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Minimum weight design of curvilinearly grid-stiffened variable-stiffness composite fuselage panels considering buckling and manufacturing constraints

Alhajahmad, A. ; Mittelstedt, C. (2021):
Minimum weight design of curvilinearly grid-stiffened variable-stiffness composite fuselage panels considering buckling and manufacturing constraints.
In: Thin-Walled Structures, 161, p. 107526. Elsevier, ISSN 0263-8231,
DOI: 10.1016/j.tws.2021.107526,
[Article]

Item Type: Article
Erschienen: 2021
Creators: Alhajahmad, A. ; Mittelstedt, C.
Title: Minimum weight design of curvilinearly grid-stiffened variable-stiffness composite fuselage panels considering buckling and manufacturing constraints
Language: English
Journal or Publication Title: Thin-Walled Structures
Journal volume: 161
Publisher: Elsevier
Divisions: 16 Department of Mechanical Engineering
16 Department of Mechanical Engineering > Institute for Lightweight Construction and Design (KluB)
Date Deposited: 19 Mar 2021 07:43
DOI: 10.1016/j.tws.2021.107526
Official URL: https://www.sciencedirect.com/science/article/abs/pii/S02638...
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