Buckling of metal-reinforced thermoplastic composite laminated plates with holes

被引：6

作者：

Yapici, A ^{[1
]}

Sahin, ÖS ^{[1
]}

Arikan, H ^{[1
]}

机构：

[1] Selcuk Univ, Dept Mech Engn, Konya, Turkey

来源：

JOURNAL OF REINFORCED PLASTICS AND COMPOSITES | 2005年 / 24卷 / 13期

关键词：

buckling behavior; finite elements; thermoplastic; laminated plates;

D O I：

10.1177/0731684405049885

中图分类号：

TB33 [复合材料];

学科分类号：

摘要：

In this study, mechanical buckling behaviors of composite square plates of four symmetric and antisymmetric layers with holes are examined. A thermoplastic material is used as the matrix material. Two different reinforced materials are used, of which one is a galvanized steel wire and the other a woven galvanized wire. The hole type is taken as circular. The finite element method is used for the solution. First critical buckling loads of an orthotropic plate with and without hole subjected to unidirectional compression are found. The results are illustrated in figures.

引用

页码：1379 / 1386

页数：8

共 16 条

[1]

[Anonymous], 1995, BUCKLING POSTBUCKLIN

[2]

Argyris J., 1997, APPL MECH REV, V50, P285, DOI [10.1115/1.3101708, DOI 10.1115/1.3101708]

[3]

Bathe K, 2000, FINITE ELEMENT METHO

[4]

BEDNARCZYK H, 1987, COMPOS STRUCT, V4, P1424

[5]

BERGMANN HW, 1985, J THERMAL STRESSES, V8, P71

[6] Thermal budding of shear-deformable composite laminated plates by the spline finite strip method [J].

Dawe, DJ ;

Ge, YS .

COMPUTER METHODS IN APPLIED MECHANICS AND ENGINEERING, 2000, 185 (2-4) :347-366

[7]

Noor A.K., 1992, Appl. Mech. Rev, V45, P419, DOI [10.1115/1.3119742, DOI 10.1115/1.3119742]

[8]

Ram KSS, 2002, COMPOS STRUCT, V55, P157, DOI 10.1016/S0263-8223(01)00143-X

[9]

SCHLACK AL, 1964, P SOC EXPTL STRESS A, V21, P167

[10] Global buckling behaviour and local damage propagation in composite plates with embedded delaminations [J].

Tafreshi, A ;

Oswald, T .

INTERNATIONAL JOURNAL OF PRESSURE VESSELS AND PIPING, 2003, 80 (01) :9-20

← 1 2 →