IMPROVED FINITE-ELEMENTS FOR VIBRATION ANALYSIS OF TAPERED BEAMS

被引：11

作者：

THOMAS, J ^{[1
]}

DOKUMACI, E ^{[1
]}

机构：

[1] UNIV SURREY,GUILFORD,SURREY,ENGLAND

来源：

AERONAUTICAL QUARTERLY | 1973年 / 24卷 / FEB期

关键词：

D O I：

10.1017/S0001925900006405

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：39 / 46

页数：8

共 14 条

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THOMAS, J ;

DOKUMACI, E .

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[5]

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[7] THE EFFECT OF LUMPED PARAMETERS ON BEAM FREQUENCIES [J].

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LINDBERG, GM .

AERONAUTICAL QUARTERLY, 1963, 14 (03) :224-240

[8] VIBRATION OF NON-UNIFORM BEAMS [J].

LINDBERG, GM .

AERONAUTICAL QUARTERLY, 1963, 14 (04) :387-395

[9] SOME INTEGRALS RELATING TO THE VIBRATION OF A CANTILEVER BEAM AND APPROXIMATION FOR THE EFFECT OF TAPER ON OVERTONE FREQUENCIES [J].

MARTIN, AI .

AERONAUTICAL QUARTERLY, 1956, 7 (02) :109-124

[10]

PESTEL E, 1966, PROCEEDINGS

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