2005
DOI: 10.1016/j.compositesb.2004.06.002
|View full text |Cite
|
Sign up to set email alerts
|

Experimental and numerical study of buckling response of composite shells compressed transversely between rigid platens

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2

Citation Types

1
1
0

Year Published

2015
2015
2021
2021

Publication Types

Select...
5

Relationship

1
4

Authors

Journals

citations
Cited by 6 publications
(2 citation statements)
references
References 12 publications
1
1
0
Order By: Relevance
“…Limit point buckling was evident for single-curved shells made from laminated materials. The shells collapsed after the initial buckling [7,8]. These phenomena were similar to what was observed in the isotropic metal shells [9].…”
Section: Introductionsupporting
confidence: 68%
“…Limit point buckling was evident for single-curved shells made from laminated materials. The shells collapsed after the initial buckling [7,8]. These phenomena were similar to what was observed in the isotropic metal shells [9].…”
Section: Introductionsupporting
confidence: 68%
“…Although the snap-through behaviour of the relevant c structural elements resemble each other generally, the details of the concerning phenomenon (which is different for different structural elements, dimensional characteristics, materials used) can be crucially important from the point of design and analysis of such systems. Therefore, it is not a surprise to observe publications on this subject receiving much attention for many years, including those in recent years [12][13][14][15][16][17][18][19][20][21][22][23][24][25][26][27][28].…”
Section: Introductionmentioning
confidence: 99%