Elasticity solution for a sandwich plate having composite facesheets with in-plane grading
Source abstract
Abstract
A convergent series solution based on the theory of elasticity is presented for bending of a sandwich plate strip with an isotropic homogeneous core and composite orthotropic facesheets with variable fibre volume fraction in the in-plane direction. The accuracy of first-order shear deformation theory is assessed against this benchmark solution. Further, it is shown that the benefit of using functionally graded material facesheets depends critically on the span-to-thickness ratio of the plate.
Source: crossref · Quality: baseline
Research context
OpenAlex topics: Composite Structure Analysis and Optimization · Structural Analysis and Optimization · Structural Load-Bearing Analysis
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
Affiliations
Department of Aerospace Engineering, Indian Institute of Technology, Chennai, India
References (39)
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1. 10.1016/0263-8223(90)90014-610.1016/0263-8223(90)90014-6 ↗
2. 10.1016/j.compstruct.2017.02.07810.1016/j.compstruct.2017.02.078 ↗
3. 10.1177/00219983690030030410.1177/002199836900300304 ↗
4. 10.1177/00219983700040010210.1177/002199837000400102 ↗
5. 10.1177/109963620403539510.1177/1099636204035395 ↗
6. 10.1177/109963620706567510.1177/1099636207065675 ↗
7. 10.1016/j.compstruct.2007.03.00310.1016/j.compstruct.2007.03.003 ↗
8. 10.1115/1.296617410.1115/1.2966174 ↗
9. 10.1177/109963621141912710.1177/1099636211419127 ↗
10. 10.4028/www.scientific.net/AMM.110-116.145810.4028/www.scientific.net/AMM.110-116.1458 ↗
11. 10.1016/j.compstruct.2017.06.00810.1016/j.compstruct.2017.06.008 ↗
12. 10.1016/S0263-8223(03)00013-810.1016/S0263-8223(03)00013-8 ↗
13. 10.2514/2.685310.2514/2.6853 ↗
14. 10.1016/j.jsv.2007.09.01810.1016/j.jsv.2007.09.018 ↗
15. 10.1016/j.compstruct.2008.06.01310.1016/j.compstruct.2008.06.013 ↗
16. 10.1016/j.compstruct.2007.12.00310.1016/j.compstruct.2007.12.003 ↗
17. 10.1080/15376494.2010.51772810.1080/15376494.2010.517728 ↗
18. 10.1016/j.ijmecsci.2011.07.01110.1016/j.ijmecsci.2011.07.011 ↗
19. 10.1177/095440621244066910.1177/0954406212440669 ↗
20. 10.1017/S000192400000764810.1017/S0001924000007648 ↗
21. Darabi M, Ganesan R. Exact 3-D stress and stiffness analysis of functionally graded sandwich plates using sampling surfaces method. In: Proceedings of the ASME International-Mechanical Engineering Congress and Exposition , Montreal, Quebec, Canada, 14–20 November 2014, paper no. IMECE2014-38400, pp. 1–11. New York: ASME.10.1115/IMECE2014-38400 ↗
22. 10.1016/j.euromechsol.2015.06.01110.1016/j.euromechsol.2015.06.011 ↗
23. 10.1007/s10483-011-1470-910.1007/s10483-011-1470-9 ↗
24. 10.1016/j.compositesb.2014.05.01210.1016/j.compositesb.2014.05.012 ↗
25. 10.1177/109963621452685210.1177/1099636214526852 ↗
26. 10.12989/was.2016.22.3.29110.12989/was.2016.22.3.291 ↗
27. 10.1177/109963621668039710.1177/1099636216680397 ↗
28. 10.1142/S021945541950028710.1142/S0219455419500287 ↗
29. Sayyad AS, Ghugal YM. Modeling and analysis of functionally graded sandwich beams: a review. Mech Adv Mater Struct . Epub Ahead of Print 19 March 2018. DOI: 10.1080/15376494.2018.1447178.10.1080/15376494.2018.1447178 ↗
30. 10.1016/j.engstruct.2010.02.01010.1016/j.engstruct.2010.02.010 ↗
31. 10.1177/109963621561977510.1177/1099636215619775 ↗
32. 10.1016/j.compstruct.2017.04.04610.1016/j.compstruct.2017.04.046 ↗
33. Houmat A. Three-dimensional solutions for free vibration of variable stiffness laminated sandwich plates with curvilinear fibres. J Sandwich Struct Mater . Epub Ahead of Print 24 May 2018. DOI: 10.1177/1099636218778731.10.1177/1099636218778731 ↗
34. 10.1016/j.euromechsol.2018.12.00910.1016/j.euromechsol.2018.12.009 ↗
35. 10.1115/1.278901510.1115/1.2789015 ↗
36. Maalawi K. Optimization of functionally graded material structures: some case studies.In: Optimum Composite Structures (Chapter 9) , June, 2018, pp.157–191. IntechOpen.10.5772/intechopen.82411 ↗
37. Callister WD · 2013
38. Miracle DB · 2001
39. 10.1007/978-94-007-1715-210.1007/978-94-007-1715-2 ↗