Maruyama, Daigodaigo.maruyama (at) dlr.deUNSPECIFIED
Liu, Dishidishi.liu (at) dlr.deUNSPECIFIED
Görtz, StefanStefan.Goertz (at) dlr.deUNSPECIFIED
Date:November 2015
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Volume:2015
Page Range:pp. 54-55
Series Name:STAB-Mitteilung
Status:Published
Keywords:uncertainty, robust design, CFD, aerodynamics, surrogate model, adjoint, gradient, Kriging, quasi Monte Carlo, TAU, Subplex
Event Title:17. STAB Workshop
Event Location:Göttingen, Deutschland
Event Type:Workshop
Event Dates:10.-11. Nov. 2015
Organizer:AB STAB
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:fixed-wing aircraft
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Simulation and Validation
Location: Braunschweig
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > C²A²S²E - Center for Computer Applications in AeroSpace Science and Engineering
Deposited By: Görtz, Stefan
Deposited On:10 Dec 2015 15:17
Last Modified:13 Dec 2017 09:15

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