The stress-strain state of a plate is weakened by a circular cutout and reinforced by two round patches

Сергій Сергійович Курєннов, Костянтин Петрович Барахов, Олексій Олександрович Вамболь, Володимир Миколайович Степаненко

Abstract


The problem of axisymmetric deformation of a structure was solved in this article. This structure consists of a plate that was weakened by a circular cutout and at the same time reinforced by two concentric round patches. The patches are glued overlapping on both sides of the plate, in the place of the cutout. The patches are joined to the main plate by a thin adhesive layer and perceive shearing and tearing forces. To solve the problem, some hypotheses were used, namely: it was assumed that the stresses were distributed uniformly over the thickness of the adhesive layer. For patches, the Kirchhoff-Love hypothesis is adopted. The adhesive layer is considered an elastic Winkler base. An axisymmetric problem is considered. It is assumed that the displacement of the layers depends only on the radial coordinate and doesn’t depend on the angular coordinate. The main plate is not subjected to bending due to the symmetry of the structure. This problem is a generalization of the classic model of the stress state of the adhesive joint for the rods to an area with radial symmetry. These assumptions have allowed obtaining a solution to the problem in an analytical form. The problem is considered separately in the adhesive joint area and as well as the outside of the adhesive joint area. In the area of gluing, the problem is reduced to a seventh-order differential equation concerning shear stresses. The solution to this problem is presented as an expansion into a functional series in terms of modified Bessel functions of the second kind. The obtained shear stresses make it possible to obtain normal stresses, as well as radial and transverse displacements of the layers in the adhesive joint zone. The displacements outside the adhesive joint zone were obtained from the well-known differential equations for the deformation of round plates in the absence of shear forces. The unknown coefficients in both cases are found from the boundary and conjugation conditions. The model task was solved. A finite element model of an adhesive joint has been developed. The largest size of the adhesive layer element is chosen to be sufficiently small and equal to half the thickness of the adhesive layer because of the enormous stress gradients in the adhesive layer. The results of the analytical model were compared with those results of the finite element model. The comparison showed the high accuracy of the proposed model.

Keywords


adhesive joint; axisymmetric model; analytical solution; round plate

References


Okafor, A. C., Singh, N., Enemuoh, U. E., Rao, S. V. Design, analysis and performance of adhesively bonded composite patch repair of cracked aluminum aircraft panels. Composite Structures, 2005, vol. 71, iss. 2, pp. 258-270. DOI: 10.1016/j.compstruct.2005.02.023.

Tomblin, J. S., Salah, L., Welch, J. M., Borgman, M. D. Bonded Repair of Aircraft Composite Sandwich Structures. Report DOT/FAA/AR-03/74, 2004.

Wang, Gul-Fang. Stress analysis of plates with a circular hole reinforced by flange reinforcing member. Applied Mathematics and Mechanics, 1987, vol. 6, pp. 569-588. DOI: 10.1007/bf02017406.

Bakuckas, J. G., Chadha, R., Swindell, P., Fleming, M., Lin, J. Z., Ihn, J. B., Freisthler, M. Bonded Repairs of Composite Panels Representative of Wing Structure. Lecture Notes in Mechanical Engineering, 2019, pp. 565–580. DOI: 10.1007/978-3-030-21503-3_45.

Zemlyanova, A. Y. Reinforcement of a plate weakened by multiple holes with several patches for different types of plate-patch attachment. Mathematics and Mechanics of Solids, 2016, vol. 21, iss. 3, pp. 281-294. DOI: 10.1177/1081286513519812.

Kurennov, S., Smetankina, N. Stressed State of an Infinite Plate with a Circular Opening and a Concentric Cover Plate. Lecture Notes in Networks and Systems, 2021, vol. 188, pp. 344-354. DOI: 10.1007/978-3-030-66717-7_29.

Khan, M. A., Aglietti, G. S., Crocombe, A. D., Viquerat, A. D., Hamar, C. O. Development of design allowables for the design of composite bonded double-lap joints in aerospace applications. International Journal of Adhesion and Adhesives, 2018, vol. 82, pp. 221–232. DOI: 10.1016/j.ijadhadh.2018.01.011.

da Silva, L. F. M., das Neves, P. J. C., Adams, R. D., Spelt, J. K. Analytical models of adhesively bonded joints. Part I: Literature survey. Int. Journal Adhes. & Adhesiv, 2009, vol. 29, pp. 319 330. DOI: 10.1016/j.ijadhadh.2008.06.005.

Wong, E. H., Liu, J. Interface and interconnection stresses in electronic assemblies – A critical review of analytical solutions. Microelectronics Reliability, 2017, vol. 79, pp. 206 220. DOI: 10.1016/j.microrel.2017.03.010.

Kurennov, S. S. Determining Stresses in an Adhesive Joint with a Longitudinal Un-adhered Region Using a Simplified Two-Dimensional Theory. J Appl Mech Tech Phy, 2019, vol. 60, pp. 740–747. DOI: 10.1134/S0021894419040199.

Kurennov, S. S., Barakhov, K. P. The Stressed state of the double-layer rectangular plate under shift. The Simplified two-dimensional model. PNRPU Mechanics Bulletin, 2019, vol. 3, pp. 166-174. DOI: 10.15593/perm.mech/2019.3.16.

Starovoitov, E. I., Leonenko, D. V., Tarlakovskii, D. V. Thermoelastic deformation of a circular sandwich plate by local loads. Mechanics of Composite Materials, 2018, vol. 54, iss. 3, pp. 299-312. DOI: 10.1007/s11029-018-9740-x.

Kudin, A. V., Choporov, S. V. Gomenyuk, S. I. Axisymmetric bending of circular and annular sandwich plates with nonlinear elastic core material. Math Models Comput Simul, 2017, vol. 9, pp. 601-612. DOI: 10.1134/S2070048217050076.

Rodichev, Yu. M., Smetankina, N. V., Shupikov, O. M., Ugrimov, S. V. Stress-strain assessment for laminated aircraft cockpit windows at static and dynamic loads. Strength of Materials, 2018, vol. 50, iss. 6, pp. 868-873. DOI: 10.1007/s11223-019-00033-4.

Barakhov, K. P. Uzahalnennia modeli Holanda i Reissnera na vypadok osovoi symetrii [Generalization of the Holland and Reissner Model in Case of Axial Symmetry]. Aviacijno-kosmicna tehnika i tehnologia – Aerospace technic and technology, 2021, no. 2(170), pp. 12 – 19. DOI: 10.32620/aktt.2021.2.02.

Barakhov, K., Dvoretska, D., Poliakov, O. One-Dimensional Axisymmetric Model of the Stress State of the Adhesive Joint. Lecture Notes in Networks and Systems, 2021, vol. 188, pp. 310-319. DOI: 10.1007/978-3-030-66717-7_26.

Campilho, R. D. S. G., Banea, M. D., Pinto, A. M. G., da Silva, L. F. M., de Jesus, A. M. P. Strength prediction of single- and double-lap joints by standard and extended finite element modelling. International Journal of Adhesion and Adhesives, 2011, vol. 31, iss. 5, pp. 363-372. DOI: 10.1016/j.ijadhadh.2010.09.008.

Osnes, H., McGeorge, D. Analysis of overlaminated double-lap joints. Composites Part B: Engineering, 2005, vol. 36, iss. 6-7, pp. 544–558. DOI: 10.1016/j.compositesb.2005.01.002.

Timoshenko, S. P., Woinowsky-Krieger, S. Theory of Plates and Shells. McGraw-Hill, New York, 1959, second edition. 595 p.

Kurennov, S. S. Longitudinal-Flexural Vibrations of a Three-Layer Rod. An Improved Model. J Math Sci, 2016, vol. 215, iss. 2, pp. 159 169. DOI: 10.1007/s10958-016-2829-7.

Kurennov, S. S. Refined Mathematical Model of the Stress State of Adhesive Lap Joint: Experimental Determination of the Adhesive Layer Strength Criterion. Strength Mater, 2020, vol. 52, pp. 779–789. DOI: 10.1007/s11223-020-00231-5.

Wang, J., Zhang, C. Three-parameter elastic foundation model for analysis of adhesively bonded joints. Int. J. Adhesion Adhesives, 2009, vol. 29, pp. 495-502. DOI: 10.1016/j.ijadhadh.2008.10.002.

Frostig, Y., Thomsen, O. T., Mortensen, F. Analysis of adhesive-bonded joints, square-end, and spew-fillet—high-order theory approach. J. of Engineering Mechanics, 1999, vol. 125, pp. 1298–1307. DOI: 10.1061/(ASCE)0733-9399(1999)125:11(1298).

Amidi, S., Wang, J. An analytical model for interfacial stresses in double-lap bonded joints. The J. Adhesion, 2019, vol. 95, iss. 11, pp. 1031 1055. DOI: 10.1080/00218464.2018.1464917.




DOI: https://doi.org/10.32620/aktt.2022.2.01