VIBRATION AND STABILITY OF CIRCULAR PLATES UNDER PARTIALLY DISTRIBUTED OR CONCENTRATED INPLANE LOADS

被引：7

作者：

NARITA, Y

机构：

[1] Computer Center, Hokkaido Institute of Technology, Teine Maeda, 419-2, Japan

来源：

JOURNAL OF APPLIED MECHANICS-TRANSACTIONS OF THE ASME | 1985年 / 52卷 / 03期

关键词：

Gas turbines - Buckling;

D O I：

10.1115/1.3169099

中图分类号：

O3 [力学];

学科分类号：

08 ; 0801 ;

摘要：

A method is presented for analyzing the free transverse vibration and elastic stability of circular plates under nonuniform distribution of the inplane stresses. A general solution procedure is developed, and a frequency equation is derived for the case when a pair of loads are locally distributed in the plane along the edge. Numerical results are presented for natural frequencies and buckling loads of the plates, and the effect of the partial inplane loading is discussed. A limiting case for a concentrated inplane load is also considered. © 1985 by ASME.

引用

页码：549 / 552

页数：4

共 16 条

[1]

CELEP Z, 1982, J SOUND VIB, V80, P421, DOI 10.1016/0022-460X(82)90283-8

[2] AXIALLY-SYMMETRIC STABILITY OF A COMPLETELY FREE CIRCULAR PLATE SUBJECTED TO A NON-CONSERVATIVE EDGE LOAD [J].