Numerical modeling of nonlinear deformation and buckling of composite plate-shell structures under pulsed loading

1999 ◽  
Vol 35 (6) ◽  
pp. 495-506 ◽  
Author(s):  
N. A. Abrosimov
Author(s):  
Kasmidi Gunaryo ◽  
Heri Heriana ◽  
M. Rafiqi Sitompul ◽  
Andi Kuswoyo ◽  
Bambang K. Hadi

2021 ◽  
Vol 264 ◽  
pp. 02018
Author(s):  
Rustam Khalmuradov ◽  
Utkir Nishonov

The stress-strain state of a circular disc, discretely finned in a circle, under the influence of the pulse loading, is numerically investigated. Thus the geometric nonlinearity between displacement and deformation is taken into account. The structure consists of boarding and reinforced ribs, the materials of which are the same and obey Hooke's law. The sections of the ribs are constant. The height of the ribs and their locations are specified using a unit function. It is considered that the plate is deformed under the influence of the pulsed loading. A numerical method is used to solve the problem.


2019 ◽  
Vol 17 (06) ◽  
pp. 1950020
Author(s):  
Hoang Lan Ton-That ◽  
Hieu Nguyen-Van ◽  
Thanh Chau-Dinh

This paper deals with numerical linear analyses of laminated composite plate/shell structures. The method is based on a four-node quadrilateral element, namely, SQ4T, within the framework of the first-order shear deformation theory (FSDT). This element is established by incorporating the twice interpolation strategy (TIS) into a traditional four-node finite element to build the membrane, bending and shear stiffness matrices. Many desirable characteristics of this efficient numerical method are shown as continuous nodal gradients, higher-order polynomial basis, no increase in number of the degree of freedom of the system. The performance of the proposed element is validated and demonstrated through several numerical benchmark problems. Convergence studies and comparison with other existing solutions in the literature suggest that the present element is efficient, accurate and free of lockings.


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