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Frontiers of Mechanical Engineering

ISSN 2095-0233

ISSN 2095-0241(Online)

CN 11-5984/TH

Postal Subscription Code 80-975

2018 Impact Factor: 0.989

Front Mech Eng    2011, Vol. 6 Issue (4) : 409-418    https://doi.org/10.1007/s11465-011-0245-8
RESEARCH ARTICLE
Dynamic analysis of composite beam subjected to harmonic moving load based on the third-order shear deformation theory
Mohammad Javad REZVANIL1(), Mohammad Hossein KARGARNOVIN2, Davood YOUNESIAN3
1. Department of Mechanical Engineering, Semnan Branch, Islamic Azad University, Semnan, Iran; 2. School of Mechanical Engineering, Sharif University of Technology, Tehran, Iran; 3. Railway Engineering Department, Iran University of Science and Technology, Tehran, Iran
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Abstract

The response of an infinite Timoshenko beam subjected to a harmonic moving load based on the third-order shear deformation theory (TSDT) is studied. The beam is made of laminated composite, and located on a Pasternak viscoelastic foundation. By using the principle of total minimum potential energy, the governing partial differential equations of motion are obtained. The solution is directed to compute the deflection and bending moment distribution along the length of the beam. Also, the effects of two types of composite materials, stiffness and shear layer viscosity coefficients of foundation, velocity and frequency of the moving load over the beam response are studied. In order to demonstrate the accuracy of the present method, the results TSDT are compared with the previously obtained results based on first-order shear deformation theory, with which good agreements are observed.

Keywords timoshenko composite beam      pasternak viscoelastic foundation      third-order shear deformation theory (TSDT)      harmonic moving load     
Corresponding Author(s): REZVANIL Mohammad Javad,Email:m.rezvani@semnaniau.ac.ir   
Issue Date: 05 December 2011
 Cite this article:   
Mohammad Javad REZVANIL,Mohammad Hossein KARGARNOVIN,Davood YOUNESIAN. Dynamic analysis of composite beam subjected to harmonic moving load based on the third-order shear deformation theory[J]. Front Mech Eng, 2011, 6(4): 409-418.
 URL:  
https://academic.hep.com.cn/fme/EN/10.1007/s11465-011-0245-8
https://academic.hep.com.cn/fme/EN/Y2011/V6/I4/409
Fig.1  Deformation of a transverse normal according to the FSDT and TSDT
Fig.2  Pasternak viscoelastic foundation with viscous shear layers
Number of layers/NWidth of layers b/cmAngle of layers θ/(o)Total thickness of the beam h/cm
45(0/90/90/0)10
Tab.1  Geometrical data for the composite layers beam
T300/5208Glass-epoxy
ρ1540 kg/m32000 kg/m3
E1132 GPa53.7 GPa
E210.8 GPa17.9 GPa
G125.65 GPa8.96 GPa
G133.38 GPa8.96 GPa
G233.38 GPa3.44 GPa
v120.240.25
v230.590.34
v130.590.25
Tab.2  Mechanical properties of composite materials
Rocking stiffness k?/(MN)Rocking damping η?/(N·s)Normal stiffness k/MPaNormal damping η/(kN·s·m-2)Shear viscosity μ/(kN·s)Load magnitude F/kNLoad velocity v/(m·s-1)Load frequency ω/Hz
13.8552069138100144.640200
Tab.3  The properties of the foundation
Fig.3  Deflection of T300/5208 composite beam, according to TSDT for different stiffness coefficients
Fig.4  Phase angle of the deflection
Fig.5  Deflection of T300/5208 composite beam, according to TSDT for different viscosity coefficients
Fig.6  Deflection of T300/5208 composite beam, according to TSDT for different load velocity
Fig.7  Deflection of T300/5208 composite beam, according to TSDT for different load frequency
Fig.8  Bending moment of T300/5208 composite beam, according to TSDT for different stiffness coefficients
Fig.9  Phase angle of the bending moment
Fig.10  Bending moment of T300/5208 composite beam, according to TSDT for different viscosity coefficients
Fig.11  Bending moment of T300/5208 composite beam, according to TSDT for different load velocity
Fig.12  Bending moment of T300/5208 composite beam, according to TSDT for different load frequency
Fig.13  Deflection of beam, according to TSDT for two types of composite materials
Fig.14  Bending moment of beam, according to TSDT for two types of composite materials
Fig.15  Deflection of composite beam based on the FSDT and TSDT
Fig.16  Bending moment of composite beam based on the FSDT and TSDT
Fig.17  Stress of composite beam based on the FSDT and TSDT
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