ASYMMETRIC POSTBUCKLING OF SYMMETRICALLY LAMINATED CROSS PLY, SHORT CYLINDRICAL PANELS UNDER COMPRESSION

被引:26
作者
HUI, D
机构
[1] Ohio State Univ, Boyd Lab, Columbus,, OH, USA, Ohio State Univ, Boyd Lab, Columbus, OH, USA
关键词
AEROSPACE AND OCEAN ENGINEERING - CLOSED CIRCULAR CYLINDRICAL SHELLS - IMPERFECTION SENSITIVITY - LIGHTWEIGHT COMPOSITE MATERIALS;
D O I
10.1016/0263-8223(85)90029-7
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
引用
收藏
页码:81 / 95
页数:15
相关论文
共 28 条
[11]  
HUI D, 1984, INT J SOLIDS STRUCTU, V24
[12]  
HUI D, 1983, UTIAS247 U TOR I AER
[13]  
HUI D, 1981, ASME J APPLIED MECHA, V48, P915
[14]   IMPERFECTION-SENSITIVITY OF ECCENTRICALLY STIFFENED CYLINDRICAL SHELLS [J].
HUTCHINS.JW ;
AMAZIGO, JC .
AIAA JOURNAL, 1967, 5 (03) :392-&
[15]  
JONES RM, 1975, MECHANICS COMPOSITE
[16]   FURTHER COMPARISON OF THE NUMERICAL AND EXPERIMENTAL BUCKLING BEHAVIORS OF COMPOSITE PANELS [J].
KHOT, NS ;
BAULD, NR .
COMPUTERS & STRUCTURES, 1983, 17 (01) :61-68
[17]  
KHOT NS, AFFDLTR79125
[18]  
KOITER WT, 1956, S476 NAT AER RES I R
[19]  
SIMITSES GJ, 1982, UNPUB 9TH US C APPL
[20]   VIBRATION AND BUCKLING OF CROSS-PLY LAMINATED CIRCULAR CYLINDRICAL PANELS [J].
SINHA, PK ;
RATH, AK .
AERONAUTICAL QUARTERLY, 1975, 26 (AUG) :211-218