On the Compressed Elastic Rod with Rotary Inertia on a Viscoelastic Foundation

نویسندگان

  • B. STANKOVIĆ
  • T. M. ATANACKOVIĆ
  • T. M. Atanacković
چکیده

1. Formulation of the Problem Consider an elastic rod simply supported at both ends. Let L be the length of the rod. We assume that the rod is loaded by an axial force P (t) that is a known function of time and has a fixed direction coinciding with the rod axis in the initial (undeformed) state. In this work we shall generalize our previous analysis [1] in two directions. First, we assume here that the 8 B. Stanković, T. M. Atanacković axial force is given by generalized functions and second we assume that the rod has a (not negligible) rotary inertia. Thus we allow for impulsive (described by a Dirac distribution) axial loading of the rod. The rod is positioned on a viscoelastic foundation described by a fractionl derivative type constitutive equation (see Figure 1). Figure 1. Coordinate system and load configuration Such foundations are important for vibration damping and have been recently analyzed in the context of the railpad in the railway track model (see [2] and [3] for the physical explanation of the model). The equilibrium equations of active and inertial forces are (see [4] p. 338) ∂H ∂S = ρ0 ∂2x ∂t2 − qx, ∂V ∂S = ρ0 ∂2y ∂t2 − qy, ∂M ∂S = −V cosθ+H sinθ− J ∂ 2θ ∂t2 , ∂x ∂S = cosθ, ∂y ∂S = sinθ, ∂θ ∂S = M EI , S ∈ (0, L) , t ≥ 0, (1) where x and y are coordinates of an arbitrary point on the rod axis, S is the arc length of the rod axis in the undeformed state so that S ∈ (0, L), t is the time, H and V are components of the force in an arbitrary cross–section of the rod along the x̄ and ȳ axes of a rectangular Cartesian coordinate system x̄ − B − ȳ, respectively, M is the bending moment, and qx, qy are the intensities of the distributed forces per unit length of the rod axis in the undeformed state, J is moment of inertia of a part of the rod of unit length, θ is the angle between the tangent to the rod axis and the x̄ axis, ρ0 is the line density of the rod, EI is the bending rigidity of the rod. For the rod On the compressed elastic rod with rotary inertia 9 shown in Figure 1 the boundary conditions are y (0, t) = 0, x (0, t) = 0; y (L, t) = 0, M (0, t) = 0, M (L, t) = 0; H (L, t) = −P , t ≥ 0. (2) Suppose that the rod is positioned on a viscoelastic foundation. We assume that the foundation is of the fractional derivative type. If the foundation is made of a fractional type viscoelastic material, then the force in the foundation Q and deformation Δ of the foundation (in our case Δ = y) are connected as Q+ τQQ = Ep ( y + τyy ) , (3) with 0 < β < 1. In (3) we used (·) to denote the β-th derivative of a function (·) taken in Riemann-Liouville form as (see [5], and [6]) g ≡ d β dtβ g (t) ≡ d dt 1 Γ (1− β) ∫ t 0 g (ξ) dξ (t− ξ) . (4) The dimension of the constants τy and τQ is [time] α . The constants Ep, τQ and τy in (3) are called the instantaneous modulus of the pad and the relaxation times, respectively. In Figure 1 the rheological model of the foundation is presented, as given in [7], for example. We assume that the following inequality, as a consequence of the second law of thermodynamics, is satisfied (see [9] and [8]) E > 0, τQ > 0, τy > τQ. (5) We assume that the pads are positioned under the rod so that qx = 0, qy = −bQ, (6) where b is a constant depending on the part of the rod’s width that is supported by pads. Note that in the case β = 1 the foundation becomes a standard viscoelastic solid. The trivial solution to the system (1),(2),(3) and (5) in which the rod axis is straight reads H (S, t) = −P , V 0 (S, t) = 0, M (S, t) = 0, x (S, t) = S, y (S, t) = 0, θ (S, t) = 0, Q (S, t) = 0. (7) Let the solution to (1),(2),(3) and (5) be written in the form H = H0 + ΔH, ...Q = Q0 + ΔQ, where ΔH, ...,ΔQ are perturbations, assumed to be 10 B. Stanković, T. M. Atanacković small. By substituting this in (7) and neglecting the higher order terms in the perturbations ΔH, ...,ΔQ, we obtain ∂ΔH ∂S = ρ0 ∂2Δx ∂t2 , ∂ΔV ∂S = ρ0 ∂2Δy ∂t2 + bΔQ, ∂ΔM ∂S = −ΔV − PΔθ− J ∂ 2Δθ ∂t2 , ∂Δx ∂S = 0, ∂Δy ∂S = Δθ, ∂Δθ ∂S = ΔM EI , ΔQ+ τQΔQ = Ep ( Δy + τyΔy ) , (8)

برای دانلود متن کامل این مقاله و بیش از 32 میلیون مقاله دیگر ابتدا ثبت نام کنید

ثبت نام

اگر عضو سایت هستید لطفا وارد حساب کاربری خود شوید

منابع مشابه

Low Velocity Impact on Relatively Thick Rectangular Plate under In-plane Loads Resting on Pasternak Elastic Foundation

This study deals with the elastic-plastic impact on moderately thick rectangular plate subjected to uniform in-plane compressive loads resting on the Pasternak elastic foundation. The proposed rectangular plates have two opposite edges simply-supported, while all possible combinations of free, simply-supported and clamped boundary conditions are applied to the other two edges. The dimensionless...

متن کامل

A Power Series Solution for Free Vibration of Variable Thickness Mindlin Circular Plates with Two-Directional Material Heterogeneity and Elastic Foundations

In the present paper, a semi-analytical solution is presented for free vibration analysis of circular plates with complex combinations of the geometric parameters, edge-conditions, material heterogeneity, and elastic foundation coefficients. The presented solution covers many engineering applications. The plate is assumed to have a variable thickness and made of a heterogeneous material whose p...

متن کامل

Nonlocal Vibration Behavior of a Viscoelastic SLGS Embedded on Visco- Pasternak Foundation Under Magnetic Field

This paper is concerned with the surface and small scale effects on transverse vibration of a viscoelastic single-layered graphene sheet (SLGS) subjected to an in-plane magnetic field. The SLGS is surrounded by an elastic medium which is simulated as Visco-Pasternak foundation. In order to investigate the small scale effects, the nonlocal elasticity theory is employed due to its simplicity and ...

متن کامل

Analytical Approach for Thermo-electro-mechanical Vibration of Piezoelectric Nanoplates Resting on Elastic Foundations based on Nonlocal Theory

In the present work, thermo-electro vibration of the piezoelectric nanoplates resting on the elastic foundations using nonlocal elasticity theory are considered. In-plane and transverse displacements of the nanoplate have been approximated by six different modified shear deformation plate theories considering transverse shear deformation effects and rotary inertia. Moreover, two new distributio...

متن کامل

Magneto-Electro-Thermo-Mechanical Response of a Multiferroic Doubly-Curved Nano-Shell

Free vibration of a simply-supported magneto-electro-elastic doubly-curved nano-shell is studied based on the first-order shear deformation theory in the presence of the rotary inertia effect. To model the electric and magnetic behaviors of the nano-shell, Gauss’s laws for electrostatics and magneto statics are used. By using Navier’s method, the partial differential equations of motion are red...

متن کامل

ذخیره در منابع من


  با ذخیره ی این منبع در منابع من، دسترسی به آن را برای استفاده های بعدی آسان تر کنید

برای دانلود متن کامل این مقاله و بیش از 32 میلیون مقاله دیگر ابتدا ثبت نام کنید

ثبت نام

اگر عضو سایت هستید لطفا وارد حساب کاربری خود شوید

عنوان ژورنال:

دوره   شماره 

صفحات  -

تاریخ انتشار 2006