2014
DOI: 10.1016/j.ijmecsci.2014.04.019
|View full text |Cite
|
Sign up to set email alerts
|

Optimum design of laminates containing an elliptical hole

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
3
2

Citation Types

1
14
0

Year Published

2016
2016
2020
2020

Publication Types

Select...
6
2

Relationship

0
8

Authors

Journals

citations
Cited by 37 publications
(15 citation statements)
references
References 21 publications
1
14
0
Order By: Relevance
“…the highest failure strength was observed for the horizontal ellipses and the lowest for the vertical elliptical holes. The obtained optimal fibre orientations presented by Sharma et al [59] are different than those presented above since the mentioned authors analysed infinite plates only.…”
Section: Buckling Of Cylindrical Shells With Domed Headsmentioning
confidence: 56%
See 1 more Smart Citation
“…the highest failure strength was observed for the horizontal ellipses and the lowest for the vertical elliptical holes. The obtained optimal fibre orientations presented by Sharma et al [59] are different than those presented above since the mentioned authors analysed infinite plates only.…”
Section: Buckling Of Cylindrical Shells With Domed Headsmentioning
confidence: 56%
“…The results of buckling investigations for spherical and ellipsoidal domes with and without cylindrical portions and the possibility of optimal design were studied in details by Muc [57,58]. For a infinite laminated plates subjected to axial/biaxial compression/tension or in-plane shear and having a circular/ elliptical hole the optimum design of laminate stacking sequence is presented by Sharma et al [59]. The authors of the paper adapted the formulation and the solution given by Lekhnitski [60], Savin [61] for stresses around holes in an infinite angle-ply balanced symmetric laminated plates under in-plane loading (Fig.1)…”
Section: Buckling Of Cylindrical Shells With Domed Headsmentioning
confidence: 99%
“…Therefore, how to decide the two angles of an orthotropic plate in minimization of the stress concentration is important. Sharma et al (2014) researched the optimization of fiber orientation angle for single lamina of composite materials (graphite/epoxy and glass/epoxy) with circular and elliptical holes; however, the hole orientation angle was not taken into consideration. In this paper, not only the fiber orientation angle but also the hole orientation angle are taken into consideration, and other more complicated shapes of holes are considered, in which the maximum absolute value of the tangential stress reaches its minimum value.…”
Section: Introductionmentioning
confidence: 99%
“…Jafari and Rohani 14 used the analytical solution to determine the stress distribution around different cutouts in perforated composite plates. An optimum design of symmetric laminated plate containing an elliptical cutout and subjected to various in-plane loading conditions was presented by Sharma et al 15 using complex variable approach and GA.…”
Section: Introductionmentioning
confidence: 99%