Dynamic response with mass variation of laminated composite twisted plates

被引：10

作者：

Anish ^{[1
]}

Gupta, Kamal Kumar ^{[1
]}

Kumar, Ajay ^{[1
]}

Barnat-Hunek, Danuta ^{[2
]}

Andrzejuk, Wojciech ^{[3
]}

机构：

[1] Natl Inst Technol Patna, Dept Civil Engn, Patna 800005, Bihar, India

[2] Lublin Univ Technol, Dept Construct, 40 Nadbystrzycka, PL-20618 Lublin, Poland

[3] Pope John Paul II State Sch Higher Educ Biala Pod, 95-97 Sidorska, PL-21500 Biala Podlaska, Poland

来源：

JOURNAL OF MECHANICAL SCIENCE AND TECHNOLOGY | 2018年 / 32卷 / 09期

关键词：

Additional mass; Cutout; Free vibration; Plates; Mode shape; DEPENDENT FREE-VIBRATION; SHEAR DEFORMATION; NANOPLATE; SHELLS; LAYERS;

D O I：

10.1007/s12206-018-0812-6

中图分类号：

TH [机械、仪表工业];

学科分类号：

0802 ;

摘要：

In this study, the dynamic response of free vibration of laminated composite twisted (skewed) plate with mass variation via cutout and additional mass is investigated. The mathematical model employs cubic variation of the thickness coordinates in the displacement field. The mathematical formulation also includes the effects of transverse shear and rotatory inertia. A realistic parabolic distribution of transverse shear strains through the plate thickness is assumed and the use of the shear correction factor is avoided. A C-0 finite element formulation of the mathematical model is developed to analyze the dynamic behavior of laminated composite twisted plate with cutout and additional mass. Given that no results on the present problem of free vibration of laminated composite twisted plate with cutout and additional mass are available in literature, novel results for different twist angles of laminated composite plates along with mode shapes are presented by varying the geometry, boundary conditions, and ply orientations.

引用

页码：4145 / 4152

页数：8

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