VIBRATION AND STABILITY OF SHELL PANELS WITH SLIGHT INTERNAL DAMPING UNDER FOLLOWER FORCES

被引：9

作者：

ALTMAN, W ^{[1
]}

DEOLIVEIRA, MG ^{[1
]}

机构：

[1] INST TECNOL AERONAUT,DIV ENGN INFRA ESTRUTURA AERONAUT,BR-12225 SAO JOSE CAMPOS,SP,BRAZIL

来源：

JOURNAL OF SOUND AND VIBRATION | 1990年 / 136卷 / 01期

关键词：

D O I：

10.1016/0022-460X(90)90936-T

中图分类号：

O42 [声学];

学科分类号：

070206 ; 082403 ;

摘要：

An analysis of vibration and stability of conical and cylindrical shell panels with slight internal damping under follower forces is presented. An extended form of the principle of virtual work is utilized. Examples of cantilevered conical and cylindrical shell panels with and without small internal damping are solved. Plots of these solutions illustrate graphically the influence of internal damping. © 1990.

引用

页码：45 / 50

页数：6

共 8 条

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ALTMAN, W ;

DEOLIVEIRA, MG .

JOURNAL OF SOUND AND VIBRATION, 1988, 122 (02) :291-298

[2]

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[3]

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[4]

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[7]

Soedel W., 1981, VIBRATION SHELLS PLA

[8]

ZIEGLER H, 1952, ING ARCH, V20, P40

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