Castro, Saullo und Arbelo, Mariano und Degenhardt, Richard und 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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Kurzfassung
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.
elib-URL des Eintrags: | https://elib.dlr.de/96865/ | ||||||||||||||||||||
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Dokumentart: | Konferenzbeitrag (Vortrag) | ||||||||||||||||||||
Titel: | Single perturbation load approach: new definition for P1 and explaining the constancy of the buckling load | ||||||||||||||||||||
Autoren: |
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Datum: | 25 März 2015 | ||||||||||||||||||||
Referierte Publikation: | Ja | ||||||||||||||||||||
Open Access: | Ja | ||||||||||||||||||||
Gold Open Access: | Nein | ||||||||||||||||||||
In SCOPUS: | Nein | ||||||||||||||||||||
In ISI Web of Science: | Nein | ||||||||||||||||||||
Status: | veröffentlicht | ||||||||||||||||||||
Stichwörter: | Buckling, knock-down factor, knockdown factor, space, design, structural analysis, thin-walled structure, composite, single perturbation load approach (SPLA) | ||||||||||||||||||||
Veranstaltungstitel: | 3rd Int. Conference on Buckling and Postbuckling Behaviour of Composite Laminated Shell Structures | ||||||||||||||||||||
Veranstaltungsort: | Braunschweig | ||||||||||||||||||||
Veranstaltungsart: | internationale Konferenz | ||||||||||||||||||||
Veranstaltungsbeginn: | 25 März 2015 | ||||||||||||||||||||
Veranstaltungsende: | 27 März 2015 | ||||||||||||||||||||
Veranstalter : | DLR | ||||||||||||||||||||
HGF - Forschungsbereich: | Luftfahrt, Raumfahrt und Verkehr | ||||||||||||||||||||
HGF - Programm: | Raumfahrt | ||||||||||||||||||||
HGF - Programmthema: | Raumtransport | ||||||||||||||||||||
DLR - Schwerpunkt: | Raumfahrt | ||||||||||||||||||||
DLR - Forschungsgebiet: | R RP - Raumtransport | ||||||||||||||||||||
DLR - Teilgebiet (Projekt, Vorhaben): | R - Raumfahrzeugsysteme - HL-Primärstrukturen für Orbitale Systeme (alt) | ||||||||||||||||||||
Standort: | Braunschweig | ||||||||||||||||||||
Institute & Einrichtungen: | Institut für Faserverbundleichtbau und Adaptronik > Strukturmechanik | ||||||||||||||||||||
Hinterlegt von: | Degenhardt, Prof. Dr. Richard | ||||||||||||||||||||
Hinterlegt am: | 13 Sep 2023 11:57 | ||||||||||||||||||||
Letzte Änderung: | 24 Apr 2024 20:02 |
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