Structural Optimization of Stiffened Composite Panels for Highly Flexible Aircraft Wings

Bach, Tobias and Hühne, Christian (2018) Structural Optimization of Stiffened Composite Panels for Highly Flexible Aircraft Wings. In: Advances in Structural and Multidisciplinary Optimization Springer International Publishing AG. doi: 10.1007/978-3-319-67988-4. ISBN 978-3-319-67988-4.

Full text not available from this repository.

Item URL in elib:

https://elib.dlr.de/118957/

Document Type:

Book Section

Title:

Structural Optimization of Stiffened Composite Panels for Highly Flexible Aircraft Wings

Authors:

Authors	Institution or Email of Authors	Author's ORCID iD	ORCID Put Code
Bach, Tobias	Tobias.Bach (at) dlr.de	UNSPECIFIED	UNSPECIFIED
Hühne, Christian	christian.huehne (at) dlr.de	UNSPECIFIED	UNSPECIFIED

Date:

January 2018

Journal or Publication Title:

Advances in Structural and Multidisciplinary Optimization

Refereed publication:

Yes

Open Access:

Gold Open Access:

In SCOPUS:

In ISI Web of Science:

DOI:

10.1007/978-3-319-67988-4

Publisher:

Springer International Publishing AG

ISBN:

978-3-319-67988-4

Status:

Published

Keywords:

Sizing optimization, composites, stiffened panels, gradient–based optimization, DFEM

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 - Structures and Materials (old)

Location:

Braunschweig

Institutes and Institutions:

Institute of Composite Structures and Adaptive Systems > Functional Lightweight Structures

Deposited By:

Bach, Tobias

Deposited On:

05 Mar 2018 06:45

Last Modified:

05 Mar 2018 06:45

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