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      KCI등재후보 SCIE SCOPUS

      Stochastic hygrothermoelectromechanical loaded post buckling analysis of piezoelectric laminated cylindrical shell panel

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      https://www.riss.kr/link?id=A104818851

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      다국어 초록 (Multilingual Abstract)

      The present work deals with second order statistics of post buckling response of piezoelectric laminated composite cylindrical shell panel subjected to hygro-thermo-electro-mechanical loading with random system properties. System parameters such as th...

      The present work deals with second order statistics of post buckling response of piezoelectric laminated composite cylindrical shell panel subjected to hygro-thermo-electro-mechanical loading with random system properties. System parameters such as the material properties, thermal expansion coefficients and lamina plate thickness are assumed to be independent of the temperature and electric field and modeled as random variables. The piezoelectric material is used in the forms of layers surface bonded on the layers of laminated composite shell panel. The mathematical formulation is based on higher order shear deformation shell theory (HSDT) with von-Karman nonlinear kinematics. A efficient C0 nonlinear finite element method based on direct iterative procedure in conjunction with a first order perturbation approach (FOPT) is developed for the implementation of the proposed problems in random environment and is employed to evaluate the second order statistics (mean and variance) of the post buckling load of piezoelectric laminated cylindrical shell panel. Typical numerical results are presented to examine the effect of various environmental conditions, amplitude ratios, electrical voltages, panel side to thickness ratios, aspect ratios, boundary conditions, curvature to side ratios, lamination schemes and types of loadings with random system properties. It is observed that the piezoelectric effect has a significant influence on the stochastic post buckling response of composite shell panel under various loading conditions and some new results are presented to demonstrate the applications of present work. The results obtained using the present solution approach is validated with those results available in the literature and also with independent Monte Carlo Simulation (MCS).

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      참고문헌 (Reference)

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      1 Akhras, G., "Three-dimensional thermal buckling analysis of piezoelectric antisymmetric angle-ply laminates using finite layer method" 92 (92): 31-38, 2010

      2 Xu, K., "Three dimensional analytical solutions for coupled thermoelectroelastic response of multilayered cylindrical shells" 34 (34): 802-812, 1996

      3 Oh, II-Kwon, "Thermopiezoelastic nonlinear dynamics of active piezolaminated plates" 14 (14): 823-845, 2005

      4 Shen, H. S., "Thermal post buckling analysis of laminated cylindrical shell with piezoelectric actuators" 55 (55): 13-22, 2002

      5 Lal, A., "Thermal buckling response of laminated composite plate with random system properties" 6 (6): 1-25, 2009

      6 Verma, V.K., "Thermal buckling of laminated composite plates with random geometric and material properties" 9 (9): 187-211, 2009

      7 Singh, B.N., "Thermal buckling of laminated composite conical shell panel with and without piezoelectric layer with random material properties" 14 (14): 73-81, 2009

      8 Panda, S.K., "Thermal Post-buckling behavior of laminated composite cylindrical/ hyperboloid shallow shell panel using nonlinear finite element method" 91 (91): 366-374, 2009

      9 Klieber, M., "The stochastic nite element method" Chichester 1992

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      45 Varelis, D., "Coupled finite element for non-linear laminated piezoelectric composite shells with applications to buckling and post buckling behavior" 19-22, 2004

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      47 Ganesan, N., "Buckling and dynamic analysis of piezothermoelastic composite cylindrical shell" 59 (59): 45-60, 2003

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      학술지 인용정보

      학술지 인용정보
      기준연도 WOS-KCI 통합IF(2년) KCIF(2년) KCIF(3년)
      2016 1.17 0.44 1.04
      KCIF(4년) KCIF(5년) 중심성지수(3년) 즉시성지수
      0.97 0.88 0.318 0.18
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