EXPLANATION OF FREQUENCY CROSS OVERS AND CORRESPONDING MODE SHAPE CHANGES IN THE FREE VIBRATION PROBLEM OF CLAMPED CYLINDRICAL PANELS

2003 ◽  
Vol 259 (3) ◽  
pp. 724-732 ◽  
Author(s):  
B. SIVASUBRAMONIAN ◽  
A.M. KULKARNI ◽  
G. VENKATESWARA RAO
2011 ◽  
Vol 393-395 ◽  
pp. 149-152
Author(s):  
Bao Ying Xing ◽  
Xiao Cong He ◽  
Mo Sheng Feng

This paper studies the influence of adhesive dimensions on the transverse free vibration of the single-lap adhesive cantilevered beams. The researches are performed by employing software ansys .Efficient analytic results of natural frequencies and mode shapes of transverse free vibration of the beams are provided, corresponding to different adhesive dimensions of bonded thicknesses and bondlines length. Bondlines length has more significant influence on the transverse natural frequencies and the lap joint’s mode shapes of the beams than bonded thickness. The transverse natural frequencies decrease with a decrease in the bondlines length of adhesive, but do not appear to variation observably with a decrease in the bonded thickness. Bondlines length shorting, the lap joint has a sharper mode shape. Simultaneously, the lap joint of even mode shapes influences the dynamic response of the beams significantly. These results indicate a local crack in adhesive layers because of the existence of stress concentration.


Author(s):  
Slaviša Šalinić ◽  
Aleksandar Obradović ◽  
Momčilo Dunjić ◽  
Dragan Sekulić ◽  
Željko Lazarević

2006 ◽  
Vol 84 (22-23) ◽  
pp. 1506-1518 ◽  
Author(s):  
M. D’Ottavio ◽  
D. Ballhause ◽  
B. Kröplin ◽  
E. Carrera

2005 ◽  
Vol 05 (03) ◽  
pp. 409-434 ◽  
Author(s):  
HUMAYUN R. H. KABIR ◽  
HASAN ASKAR

Presented here is an analytical solution to the free vibration problem of an isotropic cylindrical panel with SS2-type simply supported boundary conditions based on Reddy's third order shear deformation shell theory. Using the principle of virtual work, the Reddy's shell theory generates five highly coupled partial differential equations in terms of three unknown displacements and two unknown rotations. The partial differential equations in conjunction with the prescribed boundary conditions are solved using displacement functions expressed in terms of double Fourier series expansion. Cylindrical panels with various aspect and thickness ratios are considered in the study of convergence behavior and parametric variation of the eigenvalues. The eigenvalues and mode shapes obtained in this study are compared with those obtained from the finite element software package ANSYS. The hitherto unavailable analytical solutions can be used as benchmarks for checking the accuracy of various approximate methods such as the Rayleigh–Ritz, finite element and finite difference methods.


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