2010
DOI: 10.1007/s10778-010-0328-y
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Flutter of a viscoelastic plate in a supersonic gas flow

Abstract: The flutter of a viscoelastic plate in a supersonic gas flow is studied. A technique and algorithm for numerical solution of nonlinear integro-differential equations with weakly singular kernels are elaborated. The critical flutter speed of viscoelastic plates is determined Keywords: viscoelasticity, supersonic flow, critical speed, nonlinear integro-differential equations with weakly singular kernels, flutter of plate Introduction. In studying elastic and viscoelastic plates in a gas flow, use is often made o… Show more

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Cited by 17 publications
(5 citation statements)
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“…The curves shown in the figure refer to the following parameter values α = 0.1 (1), α = 0.7 (2). At α = 0.1, a singular, rapidly damping oscillatory process occurs [20][21][22][23][24][25][26][27][28][29][30][31][32][33][34][35][36][37]. (L is the length of overhang) on dimensionless time  for various values of mass ratio β12.…”
Section: Numerical Resultsmentioning
confidence: 99%
“…The curves shown in the figure refer to the following parameter values α = 0.1 (1), α = 0.7 (2). At α = 0.1, a singular, rapidly damping oscillatory process occurs [20][21][22][23][24][25][26][27][28][29][30][31][32][33][34][35][36][37]. (L is the length of overhang) on dimensionless time  for various values of mass ratio β12.…”
Section: Numerical Resultsmentioning
confidence: 99%
“…Thus, according to the numerical method for the unknowns, a system of algebraic equations is obtained [21][22][23][24][25]. To solve the system, the Gauss method is used.…”
Section: Numerical Procedures Of Solving the Algebraic Systemmentioning
confidence: 99%
“…Equations of motion 7are integrated by a numerical method based on the use of quadrature formulas [18,19,23,[27][28][29][30][31]. Results of calculations are given in Tables 1 and 2 and are presented by the graphs in Figs.…”
Section: Formulation Of the Problem 21 Nonlinear Flutter Of Viscoelamentioning
confidence: 99%