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IssuesArchive of Issues2005-1pp.142-152

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V. V. Bolotin, A. V. Petrovskii, and V. P. Radin, "Stability and postcritical behavior of a multilink system of rigid bodies subjected to nonpotential loading," Mech. Solids. 40 (1), 142-152 (2005)
Year 2005 Volume 40 Number 1 Pages 142-152
Title Stability and postcritical behavior of a multilink system of rigid bodies subjected to nonpotential loading
Author(s) V. V. Bolotin (Moscow)
A. V. Petrovskii (Moscow)
V. P. Radin (Moscow)
Abstract A multilink system of rigid bodies is considered, the links of which are loaded by dead forces (inertia forces). The rear link is loaded by a follower force (thrust force) directed along the axis of the lowest link. The links are connected to each other by viscoelastic elements the characteristics of which are assumed to be linear. The principal axes of these elements are orthogonal to each other. In the unloaded state, the planes of these axes (principal planes) are orthogonal to the axes of the links of the system and parallel to each other. In the loaded state, the axes are turned relative to each other in the principal planes. The stability of the trivial solution of the problem, for which the deviation of the longitudinal axes of the links from the vector of acceleration of the center of mass of the system is zero, is analyzed. The boundaries of the divergence and flutter domains are constructed. The postcritical behavior of the system is analyzed numerically. In particular, the dynamic behavior of the system under slowly changing thrust force is analyzed. This analysis made it possible to establish the types of dynamic behavior, find the bifurcations of the modes, and determine the domains of chaotic behavior of the system.

The behavior of elastic systems subjected to nonpotential (in particular, follower) forces has been studied fairly thoroughly [1-6]. However, quite a lot of problems still remain, which are of interest from the standpoint of the nonlinear dynamics. One of such problems is that of the dynamic behavior of a system of rigid bodies (links) connected by viscoelastic elements and loaded by dead and follower forces. An example of dead forces are the inertia forces, provided that the direction of the vector of acceleration of the center of mass is constant. A follower force is the thrust force. In this system, the quasistatic (divergence) and dynamic (flutter) types of loss of stability are possible. It is of interest to analyze the combination of these types. In this case, the effect of secondary flutter is possible in the divergence domain. This effect was first observed for aeroelastic systems [7] and then thoroughly analyzed [8-10]. In the present study, the complete systematic analysis of both the equilibrium states of divergence kind and the motions in the flutter domain is performed for a system of three links. Major attention is given to the analysis of stability of the direction of the acceleration of the center of mass of the system.
References
1.  V. V. Bolotin, "On the vibrations and stability of rods loaded by nonconservative forces," in Vibrations in Turbomachines [in Russian], pp. 23-42, Izd-vo AN SSSR, Moscow, 1959.
2.  V. V. Bolotin, Nonconservative Problems of the Theory of Elastic Stability [in Russian], Fizmatgiz, Moscow, 1961.
3.  V. V. Bolotin nad N. I. Zhinzher, "Effects of damping on stability of elastic systems subjected to nonconservative forces," Int. J. Solid Struct., Vol. 5, No. 9, pp. 965-989, 1969.
4.  N. I. Zhinzher, "Influence of dissipative forces with incomplete dissipation on the stability of elastic systems," Izv. AN. MTT [Mechanics of Solid], No. 1, pp. 149-155, 1994.
5.  J.-D. Jin, "Bifurcation analysis of double pendulum with a follower force," J. Sound Vibr., Vol. 154, No. 2, pp. 191-204, 1992.
6.  A. N. Kounadis, "On the failure of static stability analyses of nonconservative systems in domains of divergence instability," Int. J. Solids and Structures, Vol. 31, No. 15, pp. 2099-2120, 1994.
7.  V. V. Bolotin, A. V. Petrovsky, and A. A. Grishko, "Secondary bifurcations and global instability of an aeroelastic nonlinear system in the divergence domain," J. Sound Vibr., Vol. 191, No. 3, pp. 431-451, 1996.
8.  A. A. Grishko, A. V. Petrovskii, and V. P. Radin, "On the influence of the internal friction on the stability of a panel in the supersonic gas flow," Izv. AN. MTT [Mechanics of Solid], No. 1, pp. 173-181, 1998.
9.  V. V. Bolotin, A. A. Grishko, A. N. Kounadis, and Ch. Gantes, "Non-linear panel flutter in remote post-critical domain," Int. J. Non-Linear Mechanics, Vol. 33, No. 5, pp. 753-764, 1998.
10.  V. V. Bolotin, A. A. Grishko, A. N. Kounadis, Ch. Gantes, and J. B. Roberts, "Influence of initial conditions on the postcritical behavior of nonlinear aeroelastic systems," J. Nonlinear Dynamics, No. 15, pp. 63-81, 1998.
11.  A. V. Petrovskii, "Stability and postcritical bshavior of an inverted three-dimensional pendulum subjected to nonpotential loading," Izv. AN. MTT [Mechanics of Solid], No. 1, pp. 165-176, 2002
12.  V. V. Bolotin (Editor), Vibrations in Engineering. Handbook. Volume 1. Vibrations of Linear Systems [in Russian], Mashinostroenie, Moscow, 1999.
13.  A. A. Grishko, Yu. A. Dubovskikh, and A. V. Petrovskii, "On the postcritical behavior of nonlinear dissipative systems," Prikladnaya Mekhanika, Vol. 34, No. 6, pp. 92-98, 1998.
Received 27 April 2004
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