Abstract
The stress-strain state (SSS) of three-layer shells with cutouts has not been sufficiently studied, which is one of the reasons limiting their use in modern designs. Based on the block finite element approach, a refined model of the layer-by-layer analysis of the SSS of irregular three-layer shells is developed. The considered approach allows us to fairly accurately model the heterogeneity of the package of layers and the aggregate layer, the conditions for fixing the layers and the application of loads to them, to apply various models to study the bearing layers and the aggregate. Using approximations of the finite elements (FE) of the bearing layers, approximating functions of the displacements of the three-dimensional FE of the aggregate are constructed and based on them, a model is developed for the accurate calculation of the SSS, allowing to take into account the change in the characteristics of the material and the stress state, including the radial coordinate in the aggregate layer. The study of the stress-strain state in the layers of three-layer shells with cuts, including through-holes, was carried out in a refined formulation. A significant reduction and smoothing of the stresses of the edge effect in the layers of three-layer shells with non-through cutouts compared with through cut due to the redistribution of the load was revealed, since a significant part of it is taken over by layers with undisturbed continuity.
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24 March 2020
There was a mistake in the affiliations. The right affiliation is “Institute of Applied Mechanics of the Russian Academy of Sciences, Leningradskii pr. 7, Moscow, 125040 Russia.”
References
V. N. Bakulin, I. F. Obraztsov, and V. A. Potopakhin, Dynamic Problems of the Nonlinear Theory of Multilayer Shells: Effect of Intensive Thermal-Force Loads, Concentrated Energy Flows (Fizmatlit, Moscow, 1998) [in Russian].
V. N. Bakulin and A. V. Ostrik, The Complex Effect of Radiation and Particles on Thin-walled Structures with Heterogeneous Coatings (Fizmatlit, Moscow, 2015) [in Russian].
V.V. Vasiliev, Mechanics of Structures made of composite materials (Mashinostroenie, Moscow, 1988) [in Russian].
Ya. M. Grigorenko and A. Ya. Grigorenko, “Static and Dynamic Problems for Anisotropic Inhomogeneous Shells with Variable Parameters and Their Numerical Solution (Review),” Prikl. Mekh. 49(2), 3–70 (2013) [Int. App. Mech. (Engl. Transl.) 49 (2), 123–193 (2013)].
V. N. Paimushin, “Theory of Moderately Large Deflections of Sandwich Shells Having a Transversely Soft Core and Reinforced Along Their Contour,” Mech. Comp. Mat. 53(1), 3–26 (2017).
E. I. Grigolyuk and F. A. Kogan, “The Basic Mathematical Models of the Deformation and Strength of Multilayer Anisotropic Shells,” in Applied Problems of the Mechanics of Thin-Walled Structures. Collection of Scientific Articles of the Institute of Mechanics MGU (MGU, Moscow, 2000), pp. 56–109.
A. N. Guz’, I. S. Chernyshenko, Val. N. Chekhov, et al., “Investigations in the Theory of thin Shells with Openings (Review),” Prikl. Mekh. 15(11), 3–37 (1979) [Int. App. Mech. (Engl. Transl.) 15 (11), 1015–1043 (1979)].
A. N. Guz’, I. S. Chernyshenko, Val. N. Chekhov, et al., Theory of Thin Shells Weakened by Apertures, Vol. 1: Computation Methods for Shells (Naukova Dumka, Kiev, 1980) [in Russian].
V. A. Salo, Static Boundary-Value Problems for Shells with Holes (Nats. Tekhn. Univ. “KhHPI,” Kharkov, 2003) [in Russian].
V. N. Bakulin and V. P. Revenko, “Analytical and Numerical Method of Finite Bodies for Calculation of Cylindrical Orthotropic Shell with Rectangular Hole,” Izv. Vys. Uch. Zav. Math., No. 6, 3–14 (2016) [Rus. Math. (Engl. Transl.) 60 (6), (2016)].
M. I. Dlugach, G. D. Gavrilenko, “Grid Calculations on Ribbed Cylindrical Shells with Large Rectangular Holes,” Prikl. Mekh. 11(12), 25–30 (1975) [Sov. App. Mech. (Engl. Transl.) 11 (12), 1015–1043 (1975)].
M. I. Dlugach and N. V. Koval’chuk “The Finite Element Method Applied to the Calculation of Cylindrical Shells with Rectangular Holes,” Prikl. Mekh. 9(11), 35–41 (1973) [Sov. App. Mech. (Engl. Transl.) 9 (11), 1180–1185 (1973)].
V. S. Morozov, “Numerical Calculation of the Displacement Field of a Cantilever Cylindrical Shell with a Rectangular Cut in Lateral Bending,” in Numerical and Experimental Methods for Studying the Strength, Stability and Vibrations of Aircraft Structures (MAI, Moscow, 1983), pp. 47–52 [in Russian].
V. N. Bakulin and V. V. Repinsky, “On the Effect of the Dimensions of a Rectangular Cutout on the Stress-Strain State of a Circular Cylindrical Shell,” in Numerical Methods for Studying the Durability of Aircraft. Thematic Collection of Scientific Papers (MAI, Moscow, 1988), pp. 5–10 [in Russian].
V. N. Bakulin and S. L. Snesarev, “Natural Vibrations of Cylindrical Shells with Rectangular Cutout,” Izv. VUZ. Avia. Tekh., No. 4, 3–6 (1988).
I. M. Pirogov, V. P. Yumatov, and S. M. Kutepov, “Experimental Investigation of the Stresses in the Region of a Rectangular Cutout in a Plexiglas Cylindrical Shell,” in Sb. Tr. Vses. Zaoch. Pol. Inst., No. 81, 139–196 (1973) [in Russian].
V. V. Vorobei, “Deformability of an Impregnated Fiberglas Shell Reinforced Around a Hole,” Prikl. Mekh. 15(1), 82–85 (1979) [Sov. App. Mech. (Engl. Transl.) 15 (1), 63–66 (1979)].
V. N. Bakulin, T. L. Martynovich, and V. P. Revenko, “Calculation of the Stress State of a Cylindrical Composite Shell with a Rectangular Hole,” in Proceedings of the Scientific and Technical Conference “The Use of Composite Materials on Polymer and Metal Matrices in Mechanical Engineering,” Ufa, USSR, 1985 (Ufa, 1985), pp. 80–81.
I. N. Preobrazhenskii, Yu. L. Golda, and V. G. Dmitriev, “Numerical Method of Studying the Stress-Strain State of Flexible Composite Shells of Revolution Weakened by Notches of Different Shapes,” Mekh. Komp. Mat., No. 6, 1030–1035 (1985) [Mech. Comp. Mat. (Engl. Transl.) 21 (6), 704–708 (1986)].
V. P. Revenko, “Analysis of the Stress-Strain State of a Non-Shallow Orthotropic Cylindrical Shell with an Elliptical Hole,” Prikl. Mekh. 24(4), 57–63 (1988) [Sov. App. Mech. (Engl. Transl.) 24 (4), 368–373 (1988)].
V. N. Bakulin, V. V. Repinsky, and S. L. Snesarev, “The Effect of the Reinforcing Lining on the Stress-Strain State of Orthotropic Cylindrical Shells with a Rectangular Cut,” in Numerical Methods for Studying the Durability of Aircraft. Thematic Collection of Scientific Papers (MAI, Moscow, 1989), pp. 4–6 [in Russian].
G. A. Van Fo Fy and A. A. Savichenko, “Stress State Around a Circular Cutout in a Spherical Sandwich Shell,” Prikl. Mekh. 6(8), 112–116 (1970) [Sov. App. Mech. (Engl. Transl.) 6 (8), 897–900 (1970)].
G. A. Van Fo Fy and A. I. Zhalilo, in Design and Construction of Articles Made of Glass Plastic (Naukova Dumka, Kiev, 1970), pp. 79–106 [in Russian].
G. A. Vanin and A. A. Savichenko, “Interference of Two Holes on the Stressed State in a Three-Layered Spherical Shell,” Prikl. Mekh. 11(12), 15–21 (1975) [Sov. App. Mech. (Engl. Transl.) 11 (12), 1260–1264 (1975)].
A. A. Savichenko, “Effect of Shear Deformation of the Stressed State of a Three-Layer Spherical Shell Weakened by an Aperture,” Prikl. Mekh. 12(3), 47–54 (1976) [Sov. App. Mech. (Engl. Transl.) 12(3), 250–256 (1976)].
B. L. Pelekh and A. A. Syas’kii, Stress Distribution near Apertures in Anisotropic Shells Pliable to Shear (Naukova Dumka, Kiev, 1975) [in Russian].
K. B. Aksentyan and I. A. Krasnobaev, “The Basic Equations of Bending and the Calculation Method of a Circular Three-Layer Cylindrical Shell with a Large Rectangular Cut,” in Theory of Shells and Plates (Nauka, Moscow, 1973), pp. 601–605 [in Russian].
K. B. Aksentyan and I. A. Krasnobaev, “Calculation of a Circular Three-Layer Cylindrical Shell with a Large Rectangular Cut,” Izv. VUZ. Str. Arhk., No. (2), 45–51 (1973).
V. N. Bakulin, A. P. Dyachina, T. L. Martynovich, et al., “An Experimental and Theoretical Study of the Axial Compression Problem of a Three-Layer Composite Cylindrical Shell Weakened by Rectangular Holes,” in Proceedings of All-Union Conference “Modern Problems of Structural Mechanics and Durability of Aircraft,” Moscow, USSR, 1989, (MAI, Moscow, 1989), pp. 4–6 [in Russian].
N. A. Alfutov, P. A. Zinoviev, and B. G. Popov, Calculation of Multilayer Plates and Shells of Composite Materials (Mashinostroenie, Moscow, 1984) [in Russian].
V. N. Bakulin, The Finite Element Method for Studying the Stress Strain State of Three-Layer Cylindrical Shells (CNII Informacii, Moscow, 1985) [in Russian].
A. O. Rasskazov, I. I. Sokolovskaya, and N. A. Shulga, Theory and Calculation of Layered Orthotropic Plates and Shells (Vysshaya Shkola, Kiev, 1986) [in Russian].
V. G. Piskunov, V. E. Verizhenko, V. K. Prisyazhnyuk, V. K. Sipetov, et. al. Calculation of Non-Uniform Flat Shells and Plates by the Finite Element Method (Vysshaya Shkola, Kiev, 1987) [in Russian].
V. N. Bakulin and A. A. Rassoha, The Finite Element Method and Holographic Interferometry in the Mechanics of Composites (Mashinostroenie, Moscow, 1987) [in Russian].
R. B. Rickards, The Finite Element Method in the Theory of Shells and Plates (Zinatne, Riga, 1988) [in Russian].
A. I. Golovanov, O. N. Tyuleneva, and A. F. Shigabutdinov, The Finite Element Method in Statics and Dynamics of Thin-Walled Structures (Fizmatlit, Moscow, 2006) [in Russian].
V. N. Bakulin, “A Corrected Model of Layer-by-Layer Analysis of Three-Layer Irregular Conical Shells,” Dokl. Ros. Akad. Nauk 472(3), 272–277 (2017) [Dokl. Phys. (Engl. Transl.) 62 (1), 37–41 (2017)].
V. N. Bakulin, “An Efficient Model for Layer-by-Layer Analysis of Sandwich Irregular Cylindrical Shells of Revolution,” Dokl. Ros. Akad. Nauk 478(2), 148–152 (2018) [Dokl. Phys. (Engl. Transl.) 63 (1), 23–27 (2018)].
V. N. Bakulin, “Block Finite-Element Model of Layer-by-Layer Analysis of the Stress Strain State of Three-Layer Generally Irregular Shells of Double-Curvature Revolution,” Dokl. Ros. Akad. Nauk 484(1), 35–40 (2019) [Dokl. Phys. (Engl. Transl.) 64 (1), 9–13 (2018)]
G. Kantin and R. V. Klauf, “Curved Discrete Elements of a Cylindrical Shell,” Raket. Tekh. Kosmon., No. 6, 82–86 (1968).
V. N. Bakulin, “Three-Layered Finite Element of Natural Curvature,” Izv. VUZ. Mash., No. 5, 5–10 (1978).
L. P. Zheleznov and V. V. Kabanov, “Functions of Displacements of Finite Elements of the Rotation Shell as Solids,” Izv. Akad. Nauk. SSSR Mekh. Tv. Tela, No., 131–136 (1990). [Mech. Sol. (Engl. Transl.)].
V. N. Bakulin, “Construction of Approximations for Modeling the Stress Strain State of Carrier Layers and Filler Layers of Three-Layer Nonaxisymmetric Cylindrical Shells,” Mat. Mod. 18(8), 101–110 (2006).
V. N. Bakulin “Effective Models for the Refined Analysis of the Deformed State of Three-Layer Nonaxisymmetric Cylindrical Shells,” Dokl. Ross. Akad. Nauk 414(5), 613–617 (2007) [Dokl. Phys. (Engl. Transl.) 52 (6), 330–334 (2007)].
V. N. Bakulin, “Construction of Approximations and Models for the Study of SSS Three-Layer Nonaxisymmetric Cylindrical Shells,” Mat. Model. 19(12), 118–128 (2007).
V. N. Bakulin and V. O. Kalendin, “On the Approach to the Construction of Finite Element Approximation for the Effective Solution of Problems of the Theory of Layered Shells,” in Proceedings of 3rdAll-Union Conference of Mechanics of Heterogeneous Ftructures, Lviv, 1991 (Lviv, Institute of Applied Problems of Mechanics and Mathematics of AS USSR, Lviv, 1991), pp. 17–18.
V. O. Kaledin and S. V. Shpital, “The Choice of the Design Scheme for the Study of the Axisymmetric Edge Effect in Three-Layered Cylindrical Shells with Lightweight Aggregate,” Mekh. Komp. Mat., No. 5, 657–665 (1993).
I. F. Obraztsov and V. N. Bakulin, “Updated Models for Studies of the Stressed-Strained State of Sandwich Cylindrical Shells,” Dokl. Ros. Akad. Nauk 407(1), 36–39 (2006) [Dokl. Phys. (Engl. Transl.) 51 (1), 138–131 (2006)].
V. N. Bakulin, “Finite-Element Model for Analysis of Stress-Strained State of Sandwich Shells,” Mat. Mod. 18(1), 3–9 (2006).
V. N. Bakulin, “Testing a Finite Element Model Designed to Study the Stress Strain State of Layered Irregular Shells,” Mat. Mod. 21(8), 121–128 (2009).
V. V. Novozhilov, Theory of thin shells (Sudpromgiz, Leningrad, 1951) [in Russain].
V. V. Repinsky, “Effective Finite Elements for Calculating the Stability of thin Anisotropic Shells of Revolution,” Vopr. Obor. Teck. Ser. 15. Iss. 1(117), 3–7 (1997).
V. N. Bakulin, V. S. Krivtsov, and A. A. Rassokha, “Algorithm for Deriving the Finiteelement Stiffness Matrix for an Anisotropic Shell,” Izv. VUZ. Avia. Tekh., No. 4, 14–18 (1983).
V. N. Bakulin, V. S. Krivtsov, A. A. Rassokha “Algorithm for Deriving the Finiteelement Stiffness Matrix for an Anisotropic Shell,” Izv. VUZ. Avia. Tekh., No. 4, 14–18 (1983).
V. A. Postnov and I. Ya. Kharkhurim, Finite Element Method in Ship Structure Computations (Sudostroenie, Leningrad, 1974) [in Russian].
V. N. Bakulin and V. V. Repinsky, “Calculation of Conical Shells Under Local Loads by Finite Element Method,” in Proceedings of the XIX International Conference on Computational Mechanics and Modern Applied Software Systems, May 25–31, 2010, Alushta (MAI, Moscow, 2015), pp. 206–208 [in Russian].
V. N. Bakulin, “Block-Based Finite Element Model for Layer-Analysis of Stressed Strain State of Three-Layered Shells with Irregular Structure,” Izv. Ros. Akad. Nauk. Mekh. Tv. Tela, No. 4, 66–73 (2018) [Mech. Sol. (Engl. Transl.) 53 (4) 411–417 (2018)].
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The work was carried out as part of a state assignment, topic state registration number AAAA-A19-119012290177-0.
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Russian Text © Author(s), 2019, published in Izvestiya Akademii Nauk, Mekhanika Tverdogo Tela, 2019, No. 2, pp. 64–73.
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Bakulin, V.N. Layer-by-Layer Analysis of the Stress-Strain State of Three-Layer Shells with Cutouts. Mech. Solids 54, 448–460 (2019). https://doi.org/10.3103/S0025654419020092
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DOI: https://doi.org/10.3103/S0025654419020092