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JOURNALS // Prikladnaya Mekhanika i Tekhnicheskaya Fizika // Archive

Prikl. Mekh. Tekh. Fiz., 2013 Volume 54, Issue 4, Pages 74–85 (Mi pmtf1159)

This article is cited in 13 papers

Nonlinear flutter of viscoelastic rectangular plates and cylindrical panels of a composite with a concentrated masses

B. Kh. Eshmatova, Kh. Eshmatova, D. A. Khodzhaevb

a University of Buffalo, New York, 14260-4400, USA
b Tashkent Institute of Irrigation and Reclamation, Tashkent, 100000, Uzbekistan

Abstract: The problem of flutter of viscoelastic rectangular plates and cylindrical panels with concentrated masses is studied in a geometrically nonlinear formulation. In the equation of motion of the plate and panel, the effect of concentrated masses is accounted for using the $\delta$-Dirac function. The problem is reduced to a system of nonlinear ordinary integrodifferential equations by using the Bubnov–Galerkin method. The resulting system with a weakly singular Koltunov–Rzhanitsyn kernel is solved by employing a numerical method based on quadrature formulas. The behavior of viscoelastic rectangular plates and cylindrical panels is studied and the critical flow velocities are determined for real composite materials over wide ranges of physicomechanical and geometrical parameters.

Keywords: Kirchhoff–Love hypothesis, composite materials, viscoelastic rectangular plate, viscoelastic cylindrical panel, concentrated mass, Bubnov–Galerkin method, nonlinear flutter.

UDC: 539.3

Received: 21.04.2009
Revised: 26.11.2012


 English version:
Journal of Applied Mechanics and Technical Physics, 2013, 54:4, 578–587

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