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The influence of the manufacturing process and test boundary conditions on the buckling load of thin-walled cylindrical CFRP shells

Hartwich, Tobias S. and Panek, Stefan and Wilckens, Dirk and Bock, Matthias and Krause, Dieter (2023) The influence of the manufacturing process and test boundary conditions on the buckling load of thin-walled cylindrical CFRP shells. Composite Structures. Elsevier. doi: 10.1016/j.compstruct.2023.116674. ISSN 0263-8223.

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Official URL: https://www.sciencedirect.com/science/article/pii/S0263822323000181?via%3Dihub

Abstract

Thin-walled cylindrical CFRP shells tend to buckle under compressive loads. The experimental buckling load is significantly lower than the theoretical one. The reason for this are various kinds of imperfections which are partially caused by the manufacturing process and the test conditions. A major challenge in the design of these shells is the lack of experimental data. Additionally, the quality of test results is rarely critically reviewed in the validation of design approaches. In this paper, the influence of two different manufacturing processes on the geometric imperfections and the influence of three different test rigs on the buckling load are investigated in an experimental campaign with 12 cylindrical CFRP shells. Furthermore, the influence of varying the test rig boundary conditions is analysed.

Item URL in elib:https://elib.dlr.de/197221/
Document Type:Article
Title:The influence of the manufacturing process and test boundary conditions on the buckling load of thin-walled cylindrical CFRP shells
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Hartwich, Tobias S.TU HHUNSPECIFIEDUNSPECIFIED
Panek, StefanTU HHUNSPECIFIEDUNSPECIFIED
Wilckens, DirkUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Bock, MatthiasUNSPECIFIEDhttps://orcid.org/0000-0002-1043-713XUNSPECIFIED
Krause, DieterTU HHUNSPECIFIEDUNSPECIFIED
Date:January 2023
Journal or Publication Title:Composite Structures
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:Yes
DOI:10.1016/j.compstruct.2023.116674
Publisher:Elsevier
Series Name:Elsevier
ISSN:0263-8223
Status:Published
Keywords:Buckling, Composite shells, Imperfections, Test rig
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Components and Systems
DLR - Research area:Aeronautics
DLR - Program:L CS - Components and Systems
DLR - Research theme (Project):L - Structural Materials and Design
Location: Braunschweig
Institutes and Institutions:Institut für Systemleichtbau > Central Services
Institut für Systemleichtbau > Structural Mechanics
Deposited By: Schlegel, Linda
Deposited On:18 Sep 2023 11:38
Last Modified:19 Sep 2023 08:44

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