Vibration and buckling of tapered rectangular plates with two opposite edges simply supported and the other two edges elastically restrained against rotation

Abstract The paper describes an application of a method of power series expansions to the free vibration and buckling problems of isotropic rectangular plates with linear thickness variation. The plates are simply supported on the two opposite edges parallel to the direction of thickness variation and the other two edges are elastically restrained against rotation. By the present method, one can solve exactly the governing equation with variable coefficients. The choice of the origin for the power series expansion plays an important role in obtaining rapid convergence and accurate results. The effects of thickness variation and rotational stiffness of the elastic spring on the eigenvalues and mode shapes are shown numerically and graphically on the basis of new results obtained by the present exact analysis.

[1]  M. Mukhopadhyay,et al.  Free vibration of rectangular plates with edges having different degrees of rotational restraint , 1979 .

[2]  D. S. Chehil,et al.  Buckling of Rectangular Plates With General Variation in Thickness , 1973 .

[3]  P.A.A. Laura,et al.  Transverse vibration of a rectangular plate elastically restrained against rotation along three edges and free on the fourth edge , 1978 .

[4]  F. C. Appl,et al.  Fundamental Frequency of Simply Supported Rectangular Plates With Linearly Varying Thickness , 1965 .

[5]  T. Mizusawa,et al.  Vibration and buckling of rectangular plates with nonuniform elastic constraints in rotation , 1987 .

[6]  W. H. Wittrick,et al.  Buckling of Tapered Rectangular Plates in Compression , 1962 .

[7]  P.A.A. Laura,et al.  On the effect of different edge flexibility coefficients on transverse vibrations of thin, rectangular plates , 1978 .

[8]  P.A.A. Laura,et al.  A note on the determination of the fundamental frequency of vibration of thin, rectangular plates with edges possessing different rotational flexibility coefficients , 1977 .

[9]  P. Morse,et al.  Methods of theoretical physics , 1955 .

[10]  Hans H. Bleich,et al.  Buckling strength of metal structures , 1952 .

[11]  T. E. Carmichael,et al.  THE VIBRATION OF A RECTANGULAR PLATE WITH EDGES ELASTICALLY RESTRAINED AGAINST ROTATION , 1959 .

[12]  S. Timoshenko Theory of Elastic Stability , 1936 .

[13]  Eugene E. Lundquist,et al.  Critical Compressive Stress for Flat Rectangular Plates Supported Along all Edges and Elastically Restrained Against Rotation Along the Unloaded Edges, Special Report 189 , 1941 .

[14]  S. L. Edney,et al.  Vibrations of rectangular plates with elastically restrained edges , 1984 .

[15]  Variation of Tapered Plates by Finite Strip Method , 1976 .

[16]  P. Laura,et al.  Free vibrations of a rectangular plate of variable thickness elastically restrained against rotation along three edges and free on the fourth edge , 1979 .

[17]  P.A.A. Laura,et al.  A note on the vibrations of rectangular plates of variable thickness with two opposite simply supported edges and very general boundary conditions on the other two , 1977 .

[18]  Keiichiro Sonoda,et al.  Buckling of Rectangular Plates with Tapered Thickness , 1990 .

[19]  Critical Bending Stress for Flat Rectangular Plates Supported Along All Edges and Elastically Restrained Against Rotation Along the Unloaded Compression Edge , 1953 .