Manufacture and buckling test of a variable-stiffness, variable-thickness composite cylinder under axial compression

2022 ◽  
Author(s):  
Reece Lincoln ◽  
Paul Weaver ◽  
Alberto Pirrera ◽  
Rainer M. Groh
2011 ◽  
Vol 93 (7) ◽  
pp. 1939-1946 ◽  
Author(s):  
Jingxuan He ◽  
Mingfa Ren ◽  
Shiyong Sun ◽  
Qizhong Huang ◽  
Xiannian Sun

2021 ◽  
Author(s):  
Peng Jiao ◽  
Zhiping Chen ◽  
Ma He ◽  
Delin Zhang ◽  
Jihang Wu ◽  
...  

2018 ◽  
Vol 35 (1) ◽  
pp. 201-211 ◽  
Author(s):  
Jifan Zhong ◽  
Yaochen Zheng ◽  
Jianqiao Chen ◽  
Zhao Jing

2013 ◽  
Vol 701 ◽  
pp. 425-429 ◽  
Author(s):  
M. S Ismail ◽  
B. T. H. T Baharudin ◽  
S. A. Yahya ◽  
H. A. Kahar

Results from Finite Element (FE) study on the response of composite cylinder shells with cutouts and subjected to internal pressure and axial compression are presented. The objective of the study is to improving the buckling load by applying the internal pressure whilst the compression load is applied. The effect of localized stress concentration distributed around the cutout region also being examined. The numerical results are obtained using ABAQUS finite element code software package. The composite cylinder shells were tested in two conditions which are a combination of axial compression load with internal pressure and a single axial compression load. The effects of varying internal pressure and cutout size on the pre-buckling, buckling, and post-buckling responses of the shell are demonstrated. Reasonable results comparison was obtained by reviewing previous literature. Results indicated that the load distribution and displacement of the cutout significantly influence the structural response of the shell. The results also indicate that the stress distributions can be affected by the size of the cutout under axial compression load.


2015 ◽  
Vol 22 (2) ◽  
pp. 149-156 ◽  
Author(s):  
Mohammad Rouhi ◽  
Hossein Ghayoor ◽  
Suong V. Hoa ◽  
Mehdi Hojjati

AbstractThe fiber steering capability of automated fiber placement machines offers the designers more room to fully exploit the directional properties of composite materials. Circumferential stiffness tailoring by fiber steering can considerably increase the bending-induced buckling performance of laminated composite cylinders. The potential structural improvement resulting from fiber steering depends on different design parameters such as the number of plies considered for fiber steering in a laminate. In this study, the buckling performance improvement of a variable stiffness (VS) composite cylinder is investigated for different percentages of plies considered for fiber steering in a multilayered composite laminate. A surrogate-based modeling along with a multi-step optimization is used in the design procedure of this study. The improvements in the buckling performance are shown and verified using finite element analysis in ABAQUS software. The mechanisms leading to buckling performance improvement of VS composites are also investigated and presented for different percentages of fiber-steered plies.


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