Asymmetric flexural vibration and thermoelastic stability of FGM circular plates using finite element method

被引：152
作者：
Prakash, T.
Ganapathi, M. [1 ]
机构：
[1] Inst Armament Technol, FEA Grp, Pune 411025, Maharashtra, India
[2] Indian Inst Technol, Dept Appl Mech, New Delhi 110016, India
来源：
COMPOSITES PART B-ENGINEERING | 2006年 / 37卷 / 7-8期
关键词：
buckling; vibration; thermal properties; finite element analysis (FEA);
D O I：
10.1016/j.compositesb.2006.03.005
中图分类号：
T [工业技术];
学科分类号：
08 ;
摘要：
Here, asymmetric free vibration characteristics and thermoelastic stability of functionally graded circular plates are investigated using finite element procedure. A three-noded shear flexible plate element based on the field-consistency principle is used. Temperature field is assumed to be a uniform distribution over the plate surface and varied in thickness direction only. Material properties are graded in the thickness direction according to simple power law distribution. For the numerical illustrations, aluminum/alumina is considered as functionally graded material. The variation in critical buckling load is highlighted considering gradient index, temperature, radius-to-thickness ratios, circumferential wave number and boundary condition of the plate. (c) 2006 Elsevier Ltd. All rights reserved.
引用
收藏
页码：642 / 649
页数：8
相关论文
共 28 条
[1]   RESPONSE OF FUNCTIONALLY GRADED COMPOSITES TO THERMAL-GRADIENTS [J].
ABOUDI, J ;
ARNOLD, SM ;
PINDERA, MJ .
COMPOSITES ENGINEERING, 1994, 4 (01) :1-18
[2]  
Balakrishna C., 1989, J AERONAUT SOC INDIA, V41, P89
[3]   Modeling of functionally graded materials in dynamic analyses [J].
Banks-Sills, L ;
Eliasi, R ;
Berlin, Y .
COMPOSITES PART B-ENGINEERING, 2002, 33 (01) :7-15
[4]  
Birman V., 1995, P 10 C ENG MECH, V2, P1199
[5]   Three-dimensional thermoelastic deformations of a functionally graded elliptic plate [J].
Cheng, ZQ ;
Batra, RC .
COMPOSITES PART B-ENGINEERING, 2000, 31 (02) :97-106
[6]   Buckling analysis of functionally graded plates subjected to uniaxial loading [J].
Feldman, E ;
Aboudi, J .
COMPOSITE STRUCTURES, 1997, 38 (1-4) :29-36
[7]   Supersonic flutter analysis of thermally stressed laminated composite flat panels [J].
Ganapathi, M ;
Touratier, M .
COMPOSITE STRUCTURES, 1996, 34 (02) :241-248
[8]   Active control of FGM plates with integrated piezoelectric sensors and actuators [J].
He, XQ ;
Ng, TY ;
Sivashanker, S ;
Liew, KM .
INTERNATIONAL JOURNAL OF SOLIDS AND STRUCTURES, 2001, 38 (09) :1641-1655
[9]   Thermal buckling of functionally graded plates [J].
Javaheri, R ;
Eslami, MR .
AIAA JOURNAL, 2002, 40 (01) :162-169
[10]   FGM activities in Japan [J].
Koizumi, M .
COMPOSITES PART B-ENGINEERING, 1997, 28 (1-2) :1-4
123