Eine Plattform für die Wissenschaft: Bauingenieurwesen, Architektur und Urbanistik
Eine Plattform für die Wissenschaft: Bauingenieurwesen, Architektur und Urbanistik
Transient dynamic response of composite circular cylindrical shells under radial impulse load and axial compressive loads
AbstractFree and forced vibration of composite circular cylindrical shells are investigated based on the first love's approximation theory using the first-order shear deformation shell theory. The boundary conditions (BCs) are considered as clamped-free edges. The dynamic response of the composite shells is studied under transverse impulse and axial compressive loads. The axial compressive load was less than critical buckling loads. The modal technique is used to develop the analytical solution of the composite cylindrical shell. The solution for the shell under the given loading conditions can be found using the convolution integrals. The effect of fiber orientation, axial load, and some of the geometric parameters on the time response of the shells has been shown. The results show that dynamic responses are governed primarily by natural period of the structure. The accuracy of the analysis has been examined by comparing results with those available in the literature and experiments.
Transient dynamic response of composite circular cylindrical shells under radial impulse load and axial compressive loads
AbstractFree and forced vibration of composite circular cylindrical shells are investigated based on the first love's approximation theory using the first-order shear deformation shell theory. The boundary conditions (BCs) are considered as clamped-free edges. The dynamic response of the composite shells is studied under transverse impulse and axial compressive loads. The axial compressive load was less than critical buckling loads. The modal technique is used to develop the analytical solution of the composite cylindrical shell. The solution for the shell under the given loading conditions can be found using the convolution integrals. The effect of fiber orientation, axial load, and some of the geometric parameters on the time response of the shells has been shown. The results show that dynamic responses are governed primarily by natural period of the structure. The accuracy of the analysis has been examined by comparing results with those available in the literature and experiments.
Transient dynamic response of composite circular cylindrical shells under radial impulse load and axial compressive loads
Jafari, A.A. (Autor:in) / Khalili, S.M.R. (Autor:in) / Azarafza, R. (Autor:in)
Thin-Walled Structures ; 43 ; 1763-1786
06.06.2005
24 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Buckling Loads of Small Cylindrical Shells under Axial Compressive Loads
| British Library Conference Proceedings | 2004