Abstract
In this study, the buckling and free vibration behavior of tapered functionally graded material (FGM) sandwich columns is explored. The connections are considered to be semi-rigid. The core material is functionally graded along the beam depth according to the simple power law form. Euler–Bernoulli beam theory and the Ritz method will be employed to derive the governing equations. Legendre polynomials are chosen as auxiliary functions. After reducing the order of Euler’s buckling equation, an Emden–Fowler differential equation will be obtained. To reach a closed-form solution, the flexural rigidity of the column will be approximated with an exponential function by enforcing least-squares method. Non-dimensional natural frequencies and critical buckling loads will be presented for various cross-sectional types. The effects of FGM power, taper ratio, and spring rigidities on the critical buckling loads, and natural frequencies will be also investigated. Numerical results for various boundary conditions and configurations reveal the high accuracy of authors’ scheme.
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Abbreviations
- E :
-
Modulus of elasticity
- \(\rho\) :
-
Density
- \({V_{\text{m}}}\) :
-
Volume fraction of metal phase
- \(h\) :
-
Height of the core
- \({h_{\text{f}}}\) :
-
Thickness of the facings
- p :
-
FGM power
- \(\Omega\) :
-
Taper parameter
- \(\lambda\) :
-
Taper ratio
- u :
-
Longitudinal displacement
- w :
-
Transverse displacement
- \({C_{\text{t}}}\) :
-
Transitional spring rigidity factor
- \({C_{\text{r}}}\) :
-
Rotational spring rigidity factor
- \(\overline {\omega }\) :
-
Normalized natural frequency
- \({Q^{\text{i}}}\) :
-
Constitutive coefficient
- \(\nu\) :
-
Poisson’s ratio
- \({\varepsilon ^*}\) :
-
Fitness error
- \(\alpha ,\beta\) :
-
Constants of the exponential flexural rigidity function
- J, Y :
-
Bessel functions of second order
- \(\mu\) :
-
Normalized buckling parameter
- L :
-
Length of the column
- \(\dot {u},\dot {w}\) :
-
Velocity
- C :
-
Integration constants
- A :
-
Cross-sectional area
- \(\xi\) :
-
Rotational spring rigidity ratio
- \(\psi\) :
-
Transitional spring rigidity
- \(\eta\) :
-
Flexural rigidity coefficient
- \({\overline {P} _{Cr}}\) :
-
Normalized critical buckling load
- H :
-
Total height of the cross section at \(x=0\)
- g :
-
Shape function
- \({L_{\text{j}}}\) :
-
Legendre polynomial
- K :
-
Stiffness matrix
- M :
-
Mass matrix
- \({U_{{\text{int}}}}\) :
-
Strain energy
- V :
-
External energy
- \({K_{\text{e}}}\) :
-
Kinetic energy
- \(\Pi\) :
-
Total potential energy
- \(I\) :
-
Moment of inertia
- P :
-
Compressive load
- \({P_{{\text{Cr}}}}\) :
-
Critical buckling load
- \(\omega\) :
-
Natural frequency
- \(\sigma\) :
-
Axial stress
- \(\varepsilon\) :
-
Axial strain
- t :
-
Time
- \(\gamma\) :
-
Shear strain
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Appendices
Appendix A
The coefficients \({\eta _1}\)–\({\eta _4}\) of Eq. (12) are simplified and given in a closed form below:
Appendix B
Herein, the Bessel functions appeared in Eq. (23) are presented:
In the Bessel relations, \(\Gamma\) denotes the gamma function. It is obvious that these harmonic functions lead to sinusoidal and cosinusoidal functions under certain circumstances.
Appendix C
The determinant of coefficients matrix given in Eq. (25) in a closed form is:
Appendix D
The entries of the coefficient matrix of Eq. (25) together with the correlation coefficient are expressed by the following:
Appendix E
The shifted Legendre polynomials are given by the following:
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Rezaiee-Pajand, M., Mokhtari, M. & Masoodi, A.R. Stability and free vibration analysis of tapered sandwich columns with functionally graded core and flexible connections. CEAS Aeronaut J 9, 629–648 (2018). https://doi.org/10.1007/s13272-018-0311-6
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DOI: https://doi.org/10.1007/s13272-018-0311-6