Experimental investigations of compressed sandwich composite/honeycomb cylindrical shells
Authors:
- A. Muc,
- A. Stawiarski,
- P. Romanowicz
Abstract
This article explains in some details the behaviour of thick, deep cylindrical sandwich panels subjected to compressive loads. In general, experimental results indicated that two different forms of failure have been observed – the first corresponds to the overall buckling and the second to the facesheet wrinkling. The obtained experimentally damages of shells are verified and validated with the use of the FE analysis, 2-D and 3-D both in the linear and non-linear approach. The unidirectional strain gauges were applied to detect the initiation of the overall buckling mode.
- Record ID
- CUT60add0e237f24223ac8343fa9812bf12
- Publication categories
- ;
- Author
- Journal series
- Applied Composite Materials, ISSN 0929-189X, e-ISSN 1573-4897
- Issue year
- 2018
- Vol
- 25
- No
- 1
- Pages
- 177-189
- Other elements of collation
- fot.; schem.; wykr.; Bibliografia (na s.) - 188-189; Bibliografia (liczba pozycji) - 19; Oznaczenie streszczenia - Abstr.; Data udostępnienia on-line - 2017-06-30; Numeracja w czasopiśmie - Vol. 25, Iss. 1
- Keywords in English
- sandwich cylindrical shell, buckling, failure analysis, experimental study
- DOI
- DOI:10.1007/s10443-017-9614-8 Opening in a new tab
- URL
- https://link.springer.com/article/10.1007/s10443-017-9614-8 Opening in a new tab
- Language
- eng (en) English
- License
- Score (nominal)
- 30
- Additional fields
- Indeksowana w: Web of Science, Scopus
- Uniform Resource Identifier
- https://cris.pk.edu.pl/info/article/CUT60add0e237f24223ac8343fa9812bf12/
- URN
urn:pkr-prod:CUT60add0e237f24223ac8343fa9812bf12
* presented citation count is obtained through Internet information analysis, and it is close to the number calculated by the Publish or PerishOpening in a new tab system.