IMPERFECTION-SENSITIVITY OF CYLINDRICAL PANELS UNDER COMPRESSION USING KOITERS IMPROVED POSTBUCKLING THEORY

被引:9
作者
HUI, D
CHEN, YH
机构
[1] Ohio State Univ, Columbus, OH, USA, Ohio State Univ, Columbus, OH, USA
关键词
DOMES AND SHELLS - Buckling;
D O I
10.1016/0020-7683(87)90090-4
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
This paper deals with the use of Koiter's improved postbuckling theory in axial buckling of integrally stiffened cylindrical panels. Acording to Koiter's improved theory, the postbuckling coefficients are evaluated at the actual applied load rather than at the classical buckling load. Substantial positive shift of the postbuckling is found which indicates that the imperfection-sensitivity predicted by Koiter's 1945 general theory may significantly overestimate the degrading effects of these imperfections. Such a positive shift is especially crucial in studying mode interactions such as local and overall buckling mode interactions of stringer-reinforced cylindrical shells.
引用
收藏
页码:969 / 982
页数:14
相关论文
共 47 条
[1]  
ARBOCZ J, 1974, THIN SHELL STRUCTURE, P59
[2]  
BAULD NR, 1979, AFFDLTR793038 AIR FO
[3]  
BUDIANSKY B, 1974, BUCKLING STRUCTURES
[4]  
BUDIANSKY B, 1964, 11TH P INT C APPL ME, P636
[5]  
BUDIANSKY B, 1979, P S DED 65 BIRTHD WT, P93
[6]  
BUSHNELL D, 1985, MECHANICS ELASTIC 9
[7]   MODE INTERACTION IN AXIALLY STIFFENED CYLINDRICAL-SHELLS [J].
BYSKOV, E ;
HUTCHINSON, JW .
AIAA JOURNAL, 1977, 15 (07) :941-948
[8]  
Citerley R.L., 1982, PRESSURE VESSELS PIP, P27
[9]  
CITERLEY RL, 1984, AFWALTR843006 AIR FO
[10]  
CITERLEY RL, 1986, WRC B, V313