Buckling analysis of a laminated cylindrical shellunder torsion subjected to mixed boundary conditions

International Journal of Solids and Structures

Volumn 36, Issue 25, 1999, Pages 3821-3835

  Mao, Renjie ^a   Lu, C H ^b  

^a SHANGHAI JIAO TONG UNIVERSITY   (China)

^b Mechanical Systems   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY CONDITIONS; BUCKLING; LAMINATED COMPOSITES; MATRIX ALGEBRA; NUMERICAL METHODS; SHEAR STRESS; TORSIONAL STRESS;

BUCKLING ANALYSIS; LAMINATED CYLINDRICAL SHELL; MIXED BOUNDARY CONDITIONS;

SHELLS (STRUCTURES);

EID: 0033197158     PISSN: 00207683     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0020-7683(98)00178-4     Document Type: Article

References (5)

1. Flugge, W., 1960. Stresses in Shells. Springer-Verlag, Berlin, Gottingen, Heidelberg.
2. Hui, D., Du, I.H.Y., 1987. Initial postbuckling behavior of imperfect antisymmetric cross-plycylindrical shells under torsion. ASME J. Appl. Mech. 54, 174-180.
3. Simitses, G.J., Shaw, D., 1985. Imperfection sensitivity of laminated cylindrical shells in torsion andaxial compression. Composite Structures 4, 335-360.
4. Stein, M., 1986. Nonlinear theory for plates and shells including the effects of transverse shearing.AIAA J. 24, 1537-1544.
5. Tabiei, A., Simitses, G.J., 1994. Buckling of moderately thick, laminated cylindrical shells undertorsion. AIAA J. 32, 639-647.