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The Development and Status of TAU Inverse Design & TAU Adjoint Gradient Optimization Chain

Ma, Fei (2016) The Development and Status of TAU Inverse Design & TAU Adjoint Gradient Optimization Chain. Other. Other. EB 124-2016/907, 22 S.

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Abstract

The report reviews the TAU-Takanashi inverse design and the TAU adjoint gradient-based optimization process. The optimization process was successfully used for solving airfoil inverse design problems including optimizing lift, drag and pitching moment. For 3D inverse design Problems with twist, the TAU gradient-based optimization tried to approach to the target pressure distribution and geometry but a perfect match could not be achieved.

Item URL in elib:https://elib.dlr.de/109372/
Document Type:Monograph (Other, Other)
Additional Information:Ergebnisbericht
Title:The Development and Status of TAU Inverse Design & TAU Adjoint Gradient Optimization Chain
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Ma, Feifei.ma (at) dlr.deUNSPECIFIED
Date:2016
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:22
Status:Published
Keywords:CFD, Gradient-based Optimization, Adjoint, Inverse Design, Aerodynamics
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: Seyfried, Beate
Deposited On:13 Dec 2016 09:20
Last Modified:13 Dec 2016 09:20

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