Spline collocation method for free vibration analysis of laminated shallow shells https://doi.org/10.33108/visnyk_tntu2018.02.060

Main Article Content

Oleg Pavlenko

Abstract

The presented study deals with free vibration of cross-ply symmetrically laminated composite doubly-curved panels with constant thickness. Based on the first-order shear deformation theory (FSDT) the equations of motion are derived by applying the Hamilton’s principle. Spline function approximation technique, which includes B-splines of the third order, is used to reduce two-dimensional system of coupled differential equations in terms of displacement and rotational functions to one-dimensional. A generalized eigenvalue problem is obtained by applying a point collocation method with suitable boundary conditions. The vector-matrix form of
the governing equations with different boundary conditions, from which values of a frequency parameter is obtained, is presented. These systems of ordinary differential equations are solved using the Godunov's discrete orthogonalization method. The effects of curvature ratio and thickness-to-length ratio on the fundamental natural
frequencies of composite doubly-curved panels with all sides simply supported are investigated. In order to verify the accuracy of the employed method the frequency parameters are evaluated in comparison with the previous paper available in the literature. Good agreement with other available data demonstrates the capability and
reliability of the spline collocation method and the adopted composite doubly-curved shell model used.

Article Details

Section

Articles

References

1. Kreja I.A. A literature review on computational models for laminated composite and sandwich panels. Central European Journal of Engineering, 2011, vol. 1, no. 1, pp. 59 – 80.

2. Qatu M.S., Sullivan R.W., Wang W. Recent research advances on the dynamic analysis of composite shells: 2000-2009. Composite Structures, 2010, vol. 93, no. 1, pp. 14 – 31.

https://doi.org/10.1016/j.compstruct.2010.05.014

3. Sayyad A.S., Ghugal Yu.M. On the free vibration analysis of laminated composite and sandwich plates: A review of recent literature with some numerical results. Composite Structures, 2015, vol. 129, pp. 177 – 201.

https://doi.org/10.1016/j.compstruct.2015.04.007

4. Grigorenko Ya.M. Bespalova E. I., Kitajgorodskij A.B., Shinkar' A.I. Svobodnye kolebaniya e'lementov obolochechnyx konstrukcij. Kiev, Naukova dumka, 1986. 172 p. [In Russian].

5. Hryhorenko Ya.M., Budak V.D., Hryhorenko O.Ya. Rozviazannia zadach teorii obolonok na osnovi dyskretno-kontynualnykh metodiv: navchalnyi posibnyk. Mykolaiv, Ilion, 2010. 294 p. [In Ukrainian].

6. Grigorenko Ya.M., A. T. Vasilenko Metody rascheta obolochek. T. 4. Teoriya obolochek peremennoj zhestkosti. Kiev: Naukova dumka, 1981. 544 p. [In Russian].

7. Mallick P.K. Fiber-reinforced composites materials manufacturing and design. Dearborn, Michigan, CRC Press, 3rd ed., 2008. 638 p.

8. Qatu M.S. Vibration of laminated shells and plates. San Diego, CA: Elsevier, 2004. 385 p.

9. Reddy J.N. Mechanics of laminated composite plates and shells: theory and analysis. CRC Press, 2nd ed., 2004. 854 p.

https://doi.org/10.1201/b12409

10. Godunov S.K. O chislennom reshenii kraevyx zadach dlya sistem linejnyx obyknovennyx differencial'nyx uravnenij. Uspexi matematicheskix nauk, 1961, vol. 16, no. 3, pp. 171 – 174 [In Russian].