On the use of different diametral compression cracked disc shape specimens for introducing mode III deformation

Author(s):  
Mohammad Reza Mohammad Aliha ◽  
Hadi Ghesmati Kucheki ◽  
Mohammad Mahdi Asadi
2020 ◽  
Vol 2020 (10) ◽  
pp. 1177-1181
Author(s):  
A. V. Kabanova ◽  
D. V. Zaitsev ◽  
S. S. Grigor’ev ◽  
P. E. Panfilov

2012 ◽  
Vol 72 (11) ◽  
pp. 1283-1290 ◽  
Author(s):  
N.K. Kar ◽  
Y. Hu ◽  
B. Ahn ◽  
S.R. Nutt

2016 ◽  
Vol 22 (3) ◽  
pp. 259-282 ◽  
Author(s):  
András Szekrényes

The second-order laminated plate theory is utilized in this work to analyze orthotropic composite plates with asymmetric delamination. First, a displacement field satisfying the system of exact kinematic conditions is presented by developing a double-plate system in the uncracked plate portion. The basic equations of linear elasticity and Hamilton’s principle are utilized to derive the system of equilibrium and governing equations. As an example, a delaminated simply supported plate is analyzed using Lévy plate formulation and the state-space model by varying the position of the delamination along the plate thickness. The displacements, strains, stresses and the J-integral are calculated by the plate theory solution and compared with those by linear finite-element calculations. The comparison of the numerical and analytical results shows that the second-order plate theory captures very well the mechanical fields. However, if the delamination is separated by only a relatively thin layer from the plate boundary surface, then the second-order plate theory approximates badly the stress resultants and so the mode-II and mode-III J-integrals and thus leads to erroneous results.


Sign in / Sign up

Export Citation Format

Share Document