An investigation on fundamental frequencies of laminated circular cylinders given by shear deformable finite elements

Journal of Sound and Vibration

Volumn 205, Issue 3, 1997, Pages 265-273

  Sun, G ^a   Bennett, P N ^b   Williams, F W ^b  

^a SHANGHAI JIAO TONG UNIVERSITY   (China)

^b CARDIFF UNIVERSITY   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 0344514227     PISSN: 0022460X     EISSN: None     Source Type: Journal    
DOI: 10.1006/jsvi.1996.0975     Document Type: Article

References (10)

1. J. N. REDDY 1982 Fibre Science and Technology 17, 9-24. Bending of laminated anisotropic shells by a shear deformable finite element.
2. J. N. REDDY 1984 Journal of the Engineering Mechanics Division, American Society of Civil Engineers 110, 794-809. Exact solutions of moderately thick laminated shells.
3. J. N. REDDY 1986 Energy and Variational Methods in Applied Mechanics. New York: John Wiley.
4. J. L. SANDERS JR. 1959 NASA Technical Report R-24. An improved first-approximation theory for thin shells.
5. K. CHANDRASHEKHARA 1989 Computers and Structures 33, 435-440. Free vibrations of anisotropic laminated doubly curved shells.
6. R. BUTLER and F. W. WILLIAMS 1992 Computers and Structures 43, 699-708. Optimum design using VICONOPT, a buckling and strength constraint program for prismatic assemblies of anisotropic plates.
7. W. H. WITTRICK and F. W. WILLIAMS 1974 International Journal of Mechanical Sciences 16, 209-239. Buckling and vibration of anisotropic or isotropic plate assemblies under combined loadings.
8. K. J. BATHE 1982 Finite Element Procedures in Engineering Analysis. Englewood Cliffs, New Jersey: Prentice-Hall.
9. R. M. JONES and H. S. MORGAN 1975 American Institute of Aeronautics and Astronautics Journal 13, 664-671. Buckling and vibration of cross-ply laminated circular cylindrical shells.
10. M. S. ANDERSON and D. KENNEDY 1993 American Institute of Aeronautics and Astronautics Journal 31, 1963-1965. Transverse shear deformation in exact buckling and vibration of composite plate assemblies.