THE BEHAVIOR OF A LINEAR, DAMPED MODAL SYSTEM WITH A NON-LINEAR SPRING-MASS DRY FRICTION DAMPER SYSTEM ATTACHED, .2.

被引：18

作者：

FERRI, AA

DOWELL, EH

机构：

[1] Duke Univ, Durham, NC, USA, Duke Univ, Durham, NC, USA

来源：

JOURNAL OF SOUND AND VIBRATION | 1985年 / 101卷 / 01期

关键词：

STRUCTURAL ANALYSIS - Mathematical Models;

D O I：

10.1016/S0022-460X(85)80038-9

中图分类号：

O42 [声学];

学科分类号：

070206 ; 082403 ;

摘要：

In previous work, the title problem was studied. Unfortunately, a sign reversal in the damping term led to a misinterpretation of the effect of linear damping of the modal system. In the present paper this is corrected and the work previously reported is extended.

引用

页码：55 / 74

页数：20

共 7 条

[1]

DENHARTOG JP, 1931, T ASME, P107

[2] THE BEHAVIOR OF A LINEAR, DAMPED MODAL SYSTEM WITH A NON-LINEAR SPRING MASS DRY FRICTION DAMPER SYSTEM ATTACHED [J].

DOWELL, EH .

JOURNAL OF SOUND AND VIBRATION, 1983, 89 (01) :65-84

[3]

DOWELL EH, 1978, MODERN COURSE AEROEL

[4]

Hayashi C., 1964, NONLINEAR OSCILLATIO

[5] NON-LINEAR ANALYSIS OF STICK-SLIP MOTION [J].

PRATT, TK ;

WILLIAMS, R .

JOURNAL OF SOUND AND VIBRATION, 1981, 74 (04) :531-542

[6] FRICTION DAMPING OF FLUTTER IN GAS-TURBINE ENGINE AIRFOILS [J].

SINHA, A ;

GRIFFIN, JH .

JOURNAL OF AIRCRAFT, 1983, 20 (04) :372-376

[7]

Stoker J.J., 1950, NONLINEAR VIBRATIONS, V2

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