Hostname: page-component-77c89778f8-rkxrd Total loading time: 0 Render date: 2024-07-21T09:18:58.512Z Has data issue: false hasContentIssue false
  • English
  • Français

Effects of geometrical and material parameters on free vibration analysis of fiber metal laminated plates

Published online by Cambridge University Press:  14 August 2013

Faramarz Ashenai Ghasemi ,
Reza Paknejad  and
Keramat Malekzadeh Fard
Faramarz Ashenai Ghasemi*
Affiliation:
Department of Mechanical Engineering, Shahid Rajaee Teacher Training University (SRTTU), Lavizan, Postal Code 16788-15811, Tehran, Iran
Reza Paknejad
Affiliation:
Department of Mechanical Engineering, Shahid Rajaee Teacher Training University (SRTTU), Lavizan, Postal Code 16788-15811, Tehran, Iran
Keramat Malekzadeh Fard
Affiliation:
Center of Excellence for Research in Advanced Materials and Structures, Department of Mechanical Engineering, MUT University of Technology, Tehran, Iran
*
a Corresponding author: [email protected]
Get access

Abstract

Fiber metal laminates (FMLs) are high-performance hybrid structures based on alternating stacked arrangements of fiber-reinforced plastic (FRP) plies and metal alloy layers. In this paper, effect of some geometrical and material parameters on free vibrations of FML plates was studied. The first-order shear deformation theory (FSDT) as well as the Fourier series method was used to analytically solve the governing equations of the composite plate. The accuracy of the used method was verified by comparing the Rayleigh-Ritz analytical method and the ABAQUS finite element software (numerical) method. The results indicated that some of the important parameters like sequence of metal layers, aspect ratio (a/b) of plate and orientation of composite fibers were important factors affecting free vibration of the FMLs.

Keywords

Free vibrationfiber reinforced metal laminates (FMLs)fiber reinforced plastic (FRP)analytical methodfirst shear deformation theory
Type
Research Article
Information
Mechanics & Industry , Volume 14 , Issue 4 , 2013 , pp. 229 - 238
Copyright
© AFM, EDP Sciences 2013

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

Asundi, A., Choi, A.Y.N., Fiber metal laminates: an advanced material for future aircraft, Mater. Process. Technol. 63 (1997) 384–93 CrossRefGoogle Scholar
Vlot, A., Vogelesang, L.B., De Vries, Towards application of fiber metal laminates in large aircraft, Aircraft Eng. Aerospace Technol. 71 (1999) 558–70 CrossRefGoogle Scholar
Marsh, G., Airframes exploit composites in battle for supremacy, Reinforced Plastics 49 (2005) 26–32 CrossRefGoogle Scholar
Ngo-Cong, D., Mai-Duy, N., Karunasena, W., Tran-Cong, T., Free vibration analysis of laminated composite plates based on FSDT using one-dimensional IRBFN method, Comput. Struct. 85 (2011) 1–13 CrossRefGoogle Scholar
Xing, Y.F., Liu, B., New exact solution for free vibrations of orthotropic rectangular plates, Compos. Struct. 89 (2009) 567–74 CrossRefGoogle Scholar
Ganapathi, M., Kalyani, A., Mondal, B., Prakash, T., Free vibration analysis of simply supported composite laminated panels, Compos. Struct. 90 (2009) 100–03 CrossRefGoogle Scholar
Leissa, A.W., Martin, A.F., Vibration and buckling of rectangular composite plates with variable fiber spacing, Compos. Struct. 14 (1990) 339–57 CrossRefGoogle Scholar
Xiang, Y., Reddy, J.N., Natural vibration of rectangular plates with an internal line hing using the first order shear deformation plate theory, Sound Vib. 263 (2003) 285–97 CrossRefGoogle Scholar
Reddy, J.N., Kuppusamy, T., Natural vibrations of laminated anisotropic plates, Sound Vib. 94 (1984) 63–69 CrossRefGoogle Scholar
Thai, H.T., Kim, S.E., Free vibration of laminated composite plates using two variable refined plate theory, Mech. Sci. 52 (2010) 626–33 CrossRefGoogle Scholar
Aagaah, M.R., Mahinfalah, M., Jazar, G.N., Natural frequency of laminated composite plates using third order shear deformation theory, Compos. Struct. 72 (2006) 273–9 CrossRefGoogle Scholar
Swaminathan, K., Patil, S., Analytical solutions using a higher order refined computational model with 12 degrees of freedom for the free vibration analysis of antisymmetric angle-ply plates, Compos. Struct. 82 (2008) 209–16 CrossRefGoogle Scholar
Mishara, I., Kumar Sahu, Sh., An experimental approach to free vibration response of woven fiber composite plates under free-free boundary condition, Adv. Tech. Civil Eng. 1 (2012) 67–72 Google Scholar
K.M. Dutt, H.K. Shivanand, An experimental approach to free vibration response of carbon composite laminates, Adv. Eng. Appli. (2011) 66–68
Lee, S.Y., Park, T., Free vibration of laminated composite skew plates with central cutout, Struct. Eng. Mech. 31 (2009) 587–683 CrossRefGoogle Scholar
Civalek, Ö., Free vibration analysis of symmetrically laminated composite plates with first-order shear deformation theory (FSDT) by discrete singular convolution method, Finite Elements in Analysis and Design 44 (2008) 725–31 CrossRefGoogle Scholar
Thai, H.T., Kim, S.E., Free vibration of laminated composite plates using two variable refined plate theory, Mech. Sci. 52 (2010) 626–33 CrossRefGoogle Scholar
Hatami, S., Azhari, M., Saadatpour, M.M., Free vibration of moving laminated composite plates, Compos. Struct. 80 (2007) 609–20 CrossRefGoogle Scholar
Xiang, S., Wang, K.M., Free vibration analysis of symmetric laminated composite plates by trigonometric shear deformation theory and inverse multiquadric RBF, Thin-Walled Struct. 47 (2009) 304–10 CrossRefGoogle Scholar
Topal, U., Uzman, Ü., Free vibration analysis of laminated plates using first-order shear deformation theory, Springer Proceedings in Physics 111 (2007) 493–98 CrossRefGoogle Scholar
Zhen, W., Wanji, C., Free vibration of laminated composite and sandwich plates using global-local higher-order theory, Sound Vib. 298 (2006) 333–49 CrossRefGoogle Scholar
Withney, J.M., Pagano, N.J., Shear deformation in heterogeneous anisotropic plates, Appl. Mech. 37 (1970) 1031–36 CrossRefGoogle Scholar
Mindlin, R.D., Influence of rotary inertia and shear on flexural motions of isotropic elastic plates, Appl. Mech. 18 (1951) 31–38 Google Scholar
Christoforou, A.P., Swanson, S.R., Analysis of impact response in composite plates, Solids Struct. 27 (1991) 161–70 CrossRefGoogle Scholar
Khalili, S.M.R., Shokuhfar, A., Ashenai Ghasemi, F., Effect of smart stiffening procedure on low-velocity impact response of smart structures, Mater. Process. Technol. 190 (2007) 142–52 CrossRefGoogle Scholar
Carvalho, A., Soares, C.G., Dynamic response of rectangular plates of composite materials subjected to impact loads, Compos. Struct. 34 (1996) 55–63 CrossRefGoogle Scholar
Liew, K.M., Vibration of symmetrically laminated cantilever trapezoidal composite plates, Mech. Sci. 34 (1992) 299–308 CrossRefGoogle Scholar
Wong, W.O., The effects of distributed mass loading on plate vibration behavior, Sound Vib. 252 (2002) 577–83 CrossRefGoogle Scholar
L. Meirovitch, Fundamental of Vibrations, McGraw-Hill, New York, 2001
Bhat, R.H., Natural frequencies of rectangular plates using characteristic orthogonal polynomials in Rayleigh-Ritz method, Sound Vib. 102 (1985) 493–99 CrossRefGoogle Scholar
Christoforou, A.P., Yigit, A.S., Characterization of impact in composite plates, Compos. Struct. 43 (1998) 15–24 CrossRefGoogle Scholar
Payeganeh, G.H., Ashenai Ghasemi, F., Malekzadeh, K., Dynamic response of fiber-metal laminates (FMLs) subjected to low-velocity impact, Thin-Walled Struct. 48 (2010) 62–70 CrossRefGoogle Scholar