The stability of composite material stiffened conical shells under axial compression

Composite Structures

Volumn 38, Issue 1-4, 1997, Pages 169-177

  Li, Lingchuan ^a  

^a UNIVERSITY OF WESTERN ONTARIO   (Canada)

Author keywords

[No Author keywords available]

Indexed keywords

APPROXIMATION THEORY; BOUNDARY CONDITIONS; COMPOSITE STRUCTURES; STIFFNESS;

AXIAL COMPRESSION; ORTHOTROPIC SHELLS; RAYLEIGH RIZE APPROXIMATIONS;

SHELLS (STRUCTURES);

EID: 0031131239     PISSN: 02638223     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0263-8223(97)00053-6     Document Type: Article

References (13)

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3. Singer, J., Buckling of orthotropic conical shells under external pressure. J. Aero. Quar., May 1964, pp. 151-168.
4. Baruch, M. and Singer, J., General instability of stiffened circular conical shells under hydraulic pressure. Aero. Quar., May 1965, pp. 187-204.
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7. Seide, P., Axisymmetrical buckling of circular cones under axial compression. J. Appl. Mech., 1956, 23, 625-628.
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9. Seide, J., Buckling of circular cones under axial compression. J. Appl. Mech., 1961, 28, 315-319.
10. Singer, J., Buckling of circular conical shells under uniform axial compression. AIAA J. 1965, 3, 985-987.
11. Tani, J., Buckling of truncated conical shells under axial compression. AIAA J., 1970, 8, 568-571.
12. Tong, L.Y. and Wang, T.K., Buckling analysis of laminated composite conical shells. Comp. Sci. Tech., 1993, 47, 57-63.
13. Li Shunlin, Handbook for Composite Materials, Beijing, 1988