journal article·2020-05

Closed-form approximate solution for linear buckling of Mindlin plates with SRSR-boundary conditions

M. Beerhorst, S. Thirusala Suresh Babu

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Abstract

Abstract The present work deals with the buckling analysis of rectangular Mindlin plates consisting of laminated composites with symmetrical, balanced lay-up or isotropic materials. Along the longitudinal edges the plate is rotationally restrained by springs. The transversal edges are simply supported. In agreement with common notation, the boundary conditions are abbreviated as follows: simply supported (S), rotationally restrained (R), and fully clamped (C). As loading situation axial compression is considered. Aiming at high computational efficiency the problem is solved by the Rayleigh-Ritz-method. Since well suited shape functions for deflection and rotations with very few variables are used, closed-form approximate solutions for the buckling load can be obtained. For verification exact transcendental solutions and/or high fidelity finite element analyses are employed. Additionally, results are compared to those of existing closed-form approximate solutions. Apart from the special case of simply supported longitudinal edges where all methods yield exact or nearly exact results, the present method shows clear advantages: 1. Due to the type of shape functions it is able deal with unsymmetrical boundary conditions. 2. For the case of both longitudinal edges fully clamped where all closed-form approximate solutions show the greatest deviations the present method is significantly more accurate.
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Research context

OpenAlex topics: Composite Structure Analysis and Optimization · Structural Load-Bearing Analysis · Topology Optimization in Engineering

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References (32)

Show source-provided references
1. Bleich · 1952
2. Timoshenko · 1961
3. Turvey · 1995
4. Influence of rotatory inertia and shear on flexural motion of isotropic, elastic plates10.1115/1.4010217 ↗
5. Reddy · 2004
6. Generic buckling curves for specially orthotropic rectangular plates10.2514/3.8219 ↗
7. Buckling of orthotropic plates with free and rotationally restrained unloaded edges10.1016/0263-8231(95)00036-4 ↗
8. Exact solutions for the buckling of rectangular plates having linearly varying in-plane loading on two opposite simply supported edges10.1016/j.ijsolstr.2004.12.011 ↗
9. Buckling of transversely isotropic Mindlin plates10.2514/3.6326 ↗
10. Exact solution for linear buckling of rectangular Mindlin plates10.1016/j.jsv.2008.01.059 ↗
11. Analysis of symmetric cross-ply laminated elastic plates using a higher-order theory: Part II-Buckling and free vibration10.1016/0263-8223(88)90048-7 ↗
12. Stability of moderately thick rectangular plates using a high precision triangular finite element10.1016/0045-7949(75)90028-0 ↗
13. Rohwer K. Improved transverse shear stiffnesses for layered finite elements, Tech. Rep. DFVLR-FB-88-32, DFVLR; 1988.
14. Higher-Order finite strip method for postbuckling analysis of imperfect composite plates
15. Buckling analysis of thin-walled sections by semi-analytical Mindlin-Reissner finite strips: a treatment of drilling rotation problem10.1016/j.tws.2007.12.003 ↗
16. High accuracy post-buckling analysis of moderately thick composite plates using an exact finite strip10.1016/j.compstruc.2015.09.014 ↗
17. On the application of the ritz method to free vibration and buckling analysis of highly anisotropic plates10.1016/j.compstruct.2018.03.017 ↗
18. Buckling and free vibration analyses of functionally graded graphene reinforced porous nanocomposite plates based on Chebyshev-Ritz method10.1016/j.compstruct.2018.03.090 ↗
19. A Rayleigh-Ritz approach for postbuckling analysis of variable angle tow composite stiffened panels10.1016/j.compstruc.2017.10.009 ↗
20. Kollar · 2003
21. Explicit local buckling analysis and design of fiber-reinforced plastic composite structural shapes10.1016/j.compstruct.2004.09.005 ↗
22. Local buckling of wide-flange thin-walled anisotropic composite beams10.1007/s00419-006-0102-0 ↗
23. Buckling of axially loaded composite plates with restrained edges10.1177/0731684410381153 ↗
24. Fast analytical method describing the postbuckling behavior of long, symmetric, balanced laminated composite plates under biaxial compression and shear10.1016/j.compstruct.2012.01.026 ↗
25. Buckling of rectangular composite plates with restrained edges subjected to axial loads10.1177/0731684414555880 ↗
26. Efficient approximate solutions for postbuckling of axially compressed orthotropic plates with rotationally restrained and free longitudinal edges10.1007/s00419-017-1319-9 ↗
27. March HW. Effects of shear deformation in the core of a flat rectangular sandwich panel, Tech. Rep. 1583, Forest Products Laboratory; 1948.
28. Local buckling of shear-deformable laminated composite beams with arbitrary cross-sections using discrete plate analysis10.1016/j.compstruct.2014.03.022 ↗
29. Closed-form approximate solutions for the local buckling behavior of composite laminated beams based on third-order shear deformation theory
30. Plates in uniaxial compression with various support conditions at the unloaded boundaries10.1016/0020-7403(71)90047-6 ↗
31. ANSYS Inc. Release 15.0 Documentation for ANSYS, Cannonsburg, Pennsylvania, U.S.A.; 2013.
32. Altair Engineering, Inc., ESAComp 4.7 Documentation, Troy, Michigan, U.S.A.; 2018.