7,640 research outputs found
Semiconjugate Factorizations of Higher Order Linear Difference Equations in Rings
We study linear difference equations with variable coefficients in a ring
using a new nonlinear method. In a ring with identity, if the homogeneous part
of the linear equation has a solution in the unit group of the ring (i.e., a
unitary solution) then we show that the equation decomposes into two linear
equations of lower orders. This decomposition, known as a semiconjugate
factorization in the nonlinear theory, generalizes the classical operator
factorization in the linear context. Sequences of ratios of consecutive terms
of a unitary solution are used to obtain the semiconjugate factorization. Such
sequences, known as eigensequences are well-suited to variable coefficients;
for instance, they provide a natural context for the expression of the
classical Poincar\'{e}-Perron Theorem. We discuss some applications to linear
difference equations with periodic coefficients and also derive formulas for
the general solutions of linear functional recurrences satisfied by the
classical special functions such as the modified Bessel and Chebyshev.Comment: Application of nonlinear semiconjugate factorization theory to linear
difference equations with variable coefficients in rings; 29 pages,
containing the main theory and more than 8 examples worked out in detai
Asymptotic proximity to higher order nonlinear differential equations
Abstract
The existence of unbounded solutions and their asymptotic behavior is studied for higher order differential equations considered as perturbations of certain linear differential equations. In particular, the existence of solutions with polynomial-like or noninteger power-law asymptotic behavior is proved. These results give a relation between solutions to nonlinear and corresponding linear equations, which can be interpreted, roughly speaking, as an asymptotic proximity between the linear case and the nonlinear one. Our approach is based on the induction method, an iterative process and suitable estimates for solutions to the linear equation
The pullback attractors for the Higher-order Kirchhoff-type equation with strong linear damping
The paper investigates pullback the attractors for the Higher-order Kirchhoff-type equation with strong linear damping:.Firstly, we do priori estimation for the equations to obtain the existence and uniqueness of the solution inby some assumptions the Galerkin method. Then, we prove existence of the pullback attractorsin
Critical study of higher order numerical methods for solving the boundary-layer equations
A fourth order box method is presented for calculating numerical solutions to parabolic, partial differential equations in two variables or ordinary differential equations. The method, which is the natural extension of the second order box scheme to fourth order, was demonstrated with application to the incompressible, laminar and turbulent, boundary layer equations. The efficiency of the present method is compared with two point and three point higher order methods, namely, the Keller box scheme with Richardson extrapolation, the method of deferred corrections, a three point spline method, and a modified finite element method. For equivalent accuracy, numerical results show the present method to be more efficient than higher order methods for both laminar and turbulent flows
Application of the Finite Element Method to Rotary Wing Aeroelasticity
A finite element method for the spatial discretization of the dynamic equations of equilibrium governing rotary-wing aeroelastic problems is presented. Formulation of the finite element equations is based on weighted Galerkin residuals. This Galerkin finite element method reduces algebraic manipulative labor significantly, when compared to the application of the global Galerkin method in similar problems. The coupled flap-lag aeroelastic stability boundaries of hingeless helicopter rotor blades in hover are calculated. The linearized dynamic equations are reduced to the standard eigenvalue problem from which the aeroelastic stability boundaries are obtained. The convergence properties of the Galerkin finite element method are studied numerically by refining the discretization process. Results indicate that four or five elements suffice to capture the dynamics of the blade with the same accuracy as the global Galerkin method
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