Buckling Analysis of Laminated Composite Plates Submitted to Compression After Impact

被引：14

作者：

Amaro, A. M. ^{[1
,2
]}

Reis, P. N. B. ^{[3
]}

de Moura, M. F. S. F. ^{[4
]}

Neto, M. A. ^{[1
,2
]}

机构：

[1] CEMUC, P-3030 Coimbra, Portugal

[2] Univ Coimbra, Dept Mech Engn, P-3030 Coimbra, Portugal

[3] Univ Beira Interior UBI, Dept Electromech Engn, P-6200 Covilha, Portugal

[4] Univ Porto, Fac Engn, P-4200465 Oporto, Portugal

来源：

FIBERS AND POLYMERS | 2014年 / 15卷 / 03期

关键词：

Composites; Impact delamination; Buckling; Compressive strength; LOW-VELOCITY IMPACT; EPOXY COMPOSITES; DELAMINATION; FAILURE; CFRP; STRENGTH; BEHAVIOR; DAMAGE; PROPAGATION; PERFORMANCE;

D O I：

10.1007/s12221-014-0560-x

中图分类号：

TB3 [工程材料学]; TS1 [纺织工业、染整工业];

学科分类号：

0805 ; 080502 ; 0821 ;

摘要：

The aim of this work is the experimental evaluation of the residual strength of composite laminates under compression after low velocity impact. Different kinds of delaminations, partial, embedded and through-the-width, were studied. Carbon-fibre reinforced epoxy composite was used and the experimental tests were performed on [0](16), [0, 90, 0, 90](2S) and [0(i), 90(i)](s) with i=2, 3, 4, 5, using a drop-weight-testing machine. The impacted plates were inspected by the ultrasonic C-Scan to evaluate the size and the shape of the delamination. Results show that the presence of delamination decreases the compressive strength. The stacking sequence and laminate thickness were verified to have a remarkable influence on the value of the residual compressive strength, and play an important role on the observed buckling failure modes.

引用

页码：560 / 565

页数：6

共 50 条

[31] Buckling analysis of CNT reinforced functionally graded laminated composite plates
Lei, Z. X.
Zhang, L. W.
Liew, K. M.
COMPOSITE STRUCTURES, 2016, 152 : 62 - 73
[32] Compression-after impact behavior of laminated composite plates subjected to low velocity impact in high temperatures
Aktas, Mehmet
Karakuzu, Ramazan
Arman, Yusuf
COMPOSITE STRUCTURES, 2009, 89 (01) : 77 - 82
[33] Critical buckling of delaminated composite plates using exact stiffness analysis
Damghani, Mahdi
Kennedy, David
Featherston, Carol
COMPUTERS & STRUCTURES, 2011, 89 (13-14) : 1286 - 1294
[34] Buckling Analysis of Symmetrically Laminated Rectangular Thin Plates under Biaxial Compression
Altunsaray, Erkin
Bayer, Ismail
TEKNIK DERGI, 2021, 32 (06): : 11287 - 11314
[35] Research on size effects in the low-velocity impact (LVI) and compression after impact (CAI) characteristics of composite laminates
Zou, Xionghui
Gao, Weicheng
Xi, Wei
POLYMER COMPOSITES, 2024, 45 (13) : 12405 - 12420
[36] Buckling of partially-compressed laminated composite plates
Huang, Sixin
Qiao, Pizhong
THIN-WALLED STRUCTURES, 2021, 169 (169)
[37] Buckling and free vibration analysis of shear deformable graphene-reinforced composite laminated plates
Wang, Miao
Xu, Yong-Gang
Qiao, Pizhong
Li, Zhi-Min
COMPOSITE STRUCTURES, 2022, 280
[38] The response of laminated composite plates and profiles under low-velocity impact load
Gliszczynski, A.
Kubiak, T.
Rozylo, P.
Jakubczak, P.
Bienias, J.
COMPOSITE STRUCTURES, 2019, 207 : 1 - 12
[39] Buckling response of rectangular laminated composite plates with cutouts
Baba, Buket Okutan
SCIENCE AND ENGINEERING OF COMPOSITE MATERIALS, 2007, 14 (01) : 17 - 24
[40] Image-enhanced modelling of residual compressive after impact strength in laminated composites
Bull, D. J.
Spearing, S. M.
Sinclair, I.
COMPOSITE STRUCTURES, 2018, 192 : 20 - 27

← 1 2 3 4 5 →