Analysis of laminated shells with laminated stiffeners using rectangular shell finite elementsstar


Autoria(s): Venkatesh, A; Rao, KP
Data(s)

01/07/1983

Resumo

A finite element analysis of laminated shells reinforced with laminated stiffeners is described in this paper. A rectangular laminated anisotropic shallow thin shell finite element of 48 d.o.f. is used in conjunction with a laminated anisotropic curved beam and shell stiffening finite element having 16 d.o.f. Compatibility between the shell and the stiffener is maintained all along their junction line. Some problems of symmetrically stiffened isotropic plates and shells have been solved to evaluate the performance of the present method. Behaviour of an eccentrically stiffened laminated cantilever cylindrical shell has been predicted to show the ability of the present program. General shells amenable to rectangular meshes can also be solved in a similar manner.

Formato

application/pdf

Identificador

http://eprints.iisc.ernet.in/21391/1/m1.pdf

Venkatesh, A and Rao, KP (1983) Analysis of laminated shells with laminated stiffeners using rectangular shell finite elementsstar. In: Computer Methods in Applied Mechanics and Engineering, 38 (3). pp. 255-272.

Publicador

Elsevier Science

Relação

http://www.sciencedirect.com/science?_ob=MImg&_imagekey=B6V29-47XF9BB-DH-1&_cdi=5697&_user=512776&_orig=browse&_coverDate=07%2F31%2F1983&_sk=999619996&view=c&wchp=dGLbVlW-zSkzV&md5=d743298f93fb504395226f9ff076b552&ie=/sdarticle.pdf

http://eprints.iisc.ernet.in/21391/

Palavras-Chave #Aerospace Engineering (Formerly, Aeronautical Engineering)
Tipo

Journal Article

PeerReviewed