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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
doi: 10.1016/j.tws.2021.107526
Article, Bibliographie

Item Type: Article
Erschienen: 2021
Creators: Alhajahmad, A. ; Mittelstedt, C.
Type of entry: Bibliographie
Title: Minimum weight design of curvilinearly grid-stiffened variable-stiffness composite fuselage panels considering buckling and manufacturing constraints
Language: English
Date: 14 February 2021
Publisher: Elsevier
Journal or Publication Title: Thin-Walled Structures
Volume of the journal: 161
DOI: 10.1016/j.tws.2021.107526
URL / URN: https://www.sciencedirect.com/science/article/abs/pii/S02638...
Divisions: 16 Department of Mechanical Engineering
16 Department of Mechanical Engineering > Institute for Lightweight Construction and Design-KluB (2023 renamed in Leichtbau und Strukturmechanik (LSM))
Date Deposited: 19 Mar 2021 07:43
Last Modified: 19 Mar 2021 07:43
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