Abstract
Background
The end conditions, temperature gradient and geometric parameters affect the system stability.
Purpose
This research work concerns with the parametric instability study of a non-uniform asymmetric sandwich beam supported viscoelastically at the ends acted upon by a harmonic axial load and a variable temperature grade which is more appropriate along with a constant temperature grade.
Methods
Hamilton’s energy principle is used to develop the equations of motion and associated end conditions. Then the non-dimensional form of the equation of motion is obtained. Galerkin’s process is used to find a set of Hill’s equations. The parametric instability regions are acquired by means of Saito-Otomi conditions.
Results
The consequences of taper parameter, uniform as well as variable temperature grade, shear parameter, spring parameters and spring loss factors on the instability regions are examined and represented by a number of plots.
Conclusion
The results reveal that rise in the values of thermal gradient for bottom layer and shear parameter, make the beam more stable against harmonic load. Increase in the values of taper parameters and thermal gradient for top layer reduce the flexural rigidity of the system, hence worsen the system stability. The dynamic instability of the system reduces with increase in the values of spring loss factors and spring parameters.
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Abbreviations
- B :
-
Beam width
- \(l\) :
-
Beam length
- \(E_{i} \;\;\left( {i = 1,2,3} \right)\) :
-
Young’s Module, i = 1 for upper layer
- \(A_{i} \;\;\left( {i = 1,2,3} \right)\) :
-
i = 3 for bottom layer, cross sectional area
- \({{G_{2} } \mathord{\left/ {\vphantom {{G_{2} } {E_{i} \;\;\left( {i = 1,3} \right)}}} \right. \kern-0pt} {E_{i} \;\;\left( {i = 1,3} \right)}}\) :
-
The ratio of shear modulus of the core to the modulus of elasticity of the elastic layer
- \(\gamma_{2}\) :
-
Core shear strain
- \(2h_{i} \;\;\left( {i = 1,2,3} \right)\) :
-
Depth of the \(i\text{th}\) layer
- \(h_{31}\) :
-
\({{\left( {h_{3} } \right)_{0} } \mathord{\left/ {\vphantom {{\left( {h_{3} } \right)_{0} } {\left( {h_{1} } \right)}}} \right. \kern-0pt} {\left( {h_{1} } \right)}}_{0}\)
- \(h_{21}\) :
-
\({{\left( {h_{2} } \right)_{0} } \mathord{\left/ {\vphantom {{\left( {h_{2} } \right)_{0} } {\left( {h_{1} } \right)}}} \right. \kern-0pt} {\left( {h_{1} } \right)}}_{0}\)
- \(g^{*}\) :
-
\(g\left( { 1\, + \,j\eta } \right)\), shear parameter in complex form
- \(g\) :
-
Shear parameter
- \(I_{i} \;\;\left( {i = 1,2,3} \right)\) :
-
Area moment of inertia, \(i = 1\) for upper layer
- \(lh_{10}\) :
-
\({l \mathord{\left/ {\vphantom {l {\left( {h_{1} } \right)_{0} }}} \right. \kern-0pt} {\left( {h_{1} } \right)_{0} }}\)
- \(\overline{m}\) :
-
Mass/unit longitudinal dimension of beam
- \(\overline{{P_{1} }}\) :
-
Dynamic load amplitude
- \(w\,(x,t)\) :
-
Deflection of beam in transverse direction
- \(Y\) :
-
Geometric parameter
- \(\overline{t}\) :
-
Non-dimensional time
- t :
-
Time
- \(\overline{w}\) :
-
\(\frac{w}{l}\)
- \(\overline{w}^{\prime \prime }\) :
-
\(\frac{{\partial^{2} \overline{w} }}{{\partial \overline{x}^{2} }}\)
- \(\ddot{\overline{w}}\) :
-
\(\frac{{\partial^{2} \overline{w} }}{{\partial \overline{t}^{2} }}\)
- \(\overline{x}\) :
-
\(\frac{x}{l}\)
- \(U_{i,x}\) :
-
\(\frac{{\partial U_{i} }}{\partial x}\) (i = 1,3)
- \(\omega\) :
-
Frequency of forcing function
- \(\rho_{i}\) :
-
Density of ith layer
- \(\lambda\) :
-
Thermal expansion coefficient of beam material
- \(u^{\prime}_{1}\) :
-
\(\frac{{\partial u_{1} }}{\partial x}\)
- \(\overline{{u_{1} }}^{\prime \prime }\) :
-
\(\frac{{\partial^{2} \overline{u}_{1} }}{{\partial \overline{x}^{2} }}\)
- \(E\left( \xi \right)\) :
-
Modulus of elasticity at any section of beam
- δ :
-
Temperature gradient parameter
- \(E_{31}\) :
-
\({{E_{3} } \mathord{\left/ {\vphantom {{E_{3} } {E_{1} }}} \right. \kern-0pt} {E_{1} }}\)
- \(T\left( \xi \right)\) :
-
Distribution of elasticity modulus
- \(\overline{\omega }\) :
-
Non-dimensional forcing frequency
- \(\alpha\) :
-
\(\frac{{E_{1} \,A_{1} }}{{E_{3} \,A_{3}^{{}} }}\)
- \(\psi_{0}\) :
-
Reference temperature
- \(\alpha_{1}\), \(\alpha_{3}\) :
-
Taper parameters for top and bottom layer respectively
- \(\mu_{1}\) :
-
\({{\rho_{2} } \mathord{\left/ {\vphantom {{\rho_{2} } {\rho_{1} }}} \right. \kern-0pt} {\rho_{1} }}\)
- \(\mu_{2}\) :
-
\({{\rho_{2} } \mathord{\left/ {\vphantom {{\rho_{2} } {\rho_{3} }}} \right. \kern-0pt} {\rho_{3} }}\)
- \(\beta\) :
-
\({{\left( {h_{2} } \right)_{0} } \mathord{\left/ {\vphantom {{\left( {h_{2} } \right)_{0} } {\left( {h_{1} } \right)}}} \right. \kern-0pt} {\left( {h_{1} } \right)}}_{0}\)
- \(\eta_{{t_{2} }} ,\eta_{{r_{2} }}\) :
-
The spring loss at factors \(\overline{x} = 1\)
- \(\overline{k}_{{t_{1} }}^{*} ,\overline{k}_{{t_{2} }}^{*}\) :
-
Spring constants for the translational springs at \(\overline{x} = 0\) and \(\overline{x} = 1\)
- \(\overline{k}_{{\text{r}_{1} }}^{*} ,\overline{k}_{{\text{r}_{2} }}^{*}\) :
-
Spring constants for the rotational springs at \(\overline{x} = 0\) and \(\overline{x} = 1\)
- \(\eta_{{\text{t}_{1} }} ,\;\;\eta_{{\text{r}_{1} }}\) :
-
Spring loss factors at \(\overline{x} = 0\)
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Pradhan, M., Dash, P.R. Stability Study of a Sandwich Beam with Asymmetric and Non-uniform Configuration Supported Viscoelastically Under Variable Temperature Grade. J. Vib. Eng. Technol. 7, 149–157 (2019). https://doi.org/10.1007/s42417-019-00087-3
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DOI: https://doi.org/10.1007/s42417-019-00087-3