A new zig-zag model for laminated composite beams: free vibration analysis

被引:15
作者
Arya, H [1 ]
机构
[1] Indian Inst Technol, Dept Aerosp Engn, Ctr Aerosp Syst Design & Engn, Bombay 400076, Maharashtra, India
关键词
D O I
10.1016/S0022-460X(02)01489-X
中图分类号
O42 [声学];
学科分类号
070206 ; 082403 ;
摘要
引用
收藏
页码:485 / 490
页数:6
相关论文
共 9 条
[1]   A zigzag model for laminated composite beams [J].
Arya, H ;
Shimpi, RP ;
Naik, NK .
COMPOSITE STRUCTURES, 2002, 56 (01) :21-24
[2]   VIBRATION AND STABILITY OF LAMINATED PLATES BASED ON A MODIFIED PLATE-THEORY [J].
DOONG, JL ;
LEE, C ;
FUNG, CP .
JOURNAL OF SOUND AND VIBRATION, 1991, 151 (02) :193-201
[3]   BIDIRECTIONAL BENDING OF LAMINATED COMPOSITE PLATES USING AN IMPROVED ZIGZAG MODEL [J].
LEE, KH ;
LIN, WZ ;
CHOW, ST .
COMPOSITE STRUCTURES, 1994, 28 (03) :283-294
[4]   ZIGZAG THEORY FOR COMPOSITE LAMINATES [J].
LI, XY ;
LIU, DS .
AIAA JOURNAL, 1995, 33 (06) :1163-1165
[5]   HIGH-ORDER THEORY OF PLATE DEFORMATION .1. HOMOGENEOUS PLATES [J].
LO, KH ;
CHRISTENSEN, RM ;
WU, EM .
JOURNAL OF APPLIED MECHANICS-TRANSACTIONS OF THE ASME, 1977, 44 (04) :663-668
[6]   HIGH-ORDER THEORY OF PLATE DEFORMATION .2. LAMINATED PLATES [J].
LO, KH ;
CHRISTENSEN, RM ;
WU, EM .
JOURNAL OF APPLIED MECHANICS-TRANSACTIONS OF THE ASME, 1977, 44 (04) :669-676
[7]  
Rao MK, 2001, COMPOS STRUCT, V52, P149, DOI 10.1016/S0263-8223(00)00162-8
[8]   A SIMPLE HIGHER-ORDER THEORY FOR LAMINATED COMPOSITE PLATES [J].
REDDY, JN .
JOURNAL OF APPLIED MECHANICS-TRANSACTIONS OF THE ASME, 1984, 51 (04) :745-752
[9]   NONLINEAR-THEORY FOR PLATES AND SHELLS INCLUDING THE EFFECTS OF TRANSVERSE SHEARING [J].
STEIN, M .
AIAA JOURNAL, 1986, 24 (09) :1537-1544