The results of a series of numerical experiments are presented to verify some of the important developments made in the first part of this paper. Firstly, the static solution of an algebraic system obtained through Strong Formulation Finite Element Method (SFEM) is presented. Secondly, the stress and strain recovery procedure is descripted for the present technique. It will be clear that the present approach is suitable for any strong formulation finite element methodology, due to the presented general approach based on the unknown displacements and on the elasticity equations. Thirdly, the numerical solutions for some classical and other numerical results found in literature are exposed. Finally, an arbitrarily shaped composite plate is solved and good agreement is observed for all the presented cases.
Nicholas Fantuzzi, Francesco Tornabene (2014). Strong Formulation Finite Element Method for Arbitrarily Shaped Laminated Plates – II. Numerical Analysis. ADVANCES IN AIRCRAFT AND SPACECRAFT SCIENCE, 1(2), 145-175 [10.12989/aas.2014.1.2.145].
Strong Formulation Finite Element Method for Arbitrarily Shaped Laminated Plates – II. Numerical Analysis
FANTUZZI, NICHOLAS;TORNABENE, FRANCESCO
2014
Abstract
The results of a series of numerical experiments are presented to verify some of the important developments made in the first part of this paper. Firstly, the static solution of an algebraic system obtained through Strong Formulation Finite Element Method (SFEM) is presented. Secondly, the stress and strain recovery procedure is descripted for the present technique. It will be clear that the present approach is suitable for any strong formulation finite element methodology, due to the presented general approach based on the unknown displacements and on the elasticity equations. Thirdly, the numerical solutions for some classical and other numerical results found in literature are exposed. Finally, an arbitrarily shaped composite plate is solved and good agreement is observed for all the presented cases.I documenti in IRIS sono protetti da copyright e tutti i diritti sono riservati, salvo diversa indicazione.