Details
| Originalsprache | Englisch |
|---|---|
| Seiten (von - bis) | 648-656 |
| Seitenumfang | 9 |
| Fachzeitschrift | Thin-walled structures |
| Jahrgang | 107 |
| Frühes Online-Datum | 25 Aug. 2016 |
| Publikationsstatus | Veröffentlicht - Okt. 2016 |
Abstract
The buckling load of cylindrical shells is heavily dependent on geometric imperfections and other non-traditional imperfections such as scattering wall thicknesses or loading imperfections. In this paper, the probabilistic perturbation load approach (PPLA) is proposed. This procedure is independent from costly measurements of geometric imperfections and is able to include various kinds of non-traditional imperfections by integrating the single perturbation load approach into a semi-analytical probabilistic framework. It is shown that the PPLA leads to design loads which are lower than the experimental buckling loads and much less conservative than the ones obtained from NASA SP-8007 in all investigated cases.
ASJC Scopus Sachgebiete
- Ingenieurwesen (insg.)
- Tief- und Ingenieurbau
- Ingenieurwesen (insg.)
- Bauwesen
- Ingenieurwesen (insg.)
- Maschinenbau
Zitieren
- Standard
- Harvard
- Apa
- Vancouver
- BibTex
- RIS
in: Thin-walled structures, Jahrgang 107, 10.2016, S. 648-656.
Publikation: Beitrag in Fachzeitschrift › Artikel › Forschung › Peer-Review
}
TY - JOUR
T1 - Probabilistic perturbation load approach for designing axially compressed cylindrical shells
AU - Meurer, Alexander
AU - Kriegesmann, Benedikt
AU - Dannert, Mona
AU - Rolfes, Raimund
N1 - Funding information: The research leading to these results has received funding from the European Community’s Seventh Framework Programme (FP7/2007-2013) under Priority Space, Grant agreement no. 282522 ( www.DESICOS.eu ). The information in this paper reflects only the authors’ views and the European Community is not liable for any use that may be made of the information contained therein.
PY - 2016/10
Y1 - 2016/10
N2 - The buckling load of cylindrical shells is heavily dependent on geometric imperfections and other non-traditional imperfections such as scattering wall thicknesses or loading imperfections. In this paper, the probabilistic perturbation load approach (PPLA) is proposed. This procedure is independent from costly measurements of geometric imperfections and is able to include various kinds of non-traditional imperfections by integrating the single perturbation load approach into a semi-analytical probabilistic framework. It is shown that the PPLA leads to design loads which are lower than the experimental buckling loads and much less conservative than the ones obtained from NASA SP-8007 in all investigated cases.
AB - The buckling load of cylindrical shells is heavily dependent on geometric imperfections and other non-traditional imperfections such as scattering wall thicknesses or loading imperfections. In this paper, the probabilistic perturbation load approach (PPLA) is proposed. This procedure is independent from costly measurements of geometric imperfections and is able to include various kinds of non-traditional imperfections by integrating the single perturbation load approach into a semi-analytical probabilistic framework. It is shown that the PPLA leads to design loads which are lower than the experimental buckling loads and much less conservative than the ones obtained from NASA SP-8007 in all investigated cases.
KW - Buckling
KW - Cylindrical shells
KW - Imperfections
KW - Probabilistic design
KW - Single perturbation load
UR - http://www.scopus.com/inward/record.url?scp=84982719294&partnerID=8YFLogxK
U2 - 10.1016/j.tws.2016.07.021
DO - 10.1016/j.tws.2016.07.021
M3 - Article
AN - SCOPUS:84982719294
VL - 107
SP - 648
EP - 656
JO - Thin-walled structures
JF - Thin-walled structures
SN - 0263-8231
ER -