An enhanced global–local higher-order theory for the free edge effect in laminates
Source abstract
Abstract
Abstract According to the double-superposition hypothesis proposed by Li and Liu [Li XY, Liu D. Generalized laminate theories based on double superposition hypothesis. Int J Numer Methods Eng 1997;40:1197–212], an enhanced global–local higher-order theory (EGLHT- mn ) is developed to analyze the edge-effect problems in laminates. The in-plane displacement field consists of m th-order (9 ⩾ m ⩾ 3) polynomial in global coordinate z along the thickness direction and order 3 power series in local coordinate ζ within each layer whereas the transverse deflection is represented by a n th-order (9 ⩾ n ⩾ 3) polynomial of global coordinate z . By imposing the free surface conditions and the geometric and the stress continuity conditions at interfaces, the number of variables of the higher-order theory is independent of the number of layers of the laminates. As an improvement to the global–local theory proposed by Li and Liu (1997), the present higher-order theory takes into account all the effects of shear and normal stresses. A three-node triangular element satisfying the requirement of C 1 weak-continuity conditions between elements is also presented. Comparing to previous published results, it is found that the present higher-order theory is capable of treating free-edge problems in symmetric and unsymmetric laminates under extension, bending and thermal loading. Other characteristic of the present theory is that transverse shear stresses can be accurately computed directly from the constitutive equations without smoothing. However, to determine transverse normal stresses, the local equilibrium equation approach has to been adopted.
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Research context
OpenAlex topics: Composite Structure Analysis and Optimization · Structural Load-Bearing Analysis · Structural Analysis and Optimization
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References (38)
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1. Interlaminar stresses in composite laminates under axial extension10.1177/002199837000400409 ↗
2. On the calculation of interlaminar normal stress in composite laminate10.1177/002199837400800106 ↗
3. A boundary layer theory. Part II: Extension of laminated finite strip10.1177/002199837500900105 ↗
4. Boundary-layer effects in composite laminates. Part I: Free-edge stress singularities10.1115/1.3162514 ↗
5. Boundary-layer effects in composite laminates. Part II: Free-edge stress solutions and basic characteristics10.1115/1.3162521 ↗
6. An efficient method for the calculation of interlaminar stresses in composite materials10.1115/1.3171853 ↗
7. Analysis of edge stresses in composite laminates under combined thermo-mechanical loading, using a complementary energy approach10.1007/BF00365862 ↗
8. Free edge effects in anisotropic laminates under extension, bending and twisting. Part I: A stress-function-based variational approach10.1115/1.2901459 ↗
9. Free edge effects in anisotropic laminates under extension, bending and twisting. Part II: Eigenfunction analysis and the results for symmetric laminates10.1115/1.2901460 ↗
10. Iterative free-edge stress analysis of composite laminates under extension, bending, twisting and thermal loading10.1016/S0020-7683(99)00014-1 ↗
11. State space approach for stress decay in laminates10.1016/S0020-7683(99)00050-5 ↗
12. A state space finite element for laminated composite with free edges and subjected to transverse and in-plane loads10.1016/j.compstruc.2004.03.020 ↗
13. Zhang DX, Ye JQ, Sheng HY. Free-edge and ply cracking effect in cross-ply laminated composites under uniform extension and thermal loading. Compos Struct, Available on line.
14. Estimation of transverse/interlaminar stresses in laminated composites—a selective review and survey of current developments10.1016/S0263-8223(99)00126-9 ↗
15. Interlaminar stress concentrations in layered structures: Part I—A selective literature survey on the free-edge effect since 196710.1177/0021998304040566 ↗
16. Free edge effect in angle ply laminates—a new three dimensional finite difference solution
17. Some new results on edge effect in symmetric composite laminates10.1177/002199837701100110 ↗
18. Edge effects on thermally induced stresses in composite laminates10.1177/002199837701100305 ↗
19. Multi-layer higher-order finite elements for the analysis of free-edges stresses in composite laminates10.1002/(SICI)1097-0207(19980315)41:5<851::AID-NME312>3.0.CO;2-Q ↗
20. Edge effects in symmetric composite laminates: importance of satisfying the traction free-edge condition
21. Straight free-edge effects in laminated composites10.1016/j.finel.2004.03.004 ↗
22. Closed-form solution for the free-edge effect in cross-ply laminates10.1016/0263-8223(93)90042-O ↗
23. A single-layer theory approach to stresses concentration phenomena in layered plates10.1016/j.compscitech.2004.01.011 ↗
24. Three-dimensional interlaminar stress analysis at free edge of general cross-ply composite laminates10.1016/S0261-3069(02)00107-3 ↗
25. Free edge stresses analysis of general cross-ply composite laminates under extension and thermal loading10.1016/S0263-8223(02)00290-8 ↗
26. Edge effects of uniformly loaded cross-ply composite laminates10.1016/S0261-3069(03)00098-0 ↗
27. Mittelstedt C, Becker W. Fast and reliable analysis of free-edge stress fields in a thermally loaded composite strip by a layerwise laminate theory. Int J Numer Meth Eng. Available on line.
28. Generalized laminate theories based on double superposition hypothesis10.1002/(SICI)1097-0207(19970415)40:7<1197::AID-NME109>3.0.CO;2-B ↗
29. Finite element model with continuous transverse shear stress for composite laminates in cylindrical bending10.1016/S0168-874X(98)00056-0 ↗
30. Refined laminated composite plate element based on global–local higher-order shear deformation theory10.1016/j.compstruct.2004.08.019 ↗
31. An efficient higher-order theory and finite element for laminated plates subjected to thermal loading10.1016/j.compstruct.2005.01.034 ↗
32. Bazeley GP, Cheung YK, Irons BM, Zienkiewiz OC. Triangular elements in bending conforming and non-conforming solution. In: Proc. conf. matrix methods in structural mechanics, Air Force Ins. Tech., Wright-Patterson A.F. Base, OH, 1965. p. 547–76.
33. Nine-parameter triangular thin plate bending element by using refined directed stiffness method
34. Refined nine-parameter triangular thin plate bending element by using refined direct stiffness method10.1002/nme.1620380208 ↗
35. The effect of temperature gradient on the free-edge interlaminar stresses in multi-layered structures10.1177/002199839703102403 ↗
36. A high precision coupled bending–extension triangular finite element for laminated plates10.1016/S0045-7949(98)00225-9 ↗
37. On the logarithmic singularity of free-edge stress in laminated composites under uniform extension10.1115/1.3162526 ↗
38. Improved Mindlin plate stress analysis for laminated composite in finite element method10.2514/2.145 ↗