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The effect of distributed end-face and local axisymmetric operational non-stationary loads on sandwich cylindrical shell elements of rocket bodies has been studied. The action of the engine is characterized by longitudinal forces that have time-varying frequency and amplitude and are applied to the end of the shell. Additionally, we have simulated local axisymmetric external impulsive loads applied along the directrix of the cylindrical shell to the place of ribs and between them to imitate an explosion of an elongated cumulative instantaneous charge. Given the different material properties of the face layers, light core, and reinforcing ribs, it is advisable to employ the finite-element method. By finite-element modeling of the dynamics of the structure under operational loads, this research enables thoroughly investigating the effect of the light core and facilitates choosing the optimal locations for applying local axisymmetric impulsive loads. The numerical results obtained from real object simulations, based on the developed methodology, allow us to give recommendations for determining the optimal amount of cumulative charge necessary for separating the rocket's spent stage while maintaining its prescribed trajectory. [ABSTRACT FROM AUTHOR]

The effect of distributed and localized axisymmetric impulsive loads on three-layer cylindrical shell elements of rocket airframes is studied. Localized axisymmetric impulsive external loads applied along the directrix of a cylindrical shell simulate an explosion of a superquick-action elongated shaped charge. Finite-element modeling of transient processes in such elements under such loads allows correct selection of the physical and mechanical parameters of cylindrical rocket airframes. A significant effect of the behavior of dynamic loads on the transient processes in three-layer cylindrical elements is demonstrated. [ABSTRACT FROM AUTHOR]

The paper deals with the dynamics of asymmetric three-layer hemispherical shells with the discretely symmetric lightweight, rib-reinforced filler under pulsed loads. Since the distances between the ribs are much larger than the dimensions of the rib cross-sections, the theory of independent static and kinematic hypotheses for each layer is applied. In asymmetric shells, the load-bearing layers are made of different materials and have various thicknesses. The equations of motion of asymmetric three-layer spherical shells and natural boundary conditions are obtained using the Hamilton– Ostrogradsky variational principle for the Timoshenko-type shell and rod theory model. This makes it possible to develop an adequate finite element model for asymmetric three-layer shells composed of several materials and obtain numerical results on the dynamic behavior of an asymmetric three-layer elastic structure using the finite element method. The influence of physical and mechanical parameters of asymmetric layers of hemispherical shells on the stress-strain state under axisymmetric internal pulse loading is investigated. New mechanical effects are revealed. [ABSTRACT FROM AUTHOR]

The dynamics of asymmetric three-layer spherical shells with a ribbed discrete-symmetric lightweight core under nonstationary loading is studied. The elements of the elastic structure are analyzed using the Timoshenko model of the theory of shells and rods and independent static and kinematic hypotheses for each layer. The equations of motion of the shells under axisymmetric impulsive loading are derived using the Hamilton–Ostrogradsky variational principle. A finite-element shell model that relates the potential strain energy in the body and the potential of the applied forces is developed. The numerical results on the dynamics of the asymmetric three-layer elastic structure with face layers made of dissimilar materials are obtained using the finite-element method. The effect of the geometrical and mechanical parameters of the asymmetric layers of the shell on its dynamic behavior under axisymmetric internal nonstationary loading is studied. New mechanical effects are revealed. [ABSTRACT FROM AUTHOR]

The dynamics of spherical sandwich shells with a discretely symmetric light core reinforced with ribs under nonstationary loads is studied. To analyze the shell members of the elastic structure, the Tymoshenko theory of shells and rods and independent static and kinematic hypotheses for each layer are used. The equation of motion of spherical sandwich shells with a discrete-symmetric light core reinforced with ribs under axisymmetric impulsive loading is derived using the Hamilton–Ostrogradsky variational principle. Numerical results of on the vibrations of the elastic sandwich are obtained by the finite-element method. The effect of the geometrical, physical, and mechanical parameters of the symmetric layers of the shell on its dynamic behavior under axisymmetric internal impulsive loading is analyzed, and new mechanical effects are discovered. [ABSTRACT FROM AUTHOR]

The dynamics of sandwich conical shells under nonstationary loading is studied. The equations of motion of sandwich conical shells with a discrete symmetric lightweight ribbed core under axisymmetric impulsive loading are derived. In analyzing elements of an elastic shell, the Timoshenko theory of shells and rods is combined with independent static and kinematic hypotheses for each layer. The load-bearing layers in non-symmetric shells are made of dissimilar materials. The equation of motion for a non-symmetric sandwich conical shell with a discretely inhomogeneous core is derived using the Hamilton–Ostrogradsky variational principle. The numerical results on the vibrations of a sandwich elastic shell are obtained using the finite-element method. The influence of the physical and mechanical parameters of symmetric and non-symmetric layers on the stress–strain state of shells under the axisymmetric internal impulsive loading is studied. New mechanical effects are established. [ABSTRACT FROM AUTHOR]

The stress–strain state of symmetric three-layer cylindrical shells under nonstationary loads is considered. The equation of vibrations of a shell with a light core reinforced with stiffening ribs under axisymmetric impulsive loading is derived. The members of the elastic structure are analyzed using the model of Tymoshenko's theory of shells and rods. Numerical results on the dynamics of the three-layer structure are obtained using the finite-element method. The significant effect of geometric and physical parameters of shell layers on the stress–strain state under axisymmetric internal impulsive loading is investigated. [ABSTRACT FROM AUTHOR]