2018
DOI: 10.3390/ma11061019
|View full text |Cite
|
Sign up to set email alerts
|

Peculiarities in the Material Design of Buckling Resistance for Tensioned Laminated Composite Panels with Elliptical Cut-Outs

Abstract: The results of analytical and numerical studies of the buckling behavior of laminated multilayered tensioned sheets with circular and elliptical openings are presented. The analysis shows the significant influence of stress concentration effects on buckling modes and loads, particularly taking into consideration variations in the E1/E2 and E1/G12 ratios. The results of finite element (FE) computations prove that the buckling mode cannot be described by a single buckle localized at the apex of the hole. The opt… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
3
1
1

Citation Types

0
9
0

Year Published

2018
2018
2021
2021

Publication Types

Select...
10

Relationship

1
9

Authors

Journals

citations
Cited by 17 publications
(9 citation statements)
references
References 33 publications
0
9
0
Order By: Relevance
“…For composite laminated 2D structures the variety of problems connected with the definitions of appropriate design variables, objectives functions and optimization algorithms is discussed in Refs [51][52][53][54][55]. Figure A1.…”
Section: Discussionmentioning
confidence: 99%
“…For composite laminated 2D structures the variety of problems connected with the definitions of appropriate design variables, objectives functions and optimization algorithms is discussed in Refs [51][52][53][54][55]. Figure A1.…”
Section: Discussionmentioning
confidence: 99%
“…aspect ratio and plate area. Muc 90 in a recent study comparing analytical predictions of buckling strength with results of FE simulation for laminated composites with elliptical holes found that buckling resistance and stress concentration were mutually dependent.…”
Section: Buckling Of Composite Plates With Holesmentioning
confidence: 99%
“…The application of these elliptical cutouts within thin-walled structures for aeronautical applications cannot be avoided, as these cutouts being necessary for the realization of doors and windows or the presence of electrical cables and pipes in ship structures. The significance of stress concentration effect on buckling modes in tensioned laminate with circular and elliptical openings is analysed by Muc (2018). Muc and Romanowicz (2017), Muc et al (2017Muc et al ( , 2018a investigated circular and elliptical (vertical and horizontal) holes in composite laminates for static and fatigue damage.…”
Section: Introductionmentioning
confidence: 99%