INCREMENTAL COLLAPSE OF THICK-WALLED CIRCULAR-CYLINDERS UNDER STEADY AXIAL TENSION AND TORSION LOADS AND CYCLIC TRANSIENT HEATING

被引：5

作者：

SAGAR, V ^{[1
]}

PAYNE, DJ ^{[1
]}

机构：

[1] UNIV CAMBRIDGE,DEPT ENGN,CAMBRIDGE,ENGLAND

来源：

JOURNAL OF THE MECHANICS AND PHYSICS OF SOLIDS | 1975年 / 23卷 / 01期

关键词：

D O I：

10.1016/0022-5096(75)90010-1

中图分类号：

T [工业技术];

学科分类号：

08 ;

摘要：

引用

页码：39 / 53

页数：15

共 30 条

[21] LIMIT STATE OF THICK-WALLED ROTATING CYLINDERS UNDER COMBINED LOADING .I. STEADY MOTION
SKRZYPEK, J
BULLETIN DE L ACADEMIE POLONAISE DES SCIENCES-SERIE DES SCIENCES TECHNIQUES, 1967, 15 (04): : 257 - &
[22] Asymmetric bifurcations of thick-walled circular cylindrical elastic tubes under axial loading and external pressure
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[23] Transient coupled thermo-elasticity analysis of a temperature-dependent thick-walled cylinder under cyclic thermo-mechanical loads
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[25] Limit load solutions of thick-walled cylinders with fully circumferential cracks under combined internal pressure and axial tension (vol 238, pg 2155, 2008)
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[26] THE EFFECT OF INTERNAL PRESSURE ON THE BUCKLING STRESS OF THIN-WALLED CIRCULAR CYLINDERS UNDER COMBINED AXIAL COMPRESSION AND TORSION
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SUER, HS
SKENE, WT
JOURNAL OF THE AERONAUTICAL SCIENCES, 1958, 25 (02): : 142 - 143
[27] BIFURCATION OF INFLATED CIRCULAR-CYLINDERS OF ELASTIC-MATERIAL UNDER AXIAL LOADING .1. MEMBRANE THEORY FOR THIN-WALLED TUBES
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OGDEN, RW
JOURNAL OF THE MECHANICS AND PHYSICS OF SOLIDS, 1979, 27 (03) : 179 - 212
[28] Static axial tension or compression stress effects on shear cracks initiating under cyclic torsion loads in multiaxial fatigue tests
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[29] Global limit load solutions for thick-walled cylinders with circumferential cracks under combined internal pressure, axial force and bending moment - Part I: Theoretical solutions
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Li, Yuebing
Gao, Zengliang
INTERNATIONAL JOURNAL OF PRESSURE VESSELS AND PIPING, 2014, 114 : 23 - 40
[30] Global limit load solutions for thick-walled cylinders with circumferential cracks under combined internal pressure, axial force and bending moment - Part II: Finite element validation
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