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Buckling of launch-vehicle cylinders under axial compression: A comparison of experimental and numerical knockdown factors

Wagner, Ronald and Hühne, Christian and Niemann, Steffen (2020) Buckling of launch-vehicle cylinders under axial compression: A comparison of experimental and numerical knockdown factors. Thin-Walled Structures. Elsevier. doi: 10.1016/j.tws.2020.106931. ISSN 0263-8231.

Full text not available from this repository.

Official URL: https://doi.org/10.1016/j.tws.2020.106931


Item URL in elib:https://elib.dlr.de/135561/
Document Type:Article
Title:Buckling of launch-vehicle cylinders under axial compression: A comparison of experimental and numerical knockdown factors
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Wagner, RonaldRonald.Wagner (at) tu-braunschweig.dehttps://orcid.org/0000-0003-2749-1455
Hühne, ChristianChristian.Huehne (at) dlr.dehttps://orcid.org/0000-0002-2218-1223
Niemann, SteffenSteffen.Niemann (at) dlr.dehttps://orcid.org/0000-0001-9272-0635
Date:2020
Journal or Publication Title:Thin-Walled Structures
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:Yes
DOI :10.1016/j.tws.2020.106931
Publisher:Elsevier
ISSN:0263-8231
Status:Published
Keywords:Shell buckling Robust design Knockdown factor Geometric imperfection NASA SBKF
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Transportation
DLR - Research area:Raumfahrt
DLR - Program:R RP - Space Transportation
DLR - Research theme (Project):R - Raumfahrzeugsysteme - Numerische Verfahren und Simulation (old)
Location: Braunschweig
Institutes and Institutions:Institute of Composite Structures and Adaptive Systems > Functional Lightweight Structures
Deposited By: Kobus, Christine
Deposited On:27 Jul 2020 09:10
Last Modified:15 Jul 2021 16:26

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