The buckling of an orthotropic composite truncated conical shell with continuously varying thickness subject to a time dependent external pressure

Composites Part B: Engineering

Volumn 34, Issue 3, 2003, Pages 227-233

  Sofiyev, Abdullah H ^a  

^a SULEYMAN DEMIREL UNIVERSITY   (Turkey)

Author keywords

B. Anisotropy; B. Buckling; C. Analytical modeling; C. Numerical analysis; Orthotropic composite truncated conical shells

Indexed keywords

ANISOTROPY; BUCKLING; COMPUTATIONAL METHODS; DIFFERENTIAL EQUATIONS; ELASTIC MODULI; GALERKIN METHODS;

ORTHOTROPIC COMPOSITES;

COMPOSITE MATERIALS;

EID: 0037379115     PISSN: 13598368     EISSN: None     Source Type: Journal    
DOI: 10.1016/S1359-8368(02)00105-1     Document Type: Article

References (20)

1. Sachenkov A.V., Baktieva L.U. Approach to the solution of dynamic stability problems of thin shells. Studies in the theory of plates and shells. vol. 13:1978;Kazan State University. p. 137-52, in Russian.
2. Irie T., Yamada G., Kaneko Y. Free vibration of a conical shell with variable thickness. J Sound Vibr. 82:(1):1982;83-94.
3. Ershov V.V., Ryabtsev V.A., Shalitkin V.A. The buckling of rotational shells with variable thickness. Review of theory of plates and shells. 1975;Nauka, Moscow. p. 594-603, in Russian.
4. Andreev L.B., Obodan H.I. The application of the method of theory response for the definition critical load of cylindrical shells with variable thickness subjected to non-uniform external pressure. Review of theory of plates and shells. 1973;Nauka, Moscow. in Russian.
5. Takahashi S., Suzuki K., Kosawada T. Vibrations of conical shells with varying thickness (continued). Bull Jpn Soc Mech Engrs. 28:(235):1985;117-123.
6. Medvedev N.G. Maximization of the fundamental natural frequency and polymodality of vibrations modes of orthotropic shells of variable thickness. Mech Solids. 20:(3):1985;140-148.
7. Sivadas K.R., Ganesan N. Vibration analysis of laminated conical shells with variable thickness. J Sound Vibr. 148:1991;477-491.
8. Koiter W.T., Elishakoff I., Li Y.W., Starnes J.H. Buckling of an axially compressed cylindrical shell of variable thickness. Int J Solids Struct. 31:(6):1994;797-805.
9. Li Y.W., Elishakoff I., James H., Starnes J., Bushnell D. Effect of the thickness variation and initial imperfection on buckling of composite cylindrical shells: asymptotic analysis and numerical results by Bosor 4 and Panda 2. Int J Solids Struct. 34:(28):1997;3755-3767.
10. Babich D.V. Natural vibrations of a conical orthotropic shell with small curvatures of the generatrix. Int Appl Mech. 35:(3):1999;276-280.
11. Bambill D.V., Rossit C.A., Laura P.A.A., Rossi R.E. Transverse vibrations of an orthotropic rectangular plate of linearly varying thickness and with a free edge. J Sound Vibr. 235:(3):2000;530-538.
12. Agamirov V.L. Dynamic problems of nonlinear shells theory. 1990;Nauka, Moscow. in Russian.
13. Sachenkov A.V., Klementev G.G. Studies in the theory of plates and shells. Studies in the theory of plates and shells. vol. 15:1980;Kazan State University. p. 115-25, in Russian.
14. Shumik M.A. The stability of a truncated conical shell subject to a dynamic external pressure. Int Appl Mech. 9:(6):1973;107-109.
15. Vinson J.R., Sierakowski R.L. The behavior of structures composed of composite material. 1986;Nijhoft, Dordrecht.
16. Jones R.M. Mechanics of composite materials. 1975;McGraw-Hill, New York.
17. Greenberg J.B., Stavsky Y. Buckling and vibration of orthotropic composite cylindrical shells. Acta Mech. 36:1980;15-29.
18. Greenberg J.B., Stavsky Y. Vibrations and buckling of composite orthotropic cylindrical shells with non-uniform axial loads. Composites, Part B: Engng. 29:(6):1998;695-703.
19. Sofiyev A.H., Aksogan O. The dynamic stability of a non-homogeneous orthotropic elastic truncated conical shell under a time dependent external pressure. Struct Engng Mech. 13:(3):2002;329-343.
20. Aksogan O., Sofiyev A.H. Dynamic buckling of a cylindrical shell with variable thickness subject to a time dependent external pressure varying as a power function of time. J Sound Vibr. 254:(4):2002;693-702.