Thermal buckling behavior of cross-ply hybrid composite laminates with inclined crack
Source abstract
Abstract
Thermal buckling analysis of symmetric and antisymmetric cross-ply laminated hybrid composite plates with an inclined crack subjected to a uniform temperature rise are presented in this paper. The first-order shear deformation theory in conjunction with variational energy method is employed in the mathematical formulation. The eight-node Lagrangian finite element technique is used for obtaining the thermal buckling temperatures of hybrid composite laminates. The effects of crack size and lay-up sequences on the thermal buckling temperatures for symmetric and antisymmetric plates are investigated. The results are shown in graphical form for various boundary conditions.
Source: openaire · Quality: candidate unverified · Source record ↗
Research context
OpenAlex topics: Composite Structure Analysis and Optimization · Structural Load-Bearing Analysis · Structural Analysis and Optimization
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References (26)
Show source-provided references
1. Thermal buckling of orthotropic plates with angle crack10.1177/0731684404040125 ↗
2. Thermal buckling of hybrid laminated composite plates with a hole10.1016/j.compstruct.2004.03.017 ↗
3. An investigation on buckling of laminated plates with central square hole
4. Thermal buckling analysis of isotropic and composite plates with hole10.1080/01495739008927040 ↗
5. Thermal buckling of cross-ply composite laminates10.1016/0045-7949(92)90212-I ↗
6. Thermal buckling of cross-ply laminates using a first order deformation theory10.1016/0263-8223(94)90049-3 ↗
7. Thermal buckling of rectangular plates10.1016/S0020-7683(00)00240-7 ↗
8. Thermal buckling of clamped symmetric laminated plates10.1016/0263-8231(92)90024-Q ↗
9. Thermal buckling of laminated composite plates10.1016/0045-7949(94)90166-X ↗
10. Chandrashekhara MR. Buckling of multilayered composite plates under uniform temperature field. In: Birman V, Hui D. Thermal effects on structures and materials. ASME Pub., vol. 203, AMD, vol. 110; 1990. p. 29–33.
11. Thermal buckling of composite laminated plates10.1016/0045-7949(89)90413-6 ↗
12. Thermal buckling behavior of thick composite laminated plates under non-uniform temperature distribution10.1016/0045-7949(91)90176-M ↗
13. A review of laminated composite plate buckling10.1115/1.3149534 ↗
14. Buckling of plated due to self-equilibrated thermal stresses10.1080/01495738508942225 ↗
15. Thermal buckling of antisymmetric angle-ply laminated plates-an analytical levy-type solution10.1080/01495739308946237 ↗
16. Thermal buckling of laminated composite plates with transverse shear deformation10.1016/0045-7949(90)90159-Y ↗
17. Critical temperatures of hybrid laminates using finite elements10.1016/0045-7949(92)90313-O ↗
18. Thermal buckling of composite laminated plates10.1016/0045-7949(89)90413-6 ↗
19. Thermal buckling behavior of thick composite laminated plates under non-uniform temperature distribution10.1016/0045-7949(91)90176-M ↗
20. Jones · 1975
21. Buckling of laminated plates with holes10.1177/002199838902300601 ↗
22. Bathe · 1982
23. Shear correction factors for orthotropic laminates under static load10.1115/1.3422950 ↗
24. Thermal buckling behavior of thick composite laminated plates under non-uniform temperature distribution10.1016/0045-7949(91)90176-M ↗
25. Local buckling of composite laminar plates with various delaminated shapes10.1016/S0263-8231(03)00020-X ↗
26. Non-linear thermal buckling for local delamination near the surface of laminated cylindrical shell10.1016/S0020-7403(02)00028-0 ↗