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. EB 124-2016/907. Other. 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:

Authors	Institution or Email of Authors	Author's ORCID iD
Ma, Fei	UNSPECIFIED	UNSPECIFIED

Date:

2016

Refereed publication:

Open Access:

Gold Open Access:

In SCOPUS:

In ISI Web of Science:

Number of Pages:

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 (old)

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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