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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. ISBN 978-3-319-67988-4.

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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:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Bach, TobiasTobias.Bach (at) dlr.deUNSPECIFIED
Hühne, Christianchristian.huehne (at) dlr.deUNSPECIFIED
Date:January 2018
Journal or Publication Title:Advances in Structural and Multidisciplinary Optimization
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
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
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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