EFFECT OF IMPERFECTIONS ON BUCKLING OF THIN CYLINDERS AND COLUMNS UNDER AXIAL COMPRESSION

被引：3

|

作者：

DONNELL, LH

WAN, CC

机构：

来源：

JOURNAL OF APPLIED MECHANICS-TRANSACTIONS OF THE ASME | 1950年 / 17卷 / 01期

关键词：

D O I：

暂无

中图分类号：

O3 [力学];

学科分类号：

08 ; 0801 ;

摘要：

引用

收藏

页码：73 / 83

页数：11

相关论文

共 50 条

[31] Buckling characteristics of cross-ply elliptical cylinders under axial compression
Sambandam, CT
Patel, BP
Gupta, SS
Munot, CS
Ganapathi, M
COMPOSITE STRUCTURES, 2003, 62 (01) : 7 - 17
[32] Buckling Analysis of Carbon Fiber Reinforced Plastics Cylinders under Axial Compression
Huang, Da
Duan, Chenghong
ADVANCED MATERIALS AND PROCESSES III, PTS 1 AND 2, 2013, 395-396 : 76 - 79
[33] BUCKLING ANALYSIS OF GEOMETRICALLY IMPERFECT STIFFENED CYLINDERS UNDER AXIAL-COMPRESSION
SHEINMAN, I
SIMITSES, GJ
AIAA JOURNAL, 1977, 15 (03) : 374 - 382
[34] Analytical Study on the Buckling of Cylindrical Shells With Arbitrary Thickness Imperfections Under Axial Compression
Cao, Guowei
Chen, Zhiping
Yang, Licai
Fan, Haigui
Zhou, Fan
JOURNAL OF PRESSURE VESSEL TECHNOLOGY-TRANSACTIONS OF THE ASME, 2015, 137 (01):
[35] Buckling behaviour of extensively-welded steel cylinders under axial compression
Lin, X
Teng, JG
ADVANCES IN STEEL STRUCTURES, VOLS I & II, PROCEEDINGS, 2002, : 737 - 744
[36] BUCKLING OF FIBER-REINFORCED CIRCULAR CYLINDERS UNDER AXIAL COMPRESSION.
Tennyson, R.C.
Muggeridge, D.B.
Chan, K.H.
Khot, N.S.
1600,
[37] BUCKLING OF THIN CYLINDRICAL SHELLS UNDER UNIFORM AXIAL COMPRESSION
HARTSMIT.LJ
INTERNATIONAL JOURNAL OF MECHANICAL SCIENCES, 1970, 12 (04) : 299 - &
[38] EFFECT OF A DENT ON BUCKLING STRENGTH OF TUBULAR COLUMNS SUBJECTED TO AXIAL COMPRESSION
SCHACKNE, GL
MECHANICAL ENGINEERING, 1967, 89 (07) : 69 - &
[39] Influence of residual strains on buckling of thin filament-wound cylinders in axial compression
Pai, SP
Jensen, DW
JOURNAL OF AEROSPACE ENGINEERING, 2001, 14 (01) : 21 - 28
[40] Influence of fiber undulations on buckling of thin filament-wound cylinders in axial compression
Pai, SP
Jensen, DW
JOURNAL OF AEROSPACE ENGINEERING, 2001, 14 (01) : 12 - 20

← 1 2 3 4 5 →