The application of adjoint-based airfoil optimization with discretization error control to a benchmark problem

Li, Ding and Hartmann, Ralf (2014) The application of adjoint-based airfoil optimization with discretization error control to a benchmark problem. STAB Symposium 2014, 2014-11-04 - 2014-11-05, München, Germany.

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Abstract

Adjoint-based airfoil shape optimization is combined with adaptive mesh refinement and error control.

Item URL in elib:

https://elib.dlr.de/92447/

Document Type:

Conference or Workshop Item (Speech)

Title:

The application of adjoint-based airfoil optimization with discretization error control to a benchmark problem

Authors:

Authors	Institution or Email of Authors	Author's ORCID iD	ORCID Put Code
Li, Ding	Ding.Li (at) dlr.de	UNSPECIFIED	UNSPECIFIED
Hartmann, Ralf	Ralf.Hartmann (at) dlr.de	https://orcid.org/0000-0002-0403-1221	UNSPECIFIED

Date:

5 November 2014

Refereed publication:

Yes

Open Access:

Gold Open Access:

In SCOPUS:

In ISI Web of Science:

Status:

Published

Keywords:

shape optimization, adaptive mesh refinement, error estimation

Event Title:

STAB Symposium 2014

Event Location:

München, Germany

Event Type:

national Conference

Event Start Date:

4 November 2014

Event End Date:

5 November 2014

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:

Hartmann, Dr.rer.nat. Ralf

Deposited On:

25 Nov 2014 09:42

Last Modified:

24 Apr 2024 19:58

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