Design and control optimization of composite laminated truncated conical shells for minimum dynamic response including transverse shear deformation

Composite Structures

Volumn 64, Issue 2, 2004, Pages 139-150

  Fares, M E ^a   Youssif, Y G ^a   Alamir, A E ^a  

^a Mansoura University   (Egypt)

Author keywords

Active control; Design optimization; Design variables; Laminated conical shell; Shear deformation theory; Total elastic energy

Indexed keywords

DEFORMATION; DYNAMIC RESPONSE; GEOMETRY; SHELLS (STRUCTURES); STRUCTURAL OPTIMIZATION;

CONICAL SHELLS; LIAPUNOV-BELLMAN THEORY;

LAMINATED COMPOSITES;

DEFORMATION; DESIGN; FIBER ORIENTATION; FIBER REINFORCED COMPOSITE; OPTIMIZATION;

EID: 1542783249     PISSN: 02638223     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0263-8223(03)00222-8     Document Type: Article

References (26)

1. Korjakin A. Rikards R. Chate A. Altenbach H. Analysis of free damped vibrations of laminated composite conical shells Compos. Struct. 41 1998 39-47
2. Tong L. Free vibration of laminated conical shells including transverse shear deformation Int. J. Solids Struct. 31 1994 443-456
3. Tong L. Free vibration of axially loaded laminated conical shells J. Appl. Mech. 66 1999 758-763
4. Sivadas K.R. Vibration analysis of pre-stressed thick circular conical composite shells J. Sound Vib. 186 1 1995 87-97
5. Wu C.P. Lee C.Y. Differential quadrature solution for the free vibration analysis of laminated conical shells with variable stiffness Int. J. Mech. Sci. 43 2001 1853-1869
6. Li H. Influence of boundary conditions on the free vibrations of rotating truncated circular multi-layered conical shells Compos. Part B: Eng. 31 2000 265-275
7. Lim C.W. Kitipornchai S. Effects of subtended and vertex angles on the free vibration of open conical shell panels: a conical shells-ordinate approach J. Sound Vib. 219 5 1999 813-835
8. Hu H.-T. Ou S.-C. Maximization of the fundamental frequencies of laminated truncated conical shells with respect to fiber orientations Compos. Struct. 52 2001 265-275
9. Hu H-T. Ho M.-H. Influence of geometry and end conditions on optimal fundamental natural frequencies of symmetrically laminated plates J. Reinf. Plast. Compos. 15 9 1996 877-893
10. Hu H-T. Juang C.-D. Maximization of the fundamental frequencies of laminated curved panels against fiber orientations J. Aircraft 34 6 1997 792-801
11. Hu H.-T. Tsai C.-Y. Maximization of the fundamental frequencies of laminated cylindrical shells with respect to fiber orientations J. Sound Vib. 225 1999 723-740
12. Adali S. Richter A. Verijenko V.E. Minimum weight design of symmetric angle-ply laminates with incomplete information on initial imperfections J. Appl. Mech. 64 1997 90-96
13. Muc A. Krawiec Z. Design of composite plates under cyclic loading Compos. Struct. 48 2000 139-144
14. Rao S.S. Optimum design of structures under shock and vibration environment Shock Vib. Dig. 21 1989 3-15
15. Turvey G.J. Marshall I.H. Buckling and postbuckling of composite plates 1995 Chapman - Hall
16. O'Donoghue P.E. Atluri S.N. Control of dynamic response of a continuum model of a large space structure Comput. Struct. 23 1986 199-209
17. Yang J.N. Soong T.T. Recent advances in active control of civil engineering structures Probabilist. Eng. Mech. 3 1988 179-188
18. Miller R.K. Masri S.F. Dehganyer T.J. Caughey T.K. Active vibration control of large civil structures ASCE J. Eng. Mech. 114 1988 1542-1570
19. Adali S. Sadek I.S. Sloss J.M. Bruch J.C. Jr Distributed control of layered orthotropic plates with damping Optim. Control Appl. Meth. 9 1988 1-17
20. Fares M.E. Youssif Y.G. Alamir A.E. Optimal design and control of composite laminated plates with various boundary conditions using various plate theories Compos. Struct. 56 2002 1-12
21. Fares M.E. Youssif Y.G. Alamir A.E. Minimization of the dynamic response of composite laminated doubly curved shells using design and control optimization Compos. Struct. 59 3 2003 369-383
22. Youssif Y.G. Fares M.E. Hafiz M.A. Optimal control of the dynamic response of an anisotropic plate with various boundary conditions Mech. Res. Commun. 28 2001 525-534
23. Fares M.E. Youssif Y.G. Hafiz M.A. Optimization control of composite laminates for maximum thermal buckling and minimum vibrational response J. Therm. Stresses 25 11 2002 1047-1064
24. Bruch J.C. Adali S. Sloss J.M. Sadek I.S. Optimal design and control of cross-ply laminate for maximum frequency and minimum dynamic response Comput. Struct. 37 1990 87-94
25. Letov A.M. Analytical design of controllers Aftamateka Telemchanika 21 4-6 1960
26. Gabralyan MS. About stabilization of mechanical systems under continuous forces, vol. 2. YGU, Yervan, 1975, p. 47-56