You do not have permission to edit this page, for the following reason:

You are not allowed to execute the action you have requested.

You can view and copy the source of this page.

​x
 
1
Published in ''Computers and Structures'' Vol. 70 (6), pp. 635-646, 1999<br />
2
doi: 10.1016/S0045-7949(98)00165-5
3
== Abstract ==
4
​
5
The paper presents a new triangle for analysis of laminate plates and shells. The in-plane degrees of freedom are interpolated quadratically whereas a linear layer-wise approximation is chosen for the normal displacement. A substructuring technique is used to eliminate the in-plane degrees of freedom during the assembly process thus reducing substantially the computationed costs. The element performance is evaluated in the static and dynamic analysis of different laminate plate and shell structures.
6
​
7
<pdf>Media:Draft_Samper_991634081_7731_1-s2.0-S0045794998001655-main.pdf</pdf>
8
​

Return to Botello et al 1999b.

Back to Top