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Mode frequency analysis of antisymmetric angle-ply laminated composite stiffened hypar shell with cutout

Identyfikatory
Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
This article deals with finite element method for the analysis of antisymmetric angle-ply laminated composite hypar shells (hyperbolic paraboloid bounded by straight edges) that applies an eight-noded isoparametric shell element and a three-noded beam element to study the mode-frequency analysis of stiffened shell with cutout. Two-, 4-, and 10-layered antisymmetric angle-ply laminations with different lamination angles are considered. Among these, 10-layer antisymmetric angle-ply shells are considered for elaborate study. The shells have different boundary conditions along its four edges. The formulation is based on the first-order shear deformation theory. The reduced method of eigen value solution is chosen for the undamped free vibration analysis. The first five modes of natural frequency are presented. The numerical studies are conducted to determine the effects of width-to-thickness ratio (b/h), degree of orthotropy (E11/E22), and fiber orientation angle (θ) on the nondimensional natural frequency. The results reveal that free vibration behavior mainly depends on the number of boundary constraints rather than other parametric variations such as change in fiber orientation angle and increase in degree of orthotropy and widthto-thickness ratio.
Rocznik
Strony
162--171
Opis fizyczny
Bibliogr. 26 poz., rys., wykr.
Twórcy
  • Department of Civil Engineering, Heritage Institute of Technology, Kolkata 700107, India
  • Department of Mechanical Engineering, Jadavpur University, Kolkata 700032, India
  • Department of Civil Engineering, Heritage Institute of Technology, Kolkata 700107, India
Bibliografia
  • [1] Chakravorty, D., Bandyopadhyay, J.N., Sinha, P.K.: Applications of FEM on free and forced vibrations of laminated shells, ASCE J. Engg. Mech.,124(1), 1-8, 1998.
  • [2] Rikards R., Chate A., Ozolinsh O.: Analysis for buckling and vibrations of composite stiffened shells and plates, Composite Struct.,51, 361-370, 2001.
  • [3] Nayak, A.N., Bandyopadhyay, J.N.: Free vibration analysis and design aids of stiffened conoidal shells, ASCE J. Engg. Mech.,128(4), 419-427, 2002.
  • [4] Nayak, A.N., Bandyopadhyay, J.N.: On the free vibration of stiffened shallow shells, J. Sound and Vibr.,255(2), 357-382, 2002.
  • [5] Nayak, A.N., Bandyopadhyay, J.N.: Free vibration analysis of laminated stiffened shells. ASCE J. Engg. Mech., 131(1), 100-105, 2005.
  • [6] Nayak, A.N., Bandyopadhyay, J.N.: Dynamic response analysis of stiffened conoidal shells,J. Sound and Vibr.,291, 1288-1297, 2006.
  • [7] Sahoo, S., Chakravorty, D.: Finite element vibration characteristics of composite hypar shallow shells with various edge supports, J. Vibr. Control,11, 1291-1309, 2005.
  • [8] Sahoo, S., Chakravorty, D.: Stiffened composite hypar shell roofs under free vibration: behaviour and optimization aids. J. Sound and Vibr.,295, 362-377, 2006.
  • [9] Pradyumna, S., Bandyopadhyay, J.N.: Free vibration analysis of functionally graded curved panels using a higher order finite element formulation, J. Sound and Vibr.,318, 176-192, 2008.
  • [10] Kumar, A., Bhargava, P., Chakrabarti, A.: Natural Frequencies and mode shape of laminated composite skew hypar shells with complicated boundary conditions using finite element method, Adv. Mat. Res., 585, 44-48, 2012.
  • [11] Kumar, A., Bhargava, P., Chakrabarti, A.: Vibration of laminated composite skew hypar shells using higher order theory, Thin Walled Structures,63, 82-90, 2013.
  • [12] Kumar, A., Chakrabarti, A., Bhargava, P.: Vibration analysis of laminated composite skew cylindrical shells using higher order shear deformation theory, J. Vib. Control,21(4), 725-735, 2015.
  • [13] GulshanTaj, M.N.A., Chakraborty, A.: Dynamic response of functionally graded skew shell panel, Latin Amer. J. Solids Struct.,10, 1243-1266, 2013.
  • [14] Tornabene, F., Fantuzzi, N., Bacciocchi, M., Dimitri, R.: Dynamic analysis of thick and thin elliptic shell structures made of laminated composite materials, Compos. Struct.,133, 278-299, 2015.
  • [15] Dey, S.,Mukhopadhyay, T., Adhikari, S.: Stochastic free vibration analyses of composite shallow doubly curved shells-A Kriging model approach, Composite: Part B, 70, 99-112, 2015.
  • [16] Zhang, C., Jin G., Ma, X., Ye, T.: Vibration analysis of circular cylindrical double-shell structures under general coupling and end boundary conditions, Appl. Acoustics, 110, 176-193, 2016.
  • [17] Sahoo, S.: Behaviour and optimization aids of composite stiffened hypar shell roofs with cutout under free vibration, ISRN Civil Engg., ID 989785, 1-14, 2012.
  • [18] Sahoo, S.: Dynamic characters of stiffened composite conoidal shell roofs with cutouts: Design aids and selection guidelines, J. Engg., ID 230120, 1-18, 2013.
  • [19] Sahoo, S.: Free vibration of laminated composite stiffened saddle shell roofs with cutouts, IOSR J. Mech. Civil Engg., ICAET, 30-34, 2014.
  • [20] Sahoo, S.: Laminated composite stiffened shallow spherical panels with cutouts under free vibration - a finite element approach, Engg. Sci. Tech., An Int. J.,17(4), 247-259, 2014.
  • [21] Sahoo, S.: Free vibration behavior of laminated composite stiffened elliptic paraboloidal shell panel with cutout, Curved and Layered Struct.,2(1), 162-182, 2015.
  • [22] Sahoo, S.: Laminated composite stiffened cylindrical shell panels with cutouts under free vibration, Int. J. Manuf. Mat. Mech.Engg.,5(3), 37-63, 2015.
  • [23] Sahoo, S.: Performance evaluation of free vibration of laminated composite stiffened hyperbolic paraboloid shell panel with cutout, Int. J. Engg. Technol.,7, 1-24, 2016.
  • [24] Topal, U.: Mode-frequency analysis of laminated spherical shell, Proceedings of the 2006 IJME. INTERTECH International Conference-Session ENG P501-001, Kean University, NJ; 19-21 October 2006.
  • [25] Srinivasa, C.V., Suresh Y.J., Prema Kumar, W.P.: Experimental and finite element studies on free vibration of cylindrical skew panels, Int. J. Advanced Struct. Engg., 6(1), 1-11, 2014.
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Uwagi
Opracowanie rekordu w ramach umowy 509/P-DUN/2018 ze środków MNiSW przeznaczonych na działalność upowszechniającą naukę (2019).
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-8b8d1060-f33a-4eb5-9b25-f7de64c676a5
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