Because of the extensive application of thin-walled structures of composite materials in various branches of modern technology (rocket and aviation engineering), it is important to develop reliable methods ofpredicting their stress--strain and vibration state in the conditions of the effect of high-speed external loading (force, thermal, acoustic). Recently, there have been a number of detailed theoretical and experimental investigations of the nonstationary deformation of real structures which usually consist of several sections and are characterized by the presence of reinforcing elements, a locally attached weight, weakening holes, etc. The need to describe adequately the dynamic behavior of shell systems with a complicated geometrical rheological structure results in the development of comparatively complicated mathematical models. For example, the authors of [1-4] used the relationships of improved theory of Timoshenko's type for numerical simulation of the wave processes in compound shell-rod structures subjected to axial pulsed loading. In this work, we shall construct a mechanicomathematical model and a conservative difference scheme for determining the force and kinematic characteristics of wave fields in thinwalled structures with holes. The time dependences of the acceleration of combined masses are presented, and the analysis of these dependences makes it possible to estimate the effect of internal reinforcing elements, structural damping, and weakening and other factors on the evolution of transition processes. i. Formulation of the Initial Boundary-Value Problem. We shall examine thin-walled compound structures (Fig. i) whose left end is subjected to the effect of a nonaxisymmetric pulse f(~, t). The ends of the sections (shells of revolution) are rigidly fixed in thin nondeformed disks with the masses M~ ... M4. The walls of the shells are weakened with rightangled and circular holes with free or rigidly fixed edges. Each section has a constant wall thickness hj (j = i, 2, 3) and can be made of various materials (metals, composites). We shall introduce an orthogonal coordinate system s, y, z with unit vectors directed respectively along the generating line, around the circle and along the normal to the median surface of the shells, and also the radius-vector of the arbitrary point P: r(s,~ ) = [R(s) r R(s) sin ~, z(s)] T, where R(s) = AP, z(s) = OA, y = R(s)~.
Read full abstract