Semi-analytical dynamic modeling and impact mechanism analysis of a hard-coating cylindrical shell with arbitrary circular perforations.

ABSTRACT: In this paper, an innovative axial domain decomposition method, which uniquely integrates axial and circumferential perforation parameters, is developed for semi-analytical modeling of free vibration of a hard-coating cylindrical shell with arbitrary axial and circumferential perforations, based on the Love's first-order shear deformation theory and Rayleigh-Ritz method. The concept of this method is to decompose the shell into two types of domains at the upper and lower axial boundaries of the circular perforations. The generalized semi-analytical formulas of the perforated composite shell can be derived by assembling the separated energy expressions of each domain. Moreover, the result analysis find that the intrinsic influence mechanism of the circumferential perforation number on vibra

SUBMITTER: Yang J 

PROVIDER: S-EPMC11889161 | biostudies-literature | 2025 Mar

REPOSITORIES: biostudies-literature