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Single perturbation load approach: new definition for P1 and explaining the constancy of the buckling load

Castro, Saullo and Arbelo, Mariano and Degenhardt, Richard and Ziegmann, Gerhard (2015) Single perturbation load approach: new definition for P1 and explaining the constancy of the buckling load. 3rd Int. Conference on Buckling and Postbuckling Behaviour of Composite Laminated Shell Structures, 2015-03-25 - 2015-03-27, Braunschweig.

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Official URL: http://www.desicos.eu

Abstract

The single perturbation load approach is a deterministic analysis method applied in the determination of design loads for imperfection sensitive structures. As verified by Hühne et al., imperfection sensitive cylindrical structures when subjected to axial compression will exhibit a progressively decreasing load carrying capacity for growing imperfection amplitudes up to a threshold, where the buckling load remains nearly constant. The method was named single perturbation load because a unitary lateral load is used to create the geometric imperfection, and the threshold perturbation load beyond which the buckling load is nearly constant is called P1. The aim of the present paper is to summarize what has been presented by Castro et al., explaining the constancy of the buckling load and giving a precise definition for the threshold perturbation load P1.

Item URL in elib:https://elib.dlr.de/96865/
Document Type:Conference or Workshop Item (Speech)
Title:Single perturbation load approach: new definition for P1 and explaining the constancy of the buckling load
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Castro, SaulloPFH GöttingenUNSPECIFIEDUNSPECIFIED
Arbelo, MarianoPFH GöttingenUNSPECIFIEDUNSPECIFIED
Degenhardt, RichardDLRUNSPECIFIEDUNSPECIFIED
Ziegmann, GerhardTU ClausthalUNSPECIFIEDUNSPECIFIED
Date:25 March 2015
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:Buckling, knock-down factor, knockdown factor, space, design, structural analysis, thin-walled structure, composite, single perturbation load approach (SPLA)
Event Title:3rd Int. Conference on Buckling and Postbuckling Behaviour of Composite Laminated Shell Structures
Event Location:Braunschweig
Event Type:international Conference
Event Start Date:25 March 2015
Event End Date:27 March 2015
Organizer:DLR
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 - HL-Primärstrukturen für Orbitale Systeme (old)
Location: Braunschweig
Institutes and Institutions:Institute of Composite Structures and Adaptive Systems > Structural Mechanics
Deposited By: Degenhardt, Prof. Dr. Richard
Deposited On:13 Sep 2023 11:57
Last Modified:24 Apr 2024 20:02

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