Dynamic response of a cylindrical shell segment subjected to an arbitrary loading.
Dynamic response of cylindrical shell segments subjected to arbitrary load distribution
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Dynamic response of cylindrical shell segments subjected to arbitrary load distribution
Effect of shallow meridional curvature on vibration of nearly cylindrical shells
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Dynamic response of cylindrical shell to random acoustic excitation
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Elastic buckling load of cylindrical shells with dimple imperfections under external pressure, applying perturbation expansion to Karman-Donnell equations
The large amplitude vibration of a thin-walled cylindrical shell is analyzed. A perturbation method is used to solve the steady-state forced vibration problem. The simply-supported boundary conditions and the circumferential periodicity condition are satisfied. The resulting solution indicates that in addition to the fundamental mode, the response contains asymmetric modes as well as axisymmetric modes with the frequency twice that of the fundamental mode. Vibrations involving a single driven mode response are investigated. The results indicate that the nonlinearity is either softening or hardening depending on the mode. The vibrations involving both a driven mode and a companion mode are also investigated. An experimental investigation is conducted, and the results are in qualitative agreement with the theory. 'Nonstationary' response is detected at some frequencies for large amplitude response in which the amplitude drifts from one value to another. Various nonlinear phenomena are observed and comparisons with the theoretical results are made.
Resonant bending frequencies and mode shapes for thin circular cylindrical shell containing an internal liquid with a free surface
Resonant bending frequencies and mode shapes for thin, circular cylindrical shell containing an internal liquid with a free surface
Effect of boundary conditions for tangential displacement on upper critical pressure value of cylindrical shell
Thin-walled shells with strong longitudinal and transverse stiffening (for example, stressed-skin fuselages and wings) may, under certain simplifying assumptions, be treated as static systems with finite redundancies. In this report the underlying basis for this method of treatment of the problem is presented and a computation procedure for stiffened cylindrical shells with curved sheet panels indicated. A detailed discussion of the force distribution due to applied concentrated forces is given, and the discussion illustrated by numerical examples which refer to an experimentally determined circular cylindrical shell.
Results from five separate investigations on buckling and collapse of cylindrical shells suitable for structural components of missiles and launch vehicles
Theory and equations for propagating pressure waves in liquid filled cylindrical shells
Instability of eccentrically stiffened cylindrical shells under axial compression and lateral pressure