Static and dynamic response analysis of functionally graded material plates with damage

被引：19

作者：

Li, D. H. ^{[1
]}

Yang, X. ^{[2
]}

Qian, R. L. ^{[2
]}

Xu, D. ^{[2
]}

机构：

[1] Civil Aviat Univ China, Tianjin Key Lab Civil Aircraft Airworthiness & Ma, Tianjin 300300, Peoples R China

[2] Civil Aviat Univ China, Coll Aeronaut Engn, Tianjin, Peoples R China

来源：

MECHANICS OF ADVANCED MATERIALS AND STRUCTURES | 2020年 / 27卷 / 02期

关键词：

Functionally graded materials; static response; free vibration; transient analysis; extended layerwise method; EXTENDED LAYERWISE METHOD; THERMAL BARRIER COATINGS; LAMINATED COMPOSITE PLATES; CRACK GROWTH SIMULATIONS; SHEAR DEFORMATION-THEORY; VIBRATION ANALYSIS; MULTIPLE DELAMINATIONS; MIXED DESCRIPTION; PROPAGATION; STRESS;

D O I：

10.1080/15376494.2018.1459974

中图分类号：

T [工业技术];

学科分类号：

08 ;

摘要：

The typical damage pattern of functionally graded materials (FGM) is a complex three-dimensional crack with delamination and transverse cracks. The extended layerwise method (XLWM) is applied to the static, free vibration and transient response of FGM plates with typical damage pattern in this paper. In the XLWM of FGM plates, the multiple delaminations and transverse cracks are simulated by displacement assumption in thickness direction and in-plane displacement discretization of extended finite element methods (XFEM), respectively. Numerical examples are provided to validate the proposed method, and the results are compared with these of existing methods and 3D elastic models.

引用

页码：94 / 107

页数：14

共 56 条

[1] Finite element simulation of interface cracks in thermal barrier coatings [J].

Baeker, Martin .

COMPUTATIONAL MATERIALS SCIENCE, 2012, 64 :79-83

[2] ON THE ACCURACY OF INTERLAMINAR STRESS CALCULATION IN LAMINATED PLATES [J].

BARYOSEPH, P .

COMPUTER METHODS IN APPLIED MECHANICS AND ENGINEERING, 1983, 36 (03) :309-329

[3] CALCULATION OF INTERLAMINAR STRESS-CONCENTRATION IN COMPOSITE LAMINATES [J].

BARYOSEPH, P ;

PIAN, THH .

JOURNAL OF COMPOSITE MATERIALS, 1981, 15 (MAY) :225-239

[4] XFEM fracture analysis of orthotropic functionally graded materials [J].

Bayesteh, Hamid ;

Mohammadi, Soheil .

COMPOSITES PART B-ENGINEERING, 2013, 44 (01) :8-25

[5] An embedded crack in a functionally graded orthotropic coating bonded to a homogeneous substrate under a frictional Hertzian contact [J].

Ben-Romdhane, Mohamed ;

El-Borgi, Sami ;

Charfeddine, Malek .

INTERNATIONAL JOURNAL OF SOLIDS AND STRUCTURES, 2013, 50 (24) :3898-3910

[6] A NEW APPROACH TO THE APPLICATION OF MORI-TANAKA THEORY IN COMPOSITE-MATERIALS [J].

BENVENISTE, Y .

MECHANICS OF MATERIALS, 1987, 6 (02) :147-157

[7] Fatigue crack growth simulations of interfacial cracks in bi-layered FGMs using XFEM [J].

Bhattacharya, S. ;

Singh, I. V. ;

Mishra, B. K. ;

Bui, T. Q. .

COMPUTATIONAL MECHANICS, 2013, 52 (04) :799-814

[8] Mixed-mode fatigue crack growth analysis of functionally graded materials by XFEM [J].

Bhattacharya, S. ;

Singh, I. V. ;

Mishra, B. K. .

INTERNATIONAL JOURNAL OF FRACTURE, 2013, 183 (01) :81-97

[9] Fatigue Crack Growth Simulations of FGM Plate under Cyclic Thermal Load by XFEM [J].

Bhattacharya, Somnath ;

Sharma, Kamal .

STRUCTURAL INTEGRITY, 2014, 86 :727-731

[10] Evaluation of layerwise mixed theories for laminated plates analysis [J].

Carrera, E .

AIAA JOURNAL, 1998, 36 (05) :830-839

← 1 2 3 4 5 6 →