Abstract

Non-prismatic beams are widely employed in several engineering fields, e.g., wind turbines, rotor blades, aircraft wings, and arched bridges. While analytical solutions for variable cross-section beams are desirable, a model describing all stress components for beams with general variation of their cross-section under generalised loading remains an open and important problem to solve. To partly address this issue, we propose an analytical solution for stress recovery of untwisted, asymmetric, non-prismatic beams with smooth and continuous taper shape under general loading, considering plane stress conditions for isotropic materials undergoing small strains. The methodology follows Jourawski’s formulation, including the effect of asymmetric variable cross-section, with internal forces as known variables. We confirm the non-triviality of the stress field of non-prismatic beams, i.e., the dependency on all internal forces and beam geometry to shear and transverse stress distributions. As a particular novelty, the new formulation for transverse direct stress includes internal forces derivatives, resulting in greater accuracy than state-of-the-art models for distributed loading conditions. Also, closed-form solutions are introduced for non-prismatic and linearly tapered, generally asymmetric beams, both with rectangular cross-sections. For validation purposes, we consider three different practical beam models: a symmetric and an asymmetric, both linearly tapered, and an arched beam. The results, checked against commercial finite element analysis, show that the proposed model predicts the stress-field of non-prismatic beams under distributed loads with good levels of accuracy. Traction-free boundary condition requirements are naturally satisfied on the beam surfaces.

Highlights

  • Non-prismatic beams belong to a specific category of slender structures, widely employed as primary structural elements in numerous applications, including wind turbine blades, aircraft wings, helicopter rotor blades, and arches used in bridges

  • The development of an efficient analytical formulation accounting for general taper shapes and arbitrary loading is essential for exploiting the full potential of non-prismatic beams

  • Mercuri et al (2020) proposed a formulation that accounts for transverse direct stresses, but ignores essential terms related to the derivatives of the internal forces, leading to an inconsistent recovery of the Cauchy-stress stress field for distributed load cases

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Summary

Introduction

Non-prismatic beams belong to a specific category of slender structures, widely employed as primary structural elements in numerous applications, including wind turbine blades, aircraft wings, helicopter rotor blades, and arches used in bridges. Mercuri et al (2020) proposed a formulation that accounts for transverse direct stresses, but ignores essential terms related to the derivatives of the internal forces, leading to an inconsistent recovery of the Cauchy-stress stress field for distributed load cases All these restrictions in the state-of-the-art literature are addressed and remedied in the current work. We introduce an analytical solution to recover the stress distribution for untwisted, generally asymmetric, non-prismatic beams tapered in the height direction It is assumed the internal forces are known variables, as determined for example, but not necessarily by, statically determinate beam models, noting that the current methodology is indifferent to the method that evaluates internal forces.

Equilibrium equations
Stress distribution
Extended shear stress
Transverse direct stress
Closed-form solutions
Non-prismatic beams with rectangular cross-section
Linearly tapered beams
Numerical examples
Linearly asymmetric tapered beam
Arched beam
Linearly symmetric tapered beam
Conclusion
Full Text
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