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Investigation of the influence of debonding shapes and debonding locations on vibration behavior of sandwich structure

Wybrane pełne teksty z tego czasopisma
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Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
Sandwich structures are employed in many different fields including automobile, marine, and aircraft structures. However, debonding may take place at the core-face sheet interface, reducing the stiffness of the structure. Debonding may occur for a variety of reasons, including initial manufacturing faults, changes in service loads, tool drops, and foreign object impacts. It is critical to comprehend how debonding zones impact the vibration of sandwich structures because decreases in the natural frequencies (NF) could lead to a structure vibrating at resonance and lead to structural failure. This paper investigates the influence of debonding shapes and debonding locations on the free-vibration behavior of sandwich structures. Different sandwich structures that have varied debonding shapes at various locations are modeled using COMSOL MULTIPHYSICS. Debonding is modeled by using the CZM model. Validation studies were performed to validate the current study. After the validation study, free vibration analysis of all the sandwich structures was performed and the first six NF were obtained from the simulations. The results show the influence of the debonding shapes and debonding locations on the NF of the sandwich structures. From the results, it was observed that both the debonding shapes and debonding locations significantly change the NF of the sandwich structures. The debonding shapes cause a reduction and an increase depending on the debonding location. It was also revealed that both debonding shapes and debonding locations have a significant effect on the vibration behavior of sandwich structures. Using this method, the debonding shape and location, delamination shape, and location can be predicted using machine learning algorithms. This study includes free vibration analysis of sandwich structures with different debonding shapes and locations, and the results show that natural frequencies change depending on the debonding shapes and locations. This information can be implemented in machine learning for use in the field of damage detection and utilized to predict the shape and location of delamination in sandwich structures.
Rocznik
Strony
39--48
Opis fizyczny
Bibliogr. 24 poz., rys., tab.
Twórcy
  • Sivas University of Science and Technology, Faculty of Engineering and Natural Sciences, Department of Mechanical Engineering, Sivas, Turkey
  • Sivas University of Science and Technology, Faculty of Engineering and Natural Sciences, Department of Mechanical Engineering, Sivas, Turkey
Bibliografia
  • 1. Hadji L., Avcar M., Zouatnia N., Natural frequency analysis of imperfect FG sandwich plates resting on Winkler- Pasternak foundation, Materials Today: Proceedings 2022, 53, 153-160.
  • 2. Hadji L., Avcar M., Free vibration analysis of fg porous sandwich plates under various boundary conditions, Journal of Applied and Computational Mechanics 2021, 7, 2, 505-519, DOI: 10.22055/jacm.2020.35328.2628.
  • 3. Kumar A., Angra S., Chanda A.K., Stress properties optimization of a composite sandwich structure by application of hybrid Taguchi-GRA-PCA, Journal of Engineering Research 2021, 9, 203-216, DOI:10.36909/jer.EMSME.13875.
  • 4. Vaisali M.S., Nisha A.S., Damage detection using modal strain energy method in honeycomb sandwich beams with multiple delaminations, IJISET-International Journal of Innovative Science, Engineering & Technology 2015, 2, 7,533-554.
  • 5. Avcar M., Hadji L., Civalek Ö., Natural frequency analysis of sigmoid functionally graded sandwich beams in the framework of high order shear deformation theory, Composite Structures 2021, 276, June, DOI:10.1016/j.compstruct. 2021.114564.
  • 6. Thomas T., Tiwari G., Performance evaluation of reinforced honeycomb structure under blast load, Journal of Engineering Research 2021, 1-26, DOI: 10.36909/jer.11929.
  • 7. Burlayenko V.N., Sadowski T., Numerical modeling of dynamics of sandwich plates with partially debonded skinto- core interface for damage detection, Proceedings of the 8th International Conference on Structural Dynamics, EURODYN 2011, 2011, July, 2242-2249.
  • 8. Mohanan A., Pradeep K.R., Narayanan K.P., Performance assessment of sandwich structures with debonds and dents, International Journal of Scientific & Engineering Research 2013, 4, 5, 174-179.
  • 9. Moustapha I.M., El Mahi A., El Guerjouma R., Dazel O., Damping analysis in flexural vibration of sandwich beams with debonding, Sociélé Française d’Acaustique, 2012, April.
  • 10. Baba B.O., Free vibration analysis of curved sandwich beams with face/core debond using theory and experiment, Mechanics of Advanced Materials and Structures 2012, 19, 5, 350-359, DOI: 10.1080/15376494.2010.528163.
  • 11. Burlayenko V.N., Sadowski T., Influence of skin/core debonding on free vibration behavior of foam and honeycomb cored sandwich plates, International Journal of Non-Linear Mechanics 2010, 45, 10, 959-968, DOI: 10.1016/j.ijnonlinmec.2009.07.002.
  • 12. Kim H.Y., Hwang W., Effect of debonding on natural frequencies and frequency response functions of honeycomb sandwich beams, Composite Structures 2002, 55, 1, 51-62, DOI: 10.1016/S0263-8223(01)00136-2.
  • 13. Baba B.O., Thoppul S., Experimental evaluation of the vibration behavior of flat and curved sandwich composite beams with face/core debond, Composite Structures 2009, 91, 1, 110-119, DOI: 10.1016/j.compstruct.2009.04.037.
  • 14. Tsai S.N., Taylor A.C., Vibration behaviours of single/multi-debonded curved composite sandwich structures, Composite Structures 2019, 226, August, 111291, DOI:10.1016/j.compstruct.2019.111291.
  • 15. Burlayenko V.N., Sadowski T., Dynamic behaviour of sandwich plates containing single/multiple debonding, Computational Materials Science 2011, 50, 4, 1263-1268, DOI: 10.1016/j.commatsci.2010.08.005.
  • 16. Sadeghpour E., Sadighi M., Ohadi A., Free vibration analysis of a debonded curved sandwich beam, European Journal of Mechanics, A/Solids 2016, 57, 71-84, DOI: 10.1016/j.euromechsol.2015.11.006.
  • 17. Tsai S.N., Taylor A.C., Vibration behaviours of single/multi-debonded composite sandwich structures with nanoparticle-modified matrices, Composite Structures 2019, 210,August, 590-598, DOI:10.1016/j.compstruct.2018.11.071.
  • 18. Idriss M., El Mahi A., El Guerjouma R., Characterization of sandwich beams with debonding by linear and nonlinear vibration method, Composite Structures 2015, 120, 200-207, DOI: 10.1016/j.compstruct.2014.09.036.
  • 19. Tsai S.N., Vibration behaviours of multi-debonded sandwich beams with symmetric angle-ply facesheets, Journal of Composite Materials 2023, DOI: 10.1177/00219983231217131.
  • 20. Kalgutkar A.P., Banerjee S., Free vibration analysis of hygrothermally stable stiffened composite plates with platestiffener interfacial debonding, Mechanics of Advanced Materials and Structures 2024, January, 1-15, DOI: 10.1080/15376494.2024.2303726.
  • 21. Comsol Application Gallery, Forced Vibration Analysis of a Composite Laminate [Online], Available: https://www.comsol.com/model/forced-vibration-analysis-of-a-compositelaminate-67731.
  • 22. Demircioğlu U., Çakir M.T., An investigation of the influence of various shaped cutouts on the free vibration behavior of sandwich structures, Sakarya University Journal of Science 2022, August, 26, 4, 687-694, DOI: 10.16984/saufenbilder.1063422.
  • 23. Kollar L.P., Springer G.S., Mechanics of Composite Structures,1st ed. Cambridge University Press, 2003.
  • 24. Pushparaj P., Suresha B., Free vibration analysis of laminated composite plates using finite element method, Polymers and Polymer Composites 2016, 24, 7, 529-538, DOI:10.1177/096739111602400712.
Uwagi
Opracowanie rekordu ze środków MNiSW, umowa nr SONP/SP/546092/2022 w ramach programu "Społeczna odpowiedzialność nauki" - moduł: Popularyzacja nauki i promocja sportu (2024).
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-75c41058-d116-4584-beb8-2211e927b811
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