Layup optimization of symmetrically laminated thick plates for fundamental frequencies using lamination parameters

被引:46
作者
Diaconu, CG
Sato, M
Sekine, H
机构
[1] Tohoku Univ, Dept Aeronaut & Space Engn, Aoba Ku, Sendai, Miyagi 9808579, Japan
[2] Natl Aerosp Lab Japan, Kakuda Space Prop Lab, Kimigaya, Kakuda 9811525, Japan
关键词
lamination parameter; layup optimization; laminated thick plate; first-order shear deformation theory; fundamental frequency;
D O I
10.1007/s00158-002-0241-z
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
This paper examines the optimum laminate configurations for maximizing the fundamental frequencies of symmetrically laminated thick plates. The transverse shear effect is taken into consideration in the free vibration analysis of symmetrically laminated thick plates on the basis of the first-order shear deformation theory. Layup optimization is performed by introducing four out-of-plane and two in-plane lamination parameters that characterize the out-of-plane and the transverse shear stiffnesses, respectively. A variational approach is applied to find the boundary of the feasible region in the design space of the six lamination parameters. Using the information of the boundary of the feasible region, the optimum lamination parameters that give the maximum fundamental frequency are obtained for the cases of simply supported and clamped boundary conditions. The laminate configurations intended to realize the optimum lamination parameters are also obtained by using a mathematical programming method. The transverse shear effect on the optimum results is discussed in comparison with the optimum results obtained for classical laminated plate theory.
引用
收藏
页码:302 / 311
页数:10
相关论文
共 19 条
[1]   Optimization of shear-deformable laminated plates under buckling and strength criteria [J].
Adali, S ;
Richter, A ;
Verijenko, VE .
COMPOSITE STRUCTURES, 1997, 39 (3-4) :167-178
[2]   DESIGN OF LAMINATED COMPOSITE PLATES FOR MAXIMUM SHEAR BUCKLING LOADS [J].
CHANG, RR ;
CHU, KH ;
KAM, TY .
JOURNAL OF ENERGY RESOURCES TECHNOLOGY-TRANSACTIONS OF THE ASME, 1993, 115 (04) :314-322
[3]   Feasible region in general design space of lamination parameters for laminated composites [J].
Diaconu, CG ;
Sato, M ;
Sekine, H .
AIAA JOURNAL, 2002, 40 (03) :559-565
[4]   A general approach forcing convexity of ply angle optimization in composite laminates [J].
Foldager, J ;
Hansen, JS ;
Olhoff, N .
STRUCTURAL OPTIMIZATION, 1998, 16 (2-3) :201-211
[5]   STIFFNESS DESIGN METHOD OF SYMMETRICAL LAMINATES USING LAMINATION PARAMETERS [J].
FUKUNAGA, H ;
SEKINE, H .
AIAA JOURNAL, 1992, 30 (11) :2791-2793
[6]   OPTIMAL-DESIGN OF SYMMETRICAL LAMINATED PLATES FOR FUNDAMENTAL-FREQUENCY [J].
FUKUNAGA, H ;
SEKINE, H ;
SATO, M .
JOURNAL OF SOUND AND VIBRATION, 1994, 171 (02) :219-229
[7]   LAYUP OPTIMIZATION AGAINST BUCKLING OF SHEAR PANELS [J].
GRENESTEDT, JL .
STRUCTURAL OPTIMIZATION, 1991, 3 (02) :115-120
[8]  
GRENESTEDT JL, 1994, AIAA J, V32, P415
[9]  
Grenestedt JL., 1993, OPT DES ADV MAT, P311
[10]   DESIGN OF LAMINATED COMPOSITE PLATES FOR OPTIMAL DYNAMIC CHARACTERISTICS USING A CONSTRAINED GLOBAL OPTIMIZATION TECHNIQUE [J].
KAM, TY ;
LAI, FM .
COMPUTER METHODS IN APPLIED MECHANICS AND ENGINEERING, 1995, 120 (3-4) :389-402