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Browsing Research Publications (Engineering and Built Environment) by Issue Date

Now showing items 21-32 of 32

A method for optimally designing laminated plates subject to fatigue loads for minimum weight using a cumulative damage constraint

Walker, Mark (Elsevierhttp://dx.doi.org/10.1016/S0263-8223(99)00097-5, 2000)

A procedure to optimally design laminated plates for a specific cyclic life using a cumulative damage constraint is described. The objective is minimum weight, and the design variables are the fiber orientation, and the ...
Optimal design of symmetric laminates with cut-outs for maximum buckling load

Walker, Mark (Elsevierhttp://dx.doi.org/10.1016/S0045-7949(98)00167-9, 1999)

Finite element solutions are presented for the optimal design of symmetrically laminated rectangular plates with central circular cut-outs subject to a combination of simply supported, clamped and free boundary conditions. ...
Refined theory of laminated anisotropic shells for the solution of thermal stress problems

Verijenko, Viktor E.; Tauchert, T. R.; Shaikh, C.; Tabakov, Pavel Y. (Taylor & Francishttp://www.tandfonline.com/doi/pdf/10.1080/014957399281066, 1999)

A new higher order theory of laminated anisotropic shells for the solution of thermal stress problems that takes into account transverse shear stresses is developed.The theory is based on the kinematic hypotheses that ...
Multiobjective optimisation of laminated I-beams for maximum crippling, buckling and postbuckling strength

Walker, Mark (Elsevierhttp://dx.doi.org/10.1016/S1359-8368(97)00016-4, 1998)

The present study deals with the optimal design of uniaxially loaded laminated I-beams for a maximum combination of crippling and buckling load, in the first instance, and a maximum combination of buckling load and ...
A procedure to select the best material combinations and optimally design hybrid composite plates for minimum weight and cost

Walker, Mark; Reiss, Talmon; Adali, Sarp (Taylor & Francishttp://www.tandfonline.com/doi/pdf/10.1080/03052159708940987, 1997)

The optimal layup with least weight or cost for a symmetrically laminated plate subject to a buckling load is determined using a hybrid composite construction. A hybrid construction provides further tailoring capabilities ...
Optimal design of symmetrically laminated plates for minimum deflection and weight

Walker, Mark; Reiss, Talmon; Adali, Sarp (Elsevierhttp://dx.doi.org/10.1016/S0263-8223(97)00109-8, 1997)

The minimum deflection and weight designs of laminated composite plates are given. The finite element method using Mindlin plate theory is used in conjunction with optimisation routines in order to obtain the optimal ...
A procedure to select the best material combinations and optimally design hybrid composite plates for minimum weight and cost

Walker, Mark; Reiss, Talmon; Adali, Sarp (Taylor & Francishttp://dx.doi.org/10.1080/03052159708940987, 1997)

The optimal layup with least weight or cost for a symmetrically laminated plate subject to a buckling load is determined using a hybrid composite construction. A hybrid construction provides further tailoring capabilities ...
Optimal design of symmetrically laminated plates for maximum buckling temperature

Walker, Mark; Reiss, Talmon; Adali, Sarp; Verijenko, Viktor E. (Taylor & Francishttp://dx.doi.org/10.1080/01495739708956089, 1997)

The optimal designs of laminated plates subject to nonuniform temperature distributions are givenfor maximum bucklingtemperature. The method ofsolution involves the finite element method based on Mindlin plate theory and ...
Minimum weight design of composite hybrid shells via symbolic computation

Walker, Mark; Reiss, Talmon; Adali, Sarp (Elsevierhttp://dx.doi.org/10.1016/S0016-0032(96)00066-X, 1997)

The best layup for a hybrid laminated cylindrical shell subject to a buckling load constraint is determined. The objective of the optimisation is the minimum weight design of these structures. The ply angle is taken as ...
Multiobjective optimization of laminated plates for maximum prebuckling, buckling and postbuckling strength using continuous and discrete ply angles

Adali, Sarp; Walker, Mark; Verijenko, Viktor E. (Elsevier.http://dx.doi.org/10.1016/0263-8223(96)00030-X, 1996)

The optimal design of uniaxially loaded laminated plates subject to elastic in-plane restraints along the unloaded edges are given for a maximum combination of prebuckling stiffness, postbuckling stiffness and buckling ...
Optimization of symmetric laminates for maximum buckling load including the effects of bending-twisting coupling

Walker, Mark; Adali, Sarp; Verijenko, Viktor E. (Elsevierhttp://dx.doi.org/10.1016/0045-7949(95)00138-7, 1996)

Finite element solutions are presented for the optimal design of symmetrically laminated rectangular plates subjected to a combination of simply supported, clamped and free boundary conditions. The design objective is the ...
Optimal design of symmetric angle-ply laminates subject to nonuniform buckling loads and in-plane restraints

Walker, Mark; Adali, Sarp; Verijenko, Viktor E. (Elsevierhttp://dx.doi.org/10.1016/0263-8231(96)00002-X, 1996)

Optimal buckling designs of symmetrically laminated rectangular plates under in-plane uniaxial loads" which have a nonuniform distribution along the edges are presented. In particular, point loads, partial uniJorm loads ...

Now showing items 21-32 of 32

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