Dynamics Simulation of a Circular Membrane With an Eccentric Circular Areal Constraint

Author(s):  
Assaad AlSahlani ◽  
Ranjan Mukherjee

We investigate the dynamics of a circular membrane with an eccentric circular areal constraint under arbitrary initial conditions. The membrane is assumed to be fixed at its outer boundary and the constraint is assumed to impose zero displacement over a circular area of the membrane. The symmetric and antisymmetric modes of vibration of the membrane are derived and their orthogonality properties are established. Using the orthogonality conditions established in this paper, the complete solution to the constrained vibratory motion of the membrane is determined for arbitrary initial conditions. Two sets of numerical simulation results are presented.

The theory of the vibrations of the pianoforte string put forward by Kaufmann in a well-known paper has figured prominently in recent discussions on the acoustics of this instrument. It proceeds on lines radically different from those adopted by Helmholtz in his classical treatment of the subject. While recognising that the elasticity of the pianoforte hammer is not a negligible factor, Kaufmann set out to simplify the mathematical analysis by ignoring its effect altogether, and treating the hammer as a particle possessing only inertia without spring. The motion of the string following the impact of the hammer is found from the initial conditions and from the functional solutions of the equation of wave-propagation on the string. On this basis he gave a rigorous treatment of two cases: (1) a particle impinging on a stretched string of infinite length, and (2) a particle impinging on the centre of a finite string, neither of which cases is of much interest from an acoustical point of view. The case of practical importance treated by him is that in which a particle impinges on the string near one end. For this case, he gave only an approximate theory from which the duration of contact, the motion of the point struck, and the form of the vibration-curves for various points of the string could be found. There can be no doubt of the importance of Kaufmann’s work, and it naturally becomes necessary to extend and revise his theory in various directions. In several respects, the theory awaits fuller development, especially as regards the harmonic analysis of the modes of vibration set up by impact, and the detailed discussion of the influence of the elasticity of the hammer and of varying velocities of impact. Apart from these points, the question arises whether the approximate method used by Kaufmann is sufficiently accurate for practical purposes, and whether it may be regarded as applicable when, as in the pianoforte, the point struck is distant one-eighth or one-ninth of the length of the string from one end. Kaufmann’s treatment is practically based on the assumption that the part of the string between the end and the point struck remains straight as long as the hammer and string remain in contact. Primâ facie , it is clear that this assumption would introduce error when the part of the string under reference is an appreciable fraction of the whole. For the effect of the impact would obviously be to excite the vibrations of this portion of the string, which continue so long as the hammer is in contact, and would also influence the mode of vibration of the string as a whole when the hammer loses contact. A mathematical theory which is not subject to this error, and which is applicable for any position of the striking point, thus seems called for.


2014 ◽  
Vol 29 (21) ◽  
pp. 1450115
Author(s):  
Fahrettin Koyuncu ◽  
Orhan Dönmez

We have solved the General Relativistic Hydrodynamic (GRH) equations using the high resolution shock capturing scheme (HRSCS) to find out the dependency of the disk dynamics to the Mach number, adiabatic index, the black hole rotation parameter and the outer boundary of the computational domain around the non-rotating and rotating black holes. We inject the gas to computational domain at upstream and downstream regions at the same time with different initial conditions. It is found that variety of the mass accretion rates and shock cone structures strongly depend on Mach number and adiabatic index of the gas. The shock cones on the accretion disk are important physical mechanisms to trap existing oscillation modes, thereupon these trapped modes may generate strong X-rays observed by different X-ray satellites. Besides, our numerical approach also show that the shock cones produces the flip–flop oscillation around the black holes. The flip–flop instabilities which are monitored in our simulations may explain the erratic spin behavior of the compact objects (the black holes and neutron stars) seen from observed data.


1990 ◽  
Vol 45 (7) ◽  
pp. 839-846 ◽  
Author(s):  
D. Pfirsch

AbstractIn 1925 Cherry [1] discussed two oscillators of positive and negative energy that are nonlinearly coupled in a special way, and presented a class of exact solutions of the nonlinear equations showing explosive instability independent of the strength of the nonlinearity and the initial amplitudes. In this paper Cherry's Hamiltonian is transformed into a form which allows a simple physical interpretation. The new Hamiltonian is generalized to three nonlinearly coupled oscillators; it corresponds to three-wave interaction in a continuum theory, like the Vlasov-Maxwell theory, if there exist linear negative energy waves [2-4, 5, 6], Cherry was able to present a two-parameter solution set for his example which would, however, allow a four-parameter solution set, and, as a first result, an analogous three-parameter solution set for the resonant three-oscillator case is obtained here which, however, would allow a six-parameter solution set. Nonlinear instability is therefore proven so far only for a very small part of the phase space of the oscillators. This paper gives in addition the complete solution for the three-oscillator case and shows that, except for a singular case, all initial conditions, especially those with arbitrarily small amplitudes, lead to explosive behaviour. This is true of the resonant case. The non-resonant oscillators can sometimes also become explosively unstable, but the initial amplitudes must not be infinitesimally small. A few examples are presented for illustration.


Author(s):  
Assaad AlSahlani ◽  
Ranjan Mukherjee

We investigate the energetics of a freely vibrating circular membrane subjected to a sudden eccentric circular areal constraint. The membrane is assumed to be fixed at its outer boundary and the constraint is assumed to be applied at an arbitrary time during the motion of the membrane. The constraint is applied instantaneously such that immediately after application of the constraint, the geometry of the membrane outside the area of the constraint remains unchanged and the constrained area comes to rest. The change in total energy after constraint application is investigated for different sizes and locations of the constraint and time of application of the constraint. The results show that the energy can decrease or increase depending on the time of application of the constraint. The condition for maximum energy reduction is presented and simulation results based on this condition show that sequential application and removal of the constraint reduces the total energy rapidly. This provides the opportunity for active control of membrane vibration through direct physical interaction with a small area of the membrane.


2015 ◽  
Vol 811 ◽  
pp. 110-116
Author(s):  
Cristian Dragomirescu ◽  
Victor Iliescu

The paper analyses the vibratory motion of an electro-mechanical device acting medical equipment. The study is performed using the specific methods of the theory of the dynamical systems. The induced vibrations, their variation in time and the evolution of the system, as a function of the initial conditions, are studied, examining the fulfilment of the constraints prescribed in the literature, in order to achieve a maximal therapeutic benefit. The suitable operation ranges are determined, which establishes the starting point for the design of such equipment.


Author(s):  
Mario Duras

During development of MBS (Multibody System) dynamics simulation tool that evaluates contact forces between bodies, a procedure had to be developed for placing general MBS to equilibrium state. The procedure would be executed before dynamics simulation starts, to ensure stable and convergent simulation from its beginning. As very broad range of stiffnesses is coupled within the same model and additionally contact forces are evaluated, placing system to satisfactory initial state is not a simple task. Algorithm for initial conditions must place bodies to positions that would provide smallest possible (zero) resultant force on each body. After several approaches being tested, usage of PID (Proportional-Integral-Derivative) controllers showed greatest potential for solving the problem in a stable and fast manner. Such controller would be attached to each body and will move bodies to positions with smallest resultant force. To completely model PID controller, three parameters must be evaluated - gains for each controller action. For optimal combination of three parameters - conditions on force convergence and resultant force end value (zero) must be satisfied. Analysis showed that parameters for controller actions cannot be fixed and work successfully for MBSs with different number of DOF (Degrees of Freedom). Based on that, PID controller parameter range has been evaluated by Genetic Algorithm after repeated tests on systems of different types and number of DOF. Parameters choice and PID controller behavior were checked on models of engine timing drives (belt and chain drives with lashes) with several hundred DOF and simple model of Single Valve Train with just few DOF. Tests showed correct choice of PID parameters and stable iteration procedure regardless of DOF number and type of MBS. This paper focuses on determination of PID controller parameters by analyzing influence of MBS structure to procedure for reaching equilibrium state. Analysis is mainly focused on convergence and stability of the procedure.


2014 ◽  
Vol 487 ◽  
pp. 313-318
Author(s):  
Yuan Zhang ◽  
Jian Wang ◽  
Yan Song ◽  
Li Li Sun

The new type of three jaw docking mechanism is designed for use in orbiting spacecraft, the mathematical model is given and its working characteristics are analyzed. By establishing the mathematical model of the interaction of the parts under the different coordinate system, it is obtained that the corresponding kinematic characteristics; contact collision dynamics model is established by using the Hertz model theory, dynamic equation is established by Newton-Euler method, and simulation analysis are carried out by using the dynamics simulation software ADAMS, through the simulation analysis of three groups with different initial conditions, the results show that it achieve reliable grasp with good performance, it provides the lock claw curve in contact collision force and movement characteristics curve. These curves provide reference to improve the performance of docking mechanism.


1992 ◽  
Vol 114 (4) ◽  
pp. 571-579 ◽  
Author(s):  
W. C. Hsu ◽  
A. A. Shabana

This investigation is devoted to a discussion on the effect of the coupling between the longitudinal and transverse displacements of kinematically driven rotating beams. To this end, the inertia forces that act on a flexible body as the result of the finite rotation are categorized into two classes. These are the passive and active inertia forces. While the effect of the active inertia forces of kinematically driven systems is recognized in the absence of external disturbances and nonzero initial conditions, the passive inertia forces of such systems are not recognized in the case of zero initial conditions and in the absence of external excitations. Depending on the assumed displacement field, three classes of mechanical systems are defined in this paper. These are the active, partially active, and passive systems. The active system has a mathematical model in which both passive and active inertia forces are fully presented. In a partially active system, a part of the passive inertia forces and the active inertia forces appear in the mathematical model. The vibration of the kinematically driven passive system is governed by homogeneous equations which contain only the passive inertia forces. In the case of zero initial conditions and in the absence of external excitation, the response of the passive kinematically driven system is zero regardless of the value of the angular velocity. The effect of the inertia forces of the passive system appear as a time varying modification of the system parameters. It is shown in this investigation that a rotating beam model in which the axial deformation is neglected is a partially active or passive system. It is also demonstrated that the neglect of the effect of the longitudinal displacement has two significant effects. It decouples the modes of vibration and makes the form of the complementary solution independent of the sense of rotation. The behavior of the active, partially active, and passive systems when they are subjected to driving constraints (specified motion) is examined and it is shown that the response of the passive system converges to the partially active system if the effect of the initial conditions becomes dominant as compared to the effect of the active inertia forces of the partially active system.


A study is made of the linear theory of free vibrations of membranes in which, owing to the self-weight of the membrane, some sag is present in the static profile. The theory applies only to those membranes with relatively shallow profiles. However, because a major application of the theory relates to the use of certain types of cable networks to support the roofs of buildings of large span, and because such networks must be relatively flat if structural efficiency is to be achieved, the theory is of some practical importance. A detailed examination is made of the circular membrane and the rectangular membrane. It is found that the symmetric modes of vibration are heavily dependent on the value of a characteristic geometric and elastic parameter - a parameter which can vary by several orders of magnitude in the suspended membranes typical of those under consideration. In particular, when the parameter is very large the membrane may be considered inextensible. In a practical sense, this corresponds to a membrane of shallow, although appreciable, curvature. For certain intermediate values of the parameter, situations arise in which the natural frequency of a symmetric mode is identical to that of an antisymmetric mode. And when it is very small, the symmetric modes of the classical circular and rectangular membranes are recovered, although, in the case of the classical square membrane, the theory points to conclusions which could not have been drawn from classical membrane theory alone.


1978 ◽  
Vol 45 (4) ◽  
pp. 845-851
Author(s):  
H. Ainso

A general method is presented for solving shallow shell problems with finite boundaries and with an arbitrarily placed load that is uniformly distributed over a circular area of radius r0. A known solution for the distributed load on an unbounded shell is used to describe the load effects, and this particular solution is combined with Reissner’s general solution of the shallow shell equations in such a manner that all the boundary conditions are satisfied. Numerical results have been obtained for a shallow shell, clamped at the outer boundary and having a circular polar aperture free of tractions and support.


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