Hostname: page-component-586b7cd67f-t7czq Total loading time: 0 Render date: 2024-11-24T20:01:00.877Z Has data issue: false hasContentIssue false

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

Published online by Cambridge University Press:  14 August 2013

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 alternatingstacked arrangements of fiber-reinforced plastic (FRP) plies and metal alloy layers. Inthis paper, effect of some geometrical and material parameters on free vibrations of FMLplates was studied. The first-order shear deformation theory (FSDT) as well as the Fourierseries method was used to analytically solve the governing equations of the compositeplate. The accuracy of the used method was verified by comparing the Rayleigh-Ritzanalytical method and the ABAQUS finite element software (numerical) method. The resultsindicated that some of the important parameters like sequence of metal layers, aspectratio (a/b) of plate and orientation of compositefibers were important factors affecting free vibration of the FMLs.

Type
Research Article
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) 38493 CrossRefGoogle Scholar
Vlot, A., Vogelesang, L.B., De Vries, Towards application of fiber metal laminates in large aircraft, Aircraft Eng. Aerospace Technol. 71 (1999) 55870 CrossRefGoogle Scholar
Marsh, G., Airframes exploit composites in battle for supremacy, Reinforced Plastics 49 (2005) 2632 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) 113 CrossRefGoogle Scholar
Xing, Y.F., Liu, B., New exact solution for free vibrations of orthotropic rectangular plates, Compos. Struct. 89 (2009) 56774 CrossRefGoogle Scholar
Ganapathi, M., Kalyani, A., Mondal, B., Prakash, T., Free vibration analysis of simply supported composite laminated panels, Compos. Struct. 90 (2009) 10003 CrossRefGoogle Scholar
Leissa, A.W., Martin, A.F., Vibration and buckling of rectangular composite plates with variable fiber spacing, Compos. Struct. 14 (1990) 33957 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) 28597 CrossRefGoogle Scholar
Reddy, J.N., Kuppusamy, T., Natural vibrations of laminated anisotropic plates, Sound Vib. 94 (1984) 6369 CrossRefGoogle Scholar
Thai, H.T., Kim, S.E., Free vibration of laminated composite plates using two variable refined plate theory, Mech. Sci. 52 (2010) 62633 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) 2739 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) 20916 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) 6772 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) 587683 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) 72531 CrossRefGoogle Scholar
Thai, H.T., Kim, S.E., Free vibration of laminated composite plates using two variable refined plate theory, Mech. Sci. 52 (2010) 62633 CrossRefGoogle Scholar
Hatami, S., Azhari, M., Saadatpour, M.M., Free vibration of moving laminated composite plates, Compos. Struct. 80 (2007) 60920 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) 30410 CrossRefGoogle Scholar
Topal, U., Uzman, Ü., Free vibration analysis of laminated plates using first-order shear deformation theory, Springer Proceedings in Physics 111 (2007) 49398 CrossRefGoogle Scholar
Zhen, W., Wanji, C., Free vibration of laminated composite and sandwich plates using global-local higher-order theory, Sound Vib. 298 (2006) 33349 CrossRefGoogle Scholar
Withney, J.M., Pagano, N.J., Shear deformation in heterogeneous anisotropic plates, Appl. Mech. 37 (1970) 103136 CrossRefGoogle Scholar
Mindlin, R.D., Influence of rotary inertia and shear on flexural motions of isotropic elastic plates, Appl. Mech. 18 (1951) 3138 Google Scholar
Christoforou, A.P., Swanson, S.R., Analysis of impact response in composite plates, Solids Struct. 27 (1991) 16170 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) 14252 CrossRefGoogle Scholar
Carvalho, A., Soares, C.G., Dynamic response of rectangular plates of composite materials subjected to impact loads, Compos. Struct. 34 (1996) 5563 CrossRefGoogle Scholar
Liew, K.M., Vibration of symmetrically laminated cantilever trapezoidal composite plates, Mech. Sci. 34 (1992) 299308 CrossRefGoogle Scholar
Wong, W.O., The effects of distributed mass loading on plate vibration behavior, Sound Vib. 252 (2002) 57783 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) 49399 CrossRefGoogle Scholar
Christoforou, A.P., Yigit, A.S., Characterization of impact in composite plates, Compos. Struct. 43 (1998) 1524 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) 6270 CrossRefGoogle Scholar