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1.
International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395 -0056 Volume: 04 Issue: 01 | Jan -2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 907 Static and Transient Vibrational Analysis of Functionally Graded Material Anil Kumar1, Dr. D K Maiti2 1Postgraduate, Dept. of Aerospace Engineering, Indian Institute of Technology-Kharagpur, West Bengal, India 2 Professor, Dept. of Aerospace Engineering, Indian Institute of Technology-Kharagpur, West Bengal, India ---------------------------------------------------------------------***--------------------------------------------------------------------- Abstract - In the present work, Static and Transient vibrational analysis of Functionally Graded Materials under mechanical load are investigated in thermal environment. Functionally Graded Material (FGM) is a class of composite material, usually mixture of Ceramic and Metals. Thematerial properties are assumed to vary continuously through their thickness according to a Power-law distribution. Finite element method is used to study the Static, Free Vibration and Transient vibrational analyses. The numerical results on the transverse deflection in a moderately thick functionally graded plate under uniformly distributed load for various boundary conditions are discussed. The effects of Power-law index for Al/ZrO2 Functionally Graded plates on deflectionare commented. Different geometrical shapes of Al/ZrO2 Functionally Graded shells and panels are included to study the free vibration; the effect of volume fractions on their frequency characteristics is discussed. Isotropic plate and Si3N4/SUS304 Functionally Graded square platesareincluded in the study of transient vibration analysis in thermal environment and the effect of Power-law index is discussed in detail. Key Words: Functionally Graded Material, FGM, Transient Vibrational Analysis, FGM Plates, FGM Shells and Panels, Al/ZrO2 FGM, Si3N4/SUS304 FGM 1. INTRODUCTION Strength of the metal is reduced after it has been in high temperature environment for a period of time; beside metal has a low melting point. Other side, ceramic materials have excellent characteristics in strength and heat-resistance. Due to their low toughness their applications are usually limited. Composite materials have been widely used in aerospace structural components, automobile industries and many other industrial applications, due to their high specific strength, high specific stiffness, anti-corrosion ability, workability, low density, superior performance reliability, ease in fabrication of complex shapes and several other attributes. But the composite materials have some limitations such as the weakness of interfaces between layers that to de-lamination, extremethermal loadsthatmay lead to de-bonding between matrix and fibre due to mismatch of mechanical properties, residual stresses that may be present due to difference in coefficients of thermal expansion of the fibre and the matrix, etc. A new class of materials known as Functionally Graded Materials (FGMs) was proposed in 1980's which overcome the limitations that were found in traditional composite. FGMs are microscopically inhomogeneous composites usually made from a mixture of metals and ceramics. By gradually varying the volume fraction of constituent materials, their material properties exhibit a smooth and continuous change from one surface to another, thus eliminating interfaceproblemsandmitigatingthermal stress concentrations, which are very common in traditional composites. For various applications, the FGM approach has been explored to mitigate some of the major problems associated with development of a sharp interface at the join of two dissimilar materials. FGMs are usually more superior to the conventional laminated materials because of no discernable internal interfaces or boundaries, and no internal stress peaks are caused when external loads are applied and thus failure from interfacial debonding or from stress concentration can be avoided. The continuous change in the microstructureofFunctionally Graded Material (FGM) distinguishes them from the fibre- reinforced laminatedcompositematerials.AnFGMconsistof ceramic on the outside surface exposed to high temperature provides thermal resistance due to its low thermal conductivity while the metallic constituent provides toughness of the plate, that provides thermal corrosion protection and load carrying capability. The FGM are ideal for applications involving severe thermal gradients, ranging from thermal structures in advanced aircraft and aerospace engines to computer circuit boards. Fig -1: Conventional heat resistant material and FGM
2.
International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395 -0056 Volume: 04 Issue: 01 | Jan -2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 908 On the macroscopic scale, FGMs are anisotropic, inhomogeneous andpossess spatiallycontinuousmechanical properties, which bring the conventional mechanics into a brand-new field. It is extremely complex to manufacture the FGM materials with fully specified profiles of material gradations due to the large number of parameters involved in fabrication such as dispersions in microstructure, volume fraction, porosity etc. Functionally Graded Materials have been used by nature for eons. Bamboo is an excellent example of FGM, where the microstructure consists of a spatially varying concentration of voids and pores in order to maximize bendingrigidity,and bending strength, while minimizing mass. Bone has similar Functional Grading, while even human skin is graded to provide certain toughness, tactile and elastic qualities. 2. LITERATURE REVIEW A brief review of the important literature related to static, dynamic and transient analysis of functionally graded structures is carried out and presented in the following section. The technique of grading ceramics along with metals initiated by the Japanese material scientist in Sendai has marked the beginning of exploring the possibility of using FGMs for various structural applications [1]. Since the concept of FGM was first proposed, FGMs have been extensively studied by researchers, who have mainly focused on thermo-elastic behavior. Trung-kien Nguyen et al[2] are proposed the First Order Shear Deformation plate model for modeling structures made of functionally graded material. The material properties of functionally graded material areassumedtobe isotropic at each point and vary through the thickness according to a power law distribution. Kadoli et al[3] studied the static behaviour of FGM beams by using higher order shear deformation theory underambient temperature. This study reveal that, depending on whether the loading is on the ceramic rich face or metal rich face of the beam, the static deflection and the static stresses in the beam do not remain the same. Mohammad Talha et al[4] are studied Free vibration and static analysis of functionally graded material (FGM) plates using higher order shear deformation theory. They presented numerical results for different thickness ratios, aspect ratios and volume fraction index with different boundary conditions. For a given thickness ratio non- dimensional deflection increases as the volume fraction index increases. It is concluded that the gradient in the material properties plays a vital role in determining the response of the FGM plates. Based on the First order Shear deformation Theory (FSDT), Francesco Tornabene et al[5] presented the dynamic behaviour of moderately thick functionally gradedshellsand annular plates. The solution is obtained by using numerical technique termed as Generalized Differential Qudrature (GDQ) method. Numerical results illustrate the influence of power law exponent of shell and panel structure which are considered. Xiao-Lin Huang et al[6] presented the non linear Vibration and Dynamic response of functionallygradedmaterial plates in thermal environments. They used higher-order shear deformation plate theory and general von Karman-type equation, which includes thermal effects. The results reveal that the temperature field and volume fraction distribution have significant effect on the nonlinear vibration and dynamic response of the functionally graded plate. 3. MATHEMATICAL FORMULATION The determination of accurate linear behavior of the FGMs are largely depends on the theory used to model the structure. The classical plate theory (CLPT) that is based on the Kirchoff hypothesis may be inaccurate for analysis of FGM plates in which the volume fractions of two or more materials are varied continuously as a functionofpositionin thickness direction. The inaccuracy occurs due to neglecting the effects of transverse shear and normal strains in the plate. To take the effects of gradual change in material properties, the first order shear deformation theory (FSDT) may be considered. Since in the FSDT model the transverse shear strains are assumed to be constant in the thickness direction, therefore the shear correction factor have to be incorporated to adjust the transverse shear stiffness, in order to study the static or dynamic problems ofFGMplates. The accuracy of solutions of the FSDT model depends on the shear correction factors. In the present analysis shear correction factor is taken as 5/6. To reduce the computational effort, the FGM plate has been divided into finite number of imaginary layers. 3.1 First Order Shear Deformation Theory The first order shear deformation theory (FSDT) is used to describe the kinematics of deformation for the present analysis. The displacement components(u,v,w)atanypoint (x, y, z) along three perpendicular directions are expressed as follows: 0 0 0 ( , , , ) ( , , ) ( , , ) ( , , , ) ( , , ) ( , , ) ( , , , ) ( , , ) ( , , ) x y z u x y z t u x y t z x y t v x y z t v x y t z x y t w x y z t w x y t z x y t Where u, v and w are the displacements in the x, y, and z directions, while x, y and z are the rotations. These equations can be expressed in the matrix form as ' [ ]u z u
3.
International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395 -0056 Volume: 04 Issue: 01 | Jan -2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 909 Strain-displacement relation: 0 0 0 0 0 0 xx xx x yy yy y zz zz xy xy xy yz yz yz xz xz xz zk zk zk zk zk Where xx, yy, zz, xy etc. are engineering strain components and 0 xx, 0 yy, 0 zz, 0 xy etc. are generalized strain components and are expressed in terms of displacements (u0, v0,w0,x,y, z) In case of Functionally Graded Materials,material properties such as modulus of elasticity (E), Poisson ratio (), density () etc. are continuously vary through their thickness. This variation is assumed to according to a power-law distribution of the volume fractionsoftheplateconstituents. 3.2 Power -Law Function Fig -2: Functionally Graded Plate Power law function is used in the present analysis. Power law distribution in conjunction with simple law of constituent mixture as follows: 1 ( ) , 2 n c z V h (1 )m cV V Where, Vc and Vm are volume fraction of ceramic and metal respectively, z = distance from mid-surface and n = power law index, a positive real number. The effective material properties Peff are evaluated using the relation, ( , ) (T)V (z)+P (T)V ( )eff m m c cP z T P z Where, Pm and Pc stands for material properties of metals and ceramics respectively. The effective material properties of the plate, including young’s modulus E and thermal expansion (α), vary according toabove equation.Density (ρ), Poisson ratio (v) and thermal conductivity K are assumed to be independent of temperature, the above equation as follows ( ) V (z)+P V ( )eff m m c cP z P z 3.3 Energy equation The present analysis involves structural displacementsdueto external mechanical loading. The total energy of the system can thus be considered as strain energy due to mechanical loading and the kinetic energy due to inertial effects. 3.3.1 Strain energy The strain energy due to mechanical strain for plate is expressed as 1 { } [ ]{ } 2 T v U Q dv Where v is the volume of the plate 3.3.2 Kinetic energy The kinetic energy is expressed as . . . .1 1 { } ( ){ } { } [ ]{ } 2 2 T T e v A T u z u dv u u dA and ( )z is the mass density at given depth z and A is the area of the plate. 3.3.3 Potential energy The potential energy is expressed as { } { }T eW u p dA Where, {p} is the surface force vector 3.3.4 Variational principle for dynamic problem The fundamental equations of the present analysis are derived from the Hamilton's variational principle. The Hamilton’s principle states that the variation of the Lagrangian during any time interval t1 to t2 must be equal to zero 2 1 ( ) 0 t e e t T U W dt
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International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395 -0056 Volume: 04 Issue: 01 | Jan -2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 910 Using above equations all together, the global equilibrium equations are obtained after assembling Equations with respect to the global axes. .. [ ]{ } [ ]{ } { }M d K d F Where [M] and [K] are global mass and stiffness matrices and{ }d , .. { }d and{ }F are global displacement, acceleration and force vectors, respectively. It is already mention that the FGM structures mostly exposed to thermal environments. Then the governing equation written including thermal load vector {Ft} as, .. [ ]{ } [ ]{ } { } { } tM d K d F F 4. STATIC ANALYSIS OF FUNCTIONALLY GRADED PLATE FGM are meant for use where temperature fluctuations are severe. However, their performanceforloadsunderambient conditions is also necessary to be investigated since, there can exist situations where temperature fluctuations may be present for a short duration. Hence it is essential to examine the static behaviour of functionally graded plates. The governing equilibrium equation for the static analysis without thermal load can be written as [ ]{ } { }K d F Where, [ ]K is the stiffness matrix 4.1 Transverse deflection of Thick FGM Plate In this section, Transverse deflection characteristics for various plates such as ceramic ZrO2 (Zirconia), metal Al (Aluminum) and functionally graded material (Al/ZrO2) were examined. The material propertiesofceramic ZrO2 and metal Al are given in table 1. The variation of young’s modulus of FGM (Al/ZrO2) with Power Law index n=1, n=2 and n=5 are shown in Fig -3. Table -1: Material properties of Al/ ZrO2 FGM Component Material Young’s modulus (E) Gpa Density (ρ) kg/m3 Poison’s Ratio (υ) Aluminum (Al) 70 2707 0.3 Zirconia (ZrO2) 151 5700 0.3 Fig -3: Variation of Al/ZrO2 FGM’s young’s modulus with layer number A Functionally Graded plate ( Al/ZrO2) with SCSC (S-Simply supported, C-Clamped) boundary condition is subjected to unit distributed load and it’s aspect ratio and thicknessratio are taken as a/b=0.5 and a/h=20 respectively. Fig -4: Comparison central deflection along length with reference [4] Central deflection of Al/ ZrO2 FGM plate with CCFF (C- Clamped, F- Free) boundary condition under unit UDL presented below.
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International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395 -0056 Volume: 04 Issue: 01 | Jan -2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 911 Fig -5: Central deflection of Al /ZrO2 FGM plate along length under unit UDL Table -2: Comparison of Present study with Ferriera[8] Aspect Ratio(a/b) Al/Zro2 FGM plate with n=1 Deflection (W). ANSYS Ferriera et al[8] 0.5 0.112846 0.1626 1 0.677966 0.7352 2 1.505 1.9062 From Fig -4, it can be observed that, the difference between present and reference [4] results because reference[4]used higher order shear deformation theory to solvetheproblem. FGM is assumed as finite number of layers where each layer treated as homogeneous and isotropic. These assumptions may cause some non linearity in material gradation. From Fig -5, the central deflection profile increases with increasing Power Law index (n) because metal content increases with increasing Power Law index. Table -2 shows that the comparison of maximum central deflection of Al/ZrO2 FGM plate with CFCF boundaryconditionunderunit uniformly distributed load with reference [8] 5. FREE VIBRATION ANALYSIS OF FUNCTIONALLY GRADED CONICAL, CYLINDRICAL SHELLS AND ANNULAR PLATE The study of free vibration behavior is very important to analyze the transient response of graded materials which will help in designing sensors and actuators to control vibrations.Aluminum/Zirconia FunctionallyGradedMaterial is used to analyze present study, the material properties are given in Table 1. The governing equation for free vibration analysis is given below, .. [ ]{ } [ ]{ } 0 M d K d Where [M] and [K] are global mass and stiffness matrices and{ }d , .. { }d are global displacement and acceleration respectively. 5.1 Free Vibration of Functionally Graded Annular Plate In this section, free vibration of Al/ZrO2 FunctionallyGraded annular plate with C-F (C-Clamped, F- Free) boundary condition is analyzed. The first 6 natural frequencies and mode shapes are verified with available literature. Annular plate(C-F): Rb=0.5m, h=0.1m Re-Rb=1.5m, where Re is external radius. Rb is internal radius. Table -3: Comparison of Present study with Tornabene[5] Mode shape Al/ZrO2, n=1 ZrO2, n=0 Al, n=∞ A B A B A B 1 66.543 68.71 70.203 70.13 65.758 65.59 2 121.11 124.95 127.67 127.5 119.59 119.4 3 3 121.11 124.95 127.67 127.5 119.59 119.4 3 4 202.17 208.35 213.14 212.58 199.65 199.1 2 5 202.17 208.35 213.14 212.58 199.65 199.1 2 6 283.29 291.13 298.66 296.99 279.75 278.1 9 A- Present study B- Reference[5], Percentage error= 2.6- 3.15% Fig -6: First 6 mode shapes of Functionally Graded annular plate Mode 1 Mode 2 Mode 3 Mode 4 Mode 5 Mode 6
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International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395 -0056 Volume: 04 Issue: 01 | Jan -2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 912 5.2 Free Vibration of Functionally Graded Cylinder and Conical dome In this section, free vibration of Al/ZrO2 FunctionallyGraded cylinder and conical shell with C-F boundary condition is analyzed. The first 5 natural frequencies and mode shapes are given below. Cylinder(C-F): Rb=1m, h=0.1m and L0=2m Where L0 is length of cylinder Rb is radius of cylinder Conical dome(C-F): Rb=0.5m, h=0.1m and L0=2m Where L0 is length of conical dome Rb is radius of bottom portion Table -4: First 5 natural frequencies of Functionally Graded Cylinder with C-F boundary condition Mode shape ZrO2, n=0 Al/ ZrO2, n=1 Al, n=∞ 1 151.72 147.56 142.11 2 151.72 147.56 142.11 3 219.27 211.34 205.39 4 219.27 211.34 205.39 5 253.90 248.00 237.82 Fig -7: First 5 mode shapes of Functionally Graded Cylinder with C-F boundary condition Table -5: First 5 natural frequencies of Functionally Graded Conical dome with C-F boundary condition Mode shape ZrO2, n=0 Al/ ZrO2, n=1 Al, n=∞ 1 209.76 204.78 196.47 2 209.80 204.78 196.52 3 231.9 224.24 217.21 4 231.9 224.25 217.22 5 287.79 276.53 269.57 Fig -8: First 5 mode shapes of Functionally Graded conical dome with C-F boundary condition Table -3 shows the comparison of first 6 natural frequencies of annular plate with Tornabene[5]. The percentage difference betweenpresentstudyandTornabene[5]because the reference solutionisobtainedbyGeneralizedDifferential Quadrature(GDQ) numerical technique. From Table -4 and 5, the natural frequencies are given for cylinder and conical dome. The natural frequencies from ceramic to metal (i.e. n=0 to n= ∞) decreaseswithincreasing Power law index for various FGM geometries. 6. TRANSIENT VIBRATION ANALYSIS OF FUNCTIONALLY GRADED MATERIAL Transient response analysis is the most general method for computing forced dynamic response. The study of dynamic behavior of FGM plate is very much important for the design of advanced structure. The governing equation for transient analysis with thermal effect can be written as, .. * [ ]{ } [ ]{ } { }M d K d F Mode 1 Mode 2 Mode 3 Mode 4 Mode 6 Mode 1 Mode 2 Mode 3 Mode 4 Mode 5
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International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395 -0056 Volume: 04 Issue: 01 | Jan -2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 913 Where, [K*] Includes thermal preload as geometric stiffness The above problem becomes transient when themechanical force, {F} varies with time. It is solved by using Newmark’s method. 6.1 Transient Response of Isotropic Square Plate Transient response of a simply supported square plate subjected to a suddenly applied load is compared with available literature [15]. Transient response is carried out with time step Δt = 0.005 and capturing response over a period 0.25 sec. Isotropic square plate properties: Length a =283.8 cm Thickness h= 0.635 cm Poison’s ratio (υ) = 0.25 Young’s modulus (E) = 7.031×105 kg/cm2 Density (ρ) = 2.547×10-6 kg sce2/cm4 Load (q) = 4.882×10-4 kg/cm2 Fig -9: Comparison of transient response of isotropic plate with Reference [15] 6.2 Transient Response of Si3N4/SUS304 FGMPlate In this section, Si3N4/SUS304 functionally graded plate’s transient response is analyzed with time step Δt=2μs. Si3N4/SUS304 functionally graded plate is subjected 400K and 300K temperature to ceramic (Si3N4, Top) and Metal (SUS304, Bottom) respectively.Asuddenpressureof50Mpa is applied in ceramic surface and capturing response is shown below. Material properties and time step are taken from reference [14] Table -6: Material properties of Si3N4/SUS304 FGM Material Young’s modulus (E) Gpa Density (ρ) kg/m3 k Poison’s Ratio (υ) Si3N4 322 Gpa 2370 9.19 W/mK 0.3 SUS304 193Gpa 8166 12.04W/mK 0.3 Si3N4/SUS304 functionally graded plate (SSB): Length (a) =0.2 m Thickness (h) = 0.025m Applied loads: Pressure (q0) = -50 Mpa Tt =400K Tb =300K Fig -10: Transient response of Si3N4/SUS304 Functionally Graded plate (n=1) under thermal environment Fig -11: Transient response oftheSi3N4 (n=0)underthermal environment
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International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395 -0056 Volume: 04 Issue: 01 | Jan -2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 914 Fig -12: Transient response of the SUS304 (n= ∞) under thermal environment Numerical analysis carriedoutwithsameloadandboundary conditions with different Power Law index i.e. n=0, 1 and ∞. Above Fig -10, 11 and 12 results state that the amplitude of vibration is maximum for the metallic plate and a minimum for the ceramic plate. The amplitude of vibration increases smoothly as the amount of metal in the plate increases. Also, it is clear that the frequency of vibration of the ceramic plates is much higher than that of the metallic plates. The natural frequencies are reduced by increasing Power law index n and temperature rise. 7. CONCLUSION The static, free vibration and transient vibration analysis is carried out to investigate the performance of Functionally Graded Material due to mechanical load. From the static analysis itwasobservedthatforFunctionally Graded plates of Al/ZrO2, the deflections for given boundary conditions increases with increasing Power law index. From the free vibration analysis, it isfoundthatasthePower Law index (n) increases, the frequencies of all modes decreases. This effect is independent of geometrical shape. The transient analysis states that the amplitude of vibration is maximum for the metallic plate and a minimum for the ceramic plate. The natural frequencies are reduced by increasing Power law index nandtemperaturerise.Also,itis clear that the frequency of vibration of the ceramic plates is much higher than that of the metallic plates. REFERENCES [1] M. Yamanouchi, T.Hirai, I.Shiota, Overall view of the P/M fabrication of functionally graded materials, in: Proceedings of the First International SymposiumonFGMs,Sendai,Japan, 1990, pp. 59-64. [2] Trung-Kien Nguyen, Karam Sab and Guy Bonnet, First order shear deformation plate models for functionally graded material, Composite Structures 83 (2008) 25–36, Available online 20 March 2007. [3] Ravikiran Kadoli , Kashif Akhtar , N. Ganesan, Static analysis of functionally graded beams using higher order shear deformation theory, Applied Mathematical Modelling 32 (2008) 2509–2525. [4] Mohammad Talha, B.N. Singh, Static response and free vibration analysis of FGM plates using higher order shear deformation theory, Applied Mathematical Modelling 34 (2010) 3991–4011. [5] Francesco Tornabene, Free vibration analysis of FG conical, cylindrical shell and annular plate structures with a four- parameter power law distribution, Comput.Methods Appl.Mech.Engrg.198 (2009) 2911-2935. [6] X L Huang, H S Shen, Nonlinear vibration and dynamic response of FGP in thermal environment, International Journal of solid structures 41(2004) 2403-2427. [7]J.N.Reddy, Analysis of FGPs, International Journal for Numerical Methods in Engineering 47 (2000) 663-684. [8]A.J.M. Ferreira, R.C. Batra, C.M.C. Roque, L.F. Qian,P.A.L.S. Martins, Static analysis of functionally graded plates using third order shear deformation theory and a meshless method, Compos. Struct. 69 (2005) 449–457. [9] Da-Guang Zhang, You-He Zhou, A theoretical analysis of FGM thin plates based on physical neutral surface, Computational Materials Science 44 (2008) 716–720 [10] R.K. Kapania, S. Raciti, Recent advances in analysis of laminated beams and plates, Part I: Shear effect and Buckling, AIAA J. 27 (7) (1989) 923–934. [11] X. Zhao, Y. Y. Lee and K. M. Liew, Mechanical and thermal buckling analysis of functionally graded plate, Composite Structures 90 (2009) 161–171, Available online 13 March 2009. [12] A.M. Zenkour, Generalisedsheardeformationtheory for bending analysis of functionally graded plates, Appl. Math. Model. 30 (2006) 67–84. [13] H.Matsunaga, Freevibrationandstabilityoffunctionally graded plates according to a 2-D higher-order deformation theory, Composite Structures 82 (2008)499–512. [14] G.N. Praveen, J.N. Reddy, Nonlinear transient thermo elastic analysis of functionally graded ceramic-metal plates, International Journal of Solids and Structures 35 (1998) 4457-4476. [15] H U Akay, Dynamic large deflection analysis of plates using mixed finite elements, Computers & Structures Vol. 11(1980), pp 1-11.
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