elib
DLR-Header
DLR-Logo -> http://www.dlr.de
DLR Portal Home | Imprint | Privacy Policy | Accessibility | Contact | Deutsch
Fontsize: [-] Text [+]

Evaluation of the Stability and Load-Carrying Capacity of Double-Curved Unstiffened Shells Under Compression Through Analysis of Different Initial Imperfection Sources

Gliszczynski, Adrian and Franzoni, Felipe and Baciu, Theodor and Degenhardt, Richard (2025) Evaluation of the Stability and Load-Carrying Capacity of Double-Curved Unstiffened Shells Under Compression Through Analysis of Different Initial Imperfection Sources. Aerospace Science and Technology, 168. Elsevier. doi: 10.1016/j.ast.2025.110907. ISSN 1270-9638.

[img] PDF - Published version
49MB

Abstract

The article concerns the use of various sources of initial imperfections to numerically assess the stability and load-carrying capacity of thin-walled segments of isotropic and composite toroidal shells subjected to compression. The considered sources of initial imperfections are: Linear Buckling Mode-shaped Imperfection, Single Perturbation Load Imperfection and actual maps of mid-surface (MSI) and thickness imperfections, originally measured for unstiffened cylindrical and conical shells. The most conservative Knock-Down Factor estimates were determined using Linear Buckling Mode approach, while the results provided by Single Perturbation Load approach were consistent with those obtained using measured MSI but were slightly more conservative. The studies demonstrated that a slight convexity can increase the load-carrying capacity of a composite doubly curved structure compared to the nominal cylinder or cone structure. Some of the analysed concave structures exhibited characteristics of imperfection-insensitive structures, where the load-carrying capacity significantly exceeded the critical buckling load determined from linear stability analysis.

Item URL in elib:https://elib.dlr.de/216502/
Document Type:Article
Title:Evaluation of the Stability and Load-Carrying Capacity of Double-Curved Unstiffened Shells Under Compression Through Analysis of Different Initial Imperfection Sources
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Gliszczynski, AdrianLodz University of Technologyhttps://orcid.org/0000-0002-2421-093XUNSPECIFIED
Franzoni, FelipeFelipe.Franzoni (at) dlr.dehttps://orcid.org/0000-0002-9977-7607192395136
Baciu, TheodorDLRUNSPECIFIEDUNSPECIFIED
Degenhardt, RichardRichard.Degenhardt (at) dlr.dehttps://orcid.org/0000-0002-9766-9418UNSPECIFIED
Date:13 September 2025
Journal or Publication Title:Aerospace Science and Technology
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:Yes
Volume:168
DOI:10.1016/j.ast.2025.110907
Publisher:Elsevier
ISSN:1270-9638
Status:Published
Keywords:Double-curved shell, Toroidal Shell, Single perturbation load imperfection Linear buckling mode imperfection, Measured mid-surface imperfection, Knockdown factor
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Research under Space Conditions
DLR - Research area:Raumfahrt
DLR - Program:R FR - Research under Space Conditions
DLR - Research theme (Project):R - Material Design and New Materials
Location: Braunschweig
Institutes and Institutions:Institut für Systemleichtbau > Structural Mechanics
Deposited By: Degenhardt, Prof. Dr. Richard
Deposited On:22 Sep 2025 09:52
Last Modified:08 Oct 2026 09:40

Repository Staff Only: item control page

Browse
Search
Help & Contact
Information
OpenAIRE Validator logo electronic library is running on EPrints
Website and database design: Copyright © German Aerospace Center (DLR). All rights reserved.