<p>This study addresses the unclear mechanisms of shear deformation effects and the contradictory design thresholds in the buckling analysis of pultruded GFRP (glass fiber-reinforced polymer) compression members. By integrating test data from 322 specimens across 17 studies, a large-sample experimental database was established. The Engesser and Haringx shear correction theories were systematically validated, with results indicating that the Engesser model provides the optimal prediction accuracy (<i>R</i><sup>2</sup> = 0.89). Shear deformation can reduce the buckling load by up to 48%. Theoretical derivation revealed the decomposition law of the core parameter: <InlineEquation ID="IEq1"> <EquationSource Format="TEX">\(P_{{\text{E}}} /\left( {{\text{KGA}}} \right) = \left( {\pi^{2} /K} \right) \cdot \left( {E/G} \right) \cdot \lambda^{ - 2} ,\)</EquationSource> <EquationSource Format="MATHML"><math> <mrow> <msub> <mi>P</mi> <mtext>E</mtext> </msub> <mo stretchy="false">/</mo> <mfenced close=")" open="("> <mtext>KGA</mtext> </mfenced> <mo>=</mo> <mfenced close=")" open="("> <mrow> <msup> <mi>π</mi> <mn>2</mn> </msup> <mo stretchy="false">/</mo> <mi>K</mi> </mrow> </mfenced> <mo>·</mo> <mfenced close=")" open="("> <mrow> <mi>E</mi> <mo stretchy="false">/</mo> <mi>G</mi> </mrow> </mfenced> <mo>·</mo> <msup> <mi>λ</mi> <mrow> <mo>-</mo> <mn>2</mn> </mrow> </msup> <mo>,</mo> </mrow> </math></EquationSource> </InlineEquation> which for the first time clearly identifies the slenderness ratio (<InlineEquation ID="IEq2"> <EquationSource Format="TEX">\(\lambda\)</EquationSource> <EquationSource Format="MATHML"><math> <mi>λ</mi> </math></EquationSource> </InlineEquation>) as the dominant geometric factor controlling the shear effect, while the elastic modulus ratio (<InlineEquation ID="IEq3"> <EquationSource Format="TEX">\(E/G\)</EquationSource> <EquationSource Format="MATHML"><math> <mrow> <mi>E</mi> <mo stretchy="false">/</mo> <mi>G</mi> </mrow> </math></EquationSource> </InlineEquation>) is a secondary material factor. Based on this mechanism, a practical design criterion with a threshold of <InlineEquation ID="IEq4"> <EquationSource Format="TEX">\(\lambda =86.6\)</EquationSource> <EquationSource Format="MATHML"><math> <mrow> <mi>λ</mi> <mo>=</mo> <mn>86.6</mn> </mrow> </math></EquationSource> </InlineEquation> is proposed: The Engesser formula must be used for shear correction when <InlineEquation ID="IEq5"> <EquationSource Format="TEX">\(\lambda \le 86.6,\)</EquationSource> <EquationSource Format="MATHML"><math> <mrow> <mi>λ</mi> <mo>≤</mo> <mn>86.6</mn> <mo>,</mo> </mrow> </math></EquationSource> </InlineEquation> whereas the shear effect becomes negligible (&lt; 5%) when <InlineEquation ID="IEq6"> <EquationSource Format="TEX">\(\lambda &gt;86.6\)</EquationSource> <EquationSource Format="MATHML"><math> <mrow> <mi>λ</mi> <mo>&gt;</mo> <mn>86.6</mn> </mrow> </math></EquationSource> </InlineEquation>. This threshold is significantly higher than that for steel <InlineEquation ID="IEq7"> <EquationSource Format="TEX">\((\lambda \approx 31.4),\)</EquationSource> <EquationSource Format="MATHML"><math> <mrow> <mo stretchy="false">(</mo> <mi>λ</mi> <mo>≈</mo> <mn>31.4</mn> <mo stretchy="false">)</mo> <mo>,</mo> </mrow> </math></EquationSource> </InlineEquation> revealing the unique buckling characteristics of GFRP materials due to their anisotropy. The research outcomes provide a theoretical basis and practical tools for the refined design of GFRP compression members.</p>

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Shear deformation effects on buckling of pultruded GFRP columns: mechanism and critical threshold

  • Hengming Zhang,
  • Xinyuan Guo,
  • Rongfeng Lin

摘要

This study addresses the unclear mechanisms of shear deformation effects and the contradictory design thresholds in the buckling analysis of pultruded GFRP (glass fiber-reinforced polymer) compression members. By integrating test data from 322 specimens across 17 studies, a large-sample experimental database was established. The Engesser and Haringx shear correction theories were systematically validated, with results indicating that the Engesser model provides the optimal prediction accuracy (R2 = 0.89). Shear deformation can reduce the buckling load by up to 48%. Theoretical derivation revealed the decomposition law of the core parameter: \(P_{{\text{E}}} /\left( {{\text{KGA}}} \right) = \left( {\pi^{2} /K} \right) \cdot \left( {E/G} \right) \cdot \lambda^{ - 2} ,\) P E / KGA = π 2 / K · E / G · λ - 2 , which for the first time clearly identifies the slenderness ratio ( \(\lambda\) λ ) as the dominant geometric factor controlling the shear effect, while the elastic modulus ratio ( \(E/G\) E / G ) is a secondary material factor. Based on this mechanism, a practical design criterion with a threshold of \(\lambda =86.6\) λ = 86.6 is proposed: The Engesser formula must be used for shear correction when \(\lambda \le 86.6,\) λ 86.6 , whereas the shear effect becomes negligible (< 5%) when \(\lambda >86.6\) λ > 86.6 . This threshold is significantly higher than that for steel \((\lambda \approx 31.4),\) ( λ 31.4 ) , revealing the unique buckling characteristics of GFRP materials due to their anisotropy. The research outcomes provide a theoretical basis and practical tools for the refined design of GFRP compression members.