Stress–Strain Behaviour of Reparable Composite Panel with Step-Variable Thickness

dc.contributor.authorKondratiev, Andriics
dc.contributor.authorPíštěk, Václavcs
dc.contributor.authorSmovziuk, Linacs
dc.contributor.authorShevtsova, Marynacs
dc.contributor.authorFomina, Annacs
dc.contributor.authorKučera, Pavelcs
dc.coverage.issue21cs
dc.coverage.volume13cs
dc.date.accessioned2021-12-07T15:54:07Z
dc.date.available2021-12-07T15:54:07Z
dc.date.issued2021-11-05cs
dc.description.abstractThere is an urgent problem of finding an economically viable method of maintenance and restoration of the bearing capacity of structures of various applications. Repair of structures with patches made of polymeric composite materials is one of the most promising repair technologies. However, an improper choice of parameters of the composite patch leads to unjustified increase in the structure mass and the cost of its further operation. These situations result from the lack of reliable methods for developing the repair process, which take into account the influence of the patch geometry and conditions for performance of repair works on the bearing capacity of the repaired structure. The mathematical model of the reparable composite shell–type panel taking into account inhomogeneity of transverse shear deformations at stepped variation of its thickness has been developed. In contrast to the classical theory of layered shells, the model allows simplifying a three-dimensional problem by setting of the displacement field on the layers’ interfaces and their linear interpolation over thickness of the panel, as well as considering the transverse shear deformations resulting from the strength, temperature, or shrinkage loading. According to results, the maximum rise in stresses in the case of a notched panel occurs in the weakened layer, and it is from this layer the failure of the structure will start. In the event of the patch, the panel surface opposite the reinforcement is the most loaded (i.e., susceptible to failure) surface. To confirm the reliability of the developed model, we compared the analytical calculations with the results of experimental and numerical studies of the deformed state of a panel of step–variable thickness by the method of holographic interferometry and modelling by the finite element method. Displacement fields available from experiments correspond to the predicted theoretical results. The resulting maximum error does not exceed 7%. The data obtained during numerical modelling allowed us to conclude that the accuracy of theoretical calculations is sufficient for engineering practice. Results of the work can be used to solve the practical problems such as determination of stress–strain behaviour of a damaged structure or structure after repair, specification of the permissible delamination dimensions, and defining of parameters of the bonded repair process.en
dc.formattextcs
dc.format.extent1-23cs
dc.format.mimetypeapplication/pdfcs
dc.identifier.citationPolymers. 2021, vol. 13, issue 21, p. 1-23.en
dc.identifier.doi10.3390/polym13213830cs
dc.identifier.issn2073-4360cs
dc.identifier.other173126cs
dc.identifier.urihttp://hdl.handle.net/11012/203097
dc.language.isoencs
dc.publisherMDPIcs
dc.relation.ispartofPolymerscs
dc.relation.urihttps://www.mdpi.com/2073-4360/13/21/3830cs
dc.rightsCreative Commons Attribution 4.0 Internationalcs
dc.rights.accessopenAccesscs
dc.rights.sherpahttp://www.sherpa.ac.uk/romeo/issn/2073-4360/cs
dc.rights.urihttp://creativecommons.org/licenses/by/4.0/cs
dc.subjectpatchen
dc.subjectnotchen
dc.subjecttransverse shearen
dc.subjectanisotropic shellen
dc.titleStress–Strain Behaviour of Reparable Composite Panel with Step-Variable Thicknessen
dc.type.driverarticleen
dc.type.statusPeer-revieweden
dc.type.versionpublishedVersionen
sync.item.dbidVAV-173126en
sync.item.dbtypeVAVen
sync.item.insts2021.12.13 12:55:10en
sync.item.modts2021.12.13 12:16:21en
thesis.grantorVysoké učení technické v Brně. Fakulta strojního inženýrství. Ústav automobilního a dopravního inženýrstvícs
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