A Parametric Study on the Elliptical hole Effects of Laminate Composite Plates under Thermal Buckling Load
Source abstract
Abstract
Abstract In this study, a thermal buckling analysis of laminate composite square plate was performed with elliptical hole cutout using the finite element method. Graphite/Epoxy laminate plate used in this study is symmetrical stacking sequence plate [(0/90) 2 ] s . This laminate square plate was subjected to temperature loading with clamped support on all edges. Moreover, the parameters considered were fiber orientation ( θ ), a/b ratio (elliptical hole), elliptical hole inclination ( φ ), thermal expansion coefficient ratio ( α 1 / α 2 ), and thickness of plates (t). The results showed that as the thermal expansion coefficient ratio changes, the elliptical hole ratio and the elliptical hole inclination have inconsequential effects on the performance of the resistance of laminate composite plates. The maximum values of thermal buckling amplification factor were obtained when the ratio a/b = 1.0, which is a circle cutout,while the minimum values were obtained when the ratio a/b = 0.5, regardless of the thickness of plates. Moreover, the plate with elliptical or circle cutout hole provides about 4% to 9% higher buckling resistance than that of the plate without hole cutout, because when subjected to temperature loading the plate with hole can release stress better than the plate without hole.
Source: crossref · Quality: baseline
Research context
OpenAlex topics: Composite Structure Analysis and Optimization · Structural Load-Bearing Analysis · Laser and Thermal Forming Techniques
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
Affiliations
Gangneung-Wonju National University, College of Engineering , Building No. 2, Room 128 , Gangneung city , Gangwon province [25457] , Korea
Gangneung-Wonju National University, College of Engineering , Building No. 2, Room 110 , Gangneung city , Gangwon province [25457] , Korea
References (23)
Show source-provided references
1. Kweon JH, Jung JW, Kim TH, Choi JH, Kim DH. (2006), “Failure of carbon composite-to-aluminum joints with combined mechanical fastening and adhesive bonding”, Composite Structures., 75(1-4), 192–198. https://doi.org/10.1016/j.compstruct.2006.04.01310.1016/j.compstruct.2006.04.013 ↗
2. Aniskevich K, Aniskevich A, Arnautov A and Jansons J. (2012), “Mechanical properties of pultruded glass fiber-reinforced plastic after moistening”, Composite Structures., 94(9), 2914–2919. https://doi.org/10.1016/j.compstruct.2012.04.03010.1016/j.compstruct.2012.04.030 ↗
3. Fiore, V., Scalici, T., Di Bella, G., & Valenza, A. (2015), “A review on basalt fiber and its composites”, Composites Part B: Engineering., 74, 74-94. https://doi.org/10.1016/j.compositesb.2014.12.03410.1016/j.compositesb.2014.12.034 ↗
4. Zhang, Y. X., & Yang, C. H. (2009), “Recent developments in finite element analysis for laminated composite plates”, Composite Structures., 88(1), 147-157. https://doi.org/10.1016/j.compstruct.2008.02.01410.1016/j.compstruct.2008.02.014 ↗
5. Kumar, R. Vijaya, and G. Krishnamohana Rao. (2018), “Thermal Buckling Analysis of Laminated Composite Plate with Square/Rectangular, Elliptical/Circular Cutout”, Materials Today: Proceedings., 5(2), 5354-5363. https://doi.org/10.1016/j.matpr.2017.12.12110.1016/j.matpr.2017.12.121 ↗
6. Saberi, S., Memarzadeh, P., & Zirakian, T. (2019), “Study of buckling stability of cracked plates under uniaxial compression using singular FEM”, Structural Engineering and Mechanics, 69(4), 417-426. DOI: https://doi.org/10.12989/sem.2019.69.4.417
7. Fellah, M., Draiche, K., Houar, M. S. A., Tounsi, A., Saeed, T., Alhodaly, M. S., & Benguediab, M. (2019), “A novel refined shear deformation theory for the buckling analysis of thick isotropic plates”, Structural Engineering and Mechanics, 69(3), 335-345. DOI: https://doi.org/10.12989/sem.2019.69.3.335
8. Fan, H., Chen, Z., Wang, Z., & Liu, P. (2019), “Buckling of simply supported thin plate with variable thickness under bi-axial compression using perturbation technique”, Structural Engineering and Mechanics, 70(5), 525-534. DOI: https://doi.org/10.12989/sem.2019.70.5.525
9. Remil, A., Benrahou, K. H., Draiche, K., Bousahla, A. A., & Tounsi, A. (2019), “A simple HSDT for bending, buckling and dynamic behavior of laminated composite plates”, Structural Engineering and Mechanics, 70(3), 325-337. DOI: https://doi.org/10.12989/sem.2019.70.3.325
10. Kandasamy, R., Dimitri, R., & Tornabene, F. (2016). Numerical study on the free vibration and thermal buckling behavior of moderately thick functionally graded structures in thermal environments. Composite Structures157 207-221.10.1016/j.compstruct.2016.08.037 ↗
11. Nejati, M., Dimitri, R., Tornabene, F., & Hossein Yas, M. (2017). Thermal buckling of nanocomposite stiffened cylindrical shells reinforced by functionally graded wavy carbon nanotubes with temperature-dependent properties. Applied Sciences7(12), 1223.10.3390/app7121223 ↗
12. Chhorn, B., & Jung, W. (2020). Evaluation of Buckling Resistance of Basalt Fiber Reinforced Polymer Plate. Iranian Journal of Science and Technology, Transactions of Civil Engineering 1-12. https://doi.org/10.1007/s40996-019-00344-110.1007/s40996-019-00344-1 ↗
13. Chhorn B., & Jung, W (2019) Parametric study on buckling resistance ofthe thin BFRP (Basalt Fiber Reinforced Polymer) plate subjected to combined loading. J Korean Soc Adv Compos Struct 10(1):1–9. https://doi.org/10.11004/kosacs.2019.10.1.00110.11004/kosacs.2019.10.1.001 ↗
14. Carrera, E., & Valvano, S. (2019). A variable ESL/LW kinematic plate formulation for free-vibration thermoelastic analysis of laminated structures. Journal of Thermal Stresses42(4), 452-474. http://dx.doi.org/10.1080/01495739.2018.147451310.1080/01495739.2018.1474513 ↗
15. Carrera, E., & Valvano, S. (2017). A variable kinematic shell formulation applied to thermal stress of laminated structures. Journal of Thermal Stresses40(7), 803-827. http://dx.doi.org/10.1080/01495739.2016.125343910.1080/01495739.2016.1253439 ↗
16. Topal, U., & Uzman, Ü. (2008), “Maximization of buckling load of laminated composite plates with central circular holes using MFD method”, Structural and Multidisciplinary Optimization., 35(2), 131-139.10.1007/s00158-007-0119-1 ↗
17. Avci A, Kaya S, Daghan, B. Thermal buckling of rectangular laminated plates with a hole. Journal of reinforced plastics and composites 2005; 24(3): 259-272.10.1177/1731684405043554 ↗
18. Avci, A., Sahin, Ö. S., & Uyaner, M. (2005), “Thermal buckling of hybrid laminated composite plateswith a hole”, Composite structures., 68(2), 247-254. https://doi.org/10.1016/j.compstruct.2004.03.01710.1016/j.compstruct.2004.03.017 ↗
19. Chen WJ, Lin PD, Chen LW. Thermal buckling behavior of composite laminated plates with a circular hole. Composite structures 1991; 18(4): 379-397.10.1016/0263-8223(91)90005-J ↗
20. Shaterzadeh, A. R., Abolghasemi, S., & Rezaei, R. (2014), “Finite element analysis of thermal buckling of rectangular laminated composite plates with circular cutout”, Journal of thermal stresses., 37(5), 604- 623. https://doi.org/10.1080/01495739.2014.88532210.1080/01495739.2014.885322 ↗
21. Kumar, R. Vijaya, and G. Krishnamohana Rao. (2018), “Thermal Buckling Analysis of Laminated Composite Plate with Square/Rectangular, Elliptical/Circular Cutout”, Materials Today: Proceedings., 5(2), 5354-5363. https://doi.org/10.1016/j.matpr.2017.12.12110.1016/j.matpr.2017.12.121 ↗
22. Ouinas D, Achour B. Buckling analysis of laminated composite plates θ − θ containing an elliptical notch. Composites Part B: Engineering 2013; 55: 575-579.10.1016/j.compositesb.2013.07.011 ↗
23. Ounis H, Belarbi MO. On the thermal buckling behavior of laminated composite plates with cutouts. Journal of Applied Engineering Science & Technology 2017, 3(2): 63-69.10.69717/jaest.v3.i2.58 ↗