Free Vibration of Partially Supported Cylindrical Shells
Free Vibration of Partially Supported Cylindrical Shells
复制标题
DOI:
10.3233/sav-1995-2404
复制
发表时间:
1995
影响因子:
1.6
通讯作者:
S. Mirza;Y. Alizadeh
中科院分区:
文献类型:
--
作者:
S. Mirza;Y. Alizadeh
The effects of detached base length on the natural frequencies and modal shapes of cylindrical shell structures were investigated in this work. Some of the important applications for this type of problem can be found in the cracked fan and rotor blades that can be idealized as partially supported shells with varying unsupported lengths. A finite element model based on small deflection linear theory was developed to obtain numerical solutions for this class of problems. The numerical results were generated for shallow shells and some of the degenerate cases are compared with other results available in the literature. The computations presented here involve a wide range of variables: material properties, aspect ratios, support conditions, and radius to base ratio.