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Tytuł artykułu

Elastic modules identification by layered composite beams testing

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Wybrane pełne teksty z tego czasopisma
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Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
Purpose: The study aims to predict elastic properties of composite laminated plates from the measured mechanical properties. Design/methodology/approach: Elastic constants of laminates and damping properties have been determined by using an identification procedure based on experiment design, and multi-level theoretical approach. Findings: The present paper is the first attempt at proposing a novel adaptive procedure to derive stiffness parameters from forced sandwich plate’s vibration experiments. Research limitations/implications: In the future the extension of the present approach to sandwich plates with different core materials will be performed in order to test various experimental conditions. Practical implications: Structures composed of laminated materials are among the most important structures used in modern engineering and especially in the aerospace industry. Such lightweight and highly reinforced structures are also being increasingly used in civil, mechanical and transportation engineering applications. Originality/value: The main advantage of the present method is that it does not rely on strong assumptions on the model of the plate. The key feature is that the raw models can be applied at different vibration conditions of the plate by a suitable analytical ore approximation method
Rocznik
Strony
14--22
Opis fizyczny
Bibliogr. 26 poz., rys., tab.
Twórcy
autor
  • National University “Lvov Polytechnical Equipment”, 12 Bandera street, Lvov, Ukraine
autor
  • National University “Lvov Polytechnical Equipment”, 12 Bandera street, Lvov, Ukraine
Bibliografia
  • [1] D. Ross, E.E. Ungar, E.M. Kerwin, Damping of plate flexural vibrations by means of viscoelastic laminate, ASME, Structural Damping, 1959, 49-88.
  • [2] R.A. Di Taranto, Theory of vibratory bending for elastic and viscoelastic layered finite length beams // Transactions of the ASME, Journal of Applied Mechanics 32 (1965) 881-886.
  • [3] D.J. Mead, S. Markus The forced vibration of a three-layer, damped sandwich beam with arbitrary boundary conditions, Journal of Sound and Vibration 10/2 (1969) 163-175.
  • [4] S. Srinivas, C.V. Joga Rao, A.K. Rao, Flexural vibration of rectangular plates, Journal of Applied Mechanics 23 (1970) 430-436.
  • [5] K.H. Lo, R.M. Christensen, E.M. Wu, A High-Order Theory of Plate Deformation. Part 2: Laminated Plates, Journal of Applied Mechanics 44 (1977) 669-676.
  • [6] S. Karczmaryk, An Analytical model of flexural vibration and the bending of plane viscoelastic composite structures, Warsaw University of Technology, Scientific Works, Mechanic, 172, Warsaw, 1999, 159.
  • [7] N.J. Pagano, Exact solutions for composite laminates in cylindrical bending, Journal of Composite Materials 3 (1969) 398-411.
  • [8] M.K. Rao, Y.M. Desai, Analytical solutions for vibrations of laminated and sandwich plates using mixed theory, Composite Structures 63 (2004) 361-373.
  • [9] Ya. M. Grigorenko, A. T. Vasilenko, Theory of Shells of Variable Rigidity. Methods of Calculation of Shells, 1981 (in Russian).
  • [10] H. Heng, B. Salim, P.-F. Michel, D. El Mustafa, Review and assessment of various theories for modeling sandwich composites, Composite Structures 84 (2008) 282-292.
  • [11] E. Carrera, Historical review of zig-zag theories for multilayered plates and shells, Applied Mechanics Reviews 56 (2003) 287-308.
  • [12] M.P. Sheremetjev, B.L. Pelekh, To refined plate theory construction, Engineering Journal 4 (1964) 504-510 (in Russian).
  • [13] B.L. Pelekh, B.M. Diveiev, Some dynamic problems for viscoelastic anisotropic envelopes and plates. 1. The generalized dynamic equations of the theory of stratified shells in view of boundary conditions on surfaces, Mechanics of Composite Materials 2 (1980) 277-280 (in Russian).
  • [14] B.L. Pelekh, B.M. Diveiev, Some dynamic problems for viscoelastic anisotropic shells and plates. 2. An impedance of viscoelastic anisotropic shells and plates, Mechanics of Composite Materials (1980) 546-548 (in Russian).
  • [15] B. Diveiev, One approach for calculating of laminated structures. Lviv, 1991. - 53p. - (Preprint /AS USSR, Institute of applied problem of mechanic and mathematic, 16-90) (in Ukrainian).
  • [16] B.M. Diveyev, M.M. Nykolyshyn, Refined Numerical Schemes for a Stressed-Strained State of Structural Joints of Layered Elements, Journal of Mathematical Sciences 107/1 (2001) 130.
  • [17] B. Diveyev, Z.V. Stotsko, V. Topilnyckyj, Dynamic properties identification for laminated plates, Journal of Achievements in Materials and Manufacturing Engineering 20/1-2 (2007) 237-230.
  • [18] B. Diveyev, M.J. Crocker, Dynamic Properties and Damping Prediction for Laminated Plates, Proceeding of International Conference on Noise and Vibration Engineering (ISMA-2006), Katholieke Universiteit Leuven, Belgium. 2006, 1021-1028.
  • [19] E.V. Morozov, V.V. Vasiliev, Determination of the shear modulus of orthotropic materials from off-axis tension tests, Composite Structures 62 (2003) 379-382.
  • [20] M. Greediac, E. Toussaint, F. Pierron, Special virtual fields for the direct determination of material parameters with the virtual fields method. 1. Principle and definition, International Journal of Solids and Structures 39/10 (2002) 2691-2705.
  • [21] A.L. Araujo, C.M. Mota Soares, M.J. Moreira de Freitas, P. Pedersen, J. Herskovits, Combined numerical-experimental model for the identification of mechanical properties of laminated structures, Composite Structures 50 (2000) 363-372.
  • [22] R. Rikards, A. Chate, A. Gailis, Identification of elastic properties of laminates based on experimental design, International Journal of Solids and Structures 38 (2001) 5097-5115.
  • [23] R. Honysz, S. Fassois. On the identification of composite beam dynamics based upon experimental data. Journal of Achievements in Materials and Manufacturing Engineering 16/1-2 (2006) 114-123.
  • [24] B. Diveyev, I. Butiter, N. Shcherbina, Identifying the elastic moduli of composite plates by using high-order theories. Pt 1. Theoretical approach, Mechanics of Composite Materials 44/1 (2008) 25-36.
  • [25] B. Diveyev, I. Butiter, N. Shcherbina, Identifying the elastic moduli of composite plates by using high-order theories. Pt 2. Theoretical-experimental approach” Mechanics of Composite Materials 44/2 (2008) 139-144.
  • [26] I. Butiter, B. Diveyev, I. Kogut, M. Marchuk, N. Shcherbina, Identification of elastic moduli of composite beams by using combined criteria. Mechanics of Composite Materials 48 (2013) 639-648.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-b4942f70-9a1d-46cc-8c6f-5738065823be
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