Substitution approach for decoupled two-scale analysis of materially nonlinear composite plates. (15th October 2021)

• Record Type: Journal Article
• Authors: Sato, Masami; Muramatsu, Mayu; Nishi, Shinnosuke; Kawada, Tatsuya; Terada, Kenjiro
• Is Part Of: Computers & structures. Volume 255(2021)
• Publication Date: 2021-10-15
• Subjects: Composite plate -- Numerical plate testing -- Muti-scale analysis -- Substitution model -- Laminated structure; Structural engineering -- Data processing -- Periodicals; Electronic data processing -- Structures, Theory of -- Periodicals; 624.171
• DOI: 10.1016/j.compstruc.2021.106623
• Languages: English
• ISSNs: 0045-7949

Abstract

Highlights: A new substitution approach for nonlinear composite plates has been proposed. Composite plates are supposed to have in-plane periodic mesoscopic structures. An equivalent laminated plate substitutes for an original composite plate. The method of numerical plate testing is effectively utilized for homogenization. The proposed approach well expresses the equivalent nonlinear macroscopic behavior. Abstract: A new substitution approach is proposed for decoupled two-scale analysis of a materially nonlinear composite plate with in-plane periodic meso-structures within the framework of computational homogenization. The macroscopic nonlinear mechanical behavior of the plate is characterized by numerical plate tests on an in-plane unit structure (IPUS), which enables us to obtain the relationship between macroscopic resultant stresses and generalized strains. Then, we postulate that the original composite plate can be substituted by an equivalent laminated plate that exhibits approximately the same macroscopic response. The material parameters of each lamina of this substitute, which is referred to as mesoscopic substitution model (meso-SM), are identified using an optimization method so that it could be equivalent to the original IPUS. After the parameter identification, the corresponding macroscopic substitution model (macro-SM) can be analyzed with appropriate analysis software that supports laminated plate elements. Representative numerical examples are presented to validate the appropriateness of the proposed approach by performing comparative calculations with the results obtained from the original composite plates.