<p>This study presents a higher-order zigzag theory (HOZT) for the static bending analysis of laminated composite and sandwich plates under sinusoidally distributed transverse loading. The formulation superimposes higher-order through-thickness displacement polynomials onto the Murakami Zigzag Function (MZF), extending the simplified kinematics of Ali et al. [<CitationRef CitationID="CR29">29</CitationRef>], originally restricted to symmetric cross-ply laminates, to a unified framework for general lamination schemes. Transverse shear stresses are recovered through equilibrium-based integration, and analytical solutions are obtained via Navier’s method for simply supported plates. The present formulation offers three principal advances. First, the higher-order zigzag kinematics are systematically applied, within a single formulation, to symmetric and anti-symmetric cross-ply, symmetric and anti-symmetric angle-ply, arbitrary unsymmetric, and sandwich configurations. Second, compared with Murakami’s zigzag theory (MZT) and the Enhanced Refined Zigzag Theory (Enhanced-RZT), which employ linear zigzag enrichment only, the present higher-order terms provide substantially improved accuracy for thick laminates. For a four-layer anti-symmetric cross-ply plate at <InlineEquation ID="IEq4"> <EquationSource Format="TEX">\(a/h=4\)</EquationSource> <EquationSource Format="MATHML"><math> <mrow> <mi>a</mi> <mo stretchy="false">/</mo> <mi>h</mi> <mo>=</mo> <mn>4</mn> </mrow> </math></EquationSource> </InlineEquation>, errors in the in-plane displacement <InlineEquation ID="IEq5"> <EquationSource Format="TEX">\(u_2\)</EquationSource> <EquationSource Format="MATHML"><math> <msub> <mi>u</mi> <mn>2</mn> </msub> </math></EquationSource> </InlineEquation> are reduced from approximately <InlineEquation ID="IEq6"> <EquationSource Format="TEX">\(61\%\)</EquationSource> <EquationSource Format="MATHML"><math> <mrow> <mn>61</mn> <mo>%</mo> </mrow> </math></EquationSource> </InlineEquation> to below <InlineEquation ID="IEq7"> <EquationSource Format="TEX">\(4.5\%\)</EquationSource> <EquationSource Format="MATHML"><math> <mrow> <mn>4.5</mn> <mo>%</mo> </mrow> </math></EquationSource> </InlineEquation>, while errors in <InlineEquation ID="IEq8"> <EquationSource Format="TEX">\(\sigma _{yy}\)</EquationSource> <EquationSource Format="MATHML"><math> <msub> <mi>σ</mi> <mrow> <mi mathvariant="italic">yy</mi> </mrow> </msub> </math></EquationSource> </InlineEquation> decrease from over <InlineEquation ID="IEq9"> <EquationSource Format="TEX">\(22\%\)</EquationSource> <EquationSource Format="MATHML"><math> <mrow> <mn>22</mn> <mo>%</mo> </mrow> </math></EquationSource> </InlineEquation> to below <InlineEquation ID="IEq10"> <EquationSource Format="TEX">\(1\%\)</EquationSource> <EquationSource Format="MATHML"><math> <mrow> <mn>1</mn> <mo>%</mo> </mrow> </math></EquationSource> </InlineEquation>. Third, the model captures through-thickness displacement asymmetry induced by unsymmetric stacking sequences and surface loading, effects that conventional HSDT and FSDT formulations cannot reproduce. A key limitation is also identified and quantified: Because the MZF depends solely on geometric layer distribution, accuracy deteriorates for highly heterogeneous sandwich plates, with transverse displacement errors reaching approximately <InlineEquation ID="IEq11"> <EquationSource Format="TEX">\(48\%\)</EquationSource> <EquationSource Format="MATHML"><math> <mrow> <mn>48</mn> <mo>%</mo> </mrow> </math></EquationSource> </InlineEquation>. This observation provides motivation for the development of constitutively consistent higher-order zigzag theories. Comprehensive numerical studies across diverse thickness ratios, anisotropy levels, and layer counts confirm the superior predictive capability of the proposed model.</p>

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A \(C^{0}\) higher-order zigzag theory for laminated composites: analytical benchmarking against 3D elasticity solutions

  • Aamir Anwar Nezami,
  • Sunny Akhtar

摘要

This study presents a higher-order zigzag theory (HOZT) for the static bending analysis of laminated composite and sandwich plates under sinusoidally distributed transverse loading. The formulation superimposes higher-order through-thickness displacement polynomials onto the Murakami Zigzag Function (MZF), extending the simplified kinematics of Ali et al. [29], originally restricted to symmetric cross-ply laminates, to a unified framework for general lamination schemes. Transverse shear stresses are recovered through equilibrium-based integration, and analytical solutions are obtained via Navier’s method for simply supported plates. The present formulation offers three principal advances. First, the higher-order zigzag kinematics are systematically applied, within a single formulation, to symmetric and anti-symmetric cross-ply, symmetric and anti-symmetric angle-ply, arbitrary unsymmetric, and sandwich configurations. Second, compared with Murakami’s zigzag theory (MZT) and the Enhanced Refined Zigzag Theory (Enhanced-RZT), which employ linear zigzag enrichment only, the present higher-order terms provide substantially improved accuracy for thick laminates. For a four-layer anti-symmetric cross-ply plate at \(a/h=4\) a / h = 4 , errors in the in-plane displacement \(u_2\) u 2 are reduced from approximately \(61\%\) 61 % to below \(4.5\%\) 4.5 % , while errors in \(\sigma _{yy}\) σ yy decrease from over \(22\%\) 22 % to below \(1\%\) 1 % . Third, the model captures through-thickness displacement asymmetry induced by unsymmetric stacking sequences and surface loading, effects that conventional HSDT and FSDT formulations cannot reproduce. A key limitation is also identified and quantified: Because the MZF depends solely on geometric layer distribution, accuracy deteriorates for highly heterogeneous sandwich plates, with transverse displacement errors reaching approximately \(48\%\) 48 % . This observation provides motivation for the development of constitutively consistent higher-order zigzag theories. Comprehensive numerical studies across diverse thickness ratios, anisotropy levels, and layer counts confirm the superior predictive capability of the proposed model.