Interlaminar stress analysis of laminated composite beams according to global higher-order deformation theories
暂无分享,去创建一个
[1] Hiroyuki Matsunaga,et al. Vibration and stability of cross-ply laminated composite plates according to a global higher-order plate theory , 2000 .
[2] N. Pagano,et al. Exact Solutions for Composite Laminates in Cylindrical Bending , 1969 .
[3] Hidenori Murakami,et al. Laminated Composite Plate Theory With Improved In-Plane Responses , 1986 .
[4] R. C. Averill,et al. Thick beam theory and finite element model with zig-zag sublaminate approximations , 1996 .
[5] J. N. Reddy,et al. Modelling of thick composites using a layerwise laminate theory , 1993 .
[6] N. Pagano,et al. Exact Solutions for Rectangular Bidirectional Composites and Sandwich Plates , 1970 .
[7] Dahsin Liu,et al. An interlaminar stress continuity theory for laminated composite analysis , 1992 .
[8] Hiroyuki Matsunaga,et al. FREE VIBRATION AND STABILITY OF THIN ELASTIC BEAMS SUBJECTED TO AXIAL FORCES , 1996 .
[9] H. Matsunaga,et al. Buckling instabilities of thick elastic beams subjected to axial stresses , 1996 .
[10] Hiroyuki Matsunaga,et al. Vibration and Buckling of Deep Beam-Columns on Two-Parameter Elastic Foundations , 1999 .
[11] R. C. Averill,et al. C0 zig-zag finite element for analysis of laminated composite beams , 1999 .