ON THE INFLUENCE OF BOUNDARY CONDITIONS ON THE DEPENDENCE AMPLITUDE-FREQUENCY OF NON-LINEAR FLUTTER TYPE OSCILLATIONS OF RECTANGULAR PLATE AT CRITICAL SPEED
Journal Title: Հայաստանի գիտությունների ազգային ակադեմիայի տեղեկագիր․ Մեխանիկա - Year 2016, Vol 69, Issue 4
Abstract
The problem of nonlinear oscillations of an isotropic rectangular plate in a supersonic gas flow is examined. The study was conducted taking into account both types of nonlinearities: wind (quadratic and cubic) and geometric (cubic). It is known that nonlinear dependence of the frequency on the amplitude of the oscillations of the plate in absence of flowing stream has a hard character, i.e. with increasing amplitude the frequency increases. In this paper it is established that the presence of flowing stream may cause both quantitative and qualitative changes of the character of noted monotonically increasing dependence. The influence of boundary conditions along the tangential directions of simply supported plate on the dependence amplitude-frequency of non-linear flutter type oscillations at critical speeds is investigated in this paper. It is shown that transmission from one type of examined dependence to another can be controlled as via the appropriate choice of both geometrical and physical parameters of aeroelastic system, as well as via the change of boundary conditions.
Authors and Affiliations
Rafayel Saghoyan
Maxwell equations for non-homogeneous media with periodic structure.
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THE STATE EQUATIONS FOR THE FIRST AND SECOND FUNDAMENTAL PROBLEMS OF ELASTODYNAMICS FOR A CRACKED MEDIUM.
In our work we will derive the state equations the first and second fundamental dynamical problems in the frame of linear elasticity. In the first fundamental dynamical problem we will consider an infinite medium that co...
On some wave effects in non-linear elastic micropolar media.
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The determination of fluid parameters in the neighbourhood of junction of wave fronts.
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On the modulative waves of anisotropic cylindrical shell which is situated in magnetic field.
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