First-order zig-zag sublaminate plate theory and finite element model for laminated composite and sandwich panels
By Y. Cho, R. Averill. 2000
106 citations recorded by the source corpus.
Subfields: Civil and Structural Engineering, Mechanical Engineering, Mechanics of Materials
View Paper: https://www.semanticscholar.org/paper/1bbf61b8f4628b8be0bdf3bb2d889cd4a764968f
How researchers see this paper
The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.
In Civil and Structural Engineering
- Erasmo Carrera
- Alfonso Pagani
- Wenbin Yu
- S. Valvano
- Marco Petrolo
- Dewey H. Hodges
- Vitali Volovoi
- Enrico Zappino
In Mechanical Engineering
In Mechanics of Materials
- Erasmo Carrera
- Alfonso Pagani
- Wenbin Yu
- Marco Petrolo
- S. Valvano
- Dewey H. Hodges
- Enrico Zappino
- Vitali Volovoi
Citations in the corpus
- Asymptotically accurate 3-D recovery from Reissner-like composite plate finite elements (2003, background): “Most of the models that have appeared in the literature [4–7] are based on ad hoc kinematic assumptions that cannot be reasonably justified for composite structures, such as an a priori distribution of displacement through the thickness.”
- Analysis of laminated composites and sandwich structures by variable-kinematic MITC9 plate elements (2018, background): “Dozens of finite elements have been proposed based on zig-zag theories [13, 14, 15, 16].”
- Asymptotic generalization of Reissner–Mindlin theory: accurate three-dimensional recovery for composite shells (2002, background): “Most of the models that have appeared in the literature [3,10,13,19] are based on ad hoc kinematic assumptions that cannot be reasonably justified for composite structures, such as an a priori distribution of displacement through the thickness.”
- Asymptotic construction of Reissner-like composite plate theory with accurate strain recovery (2002, methodology): “Most of the models that have appeared in the literature, for example Reddy (1984); Touratier (1991); DiSciuva (1985) and Cho and Averill (2000), are based on ad hoc kinematic assumptions that cannot be reasonably justified for composite structures, such as an a priori distribution of displacement…”
- Asymptotic Approach for Thermoelastic Analysis of Laminated Composite Plates (2004, background): “For example, most high order theories (except for some layerwise theories such as Cho and Averill (2000)) assume a C continuity for the 3-D displacement field through the thickness which in reality they are piecewise continuous.”