Abstract

This paper presents exact solutions for the nonlinear bending problem, the buckling loads, and postbuckling configurations of a perfect and an imperfect bioinspired helicoidal composite beam with a linear rotation angle. The beam is embedded on an elastic medium, which is modeled by two elastic foundation parameters. The nonlinear integro-differential governing equation of the system is derived based on the Euler–Bernoulli beam hypothesis, von Kármán nonlinear strain, and initial curvature. The Laplace transform and its inversion are directly applied to solve the nonlinear integro-differential governing equations. The nonlinear bending deflections under point and uniform loads are derived. Closed-form formulas of critical buckling loads, as well as nonlinear postbuckling responses of perfect and imperfect beams are deduced in detail. The proposed model is validated with previous works. In the numerical results section, the effects of the rotation angle, amplitude of initial imperfection, elastic foundation constants, and boundary conditions on the nonlinear bending, critical buckling loads, and postbuckling configurations are discussed. The proposed model can be utilized in the analysis of bio-inspired beam structures that are used in many energy-absorption applications.

Highlights

  • Due to their exceptional strength and stiffness properties, the usage of laminated composite (LC) structures in engineering applications such as automotive, aerospace, spacecraft, energy harvester, and marine structures has increased intensely [1]

  • The numerical results are presented to clarify the effects of load position, helicoidal rotation angle, amplitude of initial imperfection, and elastic foundation parameters on the nonlinear bending behavior of composite beams

  • In this paper, based on the Laplace transform and its inversion, exact solutions were deduced for nonlinear bending and buckling behaviors of helicoidal composite perfect and imperfect beams embedded in a linear elastic medium

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Summary

Introduction

Due to their exceptional strength and stiffness properties, the usage of laminated composite (LC) structures in engineering applications such as automotive, aerospace, spacecraft, energy harvester, and marine structures has increased intensely [1]. There are many examples of helicoidal structures, such as the osteons in mammalian bones, certain plant cell walls, various insect cuticles, and DNA structure [2,3]. Motivated by these examples, several authors explored the applicability of twisted laminae arrangements rather than the conventional design of laminates [4,5]. Using the finite element (FE) method, Morozov et al [6] studied the buckling of anisotropic grid composite lattice cylindrical shells under different loading conditions.

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